ORGANIZATION LOGISTICS PLANNER'S GUIDE

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• Document Creation Date: November 17, 2016
• Document Release Date: March 17, 2000
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• Content Type: REPORT

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ORGANIZATION
LOGISTICS
PLANNER'S
GUIDE
Prepared by
OFFICE OF LOGISTICS
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ORGANIZATION
LOGISTICS PLANNER'S GUIDE
INTRODUCTION
1. The evolution of Organization materiel doctrine and the development of
different types of operations, together with the need for rapid and positive actions
to meet sudden requirements, cause the practice of Organization logistics to be
complex and ever-changing. The logistics officer has the assigned tasks of de-
veloping logistics support plans and performing those logistics functions neces-
sary to the implementation of the plans. Logistics planning, as applied in this
Guide, is that planning to accomplish:
a. Acquisition, storage, movement, maintenance, distribution, and disposi-
tion of materiel.
b. Acquisition or construction, maintenance, operation, and disposition of
facilities.
c. Acquisition or furnishing of logistic services.
d. Movement of personnel and baggage.
2. The purpose of this Guide is to provide the logistics officer with the basic
logistics planning data and formats for use in developing logistics support plans.
The Guide has been compiled to provide information, procedures, and references
in a form that will assist the user in his day-to-day planning tasks. For those
requirements which are beyond the scope of this Guide, a list of appropriate
references is included at Appendix VIII.
3. Users of this Guide are requested to submit recommendations for changes
or corrections to the Director of Logistics, Attention: Planning Staff.
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ORGANIZATION LOGISTICS PLANNER'S GUIDE
CONTENTS
INTRODUCTION
CHAPTER 1 Logistics Officer 1
CHAPTER 2 Logistical Planning 3
CHAPTER 3 Staff Writing 7
25X1 C CHAPTER 4 Planning Data 9
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tilli
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Section III ? Conex Data 13
Section IV ? Military Airlift Command ( MAC ) Tariff Instructions
and Rate Tables 14
Section V ? Aircraft Cargo Capabilities 39
APPENDIX I Format for a Logistical Estimate 117
APPENDIX II Format for a Logistical Plan ( or Annex to an Operational
Plan) 119
Tab A ? Logistics Planner's Checklist for the Preparation of a Logis-
tical Plan or Annex to an Operational Plan, Project or
Program 121
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CONTENTS (Continued)
APPENDIX IV Guide for Determining Administrative and Housekeeping
Support Requirements 129
TAB A ? Preparation of Administrative and Housekeeping Support
Requirements 131
APPENDIX V Format for a Standing Operating Procedure 133
APPENDIX VI Guide for the Preparation of a Staff Study 135
TAB A ? Format for a Staff Study 137
TAB B ? Checklist for a Staff Study 139
APPENDIX VII Checklist?Station or Base Development 141
APPENDIX VIII Standard Reference List 143
Prepared by the Office of Logistics Planning Staff
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CHAPTER 1
LOGISTICS OFFICER
1. Functions of the Logistics Officer
a. The logistics officer is a member of a group
organized to assist the chief in the execution of his
mission. He may function on an Organization staff
that deals solely with logistics matters; he may
function on an Organization support-type staff,
either individually or with other logistics or sup-
port officers; or he may function individually under
a chief of a division or station.
b. The chief and his logistics officers assist in
the accomplishment of the overall Organization
mission by providing for the successful accomplish-
ment of the missions of the support elements. The
logistics officer must utilize and help to administer
the resources of time, space, and materiel in the
accomplishment of the overall mission.
c. The proper use of these resources requires the
performance of the following basic functions:
( 1 ) Securing Information. This means more
than simply receiving and examining information.
It means going and getting it from any and all
possible sources. The information must be re-
liable, timely, and as complete as possible. In-
formation secured should also be made available
to any branch or division which needs it. Ac-
curate and complete information is required as
the basis for all action.
(2) Making Plans. Plans are based on infor-
mation and they result in decision. They must
reflect good judgment, for much of the effective-
ness of Organization projects will depend on the
quality of the planning. In order to be meaning-
ful, plans should answer the following questions:
What has to be done? Who does it? When
and where must it be done? Under what con-
ditions? How should it be done? After plans
are developed, programming and scheduling
follow.
(3) Coordinating. Within the scope of this
function, the logistics officer is required to secure
agreement to, understanding of, and assistance
in, the implementation of his task or project. He
will have to determine the need for coordination
and the people with whom to coordinate. He
will have to determine the method ( such as a
meeting or conference), and then actually ac-
complish the coordination. Effective coordina-
tion will promote cooperation and reduce friction
among those involved in the task or project.
(4) Making Decisions. The logistics officer
will be called upon to make many decisions in
carrying out the policies and directives of his
chief. These decisions must be based on the
best information available. As an example, a
logistics officer who is charged with developing
the table of equipment for a project must con-
sider carefully all factors, such as temperature,
climate, utilities, and physical characteristics of
people involved. He will normally make de-
cisions within the framework of established pol-
icy or recommend decisions to his chief as to the
specific materiel to be used. The logistics officer
usually will not be called upon to make command
or policy decisions, but when such decisions are
made by his chief, or higher authority, the logis-
tics officer must be loyal and precise in the ex-
ecution of his duties in support of these de-
cisions. If established policy or procedures are
conflicting or need changing, he should develop
and submit to his chief specific recommendations
for changes.
d. The logistics officer's specific duties will be
in the fields of supply, transportation, procurement,
real estate and construction, printing, and support
services. He may be called upon to operate as
a staff logistics officer or an operating logistics offi-
cer in performing his day-to-day work. When the
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requirements levied upon him are beyond his capa-
bilities, he should call upon the Office of Logistics
to assist him. In this respect, the Planning Staff,
Office of Logistics, is available to provide a wide
range of assistance within the field of Organization
logistics. This staff is the focal point for assistance
in the development of plans and requirements.
Direct contact with other staff elements of the
Office of Logistics should be effected during the
operational phase.
e. The logistics officer may be called upon to
perform duties both of a staff and of an operating
nature. Thus, he may be required to:
(1) Advise his chief on logistical matters and
keep him informed on the logistical status of the
Organization.
(2) Procure and maintain that logistics infor-
mation required in fulfilling his mission.
(3) Prepare logistics estimates, plans, and staff
studies.
(4) Prepare necessary documentation to ob-
tain supplies and materiel.
(5) Prepare budgetary data necessary for lo-
gistics purposes.
(6) Coordinate and monitor the activities of
his office with respect to logistics matters.
(7) Coordinate the utilization of materiel,
services, and facilities between the using and
supplying organizations.
(8) Coordinate the implemmtation of logis-
tics plans.
(9) Exercise supervision over such logistical
matters as his chief may desig aate.
f. The logistics officer may be assigned other
duties. The above list is neither detailed nor all-
inclusive. While his functions are basically cen-
tered around the fields of supp:ly, transportation,
procurement, real estate and construction, printing,
and support services, there are differences in the
scope of his activities at station. base, depot, di-
vision, and Headquarters levels.
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CHAPTER 2
LOGISTICAL PLANNING
1. Definitions
a. Planning is the systematic application of in-
telligence to a problem, the solution to which is
not immediately apparent.
b. A logistical plan is a document designed and
prepared to insure the availability of adequate re-
sources to support an operational plan.
c. The functional areas of logistics in this Or-
ganization include supply, transportation, procure-
ment, real estate and construction, printing, and
support services.
2. Logistical Estimate
a. Logistical planning must be carried out con-
currently with, or in some cases prior to, operational
planning. Coordinated logistical and operational
planning are indispensable to the successful attain-
ment of operational objectives.
b. The logistical estimate serves three broad
purposes:
(1) It will bring into focus all the logistical
implications of an operational plan.
(2) It will indicate whether the operation can
be supported adequately.
(3) It will indicate one or more logistical
courses of action to provide adequate support to
the operational plan.
c. All logistical plans should be based on logis-
tical estimates so that logistics planners can con-
fidently advise as to whether operations can be
supported.
d. A suggested format for a logistical estimate is
attached as Appendix I. It incorporates instruc-
tions concerning the processes involved in its use.
These processes are demanding in that they require
an accurate status of facilities, stocks, and person-
nel to determine logistical capabilities for com-
parison with requirements in deriving proper
courses of logistical action for support of opera-
tions.
3. Development of Logistical Plans
a. Based on the logistical estimate, logistical
plans should announce the decision of a headquar-
ters for logistics support. Logistical plans should,
where possible, provide for:
(1) Efficient use of transportation.
(2) Reduction in multiple handling of sup-
plies.
(3) Reduction in time between ordering and
receiving.
(4) Elimination, or reduction to a minimum,
of requirements that do not contribute directly
to the progress of operations.
(5) Maximum and efficient utilization of man-
power.
(6) Economy in use of supplies and equip-
ment.
(7) Elimination of nonessential and improb-
able contingency items.
(8) Establishment and maintenance of mini-
mum supply levels.
(9) Alternate means to provide support and
obtain flexibility.
b. In order to develop logistical plans, the fol-
lowing information is essential to the planner:
(1) He must be advised of the basic concept
of operations early in the planning phase. Lo-
gistical considerations often alter or even dictate
operational concepts.
(2) He must know force strengths and compo-
sition. Vehicles, weapons, transport replace-
ment and consumption materials, reserve stocks
and service requirements cannot be computed
without a reasonable idea of numbers to be sup-
ported and composition of the organization.
(3) He must know transportation require-
ments and capabilities. The logistical planner
must match these requirements against known
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capabilities to insure that materiel can be moved
in accordance with requirements. If reliable
data is unavailable, estimates must be made
based on available information. Transportation
planning data must include the following:
(a) Movement requirements for personnel
and supplies.
( b ) Number, types, and characteristics of
transport vehicles.
( c) Terminal capacities in both the loading
and unloading areas, as applicable.
( d) Condition of airports and seaports to
be used.
(4) The logistics planner must know the avail-
able sites for depots and service installations in
the loading and unloading area, as applicable.
Existing facilities should be used where feasible.
Factors which govern the location of these in-
stallations include the ability to support the
operation, accessibility to the existing transporta-
tion nets, and security conditions.
(5) The logistical planner must anticipate use
of Organization, military, and other U.S. source
labor and indigenous labor resources available.
In many instances, it may be necessary to depend
primarily on Organization personnel for labor
because of security conditions. Where possible,
other source labor should be used.
(6) A suggested format for the logistical plan
is attached as Appendix II. It incorporates in-
structions concerning the processes involved in
its use.
4. Determination of Logistical Materiel
Support Requirements
a. Planning. As a general rule, support require-
ments planning passes through three fundamental
phases: Estimation, Calculation, and Modification.
The first phase must be accomplished with few, if
any, tangible figures. Each successive step in plan-
ning is developed with more concrete and accurate
data than the preceding one until a firm list of
materiel is evolved.
(1) Estimation. The initial step in the de-
velopment of requirements often must be ac-
complished with little more than a brief state-
ment of the mission and concept of operation.
Logistics planners employ broad experience fac-
tors such as replacement and consumption data
and initial issue information. Factors represent-
ing the best available experience are used and
the planner should make only such changes as
later experience and backgrou rid dictate.
(2) Calculation. Calculation of support re-
quirements begins when estimates are received
from supported and supporting elements. Total
support requirements can be de rived from these
initial lists, which should be more accurate than
the estimates used to initiate planning. How-
ever, support estimates should be evaluated and
carefully scrutinized before acceptance. Calcu-
lation of requirements continues after the prepa-
ration of the initial support requirements. Factors
and other data used in the initial estimations are
discarded in favor of actual ( or adjusted) figures
extracted from the initial lists.
(3) Modification. Modifications, adaptations,
or alterations dictated by policy, by direction, or
by conditions peculiar to the area of operations
are applied in the third phase. Each revision
must be checked to make certain that all materiel
aspects have been considered and that the resul-
tant list is balanced.
b. Procedural Steps for the Determination of
Support Requirements. The following steps are
recommended as a guide for systematic support re-
quirement determination planning:
(1) Operational missions and objectives gen-
erate support requirements.
(2) Approved operational requirements form
the fundamental basis for determining support
requirements.
(3) A forecast of projected operational re-
quirements may be added directly or on a per-
centage basis to the initial approved operational
requirements.
( 4) Guidance must be provided from top
policy and planning staffs to lower echelons to
assist in requirement determinations.
(5) Support requirements, after determina-
tion and coordination, are sut milted to senior
echelon for approval.
(6) Upon approval, requirements are then
firmly established for basis of procurement, stor-
age, stockpile and distribution.
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(7) Requirements should be reviewed and re-
vised periodically as operational concepts are
changed.
5. Determination of Logistics Personnel
Requirements
a. The exact composition of the support orga-
nization depends upon certain variable factors
which the planner must analyze continuously to
provide adequate support. These are:
6. Standing Operating Procedures
(SOP)
a. General. A standing operating procedure
( SOP) is a set of instructions giving the methods
to be followed by a particular element for the per-
formance of those duties ( operational and admin-
istrative) which the senior member desires to make
routine. These instructions reduce the number and
length of directives that must be issued. The pur-
poses of the SOP are:
(1) To simplify the preparation and trans-
mission of directives.
(2) To facilitate and expedite actions, both
operational and administrative, and to minimize
confusion and errors.
b. Scope and Form.
( I ) Each subordinate element normally de-
velops appropriate and effective procedures con-
forming to those established by the senior ele-
ment. The SOP should be sufficiently complete
to advise new arrivals or newly attached per-
sonnel of the procedures followed within an or-
ganization. The SOP's are based upon directives
and policies of the next headquarters.
(2) The SOP's are published in a form most
effective for the type of organization. The form
utilized may be a single pamphlet or separate
pamphlets, each pertaining to a separate function.
Regardless of the form, the component parts
make up the unit SOP and are published by au-
thority of the senior representative. ( See Ap-
pendix V for recommended format for an SOP.)
7. Standard Planning References
Appendix VIII contains a recommended list of
standard references for logistics planning. It is
not all-inclusive, and users of this Guide should
consult indexes for additional references in research-
ing a staff problem.
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CHAPTER 3
STAFF WRITING
1. General
a. At all levels, the complexity of staff actions
normally requires the use of written directives, re-
ports, orders, and studies. The logistics staff officer
must, therefore, develop his ability to write accu-
rately, concisely and clearly.
b. A staff paper should satisfy the following
principles:
(1) ACCURACY
( a) Conform to facts.
(b) Be free from error.
( 2) BREVITY
Be accurate, concise and to the point.
(3) CLARITY
(a) Use simple sentences.
(b) Use correct grammatical construction.
(c) Use correct punctuation.
( d) Use only accepted abbreviations.
(e) Eliminate vague, meaningless or ambig-
uous phrases.
(f) Use topic sentences at start of each
paragraph.
( g) Should not sacrifice clarity for brevity.
( 4) COHERENCE
( a) Develop subject in logical sequence.
(b) Place related items ( ideas ) in orderly
sequence.
(c) Present subject logically.
(5) COMPLETENESS
( a) Present all logical alternatives.
(b) Indicate that views of others concerned
have been obtained and considered.
( c) Present draft orders, letters or instruc-
tions for placing recommendations into effect.
( 6) EMPHASIS
Stress the more significant points.
(7) OBJECTIVITY
( a) Maintain an impersonal viewpoint.
(b) Maintain an unbiased viewpoint.
( c) Analyze all aspects of the problem.
(8) UNITY
Adhere to the subject.
(9) SIMPLICITY
(a) Present facts simply and accurately so
as to require a minimum of effort when read-
ing the paper.
(b) Do not indulge in flowery prose which
detracts from the subject.
2. Staff Study
The staff study is a formal staff paper containing
a concise and accurate analysis and a recommended
solution of a problem. It is the result of research
and is the means of conveying to a superior a report
of the analysis made by the writer, together with
his conclusions and recommendations. It assists the
superior in making a decision. Appendix VI pre-
scribes the format of a staff study and a guide to
the content of each paragraph.
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SECTION HI
CONEX DATA
CARGO CAPACITY SHIPPING
CONEX WGHT. CUBE MAX. WGHT. CUBE
1. Type 1
9000
135
10,500
180
2. Type 2
9000
295
10,500
365
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SECTION IV
MILITARY AIRLIFT COMMAND (MAC)
TARIFF INSTRUCTIONS AND RATE TABLES
Rate tables have been divided into four tables,
as follows, to facilitate their use:
I Europe, North Africa, Northeast Cold
Countries to/from U.S.
II Mid-East between Athens and New Delhi
III Caribbean, South Atlantic, Central and
South America, South Africa to/from
U.S.
IV Alaska, Pacific Area, India to/from U.S.
To obtain any rate, consult the alphabetized In-
dex of Stations and ascertain the rate table in which
each station is located. The rate table indicated
will list the cost of movement of a passenger and
cargo.
Charges for carrying cargo are assessed by pound
or cube. The cubic foot measurement indicated
on each shipping requisition will be multiplied by
seven pounds and compared with the weight. The
larger of the two will be used for computing the
charges. No surcharge will be applied to com-
puted charges for weight catepry or valuation.
No package is considered as weighing less than
seven pounds because its cube i computed as at
least one cubic foot, i.e., one cubic foot equals
seven pounds.
Example: A cargo shipment of 640 pounds with
a cube of 180 is transported from Bangkok, Thai-
land to Dhahran, Saudi Arabia. 180 cube x 7 lbs.
(minimum weight per cube) equals 1,260 lbs.
Since 1,260 is in excess of 840, the charge will be
computed on the basis of a 1,26) lb. shipment:
Bangkok to New Delhi ( Table IV)
11.90
New Delhi to Dhahran ( Table 1[)
9.5?
1,260 times
21.4?
