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:CDRATCOM ST LOUIS MO//AMSAT-R-X//
TO
:AIG 6713
:AIG 9004
:AIG 8708
:AIG 9042
:AIG 7471
:AIG 12124
:USMILGP BUENOS AIRES AR//ARMY AND AF SEC//
:DEFAIR MATERIAL CANBERRA AS//DAAP-AF//
:ARMYLMSQN OAKEY AS
:AVN REGT HQ SQN OAKEY AS//DAVN-A//
:CDRUSARDSG CANBERRA AS
:LOGCON OTTAWA CAN//DTHEM 6-2//
:ARGENTINE AIR ATTACHE FMS WASHINGTON DC
:EGYPT AF FMS CAIRO EG//ED-MA//
:USOMC CAIRO EG//AV//
:ODC ATHENS GR//ODCSA//
:CDR4THBN228THAVN SOTO CANO HO//AVN-AMO//
:102DARMY SCOTT AFB IL//AFRC-AMO-ASF-IL//
:CHJUSMAG SEOUL KOR//MKAR//
: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//
:SPAIN ARMY FMS MADRID SP
:AIT TAIPEI TW
:TAIWAN ARMY FMS TAIPEI TW
:CJUSMAG THAI BANGKOK TH//MAGTAR-FS//
:ROYAL THAI ARMY FMS/DUSIT ORDNANCE DEP BANGKOK TH
:CDRUSARDSG LONDON UK//AMXSN-UK-SE//
:ODC LONDON UK
INFO
:CDRAMC ALEXANDRIA VA//AMCMR/AMCCS/AMCSM-WAA//
XMT
:USDAO DHAKA BG
:USDAO RANGOON BM
:USCINCPAC REP PHNOM PENH CB
:USDAO COLOMBO CE
:USDAO SUVA FJ
:OMADP JAKARTA ID
:DSA NEW DELHI IN
:AMEMBASSY ANTANANARIVO MA
:AMEMBASSY PORT LOUIS
:SAO KUALA LUMPUR MY
:AMEMBASSY KATHMANDU NP//POL-MIL//
:AMEMBASSY VICTORIA
:SAO SINGAPORE SN
ACCT
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TEXT
:UNCLAS
SUBJECT - AVIATION SAFETY ACTION MESSAGE, MAINTENANCE
MANDATORY, RCS CSLD-1860(R1), ALL CH-47D, MH-47D, AND MH-47E
AIRCRAFT, REVISION TO INSPECTION AND LUBRICATION OF THE FLIGHT
CONTROL ROD END BEARINGS (ROLLING ELEMENT) REQUIRED BY AVIATION
SAFETY ACTION MESSAGE CH-47-95-ASAM-05 (CH-47-95-ASAM-06)(TB 1-
1520-240-20-77).
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-R-
X (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
RED //X//.
B. AIRCRAFT IN DEPOT MAINTENANCE - SAME AS PARA 1A.
C. AIRCRAFT UNDERGOING MAINTENANCE SAME AS PARA 1A.
D. AIRCRAFT IN TRANSIT -
(1) SURFACE/AIR SHIPMENT - SAME AS PARA 1A
(2) FERRY STATUS - SAME AS PARA 1A.
E. MAINTENANCE TRAINERS (CATEGORY A, B) - SAME AS PARA 1A.
F. COMPONENT/PARTS IN STOCK INCLUDING WAR RESERVES AT ALL
LEVELS (DEPOT AND OTHERS) - N/A.
2. TASK/INSPECTION SUSPENSE DATE -
A. THE BEARINGS LISTED IN PARAGRAPHS 6A, 6B, 6C, 6D AND
6E SHALL BE INSPECTED AND LUBRICATED AT THE FIRST AND THIRD
PHASE INSPECTION THEREAFTER.
B. THE BEARINGS LISTED IN PARAGRAPHS 6F, 6G AND 6H, THE
PEDAL BOX BEARINGS, SHALL BE INSPECTED AT NEXT PHASE INSPECTION
AND LUBRICATED ONLY IF THEY ARE REMOVED FROM THE AIRCRAFT.
NOTE
IF THE AIRCRAFT IS CURRENTLY IN PHASE, PERFORM THE
REQUIREMENTS OF THIS MESSAGE BEFORE THE AIRCRAFT IS RELEASED
FOR FLIGHT.
