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:CDRAMCOM REDSTONE ARSENAL AL//AMSAM-SF-A//
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:AIG 8881
:AIG 9004
:AIG 7471
:AIG 12124
: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//
: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//
:CDRUSASAC NEW CUMBERLAND PA//AMSAC-SALO-UK//
:SINGAPORE AF FMS SINGAPORE SN
:ODC SINGAPORE SN
:ODC MADRID SP//ASM//
:SPAIND ARMY FMS MADRID SP
:AIT TAIPEI TW//TECH//
:TAIWAN ARMY FMS TAIPEI TW
: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
:FAA SOUTHWEST RGN HQ FORT WORTH TX//ASW-100//
:CDRAMC ALEXANDRIA VA//AMCLG-OP-AVN/AMCSF-A/AMCRDA//
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TEXT
:UNCLAS
SUBJECT - SAFETY OF FLIGHT MESSAGE, TECHNICAL, RCS CSGLD-
1860(R1), ALL H-47 AIRCRAFT, COMBINING TRANSMISSION COOLING FAN
DRIVE SHAFT INSPECTIONS, CH-47-00-07, (TB 1-1520-240-20-129).
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
IAW AR 95-1, PARA 6-6A, MACOM COMMANDERS MAY AUTHORIZE TEMPORARY
EXCEPTION FROM SOF MESSAGE REQUIREMENTS. EXCEPTION MAY ONLY
OCCUR WHEN COMBAT OPERATIONS OR MATTER OF LIFE OR DEATH IN CIVIL
DISASTERS OR OTHER EMERGENCIES ARE SO URGENT THAT THEY OVERRIDE
THE CONSEQUENCES OF CONTINUED AIRCRAFT OPERATION.
A. AIRCRAFT IN USE - UPON RECEIPT OF THIS MESSAGE, MAKE THE
FOLLOWING ENTRY ON THE DA FORM 2408-13-1. ENTER A RED HORIZONTAL
DASH //-// STATUS SYMBOL WITH THE FOLLOWING STATEMENT: "INSPECT
COMBINING TRANSMISSION COOLING FAN DRIVE SHAFT IAW CH-47-00-07,
TB 1-1520-240-20-129 PRIOR TO NEXT FLIGHT, BUT NLT 11 OCT 00."
CLEAR THE RED HORIZONTAL DASH //-// ENTRY WHEN THE PROCEDURES IAW
PARA 8 AND 9 ARE COMPLETED. THE AFFECTED AIRCRAFT SHALL BE
INSPECTED AS SOON AS PRACTICAL BUT NO LATER THAN 11 OCT 00.
COMMANDERS WHO ARE UNABLE TO COMPLY WITH THE REQUIREMENTS OF THIS
MESSAGE WITHIN THE TIME FRAME SPECIFIED WILL UPGRADE THE AFFECTED
AIRCRAFT STATUS SYMBOL TO A RED //X//.
B. AIRCRAFT IN DEPOT MAINTENANCE - DEPOT COMMANDERS WILL NOT
ISSUE AIRCRAFT UNTIL THEY ARE IN COMPLIANCE WITH THIS MESSAGE.
C. AIRCRAFT UNDERGOING MAINTENANCE - COMMANDERS AND FACILITY
MANAGERS WILL NOT ISSUE AIRCRAFT UNTIL THEY ARE IN COMPLIANCE
WITH THIS MESSAGE.
D. AIRCRAFT IN TRANSIT -
(1) SURFACE/AIR SHIPMENT - PRIOR TO FIRST FLIGHT.
(2) FERRY STATUS -
(A) PRIOR TO NEXT FLIGHT.
(B) BOEING WILL INSPECT DD 250 AIRCRAFT PRIOR TO
THOSE AIRCRAFT DEPARTING FOR FERRY TO FINAL DESTINATION.
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 - UPON RECEIPT OF THIS MESSAGE, DEPOT AND
MATERIEL ACTIVITY COMMANDERS WILL ENSURE THE MATERIEL CONDITION
TAGS OF ALL ITEMS IN ALL CONDITION CODES LISTED IN PARAGRAPHS 6
AND 7 ARE ANNOTATED TO READ: "CH-47-00-07, TB 1-1520-240-20-129,
COMBINING TRANSMISSION COOLING FAN DRIVE SHAFT INSPECTIONS NOT
COMPLIED WITH".
