1 21 161228Z FEB 99 PP PP UUUU AA ZELX
FROM
:CDRAMCOM REDSTONE ARSENAL AL//AMSAM-SF-A//
TO
:AIG 8881
:AIG 9004
:AIG 9042
: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//
:CHJUSMAG 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
:CJUSMAG THAI 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
:FAA SOUTHWEST RGN HQ FORT WORTH TX//ASW-100//
:CDRAMC ALEXANDRIA VA//AMCMR/AMCCS/AMCSM-WAA//
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TEXT
:UNCLAS
THIS IS A REVISION TO THE CORRECTED COPY.
THIS REVISION AFFECTS ONLY PARAGRAPH 9G.
SUBJECT - AVIATION SAFETY ACTION MESSAGE, MAINTENANCE MANDATORY,
RCS CSGLD-1860(R1), ALL H-47 SERIES HELICOPTERS, ACTIONS TO
REDUCE SUSCEPTIBILITY TO FLIGHT CONTROL LOCK-UP AND/OR UNCOMMANDED
MANEUVERS. CH-47-99-ASAM-02 (TB 1-1520-240-20-107)
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 ADDRESSES 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 CIRCLED RED //X//. THE CIRCLED RED //X// ENTRY WILL STATE
"AIRCRAFT RESTRICTED TO FLIGHT OPERATIONS AND INSPECTION
PROCEDURES IAW ASAM CH-47-99-ASAM-02. THE AFFECTED AIRCRAFT WILL
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 - SAME AS PARA 1A.
D. AIRCRAFT IN TRANSIT -
(1) SURFACE/AIR SHIPMENT - WITHIN 10 FLIGHT HOURS OR 14
DAYS OF ARRIVAL.
(2) FERRY STATUS -
(A) INSPECT AT FINAL DESTINATION.
(B) THOSE AIRCRAFT THAT HAVE A DD 250 AND ARE AT
BOEING HELICOPTER COMPANY WILL BE INSPECTED PRIOR TO FERRY TO
FINAL DESTINATION.
E. MAINTENANCE TRAINERS (CATEGORY A AND B) - COMPLY NO
LATER THAN 13 AUG 99.
F. COMPONENT/PARTS IN STOCK AT ALL LEVELS (DEPOT AND
OTHERS) INCLUDING WAR RESERVES - THE STATEMENT "CH-47-99-ASAM-02
NOT COMPLIED WITH" WILL BE ENTERED ON THE SERVICEABILITY TAG OF
ALL SERVOCYLINDERS LISTED IN PARAGRAPH 6 OF THIS MESSAGE.
G. COMPONENTS/PARTS IN WORK (DEPOT LEVEL AND OTHERS) - THE
STATEMENT "CH-47-99-ASAM-02 NOT COMPLIED WITH" WILL BE ENTERED ON
THE SERVICEABILITY TAG OF ALL SERVOCYLINDERS LISTED IN PARAGRAPH 6
OF THIS MESSAGE.
2. TASK/INSPECTION SUSPENSE DATE - COMPLY WITH PARAGRAPH 8
WITHIN THE NEXT 10 FLIGHT HOURS/ 14 DAYS WHICH EVER OCCURS FIRST.
3. REPORTING COMPLIANCE SUSPENSE DATE - NO LATER THAN 9 MAR 99
IAW PARA 14A OF THIS MESSAGE.
4. SUMMARY OF PROBLEM -
A. THE H-47 COMMUNITY HAS REPORTED SEVERAL INCIDENTS IN
WHICH THE AIRCRAFT EXPERIENCED UNCOMMANDED MANEUVERS OR FLIGHT
CONTROL LOCK UP IN FLIGHT. THE USASC, AMCOM, AND BOEING ARE
CONDUCTING AN INVESTIGATION INTO THIS HAZARD. THE INVESTIGATING
AGENCIES ANALYZED SUSPECT COMPONENTS AND PERFORMED ANALYTICAL
TEAR-DOWNS. AMCOM ISSUED CH-47-98-ASAM-01 AND CH-47-96-ASAM-06
AS A RESULT OF THE REPORTED INCIDENTS. FACTORS WHICH HAVE BEEN
PRESENT AND MAY CONTRIBUTE TO UNCOMMANDED MANEUVERS OR FLIGHT
CONTROL LOCK-UP INCLUDE, BUT ARE NOT LIMITED TO: CONTAMINATION OF
HYDRAULIC FLUID, INTERNAL PARTS OUT OF TOLERANCE, CORROSION ON
INTERNAL PARTS, HIGH BARIUM CONTENT IN PRESERVATIVE HYDRAULIC
FLUIDS, HANDS OFF FLYING, AND INTERNAL FOD CREATED BY WEAR OF
ALUMINUM PARTS. THE INVESTIGATION TEAM CONDUCTED SIMULATIONS TO
ANALYZE THE INTERACTION OF THESE FACTORS WITH AIRCRAFT FLIGHT.
