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:AIG 8881
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:USMILGP BUENOS AIRES AR//ARMY AND AF SEC//
:DEFAIR MATERIAL CANBERRA ACT AS//DAAP-AF//
:CDRUSARDSG CANBERRA ACT AS//AMXIP-AS//
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TEXT
:UNCLAS
SUBJECT - AVIATION SAFETY ACTION MESSAGE, MAINTENANCE MANDATORY,
RCS CSGLD-1860(R1), ALL CH-47D, MH-47D, AND MH-47E AIRCRAFT,
FORWARD AND AFT LONGITUDINAL CYCLIC TRIM YOKE BUSHING INSPECTIONS
AND AIRCRAFT MAINTENANCE MANUAL CHANGES, (CH-47-99-ASAM-04),
(TB 1-1520-240-20-109).
NOTE
THIS IS AN AVIATION SAFETY ACTION MESSAGE ISSUED IAW AR 95-1,
CHAPTER 6, 1 SEP 97. 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 ADDRESSEES WILL IMMEDIATELY VERIFY
THIS TRANSMISSION TO CDR, AMCOM, ATTN: AMSAM-SF-A (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 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 RED //X//.
B. AIRCRAFT IN DEPOT MAINTENANCE - AIRCRAFT WILL NOT BE
ISSUED UNTIL COMPLIANCE WITH THIS ASAM HAS BEEN COMPLETED.
C. AIRCRAFT UNDERGOING MAINTENANCE - AIRCRAFT WILL NOT BE
RELEASED UNTIL COMPLIANCE WITH THIS ASAM HAS BEEN COMPLETED.
D. AIRCRAFT IN TRANSIT -
(1) SURFACE/AIR SHIPMENT - PRIOR TO FIRST FLIGHT.
(2) FERRY STATUS - SAME AS PARA 1A.
E. MAINTENANCE TRAINERS (CATEGORY A/B) - SAME AS PARA 1A.
F. COMPONENT/PARTS IN STOCK AT ALL LEVELS (DEPOT AND OTHERS)
INCLUDING WAR RESERVES - N/A.
G. COMPONENTS/PARTS IN WORK (DEPOT LEVEL AND OTHERS) - N/A.
2. TASK/INSPECTION SUSPENSE DATE - WITHIN NEXT 10 FLIGHT HOURS
OR 14 DAYS.
3. REPORTING COMPLIANCE SUSPENSE DATE - NO LATER THAN 6 APRIL
1999 IAW PARA 14A OF THIS MESSAGE.
4. SUMMARY OF PROBLEM -
A. TWO INSTANCES HAVE BEEN REPORTED OF BUSHINGS BEING LEFT
OUT DURING INSTALLATION OF LONGITUDINAL CYCLIC TRIM (LCT) YOKES.
THE FIRST WAS CORRECTED BEFORE ANY DAMAGE OCCURRED. THE SECOND
INSTANCE RESULTED IN DAMAGE TO THE YOKE ASSEMBLY MOUNTING LUG ON
THE FORWARD TRANSMISSION. A REVIEW OF THE MAINTENANCE MANUAL
CONFIRMS THAT TWO BUSHINGS (PART NUMBERS NAS75-20-206 AND NAS75-
20-123) ARE NOT SUFFICIENTLY REPRESENTED IN THE TEXT OR DIAGRAMS.
(1) FORWARD LCT YOKE ASSEMBLY: IN TM 55-1520-240-23,
TASK 11-217, STEP 5.1, ITEM 9.1 IS INSTALLED (BUSHING, TM 55-1520-
240-23P, FIGURE 372, ITEM 78, PART NUMBER NAS75-20-206). PRIOR TO
CHANGE 22 IN TM 55-1520-240-23, THIS PART WAS NOT REPRESENTED IN
THE ASSOCIATED DIAGRAM. AS A RESULT, THIS BUSHING WAS OMITTED
BECAUSE IT WAS CONFUSED WITH THE PRESS-FIT SLEEVE BUSHING ON THE
TRANSMISSION HOUSING (TM 55-1520-240-23P, FIGURE 180, ITEM 22,
PART NUMBER 145D0121-14).
(2) AFT LCT YOKE ASSEMBLY: IN TM 55-1520-240-23, TASK
11-233, STEPS 7 AND 8 HAVE OMITTED THE INSTALLATION OF THE SLEEVE
BUSHING (TM 55-1520-240-23P, FIGURE 137, ITEM 135, PART NUMBER
NAS75-20-123). AS A RESULT, THE SLEEVE BUSHING WAS NOT
INSTALLED.
