Safety of Flight CH-47-02-01

 

         

UNCLASSIFIED				

MSG DTG 242132Z JAN 02

FROM CDRAMCOM, REDSTONE ARSENAL, AL  //AMSAM-SF-A//

SUBJECT - SAFETY OF FLIGHT MESSAGE, TECHNICAL, RCS CSGLD-
1860(R1), H-47, SWASHPLATE LOWER SEAL RETAINER SELF-LOCKING NUT 
INSPECTION, CH-47-02-01 (TB 1-1520-240-20-144).
                              NOTE
THIS MESSAGE IS ISSUED IAW AR 95-1, 1 SEP 97, CHAPTER 6.  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 ADDRESSEES WILL IMMEDIATELY VERIFY THIS TRANSMISSION TO 
CDR, AMCOM, ATTN:  AMSAM-SF-A (SOF COMPLIANCE OFFICER).
1.  PRIORITY CLASSIFICATION -
                             NOTE
IAW AR 95-1, PARAGRAPH 6-6A/6-14A, MACOM COMMANDERS MAY AUTHORIZE 
TEMPORARY EXCEPTION FROM 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 
SWASHPLATE LOWER SEAL RETAINER SELF-LOCKING NUTS IAW CH-47-02-01 
PRIOR TO NEXT FLIGHT, BUT NLT 8 FEB 02."  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 8 FEB 02.  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 MAINTENANCE FACILITY - 
        (1) AIRCRAFT IN AVUM, AVIM OR DEPOT - SAME AS PARA 1A. 
        (2) AIRCRAFT AT CONTRACTOR FACILITY - BOEING WILL INSPECT 
DD 250 AIRCRAFT PRIOR TO THOSE AIRCRAFT DEPARTING FOR FERRY TO 
FINAL DESTINATION.
    C.  AIRCRAFT IN TRANSIT - 
        (1) SURFACE/AIR SHIPMENT - SAME AS PARA 1A.   
        (2) FERRY STATUS - SAME AS PARA 1A.   
    D.  MAINTENANCE TRAINERS (CATEGORY A AND B) - SAME AS PARA 
1A.
    E.  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-47-02-01 (TB 1-1520-240-20-144), 
SWASHPLATE LOWER SEAL RETAINER SELF-LOCKING NUT INSPECTION 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.  DISPOSE OF DISCREPANT MATERIEL IAW PARAGRAPH 10..
    F.  COMPONENTS/PARTS IN WORK (DEPOT LEVEL AND OTHERS) - DEPOT 
AND OTHER MAINTENANCE ACTIVITY COMMANDERS WILL ENSURE ITEMS 
LISTED IN PARAGRAPHS 6 AND 7 ARE NOT ISSUED UNTIL THEY ARE IN 
COMPLIANCE WITH THIS MESSAGE.
2.  TASK/INSPECTION SUSPENSE DATE - COMPLETE THE INSPECTION IAW 
PARAGRAPH 8 PRIOR TO NEXT FLIGHT, BUT NLT 8 FEB 02. 
3.  TAMMS REPORTING COMPLIANCE SUSPENSE DATE - REPORT COMPLIANCE 
IAW PARA 14A(1) NLT 30 JAN 02.
4.  SUMMARY OF PROBLEM -
    A.  A FIELD UNIT HAS DISCOVERED THE USE OF SELF-LOCKING NUT 
P/N NAS 1758-L6 ON THE SWASHPLATE LOWER SEAL RETAINER.  THE 
OVERALL HEIGHT OF THESE NUTS DOES NOT ALLOW FULL ENGAGEMENT OF 
THE LOCKING FEATURES IN THE NUT.  USE OF THE INCORRECT NUTS COULD 
CAUSE DAMAGE TO THE STATIONARY RING DUE TO INADEQUATE CLEARANCE 
BETWEEN THE NUT AND THE STATIONARY RING, ESPECIALLY IF THE NUT 
WERE TO BACK OFF THE BOLT.  IN ADDITION, IF A NUT OR BOLT WERE TO 
BACK OFF AND DROP BELOW THE SWASHPLATE ASSEMBLY, THE POSSIBILITY 
EXISTS THAT A LINKAGE COULD BE JAMMED BY THE FASTENER, WHICH 
COULD CAUSE A PARTIAL OR COMPLETE LOSS OF ROTOR CONTROL.  
