CABLE FROM (Sanitized)

• Document Type: CREST
• Collection: General CIA Records
• Document Number (FOIA) /ESDN (CREST): CIA-RDP89B00980R000300060058-3
• Release Decision: RIPPUB
• Original Classification: S
• Document Page Count: 2
• Document Creation Date: December 15, 2016
• Document Release Date: August 22, 2003
• Sequence Number: 58
• Publication Date: December 16, 1964
• Content Type: CABLE

Approved For Release 2004105/13 : CIA-RDP89B00980R000300060058-3
185 0Z 16 DEC 64
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25X1A
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E C R E 1 7
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LD I/1 1. FSW NBR 625 DISTRIBUTION, tH{:tS MESSAGE- LIMITED TO THOSE
WITH ABSOLUTE NEED TO KNOWS
25X1A 2.
FROM AREA SERVICE.
3. NO FL IGHZS--kCCOMPL ISHED ON 14DECEMBER .
/ARTICLE NO 124 MADE GO 278. ON `15 DECEMBER. MAX ALT 43MMm1MMAA
CC
MACH 1.3 DURATION 1:10 PURPOSE, DRIVER TRAINING, NO ENGINE PROBLEMS.
5. ARTICLE 121 PRESENTLY HAVING R irNGINE (219) REPLACED BY
206. ENGINE .219 BEING REMOVED FOR INVEST IGATION OF STALL CONDITION
ENCOUNTERED DURING GO NER 156 PER FSW NBR. ,624.
6, ARTICLE 122 MADE GO 83 ON :15 DECEMBER, MAX ALT 7405 MAX MACH
25X1A
2.84 TOGW 109.6K DRIVER DURATION 1:02 PURPOSE? PERFORMANCE
AND ENGINE RE-LITE. NO TRIM PRIOR TAKEOFF AND NONE USED DURING FLIGHT.
EGT ? S FOLLOWED THE OPERATING BAND-PRETTY WELL. THE RH ENGINE 256
WAS SHUTDOWN AT 2.0 MN THEN IMMEDIATELY RE.-LIT.: SOME INLET
ROUGHNESS ENCOUNTERED BUT ENGINE RE-Li*Tg ABILITY WAS NOT AFFECTED.
USAF review(s)
completed.
Approved F
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 Approved For Release 2004/05/13 : CIA-RDP89B0098OR000300060058-3
25X1A
25X1A 7. ARTICLE 129 MADE GO 79 ON 15 DECEMBER. MAX ALT 78M MAX MACH
3.14 TOGW 121.8K DURATION 1:16 PURPOSE, PERFORMANCE.
NO TRIMMING PRIOR TO TAKEOFF,, SOME ON EACH SIDE DURING FLIGHT.
DURING TURN AT OUTBOUND END bF COURSE HAD SOME LEFT HAND NOZZLE
FLUCTUATION. AFTER THE TURN LEFT ENGINE STALLED AND EGT NOTED AT
94 0 DEGREES C. REDUCED POWER TO MILITARY AND BELOW TO BRING EGT
DOWN AND CLEAR THE STALL. RE-ADVANCED POWER TO A/B AND THEN NOTED
37,0910 PPH FUEL FLOW ON LEFT ENGINE-AND NOZZLE IN FULL OPEN POSITION.
REDUCED POWER TO IDLE AND NOTED LEFT FUEL FLOW AT 10,000 PPH SO
SHUTDOWN LEFT ENGINE AND RETURNED HOME ON RIGHT ENGINE. PRELIMINARY
INVESTIGATION FOLLOWING LANDING REVEALED BROKEN LINE IN EXHAUST
NOZZLE MANIFOLD OF THE "CLOSED" CIRCUIT. FURTHER DETAILS PENDING
ENGINE REMOVAL AND SHOP INSTPECTION,
8. ARTICLE 131 MADE GO 30 ON 15 DECEMBER. MAX ALT 47M MAX MACH
25X1A
1.45 TOGW 105K
DURATION 58 MINUTES PURPOSE,
RADIO PACKAGES. HAD SOME FLUCTUATION OF LEFT HAND EXHAUST NOZZLE
PRIOR TO TAKEOFF WHICH CLEARED AND NOZZLE THEN REPORTED AS OK
FOR ENTIRE FLIGHT. NO OTHER PROBLEMS.
Approved For Release 2004/05/13 : CIA-RDP89B0098OR000300060058-3