CABLE FROM (Sanitized)

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP89B00980R000300060034-9
• Release Decision: RIPPUB
• Original Classification: S
• Document Page Count: 3
• Document Creation Date: December 15, 2016
• Document Release Date: August 22, 2003
• Sequence Number: 34
• Publication Date: December 19, 1964
• Content Type: CABLE

Approved For.Release 2004/05/43 : CIA-RDP89B00980R000300060034-9
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OXCART
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1, FSW NBR 629 DISTRIB3UTION.T1
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ABSOLUTE NEED TO KNOWe
AREA SERVICED
3 ARTICLE 124 E'VADE' GO 280 ON 17 DEICE MAX ALT. 430s MAX MACH:
1.25 DURATION: 2:000 FURPOSEZ DRIVER TRAIT III?G0 NO ENGINE PROBLEMS.
Al. ARTICLE 1*32 MADE GO 28 ON 1i DECQ MAX ALT: 7501Mq MAX
MACH: 2.75 9 TOGW 115Kg CU R T) ON: 1:359 FUPP OSE: DATA COLLECTION.
?
DURING ACCELERAT IOW AND CY? RISE BOTH EP-IVES ?ECUIPIED A LOT CIF TIM
MINES IN A RIGHT TUPP THE K:iOPT. SHOCK POPPED. INILET : ECOVERED
AUTOMAT ICALL a Burr READ TO RECYCLE POWEP LEVER TO OBTAIN AB REL ICHT
IN DESCENT THE LEFT ENGINE BLEED LIGHT Fl.,ICXERED BUT THIS IS SUS-
FECTED TO BE CAUSED BY SWITCH ADJUSTMENT.
3. ARTICLE
1.21 MADE GO 157 ON 17 DECO
TOGW JCA.3K, MAX MACH:
2'0839 MAX ALT: ?2M9 DUPATIONs a o !3v PURPOSE: FCF0 AT 2.4 MN AND
DURING CRUISE DRIVER REPORTED SLIGHT ROUGHNESS- W}{FN BYPASS DOORS
USAF review(s) cjRWRIfo
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MESSAGE LIMITED T? THOSE WITH
Re1gape @004/#5/1'3: CIA-RD 9130
YhCtUOE:> V2004 AJTO.
$ATIC 0SWN4RAOIN2
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 Approved For Release 2004/05/13 CIA-RDP89B0098OR000300060034-9
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(IN 636329 PAGE TWO
WERE OPENED FOR DESCENT ROUT-PNESS SMOOTHED OUT, DUPING DESCENT AT
10`3 MMN, MILITARY POWER AD WAS EXPERIENCED ON RIGHT ENGINE, POWER
LEVER.: WAS RETARDED AND AD CLEANED JUST BELOW MILITARY POSITION, NO
OTHER ENGINE PROBLEMS ENCOUNTFRED,
6. ARTICLE 131 MADE GO 32 ON 17 DEC. TOGW 1R`509K, MAX MACH:
3,H4, MAX ALT: 82M, DURATION: 1:RP, PURPOSE: SYSTEM C TEST AND
INLET PERFORMANCE. JUST AFTER STARTING ENGINES NOZZLE INSTABILITY
WAS ENCOUNTERED ON THE RIGHT ENGINE AT IDLE. NOZZLE ONN LEFT ENGINE
WAS UNSTABLE WHILE TRIMMING AT THE HEAD OF RUNWAY. NOZZLE INSTABILITY
WAS EXPERIENCED ON BOTH FNGINFS DURING FLIGHT WHEN POWEP LEVERS WERE
BELOW MILITARY POSITION FOR DECELERATION, ON DOWN WING LEG OF
TRAFFIC PATTERN, NOZZLE INSTABILYTY ON RIGHT ENGINE WAS PLUS OR MINUS
5 DECREES WITH POWER LEVER BETWEEN IDLE AND `"ILITPRY0, IT DOES NOT
APPEAR THAT THE NOZZLE INSTABILITY CAUSED A MAJOR PROBLEM AS
SUBJECT ARTICLE IS SCHEDULED TO FLY PC-AIN 1g DEC.
7. ARTICLE 130 MADE GO 61 ON 17 DEC, TOOW 118K, MAX MACH: 2,93.
MAX ALT: 78M9 DURATION: 2:rfl, PURPOSE: TRAINING MISSION. ON PCCFL-
EFATION POPPED RIGHT SHOCK AT 2.,5 MN AND AS BLEW OUT. INLET PRE-
COVERED IN AUTO BUT WHEN POWER LEVER WAS RECYCLED FOR AB LIGHT
RIGHT SHOCK POPPED AGAIN, RECYCLED POWER LEVER AND OBTAINED A
NORMAL LIGHT. DURING P DECELERATION BETWEEN 2.F AND 20 6 "1014T
SHOCK WAS POPPED AGAT4. T4IS TIME SHOCK WAS SMOOTHED MANUALLY,
LATER' WHEN FORWARD BYPASS DOORS CLOSED BOTH SHOCKS POPPED, DOWN
TPIMMED ENGINES AND NO MORE POPPED SHOCKS, MADE ONE PIP TO AIP
PF.FUFLING, WHILE TAXIING ON FUEL FROM TANKER BOTH ENGINES WERE
UP TRIMMED TO ~~ o~ F~ el~a~ %2B9 1 OC P ~ q g0003AO O34-9
 Approved For Release,2004/05/13: CIA-RDP89B . 00980R000.300060034-9
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S E C R E T
(IN 63632) PAGE THREE
COMING OFF TANKEP WITH AFTERSURNEOS OF ?eT?S WERE 92M DEGREES,
DRIVER STARTED TO DOWN TRIM ENGINES BUT HIS ATTENTION WAS
DIVERTED TO TUNING THE RADIO. WHEN INSTRUMENTED PANEL WAS
MONITORED AGAIN LEFT EGT WAS 96P DEPPEFSO DRIVER ESTIMATEt
THAT LEFT EGT WAS AT 96? DECREES FOR ONE WINiTTE, MISSION WAS
ABORTED DUE TO THE OVERTEMP CONDITION, ENGINE SIN 237 WILL BE
REMOVED FOR AN OVERTEMP INSPECTION,
13o ARTICLE 127 CURRENTLY ON CO 96 AS OF 18 DECEMBER, DETAILS
NEXT F Sot ,
9, ARTICLE 124 ON SCHEDULED 00. DETAILS NEXT FSW,
END OF MESSAGE
Approved For Release 2004/05/13 : CIA-RDP89B0098OR000300060034-9