(1) WHOLESALE STOCK - N/A.
(2) RETAIL STOCK - UPON RECEIPT OF THIS MESSAGE,
COMMANDERS AND FACILITY MANAGERS MAINTAINING RETAIL STOCK AT
INSTALLATION LEVEL AND BELOW SHALL CONTACT THE SUPPORTED AVIATION
UNIT TO PERFORM THE PROCEDURES REQUIRED IAW PARAGRAPHS 8 AND 9 ON
SUSPECT MATERIEL. RETURN DISCREPANT MATERIEL IAW PARAGRAPH 10.
REPORT COMPLIANCE WITH THIS MESSAGE IAW PARAGRAPH 14D(2).
G. COMPONENTS/PARTS IN WORK (DEPOT LEVEL AND OTHERS) -
COMPONENTS/PARTS IN WORK MUST COMPLY WITH THIS MESSAGE BEFORE
THEY ARE ISSUED.
2. TASK/INSPECTION SUSPENSE DATE - COMPLETE THE INSPECTION IAW
PARAGRAPH 8 PRIOR TO NEXT FLIGHT BUT NLT 11 OCT 00 AND REPORT IAW
PARA 14B.
3. REPORTING COMPLIANCE SUSPENSE DATE - REPORT COMPLIANCE IAW
PARA 14A NLT 18 OCT 00.
4. SUMMARY OF PROBLEM -
A. A MH-47E AIRCRAFT EXPERIENCED A FAILURE OF THE COMBINING
TRANSMISSION COOLING FAN DRIVE SHAFT, P/N 145D5319-5. FAILURE OF
THIS SHAFT WAS CONTAINED BY THE "STOVE PIPE". BUT, SINCE THE
COOLING FAN WAS NO LONGER OPERATING, THE OIL TEMPERATURE OF THE
COMBINING TRANSMISSION AND BOTH ENGINE TRANSMISSIONS EXCEEDED THE
OPERATING LIMITS. THIS HIGH TEMPERATURE CONDITION REQUIRED
LANDING OF THE AIRCRAFT AS SOON AS POSSIBLE WITHOUT DELAY AND
REPLACEMENT OF THE COMBINING AND BOTH ENGINE TRANSMISSIONS.
CURRENTLY THERE IS AN ONGOING INVESTIGATION AS TO THE CAUSE OF
THE FAN SHAFT FAILURE.
B. FOR MANPOWER/DOWNTIME AND FUNDING IMPACTS SEE PARA 12.
C. THE PURPOSE OF THIS MESSAGE IS TO:
(1) REMOVE FROM SERVICE THOSE COOLING FAN SHAFTS AND
COMBINING TRANSMISSIONS FOUND UNSERVICEABLE, IAW THIS MESSAGE.
(2) GATHER DATA TO ASSIST IN THE INVESTIGATION.
(3) REQUIRE AN INITIAL AND RECURRING (EVERY 100 HOURS)
INSPECTION OF THE COMBINING TRANSMISSION COOLING FAN DRIVE SHAFT.
(4) REQUIRE AN INITIAL AND RECURRING (EVERY 100 HOURS)
INSPECTION OF THE COMBINING TRANSMISSION COOLING FAN DRIVE GEAR
SPLINES.
5. END ITEMS TO BE INSPECTED - ALL H-47 AIRCRAFT.
6. ASSEMBLY COMPONENTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
COMBINING TRANSMISSION 145D5300-21 NO NSN
145D5300-20 1615-01-464-3974
145D5300-16 1615-01-397-9921
145D5300-17 NO NSN
145D5300-15 NO NSN
145D5300-13 1615-01-310-4980
145D5300-12 1615-01-310-4981
145D5300-11 1615-01-315-9365
145D5300-10 1615-01-315-4069
145D5300-9 1615-01-312-2390
145D5300-5 1615-01-216-3828
145D5300-3 1615-01-114-0850
7. PARTS TO BE INSPECTED -
COOLING FAN DRIVE SHAFT 145D5319-5 3040-01-310-4977
8. INSPECTION PROCEDURES - THE FOLLOWING INSPECTIONS ARE
REQUIRED TO BE PERFORMED BY THE TASK/INSPECTION SUSPENSE DATE OF
PARAGRAPH 2 AND EVERY 100 FLIGHT HOURS THEREAFTER.
