01 15 191716Z OCT 00 PP PP UUUU AA ZYUW : FROM :CDRAMCOM REDSTONE ARSENAL AL//AMSAM-SF-A// TO :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// :ODC THE HAGUE NL//AVIATION SAFETY// :RNLAF MATERIAL :RNLAF OPERATIONS :RNLAF TACTICAL AIR FORCE :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// XMT : ACCT : TEXT :UNCLAS SUBJECT - AVIATION SAFETY ACTION MESSAGE (ASAM), MAINTENANCE MANDATORY, RCS CSGLD-1860(R1), ALL H-47 SERIES AIRCRAFT, INSPECTION FOR UNTESTED FLIGHT SAFETY PART (FSP) BOLTS, P/N 114R3650-6 AND 114R3650-11, CH-47-01-ASAM-02 (TB 1-1520-240-20-130). NOTE THIS IS AN AVIATION SAFETY ACTION MESSAGE (ASAM) 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 FOR UNTESTED FSP P/N 114R3650-6 AND 114R3650-11 BOLTS IAW CH-47- 01-ASAM-02 (TB 1-1520-240-20-130) WITHIN THE NEXT 15 FLIGHT HOURS, BUT NLT 18 NOVEMBER 2000." 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 18 NOVEMBER 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 - 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 - (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 PARA 10D. G. COMPONENTS/PARTS IN WORK (DEPOT LEVEL AND OTHERS) - N/A. 2. TASK/INSPECTION SUSPENSE DATE - COMPLETE THE INSPECTION IAW PARAGRAPH 8 WITHIN THE NEXT 15 FLIGHT HOURS BUT NLT 18 NOVEMBER 2000 AND REPORT IAW PARA 14B. 3. REPORTING COMPLIANCE SUSPENSE DATE - REPORT COMPLIANCE IAW PARA 14A NLT 13 NOVEMBER 2000. 4. SUMMARY OF PROBLEM - A. THE ORIGINAL QUALIFICATION (FATIGUE TESTING) OF FLIGHT SAFETY PARTS WAS DONE BY BOEING HELICOPTERS UNDER ARMY DIRECTION. THE FATIGUE TESTING OF THESE PARTS SUBSTANTIATED THEIR SERVICE LIFE AND THE PARTS DESIGN WAS CONSIDERED QUALIFIED. IN OCTOBER 1995 A CHANGE IN THE ARMY FLIGHT SAFETY PART (FSP) POLICY REQUIRED THAT PARTS MANUFACTURED BY AUTHORIZED VENDORS/SUPPLIERS AND ORIGINALLY QUALIFIED BY THE PRIME CONTRACTOR MUST BE FATIGUE TESTED. THE 114R3650-6 AND 114R3650-11 BOLT ASSEMBLIES ARE FLIGHT SAFETY PARTS. THE 114R3650-6 BOLTS (2 PER FORWARD ROTOR HEAD) ATTACH THE FORWARD CYCLIC TRIM ACTUATOR, AND FIXED LINK, TO THE SWASHPLATE. THE 114R3650-11 BOLT (1 PER FORWARD AND AFT ROTOR HEAD) ATTACH THE DRIVE SCISSORS UPPER ARM TO THE DRIVE SCISSORS LOWER ARM. SOME OF THE 114R3650-6 AND 114R3650-11 BOLTS, MANUFACTURED BY BOEING AUTHORIZED VENDORS/SUPPLIERS, WERE FIELDED BEFORE THEY WERE QUALIFIED AS AN ALTERNATE SOURCE BY FATIGUE TESTING. B. FOR MANPOWER/DOWNTIME AND FUNDING IMPACTS SEE PARA 12. C. THE PURPOSE OF THIS MESSAGE IS TO - (1) INSPECT ALL 114R3650-6 AND 114R3650-11 BOLTS INSTALLED ON H-47 AIRCRAFT AND IN STOCK. (2) REPLACE ALL SUSPECT BOLTS AT THE NEXT PHASE INSPECTION, BUT NLT 20 OCTOBER 2001. 5. END ITEMS TO BE INSPECTED - ALL H-47 SERIES AIRCRAFT. 