RELOCATE APN-135 BEACON

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP89B00980R000200180071-6
• Release Decision: RIPPUB
• Original Classification: K
• Document Page Count: 2
• Document Creation Date: December 14, 2016
• Document Release Date: October 16, 2002
• Sequence Number: 71
• Publication Date: May 3, 1962
• Content Type: FORM

Approved For Release 2002/10/31 : CIA-RDP89B0098OR000200180071-6
ENGINEERING STUDY El
LOCIIF.? AIRCRAFT CORPORATICIR
127
_
CHANGE PROPOSAL
"0
DATE MAY 3, 1962
AFFECTS : WSPO PROJECT
NAME OF MAJOR COMPONENT
PART OR LOWEST SUBASSEMBLY
PART NO. & MODEL OR TYPE
TITLE OF PROPOSAL :
RELOCATE x_135 BRAOM
NATURE OF PROPOSAL:
SEE PAGE 2
REASON FOR PROPOSAL
TO PROVIDE Ct NCURRIT USE OF SYSTEM AND APN-135 BEACCl=
ESTIMATED COST AND TIME INVOLVED
ES
ADDITIONAL FUNDING REQUIRED :
ESTIMATED COST FOR KITS OR PARTS : See Page 2
C P
ADDITIONAL FUNDING REQUIRED Y (sP_1923)
ST
ITEMS AFFECTED BY PROPOSAL
SAFETY
MISSION
EFFEC.
PERFORM-
ANCE
OPERATING
PROCEDURE
INTER-
CHANGE.
WEIGHT OR
WEIGHT &
TOOLS &
SUPPORT
MAINTE-
NANCE
SERVICE
LIFE
FLIGHT
MANUAL
MAINTE.
NANCE
TIVENESS
ABILITY
BALANCE
EQUIPMENT
PROCEDURE
MANUAL
D
?
`^
^
D
?
^
^
^
?
Cl
EST. MAN/HRS. RFQ'D. TO ACCOMPLISH CHANGE IN FIELD
SOURCE OF PARTS FOR KIT
AVAILABILITY WEEKS AFTER APPROVAL
LAC
See Page 2
DISPOSITION OF SPARES AFFECTED c991~169929~ 0994169930 AND 0994169931
S
Waveguides No Longer Used
INITIATED BYAppro~B~TRelease 2002/10/31 : -Cl
- 'f0098' 20
180071-6
XSG 992+
PROJECT
CGe IA
T
AT
 Approved For Release 2002/10/31 : CIA-RDP89B00980F~0 Q180071-6
Page 2 of 2
STAT
NAT[fl E OF PROPOSAL
1. Relocate APN-135 from R. H. cheek to a position in the top ARS fairing
between P.S. 437 and 465 aft of present engine access door. Refair
pod to extend aft to F.S. 469.5.
2. Revise and re-identify beacon to provide new mounting base and wave
guide coupler. Relocate the beacon antenna to F.S. 465 and install new
wave guide. Incorporate associated wiring changes to accomodate relocated
beacon.
4.
Re-install System VI brackets in the R. H. cheek.
Prepare and issue a Service Bulletin and fabricate the necessary kits.
Work to be accomplished at the factory along with incorporation of
rudder pedal rework and VOR installation.
SCHEDULE
To be determined by Customer and Contractor at a later date.
Time required - 1st aircraft - 5 weeks
2nd aircraft - 3 weeks
Approved For Release 2002/10/31 : CIA-RDP89B0098OR000200180071-6