Total Charge
$269.64
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INDEX OF STATIONS
Geographical Place Name
Code
Airport
Rate
Table
Adak, Aleutian Islands
ADK
Adak NAS
IV
Adana, Turkey
ADA
Incirlik AB
II
Addis Ababa, Ethiopia
ADD
Haile Selassie I Airport
II
Amman, Jordan
AMM
Amman Airport
II
Anchorage, Alaska
EDF
Elmendorf AFB
IV
ANC
Anchorage Int'l Airport
IV
Ankara, Turkey
ESB
Esenboga Airport
Argentia, Newfoundland, Canada
YAR
Argentia NAS
Ascension Island
ASI
Wideawake Field
HI
Asmara, Eritrea
ASM
Yohannes IV Airport
II
Athens, Greece
ATH
Athens Central Airport
1,11II
Aviano, Italy
AVB
Aviano AB
Bangkok, Thailand
BKK
Don Muang Airport
IV
VSH
Qu Tapao Airfield
IV
Beirut, Lebanon
BEY
Beirut Int'l Airport
II
Berlin, Germany
THF
Templehof AB
Bermuda Island, BWI
BDA
Kindley AFB
I, III
Blenheim, New Zealand
BHE
Woodbourne AS
IV
Bogota, Colombia
DDO
El Dorado Int'l Airport
III
Brindisi, Italy
BDS
Brindisi AS
Cairo, Egypt
CAI
Cairo Int'l Airport
II
Calcutta, India
CCU
Dum Dum Airport
IV
Cam Ranh Bay, Vietnam
VCR
Cam Ranh Bay AB
IV
Charleston, SC
CHS
Charleston AFB/Muni
I, III, IV
Chateauroux, France
DEO
Deols Aux Airfield
Christchurch, New Zealand
CHC
Christchurch Int'l Airport
IV
Churchill, Canada
YYQ
Churchill Airport
Cocoa Beach, Florida
COF
Patrick AFB
I, III
Danang, Vietnam
DAD
Danang AB
IV
Dhahran, Saudi Arabia
DHA
Dhahran Airfield
II
Diyarbakir, Turkey
DIY
Diyarbakir AS
II
Dover, Delaware
DOV
Dover AFB
I, III, IV
Eleuthera Island, Bahama Islands
ELH
Eleuthera Aux AFB
HI
Eniwetok Atoll, Marshall Islands
ENT
Eniwetok AB
IV
Fairbanks, Alaska
EIL
Eielson AFB
IV
FAI
Fairbanks Int'l Airport
IV
Fernando De Noronha, Brazil
FDN
Fernando De Noronha Airport
III
Frankfurt, Germany
FRF
Rhein-Main AB
Goose Bay, Labrador Canada
YYR
Goose AB
Grand Bahama Island, Bahama Islands
GBI
Grand Bahama Aux AFB
III
Grand Turk Island, BWI
GDT
Grand Turk Aux AFB
III
Guam, Mariana Islands
UAM
Andersen AFB
IV
Guantanamo Bay, Cuba
GAO
Leeward Point Airport
III
Honolulu, Hawaii
HNL
Honolulu Int'l Airport
IV
HIK
Hickam AFB
IV
Iraklion, Crete
VWH
Iraklion AS
II
Istanbul, Turkey
IST
Yesilkoy Airport
II
Iwo Jima, Volcano Islands
IWO
Iwo Jima AB
IV
Izmir, Turkey
IGL
Cigli AB
II
Jidda, Saudi Arabia
JID
Jidda Airfield
II
Johannesburg, South Africa
JNB
Jan Smuts Airport
III
Johnston Island
JON
Johnston Island AB
IV
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IP
Geographical Place Name
Code
Airport
Rate
Table
Karachi, Pakistan
KHI
Karachi Int'l Airport
Keflavik, Iceland
KEF
Keflavik Airport
Khartoum, Sudan
KRT
Khartoum Airdrome
II
Kinshasa, Republic of Congo
FIH
Kinshasa Airport
HI
Kwajalein Island, Marshall Islands
KWA
Kwajalein PMRF
IV
Lahore, Pakistan
LHE
Lahore Airport
Lajes, Azores
LGS
Lajes Field
Lisbon, Portugal
LIS
Lisbon Airport
London, England
LON
Croydon Aerodrome
Los Angeles, California
LAX
Los Angeles Int'l Airport
IV
Madrid, Spain
TOJ
Torrej on AB
Manila, Philippine Islands
CRK
Clark AB
IV
MNL
Manila Int'l Airport
IV
NOP
Mactan Airfield
IV
CUA
Cubi Point NAS
IV
Marcus Island
MUS
Marcus
IV
Mayaguana, Bahama Islands
MYG
Mayaguana Aux AFB
III
McGuire AFB, Wrightstown, NJ
WRI
McGuire AFB
I, III, IV
Midway Island, Pacific
MDY
Midway NAS
IV
Mildenhall, England
MHZ
RAF Mildenhall
Moron, Spain
OZP
Moron AB
Nandi, Fiji Islands
NAN
Nandi
IV
Naples, Italy
NAP
Capadichino Airport
New Delhi, India
NDH
Palam Airport
II, IV
New York, NY
JFK
John F. Kennedy Int'l Airport
Nicosia, Cyprus
'CO
Nicosia Airport
Norfolk NAS, Va
NGU
Norfolk NAS
I, III
Okinawa, Ryukyu Islands
DNA
Kadena AB
IV
AHA
Naha AB
IV
Oslo, Norway
FBU
Fornebu Airport
Pago Pago, American Samoa
PPG
Pago Pago Airport
IV
Panama, Canal Zone
HOW
Howard AFB
Paramaribo, Surinam
ZAN
Zandery Airport
III
Paris, France
ORY
Orly Airport
Peshawar, West Pakistan
PEW
Peshawar AS
Pisa, Italy
PSA
San Giusto Airport
Port of Spain, Trinidad
POS
Piarco Airport
Prestwick, Scotland
PIK
MOA Prestwick Airfield
Quonset Point, Rhode Island
NCO
Quonset Point NAS
Ramey AFB, Puerto Rico
BQN
Ramey AFB
Recife, Brazil
REC
Ibura Airport
III
Richmond, Australia
RCM
RAAF Airdrome
rv
Rio De Janeiro, Brazil
RIO
Galeao Airport
III
Roosevelt Roads, Puerto Rico
NRR
Roosevelt Roads NAS
III
Rota, Spain
RTA
Rota NAS
Saigon, Vietnam
SGN
Tan Son Nhut Airfield
Iv
HOA
Bien Hoa Airfield
rv
St. Johns, Antigua Island, BWI
SJH
Coolidge Airport
III
St. Lucia Island, Windward Islands
SLU
Vigie Airport
Samsun, Turkey
SSX
Samsun AS
San Antonio, Texas
SKF
Kelly AFB
IV
San Bernardino, California
SBD
Norton AFB
IV
San Francisco, California
SFO
San Francisco Intl Airport
IV
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Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
Geographical Place Name
Code
Airport
Rate
Table
San Isidro, Santo Domingo
SSO
San Isidro AB
III
San Salvador Island, Bahama Islands
SSD
San Salvador Aux AFB
III
Sao Paulo, Brazil
CUK
Cumbica Airport
III
Seattle, Washington
SEA
Seattle-Tacoma Int'l Airport
IV
TCM
McChord AFB
IV
Seoul, Korea
SEL
Kimpo AB
IV
Shemya, Aleutian Islands, Alaska
SYA
Shemya AFS
IV
Soesterberg, Netherlands
SSS
Camp New Amsterdam AB
Sondrestrom, Greenland
SFJ
Sondrestrom AB
Soudha Bay, Crete
SOC
Soudha AS
II
Stephenville, Newfoundland, Canada
YJT
Ernest Harmon AFB
Taipei, Taiwan
TPE
Taipei Int'l Airport
IV
Teheran, Iran
THR
Mehrabad Airport
II
Tel Aviv, Israel
TLV
Lod Airport
II
Thule, Greenland
THU
Thule AB
Tokyo, Japan
TAW
Tachikawa AB
IV
TYO
Tokyo Int'l Airport
IV
Trabzon, Turkey
TZX
Trabzon AS
II
Travis AFB, Fairfield, California
SUU
Travis AFB
IV
Tripoli, Libya
TIP
Wheelus Field
Wake Island, Pacific
AWK
Wake Island AS
IV
Winnipeg, Manitoba, Canada
YWG
Stevenson Field
Yalova, Turkey
TYA
Yalova Airport
II
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17
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE I-PASSENGER AND CARGO RATES
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Argentia
Athens
Aviano
Berlin
Bermuda
Brindisi
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Athens
Greece
89
16.6
Aviano
Italy
75
14.0
19
3.6
Berlin
Germany
-
-
-
-
-
-
Bermuda
British West Indies
50
11.9
120
22.3
106
19.7
-
-
Brindisi
Italy
80
14.9
9
1.7
10
1.9
-
-
111
20.(3
Chateauroux
France
55
10.2
34
6.4
20
3.8
-
-
86
15.9
25
4.7
Churchill
Canada
84
22.7
169
35.7
155
33.1
-
-
70
17.3
160
34.0
Frankfurt
Germany
64
11.8
28
5.4
9
1.8
-
-
94
17.4
20
3.7
Goose Bay
Canada
14
3.8
102
19.0
88
16.4
-
-
48
11..4
93
17.3
Keflavik
Iceland
41
11.2
63
11.8
44
8.2
-
-
87
21.9
55
10.1
Lajes
Azores
34
6.2
71
13.2
57
10.6
-
-
49
9.3
62
11.5
Lisbon
Portugal
62
11.6
43
8.2
29
5.5
-
-
93
17.3
34
6.5
Madrid
Spain
55
10.2
36
6.7
22
4.1
-
-
86
15.9
27
5.1
Mildenhall
England
55
10.2
38
7.3
19
3.7
-
-
86
15.4
29
5.6
Moron
Spain
62
11.5
42
8.0
28
5.4
-
-
93
172
33
6.3
Naples
Italy
75
14.1
14
2.6
15
2.9
-
-
106
19.3
5
1.0
Oslo
Norway
79
14.6
43
8.2
24
4.6
-
-
109
202
34
6.5
Paris
France
56
10.4
36
6.8
17
.3.2
-
-
87
16.1
27
5.1
Pisa
Italy
71
13.2
20
3.8
5
1.0
-
-
102
18.9
11
2.1
Prestwick
Scotland
61
11.3
44
8.4
26
4.8
-
-
92
16.9
36
6.8
18 Approved For Release 2000/05/31 : CIRiEREf5-00988R000700010001-4
ail
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE I-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Argentia
Athens
Aviano
Berlin
Bermuda
Brindisi
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Rota
Spain
63
11.7
44
8.3
30
5.6
-
-
94
17.4
35
6.6
Soesterberg
Netherlands
61
11.4
34
6.5
15
2.9
-
-
92
17.1
25
4.8
Sondrestrom
Greenland
43
11.8
129
24.0
115
21.4
-
-
77
19.3
120
22.3
Stephenville
Canada
6
1.6
95
17.6
81
15.0
-
-
42
9.8
86
15.9
Thule
Greenland
60
16.1
144
26.7
130
24.1
-
-
93
23.7
135
25.0
Tripoli
Libya
86
16.1
21
4.0
28
5.4
-
-
117
21.8
18
3.5
Winnipeg
Canada
64
17.4
149
30.4
135
27.8
-
-
50
12.0
140
28.7
USAPOE
East Coast
32
8.6
117
21.7
103
19.1
98
18.1
18
3.3
108
20.0
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE II JOINS THIS TABLE AT ATHENS.
RATE TABLE III JOINS THIS TABLE AT USAPOE, EAST COAST.
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Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE I-PASSENGER AND CARGO RATES (Cont'd)
Passenger Fares stated in dollars, Cargo Rates stated in cents per pound.
Between
And
Chateauroux
Churchill
Frankfurt
Goose Bay
Keflavik
Lajes
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cg n
Fax
Cgo
Churchill
Canada
135
29.3
Frankfurt
Germany
11
2.0
143
30.9
Goose Bay
Canada
68
12.6
82
22.1
77
14.2
Keflavik
Iceland
34
6.3
121
32.6
35
6.4
53
14.3
Lajes
Azores
37
6.8
108
24.4
45
8.4
47
8.6
61
16.6
Lisbon
Portugal
22
4.3
142
30.7
34
6.4
75
14.0
55
10.3
44
8.2
Madrid
Spain
14
2.6
135
29.3
25
4.6
68
12.6
48
8.9
37
6.8
Mildenhall
England
9
1.6
135
29.3
9
1.8
68
12.6
25
4.7
37
6.8
Moron
Spain
22
4.1
142
30.6
33
6.2
75
13.9
55
10.2
44
8.1
Naples
Italy
20
3.9
155
33.2
25
4.7
88
16.5
54
10.2
57
10.7
Oslo
Norway
26
4.9
158
33.7
15
2.8
92
17.0
50
9.2
61
11.3
Paris
France
4
.8
136
29.5
7
1.3
69
12.8
31
5.8
38
7.0
Pisa
Italy
16
3.0
151
32.3
15
2.8
84
15.6
50
9.3
53
9.8
Prestwick
Scotland
15
2.7
134
29.2
15
2.8
68
12.6
19
3.6
48
7.9
Rota
Spain
23
4.4
143
30.8
33
6.1
76
14.1
56
10.4
45
8.3
Soesterberg
Netherlands
11
2.1
141
30.5
6
1.1
74
13.8
31
5.9
43
8.0
Sondrestrom
Greenland
95
17.6
111
30.1
104
19.2
29
7.9
82
22.2
77
18.0
Stephenville
Canada
61
11.2
76
20.5
69
12.8
8
2.3
45
12.3
39
7.2
Thule
Greenland
110
20.3
127
34.4
118
21.9
53
14.3
98
26.6
88
16.3
Tripoli
Libya
31
5.9
166
35.2
38
7.2
100
18.6
66
12.4
68
12.7
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UN
NM
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE I?PASSENGER AND CARGO RATES (Cont'd)
Passenger Fares stated in dollars, Cargo Rates stated in cents per pound.
Between
And
Chateauroux
Churchill
Frankfurt
Goose Bay
Keflavik
Lajes
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Winnipeg
Canada
115
24.0
20
5.3
123
25.6
62
16.8
101
27.3
88
19.1
USAPOE
East Coast
83
15.3
52
14.0
91
16.9
30
8.1
69
18.6
56
10.4
Passenger Rates?Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE II JOINS THIS TABLE AT ATHENS.
RATE TABLE III JOINS THIS TABLE AT USAPOE, EAST COAST.
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Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE I-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Lisbon
Madrid
Mildenhall
Moron
Naples
Oslo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
ego
Pax
Cgo
Madrid
Spain
7
1.3
Mildenhall
England
32
6.0
23
4.3
Moron
Spain
14
2.7
7
1.3
31
5.9
Naples
Italy
29
5.5
22
4.1
30
5.7
28
5.4
Oslo
Norway
48
9.2
40
7.4
26
4.7
47
9.0
39
7.5
Paris
France
27
5.0
18
3.4
7
1.3
26
4.9
25
4.7
22
4.2
Pisa
Italy
24
4.5
16
3.1
25
4.7
23
4.4
16
Si.29
5.6
Prestwick
Scotland
36
6.7
29
5.3
6
1.1
37
7.0
36
6.E1
30
5.6
Rota
Spain
15
r
2.9
8
1.5
31
5.8
2
.6
30
5.6
49
9.3
Soesterberg
Netherlands
34
6.4
25
4.7
6
1.2
33
6.2
30
51:
20
3.9
Sondrestrom
Greenland
102
19.0
95
17.6
95
17.6
102
18.9
115
211
119
22.0
Stephenville
Canada
68
12.6
61
11.2
61
11.2
68
12.5
81
15.1
84
15.6
Thule
Greenland
117
21.7
110
20.3
110
20.3
117
21.6
130
24.2
133
24.7
Tripoli
Libya
41
7.8
34
6.4
41
7.7
40
7.7
13
2.5
52
9.9
Winnipeg
Canada
122
25.4
115
24.0
115
24.0
122
25.3
135
27.9
138
28.4
USAPOE
East Coast
90
16.7
83
15.3
83
15.3
90
16.6
103
19.2
106
19.7
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. Excess.
RATE TABLE II JOINS THIS TABLE AT ATHENS.
RATE TABLE III JOINS THIS TABLE AT USAPOE, EAST COAST.
22 Approved For Release 2000/05/31 : CiotalM85-00988R000700010001-4
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE I-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Paris
Pisa
Prestwick
Rota
Soesterberg
Sondrestrom
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pisa
Italy
20
3.8
g
Prestwick
Scotland
13
2.4
31
5.8
Rota
Spain
27
5.1
24
4.6
38
7.3
Soesterberg
Netherlands
7
1.3
21
3.9
12
2.3
34
6.5
Sondrestrom
Greenland
96
17.8
111
20.6
95
17.5
103
19.1
101
18.8
Stephenville
Canada
62
11.4
77
14.2
60
11.2
69
12.7
67
12.4
38
10.2
Thule
Greenland
111
20.5
126
23.3
110
20.3
118
21.8
116
21.5
19
5.0
Tripoli
Libya
35
6.7
29
5.5
47
8.9
42
7.9
42
8.1
126
23.5
Winnipeg
Canada
116
24.2
131
27.0
114
23.9
123
25.5
121
25.2
92
24.8
USAPOE
East Coast
84
15.5
99
18.3
82
15.2
91
16.8
89
16.5
59
16.0
Between
And
Stephenville
Thule
Tripoli
Winnipeg
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Thule
Greenland
54
14.6
Tripoli
Libya
92
17.1
141
26.2
Winnipeg
Canada
56
15.3
108
29.1
146
29.9
USAPOE
East Coast
24
6.5
75
20.4
114
21.2
32
8.7
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE II JOINS THIS TABLE AT ATHENS.
RATE TABLE III JOINS THIS TABLE AT USAPOE, EAST COAST.
Approved For Release 2000/05/31 : CIA-M8tg00988R000700010001-4 23
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE II-PASSENGER AND CARGO RATES
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Adana
Addis Ababa
Amman
Ankara
Asmara
Athens
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
ego
Pax
Cgo
Addis Ababa, Ethiopia
35
10.8
Amman, Jordan
7
2.3
28
8.8
Ankara, Turkey
6
2.0
41
12.8
14
4.3
Asmara, Eritrea
28
8.8
7
2.3
21
6.5
35
10.8
Athens, Greece
13
3.9
34
10.6
15
4.7
9
2.9
28
8.0
Beirut, Lebanon
5
1.6
31
9.5
2
.7
12
3.6
23
7.2
13
4.0
Cairo, Egypt
11
3.3
24
7.5
5
1.7
17
5.3
18
5.E,
10
3.1
Dhahran, Saudi Arabia
23
7.2
46
14.3
17
5.3
28
8.5
39
12.0
31
9.6
Diyarbakir, Turkey
5
1.5
41
12.6
12
3.8
7
2.3
33
10.2
18
5.4
Iraklion, Crete
14
4.2
31
9.5
16
4.8
11
3.3
24
7.1.
3
1.1
Istanbul, Turkey
9
2.8
39
12.1
16
5.0
4
1.2
33
10.1
7
2.0
Izmir, Turkey
9
2.8
35
10.9
14
4.4
6
1.9
29
8.0
4
1.1
Jidda, Saudi Arabia
21
6.4
15
4.6
14
4.2
27
8.5
8
2.2.
20
6.3
Karachi, Pakistan
34
10.6
65
20.0
36
11.1
37
11.4
57
17.7
47
14.5
Khartoum, Sudan
27
8.5
8
2.4
22
6.8
34
10.4
8
2.2
27
8.2
Lahore, Pakistan
45
14.0
76
23.5
47
14.6
48
14.8
69
21.2
58
17.9
New Delhi, India
46
14.3
77
23.8
48
14.9
49
15.1
70
21.E
59
18.2
Nicosia, Cyprus
3
1.1
32
9.7
5
1.5
10
3.1
25
7.7
10
3.2
Peshawar, Pakistan
50
15.4
80
24.9
52
15.9
52
16.2
73
22.6
62
19.1
Samsun, Turkey
6
1.7
41
12.6
13
4.0
4
1.2
34
10.1
13
4.1
Soudha Bay, Crete
14
4.4
32
9.8
16
5.1
12
3.6
25
7.8
3
.9
Teheran, Iran
14
4.4
54
16.6
24
7.6
17
5.1
46
14.1
27
8.3
Tel Aviv, Israel
8
2.3
-
-
-
-
14
4.3
-
-
13
4.1
Trabzon, Turkey
6
1.8
41
12.7
13
4.1
7
2.2
34
10.6
16
5.1
Yalova, Turkey
8
2.6
40
123
16
4.8
3
1.0
33
10.3
7
2.2
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE I JOINS THIS TABLE AT ATHENS.
RATE TABLE IV JOINS THIS TABLE AT NEW DELHI.
24 Approved For Release 2000/05/31 : C1RALP195-00988R000700010001-4
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE II-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Beirut
Cairo
Dhahran
Diyarbakir
Iraklion
Istanbul
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Cairo, Egypt
7
2.2
Dhahran, Saudi Arabia
18
5.6
21
6.5
Diyarbakir, Turkey
10
3.1
17
5.2
20
6.2
Iraklion, Crete
13
4.1
7
2.0
28
8.5
18
5.7
Istanbul, Turkey
14
4.4
15
4.6
32
9.7
11
3.5
8
2.6
Izmir, Turkey
12
3.7
11
3.4
30
9.4
14
4.3
4
1.3
4
1.3
Jidda, Saudi Arabia
16
4.9
10
3.2
31
9.7
26
8.0
6
1.8
25
7.8
Karachi, Pakistan
37
11.4
40
12.2
19
5.8
29
9.1
46
14.3
41
12.6
Khartoum, Sudan
24
7.3
17
5.1
38
11.6
33
10.3
23
7.2
32
9.8
Lahore, Pakistan
48
14.9
51
15.7
30
9.2
41
12.5
57
17.7
52
16.0
New Delhi, India
49
15.2
62
16.0
31
9.5
41
12.8
58
18.0
53
16.3
Nicosia, Cyprus
3
.8
7
2.3
21
6.4
8
2.6
11
3.3
13
3.9
Peshawar, Pakistan
53
16.2
55
17.1
34
10.6
45
13.9
62
19.1
56
17.4
Samsun, Turkey
11
3.3
16
5.1
28
8.5
7
2.3
14
4.4
8
2.4
Soudha Bay, Crete
14
4.4
7
2.3
28
8.8
19
5.9
2
.5
9
2.9
Teheran, Iran
22
6.9
30
9.1
11
3.4
9
2.9
36
11.0
21
6.4
Tel Aviv, Israel
-
-
-
-
-
-
12
3.8
-
-
17
5.1
Trabzon, Turkey
11
3.4
17
5.2
24
7.5
4
1.3
18
5.4
11
3.4
Yalova, Turkey
13
4.1
15
4.8
31
9.5
11
3.3
9
2.8
2
.5
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE I JOINS THIS TABLE AT ATHENS.
RATE TABLE IV JOINS THIS TABLE AT NEW DELHI.
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Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE 1I-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Izmir
Jidda
Karachi
Khartoum
Lahore
New Delhi
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Jidda, Saudi Arabia
21
6.5
Karachi, Pakistan
43
13.4
50
15.4
Khartoum, Sudan
28
8.5
15
4.7
56
17.4
Lahore, Pakistan
55
16.9
61
18.9
11
3.5
67
20.8
New Delhi, India
66
17.2
62
19.2
12
3.8
68
21.1
23
7.2
Nicosia, Cyprus
9
2.9
18
5.4
38
11.6
24
7.4
49
15.:1
50
15.4
Peshawar, Pakistan
59
18.2
66
20.3
16
4.8
72
22.2
4
1.4
28
8.6
Samsun, Turkey
10
3.1
27
8.2
37
11.4
33
10.2
48
14.8
49
15.1
Soudha Bay, Crete
5
1.6
18
5.4
47
14.5
24
7.4
58
18.0
59
18.3
Teheran, Iran
23
7.2
42
13.0
20
6.2
46
14.3
31
9.'T
32
10.0
Tel Aviv, Israel
14
4.2
-
-
42
12.9
-
-
53
16.4
54
16.7
Trabzon, Turkey
13
4.1
27
8.3
33
10.3
33
10.3
45
13.8
46
14.1
Yalova, Turkey
5
1.4
26
7.9
40
12.4
32
9.9
51
15.8
52
16.1
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE I JOINS THIS TABLE AT ATHENS.
RATE TABLE IV JOINS THIS TABLE AT NEW DELHI.
26 Approved For Release 2000/05/31 : CVeREF5-00988R000700010001-4
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE II?PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Nicosia
Peshawar
Samsun
Soudha Bay
Teheran
Tel Aviv
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Peshawar, Pakistan
53
16.5
Samsun, Turkey
9
2.8
62
16.2
Soudha Bay, Crete
12
3.6
63
19.4
15
4.7
Teheran, Iran
18
5.4
36
11.0
17
5.1
36
11.3
Tel Aviv, Israel
4
1.3
57
17.7
13
4.1
16
4.9
22
6.7
Trabzon, Turkey
9
2.9
49
15.2
3
1.0
18
5.7
13
4.1
14
4.2
Yalova, Turkey
12
3.6
56
17.2
7
2.2
10
3.0
20
6.2
16
4.9
Between
And
Trabzon
Pax
Cgo
Yalova, Turkey
10
3.2
Passenger Rates?Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE I JOINS THIS TABLE AT ATHENS.
RATE TABLE IV JOINS THIS TABLE AT NEW DELHI.
Approved For Release 2000/05/31 : CIA-ROM70988R000700010001-4 27
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE III-PASSENGER AND CARGO RATES
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Antigua
Ascension
Island
Bermuda
Bogota
Eleuthera
Island
Fernando De
Noronha
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Ascension
Island
87
28.2
Bermuda
British West Indies
-
-
-
-
Bogota
Colombia
41
10.8
113
30.8
-
-
Eleuthera
Bahamas
25
8.1
109
35.4
-
-
50
13.7
Fernando De Noronha
Brazil
64
21.0
38
12.2
-
-
91
23.6
86
28.1.