NOTE
COOLING FAN SHAFT, P/N 145D5319-7 IS NOT
INSPECTABLE UNDER THIS SOF. INSPECTIONS,
FLIGHT OPERATIONS AND RESTRICTIONS OF THE -7
FAN SHAFT ARE DIRECTED BY SAFETY OF FLIGHT
MESSAGE CH-47-98-02, TB 1-1520-240-20-105,
DTG 161231Z.
NOTE
AIRCRAFT THAT ARE AWAY FROM HOME STATION OR
THE NEAREST AVAILABLE MAINTENANCE FACILITY ARE
AUTHORIZED A RETURN FLIGHT TO HOME STATION NOT
TO EXCEED 6 FLIGHT HOURS, NOT TO EXCEED 2000 FT
AGL WITH NO FLIGHTS OVER WATER WHEN ANOTHER
GROUND ROUTE IS AVAILABLE EVEN IF THE LAND
ROUTE IS LONGER IN DISTANCE.
A. REMOVE THE FAN SHAFT IAW TM 55-1520-240-23, TASK 6-182
(CH-47D) OR TM 1-1520-252-23, TASK 6-220 (MH-47E).
B. USING 10X MAGNIFICATION, VISUALLY INSPECT THE ALUMINUM
FAN SHAFT TUBE FOR CRACKS EXTENDING FROM UNDER THE STEEL ADAPTERS.
NO CRACKS ARE ALLOWED. IF CRACKS ARE FOUND PROCEED TO PARAGRAPH 9.
CAUTION
DO NOT USE TOOLS TO CHECK FOR LOOSENESS
ON THE JO-BOLTS, DAMAGE TO SHAFT WILL RESULT.
C. INSPECT THE JO-BOLTS THAT ATTACH THE ADAPTERS TO THE FAN
SHAFT TUBE FOR LOOSENESS. ATTEMPT TO TURN THE BOLTS BY HAND ONLY.
IF THE BOLTS CAN BE TURNED BY HAND PROCEED TO PARAGRAPH 9.
D. PERFORM A CHECK OF THE FAN SHAFT SPLINE WEAR PER TM 55-
1520-240-23, TASK 6-182.1 (CH-47D) OR TM 1-1520-252-23, TASK 6-
221 (MH-47E). IF THE SPLINE WEAR EXCEEDS 0.015 INCH PROCEED TO
PARAGRAPH 9.
E. PERFORM A CHECK OF THE COMBINING TRANSMISSION OUTPUT GEAR
SPLINE WEAR USING SPLINE WEAR (GO/NO-GO) GAUGE, P/N SK33330-018.
INSERT THE SPLINE WEAR (GO/NO-GO) GAUGE INTO THE OUTPUT GEAR WHERE
THE COOLING FAN SHAFT NORMALLY FITS. IF THE GAUGE DOES NOT FIT,
THEN THE TRANSMISSION IS SERVICEABLE. IF THE GAUGE FITS INTO THE
SPLINES OF THE OUTPUT GEAR, PROCEED TO PARAGRAPH 9.
CAUTION
TORQUE WRENCH MUST BE USED DURING REINSTALLATION
OF COOLER FAN DRIVE SHAFT RETAINING SHIELD
(DO NOT EXCEED 80 INCH POUNDS). FAILURE TO USE A
TORQUE WRENCH WILL RESULT IN DAMAGE TO THE
COMBINING TRANSMISSION.
F. RECORD SERIAL NUMBERS OF COMBINING TRANSMISSION AND FAN
DRIVE SHAFT AND IF POSSIBLE DETERMINE THE P/N OF THE TRANSMISSION
CARTRIDGE ASSEMBLY 145D5307-9, -7 OR -5. REPORT THIS INFORMATION TO
THE LOGISTICS POC IN PARA 16B.
G. REINSTALL FAN SHAFT AND FAN IAW TM 55-1520-240-23, TASK
6-186 (CH-47D) OR TM 1-1520-252-23, TASK 6-222.1 (MH-47E).