3. REPORTING COMPLIANCE SUSPENSE DATE - NO LATER THAN 12 SEP 1995
PER PARA 14A OF THIS MESSAGE.
4. SUMMARY OF PROBLEM -
A. AVIATION SAFETY ACTION MESSAGE CH-47-95-ASAM-05
REQUIRED AN INSPECTION AT EVERY 3RD PHASE. AS A RESULT OF
ENGINEERING ANALYSIS, THE REQUIREMENTS OF CH-47-95-ASAM-05 NEED
REVISING. IMPLEMENT THE REQUIREMENTS OF THIS MESSAGE AT THE
NEXT PHASE INSPECTION AS REQUIRED BY CH-47-95-ASAM-05.
B. FOR MANPOWER/DOWNTIME AND FUNDING IMPACTS SEE PARA 12.
C. THIS MESSAGE SUPERSEDES AVIATION SAFETY ACTION MESSAGE
CH-47-95-ASAM-05 ENTIRELY AND MAKES THE FOLLOWING CHANGES:
(1) INSPECT AND LUBRICATE BEARINGS OF PARA 6A, 6B, 6C,
6D AND 6E AT THE NEXT PHASE INSPECTION AND AT FIRST AND 3RD
PHASE INSPECTION THEREAFTER.
(2) INSPECT THE PEDAL BOX BEARINGS (PARA 6F, 6G AND 6H)
AT NEXT PHASE INSPECTION AND LUBRICATE EACH TIME THEY ARE
REMOVED FROM AIRCRAFT.
(3) INCREASES THE NUMBER OF PARTS TO BE INSPECTED AND
THE INSPECTION CRITERIA OF THE PARTS TO BE INSPECTED.
5. END ITEMS TO BE INSPECTED - ALL CH-47D, MH-47D, AND MH-47E
AIRCRAFT.
6. ASSEMBLY COMPONENTS TO BE INSPECTED -
NOTE
ITEM AND FIGURE NUMBERS ARE REFERENCING TM 55-1520-240-23P
NOMENCLATURE PART NO.
A. FORWARD PYLON (FIGURE 372)
SWIVELING ACTUATOR INPUT (ITEM 13) 145C3340-1
2ND STAGE TO RH UPPER (ITEM 7) 145C3340-10
BELLCRANK
PIVOTING ACTUATOR INPUT (ITEM 17) 145C3340-12
B. MIXING COMPLEX (FIGURE 377)
CONNECTION LINK ASSEMBLY (ITEM 14) 145C3340-11
INPUT TO LH UPPER (ITEM 10) 145C3340-2
BELL CRANK (ITEM 166) 114C3320-22
PITCH OUTPUT 1ST TO 2ND STAGE (ITEM 22) 145C3340-7
ROLL OUTPUT 1ST TO 2ND STAGE (ITEM 33) 145C3340-8
ROLL OUTPUT 1ST TO 2ND STAGE (ITEM 39) 145C3340-9
C. TUNNEL AREA (FIGURE 374)
1ST SET OF LINKS FROM MIX 114C3010-29
ALTERNATE TO -29 114C3010-35
ALTERNATE TO -35 AND -29 (ITEM 20) 145CS340-15
D. AFT FUSELAGE (FIGURE 375)
LINK BETWEEN 2510 AND 2512 145C2010-10
BELL CRANK'S
ALTERNATE TO -10 145C2010-14
ALTERNATE TO -10 AND-14 (ITEM 15) 145CS340-1
LINK BETWEEN 2511 AND 2513 145C2010-11
BELLCRANK'S
ALTERNATE TO -11 145C2010-15
ALTERNATE TO -11 AND -15 (ITEM 21) 145CS340-3
LINK BETWEEN 2516 AND 2510 414C2520-3
BELLCRANK'S (ITEM 6)
LINK BETWEEN 2516 AND 2511 414C2520-4
BELLCRANK'S (ITEM 11)
E. AFT PYLON (FIGURE 376)
LINK BETWEEN 2512 AND 2514 145C2010-12
BELLCRANK'S
ALTERNATE TO -12 145C2010-16
ALTERNATE TO -12 AND -16 (ITEM 8) 145CS340-5
LINK BETWEEN 2513 AND 2515 145C2010-13
BELLCRANK'S
ALTERNATE TO -13 145C2010-17
ALTERNATE TO -13 AND -17 (ITEM 15) 145CS340-7
PIVOTING ACTUATOR INPUT (ITEM 27) 145C2013-3