Grand Bahama Island
Bahama Islands
28
9.2
112
36.5
-
-
53
14.8
3
1.1
87
28.3
Grand Turk Island
Bahama Islands
16
5.3
100
32.5
-
-
41
10.9
9
2.8
78
25.3
Guantanamo Bay
Cuba
22
6.0
106
33.3
-
-
28
7.0
31
8.9
83
24.8
Johannesburg
South Africa
155
60.5
82
26.6
-
-
196
60.0
190
62.1)
119
38.8
Kinshasa
Republic of Congo
131
42.7
45
14.5
-
-
158
47.9
153
49.9
82
26.7
Mayaguana
Bahama Islands
19
6.2
103
33.5
-
-
44
11.0
6
1.9
80
26.2
Panama
Canal Zone
30
8.3
10$
28.2
43
10.8
10
2.6
39
11.2
81
21.0
Paramaribo
Surinam
24
7.3
63
18.0
-
-
51
12.8
45
12.6
41
13.3
Port of Spain
Trinidad
11
3.6
75
24.6
-
-
38
9.7
33
9.5
53
16.4
Ramey AFB
Puerto Rico
8
2.6
92
29.9
20
5.1
33
8.2
17
5.5
69
22.6
Recife
Brazil
57
18.5
30
9.7
-
-
84
23.6
78
23.4
8
2.5
Rio De Janeiro
Brazil
66
17.9
54
16.7
-
-
93
23.4
87
23.2
32
8.5
Roosevelt Roads
Puerto Rico
7
2.2
93
30.4
-
-
35
8.8
20
6.'1
71
22.3
St. Lucia Island
Windward Islands
5
1.6
82
26.6
-
-
46
12.3
30
9.7
59
18.5
San Isidro
Santo Domingo
12
3.5
96
30.8
-
-
36
9.1
15
4.7
73
23.5
28 Approved For Release 2000/05/31 : CA3EW5-00988R000700010001-4
to'
Nog
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE III?PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Antigua
Ascension
Island
Bermuda
Bogota
Eleuthera
Island
Fernando De
Noronha
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
San Juan
Puerto Rico
6
2.0
93
30.2
?
?
35
8.7
19
6.1
71
23.0
San Salvador
Bahama Islands
22
7.1
106
34.4
?
?
47
12.8
3
1.0
83
25.0
Sao Paulo
Brazil
71
19.2
59
18.9
?
?
98
24.7
92
24.5
37
9.8
USAPOE
East Coast
36
11.6
119
38.9
?
?
49
12.4
11
3.5
97
31.6
Passenger Rates?Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE I JOINS THIS TABLE AT USAPOE, EAST COAST.
Approved For Release 2000/05/31 : CIA-F4DP8540988R000700010001-4 29
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE III-PASSENGER AND CARGO RATES (Cont'41)
Passenger fares stated in dollars; Cargo rates stated in cents per pound.
Between
And
Grand Ba-
hams Island
Grand Turk
Island
Guantanamo
Bay
Johannes-
burg
Kinshasa
Mayaguana
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Grand Turk Island
Bahama Islands
12
3.9
Guantanamo Bay
Cuba
28
7.8
22
6.1
Johannesburg
South Africa
194
63.1
181
57.0
187
57.7
Kinshasa
Republic of Congo
156
48.8
144
44.9
150
45.6
37
12.1
Mayaguana
Bahama Islands
9
3.0
3
.9
25
7.0
184
57.9
147
45.8
Panama
Canal Zone
42
12.3
30
8.4
18
4.5
186
57.4
148
45.3
33
9.3
Paramaribo
Surinam
48
13.7
36
9.8
42
10.5
145
47.2
108
35.L
39
10.7
Port of Spain
Trinidad
36
10.6
24
6.7
30
7.5
157
60.3
120
38.1
27
7.6
Ramey AFB
Puerto Rico
20
6.6
8
2.7
14
3.4
173
54.3
136
44.4
11
2.8
Recife
Brazil
82
26.7
70
20.6
74
21.2
112
36.3
74
24.!!
72
21.5
Rio De Janeiro
Brazil
90
24.3
78
20.4
84
21.2
136
42.3
98
30.2
81
21.3
Roosevelt Roads
Puerto Rico
22
7.2
10
3.3
16
4.0
175
66.1
138
44.0
13
4.2
St. Lucia
Windward Islands
33
10.8
21
6.8
27
7.5
163
52.3
126
40.2
24
7.7
San Isidro
Santo Domingo
18
5.8
6
1.9
17
4.4
177
57.4
140
45.1;
9
2.8
San Juan
Puerto Rico
22
7.2
10
3.2
16
3.9
175
56.9
137
44.3
13
4.1
San Salvador
Bahama Islands
6
2.1
6
1.9
28
8.0
187
61.0
150
46.1'
3
1.0
Sao Paulo
Brazil
96
25.6
92
23.8
89
22.5
141
43.6
103
31.11
86
22.6
USAPOE
East Coast
7
2.4
19
6.3
21
5.4
201
65.5
164
53.9
17
5.4
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE I JOINS THIS TABLE AT USAPOE, EAST COAST.
141.
30 Approved For Release 2000/05/31 : CAWLPP5-00988R000700010001-4
mai
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE III-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Panama
Paramaribo
Port of
Spain
Ramey
AFB
Recife
Rio De
Janeiro
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Paramaribo
Surinam
41
10.2
Port of Spain
Trinidad
28
7.1
12
3.1
Ramey AFB
Puerto Rico
22
5.7
28
7.1
16
5.3
Recife
Brazil
74
21.0
33
10.8
46
14.8
62
20.1
Rio De Janeiro
Brazil
83
20.9
42
10.6
54
13.7
70
17.7
24
6.0
Roosevelt Roads
Puerto Rico
25
6.2
30
9.0
18
5.9
2
.6
62
19.8
72
19.6
St. Lucia
Windward Islands
35
9.8
18
5.2
6
2.1
13
4.1
52
16.0
60
15.8
San Isidro
Santo Domingo
26
6.6
32
8.0
20
6.2
4
.9
66
21.0
74
18.7
San Juan
Puerto Rico
24
6.2
30
9.3
17
5.7
2
.5
63
20.5
72
19.9
San Salvador
Bahama Islands
36
10.3
42
11.7
30
8.6
14
4.6
75
22.5
84
22.3
Sao Paulo
Brazil
88
22.1
47
11.9
59
15.0
75
19.0
29
7.3
5
1.3
USAPOE
East Coast
39
9.9
55
14.0
44
14.3
27
6.9
89
29.1
98
24.6
Between
And
Roosevelt
Roads
St. Lucia
Island
San
Isidro
San Juan
San
Salvador
Sao Paulo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
St. Lucia
Windward Islands
12
3.8
San Isidro
Santo Domingo
6
1.5
17
5.0
San Juan
Puerto Rico
2
.5
11
3.6
6
1.4
San Salvador
Bahama Islands
16
5.2
27
8.7
12
3.8
16
5.1
Sao Paulo
Brazil
77
20.9
67
21.7
79
19.9
77
21.2
89
23.6
USAPOE
East Coast
30
7.4
40
13.1
25
6.3
29
7.3
14
4.5
103
25.9
Passenger Rates-Direct service is not available between all points for which a rate is published.
yr)
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE I JOINS THIS TABLE AT USAPOE, EAST COAST.
Approved For Release 2000/05/31 : CIA-MIMPY0988R000700010001-4 31
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE IV-PASSENGER AND CARGO RATES
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Adak
Anchorage
Bangkok
.-
Calcutta
Cam Ranh
Bay
Christ-
church
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Anchorage
Alaska
21
5.9
Bangkok
Thailand
141
40.3
162
46.2
Calcutta
India
164
46.8
185
52.7
23
6.5
Cam Ranh Bay
Vietnam
127
36.5
148
42.4
15
4.2
37
10.7
Christchurch
New Zealand
225
64.5
205
58.6
273
77.8
295
84.3
259
74.0
Danang
Vietnam
129
36.7
150
42.6
19
5.6
42
12.1
7
1.9
260
74.3
Eniwetok
Marshall Islands
144
41.0
164
47.0
117
33.5
140
40.0
104
29.6
179
51.2
Fairbanks
Alaska
27
7.7
6
1.8
--
48.0
-
54.7
-
44.2
-
60.4
Guam
Mariana Islands
97
28.0
118
33.9
71
20.4
94
26.9
58
16.5
201
57.5
Hickam AFB
Hawaii
111
31.9
91
26.0
158
45.3
181
51.8
145
41.4
114
32.6
Iwo Jima
Volcano Islands
79
22.7
100
28.6
97
27.8
120
34.3
83
23.8
231
66.0
Johnston Island
Pacific
130
37.3
110
31.4
145
41.4
168
47.9
131
37.5
133
37.9
Kelly AFB
Texas
96
27.4
76
21.5
249
70.9
271
77.4
234
66.8
211
60.3
Kwajalein
Marshall Islands
134
38.4
155
44.3
108
30.8
131
37.3
94
26.9
170
48.6
Manila
Philippine Islands
107
30.8
128
36.7
33
9.5
56
16.0
20
5.7
239
68.3
Marcus Island
Pacific
89
25.5
110
31.4
107
30.6
130
37.1
94
26.7
241
68.7
Midway Island
Pacific
120
34.4
121
34.6
138
39.5
161
46.0
125
35.6
144
41.2
Nandi
Fiji Islands
185
52.9
165
47.0
232
66.3
255
72.8
219
62.4
42
12.0
New Delhi
India
182
52.2
203
58.1
42
11.9
19
5.4
56
16.1
314
89.8
Okinawa
Ryukyu Islands
84
24.0
105
29.9
57
16.3
80
22.8
43
12.4
235
67.0
32 Approved For Release 2000/05/31 : CMFR85-00988R000700010001-4
Approved For Release 2000/05/31 : CIA-RDP85-00988R000700010001-4
SECRET
RATE TABLE IV-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Adak
Anchorage
Bangkok
Calcutta
Cam Ranh
Bay
Christ-
church
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pago Pago
Samoa
172
49.1
152
43.2
219
62.5
241
69.0
205
58.6
54
15.4
Richmond
Australia
231
66.2
211
60.3
278
79.5
301
86.0
265
75.7
46
13.2
Saigon
Vietnam
130
37.3
151
43.2
11
3.0
33
9.5
4
1.2
262
74.8
Seoul
Korea
81
23.3
102
29.2
99
28.4
122
34.9
85
24.4
233
66.6
Shemya
Aleutian Islands
9
2.7
30
8.6
132
37.6
155
44.3
118
33.8
235
67.0
Taipei
Taiwan
93
26.6
114
32.5
50
14.3
73
20.8
37
10.5
244
69.6
Tokyo
Japan
62
17.7
83
23.6
80
22.8
103
29.3
66
18.8
213
61.0
Wake Island
Pacific
108
31.0
129
36.9
106
30.2
129
36.7
92
26.3
167
47.7
Woodbourne
New Zealand
222
63.4
202
57.5
269
76.8
292
83.3
255
72.9
4
1.1
USAPOE
West Coast
55
15.8
35
9.9
208
59.3
230
65.8
193
55.2
170
48.7
USAPOE
East Coast
107
30.5
86
24.6
248
70.8
271
77.3
234
66.9
231
65.9
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE II JOINS THIS TABLE AT NEW DELHI.
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RATE TABLE IV-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Danang
Enivietok
Fairbanks
Guam
Hickam AFB
Iwo Jima
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Eniwetok
Marshall Islands
105
29.9
Fairbanks
Alaska
155
44.5
170
48.8
Guam
Mariana Islands
59
16.8
46
13.1
-
35.7
Hickam AFB
Hawaii
146
41.7
65
18.7
-
27.8
87
24.9
Iwo Jima
Volcano Islands
84
24.1
99
28.4
-
30.4
54
15.3
117
33.0
Johnston Island
Pacific
132
37.8
47
13.3
-
33.2
73
21.0
19
5.4
127
36.4
Kelly AFB
Texas
229
65.3
163
46.4
-
23.3
185
52.6
97
27.7
186
53.1
Kwajalein
Marshall Islands
96
27.2
9
2.7
-
46.1
36
10.4
56
16.0
90
25.7
Manila
Philippine Islands
21
6.0
84
23.9
-
38.5
38
10.8
125
35.7
63
18.1
Marcus Island
Pacific
95
27.0
109
31.1
-
33.2
63
18.0
127
36.1!
18
5.2
Midway Island
Pacific
126
36.0
95
27.3
-
36.4
117
33.5
30
8.6
76
21.8
Nandi
Fiji Islands
220
62.7
139
39.7
-
48.8
161
45.9
74
21.0
191
54.5
New Delhi
India
61
17.5
159
45.4
-
59.9
113
32.3
200
57.1:
139
39.8
Okinawa
Ryukyu Islands
45
12.7
79
22.5
-
31.7
33
9.4
122
34.T
41
11.6
Pago Pago
Samoa
206
58.9
126
35.9
-
45.0
147
42.1
60
17.1:
177
50.6
Richmond
Australia
266
76.0
185
52.9
-
62.1
207
59.2
120
34.3
237
67.7
Saigon
Vietnam
9
2.6
107
30.5
-
45.0
61
17.4
148
42.2
87
24.8
Seoul
Korea
86
24.7
101
29.0
-
31.0
56
15.9
119
34.0
37
10.7
Shemya
Aleutian Islands
119
34.1
134
38.4
36
10.4
88
25.3
121
34.E
70
20.0
Taipei
Taiwan
38
10.8
88
25.0
-
34.3
42
12.0
131
37.3
49
14.0
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RATE TABLE IV?PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Danang
Eniwetok
Fairbanks
Guam
Hickam AFB
Iwo Jima
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Tokyo
Japan
60
17.2
82
23.3
?
25.4
36
10.3
99
28.4
18
5.0
Wake Island
Pacific
93
26.6
26
7.5
?
38.7
34
9.8
53
15.1
64
18.3
Woodbourne
New Zealand
256
73.2
176
50.2
?
59.3
197
56.4
110
31.5
227
65.0
USAPOE
West Coast
188
53.7
122
34.8
?
11.7
144
41.0
56
16.1
145
41.5
USAPOE
East Coast
235
67.2
182
52.0
?
26.4
204
58.3
117
33.4
186
53.2
Passenger Rates?Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE II JOINS THIS TABLE AT NEW DELHI.
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RATE TABLE IV-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Johnston
Island
Kelly AFB
Kwajalein
Manila
Marcus
Island
Midway
Island
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Kelly AFB
Texas
116
33.1
Kwajalein
Marshall Islands
37
10.7
163
43.7
Manila
Philippine Islands
111
31.8
214
61.1
74
21.2
Marcus Island
Pacific
137
39.1
196
55.9
100
28.4
74
21.0
Midway Island
Pacific
49
14.0
127
36.3
89
25.3
105
30.0
86
24.1,
Nandi
Fiji Islands
92
26.4
171
48.7
130
37.0
199
56.7
200
57.i;
104
29.6
New Delhi
India
187
53.3
290
82.8
150
42.7
75
21.5
149
42.5,
180
51.4
Okinawa
Ryukyu Islands
107
30.4
191
54.4
69
19.8
24
6.7
49
14.1
81
23.0
Pago Pago
Samoa
79
22.5
158
44.9
116
33.2
185
52.9
187
53.4
90
25.8
Richmond
Australia
,
139
39.6
217
62.0
176
50.3
245
70.0
247
70.8
150
42.9
Saigon
Vietnam
134
38.4
238
67.9
97
27.8
23
6.5
96
27.6
128
36.5
Seoul
Korea
129
37.0
188
53.7
92
26.3
66
18.7
47
13.4
78
22.3
Shemya
Aleutian Islands
140
40.0
106
30.1
125
35.7
98
28.1
80
22.8
111
31.7
Taipei
Taiwan
116
33.0
200
57.0
78
22.3
17
4.8
58
16.7
90
25.6
Tokyo
Japan
110
31.3
169
48.1
72
20.7
46
13.2
27
7.8
58
16.7
Wake Island
Pacific
.
72
20.5
160
42.8
17
4.8
72
20.7
74
21.1.
27
7.8
Woodbourne
New Zealand
129
36.9
208
59.2
166
47.5
235
67.2
237
67.7
140
40.1
USAPOE
West Coast
75
21.5
-
-
112
32.1
173
49.5
165
44.3
86
24.7
USAPOE
East Coast
136
38.7
-
173
49.4
214
61.2
196
56.11
147
42.0
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE II JOINS THIS TABLE AT NEW DELHI.
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RATE TABLE IV-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
And
Nandi
New Delhi
Okinawa
Pago Pago
Richmond
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
New Delhi
India
274
78.2
Okinawa
Ryukyu Islands
194
55.5
99
28.2
Pago Pago
Samoa
96
27.4
260
74.4
181
51.6
Richmond
Australia
46
13.3
320
91.5
241
68.7
100
28.5
Saigon
Vietnam
222
63.3
52
14.9
46
13.3
208
59.4
268
76.5
Seoul
Korea
193
55.1
141
.
40.3
42
12.0
179
51.2
239
68.3
Shemya
Aleutian Islands
195
55.6
173
49.5
75
21.3
182
51.8
241
68.9
Taipei
Taiwan
203
58.1
92
26.3
9
2.6
190
54.2
250
71.3
Tokyo
Japan
173
49.4
122
34.7
22
6.3
160
45.6
219
62.7
Wake Island
Pacific
127
36.1
148
42.2
68
19.3
113
32.3
173
49.4
Woodbourne
New Zealand
38
11.0
311
88.7
231
66.0
50
14.3
50
14.2
USAPOE
West Coast
130
37.1
249
71.2
150
42.8
117
33.3
176
50.4
USAPOE
East Coast
190
54.4
290
82.7
191
54.5
177
50.6
237
67.6
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE II JOINS THIS TABLE AT NEW DELHI.
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RATE TABLE IV-PASSENGER AND CARGO RATES (Cont'd)
Passenger fares stated in dollars; cargo rates stated in cents per pound.
Between
Saigon
Seoul
Shemya
Taipei
Tokyo
And
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Pax
Cgo
Seoul
Korea
89 ,
25.4
Shemya
Aleutian Islands
121
34.6
72
20.6
Taipei
Taiwan
40
11.3
51
14.5
84
23.9
Tokyo
Japan
69
19.8
20
5.6
53
15.0
31
8.E1
Wake Island
Pacific
95
27.2
66
18.9
99
28.3
77
21.9
47
13.3
Woodbourne
New Zealand
258
73.8
229
65.5
231
66.0
240
68.1i
210
59.9
USAPOE
West Coast
197
56.3
147
42.1
65
18.5
159
45.4
128
36.5
USAPOE
East Coast
237
67.8
188
53.8
116
33.2
200
57.:L
169
48.2
Between
And
Wake
Island
Woodbourne
USAPOE
West Coast
Pax
Cgo
Pax
Cgo
Pax
Cgo
Wake Island
Pacific
-
-
Woodbourne
New Zealand
163
46.6
USAPOE
West Coast
109
31.2
167
47.6
USAPOE
East Coast
170
48.5
227
64.9
-
Passenger Rates-Direct service is not available between all points for which a rate is published.
Charge for passenger baggage in excess of 66 lbs. equals .005 x passenger fare x lbs. excess.
RATE TABLE II JOINS THIS TABLE AT NEW DELHI.
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SECTION V
AIRCRAFT CARGO CAPABILITIES
The aircraft cargo capacities shown below are
maximum weights capable of being airlifted under
ideal or optimum flying conditions. In planning
airlift capabilities, it should be remembered that
there are a number of variables that can reduce
cargo capability of an aircraft. Some of these are:
(a) flight altitude and head-winds, (b) flight plans
and alternate landing fields, (c) elevation of desti-
nation fields, ( d) fueling capability at destination
fields, and (e) runway lengths and weight capa-
bilities at both takeoff and landing fields.
PLANE
CARGO CAPACITY
1000 MI FLIGHT
CARGO CAPACITY
2000 MI FLIGHT
CARGO CAPACITY
3000 MI FLIGHT
CARGO DOOR
MEAS.
C-141
70,000 lbs.
70,000 lbs.
70,000 lbs.
10x2 x 9.0
C-135
87,000 lbs.
87,000 lbs.
63,000 lbs.
9x7 x 6.5
C-133
100,000 lbs.
78,000 lbs.
50,000 lbs.
12.0 x 12.2
C-130
35,000 lbs.
35,000 lbs.
8,000 lbs.
10.0 x 9.2
C-124
52,900 lbs.
38,000 lbs.
26,500 lbs.
11.6 x 11.3
C-123
16,000 lbs.
10,000 lbs.
5,000 lbs.
8.3 x 9.2
C-121
22,500 lbs.
22,500 lbs.
14,000 lbs.
9.3 x 6.1
C-119
15,000 lbs.
8,500 lbs.
NIL lbs.
8.0 x 9.2
C-118
42,000 lbs.
40,000 lbs.
23,000 lbs.
10.3 x 6.5
C-97
42,500 lbs.
36,000 lbs.
25,000 lbs.
6.5 x 6.7
C-74
54,000 lbs.
40,000 lbs.
28,000 lbs.
10.4 x 10.0
C-54
16,900 lbs.
10,200 lbs.
5,000 lbs.
5.6 x 7.9
C-47
8,000 lbs.
6,500 lbs. for 1,440 miles.
5.9 x 7.0
C-46
10,275 lbs.
10,275 lbs. for 1,895 miles.
6.8 x 8.1
NOTE: USAF policy establishes reduced payloads for over-water flights.
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DESIGN DATA FOR AIR FORCE AIRCRAFT
I. C-97 STRATOFREIGHTER
Description
a. General. The C-97 ( figure 1) is a four-
engine, low-wing, all metal, heavy transport air-
craft. The principal missions of the C-47 include
transportation of troops and cargo, medical evacu-
ation, and air resupply. There are four models of
this aircraft?C-97A, C-97C, KC-97F, and KC--
97G. The KC-97 F and G are tankers with the
air refueling equipment removed. All models
have essentially the same configuration except as
noted below ( figure 2).
Figure 1. G-97 Stratofreighter.
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C-97 cross section.
cNi
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b. Characteristics.
(1000 LB)
C--97A C-97C KC-97F KC-97G
(1) Cruising speed_ 194 knots_ 194 knots_ 215 knot. 209 knots.
(2) Takeoff distance (maximum gross 4,425 feet_ 4,425 feet_ 4,425 feei,_ 4,425 feet.
weight).
(3) Landing distance (maximum land- 2,840 feet_ 2,840 feet_ 2,870 feei,_ 2,900 feet.
ing weight).
(4) Restraint criteria:
(a) Forward ? 8.0 main cargo compartment.
? 3.0 lower cargo compartment.
(b) Aft ? 1.5.
(c) Vertical ? 2.5.
(d) Lateral ? 1.5.
40
30
10
0
?
1000
1111??????? =I= ?11?110
RANGE
NORMAL OPERATION
?
?
1
2000 3000
NAUTICAL MILES
4000
Figure 3. Payload distance, C-97A.
