01 17 1315Z MAR 97 PP UUUU AA ZYUW FROM :CDRATCOM ST LOUIS MO//AMSAT-R-X// TO :AIG 8881 :AIG 9004 :AIG 8708 :AIG 9042 :AIG 7471 :AIG 12124 :USMILGP BUENOS AIRES AR//ARMY AND AF SEC// :DEFAIR MATERIAL CANBERRA AS//DAAP-AF// :CDRUSARDSG CANBERRA 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// :CDR160TH SOAR FT CAMPBELL KY//AOAV-SI// :CDRBGAD RICHMOND KY//SIOBG-GC// :USDAO RABAT MO//AF// :ODC THE HAGUE NL//AVIATION SAFETY// :RNLAF MATERIAL :RNLAF OPERATIONS :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 ARMY FMS BANGKOK TH//BANGSUE DEPOT// :ROYAL THAI AF 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// XMT :USDAO DHAKA BG :USDAO RANGOON BM :USCINCPAC REP PHNOM PENH CB :USDAO COLOMBO CE :USDAO SUVA FJ :OMADP JAKARTA ID :DSA NEW DELHI IN :AMEMBASSY ANTANANARIVO MA :AMEMBASSY PORT LOUIS :SAO KUALA LUMPUR MY :AMEMBASSY KATHMANDU NP//POL-MIL// ACCT : TEXT :UNCLAS SUBJECT: AVIATION SAFETY ACTION MESSAGE (ASAM), MAINTENANCE MANDATORY, RCS CSGLD-1860(R1), ALL CH-47D, MH-47D, AND MH-47E AIRCRAFT, ONE TIME VISUAL INSPECTION AND REPLACEMENT OF CERTAIN P/N 4C3074 CRISSAIR, INC. CHECK VALVE INSTALLED IN POWER CONTROL MODULE ASSEMBLIES IN THE PORT MARKED "FLT CONT PUMP" ONLY (CH-47-97-ASAM-04) (TB 1-1520-240-20-96) NOTE THIS IS AN AVIATION SAFETY ACTION MESSAGE (ASAM) ISSUED PER AR 95-3, CHAPTER 5 REVISION VIA MESSAGE, HQ AVSCOM, AMSAV-XSOF, 181900Z SEP 90, SUBJECT: CHANGE TO AR 95-3, CHAPTER 5, SAFETY OF FLIGHT MESSAGES. THIS ASAM 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 THIS MESSAGE. ACTION ADDRESSEES WILL IMMEDIATELY VERIFY THIS TRANSMISSION TO COMMANDER, ATCOM, ATTN: AMSAT-R-X (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 RED HORIZONTAL DASH //-//. THE RED HORIZONTAL DASH //-// MAY BE CLEARED WHEN THE INSPECTION OF PARA 8 BELOW IS COMPLETED. THE AFFECTED AIRCRAFT SHALL 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//. NINTY DAYS ORDERR, SHIP, AND REPLACEMENT TIME IS ALLOWED ONCE DEFECTIVE CHECK VALVES ARE FOUND. PENDING AVAILABLITY, DEPOTS WILL REPLACE DEFECTIVE CHECK VALVES PRIOR TO UNIT ACCEPTANCE. B. AIRCRAFT IN DEPOT MAINTENANCE - SAME AS PARA 1A. C. AIRCRAFT UNDERGOING MAINTENANCE - SAME AS PARA 1A. D. AIRCRAFT IN TRANSIT - (1) SURFACE/AIR SHIPMENT - SAME AS PARA 1A. (2) FERRY STATUS - SAME AS PARA 1A. E. MAINTENANCE TRAINERS (CATEGORY A, B) - SAME AS PARA 1A. F. COMPONENT/PARTS IN STOCK AT ALL LEVELS (DEPOT AND OTHERS) INCLUDING WAR RESERVES - UPON RECEIPT OF THIS ASAM THE MATERIEL CONDITION TAGS OF ALL ITEMS LISTED IN PARA 6 AND 7 BELOW IN ALL CONDITION CODES SHALL BE ANNOTATED TO READ ASAM CH-47-97-ASAM- 04, ONE TIME VISUAL INSPECTION AND REPLACEMENT OF CERTAIN P/N 4C3074 CRISSAIR CHECK VALVE INSTALLED IN THE POWER CONTROL MODULE ASSEMBLIES IN THE PORT MARKED "FLT CONT PUMP" ONLY MUST BE COMPLIED WITH PRIOR TO ISSUE.. (1) WHOLESALE STOCK - UPON RECEIPT OF THIS ASAM, DEPOT COMMANDERS SHALL ENSURE INSPECTION OF ALL ITEMS LISTED IN