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:UNCLAS
SUBJECT - AVIATION SAFETY ACTION MESSAGE, MAINTENANCE MANDATORY, RCS
CSGLD-1860(R1), ALL H-47 SERIES AIRCRAFT, INSPECTION OF FORWARD AND
AFT SLIDER SHAFT SEALS, CH-47-00-ASAM-05 (TB 1-1520-240-20-123).
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 -
NOTE
IAW AR 95-1, PARA 6-6A, MACOM COMMANDERS MAY AUTHORIZE TEMPORARY
EXCEPTION FROM ASAM 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 THE
FORWARD AND AFT SLIDER SHAFT SEALS IAW CH-47-00-ASAM-05 (TB 1-
1520-240-20-123) WITHIN THE NEXT 10 FLIGHT HOURS, BUT NLT 9 AUGUST
2000." CLEAR THE RED HORIZONTAL DASH //-// ENTRY WHEN THE
PROCEDURES IAW PARA 8 ARE COMPLETED. THE AFFECTED AIRCRAFT SHALL
BE INSPECTED AS SOON AS PRACTICAL BUT NO LATER THAN 9 AUGUST 2000.
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) INSPECT AT FINAL DESTINATION.
(B) BOEING WILL INSPECT DD 250 AIRCRAFT PRIOR TO
THOSE AIRCRAFT DEPARTING FOR FERRY TO FINAL DESTINATION.
E. MAINTENANCE TRAINERS (CATEGORY A AND B) - COMPLY NLT 22
SEPTEMBER 2000.
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 PARA 6 WITH
CAGE CODE 59213 ARE ANNOTATED TO READ: "CH-47-00-ASAM-05 (TB 1-
1520-240-20-123), INSPECTION OF THE FORWARD AND AFT SLIDER SHAFT
SEALS, NOT COMPLIED WITH."
(1) WHOLESALE STOCK - REPORT RECEIPT OF THIS MESSAGE IAW
PARAGRAPH 14C(1). UPON RECEIPT OF THIS MESSAGE, DEPOT AND
MATERIEL ACTIVITY COMMANDERS WILL ENSURE ALL SERVICEABLE ITEMS
(CONDITION CODES //A//, //B//, //C//, //D//, AND //E//) LISTED IN
PARA 6 WITH CAGE CODE 59213 ARE PLACED IN CONDITION CODE //J//
AND TAGGED WITH A SUSPENDED TAG/LABEL - MATERIEL, DD FORM 1575/DD
FORM 1575-1. DO NOT REMOVE ORIGINAL CONDITION TAGS. REPORT
COMPLIANCE WITH THIS MESSAGE IAW PARAGRAPH 14D(1).
(2) RETAIL STOCK - REPORT RECEIPT OF THIS MESSAGE IAW
PARAGRAPH 14C(2). 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. DISPOSE OF DISCREPANT MATERIEL IAW PARAGRAPH 10.
REPORT COMPLIANCE WITH THIS MESSAGE IAW PARAGRAPH 14D(2).
G. COMPONENTS/PARTS IN WORK (DEPOT LEVEL AND OTHERS) -
DEPOT AND OTHER MAINTENANCE ACTIVITY COMMANDERS WILL ENSURE ITEMS
LISTED IN PARA 6 ARE NOT ISSUED UNTIL THEY ARE IN COMPLIANCE WITH
THIS MESSAGE.
2. TASK/INSPECTION SUSPENSE DATE - COMPLETE THE INSPECTION IAW
PARAGRAPH 8 WITHIN THE NEXT 10 FLIGHT HOURS BUT NLT 9 AUGUST 2000
AND REPORT IAW PARA 14B.
3. REPORTING COMPLIANCE SUSPENSE DATE - REPORT COMPLIANCE IAW
PARA 14A NLT 16 AUGUST 2000.
4. SUMMARY OF PROBLEM -
A. A UNIT REPORTED RECEIPT OF A DEFECTIVE SLIDER SHAFT SEAL
ASSEMBLY FROM THE SUPPLY SYSTEM. THE METAL PORTION OF THE SEAL
ASSEMBLY EXTENDED OUT TO THE EDGE OF THE RUBBER SEAL. THIS
CONDITION PLACES THE METAL PORTION OF THE SEAL ASSEMBLY
UNACCEPTABILITY CLOSE TO THE VERTICAL ROTOR SHAFTS.