Cargo Compartment
a. Personnel. The C-97 has a normal crew of
five (pilot, copilot, navigator, engineer, and load-
master), except the KC-97G which has a crew of
four. The following is a comparison of the troop-
carrying capabilities of the various models:
C-97A
C-57C
KC?
97F
KC?
97G
(1) Troops
86
32
130
96
Or
(2) Litters
plus
54
54
79
None
Attendants
4
4
4
None
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b. Cargo Capacities.
(1) Main compartment
(total volume)
(2) Lower compartment
? (total volume)
tot
mi0
Cubic feet
4,309
a. Floor Strength.
(1) Main deck
(2) Lower deck
(3) Treadways (single
axle load).
d. Critical Dimensions.
(1) Main cabin:
(a) Length
(b) Width (floor level)
(a) Height
(2) Main loading door:
(a) Length
1,818
200 pounds per
square foot.
100 pounds per
square foot.
12,250 pounds.
Inches
(b) Width (fore and aft)
103/72
(c) Height (above ground) _______
112
(d) Vertical clearance
84
(3) Cargo door (right side between stations
246 and 326) : Inches
(a) Height 77
(b) Width 78
(c) Height (above ground) 137
Cargo Loading Provisions
a. Loading Ramp. Heavy equipment is loaded
Inches over the organic folding ramps. The ramps are
764 27 inches wide and adjustable to two loading
108 angles?a straight-on angle of 24? or a combina-
92 tion 15? to 30? angle (figures 7 and 8). Using
the 24? angle, the overhead clearance between the
171 ramp tread and the fuselage is 81 inches. Using
(1000 LB)
60
a 40
0
a
20
0
INORMAL OPERATION
RANGE
RADIUS
0
1000
Pt
2000 3000
NAUTICAL MILES
4000
Figure 4. Payload distance, C-97C.
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the 15? to 300 angle, the clearance is 97 inches.
The ramps are normally stored in a folded posi-
tion over the cargo door opening; however, they
can be removed for air delivery operations.
b. Monorail. A cargo hoist is operated by a
winch mounted on the bulkhead at the forward
end of the main cargo compartment. By use of an
overhead monorail the hoist is capable of lifting
and traversing 2,500 pounds the entire length of
the main cargo compartment. A total of 5,000
pounds can be traversed with the use of a free
trolley. By use of snatch block, with triple line, a
horizontal towing force of 7,500 pounds can be
produced.
20
0
r..--RANGE-
- RADIUS
_46,660 LB MAX CARGO
6.44,6
FORMAL OPERATION1-
1000 2000 3000
NAUTICAL MILES
4000
Figure 5. Payload distance, KC-97F.
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(1000 LE,)
a
cc
0.
60
40
20
0
NMI*
RANGE
RADIUS
r47,000 LB MAX CARGO I
?
4?14.
NORMAL OPERATION
?
'`?
0 1000 2000 3000 4000 5000
NAUTICAL MILES
Figure 6. Payload distance, KC-97G.
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Figure 7. Cargo loading ramp, 24? angle.
Figure 8. Cargo loading ramp, 150-300 angle.
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Weight and Balance Data
a. Maximum gross weight
b. Operating weight
c. Maximum fuel weight
d. Payload
Center of gravity limits
C-97A
(pounds)
C-97C
(pounds)
KC-97F
(pounds)
KC-970
(pounds)
153,000
153,000
153,000
153,000.
83,400
83,460
89,830
88,330.
46,740
46,740
46,740
54,032.
Figure 3___
Figure 4___
Figure 5
Figure 6.
Figure 9_
Provisions for Parachutists and Air
Delivery
a. Para,chatists. There are no provisions for
paratroop delivery.
b. Air Delivery. The main cargo door can be
opened in flight, thereby permitting air delivery
50,000
40,000
IL 30.0?0
0
te
0
a.
20,000
10,000
of equipment. The monorail supports 17 air de-
livery trolleys, each of which holds up to five
containers. The system is capable of delivering
25,500 pounds of cargo in approximately 15 sec-
onds. For specific information on air delivery see
TM 10-500-series (Airdrop of Supplies and
Equipment).
FWD LIMIT
AFT LIMIT
500
550
Figure 9.
600 650
BODY STATION
Cargo center of gravity limits, C-97.
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II. C-1 18A LIFTMASTER
Description
a. General. The C-118A ( figure 10) is a long-
range, low-wing, medium transport equipped with
a pressurized cabin, air conditioning, and a low
pressure oxygen system. The principal mission of
the C-118A is the transportation of personnel,
cargo, and litter patients.
b. Characteristics.
(1) Cruising speed 220 knots.
(2) Takeoff distance (maximum 3,755 feet.
gross weight).
(3) Landing distance (maxi- '2,750 feet.
mum landing weight).
(4) Restraint criteria:
(a) Forward
1.34
(b) Aft
1.29
(c) Vertical
2. 47
(d) Lateral
1. 00
Cargo Compartment
a. Personnel. The C-118A has a normal crew
of four?pilot, copilot, navigator, and flight engi-
neer. It will carry 76 combat-equipped troops or
60 litters plus six attendants.
Cubic
b. Cargo Capacities (figure 11). feet
(1) Main cargo compartment (vol- 4, 307
ume).
(2) Forward lower compartment 213
(volume) .
(3) Aft lower compartment (vol- 247
ume).
Pounds per
c. Floor Strength. square foot
(1) Main cargo compartment 200
(2) Lower cargo compartment:
(a) Stations 90-730 75
(b) Stations 730-938 30
d. Critical Dimensions.
(1) Main compartment: Incites
(a) Length 816
(b) Width (floor level) 104
(e) Height (maximum) 93
(2) Main loading door:
(a) Width
(b) Height
Inches
124
78%
(e) Height (above ground)
107
(3) Forward loading door:
(a) Width
903/4
(b) Height
67
(e) Height (above ground :i
104
(4) Lower cargo doors (2) :
(a) Width
37
(b) Height
45
Cargo Loading Provisions
A self-powered loading elevator which folds up
for storage can be attached to either the front or
rear cargo doorframe. The maximum hoist ca-
pacity is 4,000 pounds.
Weight and Balance Data
Pounds
a. Maximum gross weight
107,000.
b. Operating weight
66,400.
e. Maximum fuel weight
32,424.
Provisions for Parachutists and Air
Delivery
There are no provisions for parachutists or air
delivery with the C-118A.
Figure 10. C-118A Liftmaster.
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a
NAVIGATOR' S
STATION
COCKPIT
RADIO OPERATOR'S STATION (on 16 initially procured A/C only)
LAVATORY
.MAIN CABIN
0 0 0 0 0 0 0 0 0 0 0
NOSE-WHEEL
WELL -
RADOM E
CARGO COMPARTMENTl
FORWARD
AFT
CARGO COMPARTMENT
TAIL SECTION
Figure 11. Cross section, C-118A.
I?C/90/000Z aseeieu JOd peAcuddv
0
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30
25
0
0 20
11.
0
MAX FWD
POSITION
OF CARGO CG
I II
I Til
'Ii
1 II?
MAX AFT POSIT:
O CARGO CO
0
10
5
200
300
400
-4-
500
600
700
CG OF CARGO (FUS STA)
Figure 12. Cargo center of gravity limits, C-118A.
800
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1000
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III. C?il 9G FLYING BOXCAR
Description
a. General. The C-119G (figure 13) is a high-
wing, twin-engine, twin-boom, medium transport.
Its principal mission is to transport cargo, per-
sonnel, or litters. In addition, it is used for air
delivery. This aircraft features removable clam-
shell doors which are removed to permit air de-
livery of heavy equipment. When the aircraft is
operated with these doors removed its flight char-
acteristics are altered somewhat, as indicated
below.
b. Characteristics.
Doors on Doors off
(1) Crusing speed_ 160 knots__ 150 knots.
(2) Takeoff 4,530 feet__ 3,985 feet.
distance (maxi-
mum gross
weight).
(3) Landing 3,098 feet__ 3,408 feet.
distance.
(4) Restraint
criteria:
(a) Forward 4. 5
(b) Aft 1.5
(c) Vertical 2. 25
(d) Lateral 1.5
Cargo Compartment
a. Personnel. The C-119G has a crew of five?
pilot, copilot, navigator, radio operator, and load-
master. The aircraft can carry 42 troops or para-
chutists. When center aisle seats are installed, it
can carry 62 troops. In the aeromedical configura-
tion, the C-119 can carry 35 litters plus four
attendants.
Figure 13. C-119G Flying boxcar.
b. Cargo Capacities (figure 14).
Cubic feet
(1) Main compartment (maximum
volume) 3, 150
(2) Main compartment (doors off) 2, 850
c. Floor Strength. The floor is designed for a
uniformly distributed load of 200 pounds per
square foot and a maximum vehicle tire pressure
of 50 pounds per square inch. The treadways
will support an axleload up to 15,500 pounds.
Each loading ramp will support a maximum load
of 9,400 pounds. When the clamshell doors are
closed and locked, the cargo door floor strength is
56 pounds per square foot.
ION
?-?-?
1111(
il
00
0
Figure 14. Cargo compartment, C-119.
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d. Critical Dimensions.
(1) Main compartment: Inches
(a) Length 443
(b) Width (maximum) 118
(a) Height 92
(2) Main cargo door:
(a) Width (floor level) 110
(b) Height 953/4
(c) Height (above ground) 451/2
(3) Paratainer well:
(a) Length 70
(b) Width 55
(4) Air delivery limitations:
(a) Length 371
(b) Width 104
(a) Height 86
Cargo Loading Provisions
a. Loading Ramps. Two detachable, treaded
loading ramps are provided to facilitate vehicle
loading (figure 15).
25000
20000
15000
10000
5000
Figure 15. Cargo entrance, C-119.
b. Swiveling Hitch. A swiveling hitch for
block and tackle, attached at thE, front or rear of
the cargo compartment, is provided for winching.
The maximum allowable pulling force is 3,160
pounds.
FUSELAGE STAT ON. INCHES
???=1......?110
111.11
NM MINI
MIN111111111111
TUE
1111.11111111
1111111111111
11111111111111
MM.=
M11110111111
11111111.111011
UMMENN.
111111.11111111
12111101111111
111111111161
111111.11.111111
1111111=1111.
uuuuuuu
MTN
MI MN
111111.
11.
U......
Nommus
300
320
340
360
380
400
420
440
Figure 10. Cargo center of gravity limits, C-119G.
460
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520
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NORMAL
OPERATION
RANGE
----RADIUS
20
?
10
?
0 500 1000 1500
NAUTICAL MILES
2000
2500
Figure 17. Payload distance, C-119G.
Weight and Balance Data
Doors on Doors off
(pounds) (pounds)
a. Maximum gross weight____ 64,000 64,000
b. Operating weight 43,498 43,068
c. Maximum fuel weight 15,540 15,540
(1. Center of gravity limits Figure 16.
e. Payload range Figure 17.
Provisions for Parachutists and Air
Delivery
a. Parachutists. The C-119 has a maximum
capacity for 42 paratroops. Exit doors are located
at the rear of the fuselage, one on each side of the
cargo compartment. Each door is six feet high and
three feet wide.
b. Air Delivery. The C-119 is equipped with an
interior overhead monorail system for inflight dis-
charge of supplies or equipment through the para-
tainer well. Capacity of the monorail is twenty
500-pound air delivery containers (10,000 pounds).
This aircraft can be fitted for ejecting supplies or
equipment from the rear of the fuselage. When
so employed, the clamshell doors are removed,
roller conveyors are positioned on the cargo com-
partment floor, and supplies or equipment are
placed on top. Capacity of the conveyor system is
governed only by the allowable cargo load and
interior dimensions of the cargo compartment.
With the clamshell doors removed, equipment and
containers can be ejected out of the open aft end.
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IV. C-121 SUPERCONSTELLATION
Description
a. General. The C-121 ( figure 18) is a four-
engine, low-wing, long-range transport. It is de-
signed for use as an overwater cargo, personnel,
and evacuation transport.
Figure 18. C-121.
b. Characteristics.
(1) Cruising speed 223 knots.
(2) Takeoff distance (maximum 3,300 feet.
gross weight).
(3) Landing distance maxi- 2,375 feet.
mum landing weight).
(4) Restraint criteria:
(a) Forward
(b) Aft
(c) Vertical
(d) Lateral
6.0
1. 5
2. 0
1. 5
Cargo Compartment
a. The C-121 has an operating crew of four?
pilot, copilot, flight engineer, and radar navigator,
plus provisions for a relief crew of four. The
C-121G has an additional crew member, a radio op-
erator, and provisions for a relief crew of five.
The C-121C can carry 75 troops, or 47 litters plus
four attendants; the C-121G can carry 72 pas-
sengers, or 47 litters plus two attendants.
b. Cargo Capacities (figure 19). Cubic feet
(1) Main cargo compartment
3,800
(2) Aft lower compartment
424
(3) Forward lower compartment.__
269
Pounds per
c. Floor Strength. square foot
(1) Main compartment_ 300
(2) Lower compartment_ 70
d. Critical Dimensions.
(1) Cargo compartment: Inches
(a) Length 983
(b) Width (maximum floor level)_.. 121
(c) Height (maximum) _
84
(2) Forward cargo door:
(a) Height
72
(b) Width
58
(c) Height (above groun d)
133
( 3) Main cargo door:
(a) Height
74. 5
(b) Width
108.5
(c) Height (above ground)
111.5
(4) Lower compartment doors (2)
:
(a) Length
40
(b) Width
30
Cargo Loading Provisions
a. Aerolift. Aerolift is a mobile, knockdown
cargo elevator with a 10 by 10 foot platform which
will rise 144 inches above the ground. The plat-
form has a load capacity of 13,000 pounds.
b. Portable Cargo Lift. Provisions are in-
corporated at the main cargo door entrance to ac-
commodate the installation and stowage of a port-
able cargo lift with a maximum capacity of 4,000
pounds.
c. Portable Litter Lift. A stowable litter lift is
provided which can lift two litters.
Provisions for Parachutists and Air
Delivery
There are no provisions for parachutists or air
delivery in the C-121.
Weight and Balance Data
Pounds
a. Maximum gross weight__133, 000
b. Operating weight 78, 360
o. Maximum fuel weight____.39, 300
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Cargo compartment, C-12I.
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(1000 LB)
30
22,500 LB
?
?
NORMAL OPERATION
1 1 [?FT I I 11-
- RANGE ?
------ RADIUS ?
10
0
0
1000
2000 3000
NAUTICAL MILES
4000
Figure 20. Payload distance, C?I21.
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? 35000
30
5
00
00
20000
15
00
CENTER OF GRAVITY OF CARGO
MUST BE WITHIN THIS AREA.
10
00
5
500 600 700 800 900 1000 1100
DISTANCE *FROM HORIZONTAL REFERENCE DATUM (FUSELAGE STATION ) IN INCHES
1200
Figure 21. Cargo center of gravity limits, C-121.
V. C-123B PROVIDER
Description
a. General. The C-123B (figure 22) is a twin-
engine, medium assault aircraft. It is used pri-
marily as a troop and cargo carrier with the
capability of operating from hastily prepared
airfields. Other missions include air delivery,
medical evacuation, and parachute operations.
b. Performance Characteristics.
(1) Cruising speed 130 knots.
(2) Takeoff distance to clear to
50-foot obstacle 4,130 feet.
(3) Landing distance to clear
50-foot obstacle 2,243 feet.
(4) Restraint criteria:
(a) Forward 8.0
(b) Aft
2.0
(c) Vertical
4.5
(d) Lateral
1.5
Figure 22. C-123B.
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Cargo Compartment
a. Personnel. The C-123B has a normal crew
of four?pilot, copilot, navigator, and loadmaster.
It is capable of carrying 60 troops; 16 parachut-
ists; or 50 litters plus six ambulatory patients.
b. Cargo Capacities and Limitations (figure
23). The rear loading ramp permits straight-in
loading into the cargo compartment, which has
2,420 cubic feet of cargo space. In placing cargo,
the following limitations should be noted in plan-
ning loads for the C-123: when the navigator's
station is installed, the overhead clearance in the
forward right portion of the cargo compartment is
limited. A bailout chute, which must be left clear,
is located beneath the navigator's seat in the vi-
cinity of station 145.
c. Critical Dimensions.
(1) Cargo compartment: Inches
(a) Length 315
(b) Width at wheel wells (in-
cluding ramp) 110(444)
(c) Height
(2) Cargo loading door:
(a) Width 110
(b) Height 98
(c) (Height above ground)
(d) Ramp angle
331/2
Degrees
15
d. Floor Strength. The treadways will with-
stand a concentrated load of 3,000 pounds or an
evenly distributed load of 200 pounds per square
foot. The inner walkway will also carry 200
pounds per square foot, but the concentrated load
is limited to 2,000 pounds. The outer walkways are
designed for a 1,000-pound concentrated load and
a distributed load of 100-pounds per square foot.
Cargo Loading Provisions
a. Auxiliary Ramps. Two auxiliary ramps are
provided for use when loading vi.thicles which re-
quire a more gradual slope than ',hat provided by
the main ramp. The auxiliary ramps may be
spaced to accommodate the tread width of any
vehicle to be loaded.
b. Load Assist Pulley. A pulley is provided
for winching loads into the aircraft. The pulley
mechanism can be bolted to the tiedown fittings in
the cargo floor. The sheave may be used with
cables up to three-quarters of an inch in diameter.
When the towing vehicle or winch is placed aft of
the aircraft, the maximum drew pull is 3,300
pounds. If the cable is routed through the front
entrance door, the maximum permissible load is
2,800 pounds.
Provisions for Air Delivery
a. Parachutists. The C-123B may be used to
jump parachutists, either from the two rear per-
sonnel doors or from the cargo ramp. For specific
details to jump from this aircraft, see TM 57-220.
b. Air Delivery. The C-123E has a limited air
delivery capability using the gravity ejection
method. Models AF 57-6185 through 57-6202 are
equipped with a pendulum release for use in cargo
extraction.
Figure 23. Cargo compartment, C-123B.
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se Weight and Balance Data
Pounds c. Fuel capacity 13,920.
a. Maximum gross weight 55,200. d. Payload Figure 24.
b. Operating weight 33,000. e. Center of gravity limits Figure 25.
al
(1000 LB)
a
a
.J
It
a.
20
15
10
5
0
1 1 1 1 1 1 1 1 1 1 1 1
55,200 LB MAX NORMAL TAKE OFF WT
5000 FT CRUISING ALTITUDE
?
.111= ? M.= ???
RANGE
?RADIUS
4
A
0 500 1000 1500 2000
NAUTICAL MILES
4111101
2500
Figure 24. Payload distance, C-123.
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20,000
18,000
16,000
14,000
12,000
10,000
8.000
6.000
4,000
2,000
1,000
INIII MN ? ?
MI IIIIIMII ?
EllIrmill I
NM MIMES ?
NM Elm. ?
1111011 ? ?
111m1INIMIIII I
IIIMMIN00.1 II
INN= NW 111
MI III
III II,
II MI 111
MI El II II
II MI III II
MI MI El II
III NM HI a
I
"rlIWA I
I
11. r
I
am i_ var
1111 ilew:Ir
MAX. FORWARD
LIMIT OF CARGO CG
MAX. AFT ?
LIMIT OF
CARGO CG
140 160 180 200 220 240 260 280 300 320 340 360 380
FUSELAGE STATIONS
Figure 25. Cargo center of gravity limits, C-123B.
VI. C-124 GLOBEMASTER
Description
a. General. The 0-124 ( figure 26) is a four-
engine, long-range, heavy transport with a princi-
pal mission of airlifting personnel and outsized
cargo. It may also be employed for air delivery or
medical evacuation. This aircraft features a clam-
shell-type door in the nose which permits straight-
in loading, and an auxiliary folding floor for
increased deck area. There are two models of this
aircraft?the C-124A and C-1240. The principal
difference between the two modols is their power-
plants. Significant differences in performance
are indicated below.
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b. Performance Characteristics.
C-124A C-124C
(1) Cruising 200 knots_ 200 knots.
speed.
(2) Takeoff dis- 4,820 feet__ 4,820 feet.
tance (maxi-
mum gross
weight).
Landing dis- 4,000 feet__ 4,200 feet.
tance (maxi-
mum landing
weight).
(4) Restraint criteria:
(a) Forward:
(3)
1. Troops in cargo compartment_
8. 0
2. No troops in cargo area
4. 0
(b) Aft
1.5
(c) Vertical
2. 0
(d) Lateral_
1. 5
Cargo Compartment
a. Personnel. The C-124 has a crew of five?
pilot, copilot, flight engineer, navigator, and ra-
dio operator. There are provisions for a relief
crew of three. The C-124 can carry 200 combat-
equipped troops; 112 parachutists; or 127 litter
patients with 25 attendants.
b. Cargo Areas (figure 27).
(1) Main cargo floor. The main cargo floor
extends from station 236 to station 1120.
From station 236 to station 360 the floor
slopes up as a continuation of the nose
loading ramps at an angle of 17?. At
236
363 460 560 660 760
CARGO CARGO
CARGO CARGO !CARGO'
DD EE
"*".. -
JOSE LOADING AREA
WHEEL
WELL
L.
FF
F
GG
0 -
Figure 26. C-124C.
station 360 the floor angle is reduced to
11? and continues to station 460. From
station 460 to station 1120 the floor is
nearly level. The main cargo floor is di-
vided into two areas?the treadway and/
or maneuvering areas and the red area.
Two 32-inch wide treadways run from
stations 236 to 1060, the entire length of
the floor. Additional high strength areas
are provided on each side of the tread-
ways to permit positioning of wheel
vehicles. Because of the steep angle of
the ramps, overhead clearance can become
critical on outsized loads (figure 28).
(2) Auxiliary floor. An auxiliary floor is
provided to increase the capacity of the
aircraft. The floor is hinged to the
fuselage and is supported by stanchions
1060 1160
920 1000 1120
CARGO CARGO
CARGO CARGO --- LAN.
CARGO
CARGO 556 ACCESS
ACCESS
AND
LIGHT
CARGO
HH
II
Figure 27. Cross-section,
I
CARGO HOIST RAILS
LOADING WELL
AUXILIARY FLOOR
C-124C.
