Safety of Flight CH-47-02-05 |
Summary of Problem: CH-47-02-03 was issued on 24 January 2002 requiring inspection of the Tie Bar Assembly and Rotor Tachometer. With regard to the tie bar inspections, the intent of the message was to inspect for cracked plates and deformation of washers only. Scores, scratches, buckling/separation of plates, and other minor installation damage are not grounds for failing this special inspection. The 1200 hour operating time special inspection will still be required. At the time the 1200 hour operating time special inspection is due, all tie bars that fail the inspection criteria of TM 55-1520-240-23, TASK 5-23.1.1 (H-47D/F), or TM 1-1520-252-23, TASK 5-31 (MH-47E), will require replacement. |
UNCLASSIFIED MSG DTG 222110Z MAR 02 FROM CDRAMCOM, REDSTONE ARSENAL, AL //AMSAM-SF-A// SUBJECT - SAFETY OF FLIGHT, TECHNICAL, RCS CSGLD-1860(R1), ALL H-47 SERIES AIRCRAFT, INSPECTION OF THE ROTARY WING HEAD TIE BAR ASSEMBLY, CH-47-02-05 (TB 1-1520-240-20-146). NOTE THIS MESSAGE SUPERCEDES INSPECTION AND CORRECTION REQUIREMENTS OF PARAGRAPHS 8B AND 9A (TIE BAR ASSY) OF CH-47-02-03 (TB 1-1520-240-20-141) FOR AIRCRAFT THAT HAVE NOT ALREADY BEEN INSPECTED. TIE BARS/AIRCRAFT THAT PASSED INSPECTION IAW CH-47-02-03 DO NOT REQUIRE RE-INSPECTION. THIS MESSAGE PROVIDES REVISED INSPECTION AND CORRECTION PROCEDURES FOR THE TIE BAR ASSY. AND PROVIDES ADDITIONAL TM CHANGES IN PARA 12 THE PROCEDURES RELATING TO THE ROTOR TACH IN CH-47-02-03 (TB 1-1520-240-20-141) REMAIN UNCHANGED. 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, 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 ENTRIES ON THE DA FORM 2408-13-1. 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//. (1) FOR ALL H-47 - ENTER A RED HORIZONTAL DASH //-// STATUS SYMBOL WITH THE FOLLOWING STATEMENT: "INSPECT TIE BAR ASSEMBLIES IAW CH-47-02-05 (TB 1-1520-240-20-146) NLT 27 MAR 02." (2) CLEAR ENTRIES REQUIRED IAW CH-47-02-03, PARA 1A(1) AND/OR 8A(1)(B) FROM THE DA FORM 2408-13-1. 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 - SAME AS PARA 1A. D. MAINTENANCE TRAINERS (CATEGORY A AND B) - COMPLY NLT 25 JAN 04. 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 PARAGRAPH 6 ARE ANNOTATED TO READ: "CH-47-02-05 (TB 1-1520-240-20-146), INSPECTION OF TIE BAR ASSEMBLIES 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 PARA 10. REPORT COMPLIANCE WITH THIS MESSAGE IAW PARA 14C(2) NLT 3 APR 02. F. COMPONENTS/PARTS IN WORK (DEPOT LEVEL AND OTHERS) - DEPOT AND OTHER MAINTENANCE ACTIVITY COMMANDERS WILL ENSURE ITEMS LISTED IN PARAGRAPH 6 ARE NOT ISSUED UNTIL THEY ARE IN COMPLIANCE WITH THIS MESSAGE. 