    B.  MANPOWER/DOWNTIME AND FUNDING IMPACTS - SEE PARA 12.
    C.  THE PURPOSE OF THIS MESSAGE IS TO 
        (1)  REQUIRE INSPECTION FOR AND REPLACEMENT OF INCORRECT 
SELF-LOCKING NUTS INSTALLED ON FORWARD AND AFT SWASHPLATE 
ROTATING RING ASSEMBLIES.
        (2)  REQUIRE INSPECTION OF SWASHPLATE STATIONARY RING FOR 
DAMAGE IF INCORRECT SELF-LOCKING NUTS ARE FOUND.
        (3)  REQUIRE INSPECTION OF ALL SWASHPLATE LOWER SEAL 
RETAINER SELF-LOCKING NUTS ON HAND/IN STOCK. 
        (4)  REQUIRE A CHANGE TO MAINTENANCE MANUALS TO 
INCORPORATE THE CORRECT NUT TORQUE VALUE AND CHANGE INSTALLATION 
PROCEDURES FROM A WET INSTALLATION TO DRY INSTALLATION. 
5.  END ITEMS TO BE INSPECTED - ALL H-47 AIRCRAFT.  
6.  ASSEMBLY COMPONENTS TO BE INSPECTED -
   NOMENCLATURE            PART NO.              NSN
SWASHPLATE ASSY            145R3551-ALL
ROTATING RING ASSY         114R3464-ALL
FWD STATIONARY RING ASSY   145R3351-ALL
AFT STATIONARY RING ASSY   145R3352-ALL
FWD STATIONARY RING ASSY   414R3351-1     1615-01-342-2310
FWD STATIONARY RING ASSY   414R3351-3     1615-01-474-4228
AFT STATIONARY RING ASSY   414R3352-3     1615-01-342-7961
7.  PARTS TO BE INSPECTED -
    NOMENCLATURE           PART NO.              NSN
NUT, SELF-LOCKING         FN22M-624       5310-00-184-0354
FWD STATIONARY RING       114R3351-ALL
AFT STATIONARY RING       114R3352-ALL
FWD STATIONARY RING       414R3351-2      1650-01-438-5361
AFT STATIONARY RING       414R3352-4      1615-01-439-4419
8.  INSPECTION PROCEDURES - 
                             NOTE
            SUPPLEMENTAL INFORMATION (PHOTOS/GRAPHICS) FOR 
            THIS INSPECTION CAN BE VIEWED AT: (USE LOWER CASE) 
            "www.redstone.army.mil/sof/suppl/c47s0201.pdf"
            FOR ASSISTANCE CONTACT THE SAFETY POC IN PARA 16E(1).
    A.  VISUALLY INSPECT FORWARD AND AFT SWASHPLATE ROTATING 
RINGS, ON AIRCRAFT, FOR CORRECT SELF-LOCKING NUT INSTALLATION ON 
THE LOWER SEAL RETAINERS.  THE CORRECT SELF-LOCKING NUTS, P/N 
FN22M-624, SHOULD BE INSTALLED SUCH THAT THREAD PROTRUSION IS 
EVIDENT. 
                             NOTE
THE INCORRECT NUT HEIGHT MEASURES 0.425"- 0.455" (NAS1758-L6)
THE CORRECT NUT HEIGHT MEASURES 0.350" MAXIMUM (FN22M-624)
    B.  IF CORRECT NUTS ARE FOUND AND THREAD PROTRUSION IS 
EVIDENT ON ALL 18 BOLTS ON EACH SWASHPLATE ASSEMBLY, NO FURTHER 
ACTION IS REQUIRED AND THE RED DASH //-// ENTRY REQUIRED IN 
PARAGRAPH 1A. MAY BE CLEARED.