THE SIMULATIONS DEMONSTRATED THAT WHEN SUCH FACTORS ARE PRESENT
AND ACTUAL HANDS ON FLYING IS NOT BEING OBSERVED, THE AIRCRAFT
MAY PERFORM UNCOMMANDED MOVEMENTS WITH A SLOW DEGRADATION IN
FLIGHT CAPABILITIES. THE COMPUTER SIMULATION IS NOT
SOPHISTICATED ENOUGH AT THIS TIME TO PRODUCE THE EXACT MANEUVERS
OF THE INCIDENT AIRCRAFT, THEREFORE WE HAVE NOT BEEN ABLE TO
ESTABLISH A RIGOROUS CAUSE AND EFFECT RELATIONSHIP BETWEEN ANY
SINGLE FACTOR OR COMBINATION OF FACTORS FOR WHICH THE SPECIFIC
FLIGHT CONTROL ANOMALIES HAVE OCCURRED. TO RESOLVE CORROSION
HAZARDS WITH THE INTEGRATED LOWER CONTROL VALVE ACTUATOR (ILCA)
CONTROL VALVE, THE CH-47 PMO WILL FUND AND REQUEST AN ENGINEERING
CHANGE TO MANUFACTURE THE CONTROL VALVE FROM CORROSIVE RESISTANT
MATERIAL.
B. FOR MANPOWER/DOWNTIME AND FUNDING IMPACTS SEE PARA 12.
C. THE PURPOSE OF THIS MESSAGE IS TO ELIMINATE THOSE KNOWN
DEFICIENCIES WHICH HAVE BEEN IDENTIFIED AS SUSPECT CAUSES OF
UNCOMMANDED MANEUVERS OR FLIGHT CONTROL LOCK UP.
5. END ITEMS TO BE INSPECTED - ALL H-47 AIRCRAFT.
6. ASSEMBLY COMPONENTS TO BE INSPECTED - THE FOLLOWING
COMPONENTS WITH A 1,200 HOUR TBO WILL BE INSPECTED AND REPORTED
TO THE LOGISTICAL POC.
NOMENCLATURE PART NO. NSN
SERVOCYLINDER, PIVOTING 145H6600-9 1650-01-151-1713
SERVOCYLINDER, PIVOTING 145H6600-10 1650-01-151-5459
SERVOCYLINDER, PIVOTING 145H6600-11 1650-01-118-5627
SERVOCYLINDER, PIVOTING 145H6600-12 1650-01-117-4131
SERVOCYLINDER, SWIVELING 145H6700-8 1650-01-118-5628
SERVOCYLINDER, SWIVELING 145H6700-9 1650-01-119-7412
SERVOCYLINDER, SWIVELING 145H6700-10 1650-01-151-9231
SERVOCYLINDER, SWIVELING 145H6700-11 1650-01-151-9232
7. PARTS TO BE INSPECTED -N/A.
8. INSPECTION PROCEDURES -
A. PERFORM A VISUAL INSPECTION OF THE FORWARD AND AFT
PIVOTING AND SWIVELING SERVOCYLINDERS (4 SERVOCYLINDERS PER
AIRCRAFT) TO DETERMINE PART NUMBER.
B. IF A SERVOCYLINDER LISTED IN PARAGRAPH 6 IS INSTALLED,
THE HISTORICAL RECORDS WILL BE REVIEWED TO DETERMINE THE HOURS
ACCRUED.
C. EACH UNIT WILL NOTIFY THE LOGISTICAL POC WITH THE NUMBER
OF SERVOCYLINDERS THAT ARE AFFECTED. THE SERIAL NUMBER OF THE
AIRCRAFT ON WHICH THE COMPONENTS ARE INSTALLED ALONG WITH THE
COMPONENT SERIAL NUMBER, PART NUMBER, TIME REMAINING UNTIL TBO
AND AN ESTIMATED DATE THAT COMPONENTS WILL REACH TBO WILL BE
REPORTED TO THE LOGISTICAL POC.