9. CORRECTION PROCEDURES -
A. THE FAN SHAFT IS UNSERVICEABLE IF CRACKS ARE FOUND OR IF
THE JO-BOLTS ARE FOUND TO BE LOOSE. CHANGE THE AIRCRAFT STATUS
TO A RED //X// AND MAKE THE FOLLOWING ENTRY ON THE 2408-13-1
"COMBINING TRANSMISSION COOLING FAN SHAFT HAS LOOSE JO-BOLTS.
CONTACT THE TECHNICAL POINT OF CONTACT IN PARAGRAPH 16A FOR
DISPOSITION INSTRUCTIONS." SUBMIT A CATEGORY I DEFICIENCY REPORT.
B. IF THE FAN DRIVE SHAFT SPLINE WEAR EXCEEDS 0.015 INCH,
CHANGE THE AIRCRAFT STATUS TO A RED //X// AND MAKE THE FOLLOWING
ENTRY ON THE 2408-13-1 "COMBINING TRANSMISSION COOLING FAN SHAFT
SPLINE WEAR EXCEEDS 0.015 INCH." CONTACT THE TECHNICAL POINT OF
CONTACT IN PARAGRAPH 16A FOR DISPOSITION INSTRUCTIONS. THE RED
//X// MAY BE CLEARED WHEN THE FAN SHAFT HAS BEEN REPLACED.
C. IF THE COMBINING TRANSMISSION FAN DRIVE GEAR FAILS THE
SPLINE WEAR (GO/NO-GO) GAUGE CHECK, THE COMBINING TRANSMISSION IS
UNSERVICEABLE. CHANGE THE AIRCRAFT STATUS TO A RED //X// AND MAKE
THE FOLLOWING ENTRY ON THE 2408-13-1 "COMBINING TRANSMISSION FAN
DRIVE GEAR FAILS THE SPLINE WEAR GAUGE CHECK." THE RED //X// MAY BE
CLEARED WHEN THE COMBINING TRANSMISSION HAS BEEN REPLACED. REFER
TO PARAGRAPH 10D FOR DISPOSITION INSTRUCTIONS.
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 USING NORMAL SUPPLY PROCEDURES. ALL REQUISITIONS SHALL USE
PROJECT CODE (CC 57-59) "X06" (X-RAY-ZERO-SIX).
NOTE
PROJECT CODE "X06"(X-RAY-ZERO-SIX) 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 -
(1) DISPOSE OF COMBINING TRANSMISSIONS REMOVED DUE TO
SPLINE WEAR USING NORMAL SUPPLY PROCEDURES. ALL TURN-IN DOCUMENTS
MUST INCLUDE PROJECT CODE (CC 57-59) "X06" (X-RAY-ZERO-SIX).
(2) CONTACT THE TECHNICAL POC LISTED AT PARA 16A FOR
DISPOSITION OF UNSERVICEABLE FAN SHAFTS.
E. DISPOSITION OF HAZARDOUS MATERIAL - N/A.
11. SPECIAL TOOLS AND FIXTURES REQUIRED - GO-NO-GO GAUGE, P/N
SK33330-018, NSN 5220-01-462-1741.
12. APPLICATION -
A. CATEGORY OF MAINTENANCE - AVUM. AIRCRAFT DOWNTIME WILL BE
CHARGED TO AVUM. REPORT AIRCRAFT NON-MISSION CAPABLE MAINTENANCE
(NMCM) WHILE UNDERGOING INSPECTION AND CORRECTION IAW THIS MESSAGE.
B. ESTIMATED TIME REQUIRED -
(1) FOR INSPECTION
(A) TOTAL OF 3 MAN-HOURS USING 1 PERSON.
(B) TOTAL OF 3 HOURS DOWNTIME FOR ONE END ITEM.
(2) FOR REPLACEMENT OF COMBINING TRANSMISSION
(A) TOTAL OF 50 MAN-HOURS USING 5 PERSONS.
(B) TOTAL OF 10 HOURS DOWNTIME FOR ONE END ITEM.
