SYNOPSIS
CH-47-94-ASAM-05 AVIATION SAFETY ACTION MESSAGE, MAINTENANCE MANDATORY,
CH-47D, MH-47D, MH-47E, ONE TIME INSPECTION OF THE 5000
POUND TIE-DOWN RECEPTACLE ASSEMBLIES AND PROVIDE INSTRUCTIONS
TO CORRECT DEFECTIVE TIE-DOWN RECEPTACLE ASSEMBLIES P/N
114S2893, (TB 1-1520-240-20-71).
251350Z APR 94, LYELL MYERS, AMSAT-C-XS, X2258.
NOTE: Enter a "Q" + <CR> to exit or <SPACEBAR> to view
the entire message. (REPORTING)
.
01 16 251350Z APR 94 PP PP
:
FROM
:CDRATCOM ST LOUIS MO//AMSAT-C-XS//
TO
:AIG 6713
:AIG 9004
:AIG 8708
:AIG 9042
:DEFARM CAMPBELL AS//DAVN-A//
:DEFARM CANBERRA AS//DOR-A//
:DEFNAV CANBERRA AS
:CDRUSARDSG CANBERRA AS
:LOGCON OTTAWA CAN//DTHEM 6-2//
:EGYPT AF FMS CAIRO EG//ED-MA//
:USOMC CAIRO EG//AV//
:ODC ATHENS GR//ODCSA//
:CDR4THBN228THAVN SOTO CANO HO//AVN-AMO//
:CHJUSMAG SEOUL KOR//MKAR//
:HQROKA TAEJON KOR//DCSLOG-AVIATION/ROKA-AVIATON//
:ROK ARMY FMS PUSAN KOR//ALC-LSD-L//
:CDR160TH SOAR FT CAMPBELL KY//AOAV-SI//
:CDRBGAD RICHMOND KY//SDSBG-GC//
:USDAO RABAT MO//AF//
:CHUSAS RIYADH SA//ASAV//
:ODC MADRID SP//ASM//
:AIT TAIPEI TW
:CJUSMAG THAI BANGKOK TH//MAGTAR-FS//
:CDRUSARDSG LONDON UK//AMXSN-UK-SE//
:ODC LONDON UK
INFO
:CDRAMCCOM ROCK ISLAND IL//AMSAR-QAS-P//
:CDRAMC ALEXANDRIA VA//AMCMR/AMCCS/AMCSM-WAA//
XMT
:USDAO DHAKA BG
:USDAO RANGOON BM
:USDAO COLOMBO CE
:USDAO SUVA FJ
:OMADP JAKARTA ID
:DSA NEW DELHI IN
:USDAO ANTANANARIVO MA
:CDRATCOM ST LOUIS MO//AMSAT-C-XS//
:SAO KUALA LUMPUR MY
:USDAO KATHMANDU NP//SAO//
:USDAO SINGAPORE SN
ACCT
:
TEXT
:UNCLAS
SUBJECT - AVIATION SAFETY ACTION MESSAGE, MAINTENANCE MANDATORY, RCS
CSGLD-1860(R1), CH-47D, MH-47D, MH-47E, ONE TIME INSPECTION OF THE
5000 POUND TIE-DOWN RECEPTACLE ASSEMBLIES AND PROVIDE INSTRUCTIONS TO
CORRECT DEFECTIVE TIE-DOWN RECEPTACLE ASSEMBLIES P/N 114S2893
(CH-47-94-ASAM-05) (TB1-1520-240-20-71).
NOTE - THIS IS AN AVIATION SAFETY ACTION MESSAGE ISSUED PER AR 95-3,
CHAPTER 5 REVISION VIA MESSAGE HQ AVSCOM, AMSAV-XSOF, 181900Z SEP 90,
SUBJECT: CHANGE TO AR 95-3, CHAPTER 5, SAFETY OF FLIGHT MESSAGES.
