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:081943Z OCT 99 OO PP UUUU AA ZYUW
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:CDRAMCOM REDSTONE ARSENAL AL//AMSAM-SF-A//
TO
:AIG 8881
:AIG 9004
:AIG 7471
:AIG 12124
:USMILGP BUENOS AIRES AR//ARMY AND AF SEC//
:DEFAIR MATERIAL CANBERRA ACT AS//DAAP-AF//
:CDRUSARDSG CANBERRA ACT AS//AMXIP-AS//
:ARGENTINE AIR ATTACHE FMS WASHINGTON DC
:EGYPT AF FMS CAIRO EG//ED/MA//
:USOMC CAIRO EG//AV//
:ODC ATHENS GR//ODCSA//
:CDR1STBN228THAVN SOTO CANO HO//AVN-AMO//
:CHJUSMAGK SEOUL KOR//MKAR-AV//
:ROK ARMY FMS PUSAN KOR//ALC-LSD-L//
:CDR160THSOAR FT CAMPBELL KY//AOAV-SI//
:CDRBGAD RICHMOND KY//SIOBG-GC//
:USDAO RABAT MO//AF//
:ODC THE HAGUE NL//AVIATION SAFETY//
:RNLAF MATERIAL THE HAGUE NL
:RNLAF OPERATIONS THE HAGUE NL
:CDRUSASAC NEW CUMBERLAND PA//AMSAC-SALO-UK//
:CHUSAS RIYADH SA//ASAV//
:SAO SINGAPORE SN//AVIATION SAFETY//
:ODC MADRID SP//ASM//
:SPAIN ARMY FMS MADRID SP
:AIT TAIPEI TW
:TAIWAN ARMY FMS TAIPEI TW
:CJUSMAGTHAI BANGKOK TH//MAGTAR-FS//
:ROYAL THAI AF FMS BANGKOK TH//BANGSUE DEPOT//
:ROYAL THAI ARMY FMS BANGKOK TH//DUSIT ORDANCE DEPOT//
:CDRUSARDSG LONDON UK//AMXSN-UK-SE//
:ODC LONDON UK
INFO
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:CDRAMC ALEXANDRIA VA//AMCMR/AMCCS/AMCSM-WAA//
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TEXT
:UNCLAS
SUBJECT - SAFETY OF FLIGHT MESSAGE, OPERATIONAL, RCS CSGLD-
1860(R1), CH-47D, MH-47D, AND MH-47E AIRCRAFT, OPERATIONAL
RESTRICTIONS AND REVISION TO HISTORICAL RECORDS FOR T-62T-2B
AUXILIARY POWER UNIT (APU), CH-47-00-01 (TB 1-2835-205-20-4).
NOTE - THIS IS A SAFETY OF FLIGHT 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 ADDRESSES WILL IMMEDIATELY VERIFY
THIS TRANSMISSION TO CDR, AMCOM, ATTN: AMSAM-SF-A (SOF COMPLIANCE
OFFICER).
1. PRIORITY CLASSIFICATION -
NOTE - SEE AR 95-1, PARA 6-6A, FOR EXCEPTION AUTHORITY OF MAJOR
COMMANDERS.
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 //-//ENTRY SHALL STATE
"COMPLETE THE INSPECTION PROCEDURES IAW SOF CH-47-00-01 PRIOR TO NEXT
FLIGHT OR APU START". THE RED DASH //-// ENTRY MAY BE CLEARED WHEN
THE CRITERIA OF PARA 8 AND 9 ARE 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 SPECIFIED WILL
CAUSE THE STATUS SYMBOL OF THE AFFECTED AIRCRAFT 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 AND B) - SAME AS PARA 1A.
F. COMPONENT/PARTS IN STOCK AT ALL LEVELS (DEPOT AND OTHERS)
INCLUDING WAR RESERVES - SAME AS PARA 1A.