2. TASK/INSPECTION SUSPENSE DATE - A. COMPLETE THE PROCEDURES IAW PARAGRAPH 8A NLT 27 MAR 02. B. COMPLETE THE INSPECTION IAW PARAGRAPH 8B AT THE NEXT ROTOR HEAD REMOVAL, BUT NLT THE NEXT PHASE INSPECTION OR 25 JAN 04, WHICHEVER OCCURS FIRST. 3. TAMMS REPORTING COMPLIANCE SUSPENSE DATE - REPORT COMPLIANCE IAW PARA 14A(1) NLT 27 MAR 02. 4. SUMMARY OF PROBLEM - A. CH-47-02-03 WAS ISSUED ON 24 JANUARY 2002 REQUIRING INSPECTION OF THE TIE BAR ASSEMBLY AND ROTOR TACHOMETER. WITH REGARD TO THE TIE BAR INSPECTIONS, THE INTENT OF THE MESSAGE WAS TO INSPECT FOR CRACKED PLATES AND DEFORMATION OF WASHERS ONLY. SCORES, SCRATCHES, BUCKLING/SEPARATION OF PLATES, AND OTHER MINOR INSTALLATION DAMAGE ARE NOT GROUNDS FOR FAILING THIS SPECIAL INSPECTION. THE 1200 HOUR OPERATING TIME SPECIAL INSPECTION WILL STILL BE REQUIRED. AT THE TIME THE 1200 HOUR OPERATING TIME SPECIAL INSPECTION IS DUE, ALL TIE BARS THAT FAIL THE INSPECTION CRITERIA OF TM 55-1520-240-23, TASK 5-23.1.1 (H-47D/F), OR TM 1-1520-252-23, TASK 5-31 (MH-47E), WILL REQUIRE REPLACEMENT. B. MANPOWER/DOWNTIME AND FUNDING IMPACTS - SEE PARA 12. C. THE PURPOSE OF THIS MESSAGE IS TO - (1) REVISE THE TIE BAR INSPECTION PROCEDURES REQUIRED BY CH-47-02-03 (TB 1-1520-240-20-141). (2) ADD ADDITIONAL MANUAL CHANGES FOR TIE BAR ASSEMBLY INSPECTION CRITERIA TO PARAGRAPH 12E. 5. END ITEMS TO BE INSPECTED - ALL H-47 SERIES AIRCRAFT. 6. ASSEMBLY COMPONENTS TO BE INSPECTED - NOMENCLATURE PART NO. NSN ROTOR HEAD ASSEMBLY 145R2003-ALL ALL ROTOR HEAD ASSEMBLY 145R2004-ALL ALL TIE BAR ASSEMBLY 114R2155-1 1615-00-740-6480 7. PARTS TO BE INSPECTED - N/A. 8. INSPECTION PROCEDURES - NOTE DUE TO THE POSSIBILITY OF HANDLING DAMAGE, TIE BAR ASSEMBLIES THAT WERE PREVIOUSLY REJECTED DURING COMPLIANCE WITH SOF CH-47-02-03 DUE TO FAILING THE INSPECTION REQUIREMENTS OF TM 55-1520-240-23, TASK 5-23.1.1 (H-47D/F), OR TM 1-1520-252-23, TASK 5-31 (MH-47E), FOR OTHER THAN CRACKS AND/OR DEFORMED WASHERS, SHALL BE DISPOSED OF IAW PARA 10D. NOTE READ AND COMPLETE ALL PARAGRAPH 8 INSPECTION PROCEDURES FOR EACH PART PRIOR TO PROCEEDING TO THE CORRECTION PROCEDURES IN PARAGRAPH 9. A. UTILIZING THE INSPECTION RESULTS OF CH-47-02-03 (TB 1-1520-240-20-141), PARA 8A, PROCEED AS FOLLOWS - (1) IF TSN IS LESS THAN 4800 HOURS - (A) CHANGE THE ROTOR HEAD DA FORM 2408-16 TO INDICATE A NEW RETIREMENT LIFE FOR THE TIE BAR ASSEMBLY OF 4800 HRS TSN. (B) CLEAR THE RED HORIZONTAL DASH //-// ENTRY REQUIRED IAW PARA 1A(1) OF THIS MESSAGE AND ENTER A NEW RED HORIZONTAL