B. FOR MANPOWER/DOWNTIME AND FUNDING IMPACTS SEE PARA 12.
C. THE PURPOSE OF THIS MESSAGE IS TO VISUALLY INSPECT THE
SLIDER SHAFT SEAL ASSEMBLIES FOR DEFECTS.
5. END ITEMS TO BE INSPECTED - ALL H-47 SERIES AIRCRAFT.
6. ASSEMBLY COMPONENTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
SLIDER SHAFT SEAL ASSEMBLY 145R3131-1 1615-01-113-0258
SLIDER SHAFT SEAL ASSEMBLY 145R3131-2 1615-01-113-0261
7. PARTS TO BE INSPECTED - N/A.
8. INSPECTION PROCEDURES -
NOTE
DISASSEMBLY IS NOT REQUIRED FOR VISUAL
INSPECTION.
NOTE
THE SEAL IS MADE UP OF TWO SEPARATE HALVES
AROUND EACH ROTOR SHAFT. EACH HALF NEEDS TO
BE INSPECTED.
A. FOR SEAL ASSEMBLIES THAT ARE INSTALLED ON THE AIRCRAFT -
(1) GAIN ACCESS TO THE SLIDER SHAFT -
(A) AFT SLIDER SEAL ASSEMBLY - TM 55-1520-240-23P,
FIGURE 199, ITEM 203, OR TM 1-1520-252-23P, FIGURE 6-25, ITEM 194.
(B) FORWARD SLIDER SEAL ASSEMBLY - TM 55-1520-240-23P,
FIGURE 179, ITEM 33, OR TM 1-1520-253-23P, FIGURE 6-2, ITEM 33.
(2) USING A FLASHLIGHT AND INSPECTION MIRROR, LOCATE THE
DUST SEAL ON TOP OF THE SLIDER SHAFT AND VERIFY THAT THE RUBBER
SEAL OVERLAPS THE INSIDE EDGE OF THE METAL BASE.
(3) PERFORM THE INSPECTION PROCEDURES IAW TASK 6-58, STEP 7
OF TM 55-1520-240-23, OR TASK 6-68, STEP 7 OF TM 1-1520-252-23.
(4) IF THE INSIDE DIAMETER OF THE RUBBER SEAL EXTENDS BEYOND
THE INSIDE EDGE OF THE METAL BASE IAW 8A(2), AND MEETS THE CLEARANCES
SPECIFIED IAW 8A(3), THE INSPECTION OF THE AFT SEAL IS COMPLETE.
(5) IF THE INSIDE DIAMETER OF THE RUBBER IS FOUND TO BE EVEN
WITH THE INSIDE DIAMETER OF THE METAL BASE, PROCEED TO PARAGRAPH 8B.
B. IF THE SEAL ASSEMBLY AROUND THE AFT OR FORWARD ROTOR
SHAFT IS FOUND DEFECTIVE -
(1) REMOVE THE SEAL ASSEMBLY. TO GAIN ADEQUATE ACCESS
TO THE SEAL ASSEMBLY IT MAY BE NECESSARY TO FIRST REMOVE THE
ROTOR HEAD AND RAIN SHIELD (C/MH-47D - TM 55-1520-240-23,
CHAPTERS 5 & 6, AND MH-47E - TM 1-1520-252-23, CHAPTERS 5 & 6).
(2) REMOVE THE SEAL FROM THE SLIDER SHAFT.
(3) INSPECT THE VERTICAL ROTOR SHAFT FOR ANY DAMAGE THAT
MAY HAVE BEEN CAUSED AS A RESULT OF THE DEFECTIVE SEAL.
(A) IF DAMAGE IS FOUND TO THE VERTICAL ROTOR SHAFT,
CONTACT THE TECH POC IN PARAGRAPH 16A.
(B) IF NO DAMAGE IS FOUND TO THE VERTICAL ROTOR
SHAFT, PROCEED TO PARAGRAPH 9.
C. FOR SEAL ASSEMBLIES NOT INSTALLED ON THE AIRCRAFT -
(1) IDENTIFY ALL SEAL ASSEMBLIES WITH CAGE CODE 59213.
(2) PERFORM A VISUAL INSPECTION TO ENSURE THE INSIDE
DIAMETER OF THE RUBBER EXTENDS PAST THE INSIDE DIAMETER OF THE
METAL BASE.