B. FOR MANPOWER, DOWNTIME AND FUNDING IMPACTS SEE PARA 12.
C. THE PURPOSE OF THIS MESSAGE IS TO: INSPECT BOTH FORWARD
AND AFT LCT YOKE ASSEMBLIES TO INSURE PROPER BUSHING
INSTALLATIONS AND ANNOTATE CHANGES TO THE MAINTENANCE MANUALS.
5. END ITEMS TO BE INSPECTED - ALL CH-47D, MH-47D, AND MH-47E
AIRCRAFT.
6. ASSEMBLY COMPONENTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
YOKE ASSEMBLY 145C3050-3 1560-01-116-4203
COVER ASSY, UPPER 145D1302-9 1615-01-112-5875
YOKE ASSEMBLY 114C3043-6 1615-00-115-4718
BEAM ASSEMBLY 114S4119-60 N/A
7. PARTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
SHAFT, SHOULDERED 145C3051-1 3040-01-116-4323
BUSHING NAS75-20-206 3120-01-156-7812
SHAFT 114C3044-2 1560-00-868-8468
BUSHING, SLEEVE NAS75-20-123 3120-00-159-7016
8. INSPECTION PROCEDURES -
A. INSPECT BOTH THE FORWARD AND AFT LCT YOKE ASSEMBLIES TO
CONFIRM THE INSTALLATION OF THE BUSHING (PART NUMBER NAS75-20-
206), AND SLEEVE BUSHING (PART NUMBER NAS75-20-123). VISUAL
INDICATIONS THAT THE BUSHINGS HAVE NOT BEEN INSTALLED ARE RADIAL
MOVEMENT OF THE SHOULDERED SHAFT AND/OR NO GAP BETWEEN THE LCT
YOKE AND THE WASHER ON THE SHAFT HEAD.
B. IF THESE INSPECTIONS DO NOT CONFIRM THE INSTALLATION OF
THE BUSHINGS, THE FOLLOWING MAINTENANCE PROCEDURES SHOULD BE
PERFORMED: DISASSEMBLE IAW TM 55-1520-240-23, TASKS 11-212 AND/OR
11-227 OR TM 1-1520-252-23, TASK 11-230 AND/OR 11-245.
C IF THE INSPECTION CONFIRMS INSTALLATION OF THE
BUSHING (PART NUMBER NAS75-20-206), AND SLEEVE BUSHING (PART
NUMBER NAS75-20-123), NO FURTHER ACTION IS REQUIRED FOR THIS LCT
YOKE. REASSEMBLE IAW TM 55-1520-240-23, TASK 11-217 AND/OR 11 -
233 OR TM 1-1520-252-23, TASKS 11-235 AND/OR 11-251 SHALL BE
PERFORMED.
D. IF EITHER BUSHING IS NOT INSTALLED, CONTACT THE TECHNICAL
POINT OF CONTACT FOR THIS MESSAGE FOR FURTHER INSPECTION
INSTRUCTIONS.
9. CORRECTION PROCEDURES -
A. ANNOTATE THE FOLLOWING CHANGES TO TM 1-1520-252-23, TASK
11-230, REMOVE FORWARD LCT YOKE:
(1) DELETE STEP 11.
(2) ADD THE FOLLOWING NOTE AFTER STEP 10: "ENSURE THAT
SLIDER BUSHING (21) IS NOT REMOVED AND REMAINS IN THE YOKE MOUNT
(20)."
B. ANNOTATE THE FOLLOWING CHANGES TO TM 1-1520-252-23, TASK
11-235, INSTALL FORWARD LCT YOKE:
(1) ADD THE FOLLOWING NOTE PRIOR TO STEP 3:"ENSURE THAT
THE SLIDER BUSHING(31) REMAINS IN THE YOKE MOUNT (10)."
(2) ADD THE FOLLOWING WARNING AFTER STEP 5: "FLIGHT
SAFETY PARTS. THIS IS AN INSTALLATION CRITICAL FLIGHT SAFETY
PART. ALL ASPECTS OF ITS ASSEMBLY AND INSTALLATION MUST BE
ENSURED. ENSURE THAT THE SLIDER BUSHING (31) IS RETAINED IN THE
MOUNT LUG (10). "
C. ANNOTATE THE FOLLOWING CHANGE TO TM 1-1520-252-23, TASK
11-245, REMOVE AFT LCT YOKE: ADD THE FOLLOWING NOTE AFTER STEP
13: "ENSURE THAT SLIDER BUSHING (28.1), NOT SHOWN IN THE
ACCOMPANYING DIAGRAM, IS NOT REMOVED AND REMAINS IN THE SUPPORT
(29)."