G. COMPONENTS/PARTS IN WORK (DEPOT LEVEL AND OTHERS) - SAME
AS PARA 1A.
2. TASK SUSPENSE DATE PRIOR TO NEXT FLIGHT OR APU START.
NOTE
AIRCRAFT MAY COMPLETE A ONE TIME FLIGHT, WITH
INTERMEDIATE STOPS, TO A SUITABLE MAINTENANCE
FACILITY PRIOR TO INSPECTION. THE ONE TIME FLIGHT
WILL NOT EXCEED 20 APU STARTS.
3. REPORTING COMPLIANCE SUSPENSE DATE - NO LATER THAN 29 OCT 99
IAW PARA 14A OF THIS MESSAGE.
4. SUMMARY OF PROBLEM -
A. BACKGROUND
(1) IN 1995 THERE WAS AN INCIDENT WHERE AN APU COMPRESSOR
WHEEL BURST DURING START-UP (SEE REFERENCE 13A). THE FAILURE WAS
ATTRIBUTED TO FATIGUE WHICH ORIGINATED FROM BOLTHOLES ON THE BACK OF
THE WHEEL (SEE REFERENCE 13B). THE DAMAGING FATIGUE CYCLES ARE
INCURRED BY STARTING THE APU.
(2) PREVIOUSLY, APU STARTS HAVE NOT BEEN RECORDED AND HAVE
NOT BEEN MAINTAINED AND TRANSFERRED WITH THE APU. CURRENTLY, START
CYCLES FOR A PARTICULAR COMPRESSOR WHEEL ARE ESTIMATED BASED ON THE
HOURS LOGGED ON THE AIRCRAFT RECORDS. THE ESTIMATES USE FOUR APU
STARTS FOR ONE FLIGHT HOUR.
(3) APU'S OVERHAULED SINCE NOVEMBER 1996 WERE SUBJECT TO
MAGNETIC PARTICLE INSPECTION OF THE COMPRESSOR WHEEL FOR FATIGUE
CRACKS AND ARE GIVEN A ONE-TIME LIFE EXTENSION OF 2100 STARTS SINCE
INSPECTION AT DEPOT (SEE "NOTE" IN PARA 9). ONLY APU'S SPECIFICALLY
LISTED IN PARAGRAPH 9B BELOW ARE AUTHORIZED TO OPERATE UP TO 525 HRS
OR 2100 STARTS SINCE INSPECTION (SSI). FUTURE APUS FROM DEPOT SHALL
HAVE FORMS AND RECORDS REFLECTING THIS NEW RETIREMENT LIFE.
(4) THE DATA FROM THESE INSPECTIONS INDICATE THAT WITH NO
LIFE LIMIT, WHICH IS THE CURRENT SITUATION, THE T-62T-2B APU
COMPRESSOR WHEEL HAS A HIGH PROBABILITY OF CATASTROPHIC FAILURE.
IN THE EVENT OF AN IMPELLER BURST, UP TO THREE PIECES OF THE IMPELLER
MAY EXIT THE APU RADIALLY. THESE PIECES WILL WEIGH UP TO 1.1 POUNDS
EACH AND WILL BE MOVING AT EXTREMELY HIGH VELOCITY.
(5) A NEW DESIGN HAS BEEN APPROVED FOR THE COMPRESSOR WHEEL
WHICH WILL HAVE A GREATER FATIGUE LIFE. THE NEW WHEELS WILL BE
INCORPORATED BY OLR TEAM USING MWO OR BY DEPOT.
B. FOR MANPOWER/DOWNTIME AND FUNDING IMPACTS SEE PARA 12.
C. THE PURPOSE OF THIS MESSAGE IS TO IMPOSE A RETIREMENT LIFE ON
APU COMPRESSOR WHEELS INSTALLED ON APU P/N 160150-10 OR 160150-100
AND STARTS SINCE INSPECTION (SSI) LIMITS FROM TIME OF DEPOT
INSPECTION. ADDITIONALLY, THIS MESSAGE ADDS HISTORICAL RECORD
REQUIREMENTS THAT WILL ALLOW TRACKING OF APU USAGE BY STARTS. IT
ALSO IMPOSES RESTRICTIONS ON APU'S WITH NON-INSPECTED WHEELS.