(A) THE INSIDE DIAMETER OF THE METAL BASE SHOULD
MEASURE 7.5 INCHES AND THE INSIDE DIAMETER OF THE RUBBER SHOULD
EXTEND BEYOND THE INSIDE DIAMETER OF THE METAL BASE BY AT LEAST
0.375 INCHES.
(B) IF THE SEAL FALLS WITHIN THESE PARAMETERS, THE
INSPECTION OF THE SEAL IS COMPLETE.
(C) IF THE RUBBER IS EVEN WITH THE METAL BASE,
PROCEED TO PARA 9.
9. CORRECTION PROCEDURES - IF A SEAL ASSEMBLY IS FOUND TO BE
DEFECTIVE -
A REPLACE THE SEAL WITH A PROPERLY MANUFACTURED SEAL AND
REASSEMBLE.
B. IF NO SEALS ARE AVAILABLE, SEND THE SEAL TO THE AVIM
SUPPORT FACILITY WHERE THE SEAL ASSEMBLY CAN BE REWORKED TO THE
PROPER SPECIFICATIONS. NOTIFY THE LOGISTICAL POINT OF CONTACT IN
PARAGRAPH 16B WHO WILL FORWARD THE TECHNICAL DRAWINGS TO THE LAR.
10. SUPPLY/PARTS AND DISPOSITION -
A. PARTS REQUIRED - ITEMS CITED IN PARA 6 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) "X01" (XRAY-ZERO-ONE).
NOTE
PROJECT CODE "X01" 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 - HOLD ANY DISCREPANT PART/COMPONENT FOR
POSSIBLE REWORK INSTRUCTIONS FROM LOGISTICAL POINT OF CONTACT IN
PARA 16B.
E. DISPOSITION OF HAZARDOUS MATERIAL - N/A.
11. SPECIAL TOOLS AND FIXTURES REQUIRED - N/A.
12. APPLICATION -
A. CATEGORY OF MAINTENANCE -
(1) AVUM FOR INSPECTION AND REINSTALLATION AS REQUIRED.
(2) AVIM FOR REWORK OF THE SEAL ASSEMBLY.
B. ESTIMATED TIME REQUIRED -
(1) TO CONDUCT THE INITIAL INSPECTION -
(A) TOTAL OF 0.5 MAN-HOURS USING 1 PERSON.
(B) TOTAL OF 0.5 HOUR DOWNTIME FOR ONE END ITEM.
(2) TO REMOVE AND REPLACE A SEAL ASSEMBLY -
(A) TOTAL OF 16 MAN-HOURS USING 4 PERSONS.
(B) TOTAL OF 4 HOUR DOWNTIME FOR ONE END ITEM.
C. ESTIMATED COST IMPACT TO THE FIELD -
NOMENCLATURE PN/NSN QTY COST EA TOTAL
SLIDER SHAFT SEAL 145R3131-1 2 $111.74 $223.48
ASSEMBLY 1615-01-113-0258
SLIDER SHAFT SEAL 145R3131-2 2 $162.08 $324.16
ASSEMBLY 1615-01-113-0261
TOTAL COST PER AIRCRAFT = $547.64
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 55-1520-240-23 AND TM 55-1520-252-23 SHALL BE
CHANGED 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. CHANGES TO THE TM'S
WILL BE AS FOLLOWS -
(1) TM 55-1520-240-23, TASK 6-50, INSTRUCTION 33, SHALL
BE CHANGED TO READ AS FOLLOWS: "POSITION SEAL HALVES (64 AND 65)
ON SHAFT (54). APPLY A LIGHT COAT OF OIL (E253), (E254), OR (E254.1)
TO THE THREAD OF 12 BOLTS (66). INSTALL THE BOLTS AND WASHERS (67).
ENSURE THAT A MINIMUM CLEARANCE OF 0.050 INCH EXISTS BETWEEN THE
RUBBER SEAL AND THE SURFACE OF THE ROTOR SHAFT. IF A MINIMUM
CLEARANCE DOES NOT EXIST, MOVE THE SEAL (64 OR 65) RADIALLY AS FAR
AWAY FROM THE SHAFT AS POSSIBLE AND RECHECK CLEARANCE. TORQUE THE
BOLTS TO 60 INCH-POUNDS."