D. ANNOTATE THE FOLLOWING CHANGE TO TM 1-1520-252-23, TASK
11-251, INSTALL AFT LCT YOKE:
(1) ADD THE FOLLOWING NOTE PRIOR TO STEP 3: "ENSURE THAT
THE SLIDER BUSHING (18.1) REMAINS IN THE YOKE MOUNT (17)."
(2) ADD THE FOLLOWING WARNING AFTER STEP 5: "FLIGHT
SAFETY PARTS. THIS IS AN INSTALLATION CRITICAL FLIGHT SAFETY
PART. ALL ASPECTS OF ITS ASSEMBLY AND INSTALLATION MUST BE
ENSURED. ENSURE THAT THE SLIDER BUSHING (18.1) IS RETAINED IN
THE MOUNT LUG (17)."
(3) ADD THE FOLLOWING NOTE AFTER STEP 5: "SLIDER BUSHING
(18.1) IS NOT PICTURED IN THE ACCOMPANYING DIAGRAM."
E. ANNOTATE THE FOLLOWING CHANGE TO TM 55-1520-240-23, TASK
11-212, REMOVE FORWARD LCT YOKE: ADD THE FOLLOWING NOTE AFTER
STEP 10: "ENSURE THAT SLIDER BUSHING (21), NOT SHOWN IN THE
ACCOMPANYING DIAGRAM, IS NOT REMOVED AND REMAINS IN THE YOKE
MOUNT (20)."
F. ANNOTATE THE FOLLOWING CHANGES TO TM 55-1520-240-23, TASK
11-217, INSTALL FORWARD LCT YOKE:
(1) ADD THE FOLLOWING NOTE PRIOR TO STEP 3: "ENSURE THAT
THE SLIDER BUSHING (9.1) REMAINS IN THE YOKE MOUNT (10)."
(2) ADD THE FOLLOWING WARNING AFTER STEP 5: "FLIGHT
SAFETY PARTS. THIS IS AN INSTALLATION CRITICAL FLIGHT SAFETY
PART. ALL ASPECTS OF ITS ASSEMBLY AND INSTALLATION MUST BE
ENSURED. ENSURE THAT THE SLIDER BUSHING (9.1) IS RETAINED IN THE
MOUNT LUG (10). "
(3) ADD THE FOLLOWING NOTE AFTER STEP 5: "FOR MANUALS
PRIOR TO CHANGE 22, THE SLIDER BUSHING (9.1) IS NOT PICTURED IN
THE ACCOMPANYING DIAGRAM."
G. ANNOTATE THE FOLLOWING CHANGE TO TM 55-1520-240-23, TASK
11-227, REMOVE AFT LCT YOKE: ADD THE FOLLOWING NOTE AFTER STEP
13: "ENSURE THAT SLIDER BUSHING (28.1), NOT SHOWN IN THE
ACCOMPANYING DIAGRAM, IS NOT REMOVED AND REMAINS IN THE SUPPORT
(29)."
H. ANNOTATE THE FOLLOWING CHANGES TO TM 55-1520-240-23, TASK
11-233, INSTALL AFT LCT YOKE:
(1) ADD THE FOLLOWING NOTE PRIOR TO STEP 3: "ENSURE THAT
THE SLIDER BUSHING (18.1) REMAINS IN THE YOKE MOUNT (17)."
(2) ADD THE FOLLOWING WARNING AFTER STEP 5: "FLIGHT
SAFETY PARTS. THIS IS AN INSTALLATION CRITICAL FLIGHT SAFETY
PART. ALL ASPECTS OF ITS ASSEMBLY AND INSTALLATION MUST BE
ENSURED. ENSURE THAT THE SLIDER BUSHING (18.1) IS RETAINED IN
THE MOUNT LUG (17)."
(3) ADD THE FOLLOWING NOTE AFTER STEP 5: "SLIDER BUSHING
(18.1) IS NOT PICTURED IN THE ACCOMPANYING DIAGRAM."
10. SUPPLY/PARTS AND DISPOSITION -
A. PARTS REQUIRED - ITEMS LISTED BELOW MAY BE REQUIRED TO
REPLACE DEFECTIVE ITEMS.