5. END ITEMS AFFECTED - ALL CH-47D, MH-47D, AND MH-47E AIRCRAFT.
6. ASSEMBLY COMPONENTS TO BE INSPECTED T-62T-2B (APU), P/N
160150-10 OR 160150-100.
7. PARTS TO BE INSPECTED - N/A.
8. INSPECTION PROCEDURES
A. INSPECT AIRCRAFT CONDITION CHANGE DA FORM 2408-16 TO
DETERMINE TIME SINCE NEW (TSN) OF THE APU (BASED UPON AIRCRAFT
FLIGHT HOURS).
B. IF THE APU SERIAL NUMBER IS LISTED IN PARAGRAPH 9B BELOW, IT
HAS A COMPRESSOR WHEEL WHICH WAS INSPECTED DURING DEPOT OVERHAUL.
DETERMINE THE TIME IT HAS BEEN OPERATING SINCE THE INSPECTION. IF
HOURS CANNOT BE DETERMINED, CONTACT EITHER 2410 HOTLINE (LISTED IN
PARA 16D) OR LOGISTICAL POC (LISTED IN PARA 16B).
NOTE
ALL HISTORICAL RECORD DATA FOR APU HOURS
REFERS TO AIRCRAFT OPERATING TIME, NOT APU
OPERATING TIME.
C. FOR TSN (8A ABOVE) AND TIME SINCE INSPECTED IF APPLICABLE
(8B ABOVE), CALCULATE THE STARTS ACCUMULATED. MULTIPLY THE TSN AND
THE AIRCRAFT TIME SINCE INSPECTED BY 4. THIS CALCULATED NUMBER OF
STARTS BASED UPON APU TIME SINCE NEW WILL BE USED TO DETERMINE THE
LIFE LIMIT AND RESTRICTIONS AS STATED IN PARAGRAPH 9C BELOW AS WELL
AS THE BASIS FOR RECORDING AND MAINTAINING APU STARTS IN THE FUTURE.
THE TIME SINCE INSPECTED START NUMBER WILL BE USED TO ALLOW EXTENDED
LIFE OF THE APU WHEEL BASED UPON THE INSPECTION AND PREDICTED CRACK
GROWTH PROPAGATION.
9. CORRECTION PROCEDURES
NOTE
THE 5360 STARTS SINCE NEW MAY ONLY BE EXCEEDED
IF THE APUS HAVE UNDERGONE NDI INSPECTION OF
THE COMPRESSOR WHEEL. IN THIS CASE AN
ADDITIONAL 2100 STARTS SINCE INSPECTION IS
AUTHORIZED REGARDLESS OF THE ORIGINAL STARTS
SINCE NEW.
A. ANY APU EXCEEDING 5360 STARTS IS UNSERVICEABLE (1340 TIMES 4
EQUALS 5360) UNLESS A NDI INSPECTION OF COMPRESSOR WHEEL WAS
PERFORMED AT OVERHAUL OR EXTENSION IS AUTHORIZED PER PARA 9B.
B. THE FOLLOWING T-62T-2B APU'S HAVE AN OPERATING LIMIT OF
2100 STARTS SINCE INSPECTION (SSI) (525 HOURS TIMES 4 EQUALS 2100
STARTS). FOR APUS LISTED USE EITHER STARTS SINCE NEW (5360) OR
STARTS SINCE INSPECTION (2100) TO ESTABLISH THE LIMIT WHICHEVER
YIELDS THE GREATER REMAINING LIFE.