9. CORRECTION PROCEDURES -
NOTE
ENSURE THAT ALL CLOSED OR STAND ALONE HYDRAULIC
COMPONENTS SUCH AS LANDING GEAR STRUT ASSEMBLIES
AND BLADE LAG SHOCK ABSORBERS ARE SERVICED WITH
MIL-H-5606 ONLY.
A. UNITS WHICH HAVE INSPECTED AND REPORTED SERVOCYLINDERS
LISTED IN PARAGRAPH 6 WILL FUND THE ENHANCED SPECIAL REPAIR
ACTIVITY (ESRA) LOCATIONS AT FT. CAMPBELL OR FT. RUCKER TO:
(1) ORDER REPLACEMENT STEEL END CAPS AND ASSOCIATED
HARDWARE FOR THE REPORTED SERVOCYLINDERS. THE ALUMINUM END CAPS
WILL BE REPLACED WITH CHROME PLATED STEEL END CAPS. THE NEW
STEEL END CAPS ARE NOT AVAILABLE AT THIS TIME. UNITS WILL
REPLACE THE ACTUATOR OR HAVE THE ESRA CHANGE THE END CAPS NLT 30
JUNE 2001. ALL SERVOCYLINDERS WHICH HAVE CHROME PLATED ALUMINUM
END CAPS WILL BE REPLACED TO REDUCE THE POSSIBILITY OF CHROME
FLAKES CONTAMINATING THE SYSTEM.
(2) REPLACE THE INDIVIDUAL PARTS WHICH WERE ORDERED FOR
THE SERVOCYLINDERS.
(3) PERFORM A LEAK CHECK OF THE REPAIRED SERVOCYLINDERS.
B. FOR ANY FLIGHT CONTROL OR UTILITY SYSTEM HYDRAULIC
COMPONENT RECEIVED FROM SUPPLY, MAINTENANCE PERSONNEL WILL DRIP
DRAIN PRESERVATIVE FLUID. MAINTENANCE PERSONNEL WILL MANUALLY
STROKE ACTUATORS, ROTATING PUMP SHAFTS, AND MOTOR SHAFTS (IF
POSSIBLE) TO PURGE ALL PRESERVATIVE FLUID. REFILL THE COMPONENT
WITH MIL-H-83282 PRIOR TO INSTALLATION (IF POSSIBLE).
C. USE FACTORY SEALED HYDRAULIC FLUID CONTAINERS ONLY. DO
NOT USE HYDRAULIC FLUIDS THAT HAVE BEEN EXPOSED TO THE
ENVIRONMENT. HYDRAULIC FLUIDS HAVE A NATURAL TENDENCY TO ABSORB
MOISTURE WHICH WILL CONTAMINATE THE FLUID AND INCREASE THE
PROBABILITY OF CORROSION DAMAGE.
D. CONTINUE TO OBSERVE PROPER MAINTENANCE PROCEDURES FOR
AIRCRAFT HYDRAULIC SYSTEMS.
(1) UPON REMOVAL FOR MAINTENANCE, CAP OR PLUG ALL
DISCONNECTED LINES, FITTINGS, AND COMPONENTS AS SOON AS PRACTICAL.
(2) INSPECT FOR CONTAMINATION ALL HYDRAULIC COMPONENTS
AND LINES NOT INSTALLED ON AIRCRAFT OR IN SUPPLY. CAP THOSE
COMPONENTS AND LINES AFTER INSPECTION AND/OR CLEANING.
E. UPON RECEIPT OF THE PURIFICATION EQUIPMENT, HYDRAULIC
SYSTEM PURIFICATION WILL BE PERFORMED AT THE END OF EACH PHASE
INSPECTION. UNITS WILL PURIFY ALL AIRCRAFT HYDRAULIC SYSTEMS TO
REMOVE WATER, CHLORINE, AND PARTICLES. THE CH-47 PM OFFICE (PMO)
IS ACQUIRING HYDRAULIC PURIFIERS FOR EACH CH-47 UNIT AND AVIM
THAT SUPPORTS THE CH-47 FLEET. THESE PURIFIERS WILL REMOVE
WATER, CHLORINE, AND PARTICULATES FROM THE AIRCRAFT HYDRAULIC
SYSTEM. EACH UNIT AND AVIM WILL PROVIDE A LOCAL POC TO THE
LOGISTICS POC LISTED IN PARA 16B. THE LOGISTICS POC WILL CONTACT
THE LOCAL POC WHEN THE PURIFICATION EQUIPMENT IS AVAILABLE. AN
OLR TEAM WILL TRAIN UNIT PERSONNEL TO OPERATE THE PURIFIER.