C. ESTIMATED COST IMPACT TO THE FIELD -
NOMENCLATURE PART NO./NSN QTY COST EA. TOTAL $
COOLING FAN DRIVE SHAFT 145D5319-5 1 $5618.00 $5618.00
3040-01-310-4977
OR
COMBINING TRANSMISSION 145D5300-20 1 $360,000.00 $360,000.00
1615-01-464-3974
OR
145D5300-21 1 $384,000.00 $384,000.00
NO NSN ASSIGNED
MAX TOTAL COST PER AIRCRAFT = $384,000.00
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 - THE FOLLOWING PUBLICATIONS SHALL BE CHANGED AS NOTED
BELOW TO REFLECT 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.
(1) TM 55-1520-240-23, AVIATION UNIT AND AVIATION
INTERMEDIATE MAINTENANCE MANUAL, CH-47D HELICOPTER.
(A) ADD A 100 HOUR INSPECTION TO TASK 1-92, OPERATING
TIME SPECIAL INSPECTION FOR AIRCRAFT ON PM/PMD. THE INSPECTION
REQUIREMENT SHALL READ AS FOLLOWS, "INSPECT THE COMBINING
TRANSMISSION COOLING FAN SHAFT PER TASK 6-182.1". ULLS-A UNITS WILL
USE THIS MESSAGE AS AUTHORITY TO ADD INSPECTION NUMBER A216 TO THE
ULLS-A INSPECTION MASTER FILE FOR TASK 6-182.1.
(B) ADD A 100 HOUR INSPECTION TO TASK 1-92, OPERATING
TIME SPECIAL INSPECTION FOR AIRCRAFT ON PM/PMD. THE INSPECTION SHALL
REQUIRE A CHECK OF THE COMBINING TRANSMISSION OUTPUT GEAR SPLINE WEAR
STEP USING THE SPLINE WEAR (GO/NO-GO) GAUGE, P/N SK33330-018. ULLS-A
UNITS WILL USE THIS MESSAGE AS AUTHORITY TO ADD INSPECTION NUMBER
A217 TO THE ULLS-A INSPECTION MASTER FILE FOR COMBINING TRANSMISSION
OUTPUT GEAR SPLINE WEAR.
(C) REVISE TASK 6-182.1 TO INCORPORATE THE INSPECTIONS
LISTED IN PARAGRAPHS 8 OF THIS SOF.
(2) TM 1-1520-252-23, AVIATION UNIT AND AVIATION
INTERMEDIATE MAINTENANCE MANUAL, MH-47E HELICOPTER.
(A) ADD A 100 HOUR INSPECTION TO TASK 1-100, OPERATING
TIME SPECIAL INSPECTION/ACTIONS FOR AIRCRAFT ON PM/PMD. THE
INSPECTION REQUIREMENT SHALL READ AS FOLLOWS, "INSPECT THE COMBINING
TRANSMISSION COOLING FAN SHAFT PER TASK 6-221".
(B) ADD A 100 HOUR INSPECTION TO TASK 1-100, OPERATING
TIME SPECIAL INSPECTION/ACTIONS FOR AIRCRAFT ON PM/PMD. THE
INSPECTION SHALL REQUIRE A CHECK OF THE COMBINING TRANSMISSION
OUTPUT GEAR SPLINE WEAR STEP USING THE SPLINE WEAR (GO/NO-GO) GAUGE,
P/N SK33330-018.
(C) REVISE TASK 6-221 TO INCORPORATE THE INSPECTIONS
LISTED IN PARAGRAPHS 8 OF THIS SOF.
13. REFERENCES -
A. DA PAM 738-751, 15 MAR 99.
B. TM 55-1520-240-23, AVIATION UNIT AND AVIATION INTERMEDIATE
MAINTENANCE MANUAL, CH-47D HELICOPTER.
C. TM 1-1520-252-23, AVIATION UNIT AND AVIATION INTERMEDIATE
MAINTENANCE MANUAL, MH-47E HELICOPTER.
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, COMMANDERS WILL FORWARD A PRIORITY MESSAGE,
DATAFAX OR E-MAIL TO CDR, AMCOM, ATTN: AMSAM-SF-A (SOF COMPLIANCE
OFFICER), REDSTONE ARSENAL, AL 35898-5000, 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
AND TB 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, COMMANDERS WILL FORWARD A PRIORITY
MESSAGE TO: LOGISTIC POC, PARAGRAPH 16B. THE REPORT WILL CITE
THIS MESSAGE AND TB NUMBER, DATE OF INSPECTION, AIRCRAFT SERIAL
NUMBER, AIRCRAFT AND COMPONENT HOURS, AND RESULTS OF THE INSPECTION.