827502 827503 827504 827514 827516 827517
827523 827528 837504 837508 837509 837511
837515 837519 837520 837523 837524 837525
847504 847507 847509 847512 847514 847515
847516 847519 847520 847523 847802 850606
857501 857519 857525 857529 857538 857540
857546 857548 857555 857565 857566 857567
857571 867501 867502 867503 867506 867508
867516 867519 867527 867532 867533 867535
867545 867548 867558 867591 867559 877501
877502 877505 877507 877508 877509 877525
877528 877529 877535 877539 877552 877556
877557 877562 877563 877564 877570 877572
887507 887511 887514 887528 887530 887533
887536 887543 887556 887557 887558 897507
897509 897511 897514 897517 897520 897521
897524 897526 897537 897539 897546 897547
897549 897550 897561 897564 897568 897569
897570 897572 897575 897583 910004 910010
920074 920077 920115 920119 930135 930138
930152 930167 930168 930191 930199
A00001 A00002 A00003 A00014 A00028
A00029 A00031 A00050 A00053 A00066
A00059 A00060 A00067 A00077 A00082
A00083 A00095 A00104
SP-E910004 SP-E910010 SP-E920077
SP-E920093 SP-E920119 SPE-930135
SP-E930136 SP-E930145 SP-E930146
SP-E930158 SP-E920130 SP-E930137
SP-E93167 SP-E930168 SPE930170
SP-E930191 SP-E930199
IN ADDITION, COMPRESSOR WHEELS INSPECTED IN THE FUTURE WILL BE
IDENTIFIED WITH A SERIAL NUMBER SUFFIX OF //IW//. THIS WILL BE
REFLECTED IN THE DA FORM 2410 ACCOMPANYING THE UNIT.
C. THE FOLLOWING RESTRICTIONS APPLY TO SERVICEABLE APUS WITH
OVER 2100 STARTS (525 APU HOURS TIMES 4 EQUALS 2100 STARTS TSN OR
TSI) WHICH DO NOT HAVE A SERVICE LIFE EXTENSION AUTHORIZED PER PARA
9B. THOSE AIRCRAFT WILL HAVE THE CONDITION STATUS CODE CHANGED TO A
CIRCLED RED //X//. THE CIRCLED RED //X// ENTRY SHALL STATE "AIRCRAFT
RESTRICTED TO APU GROUND AND FLIGHT OPERATIONS IAW SOF CH-47-00-01".
WHILE THE AIRCRAFT IS ON A CIRCLED RED //X// IT MAY BE REPORTED AS
FULLY MISSION CAPABLE (FMC).
(1) DO NOT OPERATE THE APU IN-FLIGHT UNLESS AN EMERGENCY
CONDITION EXISTS. ACCEPTABLE EMERGENCY CONDITIONS ARE FOUND IN
CHAPTER 9 OF TM 55-1520-240-10 AND TM 1-1520-252-10.
(2) ONLY MAINTENANCE REQUIRING APU OPERATION SHOULD BE
PERFORMED WITH THE APU RUNNING. EVERY EFFORT SHOULD BE MADE TO
MINIMIZE APU STARTS.
(3) DURING OPERATIONAL USE OF THE AIRCRAFT, NO ONE OTHER
THAN ESSENTIAL PERSONNEL SHALL BE ON BOARD AT ANY TIME THE APU IS IN
OPERATION (EXCEPT IN CASE OF EMERGENCIES). AVOID STANDING IN THE
PLANE OF ROTATION OF THE APU, EITHER ON THE RAMP, OR TO EITHER SIDE
OF THE AIRCRAFT AT STATION 594 WHEN THE APU IS IN OPERATION. NO ONE
SHALL BE PERMITTED TO MOVE INTO OR OUT OF THE AIRCRAFT BY WAY OF THE
RAMP WHEN THE APU IS IN OPERATION. ANY MOVEMENT THROUGH THE PLANE OF
ROTATION OF THE APU ALONGSIDE OF THE AIRCRAFT SHALL BE ACCOMPLISHED
AS QUICKLY AS POSSIBLE.