THIS MESSAGE HAS NOT BEEN TRANSMITTED TO UNITS SUBORDINATE TO
ADDRESSEES. ADDRESSEES SHOULD IMMEDIATELY RETRANSMIT THIS MESSAGE TO
ALL SUBORDINATE UNITS, ACTIVITIES OR ELEMENTS AFFECTED OR CONCERNED.
THE RETRANSMITTAL SHALL REFERENCE THE MESSAGE. ACTION ADDRESSES WILL
IMMEDIATELY VERIFY THIS RETRANSMISSION TO COMMANDER, ATCOM, ATTN -
AMSAT-C-XS (SOF COMPLIANCE OFFICER).
1. PRIORITY CLASSIFICATION -
A. AIRCRAFT IN USE - UPON RECEIPT OF THIS MESSAGE THE CONDITION
STATUS SYMBOL OF THE CITED AIRCRAFT WILL BE CHANGED TO A RED
HORIZONTAL DASH //-//. THE RED HORIZONTAL DASH //-// MAY BE CLEARED
WHEN THE INSPECTION OF PARA 8 BELOW IS COMPLETED. THE AFFECTED
AIRCRAFT SHALL BE INSPECTED AS SOON AS PRACTICAL BUT NO LATER THAN
THE TASK/INSPECTION SUSPENSE DATE. FAILURE TO COMPLY WITH THE
REQUIREMENTS OF THIS MESSAGE WITHIN THE TIME FRAME WILL CAUSE THE
STATUS SYMBOL TO BE UPGRADED TO A CIRCLED RED //X// FOR THE 5000
POUND TIE-DOWN RECEPTACLES ONLY.
B. AIRCRAFT IN DEPOT MAINTENANCE - SAME AS PARA 1A. AIRCRAFT
WILL NOT BE ISSUED UNTIL COMPLIANCE WITH THIS ASAM HAS BEEN
COMPLETED.
C. AIRCRAFT UNDERGOING MAINTENANCE - SAME AS PARA 1A.
AIRCRAFT WILL NOT BE RELEASED UNTIL COMPLIANCE WITH THIS ASAM
MESSAGE HAS BEEN COMPLETED.
D. AIRCRAFT IN TRANSIT -
(1) SURFACE/AIR SHIPMENT - PRIOR TO FIRST FLIGHT.
(2) FERRY STATUS -
(A) INSPECT AT FINAL DESTINATION.
(B) THOSE AIRCRAFT THAT HAVE A DD250 AND ARE AT BOEING
HELICOPTER COMPANY WILL BE INSPECTED PRIOR TO FERRY TO FINAL
DESTINATION.
E. MAINTENANCE TRAINERS (CATEGORY A, B AND C) - COMPLY
WITHIN 30 DAYS OF RECEIPT OF THIS MESSAGE.
F. COMPONENT/PARTS IN STOCK INCLUDING WAR RESERVES AT ALL
LEVELS (DEPOT AND OTHERS) - NOT APPLICABLE TO DEPOT. UNITS WILL
PERFORM INSPECTION PRIOR TO INSTALLATION IN AIRCRAFT. TM CHANGES
WILL REFLECT THIS INSPECTION.