6. ASSEMBLY COMPONENTS TO BE INSPECTED - N/A. 7. PARTS TO BE INSPECTED - NOMENCLATURE PART NO. NSN BOLT ASSEMBLY 114R3650-6 1615-00-003-1148 BOLT ASSEMBLY 114R3650-11 1615-00-003-1153 8. INSPECTION PROCEDURES - NOTE THERE MAY BE TWO DIFFERENT FIVE DIGIT CODES MARKED ON THE PART. THE FIVE DIGIT CODE 81996 IS NOT THE MANUFACTURERS CAGE CODE. IF FOUND, THE NUMBER 81996 IDENTIFIES THE PART AS HAVING BEEN MANUFACTURED IAW A GOVERNMENT TECHNICAL DATA PACKAGE (TDP). USE THE OTHER FIVE-DIGIT CODE WHICH IS THE MANUFACTURERS CAGE CODE. A. 114R3650-6 BOLT ASSEMBLY - (1) LOCATE BOTH APPLICATIONS OF THE 114R3650-6 BOLT ASSEMBLY - ATTACHMENT, CYCLIC TRIM ACTUATOR; AND FIXED LINK TO THE SWASHPLATE, FORWARD ROTOR HEAD (TM 55-1520-240-23P, FIGURE 177, ITEM 38) OR TM 1-1520-252-23P, FIGURE 05-6, ITEM 38). (2) IDENTIFY THE FIVE DIGIT MANUFACTURERS CAGE CODE OR MANUFACTURERS NAME ON THE BOLT HEAD. IF THE 114R3650-6 BOLT IS MARKED WITH EITHER OF THE FOLLOWING, THE BOLTS ARE SERVICEABLE. (A) 56878 OR SPS FOR PARTS MANUFACTURED BY SPS TECHNOLOGIES INC. (B) 84256 OR AVIBANK FOR PARTS MANUFACTURED BY AVIBANK MANUFACTURING CO. B. 114R3650-11 BOLT ASSEMBLY - (1) LOCATE THE TWO APPLICATIONS OF THE 114R3650-11 BOLT ASSEMBLY - ATTACHMENT, DRIVE SCISSORS UPPER ARM TO THE DRIVE SCISSORS LOWER ARM, FORWARD AND AFT ROTOR HEADS (TM 55-1520-240-23P, FIGURE 177, ITEM 45) OR (TM 1-1520-252-23P, FIGURE 05-6, ITEM 45). (2) IDENTIFY THE FIVE DIGIT MANUFACTURERS CAGE CODE OR MANUFACTURERS NAME ON THE BOLT HEAD. IF THE 114R3650-11 BOLT IS MARKED WITH EITHER 84256 OR AVIBANK, THE BOLT IS SERVICEABLE. C. IF THE 114R3650-6 AND 114R3650-11 BOLTS ARE DETERMINED SERVICEABLE, THE RED HORIZONTAL DASH //-// WILL BE CLEARED AND COMPLIANCE WITH CH-47-01-ASAM-02 (TB 1-1520-240-20-130) WILL BE NOTED. D. IF THE MARKINGS ON THE BOLTS ARE ANYTHING OTHER THAN THE CAGE CODES OR MANUFACTURES NAME LISTED IAW PARA 8A(2) AND 8B(2) ABOVE, OR IF THE CAGE CODE OR MANUFACTURES NAME CANNOT BE IDENTIFIED, PROCEED TO THE CORRECTION PROCEDURES IN PARA 9. 9. CORRECTION PROCEDURES - A. CLEAR THE RED HORIZONTAL DASH //-// AND MAKE THE FOLLOWING ENTRY ON THE DA FORM 2408-13-1. ENTER A RED HORIZONTAL DASH //-// STATUS SYMBOL WITH THE FOLLOWING STATEMENT: "REPLACE UNTESTED (ENTER EITHER P/N 114R3650-6 AND/OR 114R3650-11) BOLTS AT THE NEXT PHASE INSPECTION INTERVAL BUT NLT 20 OCTOBER 2001, WHICHEVER OCCURS FIRST." B. AT THE NEXT SCHEDULED PHASE INSPECTION, BUT NLT 20 OCT 01 - (1) REMOVE AND REPLACE UNSERVICEABLE 114R3650-6 BOLTS WITH A TESTED BOLT FROM THE SUPPLY SYSTEM THAT IS SERVICEABLE AS DEFINED IN PARA 8 ABOVE. (A) H-47D AIRCRAFT - REFER TO TM 55-1520-240-23-4, TASK 5-116 (REMOVAL) AND TASK 5-132 (INSTALL). (B) MH-47E AIRCRAFT - REFER TO TM 1-1520-252-23-5, TASK 5-168 (REMOVAL) AND TASK 5-187 (INSTALL). (2) REMOVE AND REPLACE UNSERVICEABLE 114R3650-11 BOLTS WITH A TESTED BOLT FROM THE SUPPLY SYSTEM THAT IS SERVICEABLE AS DEFINED IN PARA 8 ABOVE. (A) H-47D AIRCRAFT - REFER TO TM 55-1520-240-23-4, TASK 5-101 (REMOVAL), TASK 5-112 (INSTALL). (B) MH-47E AIRCRAFT - REFER TO TM 1-1520-252-23-5, TASK 5-152 (REMOVAL), TASK 5-163 (INSTALL). C. AFTER COMPLETION OF THE ABOVE CORRECTION PROCEDURE, THE RED HORIZONTAL DASH //-// ENTRY WILL BE CLEARED AND COMPLIANCE WITH CH-47-01-ASAM-02 (TB 1-1520-240-20-130) WILL BE NOTED. 