(4) NO APU WITH GREATER THAN 2100 STARTS TSN OR TSI SHALL
BE USED IN PUBLIC DISPLAYS.
(5) UTILIZE AVIATION GROUND POWER UNIT (AGPU) FOR STARTING
AND MAINTENANCE WHENEVER POSSIBLE.
(6) DO NOT OPERATE THE APU WHILE INSIDE A HANGAR.
(7) THE PERSON IN THE COCKPIT WHILE THE APU IS STARTED
WILL MONITOR THE APU UNTIL THE "APU ON" LIGHT IS ON. THIS PERSON
WILL ACTIVATE THE APU SHUTOFF SWITCH IN THE EVENT A COMPRESSOR BURST
OCCURS DURING APU START.
(8) POST A FIRE GUARD ANY TIME THE APU IS STARTED.
(9) MINIMIZE APU STARTS IN HIGH DENSITY AREAS.(PERSONNEL,
EQUIPMENT OR STRUCTURES).
D. THE FOLLOWING FORMS AND RECORDS INSTRUCTIONS WILL APPLY:
(1) APU STARTS WILL NOW BE COUNTED. ONCE THE APU START
NUMBER HAS BEEN CALCULATED IAW PARA 8 ABOVE, ENTER THE NUMBER OF
STARTS IN THE DA FORM 2408-13, BLOCK 7 (APU HISTORY) CURRENT STARTS.
(2) APU STARTS FOR EACH FLIGHT WILL BE DOCUMENTED IN DA
FORM 2408-12, BLOCK 6A (APU: STARTS) AND AT THE END OF THE MISSION
DAY TOTALED IN BLOCK 8 (APU: STARTS), THEN TRANSFERRED TO DA FORM
2408-13, BLOCK 7, TODAY STARTS. APU STARTS FOR MAINTENANCE OR OTHER
PURPOSES (DAILIES, RAISING THE RAMP, USING THE HEATER, ETC) NOT
ASSOCIATED WITH A FLIGHT NOR ACCOUNTED FOR ON THE DA FORM 2408-12
WILL BE RECORDED, IN PENCIL ON THE DA FORM 2408-13, BLOCK 7, APU
HISTORY STARTS TODAY BLOCK. WHEN CLOSING OUT THE FORMS AT THE END OF
A MISSION DAY, THE TOTAL, FROM THE DA FORM 2408-12 WILL BE BROUGHT
FORWARD AND APPENDED TO THE STARTS IN THE 13 APU HISTORY STARTS TODAY
BLOCK BEFORE ADDING TO CURRENT STARTS TO GET THE TOTAL STARTS.
(3) A RUNNING TOTAL OF STARTS WILL BE KEPT ON THE DA FORM
2408-13. APU STARTS WILL NOT BE ZEROED AT THE 15TH OR END OF THE
MONTH. ANY TIME A T-62T-2B APU IS REMOVED/REPLACED OR TURNED IN FOR
REPAIR, COPY THE TOTAL NUMBER OF ACCUMULATED STARTS FROM THE LATEST
DA FORM 2408-13 TO THE APU DA FORM 2408-5-1 (EQUIPMENT MODIFICATION
RECORD COMPONENT) AND THE DA FORM 2408-16 (FOR THE APU) ALONG WITH
THE DATE, AND THE AIRCRAFT TAIL NUMBER. ALSO, COMPLETE BLOCKS 16 (APU
SSN) ON THE DA FORM 2410.
(4) ENSURE THAT THE DA FORM 2408-13, BLOCK 7, CURRENT
STARTS, ARE CHANGED WHEN AN APU IS REMOVED/REPLACED. GET THE NEW APU
STARTS FROM THE APU DA FORM 2408-5-1 OR THE APU DA FORM 2408-16.