2. TASK/INSPECTION SUSPENSE DATE - WITHIN 10 HOURS/14 DAYS.
3. REPORTING COMPLIANCE SUSPENSE DATE - NO LATER THAN 16 MAY
93 PER PARA 14A OF THIS MESSAGE.
4. SUMMARY OF PROBLEM -
A. TWO INCIDENTS HAVE BEEN REPORTED OF CREW MEMBERS SAFETY
HARNESS BECOMING UNSECURED FROM THE 5000 POUND TIE-DOWN RECEPTACLE
P/N 114S2893 WHEN THE TIEDOWN ADAPTER BECAME UNSCREWED FROM THE
TIE-DOWN FITTING. UPON LANDING, THE TIE-DOWN FITTING AND ADAPTER
WERE VISUALLY INSPECTED, AND IT WAS FOUND THAT THE TIE DOWN ADAPTER
HAD UNSCREWED FROM THE RECEPTACLE RETAINING BUSHING. THERE WAS NO
EVIDENCE OF SEALANT ON THE ADAPTER STUD THREADS WHICH IS REQUIRED TO
KEEP THE FITTING FROM UNSCREWING. ADDITIONAL INVESTIGATION
REVEALED THAT THE EXACT CAUSE OF THE PROBLEM WAS MISSING MIL-S-
22473 SEALANT COATING ON THE RETAINING BUSHING THREADS, AND SEIZURE
OF THE BUSHING DUE TO PAINT OVERSPRAY, ALLOWING THE TIE-DOWN RING TO
UNSCREW ON ROTATION.
B. THE PURPOSE OF THIS MESSAGE IS TO DIRECT A ONE TIME
INSPECTION OF THE 5000 POUND TIE-DOWN RECEPTACLE ASSEMBLIES AND
PROVIDE INSTRUCTIONS TO CORRECT DEFECTIVE TIE-DOWN ASSEMBLIES.
5. END ITEMS TO BE INSPECTED - ALL MH-47D, CH-47D AND MH-47E
AIRCRAFT. SERIAL NUMBERS 81-23381 THROUGH SUBSEQUENT. AIRCRAFT
SERIAL NUMBERS 92-00308 AND SUBSEQUENT WILL BE INSPECTED/CORRECTED
BY CONTRACTOR DURING PRODUCTION AND THEREFORE RECORDS FOR AIRCRAFT
SERIAL NUMBERS 92-00308 AND SUBSEQUENT WILL NOT REQUIRE
IDENTIFICATION OF THIS ACTION.
6. ASSEMBLY COMPONENTS TO BE INSPECTED - N/A
NOMENCLATURE PART NO. NSN
TIE-DOWN RECEPTACLE ASSY 114S2893-6 1670-00-410-5920
TIE-DOWN RECEPTACLE ASSY 114S2893-13 1670-00-410-5919
7. PARTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
TIE-DOWN RING (ADAPTER) 114S2801-1 N/A
22622-51 N/A
TIE-DOWN BUSHING 114S2828-1 N/A
8. INSPECTION PROCEDURES -
INSPECT THE 5000 POUND TIEDOWN RING ASSEMBLY IN CABIN FLOOR AND RAMP
FOR SERVICEABILITY AS FOLLOWS:
A. ROTATE THE RING ASSEMBLY BY HAND IN BOTH DIRECTIONS.
B. IF RING CANNOT BE ROTATED BY HAND, THE ASSEMBLY IS SUSPECT
AND MUST BE REPAIRED OR REPLACED.
C. ATTACH A SPRING SCALE TO THE TIEDOWN RING AND APPLY 5 POUNDS
OF FORCE IN AN UPWARD DIRECTION. WHILE MAINTAINING THE TENSION ON
THE SCALE, ROTATE THE RING ASSEMBLY 10 COUNTER-CLOCKWISE TURNS. IF
THE RING STARTS TO UNSCREW, OR SCREWS OUT OF THE RETAINING BUSHING,
PROCEED TO PARA 9 FOR THE CORRECTIVE PROCEDURES.
9. CORRECTION PROCEDURES -
NOTE
THE 5000 POUND TIE-DOWN ASSEMBLIES ARE ATTACHED TO RAIL ASSEMBLIES.
THE TIE-DOWN ASSEMBLIES CONSIST OF A RECEPTACLE, RING ADAPTER, AND
BUSHING. THE ASSEMBLY IS ATTACHED TO BEAM ASSEMBLIES BY RIVETING THE
RECEPTACLE TO THE BEAM. THE BEAM IS SECURED TO THE AIRCRAFT MAIN
FLOOR BEAMS BY FOUR SCREWS IN THE BOTTOM OF EACH RECEPTACLE.