DASH //-// STATUS SYMBOL WITH THE FOLLOWING STATEMENT: "INSPECT ALL TIE BAR ASSEMBLIES IAW PARA 8B, CH-47-02-05 (TB 1- 1520-240-20-146) AT THE NEXT ROTOR HEAD REMOVAL, BUT NLT THE NEXT PHASE INSPECTION OR 25 JAN 04." NOTE ROTOR HEADS WHICH HAVE ZERO HOURS TIME SINCE OVERHAUL (TSO) OR ZERO HOURS TIME SINCE NEW (TSN) DO NOT REQUIRE INSPECTION OF THE TIE BAR ASSEMBLIES IAW PARA 8B. (2) IF TSN IS EQUAL TO OR GREATER THAN 4800 HOURS, CORRECT IAW PARA 9. NOTE AIRCRAFT THAT WERE INSPECTED IAW CH-47-02-03 (TB 1-1520-240-20-141) DO NOT REQUIRE RE-INSPECTION IAW PARA 8B. B. AT THE NEXT ROTOR HEAD REMOVAL, BUT NLT THE NEXT PHASE INSPECTION OR (25 JAN 04), WHICHEVER OCCURS FIRST, INSPECT THE TIE BAR ASSEMBLIES AS FOLLOWS - (1) REMOVE TIE BAR ASSEMBLIES IAW TM 55-1520-240-23, TASK 5-23.1 (H-47D/F), OR TM 1-1520-252-23, TASK 5-30 (MH-47E). NOTE THE PROCEDURE IN PARA 8B(2) IS ONLY FOR THE INSPECTION OF TIE BAR ASSEMBLIES FOR CRACKED PLATES AND DEFORMED OR CRACKED WASHERS. THE TIE BAR ASSEMBLY WILL BE INSPECTED PER TM 55-1520-240-23 (H-47D/F), OR TM 1-1520-252-23 (MH-47E), AT THE NEXT HORIZONTAL HINGE PIN ROTATION. THE SPECIAL INSPECTION REQUIRED BY THIS SAFETY OF FLIGHT DOES NOT ZERO THE 1200 HOUR OPERATING TIME SPECIAL INSPECTION REQUIRED IN TM 55-1520-240-23, TASK 1-92 (H-47D/F), REF NO. 21, 0R TM 1-1520-252-23, TASK 1-100 (MH-47E), REF NO. 17. (2) INSPECT TIE BAR ASSEMBLIES AS FOLLOWS - (A) VISUALLY INSPECT TIE BAR PLATES FOR CRACKS USING 10X MAGNIFICATION. NO CRACKS ALLOWED. NOTE SURFACE IRREGULARITIES (I.E. SCRATCHES AND MANUFACTURING DEFECTS) FOUND WHILE USING THE 10X MAGNIFICATION ARE NOT GROUNDS FOR REJECTION. (B) INSPECT THE FOUR TIE BAR SLOTS USING A BORESCOPE WITH A RIGID RIGHT ANGLE PROBE. INSERT THE BORESCOPE PROBE IN EACH SLOT AND EXAMINE THE PLATES FOR CRACKS ALONG THE FULL DEPTH AND SPAN OF THE SLOT. RECOMMEND THE PROBE NOT EXCEED 0.110 INCH DIAMETER. IF A SUITABLE BORESCOPE AND PROBE ARE NOT AVAILABLE, VISUALLY INSPECT EACH SLOT USING A LIGHT SOURCE. NOTE CRACKS WILL APPEAR PERPENDICULAR TO THE PLATE SURFACES AND SHOULD NOT BE CONFUSED WITH HORIZONTAL SCRATCHES OR TOOL MARKS. (C) INSPECT WASHERS FOR DEFORMATION (DISHING) AND CRACKS. A DISHED WASHER WILL HAVE A GAP BETWEEN IT AND THE ADJACENT PLATE. THE MAXIMUM SEPARATION BETWEEN THE WASHER AND THE ADJACENT PLATE IS 0.015 INCH. NO CRACKS ALLOWED. (3) IF A TIE BAR ASSEMBLY FAILS AN INSPECTION IAW PARA 8B, CORRECT IAW PARA 9. (4) IF NO DAMAGE IS FOUND - (1) REINSTALL THE ROTARY WING HEAD TIE BAR ASSEMBLIES IAW TM 55-1520-240-23, TASK 5-23.2 (H-47D/F) OR TM 1-1520-252-23, TASK 5-32 (MH-47E). (2) CLEAR THE RED HORIZONTAL DASH //-// ENTRY. 