SWIVELING ACTUATOR INPUT (ITEM 34) 145C2013-4
F. CONTROLS, INSTL, FLIGHT, COCKPIT (FIGURE 361)
CONNECTING LINK ASSEMBLY (ITEM 7) 114C1013-7
CONNECTING LINK ASSEMBLY (ITEM 12) 114C1013-5
CONNECTING LINK ASSEMBLY (ITEM 17) 114C1013-4
CONNECTING LINK ASSEMBLY (ITEM 28) 114C1013-3
CONNECTING LINK ASSEMBLY (ITEM 32) 114C1013-1
CONNECTING LINK ASSEMBLY (ITEM 37) 114C1013-6
CONNECTING LINK ASSEMBLY (ITEM 21) 114C1014-9
G. CONTROLS ASSY, COPILOT, COCKPIT (FIGURE 362)
LINK ASSEMBLY (ITEM 11) 114C1014-1
LINK ASSEMBLY (ITEM 12) 114C1014-3
LINK ASSEMBLY (ITEM 13) 114V1014-21
LINK ASSEMBLY (ITEM 14) 114C1014-2
LINK ASSEMBLY (ITEM 15) 114C1014-22
H. CONTROLS ASSY, PILOT, COCKPIT (FIGURE 363)
LINK ASSEMBLY (ITEM16) 114C1014-1
LINK ASSEMBLY (ITEM 17) 114C1014-3
LINK ASSEMBLY (ITEM 18) 114C1014-21
LINK ASSEMBLY (ITEM 19) 114C1015-1
LINK ASSEMBLY (ITEM 20) 114C1015-2
7. PARTS TO BE INSPECTED-
NOMENCLATURE PART NO. NSN
ROD END BEARING MS21221-4G 3110-00-514-4828
ROD END BEARING MS21221-5G 3110-00-198-0252
ROD END BEARING MS21221-6G 3110-00-198-2239
ROD END BEARING SM4-5C 3110-00-088-8626
ROD END BEARING SM4-6T 3110-00-159-1636
ROD END BEARING SM5-8C 3110-00-198-0252
ROD END BEARING 114CS103-2 3110-00-088-8626
ROD END BEARING 114CS103-4 3110-01-096-0895
8. INSPECTION PROCEDURES -
CAUTION
THE FOLLOWING INSPECTIONS SHALL BE CAREFULLY PERFORMED DUE TO
THE SENSITIVITY OF BEARING SEALS.
A. INSTALL SERVOCYLINDER SAFETY BLOCKS PER TM 55-1520-240-
23 MAINTENANCE MANUAL, TASK 11-28.
B. TURN OFF ELECTRICAL AND HYDRAULIC POWER. DISCONNECT
THE BATTERY PER TM 55-1520-240-23, TASK 1-39.
C. INSPECT ROD END BEARINGS (ROLLING ELEMENT) LOCATED IN
ALL AREAS SPECIFIED IN PARA 6 IAW TM 55-1520-240-23 AND AS
FOLLOWS:
NOTE
ROLLING ELEMENT BEARINGS AFFECTED BY THIS ASAM ARE LOCATED
IN THE 1ST AND 2ND STAGE MIXING UNITS, FORWARD PYLON, TUNNEL
AREA, AFT FUSELAGE, AFT PYLON AND PEDAL BOX AREA ONLY.
(1) DISCONNECT SUFFICIENT PARTS OF THE SYSTEM AS
REQUIRED SO THAT THE INDIVIDUAL BEARINGS MAY BE EXAMINED BY
HAND ROTATION. SERVICEABLE CONDITION, WELL-LUBRICATED BEARINGS
FEEL SMOOTH WITH NO PERCEPTIBLE ROUGHNESS, CATCHING OR BINDING.
EXCESSIVE EXTERNAL CORROSION OR WORN PLATING SHOULD NOT BE
EVIDENT ON THE BEARING EXTERIOR, AND SHIELDS AND SEALS SHOULD
BE UNDAMAGED AND OPERABLE.
(2) UNSERVICEABLE BEARINGS ARE THOSE WHICH HAVE ONE OR
MORE OF THE FOLLOWING DISCREPANCIES:
(A) "FRACTURED COMPONENTS": REPLACE ALL
BEARINGS WITH CRACKED OR BROKEN RINGS, RETAINERS, OR ROLLING
ELEMENTS.