A. IF SUSPECT RING ASSEMBLIES ARE LOCATED ON THE LEFT OR RIGHT
OUTBOARD BL 44 BEAMS PROCEED AS FOLLOWS:
(1) REMOVE FLOOR PANELS ADJACENT TO THE SUSPECT RING.
CAUTION
TO PREVENT DAMAGE TO THE FLOOR SUPPORT BEAM, INSERT A WOODEN BLOCK,
OR A PIECE OF PHENOLIC BETWEEN THE RECEPTACLE AND THE FLOOR SUPPORT
BEAM WHEN DRILLING OUT RECEPTACLE RIVETS.
(2) DRILL OUT RIVETS ATTACHING THE RECEPTACLE TO THE
BEAM ASSEMBLY.
(3) REMOVE THE TIE-DOWN ASSEMBLY FROM THE BEAM.
(4) SECURE THE BUSHING WITH A SUITABLE TOOL AND REMOVE
TIE-DOWN RING AND BUSHING FROM THE RECEPTACLE.
WARNING
METHYL-ETHL-KETONE IS FLAMMABLE AND TOXIC. IT CAN IRRITATE SKIN AND
CAUSE BURNS. USE ONLY WITH ADEQUATE VENTILATION, AWAY FROM HEAT OR
OPEN FLAME. AVOID CONTACT WITH SKIN, EYES, OR CLOTHING. IN CASE OF
CONTACT, IMMEDIATELY FLUSH SKIN OR EYES WITH WATER FOR AT LEAST 15
MINUTES. GET MEDICAL ATTENTION FOR EYES.
(5) CLEAN THE RING ADAPTER THREADS, AND BUSHING THREADS
USING A WIRE BRUSH AND CLEANING SOLVENT (METHYL-ETHYL-KETONE).
WARNING
SEALANT MIL-S-22473 IS FLAMMABLE AND TOXIC. IT CAN IRRITATE SKIN AND
CAUSE BURNS. USE ONLY IN A WELL VENTILATED AREA, AWAY FROM HEAT AND
OPEN FLAME. IN CASE OF CONTACT, IMMEDIATELY FLUSH SKIN OR EYES WITH
WATER FOR AT LEAST 15 MINUTES. GET MEDICAL ATTENTION FOR EYES.
(6) COAT THE THREADS OF THE ADAPTER AND BUSHING WITH
PRIMER ACTIVATOR MIL-S-22473 GRADE T, USING A BRUSH (MIL-B-23958).
WEAR GLOVES (MIL-G-10902). ALLOW THE PRIMER ACTIVATOR TO AIR DRY FOR
A MINIMUM OF FIVE MINUTES PRIOR TO APPLICATION OF SEALANT.
(7) COAT THE THREADS OF THE ADAPTER AND BUSHING WITH
SEALANT MIL-S-22473 USING A BRUSH (MIL-B-23958). WEAR GLOVES
(MIL-G-10902).
(8) REINSTALL THE TIE-DOWN RECEPTACLE ASSEMBLY PER TASK
2-206, STEPS 2 THROUGH 5. ENSURE THAT THE BUSHING IS COMPLETELY
THREADED ONTO THE RING ADAPTER. LOCKING SURFACES SHALL BE COVERED
WITH SEALANT AS EVIDENCED BY A CONTINUOUS FILLET AT THE PARTING LINE
OF THE BUSHING AND ADAPTER. REMOVE EXCESS SEALANT. ALLOW THE
SEALANT TO CURE FOR ONE HOUR AT 70 DEGREES F OR ABOVE AND 24 HOURS
AT 40-70 DEGREES F.
(9) REINSTALL THE CABIN FLOOR PANEL PER TASK 2-207.
B. IF SUSPECT RING ASSEMBLIES ARE LOCATED ON THE INBOARD
BEAM ASSEMBLIES PROCEED AS FOLLOWS:
(1) REMOVE FLOOR PANELS ON THE LEFT AND RIGHT HAND SIDES OF
THE ENTIRE LENGTH OF THE TIE-DOWN BEAM ASSEMBLIES.