    C.  IF INCORRECT NUTS ARE FOUND OR NO THREAD PROTRUSION IS 
OBSERVED, THE NUTS SHALL BE REPLACED, ONE AT A TIME, AND THE 
SWASHPLATE STATIONARY RING INSPECTED FOR DAMAGE.  
        (1)  VISUALLY INSPECT TOP SURFACE OF FORWARD AND AFT 
SWASHPLATE STATIONARY RINGS, ON AIRCRAFT, FOR GROOVES OR GOUGES 
IN THE AREA UNDERNEATH THE LOWER SEAL RETAINER NUTS.  
        (2)  A GROOVE IN THE STATIONARY RING INDICATES AN 
UNSERVICEABLE SWASHPLATE ASSEMBLY AND REQUIRES SWASHPLATE 
ASSEMBLY REPLACEMENT.  PROCEED TO PARAGRAPH 9 FOR CORRECTION 
PROCEDURES.
9.  CORRECTION PROCEDURES - 
                             NOTE
            THE FORWARD AND AFT SWASHPLATE ROTATING RING 
            LOWER SEAL RETAINER NUTS MAY BE REPLACED ON AIRCRAFT.
            HOWEVER, IF AN UNSERVICEABLE SWASHPLATE STATIONARY 
            RING IS FOUND, REPLACE SWASHPLATE ASSEMBLY.  
            IF UNABLE TO CHANGE/REPLACE THE NUT WITH 
            SWASHPLATE ON AIRCRAFT DUE TO ANY REASON, THEN 
            REMOVE SWASHPLATE AND ACCOMPLISH OFF AIRCRAFT.
                             WARNING
            IF A NUT, WASHER, BOLT, OR OTHER FOREIGN 
            OBJECT IS SUBSEQUENTLY DROPPED DURING REPLACEMENT, 
            IT MUST BE RECOVERED PRIOR TO FLIGHT.  
            FAILURE TO SECURE THE DROPPED ITEM WILL RESULT 
            IN A RED //X// CONDITION FOR THAT AIRCRAFT UNTIL 
            THE ITEM HAS BEEN RECOVERED.
    A.  IF INCORRECT NUTS ARE FOUND, BUT NO DAMAGE IS FOUND ON 
THE FORWARD AND AFT STATIONARY SWASHPLATE (ON AIRCRAFT)-
        (1)  HAVE HELPER SLOWLY ROTATE BLADES AND POSITION 
INCORRECT NUT IN AN OPEN AREA OF THE SWASHPLATE, WHICH WILL ALLOW 
IT TO BE EASILY REMOVED.  
                             CAUTION
            HAVE A HELPER HOLD THE ROTOR BLADES IN PLACE SO 
            THAT THE SWASHPLATE ROTATING RING DOES NOT MOVE.
        (2)  REPLACE ALL INCORRECT SWASHPLATE LOWER SEAL RETAINER 
NUTS WITH THE CORRECT NUT.  IF P/N FN22M-624 SELF-LOCKING NUTS 
ARE NOT AVAILABLE, P/N HS4143-4 IS AN ACCEPTABLE SUBSTITUTE.  
TORQUE NUTS TO A DRY TORQUE OF 350-380 INCH-POUNDS.
     B.  IF DAMAGE DUE TO INCORRECT NUT INSTALLATION IS FOUND ON 
EITHER THE FORWARD AND/OR AFT SWASHPLATE, REPLACE SWASHPLATE 
ASSEMBLY. 
     C.  PURGE ALL ON-HAND STOCK OF INCORRECT SWASHPLATE LOWER 
SEAL RETAINER SELF LOCKING NUTS
                             NOTE
THE INCORRECT NUT HEIGHT MEASURES 0.425"- 0.455" (NAS1758-L6)
THE CORRECT NUT HEIGHT MEASURES 0.350" MAXIMUM (FN22M-624)
10.  SUPPLY/PARTS AND DISPOSITION -
     A.  PARTS REQUIRED -ITEMS CITED IN PARAGRAPH 12C 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) "X-1-L" (X-RAY-ONE-LIMA).