9. CORRECTION PROCEDURES - IF THE TSN IS EQUAL TO OR MORE THAN 4800 HRS, OR IF A TIE BAR ASSEMBLY FAILS AN INSPECTION IAW PARA 8B, PROCEED AS FOLLOWS - A. CHANGE THE ROTOR HEAD DA FORM 2408-16 TO INDICATE A NEW RETIREMENT LIFE FOR TIE BAR ASSEMBLY OF 4800 HRS TSN. B. CLEAR THE RED HORIZONTAL DASH //-// ENTRY AND ENTER A RED //X// STATUS SYMBOL WITH THE FOLLOWING STATEMENT: "REPLACE THE ROTARY WING HEAD TIE BAR ASSEMBLIES IAW CH-47-02-05 (TB 1- 1520-240-20-146)." C. SUBMIT A CATEGORY I DEFICIENCY REPORT ON ANY TIE BAR ASSEMBLY THAT HAS FAILED THE INSPECTION REQUIRED IAW PARA 8B DUE TO CRACKS. D. IF YOU HAVE TIE BARS ON HAND WHICH PREVIOUSLY FAILED THE INSPECTION IAW CH-47-02-03 FOR OTHER THAN CRACKS AND/OR DEFORMED WASHERS, REFER TO PARAGRAPH 10D FOR DISPOSITION INSTRUCTIONS. E. IF TSN IS EQUAL TO OR MORE THAN 4800 HOURS, CONTACT THE TECH POC IN PARA 16A FOR DISPOSITION INSTRUCTIONS. NOTE ENSURE THAT REPLACEMENT TIE BAR ASSEMBLIES ARE INSPECTED AND IN COMPLIANCE WITH THIS SOF PRIOR TO INSTALLATION. F. REPLACE THE ROTARY WING HEAD TIE BAR ASSEMBLIES IAW TM 55-1520-240-23, TASK 5-23.2 (ALL H-47D/F) OR TM 1-1520-252-23, TASK 5-32 (MH-47E). G. CLEAR THE RED //X// ENTRY FROM PARA 9B. 10. SUPPLY/PARTS AND DISPOSITION - A. PARTS REQUIRED - ITEMS CITED IN PARAGRAPH 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) "X13" (X-RAY-ONE-THREE). NOTE PROJECT CODE "X13" 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 - THE FOLLOWING MATERIALS WILL BE REQUIRED - NOMENCLATURE PART NO. NSN BOLT 114R2162-1 5306-00-926-5684 NUT, SELF-LOCK MS21083N4 5310-00-903-8282 BOLT AN4H30A 5306-00-182-2022 SEAL 114R2142-3 5330-00-913-0933 SEAL 114RS215-1 5330-00-248-5142 D. DISPOSITION - (1) IF CRACKS ARE FOUND IN THE TIE BAR ASSEMBLY, DISPOSITION INSTRUCTIONS WILL BE PROVIDED UPON RECEIPT OF THE CATEGORY I DEFICIENCY REPORT. (2) IF TIE BAR FAILED INSPECTION DUE TO DEFORMED WASHER, DISPOSE OF USING NORMAL SUPPLY PROCEDURES. (3) TIE BARS ON HAND WHICH PREVIOUSLY FAILED THE INSPECTION IAW CH-47-02-03 FOR OTHER THAN CRACKS AND/OR DEFORMED WASHERS SHALL BE SHIPPED TO - SR CORPUS CHRISTI ARMY DEPOT SRA BUILDING 1846 CORPUS CHRISTI, TX 78419-6030 (4) IF TIE BAR ASSEMBLY TSN IS EQUAL TO OR MORE THAN 4800 HOURS, CONTACT THE TECH POC IN PARA 16A 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. B. ESTIMATED TIME REQUIRED - (1) TIME TO COMPLETE RECORDS CHECK - TOTAL OF 0.5 HOURS USING 1 PERSON. (2) TIME TO COMPLETE INSPECTION OF THE TIE BAR ASSY. - (A) TOTAL OF 124 