NOMENCLATURE PART NO. NSN COST
YOKE ASSEMBLY 145C3050-3 1560-01-116-4203 $16291.38
YOKE ASSEMBLY 114C3043-6 1615-00-115-4718 $4443.49
BUSHING, SLEEVE 145D0121-15 3120-01-116-4456 $30.99
BUSHING, SLEEVE 145D0121-14 3120-01-116-4455 $71.55
BUSHING, SLEEVE 114S4829-1 3120-01-128-1827 $42.18
BUSHING, SLEEVE NAS75-20-206 3120-01-156-7812 $12.32
BUSHING, SLEEVE NAS75-20-123 3120-00-159-7016 $8.54
SHAFT, SHOULDERED 145C3051-1 3040-01-116-4323 $859.13
SHAFT 114C3044-2 1560-00-868-8468 $135.00
NUT MS17826-12 5310-00-047-2965 $2.59
PIN, COTTER MS24665-376 5315-00-236-8362 $4.05
NUT MS21025-20 5310-00-838-0265 $11.57
PIN, COTTER MS24665-379 5315-00-059-0494 $6.95
IF ONE AIRCRAFT WERE TO HAVE A BUSHING NOT INSTALLED IN BOTH
FORWARD AND AFT YOKE ASSEMBLIES AND THE YOKES HAVE BEEN DAMAGED
BEYOND REPAIR. COST $21919.74
IF THE FORWARD YOKE SUPPORT ASSEMBLY HAS BEEN DAMAGED, THE FORWARD
TRANSMISSION MUST BE REPLACED.
P/N 145D1300-9 NSN 1615-01-317-6446 $343,650.00
B. REQUISITIONING INSTRUCTIONS - IF THE SLIDER BUSHINGS ARE
NOT INSTALLED IN THE YOKE MOUNT, CONTACT LOGISTICAL POINT OF
CONTACT IN PARAGRAPH 16B FOR REQUISITIONING INSTRUCTIONS. ALL
REQUISITIONS SHALL USE PROJECT CODE (CC 57-59) "XFK","X-RAY-
FOXTROT-KILO".
NOTE
PROJECT CODE "XFK","X-RAY-FOXTROT-KILO" IS
REQUIRED TO TRACK AND ESTABLISH A DATA BASE
OF STOCK FUND EXPENDITURES INCURRED BY THE
FIELD AS A RESULT OF SOF ACTIONS.
C. BULK AND CONSUMABLE MATERIALS - N/A.
D. DISPOSITION - DISPOSE OF REMOVED PARTS/COMPONENTS USING
NORMAL SUPPLY PROCEDURES.
E. DISPOSITION OF HAZARDOUS MATERIAL IAW ENVIRONMENTAL
PROTECTION AGENCY DIRECTIVES AS IMPLEMENTED BY YOUR SERVICING
ENVIRONMENTAL COORDINATOR (AR 200-1).
11. SPECIAL TOOLS AND FIXTURES REQUIRED - AS REQUIRED.
12. APPLICATION -
A. CATEGORY OF MAINTENANCE - AVUM. AIRCRAFT DOWNTIME WILL
BE CHARGED TO AVUM.
B. ESTIMATED TIME REQUIRED -
(1) FOR VISUAL INSPECTION -
(A) TOTAL OF 1 MAN-HOURS USING 1 PERSONS.
(B) TOTAL OF 0 HOURS DOWNTIME FOR ONE END ITEM.
(2) FOR DISASSEMBLY AND INSPECTION -
(A) TOTAL OF 40 MAN-HOURS USING 4 PERSONS.
(B) TOTAL OF 10 HOURS DOWNTIME FOR ONE END ITEM.
C. ESTIMATED COST IMPACT TO THE FIELD - $200.00 FOR CONSUMABLES
USED DURING THE INSPECTION.
D. TB/MWOS TO BE APPLIED PRIOR TO OR CONCURRENTLY WITH THIS
INSPECTION - N/A.
E. PUBLICATIONS WHICH REQUIRE CHANGE AS A RESULT OF THIS
INSPECTION - TM 1-1520-252-23 AND TM 55-1520-240-23 SHALL BE
CHANGED TO REFLECT PARAGRAPH 9 OF THIS MESSAGE. A COPY OF THIS
MESSAGE SHALL BE INSERTED IN THE APPROPRIATE TM AS AUTHORITY TO
IMPLEMENT THE CHANGE UNTIL THE PRINTED CHANGE IS RECEIVED.