(2) REMOVE THE FOUR SCREWS AT THE BOTTOM OF EACH OF THE
TIE-DOWN RECEPTACLES, AND THE SCREWS AT EACH ATTACHING END OF THE
BEAM ASSEMBLY.
(3) REMOVE THE BEAM ASSEMBLY FROM THE AIRCRAFT.
(4) SECURE THE BUSHING WITH A SUITABLE TOOL AND REMOVE
TIE-DOWN RING AND BUSHING FROM THE RECEPTACLE.
WARNING
METHYL-ETHL-KETONE IS FLAMMABLE AND TOXIC. SEE WARNING IN PARA 9A4.
(5) CLEAN THE RING ADAPTER THREADS, AND BUSHING THREADS
USING A WIRE BRUSH AND CLEANING SOLVENT (METHYL-ETHYL-KETONE).
WARNING
SEALANT MIL-S-22473 IS FLAMMABLE AND TOXIC. SEE WARNING IN PARA 9A5.
(6) COAT THE THREADS OF THE ADAPTER AND BUSHING WITH
PRIMER ACTIVATOR MIL-S-22473 GRADE T, USING A BRUSH (MIL-B-23958).
WEAR GLOVES (MIL-G-10902). ALLOW THE PRIMER ACTIVATOR TO AIR DRY FOR
A MINIMUM OF FIVE MINUTES PRIOR TO APPLICATION OF SEALANT.
(7) COAT THE THREADS OF THE ADAPTER AND BUSHING WITH SEALANT
MIL-S-22473 USING A BRUSH (MIL-B-23958). WEAR GLOVES (MIL-G-10902).
(8) REINSTALL THE TIE-DOWN RECEPTACLE ASSEMBLY PER TASK
2-206, STEPS 2 THROUGH 5. ENSURE THAT THE BUSHING IS COMPLETELY
THREADED ONTO THE RING ADAPTER. LOCKING SURFACES SHALL BE COVERED
WITH SEALANT AS EVIDENCED BY A CONTINUOUS FILLET AT THE PARTING LINE
OF THE BUSHING AND ADAPTER. REMOVE EXCESS SEALANT. ALLOW THE
SEALANT TO CURE FOR ONE HOUR AT 70 DEGREES F OR ABOVE AND 24 HOURS AT
40-70 DEGREES F.
(9) REINSTALL THE BEAM ASSEMBLIES IN THE AIRCRAFT.
(10) REINSTALL THE CABIN FLOOR PANELS PER TASK 2-207.
C. IF SUSPECT RING ASSEMBLIES ARE LOCATED ON THE RAMP,
PROCEED AS FOLLOWS:
(1) REMOVE THE AFFECTED RAMP FLOOR PANEL PER TASK 2-247.
(2) SECURE THE BUSHING WITH A SUITABLE TOOL AND REMOVE
TIE-DOWN RING AND BUSHING FROM THE RECEPTACLE.
WARNING
METHYL-ETHL-KETONE IS FLAMMABLE AND TOXIC. SEE WARNING IN
PARA 9A4.
(3) CLEAN THE RING ADAPTER THREADS, AND BUSHING
THREADS USING A WIRE BRUSH AND CLEANING SOLVENT (METHYL-ETHYL-
KETONE).
WARNING
SEALANT MIL-S-22473 IS FLAMMABLE AND TOXIC. SEE WARNING
IN PARA 9A5.
(4) COAT THE THREADS OF THE ADAPTER AND BUSHING WITH
PRIMER ACTIVATOR MIL-S-22473 GRADE T, USING A BRUSH (MIL-B-23958).
WEAR GLOVES (MIL-G-10902). ALLOW THE PRIMER ACTIVATOR TO AIR DRY FOR
A MINIMUM OF FIVE MINUTES PRIOR TO APPLICATION OF SEALANT.
(5) COAT THE THREADS OF THE ADAPTER AND BUSHING WITH SEALANT
MIL-S-22473 USING A BRUSH (MIL-B-23958). WEAR GLOVES (MIL-G-10902).