(B) "FROZEN BEARINGS": REPLACE ALL BEARINGS
THAT ARE FROZEN AND CANNOT BE ROTATED.
(C) "DAMAGED SEALS AND SHIELDS": REPLACE
BEARINGS IF SEALS AND SHIELDS ARE DAMAGED, WARPED, OR BENT.
(D) "ROUGH BEARINGS": REPLACE ANY BEARING THAT
HAS ANY OBVIOUS CATCHING OR BINDING WHEN ROTATED BY HAND.
ROUGHNESS MAY BE CAUSED BY CAKED OR DETERIORATED GREASE,
FOREIGN PARTICLES, CORROSION, BRINELLING FROM IMPROPER
INSTALLATION, SPALLING OF THE ROLLING ELEMENTS FROM METAL
FATIGUE. THE LATTER THREE CAUSES OF ROUGHNESS CAN BE CORRECTED
ONLY BY REPLACEMENT OF THE BEARING. THE FIRST TWO CAUSES MAY
BE CORRECTED BY CLEANING AND RE-LUBRICATION.
(E) "LOOSE BEARINGS": REPLACE THE BEARING IF
LOOSENESS IS DETECTED IN EITHER AXIAL OR RADICAL PLAY. REFER
TO THE APPROPRIATE MAINTENANCE MANUAL FOR ALLOWABLE LIMITS.
(F) "NOISY BEARINGS": NOISY BEARINGS USUALLY
INDICATE A LACK OF LUBRICANT. RETURN THE BEARINGS TO SERVICE
IF LUBRICATION ALLEVIATES THE PROBLEM. REPLACE THE BEARING IF
RE-LUBRICATION DOES NOT CORRECT THE PROBLEM.
(G) "CORRODED BEARINGS": EXCESSIVE EXTERNAL
CORROSION FREQUENTLY INDICATED THAT THE INTERIOR MAY BE
CORRODED. REPLACE THE BEARING.
(H) "CAKED OR DETERIORATED GREASE": DAMAGE TO
BEARINGS MAY RESULT FROM LACK OF LUBRICANT, CAKED OR
DETERIORATED GREASE. REPLACE THE BEARING IF LUBRICATION DOES
NOT CORRECT THE PROBLEM.
(I) "ROD ENDS": WHEN ROD ENDS ARE INSPECTED,
THE THREADED PORTION OF THE SHANK SHOULD BE EXAMINED FOR
DAMAGED THREADS OR LOOSENESS BETWEEN THE SHANK AND THE LINKAGE
OR ROD, AND FRETTING ABRASION OR WEAR. CHECK FOR CRACKS IN THE
THIN SECTION OF THE HOUSING ADJOINING THE SHANK. REPLACE THE
ROD END BEARING FOR ANY OF THE ABOVE CONDITIONS. THE ABOVE
INSPECTION IS ACCOMPLISHED WITHOUT REMOVING ROD END FROM FLIGHT
CONTROL ROD.
NOTE
ROD END BEARINGS MAY HAVE EITHER OF TWO TYPES OF INTEGRAL
LUBRICATION PROVISIONS (GREASE FITTINGS):
(A) RED NYLON TYPE
(B) NAS516-1A BALL CHECK TYPE
THE NOZZLE TO BE USED FOR LUBRICATING THE BEARING IS EITHER
MS24203 NOZZLE OR ALEMITE NOZZLE 314150.
9. CORRECTION PROCEDURES -
CAUTION
THE FOLLOWING PROCEDURES SHALL BE PERFORMED CAREFULLY DUE
TO THE SENSITIVITY OF BEARING SEALS.
NOTE
THE ROD END BEARINGS THAT ARE LOCATED IN PEDAL BOX AREA,
FLIGHT COCKPIT CONTROLS, PILOT COCKPIT CONTROLS ASSEMBLY, AND
COPILOT COCKPIT CONTROLS ASSEMBLY (PARAGRAPHS 6F, 6G AND 6H),
ARE NOT EXPOSED TO THE SAME SEVERE CONDITIONS AS THE OTHER
BEARINGS IN THIS ASAM. THE PEDAL BOX BEARINGS ARE IN AN
ENCLOSED PROTECTIVE AREA AND WOULD BE DIFFICULT TO LUBRICATE
BEARINGS WITHOUT REMOVING THEM FROM THE AIRCRAFT;
THEREFORE, THE NEED TO LUBRICATE THESE BEARINGS AT THE SAME
SCHEDULE AS THE OTHER BEARINGS IS NOT NEEDED.