REPLACEMENT FILTERS AND MAINTENANCE OF THE PURIFIER WILL BE THE
RESPONSIBILITY OF THE OWNING UNIT.
F. PERFORM THE ILCA JAM TEST, PHASE I, OF TM 55-1520-240-
23-6, TASK 7-104.1 OR TM 1-1520-252-23-7, TASK 7-124 PRIOR TO THE
FIRST FLIGHT OF EACH DAY. ANNOTATE DA FORM 2408-13-1 TO REFLECT
THIS INSPECTION REQUIREMENT. THE FOLLOWING PRECAUTIONS WILL BE
TAKEN TO MINIMIZE WEAR AND TEAR ON THE JAM BUTTONS AND THEIR
SEALS:
CAUTION
EXCESSIVE FORCE APPLIED TO THE JAM BUTTON MAY
CAUSE DAMAGE TO THE BUTTON, REQUIRING THE REPLACEMENT
OF THE ENTIRE ACTUATOR ASSEMBLY.
(1) CLEAN THE JAM BUTTON WITH A CLEAN CLOTH PRIOR TO
PERFORMING THE TEST.
(2) DO NOT USE A STEEL TOOL TO DEPRESS THE BUTTON. USE
HAND PRESSURE WITH A DRIFT MADE OF A SOFTER MATERIAL SUCH AS
ALUMINUM, BRASS, OR WOOD TO DEPRESS THE BUTTON.
G. COMMANDERS AND UNIT INSTRUCTOR PILOTS WILL BRIEF ALL FLIGHT
CREWS THAT THE AFCS IS NOT AN AUTOMATIC PILOT AND IT IS IMPERATIVE
THAT A PILOT CONTINOUSLY MONITOR AIRCRAFT ATTITUDE WHILE UTILIZING
THE FUNCTIONS OF AFCS. IN THE EVENT THE AIRCRAFT DEVIATES FROM THE
DESIRED ATTITUDE THE PILOT WILL IMMEDIATELY MAN THE FLIGHT CONTROLS
AND MAKE CORRECTIVE INPUTS TO CORRECT DEVIATIONS.
H. ALL DEPOTS, FIELD/SUPPORT UNITS, AND CONTRACTOR
MAINTENANCE FACILITIES WILL NOT USE ALCOHOL OR CHLORINATED
SOLVENTS OR CLEANERS IN HYDRAULIC MAINTENANCE OR TO CLEAN PARTS
OF THE HYDRAULIC SYSTEM.
I. ALL DEPOTS, FIELD/SUPPORT UNITS, AND CONTRACTORS
MAINTENANCE FACILITIES WILL ENSURE THAT HYDRAULIC TEST STANDS FOR
H-47 FLIGHT CONTROL AND UTILITY SYSTEM COMPONENTS ARE SERVICED
WITH MIL-H-83282. THIS FLUID WILL BE USED AS A PRESERVATIVE FLUID
TO ELIMINATE TRACES OF BARIUM IN HYDRAULIC COMPONENTS. MIL-H-83282
CONTAINS SUFFICIENT CORROSION PROTECTION FOR COMPONENT STORAGE.
J. NUMBER 1 AND NUMBER 2 FLIGHT BOOST PRESSURE AND RETURN
FILTER ELEMENTS WILL BE REPLACED AT THE NEXT PHASE AND EVERY 400
HOURS THERE AFTER. ULLS-A UNITS WILL USE INSPECTION LEGITIMATE
CODE NUMBER A-380 FOR THE NUMBER 1 AND 2 FLIGHT BOOST PRESSURE
AND RETURN FILTER REPLACEMENT DUE EVERY 400 HOURS.
10. SUPPLY/PARTS AND DISPOSITION -
A. PARTS REQUIRED -ITEMS CITED IN PARAGRAPH 6 ARE REQUIRED
TO BE REPLACED OR HAVE END CAPS REPLACED.