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MAXIMUM HEIGHT-INCHES
140
120
100
80
60
40
20
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rim
M. . itsm.,.. 1 .
.- raligprii 92 WID7M11111 I!
nemosn Er? " ?
"'?WilircIMINlia.a 411:11111111.6 Pill 11
illraminAtralr! limmi..5.11
m.-- ..-.1 NIL
UMMUMNIIIIMIIIIMMIlliglAIM
11111111MMISINLER MIN.
11111.114%. 100" WIDE -dill ri
Link, - sid la . -I
rir '
. .. smINIIIIIIMIll WM
Illehani I ? .1177..Emor ? Ii
I mi
......... ...
(6011
-I -= mobioNge
111111
. . i? . E.. ]
120" WIDE
1 111 I
MIMI II II
:1111 III
,
I I I iii
III
II
?11111 130" WIDE 11111 11
1 IINI ilii ki,..m.,_
I. I
I !!!!!!! 01 ---1
IIIMM I:11"e
MOE ?el
uremtivisue miirreris mmarno to
......
Ihniem=r.F.a...9.1 iiiMmi HMIs II riBillibli Pm
I 111Mmit IIIIIIIIIIIM
20 40 60 80 100
OVERHANG (FRONT OR REAR)?INCHES
---
CHART SHOWS MAXIMUM
ALLOWABLE HEIGHT OF
VEHICLE AT VARIOUS
WIDTHS. IT ALSO INDI-
CATES THE MAXIMUM
ALLOWABLE OVERHANG
(FRONT OR REAR) FROM
AXLE CENTERLINES.
EXAMPLE: A VEHICLE 120
INCHES WIDE, WITH AN
OVERHANG OF 75 INCHES-
THE MAXIMUM ALLOWABLE
HEIGHT WOULD BE
87 INCHES.
120
140
HEIGHT CLEARANCE CHART
Figure 28. Nose loading clearance chart, C-124.
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attached to the main cargo floor. The
auxiliary floor is constructed in sections
which may be used independently of each
other. This allows flexibility in load
planning, particularly when employing
mixed loads of personnel and equipment.
e. Floor Strength. The maximum single axle-
load on the treadways and maneuvering areas is
20,000 pounds. The red area will support a dis-
tributed load of 30 pounds per square inch. The
auxiliary floor is designed for low density cargo
and personnel only. The maximum load is 43
pounds per square foot.
d. Critical Dimensions.
(1) Main cargo compartment: Inehe8
(a) Length 884
(b) Width (floor level) 136
(e) Height (maximum clearance) 1391/,
(d) Height (auxiliary floor in-
stalled) 73,3A
(2) Nose loading door:
(a) Width 136
(b) Height 140
Degrees
(C) Ramp angle 17
(3) Loading well: Ineh.es
(a) Length 159
(b) Width 93
(e) Vertical clearance (from
ground) 105
Cargo Loading Provisions
a. Nose Loading Ramps. The nose loading
ramps (figure 29) consist of two separate, laterally
adjustable, 36-inch wide ramps. The ramps may
be positioned to a, maximum of 50 inches apart and
a minimum of 24 inches apart, measured from
inside edge to inside edge. The nose, loading
ramps are used when loading vehicles and large,
heavy cargo; they are capable of supporting
Figure 29. Loading ramp, C?I24.
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50,000 pounds or a single axle load of 17,800
pounds.
b. Loading Well Platform. The loading well
platform is located between stations 760 and 920;
when in place it forms the cargo floor over the top
of the loading well. The platform is capable of
supporting a maximum load of 9,300 pounds. Two
traveling cranes serve as the elevator mechanism
for lowering and raising the platform.
c. Traveling Cranes. To assist in the loading
and positioning of cargo in the aircraft, two dual
hoist, bridge-type traveling cranes are installed
Weight and Balance Data
a. Maximum gross weight
b. Operating weight
c. Maximum fuel weight
d. Allowable cargo load
e. Center of gravity limits
on rails in the main cargo compartment from sta-
tions 436 to 1000. Each crane is equipped with
two hoist cables. The maximum allowable load
that each cable can hoist unassisted is 2,000
pounds; however, with the use of snatch blocks,
the maximum is increased to 16,000 pounds when
both traveling cranes are used.
d. Winch Cable Pulleys. Two large pulleys
are installed at station 1117 for winching heavy
cargo into the aircraft. The pulleys are designed
for use with a %-inch cable with a maximum pull
of 30,000 pounds.
C-124A
(pounds)
C-12.4C
(pounds)
175,000
185,000.
112,880
114,685.
65,143
66,760.
Figure 30
Figure 31.
Figure 32
(1000 LB)
80
60
40
20
RANGE
RADIUS
52,144 LB
=mom etwoM
-I CRUISE AT 10,000
FT
.?1?110?01,
1000 2000 3000
NAUTICAL MILES
4000 5000
Figure 30. Payload distance, C-124A.
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El
IMO
int
MIN
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(1000 LB)
80
60
40
20
0
56,286 LE71
1?111?II.
RANGE
RADIUS
CRUISE AT 5000
FT
0
1000
2000
NA
30
UTICAL
00
MILES
40
00
50
00
Figure 31. Payload distance, C-124C.
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70000
65.000
60,000
55,000
50,000
a 45,000
0
2
II

40.000
35,000
30.000
25,000
20.000
15,000
10,000
5,000
1. THIS CHART SHOWS THE RANGE OF
TOTAL CARGO CG.
2. ARRANGE THE CARGO SO THAT THE
CARGO CG WILL BE AS CLOSE AS
POSSIBLE TO THE STATION MIDWAY
BETWEEN THE LIMIT CURVES FOR
THE APPLICABLE CARGO WEIGHT.
MAXIMUM AFT POSITION CURVE
FOR CARGO CG.
MAXIMUM FVVD
POSITION CURVES
FOR CARGO CG
570
590
610
630
650
CARGO
670
690
710
730
PLACEMENT-FUSELAGE STATIONS
Figure 32. Cargo center
Provisions for Air Delivery
a. Para,ckatists. The C-124 can deliver 112
parachutists. For specific procedures for rigging
the aircraft for jumping, see TM 57-220.
of gravity limits, C?I24.
750
770
790
810
b. Air Delivery. The C-124 may be used for
air delivery of equipment through the elevator
well. Specific information for air delivery is con-
tained in the TM 10-500-series.
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VII. C-130 HERCULES
Description
a. General. The C-130 (figures 33 and 34) is
a four-engine, turboprop, medium assault trans-
port. There are three models of this aircraft?
the C-130A, B and E. Principal differences in-
clude powerplants, cargo door size, and fuel capac-
ity. The C-130A and B are used for tactical air-
lift, while the C-130E, with its increased gross
weight and fuel capacity, is used for both stra-
tegic and tactical airlift. Missions of the C-130
include air transport, assault missions, air delivery,
and medical evacuation. Special features of the
0-130 are cargo compartment pressurization,
ground and in-flight air conditioning, and an up-
swept aft fuselage which contains a built-in load-
ing ramp that serves as the rear door (figure 35).
Figure 33. C-130E.
CREW
COMP'T
TROOP AND CARGO COMP' T
Figure 34. Cross section, C-130.
LOADING_._
RAMP
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b. Performance Characteristics.
(1) Cruising speed
(2) Takeoff distance
(3) Landing distance
(4) Restraint criteria (all models) :
(a) Forward (airlanded mission/air
(b) Aft (with JATO assist)
(c) Vertical
(d) Lateral
C-130A C-130B
290 knots 275 knots
2,540 feet 3,000 feet
1,555 feet 2,100 feet
delivery)
Figure 35. Cargo loading ramp, C-130.
Cargo Compartment
a. Personnel. The 0-130 has a crew of five?
pilot, copilot, navigator, flight engineer, and load-
master. It can carry a total of 92 personnel; 64
parachutists; or 74 litters plus two attendants.
b. Floor Strength. On the C-130A model, 21-
inch wide treadways are installed 58 inches apart.
On 0-130B and E models, 35-inch wide treadways
are installed 30 inches apart. The treadways will
support an axleload of 13,000 pounds except that
during flight the load on the treadway, forward
of station 337 and aft of station 682, is limited to
6,000 pounds per axle. Outside the treadway areas
the load must not exceed 2,500 pounds per wheel.
These axle and wheel limitations are based on a
tire pressure of 100 pounds per square inch. A
load of 5,000 pounds may be placed on the ramp
provided the load does not exceed 125 pounds per
square foot.
c. Critical Dimensions. Inches
(1) Cargo compartment:
(a) Length (including range) __ 492 (612)
(b) Width 123
(c) Height 108
(d) Maximum width for air
delivery
(2) Cargo loading door:
(a) Width (ramp level) 1191/2
(b) Height (C-130A/C-130 B
and E) 106/109
(c) Height (above ground,
nominal) 40
Degrees
11
C-130E
275 knots.
4,210 feet.
2,230 feet.
8. 0/4. 0
1.5 (2.0)
2. 0
1.5
113
(d) Ramp angle
Cargo Loading Provisions
a. Auxiliary Loading R a IL p s. Auxiliary
truckloading and auxiliary grottndloading ramps
are used to bridge any gap between the ramp and
the truck, platform, or ground. These auxiliary
ramps are attached to the aft end of the loading
ramp and may be adjusted to conform to vehicle
tread widths as required.
b. Snatch Blocks. Two moveable snatch blocks
are provided for winching loads into and within
the aircraft. The cable to the prime mover may
be routed either through the rear or forward cargo
door. (On later models of the (J-130E there is
no forward cargo door.)
c. Portable Winch. A portable cargo- winch
capable of winching any authorized load into the
aircraft with the aid of snatch blocks is provided.
The winch may be attached to any 10,000- or
25,000-pound tiedown fitting.
Provisions for Air Delivery
a. General. The C-130 has the dual-rail air-
drop system installed. Single platform loads up
to 25,000 pounds, or multiple loads up to the ca-
pacity of the aircraft, may 1343 delivered. For
procedures on air delivery of cargo, see TM 10-500
series.
b. Parachutists. Sixty -four parachutists may
be delivered from the 0-130 using the paratroop
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doors aft of the wheel wells. When this aircraft boards and roller conveyors block the paratroop
is used for heavy drop, parachutists will follow doors. For specific procedures for jumping from
the loads out the rear cargo door since the buffer the C-130, see TM 57-220.
Es Weight and Balance Data
C-180A (pounds)
C-180B (pounds)
C-130E (pounds)
a. Maximum gross weight
124,200
135,000
155,000.
b. Operating weight
61,192
69,341
76,000.
c. Maximum fuel capacity
34,125
44,850
62,920.
d. Allowable cargo load
e. Center of gravity limits
Figure 36
Figure 39
Figure 37
Figure 38.
mi
(1000 LB)
a
a
a.
40
30
20
10
0
d
NORMAL OPERATION
ak.
I I
OPTIMUM CRUISE ALT.
RANGE
RADIUS
0 1000 2000 3000
NAUTICAL MILES
Figure 36. Payload distance, C-130A.
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(1000 LB)
40
30
20
10
0
wpmedlimm.ImemOmm?S
OPTIMUM CRUISE ALTITUDE
.111111111MI
RANGE:
RADIUS
0 1000 2000 3000 4000
NAUTICAL MILES
Figure 37. Payload distance, C-130B.
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to
M
J
o
o
o
40
30
20
10
0
r
-
AM.
\
1
I
0
1000
r
2000 3000
NAUTICAL MILES
4000
5000
Figure 38. Payload distance, C-130E.
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CARGO LOAD
1000 LBS
35
30
25
20
15
10
5
0
FORWARD ZONE
CENTER ZONE
AFT ZONE
I ?1?
I
I
I
F
I
I
I
--I
I
I
I
I
I
I
I
i
I
?I?
I
FUS STA 245 281 337 401 457
597 627 682 737 803 869
Figure 39. Cargo center of gravity limits, C-130.
VIII. C-133 CARGOMASTER
Description
a. General. The 0-133 (figure 40) is a four-
engine, propjet, long range, heavy cargo carrier.
Its principal mission is the airlift of heavy, out-
sized cargo, such as missile systems and their sup-
port. There are two models of this aircraft in
the inventory, the A and B. The C-133B differs
from the C-133A by the incorporation of more
powerful engines and clamsher!-type aft cargo
loading doors ( figures 41 arid 42).
b. Performance Characteristics. C-133A C-133B
(1) Cruising speed 260 knots _ 270 knots.
(2) Takeoff distance 4,250 feet 4,510 feet.
(3) Landing distance 3,500 feet _ 4,135 feet.
(4) Restraint criteria:
(a) Forward 3. 0
(b) Aft 1.5
(c) Vertical 3. 0
(d) Lateral 1. 5
Figure 40. C-133A.
Cargo Compartment
a. Personnel. The 0-133 has a crew of four?
pilot, copilot, navigator, and flight engineer.
There are also provisions for a relief crew of three.
This aircraft is designed as a cargo carrier. How-
ever, if required, 120 high-density seats, or 55
litters, may be installed.
b. Floor Strength. The rated strength of the
cargo compartment floor for distributed loads is
300 pounds per square foot, except between sta-
tions 772 and 914 where the allowable floorload is
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375 pounds per square foot. The treadways will
support a single axleload up to 20,000 pounds and
a tandem axleload up to 44,000 pounds. Up to
10,000 pounds may be stowed on the ramp.
c. Critical Dimensions.
(1) Cargo compartment: Inches
(a) Length L 168
(b) Width (floor level) 142
(c) Height 143
(2) Rear cargo doors:
(a) Width (C-133 A, B)
(b) Height (C- 133 A, B)_____
(a) Height (above ground) ._
(d) Ramp angle
(3) Side cargo door:
(a) Width
(b) Height
(a) Height (above ground) ._
142, 1321/2
150,159
50
Degrees
9
Inches
106
100
50
SEARCH
RADAR
- PILOT'S COMPARTMENT
FLIGHT DECK
CREW
QUARTERS
FORWARD CARGO I OADING 0(5
?CREW ACCESS DOOR
I AVATORY
J
seclion, C-133B.
- PRESSURE
RI It (HEAD
igUrC 42. Carp) 1 (Out)!
amp. C-/33A.
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Cargo Loading Provisions c. Cargo Loading Sheaves. Heavy cargo may
be winched into the aircraft using an externally
a. Ramp Toes. Two removable ramp toe
tions, each each 30 inches wide, are furnished to provide located prime mover and two cargo loading
sheaves. The sheaves may be used with a winch-
an extension from the ground onto the rear cargo
ing cable of 34-inch diameter or less. The maxi-
ramp. The toes can be adjusted laterally to ac-
commodate tread widths up to 136% inches. mum allowable cableload is 20,000 pounds.
b. Portable Electric -Winch,. A portable winch,
Provisions for Air Delivery
which can be attached to the 25,000- or 35,000-
pound tie,down fittings, is furnished. The winch is There are no provisions for air delivery or para-
capable of a 15,000-pound drawbar pull. chutists with the C-133.
Weight and Balance Data
a. Maximum gross weight
b. Operating weight
c. Maximum fuel capacity
d. Allowable cargo load
C-133A
(pounds)
C-133B
(pounds)
275,000
286, 000.
128,000
129,000.
117,728
118,534.
Figure 43
Figure 44.
(1000 LB)
120
80
40
0
RANGE
? RADIUS
95,418 Lid
?
?
0 1000 2000 3000 4000 5000
NAUTICAL MILES
Figure 43. Payload distance, C-133A.
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(1000 LB)
120
80
0
)?
a
a.
40
RANGE
RADIUS
110,015 LB
0
1000
2000 3000
NAUTICAL MILES
4000
5000
Figure 44. Payload distance, C-133B.
IX. C-135 STRATOLIFTER
Description
a. General. The C-135 ( figure 45) is a long-
range, high performance, four-engine jet trans-
port. This aircraft is capable of hauling cargo,
troops, or litter patients. The upper deck, cock-
pit, and aft lower baggage compartment are pres-
surized and air conditioned. There are two models
of the C-135, the A and B. The C-135A has turbo-
jet engines. The C-135B has turbofan engines
and hence greater range and speed.
Figure 45. C-135A.
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b. Characteristics.
(1) Cruising speed
(2) Required runway length
(3) Restraint criteria:
(a) Forward
(b) Aft
(c) Vertical
(d) Lateral
Cargo Compartment
a. Personnel. The C-135 has a crew of four?
pilot, copilot, navigator, and loadmaster. The
aircraft is capable of carrying 126 troops using
six-abreast seating, or 75 troops using side seats.
In an aeromedical role the C-135 can carry 44 lit-
ters, 48 ambulatory patients and six attendants.
b. Capacities. Cubic feet
(1) Cargo compartment (volume) ____ 5,478
(2) Aft baggage compartment
(volume)
c. Floor Strength.
(1) Main compartment
(2) Aft baggage compartment
d. Critical Dimensions.
(1) Cargo compartment:
(a) Length
100
Pounds pier
square foot
200
40
PILOT
COPILOT
NAVIGATOR
LOADMASTER
Inches
860
C-135A C-1 35B
460 knots 467 knots.
8,850 feet 7,200 feet.
8.0 8.0.
1.5 1.5.
2.0 2.0.
1.5 1.5.
Inchee
(b) Width (maximum)
136
(c) Height
85
(2) Main loading door:
(a) Width
117
(b) Height
78
(c) Height (above ground)
121
Cargo Loading Provisions
Due to the 10-foot height of the cargo door above
the ground, materiel handling equipment, such as
high lift trucks or forklifts, is required to load
heavy cargo. The C-135 is partimlarly adaptable
to palletized loads. The cargo handling system
includes a ball transfer plate, roller conveyors,
guide rails, and pallet locks. The ball transfer
plate, adjacent to the cargo door, provides for a
90? change of direction for loading and unloading
pallets.
FWD FUEL
AIR-COND &
FUEL
AFT LOWER
LWR
MAIN
NOSE
COMPT
I
BAY
WHEEL
WELL
AFT BAY
BAGGAGE
COMPT
Weight and Balance Data
a. Maximum gross weight
b. Operating weight
c. Maximum fuel weight
d. Payload distance
e. Center of gravity limits
Provisions for Airdrop
Figure 46.
Cross section, C-135.
C-135A
(pounds)
C-135B
(pounds)
270,000
274,000.
112,000
117,500.
170,864
167,588.
Figure 47
Figure 48.
Figure 49
There are no provisions for parachutists or airdrop with the C-135.
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1000
80
60
40
20
RANGE
-- RADIUS
11.
't
???
A
AIL
AM.
2
V
4
6
DISTANCE (1000 NAUTICAL MILES)
Figure 47. Payload distance, C-135A.
8
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100
80
0 60
I
a.
40
20
1?11.
11111111111MI
jimmoiON
RANGE
RADIUS------
A
1000 2000 3000 4000 5000 6000 7000 8000
NAUTICAL MILES
Figure 48. Payload distance, C-135B.
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90,000
80,000
70,000
60,000
0
0
4
50,000
IL.
0
IA
0
40,000
30,000
20,000
10,000
I T- 1
MAXIMUM PAYLOAD
FORWARD LIMIT
?
MI
111NNW
11
NE In
ME SI
II MB NI
II MEM
II NNE MI
II MI El
111 MIMI MI
II RIM IN
II NMI NI
?MEE IN
?UI'.
MIME III
MEE NM
MEIN
iU
MEIN
F.
Ai. LIMIT
1.1111.11.
NMI.
MIME
NMI
MUM
MEM
11111111.
111111.11111
400
500
600
700
800
BODY STATION
900
Figure 49. Cargo center of gravity limits, C-135.
1000
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X. C-141A STARLIFTER
Description
a. General. The C-141A ( figure 50) is a high-
wing, four-engine, heavy transport. Its mission
is the transport of cargo and personnel. Features
of this aircraft include crew and cargo compart-
ment pressurization, and ground and in-flight, air
conditioning. This turbofan aircraft will become
the backbone of the strategic airlift capability of
the U.S. Air Force. The data listed for the C-141
is design data and is subject to change based on
actual flight tests.
b. Performance.
(1) Cruising speed 440 knots.
(2) Takeoff roll 3, 900 feet.
(3) Landing roll 1, 750 feet.
(4) Restraint criteria:
(a) Forward
8. 0
(b) Aft
1. 5
(c) Vertical
2. 0
(d) Lateral
1.5
Cargo Compartment
a. Personnel. The C-141A has a crew of four?
pilot, copilot, navigator, and flight engineer. It
will carry up to 154 troops; 123 parachutists; or
80 litters plus eight attendants.
b. Cargo Capacity (figure 51).
(1) Volume (excluding 6, 524 cubic feet.
ramp area) .
(2) Design payload 68, 500 pounds.
c. Critical Dimensions.
(1) Cargo compartment: Inches
(a) Length 840
(b) Height 109
(c) "Width 1231/4
(2) Cargo loading door:
(a) Width
(b) Height
(c) Height (above ground)
(d) Ramp angle_
1231/4
109
50
Degrees
11
Figure 50. C-141A.
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d. Floor Strength. The cargo floor is designed
for a distributed load of 300 pounds per square
foot and an axleloading of 10,000 pounds, except
in the high strength area between stations 678 and
98 where the floor limit is 100 pounds per square
foot and a 20,000 pound axleload. The ramp may
be loaded to 200 pounds per square foot with a
total load limitation of 7,500 pounds.
Cargo Loading Provisions
a. Loading Ramp. Only rear end loading is
provided on the C-141A. The aft cargo compart-
ment is furnished with the ramp and the pres-
sure door. The ramp, hinged at its forward end,
lowers to a position in the plane of the cargo floor
(for truck-bed-height loading), or to the ground
for loading vehicles.
b. 463L System. The C-141A is equipped with
the 463L pallet system. Four rows of roller con-
veyors run the entire length of the cargo compart-
ment and ramp. These conveyors are easily de-
tached from the floor and can be stowed in an in-
verted position in recesses in the floor to present
a flush surface when not in use. Restraint rails
are installed to be compatible with the cargo
pallets of the system. The cargo compartment
will handle nine 463L pallets on the main floor and
one on the ramp ( figure 52).
lemsaumull11111111
?/:,
,11
)44%11
INIIIiimmul??""111111:11
- -
CREW
COMP'T
CARGO COMP'T
Figure 51. Cross section, C-141A.
INTEGRAL PROVISIONS FOR 463L PALLET SYSTEM
Figure 52. C-141 cargo floor design.