A. ROD END BEARINGS LOCATED IN THE PEDAL BOX AREA AS
SPECIFIED IN PARA 6F, 6G AND 6H SHALL BE LUBRICATED ONLY WHEN
THE PEDAL BOXES ARE REMOVED FROM THE AIRCRAFT FOR OTHER
REASONS.
B. ROD END BEARINGS LOCATED IN THE AREAS SPECIFIED IN
PARA 6A, 6B, 6C, 6D, AND 6E SHALL BE LUBRICATED BY THE
TASK/INSPECTION SUSPENSE DATE AND EVERY PHASE 1 AND 3
INSPECTIONS THEREAFTER.
C. LUBRICATE THE FLIGHT CONTROL ROD END ROLLING ELEMENT
BEARINGS AS FOLLOWS:
(1) IDENTIFY AND LOCATE BEARINGS TO BE RE-
LUBRICATED. SEE PARAGRAPH 7 FOR BEARINGS THAT ARE EFFECTED.
(2) PRIOR TO LUBRICATION, ENSURE THAT THE
GREASE GUN AND NOZZLE ARE CLEAN AND FREE OF CONTAMINATION.
(3) FILL THE GREASE GUN WITH MIL-G-81322 WIDE
TEMPERATURE GREASE.
(4) REMOVE SUFFICIENT AMOUNT OF HARDWARE TO
OBTAIN ACCESS TO THE ROD END BEARING GREASE FITTING.
(5) CLEAN THE EXTERIOR OF THE BEARING USING A
CLEAN CLOTH.
NOTE
CLEANLINESS CANNOT BE OVER-EMPHASIZED WITH RESPECT TO
PROLONGING BEARING LIFE.
(6) DO NOT REMOVE BEARING FROM ROD END
COMPONENT.
CAUTION
DURING APPLICATION OF GREASE TAKE CARE IN OPERATING THE
GREASE GUN SO THAT YOU DO NOT OVER-PRESSURIZE AND DAMAGE THE
BEARING SEALS/SHIELDS. OPERATE THE GREASE GUN IN A SLOW AND
SMOOTH TECHNIQUE DURING APPLICATION.
(7) USING MIL-G-81322 GREASE AND A HAND
OPERATED GREASE GUN, ATTACH THE GUN AND PRESSURIZE.
(8) ALLOW THE GREASE TO FLOW UNTIL GREASE THAT
EXUDES OUT FROM AROUND THE BEARING IS CLEAN. THE BEARING
SHOULD BE ROTATED 360 DEGREES DURING LUBRICATION.
NOTE
THE ABOVE PROCEDURE REMOVES SOME DIRTY GREASE FROM THE
BEARING CAVITY AND TENDS TO MAXIMIZE THE AMOUNT OF GREASE
LEFT INSIDE. THE PURPOSE OF THIS TYPE OF RE-LUBRICATION IS
TO MAINTAIN INTERNAL CORROSION PROTECTION AS MUCH AS TO
SUSTAIN LOW FRICTION.
(9) USING A CLEAN CLOTH, WIPE THE EXCESS GREASE
OFF THE BEARING ROD END.
(10) TURN ON THE ELECTRICAL AND HYDRAULIC
POWER.
(11) REMOVE SERVOCYLINDER SAFETY BLOCKS PER TM
55-1520-240-23 MAINTENANCE MANUAL, TASK 11-29.
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 "XA5" PER
THIS MESSAGE.
NOTE
PROJECT CODE "XA5" IS REQUIRED TO TRACK AND ESTABLISH A
DATA BASE OF STOCK FUND EXPENDITURES INCURRED BY THE FIELD AS
A RESULT OF ASAM/SOF ACTIONS.
C. BULK AND CONSUMABLE MATERIALS - MIL-G-81322.
D. DISPOSITION - DISPOSE OF REMOVED PARTS/COMPONENTS IN
ACCORDANCE WITH NORMAL SUPPLY PROCEDURES.
E. DISPOSITION OF HAZARDOUS MATERIAL - N/A.
11. SPECIAL TOOLS, JIGS AND FIXTURES REQUIRED - MS24203 OR
ALEMITE NOZZLE P/N 314150.