B. REQUISITIONING INSTRUCTIONS - REQUISITION REPLACEMENT
PARTS THROUGH NORMAL SUPPLY CHANNELS USING NORMAL SUPPLY
PROCEDURES. ALL REQUISITIONS WILL USE PROJECT CODE "XFD" (X-RAY-
FOXTROT-DELTA) PER THIS MESSAGE. UNITS DECIDING TO REQUISITION
END CAPS AND PAY TO HAVE THE ESRA AT FORT RUCKER OR FORT CAMPBELL
INSTALL THEM SHOULD CONTACT THE ESRA SITE DIRECTLY. SEE
LOGISTICAL POINT OF CONTACT.
C. BULK AND CONSUMABLE MATERIALS - N/A.
D. DISPOSITION - DISPOSE OF REMOVED PARTS/COMPONENTS USING
NORMAL SUPPLY PROCEDURES. A QDR IS NOT REQUIRED. HOLD ANY
UNSERVICEABLE PART/COMPONENT PENDING DISPOSITION INSTRUCTIONS
FROM THE LOGISTICAL POC IN PARAGRAPH 16B.
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 - OLR TEAMS WILL FURNISH
SPECIAL PURIFICATION EQUIPMENT.
12. APPLICATION -
A. CATEGORY OF MAINTENANCE - AVUM AND OLR TEAM. AIRCRAFT
DOWNTIME WILL BE CHARGED TO AVUM MAINTENANCE.
B. ESTIMATED TIME REQUIRED -
(1) TOTAL OF 1 MAN-HOUR USING 1 PERSON PER AIRCRAFT TO
INSPECT AND REPORT UPPER BOOST ACTUATORS.
(2) TOTAL OF 1 HOUR DOWNTIME FOR ONE END ITEM.
C. ESTIMATED COST IMPACT TO THE FIELD -
NOMENCLATURE PART NO./NSN QTY COST EA. TOTAL $
SERVOCYLINDER 145H6600-20 1 $ 8,990.06 $ 8,990.06
1650-01-303-7897
SERVOCYLINDER 145H6600-19 1 $ 8,989.00 $ 8,989.00
1650-01-304-9016
SERVOCYLINDER 145H6700-18 1 $14,813.03 $14,813.03
1650-01-303-7898
SERVOCYLINDER 145H6700-19 1 $16,850.38 $16,850.38
1650-01-302-0076
END CAP 114H4007-3 2 $ 511.06 $ 1,022.12
1650-01-306-6403
END CAP 114H4007-4 2 $ 855.04 $ 1,710.08
1650-01-311-1162
END CAP 114H4048-3 2 $ 998.40 $ 1,996.80
1650-01-306-6402
END CAP 114H4048-4 2 $ 855.40 $ 1,710.80
1650-01-310-5859
FILTER ELEMENT AC-A620F5 4 $ 102.48 $ 409.92
1650-01-114-6385
PACKING M83461/1-132/
5330-01-146-4563 4 $ 0.18 $ 0.72
RETAINER MS28744-132 4 $ 0.26 $ 1.04
5330-00-848-9128
PACKING MS28775-017 4 $ 0.03 $ 0.12
5330-00-618-1920
PACKING M83461/1-024/ 4 $ 0.11 $ 0.44
5331-01-107-9249
PIN, ROLL 79-022-094-0375 8 $ 0.63 $ 5.04
5315-00-039-5563
RETAINER MS28774-128 8 $ 0.18 $ 1.44
5330-00-892-1608
PACKING MS28775-128 8 $ 0.13 $ 1.04
5330-00-702-5643
PIN, COTTER MS24665-153 4 PER HD $ 1.56
5315-00-241-7330
NUT MS21224-5 4 $ 3.51 $ 14.04
5310-00-151-5430
BOLT MS27576-4-19 4 $ 8.56 $ 34.24
5306-00-408-6864
NUT, PLAIN AN320-8 2 PG $ 17.08
5310-00-176-8112
BOLT 145R3650-6 2 $ 146.66 $ 293.32
5306-01-322-2892
BOLT 145R3650-5 2 $ 226.06 $ 452.12
5306-01-319-9023
BOLT BACB30ST8-31 2 $ 36.38 $ 72.76
5306-00-008-5025
BOLT BACB30ST8-35 2 $ 28.90 $ 57.80
5306-00-008-5027
BOLT 114R3650-3 2 $ 72.83 $ 145.66
1615-00-003-1146
PIN, COTTER MS24665-374 4 PER HD $ 2.70
5315-00-241-7332
NUT, PLAIN AN320-10 2 $ 13.16 $ 26.32
5310-00-176-8114
BOLT 145R3650-1 2 $ 297.57 $ 595.14
1615-01-115-3609
TOTAL COST PER AIRCRAFT =
FOR AIRCRAFT REPLACING ALL ACTUATORS.............$49,066.15
FOR AIRCRAFT HAVING END CAP REPLACEMENTS $5,863.48
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 -
(1) TM 55-1520-240-23
(2) TM 1-1520-252-23
(3) TM 1-1520-252-23-PM
(4) TM 55-1520-240-PM
(5) TM 55-1520-240-PMD
(6) TM 1-1520-252-PMD
(7) HYDRAULIC COMPONENT DMWR'S WILL BE CHANGED TO
REFLECT THIS MESSAGE. A COPY OF THIS MESSAGE WILL BE INSERTED IN
THE APPROPRIATE PUBLICATION AS AUTHORITY TO IMPLEMENT THE CHANGE
UNTIL THE PRINTED CHANGE IS RECEIVED.