(5) UNITS WILL CREATE A DA FORM 2408-16 FOR EACH APU. ANY
TIME AN APU IS MOVED FROM ONE AIRCRAFT TO ANOTHER OR TURNED IN FOR
OVERHAUL, THE TOTAL NUMBER OF ACCUMULATED STARTS WILL BE TAKEN FROM
THE LATEST DA FORM 2408-13 AND ENTERED IN BLOCK 7, SIGNIFICANT
HISTORICAL DATA, OF DA FORM 2408-16 AND BLOCK 16 OF THE DA FORM 2410.
FOR APU'S RECEIVED FROM OVERHAUL THE NUMBER OF ACCUMULATED STARTS
WILL BE TRACKED AGAINST THE COMPRESSOR WHEEL.
(6) NEW COMPRESSOR WHEELS, P/N 4503340 AND NEW TURBINE
WHEEL P/N 4503999, WHICH MAKE UP THE NEW TURBINE ASSY, P/N 4504001,
WILL HAVE ACCUMULATIVE STARTS TRACKED. THESE PARTS ARE USED ON APU
P/N 160150-10A OR 160150-100A.
10. SUPPLY/PARTS AND DISPOSITION -
A. PARTS REQUIRED - ITEMS CITED IN PARAGRAPHS 6 MAY BE REQUIRED
TO REPLACE DEFECTIVE ITEMS.
B. REQUISITIONING INSTRUCTIONS - CONTACT LOGISTICAL POINT OF
CONTACT IN PARAGRAPH 16B FOR REQUISITIONING INSTRUCTIONS FOR ITEMS
CITED IN PARAGRAPH 6.
C. BULK AND CONSUMABLE MATERIALS - N/A.
D. DISPOSITION - HOLD ANY DISCREPANT PART/COMPONENT PENDING
DISPOSITION INSTRUCTIONS FROM LOGISTICAL POINT OF CONTACT IN
PARAGRAPH 16B IF DISPOSITION WAS NOT RECEIVED WITH REQUISITIONING
INSTRUCTIONS. RETAIL SMA ACTIVITIES WILL PROVIDE 100% CREDIT FOR
TURN-INS REFLECTING THE DEFECTIVE ARMY MANAGED NSN AND PROJECT
CODE "XF3" (X-RAY-FOXTROT-THREE). AMCOM WILL PROVIDE 100% CREDIT
TO ARMY NATIONAL GUARD UNITS THAT RETURN THE DEFECTIVE PART USING
THE SAME CRITERIA. IN ORDER TO PROVIDE THE QUICKEST TURN-AROUND
OF SERVICEABLE ASSETS, RETURNED UNSERVICEABLE APUS SHOULD BE SHIPPED
IN THE MOST EXPEDITIOUS MANNER POSSIBLE.
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 - N/A.
12. APPLICATION -
A. CATEGORY OF MAINTENANCE AVUM/AVIM/DEPOT/CONTRACTOR TEAM, AS
APPLICABLE. AIRCRAFT DOWNTIME IS - N/A.
B. ESTIMATED TIME REQUIRED 0.5 HRS FOR RECORDS CHECKS.
C. ESTIMATED COST IMPACT TO THE FIELD N/A.
E. PUBLICATIONS WHICH REQUIRE CHANGE AS A RESULT OF THIS
MESSAGE -
(1) TB 1-1500-341-01
(2) TM 55-1520-240-23-1
(3) TM 1-1520-252-23-1
(4) TM 55-2835-205-23P
(5) DA 738-751
A COPY OF THIS MESSAGE SHALL BE INSERTED IN THE APPROPRIATE TB AS
AUTHORITY TO IMPLEMENT THE CHANGE UNTIL THE PRINTED CHANGE IS
RECEIVED.
