SUMMARY REPORT ART 342 ACCIDENT

Document Type: 
Collection: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP74B00447R000100010003-8
Release Decision: 
RIPPUB
Original Classification: 
S
Document Page Count: 
3
Document Creation Date: 
December 12, 2016
Document Release Date: 
February 5, 2002
Sequence Number: 
3
Case Number: 
Publication Date: 
March 23, 1966
Content Type: 
CABLE
File: 
AttachmentSize
PDF icon CIA-RDP74B00447R000100010003-8.pdf289.09 KB
Body: 
25X1A Approve ,.,NIT MD UXT 25X1A AF' 23 IKAR 66 25t IDEALISt LOGS MAIN'T CLASSIFIED ME SA E ease' 02N6I1 ff : CTA P SUBJECTS SUMMARY REPORT ART $42 ACCIDRNT NARRATIVE: ART 342 WAS LAUNCHED 25 FED FOR A PRACTICE ';F REFUELI MISSION, NINE BOOR-UPS WERE ACCOMPLISHED AT AIR. AT NO TIME DID THE ARTICLE ENTER AIRCRAFT TURBULENCE, COMPLETION OF T ITT HOOK-UP (ALA. DRY) A BREAK AWAY WAS NSTITt1?1' THE ART DROPPED BRCS AND MOVED TO TIM RIGHT OF THE TAN IA.W TA DOCTAINL ART TEEN ACCT LERATZD AND TOOK UP A POSITION ON LIB WX'` THE TAI WO COCKPITS TO THE RIGHT AND SLIGHTLY, HIGHER, AIRSPE 25X1A AT TES,TIME 'PAS BETWEEN 210 AND 220 ZABL FM LOAD WA$ PAX At1LY IN AUX 'IANJ B AND SUMP, AFTER ABOUT A MINUTE A CLIMB WAS INITIA`' FOLL0' BY A RIGHT TtRL AT T8lS POINT THE LIFT .HIS FAI RAT -in ROOT AND THE AIRCRAFT DISINTB A'#EDa THE PILOT SUCCESSFULLY E 2. FINDINGS: THE INVESTIGATION DISCLOSED INAD'PERTEN" CW '1USS OF 'SIB AIRCRAFT PRIMARY STRUCTURE IN A ROLLING PU -UP v91, Se IT 13 .mss WORTS' TIT PILOT STA'D slT RELEASING OFFrc idT RXIIPUT WT /, 6W-i6P R iWi "003-8 L J $A aE OORI G Approved Foel se 2002/06/18: CIA-RDP74B0 UNI1 SECRET 2 EXT 3 CATS. 4, 5 TO PAGE 2 11 -000 ROUTINE !!- ERTIOF.;}\ IMMEDIAT IN XNAL MAXEU! R WERE SIGNIFICANTLY LESS 7W THOSE NO" Y DESTRIVB FORCES CAN BE APPLIED N' R} D AT TAKE-OFF, THIS IS UNDERSTANDABLE WHERE ,CO tOL FORCES ARC SMOOTHLY APPLIED: AND SERVES TO UNDERLINE THE EASE WITH rill q THE AIMP 'D WAS WELL WITHIN THE LIMITS OF TEE A11 C *YT I T$ DIAGRAM o T iIS IS TRUE BUT COGNIZANCE M T , + , : FACT THAT THE PUBLISHED STRENGTH. DIACR3AM A'SSUM$S SY .7RI CAL LOANING OF THE AIRCB4PTa A ROLLING PULL-UP MANEUVER CULTS IN #SS rEI AL WADING 1 IC$ MAY REDUCE TM STRENGTH RNYEL IPE AY Ab" l UCR AS 33 PERCENT. (THIS IS AN APPROXIMATE FIGURE TO BE FURT REF D 25X1A BY 0 4. ACTION BEING TAZEN: A. ALL PILOTS, WILL RECEIVE ADDITIONAL INSTRUCTION REOA DING 25X1A GBT/$'I NG Pte' 8 IN MANEUVERS WITH PARTIAL, FUEL ,LOADS . I WO RE6ARDING STRUCTURAL LIMITS WHILE MENEU i,ING P7 APROPRI 8,. WILL PROVIDE MUI,E DEFINITIZED FIGHT CQO 1NA~TiNG OFFF!Lm SECRET FILER GA I i(tG ut * 1 rE4 ~,i.-7Hi}NTI pprove {or &e F ~p u Ri F (ease 00 M/11 . &=F~DP7 ~~044 I OUVT b 003-8C~'"'' ; c ORtG trXT DATE. S 0 INFO BE) OF MSAGE IIrgaIOBa ACAPMA S E C E E T 25X1A RpproRv oOrr.Release lj/0j 18 `~ ~A=R~P7 B0 4t1 b~D b'0~?I 103-8 00100010003-3p' ROUTINE RELEA N o t__ - AUTHENTICA ~. MESSAGE ` Approved Fot' eIease 2002/06/18 CIA-RDP74BOO