13. REFERENCES -
A. TM 55-1520-240-23P.
B. TM 1-1520-252-23P.
C. TM 55-1520-240-23.
D. TM 1-1520-252-23.
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) -
UPON COMPLETION OF INSPECTION, UNITS WILL FORWARD A PRIORITY
MESSAGE TO: PM CH-47, ATTN: SFAE-AV-CH-L, DSN 897-4304 OR (256)
313-4304, "OLSONW@PEOAVN.REDSTONE.ARMY.MIL". THE REPORT WILL
CITE THIS MESSAGE NUMBER, DATE OF INSPECTION, AIRCRAFT SERIAL
NUMBER, AIRCRAFT AND COMPONENT HOURS, AND RESULTS OF THE
INSPECTION. INSPECTION AND REPORTS WILL BE COMPLETED NO LATER
THAN 30 DAYS AFTER TASK/INSPECTION SUSPENSE DATE.
C. REPORTING MESSAGE RECEIPT (SPARES) -
(1) MATERIEL IN WHOLESALE DEPOT STORAGE - N/A.
(2) MATERIEL IN RETAIL STORAGE - 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 2408-5-1, EQUIPMENT MODIFICATION RECORD
(ACTUATOR).
(2) DA FORM 2408-13, AIRCRAFT STATUS INFORMATION
RECORD.
(3) DA FORM 2408-13-1, AIRCRAFT INSPECTION AND
MAINTENANCE RECORD.
(4) DA FORM 2408-14, UNCORRECTED FAULT RECORD.
(5) DA FORM 2408-15, HISTORICAL RECORD FOR AIRCRAFT.
(6) DA FORM 2408-16, AIRCRAFT COMPONENT HISTORICAL
RECORD.(IF ACTUATOR IS REMOVED/REPLACED)
(7) DA FORM 2408-18, EQUIPMENT INSPECTION LIST.
(8) DA FORM 2410, COMPONENT REMOVAL AND
REPAIR/OVERHAUL RECORD.(IF ACTUATOR IS REMOVED/REPLACED)
(9) DD FORM 1574/DD FORM 1574-1, SERVICEABLE TAG/LABEL
- MATERIEL (COLOR YELLOW). ANNOTATE REMARKS BLOCK WITH "INSPECTED
SERVICEABLE IAW CH-47-99-ASAM-02."
(10) DD FORM 1577-2/DD FORM 1577-3, UNSERVICEABLE
(REPARABLE) TAG/LABEL - MATERIEL (COLOR GREEN). ANNOTATE REMARKS
BLOCK WITH UNSERVICEABLE IAW CH-47-99-ASAM-02."
15. WEIGHT AND BALANCE - N/A.
16. POINTS OF CONTACT -
A. TECHNICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. MATT
WESSELSCHMIDT, AMSAM-AR-E-I-C-H, DSN 897-4286 OR (256) 313-4286,
DATAFAX IS DSN 897-4348 OR (256) 313-4348.
E-MAIL IS "WESSELSCHMIDT-ML@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
BROCK, AMSAM-SF-A, DSN 788-8632 OR (256) 842-8632, DATAFAX IS DSN
897-2111 OR (256) 313-2111.
E-MAIL IS "BROCK-RD@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.