(2) TM 55-1520-240-23, TASK 6-54, INSTRUCTION 35, AND
TM 1-1520-252-23, TASK 6-64, INSTRUCTION 35, SHALL BE CHANGED TO
READ: "POSITION TWO HALVES OF SEAL (35) ON SHAFT (31). INSTALL 12
WASHERS (36) AND BOLTS (34). ENSURE THAT A MINIMUM CLEARANCE OF
0.050 INCH EXISTS BETWEEN THE RUBBER SEAL (35) AND THE SURFACE OF
THE ROTOR SHAFT (31). IF A MINIMUM CLEARANCE DOES NOT EXIST,
MOVE THE SEAL (35) RADIALLY AS FAR AWAY FROM THE SHAFT (31) AS
POSSIBLE AND RECHECK CLEARANCE. TORQUE BOLTS TO 60 INCH-POUNDS.
LOCK WIRE BOLTS (34). USE LOCK WIRE (E278)."
(3) TM 1-1520-252-23, TASK 6-59, INSTRUCTION 34, SHALL
BE CHANGED TO READ AS FOLLOWS: "COAT THREADS OF BOLTS (70) WITH
OIL (E303) AND POSITION SEAL HALVES (68 AND 69) ON SHAFT (58).
INSTALL 12 BOLTS (70) AND WASHERS (71). WEAR GLOVES (E226).
ENSURE THAT A MINIMUM CLEARANCE OF 0.050 INCH EXISTS BETWEEN THE
RUBBER SEAL AND THE SURFACE OF THE ROTOR SHAFT. IF A MINIMUM
CLEARANCE DOES NOT EXIST, MOVE THE SEAL (64 OR 65) RADIALLY AS
FAR AWAY FROM THE SHAFT AS POSSIBLE AND RECHECK CLEARANCE.
TORQUE BOLTS TO 60 INCH-POUNDS."
13. REFERENCES -
A. TM 55-1520-240-23.
B. TM 55-1520-240-23P.
C. TM 1-1520-252-23.
D. TM 1-1520-252-23P.
E. DA PAM 738-751.
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 CH-47-00-ASAM-05
(TB 1-1520-240-20-123), 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: CDR, AMCOM, ATTN: SFAE-AV-CH-L (MR. WILLIAM OLSON,
DSN 897-3379 OR (256) 313-3379, DATAFAX IS 897-4348, E-MAIL
"WILLIAM.OLSON@PEOAVN@REDSTONE.ARMY.MIL".) THE REPORT WILL CITE
CH-47-00-ASAM-05 (TB 1-1520-240-20-123), DATE OF INSPECTION,
AIRCRAFT SERIAL NUMBER, AIRCRAFT AND COMPONENT HOURS, AND RESULTS
OF THE INSPECTION. INSPECTION AND REPORTS WILL BE COMPLETED NLT 11
AUGUST 2000.
C. REPORTING MESSAGE RECEIPT (SPARES) -
(1) MATERIEL IN WHOLESALE DEPOT STORAGE - DEPOT AND
MATERIEL ACTIVITY COMMANDERS WILL REPORT RECEIPT OF THIS MESSAGE
BY E-MAIL OR DATAFAX TO THE WHOLESALE MATERIEL (SPARES) POINT OF
CONTACT LISTED IN PARAGRAPH 16C NLT 11 AUGUST 2000. PROVIDE A
LOCAL POINT OF CONTACT.