MAN-HOURS USING 8 PERSONS. (B) TOTAL OF 20.0 HOURS DOWNTIME FOR ONE END ITEM. DOWNTIME INCLUDES TIME REQUIRED MAINTENANCE TEST FLIGHT. C. ESTIMATED COST IMPACT TO THE FIELD - NOMENCLATURE PART NO./NSN QTY COST EA. TOTAL $ TIE BAR ASSEMBLY 114R2155-1 6 $5675.15 $34,050.90 1615-00-740-6480 TIE BAR PIN 114R2168-3 6 33.34 200.04 1615-00-740-6477 TIE BAR PIN 114R2168-4 6 63.05 378.30 1615-01-115-3619 TOTAL COST PER AIRCRAFT = $34,629.24 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, TASK 5-23.1.1 - (A) CHANGE PARA 2.G. TO READ AS FOLLOWS - INSPECT WASHERS FOR DEFORMATION (DISHING) AND CRACKS. A DISHED WASHER WILL HAVE A GAP BETWEEN IT AND THE ADJACENT PLATE. THE MAXIMUM SEPARATION BETWEEN THE WASHER AND THE ADJACENT PLATE IS 0.015 INCH. NO CRACKS ALLOWED." (B) CHANGE TITLE OF TASK 5-23.1.1 TO READ AS FOLLOWS - "1200 HOUR TIE BAR AND PIN ASSEMBLIES INSPECTION". (2) TM 55-1520-240-23, AVIATION UNIT AND AVIATION INTERMEDIATE MAINTENANCE MANUAL, CH-47D HELICOPTER, TASK 5-23.2 - ADD THE FOLLOWING TO THE "INITIAL SETUP" SECTION TO READ AS FOLLOWS: "EQUIPMENT CONDITION: TIE BAR INSPECTED IAW TASK 5-23.1.2" (3) TM 1-1520-252-23, AVIATION UNIT AND AVIATION INTERMEDIATE MAINTENANCE MANUAL, MH-47E HELICOPTER, TASK 5-31 - (A) CHANGE PARA 2.F. TO READ AS FOLLOWS- -"INSPECT WASHERS FOR DEFORMATION (DISHING) AND CRACKS. A DISHED WASHER WILL HAVE A GAP BETWEEN IT AND THE ADJACENT PLATE. THE MAXIMUM SEPARATION BETWEEN THE WASHER AND THE ADJACENT PLATE IS 0.015 INCH. NO CRACKS ALLOWED." (B) CHANGE TITLE OF TASK 5-31 TO READ AS FOLLOWS - "1200 HOUR TIE BAR AND PIN ASSEMBLIES INSPECTION". (4) TM 1-1520-252-23, AVIATION UNIT AND AVIATION INTERMEDIATE MAINTENANCE MANUAL, MH-47E HELICOPTER, TASK 5-32 - ADD THE FOLLOWING TO THE "INITIAL SETUP" SECTION UNDER 'EQUIPMENT CONDITION' TO READ AS FOLLOWS: "TIE BAR INSPECTED IAW TASK 5-31.1" (5) TM 55-1520-240-23, TASK 5-23.1.2 (CH-47D) AND TM 1-1520-252-23, TASK 5-31.1 (MH-47E) - INSERT A NEW TASK, TITLE SHOULD READ: "INSPECT TIE BAR ASSEMBLY", PROCEDURES TO READ AS FOLLOW - (1) VISUALLY INSPECT TIE BAR PLATES FOR CRACKS USING 10X MAGNIFICATION. NO CRACKS ALLOWED. (2) INSPECT THE FOUR TIE BAR SLOTS USING A BORESCOPE WITH A RIGID RIGHT ANGLE PROBE. INSERT THE BORESCOPE PROBE IN EACH SLOT AND EXAMINE THE PLATES FOR CRACKS ALONG THE FULL DEPTH AND SPAN OF THE SLOT. RECOMMEND THE PROBE NOT EXCEED 0.110 INCH DIAMETER. IF A SUITABLE BORESCOPE AND PROBE ARE NOT AVAILABLE, VISUALLY INSPECT EACH SLOT USING A LIGHT SOURCE. NOTE CRACKS WILL APPEAR PERPENDICULAR TO THE PLATE SURFACES AND SHOULD NOT BE CONFUSED WITH HORIZONTAL SCRATCHES OR TOOL MARKS. (3) INSPECT WASHERS FOR DEFORMATION (DISHING) AND CRACKS. A DISHED WASHER WILL HAVE A GAP BETWEEN IT AND THE ADJACENT PLATE. THE MAXIMUM SEPARATION BETWEEN THE WASHER AND THE ADJACENT PLATE IS 0.015 INCH. NO CRACKS ALLOWED." 