13. REFERENCES
A. MESSAGE, CDR ATCOM, CH-47-96-ASAM-02.
B. MESSAGE, CDR ATCOM, CH-47-97-ASAM-09.
C. TM 55-1520-240-10, CH-47D OPERATORS MANUAL.
D. TM 1-1520-252-10, MH-47E OPERATORS MANUAL.
E. TB 55-1500-341-01, AIRCRAFT COMPONENTS REQUIRING
MAINTENANCE MANAGEMENT AND HISTORICAL REPORTS.
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), 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) -
UPON COMPLETION OF INSPECTION, UNITS WILL FORWARD A PRIORITY MESSAGE
TO THE LOGISTICAL POINT OF CONTACT IDENTIFIED IN PARAGRAPH 16B. THE
REPORT WILL CITE AIRCRAFT SERIAL NUMBER, APU SERIAL NUMBER, AND APU
TIME SINCE NEW (TSN), SSI, THE NEW RECORDED STARTS AND THE DATE
RECORDS WERE CONVERTED. INSPECTION AND REPORT WILL BE COMPLETED NO
LATER THAN 7 DAYS AFTER RECEIPT OF MESSAGE.
C. REPORTING MESSAGE RECEIPT (SPARES) - N/A.
D. TASK/INSPECTION REPORTING SUSPENSE DATE (SPARES) - REPORT
S/N AND TSN OF ALL APU'S IN STOCK AT ALL LEVELS TO THE LOGISTICAL
POINT OF CONTACT IN PARAGRAPH 16B. UNITS UPON RECEIPT OF SPARE APU'S
THAT HAVE NOT CONVERTED THE HOURS WILL CONVERT TO STARTS AT THIS
TIME.
E. THE FOLLOWING FORMS ARE APPLICABLE AND ARE TO BE COMPLETED
IAW DA PAM 738-751, 15 MAR 99 -
NOTE
ULLS-A USERS WILL USE APPLICABLE "E" FORMS.
(1) DA FORM 2408-5-1, EQUIPMENT MODIFICATION RECORD (APU).
(2) DA FORM 2408-13, AIRCRAFT STATUS INFORMATION RECORD.
(3) DA FORM 2408-13-1, AIRCRAFT INSPECTION AND MAINTENANCE
RECORD.
(4) DA FORM 2408-15, HISTORICAL RECORD FOR AIRCRAFT
(ANNOTATE THE SERIAL NUMBER OF THE APU).
(5) DA FORM 2408-16, AIRCRAFT COMPONENT HISTORICAL RECORD.
15. WEIGHT AND BALANCE - N/A.
16. POINTS OF CONTACT -
A. TECHNICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. JAMES
M. WILSON, AMSAM-RD-AE-I-C-H, DSN 897-3337 OR (256) 313-3337,
DATAFAX IS 897-4348. E-MAIL IS "JAMES.WILSON@REDSTONE.ARMY.MIL".
B. LOGISTICAL POINT OF CONTACT FOR THIS MESSAGE IS CW5 AL
TRIVITT, SFAE-AV-CH-L, DSN 897-3381 OR (256) 313-3381, DATAFAX
897-4348. E-MAIL IS "TRIVITTA@PEOAVN.REDSTONE.ARMY.MIL".
C. WHOLESALE MATERIEL POINT OF CONTACT (SPARES) - N/A.
D. 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. E-MAIL IS "WALDECK-AB@REDSTONE.ARMY.MIL".
THE "2410 HOTLINE" IS DSN 897-2410 OR (256)313-2410. ALTERNATE
NUMBER IS DSN 788-6092 OR (256)842-6092.
E. 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".
F. 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
"WITTSTROM-JL@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 "SAMMONS-RW@REDSTONE.ARMY.MIL".
HUNTSVILLE, AL IS GMT MINUS 6 HRS.
G. AFTER HOURS CONTACT THE AMCOM COMMAND OPERATIONS CENTER
(COC) DSN 897-2066/7 OR (256) 313-2066/7.
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