(2) MATERIEL IN RETAIL STORAGE - COMMANDERS AND FACILITY
MANAGERS WILL REPORT RECEIPT OF THIS MESSAGE BY E-MAIL OR DATAFAX TO
THE LOGISTICAL POINT OF CONTACT LISTED IN PARAGRAPH 16B NLT 18 AUGUST
2000. PROVIDE A LOCAL POINT OF CONTACT.
D. TASK/INSPECTION REPORTING SUSPENSE DATE (SPARES).
(1) MATERIEL IN WHOLESALE DEPOT STORAGE - DEPOT AND
MATERIEL ACTIVITY COMMANDERS WILL REPORT COMPLIANCE WITH THIS MESSAGE
TO THE WHOLESALE MATERIEL POINT OF CONTACT (SPARES) LISTED IN
PARAGRAPH 16C NLT 18 AUGUST 2000 ON DD FORM 1225. PROVIDE THE COST
OF COMPLIANCE WITH THIS MESSAGE TO INCLUDE AN ESTIMATE OF THE COST
REIMBURSABLE FUNDING REQUIRED TO MOVE SERVICEABLE ITEMS ON HAND
LISTED IN PARAGRAPHS 6 AND 7 TO A WORK AREA, UNPACK THE MATERIEL,
REPACK THE MATERIEL AFTER INSPECTION BY AMCOM INSPECTORS, AND TO
RETURN THE MATERIEL TO STORAGE, AS APPROPRIATE. REPORT, BY ORIGINAL
SERVICEABLE CONDITION CODE, THE QUANTITY OF MATERIEL PLACED IN
CONDITION CODE //J//. REPORT BY E-MAIL OR DATAFAX AND PROVIDE A
LOCAL POINT OF CONTACT.
(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 9 AUGUST 2000. REPORT THE
QUANTITY INSPECTED BY CONDITION CODE AND THE RESULTING CONDITION
CODE. REPORT BY E-MAIL OR DATAFAX AND PROVIDE A 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 2408-13, AIRCRAFT STATUS INFORMATION RECORD.
(2) DA FORM 2408-13-1, AIRCRAFT INSPECTION AND
MAINTENANCE RECORD.
(3) DA FORM 2408-15, HISTORICAL RECORD FOR AIRCRAFT.
(4) DD FORM 1574/DD FORM 1574-1, SERVICEABLE TAG/LABEL -
MATERIEL (COLOR YELLOW). ANNOTATE REMARKS BLOCK WITH "INSPECTED
SERVICEABLE IAW CH-47-00-ASAM-05 (TB 1-1520-240-20-123)."
(5) DD FORM 1575/DD FORM 1575-1, SUSPENDED TAG/LABEL -
MATERIEL (COLOR BROWN). ANNOTATE REMARKS BLOCK WITH "SUSPENDED
IAW CH-47-00-ASAM-05 (TB 1-1520-240-20-123)."
(6) DD FORM 1577-2/DD FORM 1577-3, UNSERVICEABLE
(REPARABLE) TAG/LABEL - MATERIEL (COLOR GREEN). ANNOTATE REMARKS
BLOCK WITH UNSERVICEABLE IAW CH-47-00-ASAM-05 (TB 1-1520-240-20-
123)."
(7) SF 368, PRODUCT QUALITY DEFICIENCY REPORT
15. WEIGHT AND BALANCE - N/A.
16. POINTS OF CONTACT -
A. TECHNICAL POINT OF CONTACT IS MR. LARRY WIESCHHAUS,
AMSAM-RD-AE-I-P-C, DSN 897-3341 OR (256) 313-3341, DATAFAX IS 897-
4348. E-MAIL IS "LARRY.WIESCHHAUS@REDSTONE.ARMY.MIL".
B. LOGISTICAL POINT OF CONTACT IS MR. WILLIAM OLSON, SFAE-
AV-CH-L, DSN 897-3379 OR (256) 313-3379, DATAFAX IS 897-4348.
E-MAIL IS "WILLIAM.OLSON@PEOAVN@REDSTONE.ARMY.MIL".
C. WHOLESALE MATERIEL POINT OF CONTACT (SPARES) IS MR. PAUL
HUGHES, DSCR-XB, DSN 695-6328 OR (804) 279-6328, DATAFAX IS DSN
695-5190. E-MAIL IS "PHUGHES@DSCR.DLA.MIL".
D. FORMS AND RECORDS POINT OF CONTACT 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".
E. SAFETY POINTS OF CONTACT ARE -
(1) PRIMARY - MR. HARRY TRUMBULL (SAIC), AMSAM-SF-A,
DSN 897-2095 OR (256) 313-2095, DATAFAX IS DSN 897-2111 OR (256)
313-2111. E-MAIL IS "HARRY.TRUMBULL@REDSTONE.ARMY.MIL".
(2) ALTERNATE - MR. RUSSELL PEUSCH, AMSAM-SF-A, DSN 788-
8632 OR 897-2091, COMMERCIAL (256) 842-8632 OR (256) 313-2091,
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 6 HRS.
G. AFTER HOURS CONTACT THE AMCOM COMMAND OPERATIONS CENTER
(COC) DSN 897-2066/7 OR (256) 313-2066/7.