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Provisions for Airdrop
a. Parachuti8ta. A total of 123 parachutists
may be delivered from jump doors located on each
side of the aft cargo compartment.
b. Air Delivery. The cargo ramp and aft cargo
doors are flight-operable, permitting airdrop of
loads up to 35,000 pounds per single package.
80
60
40
20
0
PAYLOAD
Weight and Balance Data
a. Maximum gross weight_
b. Operating weight (varies with
mission requirements)
e. Maximum fuel weight_
d. Payload
Pounda
316, 600
139, 174
150, 020
Figure 53
NORMAL OPERAT ON
OPTIMUM CRUISE ALTITUDE
RANGE ?
RADIUS-
1111 ?111=1 111111, .0???
It
0 1 2 3 4 5 6 7
DISTANCE-1000 NAUTICAL MILES
Figure 53. Payload distance, C-141A.
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DESIGN DATA FOR ARMY AIRCRAFT
I. 0-1 BIRD DOG
Description
a. General. The 0-1 (figure 1) is an all metal,
high-wing, two-place (tandem) monoplane pow-
ered by a Continental six cylinder, air-cooled en-
gine. There are three models?the 0-1A, 0-1E,
and TO-1D (instrument trainer). The A and E
models are observation aircraft which, with modi-
fication, can be converted to instrument trainers.
The 0-1 features the conventional fixed landing
gear. It can carry one passenger or a 250-pound
bundle under each wing attached to bomb
shackles.
b. Characteristics. (A and E models are the
same except the A model has a gross weight of
65 pounds less than the E model. TO-1D is not de-
scribed since its use is normally restricted to in-
strument training.)
(1) Cruising speed 87 knots.
(2) Takeoff distance to clear 634 feet.
50-foot obstacle.
(3) Landing distance to clear 550 feet.
50-foot obstacle.
(4) Endurance at cruising speed 4 hours 15
minutes.
Weight and Balance Data
Pounds
a. Maximum gross weight 2, 165
b. Operating weight 1, 839
e. Maximum fuel capacity 258
Figure
1, 0-1 Bird Dog with wing bundles attached.
II. U-6A
Description
a. General. The U-6A (figure 2) is an all
metal, high-wing monoplane powered by a single
Pratt and Whitney engine developing 450 horse-
power. It is designed to carry a pilot and five
passengers. The U-6A is a utility aircraft, with
a fixed conventional landing, gear used for person-
nel cargo, and medical evacuation. Two litter pa-
tients and three passengers can be transported by
BEAVER
this aircraft (figure 3). It can also be used for
parachute operations with a maximum of four
parachutists. External load capability is 1,000
pounds suspended on four bomb shackles, two un-
der each wing with a capacity of 250 pounds per
bomb shackle.
b. Characteristics.
(1) Normal cruising speed__ 105 knots.
(2) Takeoff distance to clear 50- 950 feet.
foot obstacle.
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Figure 2. The U-6A.
SEATING
ARRANGEMENT
LITTER
ARRANGEMENT
Figure 3. Seating and litter arrangement, U6A.
(3) Landing distance to clear 1, 040 feet.
50-foot obstacle.
(4) Endurance at cruising speed 5 hours, 30
(full wing tanks). minutes.
Cargo Compartment
a. Capacity. The IJ-6A is deigned for opera-
tion by one crew member, the pilot. The cargo
compartment has an entrance on each side of the
aircraft, measuring 30 by 40 in thes. The cargo
floor is limited to 100 pounds per square foot for
an evenly distributed load.
b. Diraemion8 of the Cargo Compartment.
Inoltee
(1) Length
(2) Width 48
(3) Height 51
(4) Height of floor (above ground) __ 46
Weight and Balance Data
Pounds.
a. Maximum gross weight 5, 100
b. Operating weight_ 3, 338
c. Fuel capacity 828
d. Allowable cargo load (maximum
fuel) 934
e. Allowable cargo load (50-nautical-mile
radius) 1, 558
f. Allowable cargo load (100-nautical-
mile radius) 1, 426
III. U-1A OTTER
Description
a. General. The U-1A (figure 4) is a single-
engine, high-wing airplane with fixed conventional
landing gear. It is a utility airc raft and its mis-
sions include the transport of light cargo, air
delivery, medical evacuation, arid liaison. The
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Figure 4.
1J-1A has dual controls, but is designed for opera-
tion by only a pilot.
b. Characteristics.
(1) Normal cruising speed 105 knots.
(2) Takeoff distance to clear 1, 000 feet.
50-foot obstacle.
(3) Landing distance to clear 900 feet.
50-foot obstacle.
(4) Endurance at cruising 6 hours.
speed.
Cargo Compartment
a. Capacity. The cargo compartment is fitted
with nine removable seats, giving the U-1A a
maximum passenger capacity of 10 ( figure 5). The
aircraft can also be rigged to accommodate four
Figure 5. Cargo compartment, U?IA.
The U?IA.
litters, two ambulatory patients, and one medical
attendant. Five parachutists may be dropped
from the IJ-1A. For specific procedures for para-
chuting from this aircraft, see TM 57-220. The
floor of the cargo compartment is fitted with 10
permanent and four removable tiedown rings for
securing general cargo. The floor is limited to
100 pounds per square foot. Behind the cargo
compartment is a baggage compartment with a
70-cubic-foot capacity and a floor strength of 75
pounds per square foot.
b. Dimensions.
(1) Cargo compartment:
Inches
(a) Length
156
(b) Width (floor)
60
(a) Height (maximum)
52
(2) Baggage compartment:
(a) Length
45
(b) Width
51
(c) Height
55
(3) Main cargo door:
(a) Width
45
(b) Height
46
(c) Height (above ground) _ _ _ _
39
Weight and Balance Data
Pounds
a. Maximum gross weight 8,000
b. Normal operating weight 5, 190
a. Maximum fuel capacity 1, 281
d. Allowable cargo load (50-nautical-
mile radius) 2, 522
e. Allowable cargo load (100-nautical-
mile radius) 2, 314
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IV. U-8 SEMINOLE
Description
a. General. The 1J-8 ( figure 6) is a twin-en-
gine, command-type aircraft. Its principal mis-
sion is the transport of personnel and other liaison
functions. This aircraft may be used for aerial
surveillance and target acquisition by some modi-
fications and the installation of aerial sensory de-
vices. There are two models of the U-8 in the
inventory?the ]D and F models. The F model dif-
fers from the D in that the former has a larger
passenger compartment and entrance door, and it
is powered by two fuel injection engines. Differ-
ences in performance are noted as appropriate.
b. Characteristics U-8D
(1) Normal cruising speed
(2) Takeoff distance to clear 50-foot obstacle
(3) Landing distance to clear 50-foot obstacle _ _
(4) Endurance at cruising speed
Cargo Compartment
a. U-8D. The TJ-8D has two, three-place seats.
The front seat accommodates the pilot and copilot,
plus one passenger; the rear seat carries three ad-
ditional passengers. The 15-8D has a baggage
compartment in the aft end with a capacity of 300
pounds.
b. T]-8F. The U-8F has separate pilot and
passenger compartments. The passenger com-
partment has five airline-type reclining seats which
are readily removable to convert the aircraft into
a light cargo carrier. The 13-8F also has a 300-
pound baggage compartment aft of the passenger
compartment.
U-8F
155 knots 155 knots.
2,155 feet 2,200 feet.
2,135 feet 2,125 feet.
5 hours, 40 minutes 5 hours, 30 min-
utes.
c. Critical Dimensions.
U-8D U-8F
(1) Cargo compartment: (inches) (inches)
(a) Length
50.5
110%
(b) Width
53%
55
(c) Height
46.7
55
(2) Cargo door:
(a) Width
35
5034
(b) Height
36%
26
Weight and Balance Data
U-8D U-SF
(pounds) (pounds)
a. Maximum gross weight__ _ _
. 7, 300
7,700
b. Normal operating weight _ _
5, 450
5, 950
c. Maximum fuel capacity_
1, 380
1, 380
Figure 6. The U-SF.
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V. CV-2B
Description
a. General. The CV-2B (figure 7) is an ail
metal, high-wing monoplane powered by two 1,450
horsepower reciprocating engines. The aircraft
has a fully retractable tricycle landing gear and a
power-operated cargo door and ramp which, in
conjunction with the up-swept rear fuselage, per-
mits straight-in cargo loading. The CV-2B is a
medium transport and its missions include trans-
port of troops and cargo, air delivery of supplies
and paratroops, and medical evacuation.
b. Characteri,3ties.
(1) Normal cruising speed 157 knots.
(2) Takeoff distance to clear 550 feet.
50-foot obstacle.
(3) Landing distance to clear 740 feet.
50-foot obstacle.
(4) Endurance at cruising 6 hours,
speed. minutes.
(5) Restraint criteria.
(a) Air-landed mission:
/. Forward
8.0
CARIBOU
2. Aft
'2.0
3. Vertical
2. 0
4. Lateral,
1. 5
(b) Air delivery mission:
1. Forward
4. 0
2. Aft
1.5
3. Vertical
2. 0
4. Lateral
1.5
Cargo Compartment
a. Capacity. The CV-2 has a crew of three--
pilot, copilot, and flight, crew chief. The aircraft
is capable of carrying 32 combat-equipped troops,
24 parachutists, or 14 litters plus eight ambulatory
patients.
b. Floor Strength. Bulk loads must not, exceed
1,000 pounds per square foot, while at the same
tune not exceeding 1,200 pounds per running foot.
A running foot is a foot-wide strip extending
across the full width of the cargo floor. Vehicle
loads on the treadways must not exceed '2,000
pomids per wheel during loading and unloading.
This is also the maximum wheel loading on the
treadways forward of station 397.6 during flight.
Figure V. 'The CV-2B.
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On the treadway areas aft, of station 397.6 during
flight, and the remainder of the floor area under
all conditions, the loading must not exceed 1,000
pounds per wheel. Vehicle load limits are based
on a tire pressure of not more than 40 pounds
per square inch. Caution must be taken that lire
pressures do not exceed this value.
c. Critical Dimensions.
(1.) Cargo compartment: inches
(a) Length :145
(b) Width 731/2
(e) Height 75
(d) Height (floor above ground) 151/2
(2) Cargo door:
(a) Width
(b) Height
'731/2
75
ficgrt.c.N
(0) Ramp incline 16
Cargo Loading Provisions
a. Ramp Extensions. Two ramp extensions 120
inches long and 15 inches wide are provided for
each aircraft. When not in use, the extensions are
stored in racks above the cargo door. The d is-
tanc,e between the ramp extensions may be ad-
justed to match the wheel tread of any vehicle to
be loaded.
b. Tiedown Devices. The tiedown devices sup-
plied with each aircraft consist of six MB-1.
chain devices, 20 MC-1 webbing devices, and one
A-2 cargo net.
Air Delivery System
a. Supply Drops. The. CV-2 is equipped for air
delivery of supplies and equipment rigged on
platforms or in containers, using the extraction,
gravity, or manual ejection methods. For spe-
cific information on air delivery of supplies and
equipment from this aircraft, see TM 10-500-
5-series.
h. Personnel Drops. For instructions on
rigging the CV-2 for parachute jumping, see TM
)7-220.
Weight and Balance Data
Pounds
a. Maximum gross weight 28, 500
b. Operating weight_ 19,475
e. Fuel capacity _ 4, 968
d. Allowable cargo load (maximum
fuel aboard) 4,057
Allowable cargo load (50 nautical
mile radius) 7, 500
Allowance cargo load (100 nautical
mile radius) 7, 500
Pig are
g. Center of gravity limits 8
*Allowable cargo load is the same for 50 and 100 nau-
ti..al mile radius of action since this aircraft has a 27,000-
pound zero fuel weight. (Weight of aircraft before fuel
0- added will not exceed 27,000 poun(ls.)
*e.
* f.
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7600
7200
6800
6400-
6000
5600
5200
4800
O ? 4400
3
0
a. 4000
171 ? 3600
O 3200
U^ 2800
2400
2000
1600-
1200
800-
400
0
180 200 220
240
260
280 300
11
320 340 360 380
400 420
FUSELAGE STATION
440
460
480
500
520 540
Figure 8. Cargo center of gravity limits, CV-2B.
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VI. OH-13H SIOUX
Description
a. General. The 011-1311 ( figure 9) is a two-
place helicopter designed for training, observa-
tion, reconnaissance, medical evacuation, and gen-
eral utility missions. It is powered by a 200 horse-
power 0-435 air-cooled engine. This aircraft nor-
mally carries only one passenger seated in the
cockpit beside the pilot. It can also transport two
litter patients in pods mounted on the cross tubes
along each side of the aircraft. Light, critical
cargo may be transported by this aircraft, and it
can lay wire across difficult terrain.
b. Characteristics.
(1) Normal cruising speed__ _ _ 70 knots.
(2) Takeoff distance to clear 250 feet.
50-foot obstacle.
(3) Landing distance to clear 225 feet.
50-foot obstacle.
(4) Endurance at cruising 2 hours,
speed. 30 minutes.
Weight and Balance Data
Pounds
a. Maximum gross weight 2, 450
b. Normal operating weight 1, 941
c. Maximum fuel weight 258
VII. OH-23D RAVEN
Description
a. General. The OH-23D ( figure 10) is a three-
place, multi-purpose helicopter designed for recon-
naissance, training, medical evacuation, and ob-
servation. It is powered by a 245 horsepower
Lycoming 0 435 air-cooled engine. It has a ca-
pability of transporting two persons seated beside
the pilot or two litter patients in pods mounted on
the helicopter landing gear spring tubes. Light,
critical cargo may be transported by this aircraft,
and it can lay wire across difficult terrain.
b. Characteristics.
(1) Normal cruising speed_____ 70 knots.
(2) Takeoff distance to clear Vertical.
50-foot obstacle.
(3) Landing distance to clear Vertical.
50-foot obstacle.
(4) Endurance at cruising 2 hours, 10
speed. minutes.
Figure 9. The OH-13.
Weight and Balance Data
Pounds
a. Maximum gross weight 2, 700
b. Normal operating weight 2, 038
c. Maximum fuel weight 276
Figure 10. The OH-23D.
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VIII. UH-1 IROQUOIS
Description
a. General. The UH-1 (figure 11) is the stand-
ard utility helicopter. It is turbine powered and
features a skid-type landing gear. There are three
models of the UH-1 in the inventory?the A, B,
b. Performance.
and D. Difference between models includes engine
horsepower and size of the cargo compartment.
The UH-1 A and B are used primarily for utility
purposes, such as aerial fire support, medical evac-
uation, and aerial command posts; the ITH-1D is
used as a light tactical transport.
UH-1A
UH-1B
UH-1D
(1) Cruising speed
95 knots
95 knots
95 knots.
(2) Takeoff distance to clear 50-foot obstacle_
110 feet
0 feet
0 feet.
(3) Landing distance to clear 50-foot obstacle _
328 feet
0 feet
275 feet.
(4) Endurance at cruising speed internal
1 hour, 30
1 hour, 30
2 hours, 30
fuel.
minutes.
minutes.
minutes.
165-gallon auxiliary fuel tank
3 hours, 45
3 houts, 45
(Not applica-
minutes.
minutes.
ble).
350-gallon auxiliary fuel tank
(Not appli-
6 hours, 10
(Not applica-
cable).
minutes.
ble).
Figure P. The U11-113.
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Cargo Compartment and Sling
Assembly
a. Capacity. All models of this helicopter have
dual controls, although it is designed for operation
with only a pilot. The seating capacity (to in-
chide the cockpit) is seven persons in the UH-1A,
nine in the UH-1B, and 13 in the UH-1D (fig-
ures 12 and 13). The UH-1 A and B can carry
three litters or deliver five parachutists, while
Figure 12. Cargo compartment, UH-1B.
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the UH-1D can carry six litters or eight para- foot. The external sling load capacity of the
chutists. The cargo compartment floor in all UH-1A. is 3,000 pounds; the sling capacity of the
models has a load limit of 175 pounds per square U11-1 B and D is 4,000 pounds.
b. Dimensions.
U H-1 A
U H-1 B
U H-1 D
(1) Cargo compartment:
(inches)
(inches)
(inches)
(a) Length
48
60
92
(b) Width
8034
92
9734
(c) Height
48
54
49
(d) Height (floor above ground)
26
27
32
(2) Cargo door (one each side):
(a) Width
48
48
92
(b) Height
48
48
49
Figure 13. Cargo compartment, UH-1D.
Weight and Balance Data
a. Maximum gross weight
b. Operating weight
c. Internal fuel weight
d. Allowable cargo load (maximum internal fuel)
e. Allowable cargo load (50-nautical-mile radius)
U H -1 A UH-1B UH-1D
(pounds) (pounds) (pounds)
7,
200
8,
500
8,
4,
243
4,
635
4,
1,
008
1,
008
1,
1,
843
2,
857
2,
2,
202
2,
966
2,
800
889
430
305
582
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IX. UH-19 CHICKASAW
Description
a. General. The UH-19 (figure 14) is a utility
helicopter. The Army has two models of this
aircraft, the C and D. Essentially both models
have the same operational characteristics. It can
be used for movement of personnel, transport of
light cargo, medical evacuation, and parachute
operations. Its principal use under the ROAD
concept is medical evacuation. This aircraft is
programed to endure a wearout period and even-
tually be replaced by a turbine-powered helicopter
such as the UH-1 Bell series.
b. Characteristics.
(1) Normal cruising speed____ 70 knots.
(2) Takeoff distance to clear 50 feet.
50-foot obstacle.
(3) Landing distance to clear 180 feet.
50-foot obstacle
(4) Endurance at cruising speed 2 hours
25 minutes.
Figure 14. The UH-19D.
X. CH-21
Description
a. General. The C1-I-21 (figure 15) is an all
metal, single engine, tandem rotor helicopter.
Power is supplied by an air-cooled, radial engine
located within the fuselage aft of the cargo-passen-
ger compartment. It has dual controls and fea-
tures a fixed tricycle landing gear. Two models
of this aircraft are in the Army inventory, the B
and C models, both having essentially the same
performance characteristics. A. rescue hoist is
available with 100 feet. of cable, the winch having
a 400-pound capacity.
b. Characteri,stics.
(1) Normal cruising speed___ 85 knots.
(2) Takeoff distance to clear 515 feet.
50-foot obstacle
a. Cargo Compartment. The UH-19 is de-
signed for operation by a crew of one, the pilot.
For medical evacuation, or operations under in-
strument conditions, additional crew members
such as a copilot and medical attendant may be
required. The aircraft can transport 10 passen-
gers or six litters internally. The external cargo
book is limited to 2,000 pounds. Five parachutists
can be exited from the aircraft for parachute
operations.
d. Dimension8.
(1) Cargo compartment:
Inehes
(a) Length
120
(b) Width
66
(c) Height
60
(2) Cargo compartment door:
(a) Length
48
(b) Width
48
Weight and Balance Data
a. Maximum gross weight
b. Operating weight
c. Fuel capacity
d. Allowable cargo load (maximum fuel
aboard)
a. Allowable cargo load (50-nautical-mile
radius)
f. Allowable cargo load (100-nautical-
mile radius)
SHAWNEE
Pounds
7, 900
5,850
1, 050
508
1,487
1,073
(3) Landing distance to clear 0 feet.
50-foot obstacle.
(4) Endurance at cruising speed:
(a) Normal operations 3 hours
10 minutes.
(b) Wit. h auxiliary fuel 5 hours
tanks. 10 minutes.
Cargo Compartment
a. Capacity. The CH-21 is designed for a crew
of one, the pilot. The troop-cargo compartment
(figure 16) is capable of transporting 20 combat.
troops, 12 parachutists, or 12 litter patients with
two passengers. The external cargo hook is lim-
ited to 5,000 pounds.
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Figure 15. The CH-21.
Figure 16. Cargo compartment, CH-21C.
b. Cargo Floor. The cargo-passenger compart-
ment is made of prefabricated metal panels with
four cargo rails installed so that heavy cargo can
be slid along without puncturing the panels. There
are 25 cargo tiedown .fittings in the floor. Cargo
tiedown rings, 20 with 2,000-pound capacity and
two with 5,000-pound capacity, are bolted to the
fuselage above the floor on each side of the aircraft..
c. Dimensions.
(1) Cargo compartment: Inehc.s
(a) Length
24
(b) Width 4((:
(c) Height_ 60
(d) Height (floor above ground) 38
(2) Cargo door:
(a) Width 45
(b) Height 59
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Weight and Balance Data
a, Maximum gross weight
h. Operating weight
c. Maximum fuel capacity
Pounag
15, 200
9,251
1, 800
d. Allowable cargo load (maximum fuel
aboard)
e. Allowable cargo load (50- nautical-
mile radius)
4, 125
. CH-34 CHOCTAW
Description
a. General. The 011-31 ( figure 17) is an all
metal, single-engine helicopter with a four-blade
main rotor. It is powered by an R-1820 engine
producing a maximum of 1,125 hoursepower. It
has dual controls and a conventional fixed landing
gear. Entrance to the cabin compartment is
through a single sliding door (53 by 18 inches)
on the right side of the fuselage. Two models, A
and C, of this aircraft are in the Army inventory.
Both models are identical except for installation
of automatic stabilization equipment (ASE) in
the C model. The aircraft is a light cargo heli-
copter designed for transport, of cargo, personnel,
and medical evacuation.
96
1.,gure 17. The CH-34.
b. Characteristics.
Normal cruising speed 80 knots.
"(2) Takeoff distance to clear Vertical.
)0-foot. obstacle.
Landing distance to clear 112 feet.
50-foot obstacle.
) Endurance at cruising 2 hours, 30
speA. minutes.
(5) Restraint criteria:
(a) Forward 4.0
(b) Aft 2.0
(e) Lateral 1.5
(d) Vertical 1.0
4, 749
Cargo Compartment
a. Capacity. The CH-34 is designed for opera-
tions with a crew of one, the pilot. Under normal
circumstances it is operated by a crew of three?
pilot, co-pilot, and flight crew chief. The troop-
cargo compartment (figure 18) will accommodate
18 passengers or eight litter cases with two attend-
ants. Ten parachutists can be exited from the
aircraft. The cargo hook capacity for external
loads is rated at 5,000 pounds. A 600-pound capac-
ity hoist is available for installation for rescue
work. The hoist has a 95-foot cable. The cargo
floor is rated at 200 pounds per square foot for an
evenly distributed load.