12. APPLICATION -
A. CATEGORY OF MAINTENANCE - AVUM. AIRCRAFT DOWNTIME
WILL BE CHARGED TO AVUM.
B. ESTIMATED TIME REQUIRED -
(1) TOTAL OF 40 MANHOURS USING 4 PERSONS.
(2) TOTAL OF 10 HOURS DOWNTIME FOR ONE END ITEM.
C. ESTIMATED COST IMPACT OF STOCK FUND ITEMS TO THE FIELD
- N/A.
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 - A COPY OF THIS MESSAGE SHALL BE INSERTED IN THE
APPROPRIATE TM AS AUTHORITY TO IMPLEMENT THE CHANGE UNTIL THE
PRINTED CHANGE IS RECEIVED.
(1) TM 1-1520-252-23-12 SHALL BE CHANGED TO ADD THE
INSPECTION AND LUBRICATION PROCEDURES FROM PARAGRAPH 8 AND 9 OF
THIS MESSAGE.
(2) TM 1-1520-252-PM SHALL BE CHANGED TO IDENTIFY THE
REQUIREMENTS FOR BEARINGS TO BE LUBRICATED DURING PHASE 1 AND
PHASE 3 INSPECTIONS. IN ADDITION, LUBRICATE THE PEDAL BOX
BEARINGS ONLY IF THEY ARE REMOVED FROM THE AIRCRAFT FOR OTHER
MAINTENANCE.
(3) TM 55-1520-240-23-9 SHALL BE CHANGED TO ADD THE
INSPECTION AND LUBRICATION PROCEDURES FROM PARAGRAPH 8 AND 9 OF
THIS MESSAGE.
(4) TM 55-1520-240-PM SHALL BE CHANGED TO IDENTIFY THE
REQUIREMENTS FOR BEARINGS TO BE LUBRICATED DURING PHASE 1 AND
PHASE 3 INSPECTIONS. IN ADDITION, LUBRICATE THE PEDAL BOX
BEARINGS ONLY IF THEY ARE REMOVED FROM THE AIRCRAFT FOR OTHER
MAINTENANCE.
13. REFERENCES -
A. TM 55-1520-240-23.
B. TM 55-1520-240-23P.
C. TM 55-1520-240-PM.
D. TM 1-1520-252-23.
E. TM 1-1520-252-23P.
F. TM 1-1520-252-PM.
G. TM 55-1500-322-24.
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-R-X (SOF COMPLIANCE
OFFICER), PER AR 95-3. DATAFAX NUMBER IS DSN 693-2064 OR
COMMERCIAL 314/263-2064. E-MAIL ADDRESS IS "AMSATRXS (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 (AIRCRAFT) -
N/A.
C. REPORTING COMPLIANCE SUSPENSE DATE (SPARES) - N/A.
D. 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 2408-13-2,RELATED MAINTENANCE RECORD.
(4) DA FORM 2408-15, HISTORICAL RECORD FOR AIRCRAFT.
(5) DA FORM 2408-18, EQUIPMENT INSPECTION LIST.
15. WEIGHT AND BALANCE - N/A.
16. POINTS OF CONTACT -
A. TECHNICAL POINT OF CONTACTS FOR THIS MESSAGE ARE MR.
DAVID BRAUN, SAIC CONTRACTOR, AND MR. MIKE WRIGHT, AMSAT-R-ECC,
DSN 693-6679 OR COMMERCIAL 314/263-6679.
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 693-1821/1758 OR COMMERCIAL
314/263-1821/1758.
D. SAFETY POINT OF CONTACT FOR THIS MESSAGE IS MR. JIM
WILKINS, AMSAT-R-X, DSN 693-2258 OR COMMERCIAL 314/263-2258.
E. FOREIGN MILITARY SALES (FMS) RECIPIENTS REQUIRING
CLARIFICATION OF ACTION ADVISED BY THIS MESSAGE SHOULD CONTACT
CW5 JAY NANCE/MR. RON VAN REES, AMSAT-I-IAF, DSN 693-3826/3659
OR COMMERCIAL 314/263-3826/3659.
F. AFTER HOURS CONTACT ATCOM COMMAND OPERATIONS CENTER
(AOC) DSN 693-2066/7 OR COMMERCIAL 314./263-2066/7.