10. SUPPLY/PARTS AND DISPOSITION - A. PARTS REQUIRED - ITEMS CITED IN PARA 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) "X08" (XRAY-ZERO-EIGHT). NOTE PROJECT CODE "X08" 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 - DEMILITARIZE/MUTILATE IAW TM 1-1500-328-23 ANY PART/COMPONENT WHICH DOES NOT MEET INSPECTION CRITERIA. E. DISPOSITION OF HAZARDOUS MATERIAL - N/A. 11. SPECIAL TOOLS AND FIXTURES REQUIRED - N/A. 12. APPLICATION - A. CATEGORY OF MAINTENANCE - AVUM. AIRCRAFT DOWNTIME WILL BE CHARGED TO AVUM. B. ESTIMATED TIME REQUIRED - (1) FOR INSPECTION - (A) TOTAL OF 1 MAN-HOUR USING 2 PERSONS. (B) TOTAL OF 1 HOUR DOWNTIME FOR ONE END ITEM. (2) FOR REPLACEMENT - (1) TOTAL OF 15 MAN-HOURS USING 3 PERSONS. (2) TOTAL OF 5 HOURS DOWNTIME FOR ONE END ITEM. C. ESTIMATED COST IMPACT TO THE FIELD - NOMENCLATURE PART NO./NSN QTY COST EA. TOTAL $ BOLT ASSEMBLY 114R3650-6 2 $ 89.56 $179.12 1615-00-003-1148 BOLT ASSEMBLY 114R3650-11 2 $171.70 $343.40 1615-00-003-1153 TOTAL COST PER AIRCRAFT = $522.52 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 - N/A. 13. REFERENCES - A. DA PAM 738-751, 15 MAR 99. B. TM 55-1520-240-23. C. TM 55-1520-240-23P. D. TM 1-1520-252-23. E. TM 1-1520-252-23P. F. TM 1-1500-328-23. 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, 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-47-01-ASAM-02 (TB 1-1520-240-20-130), 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, PEO AVN, ATTN: MR. BILL OLSON, SFAE-AV-CH-L, DSN 897-3379 OR (256) 313-3379, DATAFAX IS DSN 897-4348. E-MAIL IS "WILLIAM.OLSON@PEOAVN.REDSTONE.ARMY.MIL". THE REPORT WILL CITE CH-47-01-ASAM-02 (TB 1-1520-240-20-130), DATE OF INSPECTION, AIRCRAFT SERIAL NUMBER, AIRCRAFT HOURS, AND RESULTS OF THE INSPECTION. INSPECTION AND REPORTS WILL BE COMPLETED NLT 1 DECEMBER 2000. C. REPORTING MESSAGE RECEIPT (SPARES) - 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 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-47-01-ASAM-02 (TB 1-1520-240-20-130)." (5) DD FORM 1577/DD FORM 1577-1, UNSERVICEABLE (CONDEMNED) TAG/LABEL - MATERIEL (COLOR RED). ANNOTATE REMARKS BLOCK WITH "CONDEMNED IAW CH-47-01-ASAM-02 (TB 1-1520-240-20-130) AND MUTILATED IAW TM 1-1500-328-23." 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 DSN 897-4348. E-MAIL IS "LARRY.WIESCHHAUS@REDSTONE.ARMY.MIL". B. LOGISTICAL POINT OF CONTACT IS MR. BILL OLSON, SFAE-AV-CH-L, DSN 897-3379 OR (256) 313-3379, DATAFAX IS DSN 897-4348. E-MAIL IS "WILLIAM.OLSON@PEOAVN.REDSTONE.ARMY.MIL". C. 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 "ANN.WALDECK@REDSTONE.ARMY.MIL". D. SAFETY POINTS OF CONTACT ARE - (1) PRIMARY - MR. HARRY TRUMBULL (SAIC), AMSAM-SF-A, DSN 897-2095 OR (256) 313-2095, DATAFAX IS DSN 895-2111 OR (256) 313-2111. E-MAIL IS "HARRY.TRUMBULL@REDSTONE.ARMY.MIL". (2) ALTERNATE - MR. RUSS 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". E. FOREIGN MILITARY SALES RECIPIENTS REQUIRING CLARIFICATION OF ACTION ADVISED BY THIS MESSAGE SHOULD CONTACT - (1) CW5 JOSEPH L. WITTSTROM, SECURITY ASSISTANCE MANAGEMENT, AMSAM-SA, DSN 897-0410 OR (256) 313-0410. EMAIL IS "WITTSTROMJL@REDSTONE.ARMY.MIL". (2) 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". G. AFTER HOURS CONTACT THE AMCOM COMMAND OPERATIONS CENTER (COC) DSN 897-2066/7 OR (256) 313-2066/7. HUNTSVILLE, AL IS GMT MINUS 5 HRS.