Figure 18. Cargo compartmera, CH-34.
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b. Dimensions.
(1) Cargo compartment: Inches
(a) Length 1631/2
(b) Width 59
(c) Height:
Stations 82.5 to 112 19
Stations 112 to 246 70
(d) Height (floor above ground) 34
(2) Cargo entrance door:
(a) Width 53
(b) Height 48
c. Tiedown Devices. There are 35 tiedown rings
in the cargo compartment floor rated at 1,250
pounds each. Ten 1,250-pound fabric cargo tie-
down devices are stowed in pockets along the cargo
compartment side walls.
Weight and Balance Data
Pounds
a. Maximum gross weight 13, 600
b. Operating weight 8,417
a. Fuel capacity 1, 578
d. Allowable cargo load (maximum fuel
aboard) 3,605
e. Allowable cargo load (50-nautical-
mile radius) 4,283
f.
Allowable cargo load (100-nautical-
mile radius) 3,635
XII. CH-37 MOJAVE
Description
a. General. The CH-37 (figure 19) is an all
metal, twin-engine helicopter with a single,
five blade main rotor and a single four-blade
antitorque tail rotor. It is powered by two 2,100
horsepower radial engines. It has dual controls;
retractable, conventional landing gear (two main
wheels and one tail wheel) ; clamshell cargo load-
ing doors and a loading ramp in the nose section
(figure 21). Jettisonable fuel tanks may be
mounted externally to increase the range. There
are two models of this helicopter. The CH-37A
has an adjustable stabilizer mounted on the aft
fuselage section, while the CH-3713 has a fixed-
type stabilizer on the right side of the pylon. The
performance characteristics of the two models are
essentially the same. The C11-37 is a medium
transport helicopter with a principal mission of
transporting troops and cargo. In addition, it can
be used for medical evacuation and parachute
operations.
Figure 19. The CH-37.
h. Characteristics.
(1) Cruising speed 80 knots.
(2) Takeoff distance to clear 316 feet.
50-foot obstacle.
(3) Landing distance to clear 302 feet.
50-foot obstacle.
(4) Endurance at cruising
speed:
Normal operations 1 hour, 20
minutes.
With auxiliary fuel tanks 4 hours, 10
minutes.
(5) Restraint criteria:
(a) Forward
4.0
(b) Aft
2.0
(c) Vertical
2.0
(d) Lateral
1. 5
Cargo Compartment
a. Capacity. The C11-37 is designed for a crew
of three?pilot, copilot, and flight crew chief. The
troop-cargo compartment (figure 20) is capable of
carrying 23 combat-equipped troops, 23 para-
chutists, or 24 litter patients. The external cargo
sling assembly is designed for loads up to 10,000
pounds. A monorail with an electric winch is pro-
vided for cargo loading and rescue operations.
The winch has a capacity of 2,000 pounds; how-
ever, when used for rescue or for lowering person-
nel, the maximum load is GOO pounds.
b. Floor Strength. Except for the treadways,
the cargo floor will support 300 pounds per square
foot during flight and/or loading. The outboard
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treadways between stations 160 and 187 are de-
signed to support a wheel load of 2,575 pounds, an
axleload of 5,100 pounds, or an evenly distributed
load of 1,600 pounds per square foot during flight
and/or loading. Between stations 80 and 160 the
treadways are designed to support these same
loads, except that the evenly distributed Right load
is only 700 pounds per square foot. The inboard
treadways, which extend the entire length of the
cargo compartment, are designed to support (dur-
ing loading) a wheel load of 930 pounds, an axle-
load of 1,860 pounds, or an evenly distributed load
of 950 pounds per square foot. During flight these
treadways will support the same wheel load; how-
ever, the evenly distributed load is limited to 700
pounds per square foot.
c, Critical Dimensions.
Figure 20. Cargo compartment, CH-37.
Figure 21. Loading ramp, CH-37.
(1) Cargo compartment:
(a) Length 364 inches.
(b) Width:
Stations 80 to 298-------- 871/4 inches.
Stations 298 to 444 ___.__._ Tapers
from
871/4
inches to
523/4
inches.
(c) Height:
Stations 80 to 330 -------
Stations 330 to 444
(d) Height (floor above
ground).
(2) Nose cargo door:
(a) Width
(b) Height
(c) Ramp length _
( d) Ramp incline
(3) Right side cargo door:
(a) Width
(b) Height
(4) Floor cargo hatch:
(a) Length
(b) Width
Cargo Loading Provisions
a. Traverse Hoist System. The traverse hoist
system consists of a monorail and an electrically
driven 2,000-pound capacity winth, which is capa-
ble of picking up cargo at the right side door or
through the cargo compartment.
i. Tiedown Devices. There ire 30 MC-1 tie-
down devices stowed in pockets along the side of
the cargo compartment.
811/2 inches.
66 inches.
36 inches.
871/4 inches.
72 inches.
80 inches.
13 degrees.
72 inches.
72 inches.
72 inches.
48 inches.
Weight and Balance Data
Pounds
a. Maximum gross 31,000.
b. Operating weight 22,550.
e. Maximum internal fuel ca.pac- 2,460.
it)'.
d. Allowable cargo load (maxi- 5,990.
mum internal fuel capacty).
e. Allowable cargo load (50- 6,110.
nautical-mile radius).
f. Center of gravity limits________ Figure 22.
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10,000
9000
8000
7000
tc,
? 6000
L
X
171 5000
0
X
^ 4000
3000
2000
1000
0
RAMP LOADING
LIMITATION
80 100 120 140 160 180 200 220 240
FUSELAGE STATIONS?INCHES
Figure 22. Cargo center of gravity limits, CH-37.
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X111. CH-47A CHINOOK
Description
a. General. The CH-47A ( figure 23) is a twin-
engine, tandem rotor, medium transport heli-
copter. It is powered by two 2,200 horsepower
turbine engines mounted on the aft fuselage. The
engines simultaneously drive tandem, three-blade
rotors. The helicopter is equipped with non-
retractable quadricycle landing gear. The CH-
47A has a power operated, rear loading ramp
which permits straight-in loading. The sealed hull
gives the CH-47A an emergency water landing
capability.
b, Characteristics.
(1) Normal cruising speed ] 30 knots.
(2) Takeoff distance to clear 50- Vertical.
foot obstacle.
(3) Landing distance to clear Vertical.
50-foot obstacle.
(4) Endurance at cruising 1 hour, 30
speed. minutes.
(5) Restraint criteria:
(a)
(h)
((fl)
(d)
Cargo Compartment
a, Capacity. The CH-47A normally has a crew
oI three--pilot, copilot, and flight crew chief. The
troop-cargo compartment ( figure 24) is capable of
carrying 33 combat-equipped -troops, 24 para-
chutists, or 24 litters. The exOrnal sling has a
rated capacity of 16,000 pounds. An electric
winch is provided for cargo "aiding and rescue
operations. This helicopter is mpable of inter-
nally transporting the major items of the Pershing
missile system.
b. Floor Strength. The floor area, except for
the treadways, will withstand a load of 200 pounds
per square foot. The treadways aft of station 160
will withstand a wheel load of c2,500 pounds; the
remaining treadway area will withstand a wheel
load of 1,000 pounds. When usx1 for additional
cargo space, the ramp must be positioned level
with the cargo floor and the, load )n the ramp must
not exceed 2,000 pounds.
c. Critical Dimensions.
(1)Cargo compartment:
(a) Length
(b) Width
(c) Height
(d) Height (floor above ground) __ _
2 ) Aft cargo door and ramp (figure
25):
(a) Width
(b) Height
Forward ---
_?-
8. 0
Aft
4. 0
Vertical
8.0
(
Lateral
8.0
(c) Ramp incline_
gigure 23. The CH-47A.
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Inches
366
90
78
30
90
78
Degrees
13
:kW
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Figure 24. Cargo compartment, CH-47A.
Cargo Loading Provisions
a. Auxiliary Loading Ramps. Three auxiliary
,mod
loading ramps are hinged to the aft end of the
ramp. When the ramp is lowered, these auxiliary
ramps provide flush contact between the ramp and
the ground. They may be positioned to accom-
modate various vehicle tread widths or butted
together to facilitate the loading of bulk cargo.
b. Winching System. A 3,000-pound capacity
winch is mounted on the floor in the right hand
forward 'bulkhead. The winch is provided with
150 feet of cable and is capable of winching up to
12,000 pounds of cargo with the aid of snatch
blocks.
c. firoistiug System. The hoisting system is used
for air rescue and aerial loading of light cargo
through the utility hatch in the floor. The hoist
load capacity is limited to 600 pounds.
Weight and Balance Data
Pound8
. Maximum allowable gross weight___ 33,000
b. Normal operating weight 17,154
c. Maximum fuel weight 4,090
d. Allowable cargo load (50-nautical-
mile radius), approximately 13,000
e. Allowable cargo load (100-nautical-
mile radius) *11,756
(*1.00-nautica1-mi1e radius uses 8 minutes of fuel
reserve.)
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Fi;ure 25. Loading ramp, CH-47A.
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mewl
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DESIGN DATA FOR MISCELLANEOUS AIRCRAFT
10
0
C-46F Aircraft Payload-Distance
10
0
5,000-Ft Cruising Altitude
45,000-Lb Max T-0 Wt
1-
? ????
Legend
-
?
Range
? ? Radius
?
?
??
?
????
-,
.6
?
?
?
?
0
400
800 1,200
Nautical Miles
1,600
r-
C-46 Aircraft Cargo-Size Limitations
N? ?
B
3 Ft High
4 Ft High
Box dimensions must be
within limits of this area
.111111=111111111141
rig gralnalill
di. ow la
? - ii timamm
imossimm
Ns 5 F High Irrelpill
.:614.1 1 In ---?--
.:44641111111ri MIMI
11188:Z?%11: 11110311=1
11111111111114"'.""---.....!ISIMIN
ilik Mini --oft
ile I- iwillill IPIIIIIIMMIM
MN NI _ MIIISMOIRIIIIIME II IMP
" ? - Luermiase nue
4
8
12
16
20
Length in Ft
24
28
32
36
Example: To determine whether or not a box 5.5-feet wide, 3-feet high, and 11-feet long can
be loaded through the large cargo door into cargo compartment, locate 5.5 (width) in column
marked "Width in Feet" and trace line horizontally across the graph until it contacts the "3-Feet
High" curve, By dropping a vertical line down to "Length in Feet" at base of the graph, it can
be seen that the cargo door will receive a box 5.5 feet by 3 feet by 11.4 feet. Obviously a box 5.5
feet by 3 feet by 11 feet can be loaded.
Note: This chart is for the C-46F airplane equipped with large cargo door and with troop
benches installed and folded up.
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C-47 Aircraft Mission and Description
The principal mission of ttle C-47 aircraft is the transportation of materiel and personnel,
including paratroops.
A variety of loading pros isions permits transport of engMes, heavy artillery, and other
equipment. Litters may be installed for transportation of casualties.
CAlider tow arrangement b. provided on some airplanes for towing one or more gliders.
Propellers and parapacks may b.? carried underneath the fuselage.
Cargo Clearances
Max load 'See payload.-!isme table Main compartment:
Typical load One 75 torn gun & carriage (8,4m lb) Length (overall) 30.1 ft
or Width (max) 7.4 ft
Engines (on cradles) Height (max) 6.4 ft
lour R-1830 or Main loading door:
'our V-1570 or Height (fwd/aft) 5.9/4.6 ft
Three V-1710 or Width 7.0 ft.
Two R-3350 Height from ground 4.7 ft
ly putt Load (external) Paratrooper door:
,Six Parapacks or Height 9.9 ft
Two 4 blade props Width 2.5 ft
Capacities
Personnel
Maio cargo compartment: Crew (normal) 5
V"Iume (tot) . 1,227 co ft Paratroops (max) 27
Floor area 213 sq ft or
Clider tow 17,700 lb Litters (level) 24
or
Utters (inclined) 18
plus
Attendants 2
1111.1.140
C.47D Aircraft Payload-Distance
15
E 10
0
--
5,000-Ft Cruising Altitude
31,000-Lb Max T-0 Wt
?6sa.6.....11?00?2?911i0
...................
?
? .
?
4.
?
II
. 1
.--,?
0
?
?
?
?
?
?
Legend
?? ?
Range
Radius
?
?
0
500 1,000
Nautical Miles
1,500
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C-54 Aircraft Mission and Description
The principal mission of the C-54 aircraft is to transport personnel, cargo, and combat
equipment.
Fittings are provided for carrying one T-9 tank or one 105-mm howitzer externally. Fittings
for glider tow are incorporated in the tail cone.
The principal mission of the C-54M is to transport troops or cargo to a remote base and
return with wounded personnel.
Casualty-carrying equipment, electric galley, nurse accomodations, and stowage space for
medical supplies are provided.
Cargo
Max cargo See payload-distance table.
Typical items (internal) 105-mm howitzer or engines (on
cradles)
Ten V- 1710or
Seven 12-1820 or
Main compartment:
Length (overall)
Width (max)
I height (max)
Main loading door:
Clearances
49.7 ft
8.C; ft
7.8 ft
Six 12-1830 or
Ileight
5.6 ft
Six R-3350
Width
7.9 ft
Typical Items (external)
Height from grd
8.8 ft
One 105-mm howitzer or
One T-9 tank
Personnel
Crew (normal)5
Capacities*
Max troops
45-49*
Belly compart (fwd & aft)
Boom 4-ioist
12(i cu ft (et)
2,000 lb
Litters (level)
or
32-- q)*
Glider tow (normal)
17,000 lb
Attendants
plus
*Applicable Ti) C-54G.
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C-54G Aircraft Payload-Distance
5,000-Ft Cruising Altitude
69,000-Lb Max 1-0 Wt
Legend
Range
? ? ? Radius
0
30
70
50
50
Maximum
Width
40
30
20
10
800
1,600 2,400
Nautical Miles
3,200
Mil?M.....??????=???????=014. SMI=S?=118111?IMMIN,
C-54M Aircraft Payload-Cistance
0 30
?, 20
0
10
imsm.????????....".
5,000-Ft Cruising Altitude
69,000-Lb Max 1-0 Wt
16,984-Lb Max Ccrgo
?
Legend
xmem Range
?? ? Radius
1,000 2,000 3,000
Nautical Miles
C-54 Aircraft Cargo-Size Limitations
How To Use Chart
To determine whether or not a piece of cargo cc n
be loaded through cargo doorway, measure is
width and length (the two weatest dimension:).
Next, measure its depth. Select correspondiug
numbered lines for width and length on chart. If
lines intersect within chart area and to the left
of the proper depth limit line, the shipment can
be loaded.
Any shipment with a depth of 2 inches or less
Any shipment with a depth of 30 inches or less
Any shipment with a depth of 40 inches or less
Any shipment with a depth of 52 inches or less
0 0 o 0 0 0
VD CO 0 C`l
C?4 C.1
0 0 0 0 0 0 0 0 0 0 0
CO
Co)
Csi
C') sO CO 0
C., 01 sO
'I' Co
C) CV
VI V)
Maximum length in main cargo comportment
----Maximum length in main cargo and fuel-tank compartment
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C-119 Aircraft Mission and Description
The principal mission of the C-119 aircraft is to transport cargo, personnel, litter patients,
mechanized equipment, and/or paratroops.
The cargo compartment is designed to provide ease of loading and unloading; the floor
of the cargo compartment is at approximately truck bed height and the rear cargo doors have
been removed to facilitate air drop of large or bulky cargo. Two metal ramps are provided for
loading mobile equipment.
The monorail system is incorporated for aerial delivery of paracans through doors in the
floor of the cargo compartment.
Cargo
Max load- See payload-distance tables
Typical item- 90-mm AA gun*
(partially dismounted)
*Requires special load-distributing devices.
Main loading door:
Height 8.0 ft
Width 9.2 ft
Height from ground 4.0 ft
Personnel
Capacities
Crew (normal): pilot, copilot, navigator, radio operator, and
crew chief
Main compartment
3,150 cu ft
Troops (normal)
42
Main compartment (tot floor area)
353 sq ft
or
Floor loading
200 lb/sq ft
Troops (max)
62
Ramp strength
9,400 lb ea
Of
Clearances
Litters
plus
35
Attendants
4
Main compartment:
Of
Length (overall)
36.9 ft
Emergency evacuation:
Width (max)
9.8 ft
Troops
62
Width (min)
9.1 ft
plus
Height (max)
8.0 ft
Litters
14
Height (min)
7.9 ft
plus
Height (clear under trolley)
7.7 ft
Attendants
4
C.1 19B Aircraft Payload-Distance
40
30
_a
10
0
5,000-F Cruising Altitude
62,750 Lb Max T-0 Wt
i
Legend
Range
_
? ? ? Radius
-,.
,....???
-,
?..
?,,
-
I,
....
0 500 1,000 1,500 2,000 2,500
Nautical Miles
C-1 19C Aircraft Payload-Distance
Payload ;1,000 Lb)
30
20
10
5,000-Ft Cruising Altitude
66,600-Lb Max 1-0 Wt
Legend
.,....,
I
Range
I
so
? ?
? Radius
-,
%.
%
_
%.
???
-,
?
?
?
?
?
500 1,000 1,500 2,000 2.500
Nautical Miles
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THE TYPE 331 POWERED HELI PORTER
This aircraft is a single engine, high wing,
monoplane capable of transporting personnel and
materiel.
Span
Length
[eight
DIMENSIONS
WEIGHTS
Empty with wheels
With floats, add
With skis, add
Useful load
Maximum for both take-off and landing
Maximum fuel
Pilot
Copilot
Six Passengers
PERSONNEL
CABIN COMPARTMENT
length (pilot's seat to rear cabin wall)
Additional length ( beside pilot's scat)
Width 45.7"
I feight 50.4"
Floor hatch 35.4" x 22.8"
WEIGHTS
Empty 6,176 lbs.
Useful load 1,554 lbs.
Maximum for both take-off and landing 8,730 lbs.
PERSONNEL
49'10"
Pilot
36'
Copilot
36'6"
Five Passengers
RANGE
500 NMI
2,460 lbs.
CABIN
392 lbs.
192 lbs.
Width
Height
52"
(30"
2,390 lbs.
length
96"
4,850 lbs.
Door
38" x 22"
126 US gals.
90.6"
55.1"
SIDE DOORS
( May be located on either or both sides of cabin)
Width 62.2"
Height 41"
Pilot and Copilot Door
Width 22"
Height 45"
THE
( Also known as
This aircraft is
monoplane of all
mission of which
RANGE
400 NMI
BEECH TC-455
the SNB-5 and the USAF' C-45)
a twin engine, low wing, land
metal construction, the principal
is transportation of personnel.
DIMENSION'S
Wing Span
47.7'
Length
34.2'
Height
9.65'
THE BELL MODEL 204B
The Bell Model 204B is a general purpose
helicopter.
DIMENSIONS
Overall length (rotor on) 57'0"
Fuselage length 481"
Maximum width (elevator) 9'4"
Cabin width 8'2"
Overall height 14'6"
Tread 8'8"
WEIGHTS
Basic ( empty ) 4,620 lbs.
Useful load 3,880 lbs.
Gross (certified maximum) Part 7 . 8,500 lbs.
Maximum fuel 240 US gals.
Pilot
Nine Passengers
PERSONNEL
CABIN COMPARTMENT
Cargo Area
I en gth ( overall ) 5'0"
Width ( floor level) 7'8"
Ifeight ( maximum ) 4'8"
Cargo Door Opening
I [eight 4'0"
Width 4'0"
Height above ground 2'4"
Usable Cubilge
Main cargo area 140 Cu. ft.
left side passenger area 20 Cu. ft.
Baggage compartment 30 Cu. ft.
RANGE
300 NMI
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THE DORNIER-WERKE 28A-1
This aircraft is a twin engine, high-wing, mon-
oplane capable of transporting personnel and
mei materiel.
DIMENSIONS
Wing span 46.4'
Length 30.1'
Height 10 4'
WEIGHTS
Empty 3,750 lbs.
Useful load 1568 lbs.
Maximum for both take-off and landing 5,318 lbs.
Maximum fuel 123 US gals.
PERSONNEL
Pilot
Seven Passengers
CABIN COMPARTMENT
Length 11.5'
Luggage compartment 8,8 Cu. ft.
RANGE
450 NMI
THE VOLPAR SUPER TURBO-18
(Modification of BEECH SUPER-18)
This aircraft is a twin engine, low-wing, all
metal, monoplane capable of transporting person-
nel and materiel.
DIMENSIONS
Wing span 46'
Length 37.6'
Height 9.6'
WEIGHTS
Empty 6,220 lbs.
Useful load 3,892 lbs.
Take off 10,286 lbs.
Landing 9,772 lbs.
Maximum fuel 502 US gals.
PERSONNEL
Pilot
Copilot
Nine Passengers
RANGE
1,200 NMI
CABIN COMPARTMENT
Width 52"
Height 67"
Length 96"
Air Stair & Cargo Door Approx. 54"W x or 48"H
THE HELIO STOL SUPER CARRIER
MODEL H-295 (U-10)
This aircraft is a single-engine, high-wing STOL
(short take-off, landing) aircraft capable of trans-
porting personnel and materiel.
DIMENSIONS
Span 39'
Length 31'
height 8'10"
WEI GHTS
Empty 2,010 lbs.
Maximum for both take-off and landing 3,000 lbs.
Maximum pay load 990 lbs.
Maximum fuel 60 US gals.
PERSONNEL
Pilot
Copilot
Four Passengers
CABIN COMPARTMENT
Length 10'3"
Width 3'9"
Height 4'4"
Floor Area 30 sq. ft.
THE PIPER APACHE H
(PA-23-160)
This aircraft is a twin engine, high-wing,
monoplane capable of transporting personnel and
materiel.
DIMENSIONS
Span 37'
Length 27'11/2"
Height 9'6"
WEIGHTS
Empty 2,280 lbs.
Maximum for both take-off and landing 3,800 lbs.
Maximum fuel 72 US gals.
PERSONNEL
Pilot
Copilot
Four to Five Passengers
CABIN COMPARTMENT
Maximum space ? 80 Cu. ft. with the two front scats
installed.
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THE BOEING 727C
This aircraft is a three-engine jet, low-wing air-
craft capable of transporting personnel and materiel.