(6) REINSTALL THE TIE-DOWN RECEPTACLE ASSEMBLY PER TASK
2-206, STEPS 2 THROUGH 5. ENSURE THAT THE BUSHING IS COMPLETELY
THREADED ONTO THE RING ADAPTER. LOCKING SURFACES SHALL BE COVERED
WITH SEALANT AS EVIDENCED BY A CONTINUOUS FILLET AT THE PARTING LINE
OF THE BUSHING AND ADAPTER. REMOVE EXCESS SEALANT. ALLOW THE
SEALANT TO CURE FOR ONE HOUR AT 70 DEGREES F OR ABOVE AND 24 HOURS AT
40-70 DEGREES F.
(7) REINSTALL THE RAMP FLOOR PANEL PER TASK 2-249.
10. SUPPLY/PARTS AND DISPOSITION -
A. PARTS REQUIRED - ITEMS CITED IN PARAGRAPHS 6 AND 7
MAY BE REQUIRED TO REPLACE DEFECTIVE ITEMS.
B. REQUISITIONING INSTRUCTIONS -
REQUISITION REPLACEMENT PARTS THROUGH NORMAL SUPPLY CHANNELS
USING NORMAL SUPPLY PROCEDURES. ALL REQUISITIONS SHALL USE
PROJECT CODE "XAL" PER THIS MESSAGE.
NOTE
PROJECT CODE "XAL" IS REQUIRED TO TRACK COSTS AND ESTABLISH
A DATA BASE OF STOCK FUND EXPENSE INCURRED BY THE FIELD AS A
RESULT OF ASAM/SOF ACTIONS.
C. BULK AND CONSUMABLE MATERIALS -
NOMENCLATURE NSN
PRIMER ACTIVATOR MIL-S-22473 GRADE T 8030-00-082-2508
SEALANT MIL-S-22473 8030-00-081-2340
CLEANING SOLVENT METHYL-ETHYL-KETONE
TT-M-261 6810-00-281-2785
BRUSH MIL-B-23958 7920-00-051-4384
GLOVES MIL-G-10902
ZINC CHROMATE PRIMER TT-P-1757 8010-00-297-0593
D. DISPOSITION - N/A.
E. DISPOSITION OF HAZARDOUS MATERIAL - IN ACCORDANCE WITH
ENVIRONMENTAL PROTECTIVE AGENCY DIRECTIVES AS IMPLEMENTED BY YOUR
SERVICING ENVIRONMENTAL COORDINATOR (AR 200-1).
11. SPECIAL TOOLS, JIGS AND FIXTURES REQUIRED - N/A.
12. APPLICATION -
A. CATEGORY OF MAINTENANCE - AVUM. AIRCRAFT DOWNTIME
WILL BE CHARGED TO AVUM.
B. TIME REQUIRED -
(1) TOTAL OF 2 MANHOURS USING 1 PERSON.
(2) TOTAL OF 2 HOURS DOWNTIME FOR ONE END ITEM.
C. ESTIMATED COST IMPACT OF STOCK FUND ITEMS TO THE
FIELD -
D. TB/MWOS TO BE APPLIED PRIOR TO OR CONCURRENTLY WITH THIS
INSPECTION - TM 55-1520-240-23-2 WILL BE CHANGED TO INCLUDE THIS
INSPECTION. A COPY OF THIS MESSAGE MAY BE INSERTED IN THE
APPROPRIATE MANUAL UNTIL THE PRINTED CHANGE IS RECEIVED.
E. PUBLICATIONS WHICH REQUIRE CHANGE AS A RESULT OF THIS
INSPECTION - N/A.
13. REFERENCES -
A. TM 55-1520-240-23-1, AVIATION UNIT AND INTERMEDIATE
MAINTENANCE MANUAL, CH-47D HELICOPTER, DTD 10 MAY 93, C48 30 JUL 93.