                              NOTE
            PROJECT CODE "X1L" IS REQUIRED TO TRACK
            AND ESTABLISH A DATA BASE OF STOCK FUND
            EXPENDITURES INCURRED BY THE FIELD AS A
            RESULT OF MESSAGE ACTIONS.
     C.  BULK AND CONSUMABLE MATERIALS - 
  NOMENCLATURE         PART NUMBER              NSN
NUT, SELF-LOCKING  FN22M-624 OR HS4143-4  5310-01-184-0354
     D.  DISPOSITION - CONTACT THE LOGISTICS POC LISTED AT PARA 
16 FOR DISPOSITION INSTRUCTIONS.   
     E.  DISPOSITION OF HAZARDOUS MATERIAL - N/A.   
11.  SPECIAL TOOLS AND FIXTURES REQUIRED - AS REQUIRED.
12.  APPLICATION -
     A.  CATEGORY OF MAINTENANCE - AVUM.  AIRCRAFT DOWNTIME WILL 
BE CHARGED TO AVUM MAINTENANCE.  REPORT AIRCRAFT NON-MISSION 
CAPABLE MAINTENANCE (NMCM) WHILE UNDERGOING INSPECTION AND 
CORRECTION IAW THIS MESSAGE.  REPORT AIRCRAFT NON-MISSION CAPABLE 
SUPPLY (NMCS) WHILE WAITING FOR PARTS IAW THIS MESSAGE.
     B.  ESTIMATED TIME REQUIRED - 
         (1)  TIME TO COMPLETE INSPECTION - 
              (A)  TOTAL OF 2 MAN-HOURS USING 2 PERSONS.
              (B)  TOTAL OF 1 HOURS DOWNTIME FOR ONE END ITEM.
         (2)  TIME FOR REPLACEMENT OF NUTS (ASSUMING ALL 36 NUTS 
REQUIRE REPLACEMENT) - 
              (A)  TOTAL OF 6 MAN-HOURS USING 2 PERSONS.
              (B)  TOTAL OF 3 HOURS DOWNTIME FOR ONE END ITEM.
         (3) TIME FOR REPLACEMENT OF DAMAGED STATIONARY 
SWASHPLATE - 
              (A)  TOTAL OF 60 MAN-HOURS USING 5 PERSONS.
              (B)  TOTAL OF 12 HOURS DOWNTIME FOR ONE END ITEM.
     C.  ESTIMATED COST IMPACT TO THE FIELD - 
NOMENCLATURE    PART NO./NSN      QTY     COST EA.    TOTAL $
NUT, SELF-LOCKING  FN22M-624      
               5310-01-184-0354    36      $1.51      $54.36
SWASHPLATE ASSY. FWD  145R3551-19 
               1615-01-473-4376     1   $133245.00   $133,245.00
SWASHPLATE ASSY. AFT  145R3551-20
               1615-01-475-9838     1   $133245.00   $133,245.00
(IF ALL NUTS AND SWASHPLATE REPLACED) TOTAL COST: $266,544.36
     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 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)  TASK 5-126.1, PAGE 5-450.4.2, REMOVE "EPOXY 
PRIMER (E292)" FROM THE MATERIALS LIST.
              (B)  TASK 5-126.1, PAGE 5-450.4.4, REMOVE THE 
WARNING FROM PARAGRAPH 7.
              (C)  TASK 5-126.1, PAGE 5-450.4.4, PARAGRAPH 8, 
REMOVE THE FOLLOWING: "WET WITH EPOXY PRIMER (E292)".
              (D)  TASK 5-126.1, PAGE 5-450.4.4, IN PARAGRAPHS 8 
AND 10, CHANGE "285 INCH-POUNDS" TO "350-380 INCH-POUNDS".
              (E)  TASK 5-126.1, PAGE 5-450-4.4, ADD THE 
FOLLOWING NOTE BETWEEN PARAGRAPHS 8 AND 9: 
                             "NOTE
            DO NOT RE-USE ANY NUT (5) AFTER IT HAS BEEN 
            INSTALLED ONCE."