Crew of Three
DIMENSIONS
THE CONVAIR
CV-880 MODEL 22--M
This aircraft is a four--engine jet, low-wing,
monoplane capable of transporting personnel and
materiel.
Span
,length
108'
133'2"
DIMENSIONS
Span
1
20'
Ileight
34'
Length
129'4"
WEIGHTS
Height
36'4"
Empty
89,394 lbs.
WEIGHTS
Maximum take-off
1.60,000 lbs.
Empty
93,000 lbs.
Maximum landing
135,000 lbs.
Maximum for both take-off and landing
184,500 lbs.
Maximum pay load
38,400 lbs.
Maximum pay load
24,165 lbs.
Maximum fuel
7,680 US gals.
Maximum fuel
12,534 US gals.
PERSONNEL
PERSONNEL
Crew of Three
Crew of Five
One Hundred and Thirteen Passengers
First Class Passengers ? 88;
CABIN COMPARTMENT
OR Coach Class Passengers-- 110
Lene,,th
72'8"
CABIN COMPARTMENT
Width
10'9"
Length
89'3"
Height
7'2"
Width
10'8"
;Floor Area
766 sq. ft.
Height
7'1"
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Staff or Division
Station
Program
Project
GUIDE FOR DETERMINING
ADMINISTRATIVE AND HOUSEKEEPING SUPPORT
REQUIREMENTS
Copy of
Due Date of this Report
Item
No.
Category of Support
Gross Requirements for Period Thru
Supply
Source
Remarks
Quarter
Year
Quarter
Year
Quarter
Year
Quarter
Year
Half
Year
Half
Year
A
B
C
D
E
F
G
H
I
J
1
2
3
4
5
Rations:
Class A-1
Class A-2
Class B-1
Class B-2
Clothing and Equipage:
Class A-1
Class A-2
Class A-3
Class B-1
Class B-2
Class B-3
Commissary & PX Supplies:
Class A-1-1
Class A-2
Class B-2
Office Supplies & Equipment:
Class C-1
Class C-2
Quarters & Messes:
Group I
Group II
Group III
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PREPARATION OF ADMINISTRATIVE AND
HOUSEKEEPING SUPPORT REQUIREMENTS
A. Expendable
1. This category normally includes such items as
food, clothing, commissary and post exchange com-
modities, janitorial supplies and equipment, spare
parts for vehicles, POL (petroleum, oil and lubri-
cants) and office supplies.
2. This portion will reflect administrative and
housekeeping requirements which are based on man
strength, vehicle strength and facility strength.
B. Columnar Entries
1. "Item No.," Column A, and "Category of Sup-
port," Column B
These refer to categories of strength support.
2. Columns C through H
a. Enter requirements in terms of the units
of measure indicated below.
b. These requirements will represent support
required during each respective period and will
not be cumulative:
Category of Support
Items I through 4
Class A-1
Class A-2
Class A-3
Class B-1
Class B-2
Class B-3
Unit of Measure
Average number of United States
nationals to be supported at the
individual's expense.
Average number of United States
nationals to be supported at project
expense.
Number of United States nationals
included in Class A-2 who will re-
quire initial issue of clothing and
equipment.
Average number of personnel other
than United States nationals to be
supported at the individual's ex-
pense.
Average number of personnel other
than United States nationals to be
supported at project expense.
Number of personnel other than
United States nationals included in
Class B-2, who will require initial
issue of clothing and equipment.
Category of Support
Items I through 4 (Coned)
Class C-1
Class C-2
Item 5
Group I
Group II
Group III
Item 6
Class 1
Class 2
Class 3
Class 4
TAB A
to APPENDIX IV
Unit of Measure
Average number of office personnel
who will require recurring replen-
ishment of supplies.
Average number of office personnel
included in Class C-1 who will re-
quire initial issue of office equip-
ment and furnishings.
Number of family dwellings to be
furnished or refurnished. (Specify
grade or rank of principal occu-
pant and note unusual circum-
stances under "Remarks.") The
number of dwellings now on hand,
and furnished, for which attrition
of furnishings is applicable, will be
indicated under "Remarks."
Number of additional bachelors to
be quartered who will require ini-
tial issues of furniture and furnish-
ings. (Specify grade or rank of
principal occupant and note un-
usual circumstances under "Re-
marks.")
Number of messes to be opened
and equipped, followed by num-
bers of persons to be messed: for
example, 1-40 would indicate one
new mess to be opened to accom-
modate forty persons. (Note un-
usual circumstances under "Re-
marks.")
Number of dwellings assigned to
United States personnel and/or de-
pendents.
Average number of persons quar-
tered in BOQ-type accommoda-
tions.
Average number of persons quar-
tered in barracks.
Maximum square feet of warehouse
space, by type, according to the
following code:
W? Wood floor
C ? Concrete floor
T ? Temporary structure
P ? Permanent structure
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Category of Support
items 7, 8 and 9
3. "Supply Source," Column I
For each category of support enter Code DD
as the source of supply. Specify wider Re-
marks" the supporting service (Army, Navy or
Air Force), and indicate the theater command
involved ( for example, PAC OM, EUCOM,
RYCOM).
4. "Remarks," Column J
Enter any additional remarks which may
assist Headquarters in identifying the require-
ments.
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FORMAT FOR A
STANDING OPERATING PROCEDURE
Part I ? Organization and Functions
1. Application: In this section, give the purpose
and scope of the standing operating procedure
( SOP ) and applicability of procedures prescribed.
2. Organization: Show the organization.
3. Function: A general paragraph should explain
the composition of the clement and broad respon-
sibilitics and functions of members.
Part II ? Command-Staff Relationships
Section I. General
1. Command and Technical channels.
2. Dual responsibilities, such as one individual
being both a staff officer and member of task or-
ganization.
3. Responsibility for liaison and coordination
with higher, lower and adjacent elements.
4. Cooperation between staff sections.
Section II. Intelligence
This section outlines responsibilities for and de-
scribes the procedures for all matters pertaining
to intelligence.
Section III. Estimates ? Plans ? Orders
This section outlines the responsibilities for and
describes the procedures for preparation of esti-
mates, plans and orders.
APPENDIX V
Section IV. Security
This section outlines responsibilities for security,
area security and defense and area damage control.
( This may be done by reference to an appropriate
annex in the SOP.)
Section V. Logistics
In this section, detailed procedures should be
given covering supply, transportation, procurement,
real estate and construction, printing, and support
services. This portion is closely related to the
logistics plan ( Annex ) and many aspects covered
in the SOP need not be repeated in the logistics
plan ( Annex ). However, applicable references to
the SOP should be made.
Section VI. Administration
This section should give complete and detailed
procedures pertaining to internal administrative
matters not included elsewhere. Activities such as
the following might be included: leave policy, postal
services, labor, travel, finance, law and order, rec-
ords management, office hours, courier and mes-
senger services, and handling of classified docu-
ments.
Section VII. Command and Communica-
tion
This section covers such activities as special in-
structions and reports not covered in other parts;
also included are communications operations and
standing communications instructions and location
of the headquarters, including alternate headquar-
ters.
Authorized Representative
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GUIDE FOR THE PREPARATION
OF A STAFF STUDY
1. General
Staff studies will be submitted for consideration
by a supervisor when required by him or his rep-
resentative, or when an element prepares one on
its own initiative concerning a subject which is
clearly within its scope of responsibility.
2. Purpose
The purpose of the staff study is to provide the
supervisor with a paper which will assist him in
the consideration of a problem and enable him to
reach a sound decision.
3. Format
To facilitate rapid and logical consideration by
the supervisor on matters placed before him, a
standard format is prescribed which permits an
orderly transition from the problem being con-
sidered to the conclusions reached and the recom-
mendations resulting therefrom. The format at
Tab A ( page 137) should be used for all staff
studies submitted to the supervisor for considera-
tion. The checklist at Tab B (page 139) should be
used to insure proper preparation of the staff study.
4. Principal Parts
The principal parts of the staff study, which are
as follows, are explained in the subsequent para-
graphs:
a. Statement of the Problem
b. Assumptions
c. Facts Bearing on the Problem
d. Discussion
e. Conclusions
f. Recommendations
g. Annexes
h. Attachments
i. Concurrences
APPENDIX VI
5. Statement of the Problem
A proper statement of the problem is one of the
most important sections of the staff study. It is
imperative that the author of the staff study phrase
the statement of the problem in clear and explicit
language which will enable the supervisor to com-
prehend quickly the substance of the problem to
which the staff study is addressed. The problem
to be stated is the one which faces the supervisor,
NOT the problem which faces the author of the staff
study. The following are examples of a proper
statement of the problem:
a. "In response to a request by the supervisor,
to determine whether the Blank Depot should
be retained."
b. "In response to a request by the supervisor,
to develop a policy for the assignment of priori-
ties to requisitions."
6. Assumptions
An assumption is anything taken for granted, a
supposition, or a presumption. Assumptions are
NOT REQUIRED in staff studies but may be in-
cluded at the discretion of the author of the staff
study. Any lengthy presentation of the assump-
tions deemed necessary for a thorough analysis will
be placed in a lettered annex. If an annex is used
for any or all of the assumptions, a paragraph will
be added under this section as follows: "For ( addi-
tional ) assumptions, see Annex
7. Facts Bearing on the Problem
A fact is anything that has actually happened or
is true. This section of the staff study will set forth
a summary of the pertinent facts arranged in logical
sequence to facilitate understanding of the discus-
sion in the next section. THIS SUMMARY WILL
BE FACTUAL AND DEVOID OF THE AU-
THOR'S OPINIONS, ASSUMPTIONS, AND DIS-
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CUSSION. Any detailed presentation of the facts
deemed necessary for a thorough analysis will be
placed in a lettered annex. If an annex is used, a
paragraph will be added under this section as fol-
lows: "For additional facts, see Annex
8. Discussion
This is the section of the staff study where,
'through a logical analysis and evaluation, the facts
bearing on the problem are converted into con-
clusions. Although it is desirable that the discus-
sion be as brief as possible, it should not be cur-
tailed to the extent of omitting consideration of any
essential aspect of the problem. The technique of
stating alternative solutions, the advantages and
disadvantages of each, and the rationale support-
ing the action recommended, should be employed
in those papers which lend themselves to this ap-
proach. ANY PART OR ALL OF THE DISCUS-
SION MAY BE PLACED IN AN ANNEX. In
this instance, a paragraph will be included under
this section as follows: "For ( additional) discussion,
see Annex " If the facts bearing on the
problem are considered to lead directly to the con-
clusions and discussion is considered unnecessary,
the discussion section may be omitted.
9. Conclusions
Ti ie conclusions represent the considered opinions
of the author relative to the problem and provide
the basis for the recommendations.
10. Recommendations
The recommendations will consist of concise
statements of actions to be taken. A specific recom-
mendation must be consistent with the conclusions.
In approving the dispatch of an implementing at-
tachment which reflects the conclusions in a staff
study, the supervisor does, in fact, approve the
conclusions, arid it is unnecessary to make a separate
recommendation that the conclusions be approved.
However, in rare cases, there may be conclusions
which are not reflected in an implementing attach-
ment but which the originator desires to have ap-
proved. In this instance, it is proper to recom-
mend that the supervisor approve these conclusions.
Order of Presentation of Recommendations.
The order of presentation of reccmmendations is
as follows:
( I) Recommendations pertaining to imple-
menting attachments.
( 2) Recommendation pertaining to conclu-
sions ( to be included only if tf:e implementing
attachments do not reflect the conclusions ).
11. Annexes
Information necessary to an understanding of the
problem, but too detailed for inclusion in the staff
study, accompanies the study as lettered annexes.
These must be identified and referred to in the
ASSUMPTIONS, FACTS, or DISCUSSION para-
graphs.
12. Attachments
Memorandums, messages and directives neces-
sary to implement the recommendations, if ap-
proved, are prepared in final form :E'or the signature
of the proper authority and accolipany the staff
study as numbered attachments. These must be
identified and referred to in the RECOMMENDA-
TIONS paragraphs.
13. Concurrences
Concurrences must be secured in writing from
the offices affected by the problem. This is ac-
complished by providing a place at the end of the
staff study for the office title, date and signature
of the concurring officers.
Enclosures:
Tab A -- Format for a
Staff Study
Tab B -- Checklist for a
Staff Study
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TO:
FROM:
SUBJECT:
TAB A
to APPENDIX VI
FORMAT FOR A STAFF STUDY
DATE:
1. PROBLEM
a. Specific and concise statement of problem.
2. ASSUMPTIONS
a. Use only assumptions required for a logical
discussion of problem.
b. Assumptions, while not facts, must have a
basis or foundation of fact.
c. Do not use assumptions when facts are avail-
able.
3. FACTS BEARING ON TIIE PROBLEM
a. List essential facts in logical sequence.
b. List unfavorable as well as favorable facts.
c. List only important facts bearing directly on
problem.
4. DISCUSSION
a. Analyze facts collected for both advantages
and disadvantages.
b. List all feasible solutions to the problem.
5. CONCLUSIONS
a. Eliminate alternate lines of action.
b. State the results (conclusions) derived by a
reasoned judgment of the effects and im-
plications of the essential facts.
6. RECOMMENDATIONS
a. Provide a direct solution.
b. Chart a complete, concise, and clear-cut
course of action permitting simple approval
or disapproval.
Signature
Title
Annexes: (Include detailed supporting information
in succeeding lettered annexes. Refer-
ence must be made to these in body of
study. Staff studies should be complete
without having to read annexes. An-
nexes should only provide correlating and
substantiating information.)
Concurrences: (List here other offices or individ-
uals affected by the problem. Pro-
vide space for date and signature
of concurring officer. When there
is a nonconcurrence, reasons there-
for will be stated and attached as
an annex.)
Action by Approving Authority:
Date
Approved (Disapproved), exceptions, if any.
Signature
Attachments: (Implementing memorandums, mes-
sages, and directives in final form for
the signature of the proper author-
ity.)
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CHECKLIST FOR A STAFF STUDY
1. Statement of the Problem:
a. Did you recognize and isolate the problem?
b. Did you state the problem properly?
2. Assumptions:
a. Are your assumptions things taken for granted,
suppositions or presumptions?
b. Are your assumptions essential to the solution
of the problem?
c. Are your assumptions realistically derived?
3. Facts Bearing on the Problem:
a. Are your facts things that actually happened
or are true?
b. Did you list all pertinent facts?
c. Arc your facts logically arranged?
d. Did you exclude facts which, although true,
have little or no bearing on the problem?
c. Did you exclude facts which are not valid?
f. Did you exclude "facts" which are actually
assumptions?
4. Discussion:
a. Is your discussion in sufficient detail?
b. Does it follow a logical thought sequence?
c. Does it consider the advantages and dis-
advantages of the various courses of action?
d. Does it support your conclusions and recom-
mendations?
c. Does it include facts which should be included
in paragraph 3?
f. Is it brief and to the point?
Does it contain irrelevant material?
g.
5. Conclusions:
a. Are your conclusions in sufficient detail?
b. Do they follow a logical thought sequence?
c. Do they consider the advantages and dis-
advantages of the various courses of action?
d. Do they support your discussion and recom-
mendations?
c. Do they include facts which should be in-
cluded in paragraph 3?
f. Are they brief and to the point?
g. Do they contain irrelevant material?
6. Recommendations:
a.
b.
TAB B
to APPENDIX VI
Do your recommendations offer a clear op-
portunity for decision?
Do your recommendations
from your conclusions?
c. Are your recommendations complete?
d. Are your recommendations beyond the
of the problem?
Did you include material in your recom-
mendations which should have been presented
earlier in your study?
Did you unnecessarily repeat discussion ma-
terial in your action recommended?
7. Annexes:
a. Is supporting but detailed information placed
in an annex?
b. Are the annexes referred to and identified in
the ASSUMPTIONS, FACTS, or DISCUS-
SION paragraphs of the staff study?
8. Attachments:
a. Are implementing attachments (memoran-
dums, messages, and directives) included as
attachments in final form for the signature of
the proper authority?
b. Arc the attachments referred to and identified
in the RECOMMENDATIONS paragraph?
9. General:
a. Is the meaning of the words used clear?
b. Arc the sentences too long and involved?
c. Can the thought be easily followed from
sentence to sentence and from paragraph to
paragraph?
d. Is each paragraph limited to one "thought"?
e. Does each paragraph contain a topic sentence?
f. Does the writing have force?
g. Is the level of abstraction too high (use of
words, examples, and quotations which do not
evoke concrete thoughts)?
h. Is the style consistent and easy to
i. Is proper credit given for sources
j. Is spelling accurate?
k. Have the rules of punctuation been followed?
derive logically
C.
f.
scope
read?
used?
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APPENDIX VIII
STANDARD REFERENCE LIST
This appendix contains a recommended list of Organization and standard military references
for logistics planning. It is not all-inclusive, and users of this Guide should consult appropriate
military indexes for additional references in researching a staff problem, or as requirements exist.
FM 3-5
FM 3-8
FM 5-13
FM 5-25
FM 5-31
FM 5-34
FM 5-35
FM 7-24
FM 8-10
FM 8-55
FM 9-1
FM 9-2
FM 10-10
FM 10-60
FM 10-64
FM 11-20
FM 19-15
FM 20-15
FM 23
FM 27-10
FM 31-8
FM 31-10
FM 31-11
FM 31-12
FM 31-15
FM 31-16
FM 31-20
FM 31-21
FM 31-22
FM 31-25
Dept. of Army Publications
Chemical, Biological and Radiological ( CBR ) Operations
Chemical Corps Reference Handbook ( Change 1)
The Engineer Soldier's Handbook
Explosives and Demolitions
Use and Installation of Booby Traps ( Changes 1 & 2)
Engineer Field Data
Engineers Reference and Logistical Data
Communications in Infantry and Airborne Divisions
Medical Services, Theater of Operations ( Changes 1 & 2)
Army Medical Service Planning Guide ( Changes 3 & 4)
Ordnance Service in the Field
Ordnance Corps Logistical Data
Quartermaster Service in a Theater of Operations ( Change 1)
Supply of Subsistence in a Theater of Operations ( Change 1)
Quartermaster Class II and IV Supply in Theaters of Operations
Signal Operations, Theater of Operations (Change 1)
Civil Disturbances and Disasters
Pole and Frame Supported Tents
Weapons Series
The Law of Land Warfare
Medical Services in Joint Overseas Operations
Barriers and Denial Operations
Doctrine for Amphibious Operations
Army Forces in Amphibious Operations ( The Army Landing Force) ( Change 1)
Operations Against Irregular Forces
Counterguerrilla Operations
Special Forces Operational Techniques ( Changes 1 & 2)
Guerrilla Warfare and Special Forces Operations ( Change 1)
US Army Counterinsurgency Forces
Desert Operations
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UM 31-30 jungle Operations
UM 31-50 Combat in Fortified and Built-up Areas
FM 31-60 River-crossing Operations (Change 1)
FM 31-70 Basic Cold Weather Manual (Change 1)
FM 31-71 Northern Operations
FM 31-72 Mountain Operations
FM 33-5 Psychological Operations
FM 38-1 Logistics Supply Management (packaging and shipping of materials)
FM 38-5 Logistics Maintenance Management
FM 41-10 Civil Affairs Operations
FM 54-1 The Logistical Command (Changes 1 & 2)
FM 55-6 Transportation Services in Theaters of Operations
1.,'M 55-31 Motor Transportation Service in Theaters of Operations
FM 57-10 Army Forces in joint Airborne Operations
I.A1 57-35 Airmobile Operations
FM 57-38 Pathfinder Operations
FM 60-30 Embarkation and Loading, Amphibious
FM 100-5 Field Service Regulations ? Operations ( Change 1)
FM 100-10 Field Service Regulations Administration ( Change 1)
FM 100-20 Field Service Regulations ? Counterinsurgency
FM 101-5 Staff Officers Fielt Manual; Stall Organization and Procedures
FM 101-10 Organization Technical and Logistical Data Parts I, II, and III
FM 101-31-1 Staff Officers Field Manual; Nuclear Weapons Employment
TC 5-9 Near Infrared Night Vision and Detection Equipment and its Application
DA. Pamphlet Military Publications: Index of Administrative Publications
310-1
D,A. Pamphlet Military Publications: Doctrinal, Training and Organizational Publications
310-3 ( Change 2)
DA Pamphlet Military Publications: index of Technical Manuals, Technical. Bulletins, Supply
310-4 Manuals, Supply Bulletins, Lubrication Orders, and Modification Work Orders
DA Pamphlet Military Publications: Index of Training Aids and Devices
310-5
DA Pamphlet Military Publications: Index of Supply Manuals: Signal, Types 1, .2, 3, and 10
310-21
DA Pamphlet Military Publications: Index of Supply Manuals: Transportation Materiel
310-22
DA Pamphlet Military Publications: index of Supply Manuals: Engineer Type Items (Change 1)
310-25
DA Pamphlet Military Publications: Index of Supply Manuals: Ordnance Corps (Change 3)
310-29
DA Pamphlet Military Publications: Index of Supply Manuals: Quartermaster Corp; (Change 1)
310-30
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Dept. of Air Force Publications
AFM 1-1 USAF Basic Doctrine
AFM 66-1 Maintenance Management
AFM 66-12 Vehicle Management and Maintenance
AFM 67-1 USAF Supply Manual ( Vol. I-VT, IX, & XX)
AFM 67-3 Storage and Materials Handling
AFM 68-3 Defense Yard Handbook
AFR 71-6 Preservation, Packaging, Packing, and Marking Policy and Equipment
AFM 71-4 Packaging and Handling of Dangerous Materials for Transportation by Military
Aircraft
AFM 88-12 Fuel Storage and Distribution
AFM 88-18 Storage
AFM 88-54 Air Force Civil Engineer Handbook
AFM 146-4 Standard B Ration for the Armed Forces
AFM 160-20 Administration of Medical Treatment Activities
AFM 160-27 Medical Service in Joint Overseas Operations
AFP 67-2-3 Supply Management Handbook for AF Commanders
AFR 0-2 USAF Numerical Index of Administrative Publications
AFR 400-3
AFR 400-6
AFR 400-15
Air Force Specification Bulletin
Interservice Exchange of Logistics Research Information
Military Assistance Sales
Logistic Support U. S. Non-Governmental, Non-Military Agencies and Individuals
in Overseas Military Commands
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