B. TM 55-1520-240-23P, AVIATION UNIT AND INTERMEDIATE
MAINTENANCE REPAIR PARTS AND SPECIAL TOOLS LIST (INCLUDING DEPOT
MAINTENANCE REPAIR PARTS AND SPECIAL TOOLS), CH-47D HELICOPTER, DTD 1
NOV 89.
14. RECORDING AND REPORTING REQUIREMENTS -
A. REPORTING COMPLIANCE SUSPENSE DATE (AIRCRAFT) - UPON
ENTERING REQUIREMENTS OF THIS MESSAGE ON DA FORM 2408-13-1 ON ALL
SUBJECT MDS AIRCRAFT, FORWARD A PRIORITY MESSAGE, DATAFAX OR E-MAIL
TO COMMANDER, ATCOM, ATTN: AMSAT-C-XS (SOF COMPLIANCE OFFICER), PER
AR 95-3. DATAFAX NUMBER IS DSN 693- 2064 OR COMMERCIAL 314/263-2064.
E-MAIL ADDRESS IS "AMSATCXS (AT SIGN) ST-LOUIS-EMH4.ARMY.MIL". THE
REPORT WILL CITE THIS MESSAGE NUMBER, DATE OF ENTRY IN DA FORM
2408-13-1, THE AIRCRAFT MISSION DESIGN SERIES AND SERIAL NUMBERS OF
AIRCRAFT IN NUMERICAL ORDER.
B. TASK/INSPECTION REPORTING SUSPENSE DATE (SPARES) - AVIM/AVUM
UNITS AND OTHERS HOLDING STOCK UPON COMPLETION OF THIS INSPECTION
SHALL FORWARD A PRIORITY MESSAGE REPORT OF RESULTS OF THIS INSPECTION
TO LOGISTICAL POC BELOW NLT 15 DAYS AFTER RECEIPT OF THIS MESSAGE.
THE REPORT SHALL INCLUDE QUANTITY ON HAND, QUANTITY WHICH PASSED
INSPECTION AND QUANTITY WHICH FAILED INSPECTION.
C. THE FOLLOWING FORMS ARE APPLICABLE AND ARE TO BE COMPLETED
IN ACCORDANCE WITH DA PAM 738-751, 15 JUN 92 -
(1) DA FORM 2408-13, AIRCRAFT STATUS INFORMATION RECORD.
(2) DA FORM 2408-13-1, AIRCRAFT INSPECTION AND
MAINTENANCE RECORD.
(3) DA FORM 2408-15, HISTORICAL RECORD FOR AIRCRAFT.
15. WEIGHT AND BALANCE - N/A.
16. POINTS OF CONTACT -
A. TECHNICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. MIKE
WRIGHT, AMSAT-R-ECC, DSN 693-3550 OR COMMERCIAL 314/263-3550.
B. LOGISTICAL POINT OF CONTACT FOR THIS MESSAGE IS MR.
NORM HUSTON, SFAE-AV-CH-L, DSN 693-1415 OR COMMERCIAL 314/263-1415.
C. FORMS AND RECORDS POINT OF CONTACT FOR THIS MESSAGE IS MS.
ANN WALDECK, AMSAT-I-MDM, DSN 693-1758 OR COMMERCIAL 314/263-1758.
D. SAFETY POINT OF CONTACT FOR THIS MESSAGE IS MR. LYELL
MYERS, AMSAT-C-XS, DSN 693-2258 OR COMMERCIAL 314/263-2258.
E. FOREIGN MILITARY SALES (FMS) RECIPIENTS REQUIRING
CLARIFICATION OF ACTION ADVISED BY THIS MESSAGE SHOULD CONTACT
MW5 JAY NANCE/MR. RON VAN REES, AMSAV-I-IA, DSN 693-3826/3659
OR COMMERCIAL 314/263-3826/3659.
F. AFTER HOURS CONTACT ATCOM COMMAND OPERATIONS CENTER
(COC) DSN 693-2066/7 OR COMMERCIAL 314./263-2066/7.