              (F)  TASK 5-126.1.1, PAGE 5-450.4.6, REMOVE "EPOXY 
PRIMER (E292)" FROM THE MATERIALS LIST.
              (G)  TASK 5-126.1.1, PAGE 5-450.4.8, REMOVE THE 
WARNING FROM PARAGRAPH 7.
              (H)  TASK 5-126.1.1, PAGE 5-450.4.8, PARAGRAPH 8, 
REMOVE THE FOLLOWING: "WET WITH EPOXY PRIMER (E292)".
              (I)  TASK 5-126.1.1, PAGE 5-450.4.8, IN PARAGRAPHS 
8 AND 10, CHANGE "285 INCH-POUNDS" TO "350-380 INCH-POUNDS".
              (J)  TASK 5-126.1.1, PAGE 5-450.4.8, AND ADD THE 
FOLLOWING NOTE BETWEEN PARAGRAPHS 8 AND 9: 
                             "NOTE
            DO NOT RE-USE ANY NUT (5) AFTER IT HAS BEEN 
            INSTALLED ONCE."
         (2)  TM 1-1520-252-23, AVIATION UNIT AND AVIATION 
INTERMEDIATE MAINTENANCE MANUAL, MH-47E HELICOPTER.
              (A)  TASK 5-181, PAGE 1, REMOVE "EPOXY PRIMER 
(E292)" FROM THE MATERIALS LIST.
              (B)  TASK 5-181, PAGE 3, REMOVE THE WARNING FROM 
PARAGRAPH 7.
              (C)  TASK 5-181, PAGE 3, IN PARAGRAPHS 8 AND 10 
CHANGE "285 INCH-POUNDS" TO "350-380 INCH-POUNDS".
              (D)  TASK 5-181, PAGE 3, ADD THE FOLLOWING NOTE 
BETWEEN PARAGRAPHS 8 AND 9: 
                             "NOTE
            DO NOT RE-USE ANY NUT (5) AFTER IT HAS BEEN 
            INSTALLED ONCE."
              (E)  TASK 5-181, PAGE 3, PARAGRAPH 10.1, CHANGE 
"195 INCH-POUNDS" TO "350-380 INCH-POUNDS".
              (F)  TASK 5-181.1, PAGE 1, REMOVE "EPOXY PRIMER 
(E292)" FROM THE MATERIALS LIST.
              (G)  TASK 5-181.1, PAGE 3, REMOVE THE WARNING FROM 
PARAGRAPH 7.
              (H)  TASK 5-181.1, PAGE 3, IN PARAGRAPHS 8 AND 10 
CHANGE "285 INCH-POUNDS" TO "350-380 INCH-POUNDS".
              (I)  TASK 5-181.1, PAGE 3, ADD THE FOLLOWING NOTE 
BETWEEN PARAGRAPHS 8 AND 9: 
                             "NOTE
            DO NOT RE-USE ANY NUT (5) AFTER IT HAS BEEN 
            INSTALLED ONCE."
              (J) TASK 5-181.1, PAGE 3, PARAGRAPH 10.1, CHANGE 
"195 INCH-POUNDS" TO "350-380 INCH-POUNDS".
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.  AIRCRAFT - 
         (1)  TAMMS REPORTING COMPLIANCE SUSPENSE - UPON ENTERING 
REQUIREMENTS OF THIS MESSAGE ON DA FORM 2408-13-1 FOR ALL EFFECTED 
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, NLT DATE SPECIFIED IN 
PARAGRAPH 3.  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.
         (2)  TASK/INSPECTION REPORTING SUSPENSE - UPON 
COMPLETION OF INSPECTION, COMMANDERS WILL FORWARD A PRIORITY 
MESSAGE TO THE LOGISTICAL POINT OF CONTACT LISTED IN 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 DATE SPECIFIED IN PARAGRAPH 2.
     B.  WHOLESALE SPARE PARTS/ASSEMBLIES - 
         (1) REPORTING MESSAGE RECEIPT - N/A.   
         (2) TASK/INSPECTION REPORTING SUSPENSE - N/A.   