INSPECTION AND REPORTS WILL BE COMPLETED NLT 18 OCT 00.
C. REPORTING MESSAGE RECEIPT (SPARES) - N/A
D. TASK/INSPECTION REPORTING SUSPENSE DATE (SPARES).
(1) MATERIEL IN WHOLESALE DEPOT STORAGE - N/A.
(2) MATERIEL IN RETAIL STORAGE - COMMANDERS AND FACILITY
MANAGERS WILL REPORT COMPLIANCE WITH THIS MESSAGE TO THE LOGISTICAL
POINT OF CONTACT IN PARAGRAPH 16B NLT 4 OCT 00. REPORT THE QUANTITY
INSPECTED BY CONDITION CODE AND THE RESULTING CONDITION CODE. REPORT
BY E-MAIL OR DATAFAX AND PROVIDE LOCAL POINT OF CONTACT.
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
(COMBINING TRANSMISSION).
(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.
(5) DA FORM 2408-16, AIRCRAFT COMPONENT HISTORICAL RECORD.
(6) DA FORM 2410, COMPONENT REMOVAL AND REPAIR/OVERHAUL
RECORD. (ONLY IF THE COMBINING TRANSMISSION OR FAN DRIVE SHAFT ARE
REMOVED AND REPLACED)
(7) DD FORM 1574/DD FORM 1574-1, SERVICEABLE TAG/LABEL -
MATERIEL (COLOR YELLOW). ANNOTATE REMARKS BLOCK WITH "INSPECTED
SERVICEABLE IAW CH-47-00-07, TB 1-1520-240-20-129."
(8) DD FORM 1577-2/DD FORM 1577-3, UNSERVICEABLE
(REPARABLE) TAG/LABEL - MATERIEL (COLOR GREEN). ANNOTATE REMARKS
BLOCK WITH "UNSERVICEABLE IAW CH-47-00-07, TB 1-1520-240-20-129."
(9) SF FORM 368, PRODUCT QUALITY DEFICIENCY REPORT
15. WEIGHT AND BALANCE - N/A.
16. POINTS OF CONTACT -
A. TECHNICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. LARRY
WIESCHHAUS, AMSAM-RD-AE-E-I-P-C, DSN 897-3341 OR (256) 313-3341,
DATAFAX IS DSN 897-4348 OR (256) 313 3341. E-MAIL IS
"LARRY.WIESCHHAUS@REDSTONE.ARMY.MIL".
B. LOGISTICAL POINT OF CONTACT FOR THIS MESSAGE IS BILL
OLSON, (SFAE-AV-CH-L), DSN 897-3379 OR (256) 313-3379, DATAFAX IS
EXT 4348. E-MAIL IS "WILLIAM.OLSON@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. E-MAIL IS
"ANN.WALDECK@REDSTONE.ARMY.MIL".
D. SAFETY POINTS OF CONTACT ARE -
(1) PRIMARY - MR. FRANK ROSEBERY (SAIC), AMSAM-SF-A, DSN
788-8631 OR (256) 842-8631, DATAFAX IS DSN 897-2111 OR (256) 313-
2111. E-MAIL IS "FRANK.ROSEBERY@REDSTONE.ARMY.MIL".
(2) ALTERNATE - MR. RUSSELL PEUSCH, AMSAM-SF-A, DSN
788-8632 OR (256) 842-8632, DATAFAX IS DSN 897-2111 OR (256) 313-
2111. E-MAIL IS "RUSSELL.PEUSCH@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 897-0410 OR
(256) 313-0410. EMAIL IS "WITTSTROMJL@REDSTONE.ARMY.MIL" OR MR.
RONNIE W. SAMMONS, AMSAM-SA-CS-NF, DSN 897-0408 OR (256) 313-0408.
DATAFAX IS DSN 897-0411 OR (256) 313-0411. EMAIL IS
"SAMMONSRW@REDSTONE.ARMY.MIL". HUNTSVILLE, AL IS GMT MINUS 5 HRS.
G. AFTER HOURS CONTACT THE AMCOM COMMAND OPERATIONS CENTER
(COC) DSN 897-2066/7 OR (256) 313-2066/7.
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