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, FAX OR EMAIL 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. FAX NUMBER IS DSN 897-2111 OR (256) 313-2111. EMAIL 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 - N/A. B. WHOLESALE SPARE PARTS/ASSEMBLIES - 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 PARA 16B NLT DATE SPECIFIED IN PARAGRAPH 1E(2). REPORT THE QUANTITY INSPECTED BY CONDITION CODE AND THE RESULTING CONDITION CODE. REPORT BY EMAIL OR FAX 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. (TIE BAR 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. (5) DA FORM 2410, COMPONENT REMOVAL AND REPAIR/OVERHAUL RECORD (ONLY IF ROTOR HEAD OR TIE BAR ASSEMBLIES ARE REMOVED/REPLACED). (6) DD FORM 1574/DD FORM 1574-1, SERVICEABLE TAG/LABEL - MATERIEL (COLOR YELLOW). ANNOTATE REMARKS BLOCK WITH "INSPECTED SERVICEABLE IAW CH-47-02-05 (TB 1-1520-240-20-146)." (7) DD FORM 1577-2/DD FORM 1577-3, UNSERVICEABLE (REPARABLE) TAG/LABEL - MATERIEL (COLOR GREEN). ANNOTATE REMARKS BLOCK WITH UNSERVICEABLE IAW CH-47-02-05 (TB 1-1520-240-20-146)." 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 897-2350 EXTENSION 9851 OR (256) 705-9851. EMAIL IS "STEVE.PROSISE@RDEC.REDSTONE.ARMY.MIL". B. LOGISTICAL POC IS MR. BILL OLSON, SFAE-AV-CH-L, DSN 897- 3379 OR (256) 313-3379, FAX IS EXT 4348. EMAIL IS "WILLIAM.OLSON@PEOAVN.REDSTONE.ARMY.MIL". C. WHOLESALE MATERIEL POC (SPARES) IS MIGUEL RODRIGUEZ, AMSAM-MMC-AV-CA, DSN 788-6747 OR (256) 842-6747, FAX IS DSN 897- 1106. EMAIL IS "MIGUEL.RODRIGUEZ@REDSTONE.ARMY.MIL". D. FORMS AND RECORDS POC FOR THIS MESSAGE IS MS. ANN WALDECK, AMSAM-MMC-MA-NM, DSN 746-5564 OR (256) 876-5564, FAX IS DSN 746-4904. EMAIL IS ANN.WALDECK@REDSTONE.ARMY.MIL". E. SAFETY POINTS OF CONTACT ARE - (1) PRIMARY - MR. RANDALL RUSHING (SAIC), AMSAM-SF-A, DSN 897-2092 OR (256) 313-2092, FAX IS DSN 895-2111 OR (256) 313- 2111. EMAIL IS "RANDALL.RUSHING@REDSTONE.ARMY.MIL". (2) ALTERNATE - MR. RUSS PEUSCH, AMSAM-SF-A, DSN 788- 8632 OR (256) 842-8632, FAX IS DSN 897-2111 OR (256) 313-2111. EMAIL 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. FAX IS DSN 897-6630 OR (256) 313-6630. EMAIL IS "RONNIE.SAMMONS@REDSTONE.ARMY.MIL". G. AFTER HOURS CONTACT THE AMCOM OPERATIONS CENTER (AOC) DSN 897-2066/7 OR (256) 313-2066/7.