13. REFERENCES -
A. TM 1-1520-252-23, AVIATION UNIT AND AVIATION INTERMEDIATE
MAINTENANCE MANUAL, MH-47E HELICOPTER.
B. TM 1-1520-252-23P, AVIATION UNIT AND AVIATION
INTERMEDIATE MAINTENANCE REPAIR PARTS AND SPECIAL TOOLS LIST
(INCLUDING DEPOT MAINTENANCE REPAIR PARTS AND SPECIAL TOOLS),
HELICOPTER, CARGO TRANSPORT, MH-47E, NSN 1520-01-282-3747.
C. TM 55-1520-240-23, AVIATION UNIT AND AVIATION
INTERMEDIATE MAINTENANCE MANUAL, CH-47D HELICOPTER.
D. TM 55-1520-240-23P, AVIATION UNIT AND AVIATION
INTERMEDIATE MAINTENANCE REPAIR PARTS AND SPECIAL TOOLS LIST
(INCLUDING DEPOT MAINTENANCE REPAIR PARTS AND SPECIAL TOOLS),
HELICOPTER, CARGO TRANSPORT, CH-47D, NSN 1520-01-088-3669.
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 CDR, AMCOM, ATTN: AMSAM-SF-A (SOF COMPLIANCE OFFICER),
REDSTONE ARSENAL, AL 35898-5222, IAW AR 95-1. DATAFAX NUMBER IS
DSN 897-2111 OR (256) 313-2111. E-MAIL ADDRESS IS
"SAFEADM@REDSTONE.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 (AIRCRAFT) -
NO SPECIAL REPORT OF THE RESULTS OF THIS INSPECTION IS REQUIRED.
C. REPORTING MESSAGE RECEIPT (SPARES) - N/A.
D. TASK/INSPECTION REPORTING SUSPENSE DATE (SPARES)-N/A.
E. THE FOLLOWING FORMS ARE APPLICABLE AND ARE TO BE
COMPLETED IAW DA PAM 738-751, 15 JUN 92 - NOTE
ULLS-A USERS WILL USE APPLICABLE "E" FORMS.
(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. JAMES
M. WILSON, AMSAM-AR-E-I-C-H, DSN 897-4625 OR (256) 313-4625,
DATAFAX IS DSN 897-3230 OR (256) 313-3230, E-MAIL IS
"WILSONJ@REDSTONE.ARMY.MIL".
B. LOGISTICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. BILL
OLSON, SFAE-AV-CH-L, DSN 897-4304 OR 256-313-4304, DATAFAX IS DSN
897-4348 OR 256-313-4348.
E-MAIL IS "OLSONW@PEOAVN.REDSTONE.ARMY.MIL".
C. FORMS AND RECORDS POINT OF CONTACT FOR THIS MESSAGE IS MS.
ANN WALDECK, AMSAM-MMC-RE-FF DSN 746-5564 OR (256) 876-5564,
DATAFAX IS DSN 746-4904 OR (256) 876-4904.
E-MAIL IS "WALDECK-AB@REDSTONE.ARMY.MIL".
D. SAFETY POINT OF CONTACT FOR THIS MESSAGE IS MR. ROBERT D.
BROCK, AMSAM-SF-A, DSN 788-8632 OR (256) 842-8632, DATAFAX IS DSN
897-2111 OR (256) 313-2111. E-MAIL IS
"BOB.BROCK@REDSTONE.ARMY.MIL".
E. FOREIGN MILITARY SALES RECIPIENTS REQUIRING CLARIFICATION
OF ACTION ADVISED BY THIS MESSAGE SHOULD CONTACT: CW5 JOSEPH L.
WITTSTROM, SECURITY ASSISTANCE MANAGEMENT, AMSAM-SA, DSN 897-0681
OR (256) 313-0681. EMAIL IS "WITTSTROMJL@REDSTONE.ARMY.MIL" OR
MR. RONNIE W. SAMMONS, AMSAM-SA-CS-NF, DSN 897-0869 OR (256) 313-
0869. DATAFAX IS DSN 897-0411 OR (256) 313-0411. EMAIL IS
"SAMMONSRW@REDSTONE.ARMY.MIL". HUNTSVILLE, AL IS GMT MINUS 6
HRS.
F. AFTER HOURS CONTACT THE AMCOM COMMAND OPERATIONS CENTER
(COC) DSN 897-2066/7 OR (256) 313-2066/7.