     C.  RETAIL SPARE PARTS/ASSEMBLIES - 
         (1) REPORTING MESSAGE RECEIPT - N/A.   
         (2) TASK/INSPECTION REPORTING SUSPENSE - COMMANDERS AND 
FACILITY MANAGERS WILL REPORT INSPECTION RESULTS TO THE 
LOGISTICAL POINT OF CONTACT IN PARAGRAPH 16B NLT DATE SPECIFIED 
IN PARAGRAPH 1E(2).  REPORT THE QUANTITY INSPECTED BY CONDITION 
CODE AND THE RESULTING CONDITION CODE.  REPORT BY E-MAIL OR 
DATAFAX AND PROVIDE LOCAL POINT OF CONTACT.
     D.  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 
(SWASHPLATE ASSEMBLY AND ROTATING RING ASSEMBLY ).
         (2)  DA FORM 2408-13, AIRCRAFT STATUS INFORMATION 
RECORD.
         (3)  DA FORM 2408-13-1, AIRCRAFT INSPECTION AND 
MAINTENANCE RECORD.
         (4)  DA FORM 2408-16, AIRCRAFT COMPONENT HISTORICAL 
RECORD (ONLY IF SWASHPLATE ASSY. ROTATING RING ASSY. AND/OR 
FWD/AFT STATIONARY RING IS REMOVED AND/OR REPLACED).
         (5)  DA FORM 2410, COMPONENT REMOVAL AND REPAIR/OVERHAUL 
RECORD. (ONLY IF SWASHPLATE ASSY. ROTATING RING ASSY. AND/OR 
FWD/AFT STATIONARY RING IS REMOVED AND/OR REPLACED).
         (6)  DD FORM 1574/DD FORM 1574-1, SERVICEABLE TAG/LABEL 
- MATERIEL (COLOR YELLOW).  ANNOTATE REMARKS BLOCK WITH 
"INSPECTED SERVICEABLE IAW CH-47-02-01 (TB 1-1520-240-20-144)."
         (7)  DD FORMS 1577-2/DD FORM 1577-3, UNSERVICEABLE 
(REPARABLE) TAG/LABEL - MATERIEL (COLOR GREEN).  ANNOTATE REMARKS 
-BLOCK WITH UNSERVICEABLE IAW CH-47-02-01 (TB 1-1520-240-20-
144)."
15.  WEIGHT AND BALANCE - N/A.
16.  POINTS OF CONTACT - 
     A.  TECHNICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. STEVE 
PROSISE, AMSAM-RD-AE-I-P-C, DSN 897-3377 OR (256) 313-3377, 
DATAFAX IS DSN 897-4348 OR (256) 313-4348.  E-MAIL IS 
"STEVE.PROSISE@REDSTONE.ARMY.MIL".
     B.  LOGISTICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. 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.  WHOLESALE MATERIEL POINTS OF CONTACT (SPARES) IS 
MS LUCRETIA ROBERTS, AMSAM-MMC-AV-CAB DSN 897-1526 OR (256) 313-
1526, DATAFAX IS DSN 897-1106.  E-MAIL IS 
"LUCRETIA.ROBERTS@REDSTONE.ARMY.MIL".
     D.  FORMS AND RECORDS POINT OF CONTACT FOR THIS MESSAGE IS 
MS. ANN WALDECK, AMSAM-MMC-MA-NM, DSN 746-5564 OR (256) 876-5564, 
DATAFAX IS DSN 746-4904.  E-MAIL IS 
"ANN.WALDECK@REDSTONE.ARMY.MIL".
     E.  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 
MR. RONNIE W. SAMMONS, AMSAM-SA-CS-NF, DSN 897-6856 OR (256) 313-
6856.  DATAFAX IS DSN 897-6630 OR (256) 313-6630.  EMAIL IS 
"RONNIE.SAMMONS@REDSTONE.ARMY.MIL".
     G.  AFTER HOURS CONTACT THE AMCOM COMMAND OPERATIONS CENTER 
(COC) DSN 897-2066/7 OR (256) 313-2066/7.  
DRAFT SOF/ASAM    Page 1 of 9