PARA 6 AND 7 BELOW LOCATED IN ALL WHOLESALE DEPOTS INCLUDING ALL SATELLITE WHOLESALE DEPOTS AND WAR RESERVE DEPOTS. UPON RECEIPT OF THIS ASAM DEPOT COMMANDERS AND OTHERS MAINTAINING WHOLESALE STOCK SHALL ENSURE THAT SERVICEABLE MATERIEL (CONDITION CODES //A//, //B//, AND //C//) IS PLACED IN CONDITION CODE //J// AND TAGGED WITH A SUSPENDED TAG/LABEL - DD FORM 1575/1575-1(BROWN COLOR). THE AUTHORITY BLOCK MUST REFERENCE INSPECTION REQUIRED PER THIS MESSAGE (TB 1-1520-240-20-96). REPORT COMPLIANCE WITH THIS ASAM IN ACCORDANCE WITH PARA 14D(1) BELOW. PACKAGES DATED AFTER 1 MAY 1991 DO NOT NEED TO BE OPENED. THEY ARE ACCEPTABLE. (2) RETAIL STOCK - UPON RECEIPT OF THIS ASAM COMMANDERS AND OTHERS MAINTAINING RETAIL STOCK OF ITEMS LISTED IN PARA 6 AND 7 BELOW SHALL CONTACT THEIR SUPPORT AVIATION ORGANIZATION TO PERFORM THE INSPECTION REQUIRED BY PARA 8 BELOW AND TO PERFORM THE CORRECTION PROCEDURES OF PARA 9 BELOW ON DISCREPANT MATERIEL. ALL ITEMS LISTED IN PARA 6 AND 7 BELOW SHALL BE IMMEDIATELY PLACED IN CONDITION CODE //D// AND RETAGGED WITH A TEST/MODIFICATION TAG/LABEL - DD FORM 1576/1576-1 (BLUE COLOR). THE AUTHORITY BLOCK MUST REFERENCE INSPECTION REQUIRED PER THIS MESSAGE (TB 1-1520-240-20-96). ITEMS IDENTIFIED AS SERVICEABLE IAW PARA 8 BELOW SHALL BE RETAGGED WITH A SERVICEABLE TAG/LABEL - DD FORM 1574/1574-1 (YELLOW COLOR). INDICATE COMPLIANCE WITH THIS MESSAGE (TB 1-1520-240-20-96) IN THE REMARKS BLOCK. ITEMS IDENTIFIED AS DISCREPANT IAW PARA 8 BELOW SHALL BE RETAGGED WITH UNSERVICEABLE (REPARABLE) TAG/LABEL - 1577-2/1577-3 (GREEN COLOR). ANNOTATE REMARKS BLOCK TO INDICATE THAT THE ITEM IS UNSERVICEABLE IAW THIS MESSAGE (TB 1-1520-240-20-96) DISCREPANT ITEMS SHALL BE CORRECTED IAW PARA 9 BELOW. REPORT COMPLIANCE WITH THIS ASAM IN ACCORDANCE WITH PARA 14D(2) BELOW. PACKAGES DATED AFTER 1 MAY 1991 DO NOT NEED TO OPENED. THEY ARE ACCEPTABLE G. COMPONENTS/PARTS IN WORK - ALL ITEMS LISTED IN PARA 6 AND 7 BELOW SHALL NOT BE ISSUED UNTIL COMPLIANCE WITH THIS ASAM HAS BEEN COMPLETED. 2. TASK/INSPECTION SUSPENSE DATE - WITHIN 10 HOURS/14 DAYS. 3. REPORTING COMPLIANCE SUSPENSE DATE - NO LATER THAN 3 APR 1997 PARA 14A OF THIS MESSAGE. 4. SUMMARY OF PROBLEM - A. RECENT FIELD REPORTS REVEALED THAT CERTAIN P/N 4C3074 HYDRAULIC CHECK VALVE, MANUFACTURED BY CRISSAIR, INC. (CAGE 99240), IN POWER CONTROL MODULES P/N AE-A620-14 (145H1201-5) OR P/N AE-A620-15 (145H1201-6) IS BEING FOUND WITH A RIVET MISSING FROM THE VALVE'S POPPET. FAILURE OF THE VALVE DURING AUXILIARY POWER UNIT (APU) OR EXTERNAL GROUND POWER UNIT (GPU) OPERATION COULD CAUSE THE ROTORS TO TURN IN THE OPPOSITE DIRECTION OF NORMAL ROTATION DURING OPERATION OF THE NO. 1 OR NO. 2 POWER TRANSFER UNITS (PTU). THE MISSING RIVET CAN ENTER THE HYDRAULIC SYSTEM CAUSING DAMAGE TO THE FLIGHT CONTROL PUMP WHEN THE POWER SOURCE TO THE HYDRAULIC SYSTEM IS EITHER THE APU OR AN EXTERNAL GPU. B. THE FAILURE OCCURS WHEN THE DRIVE SYSTEM IS SHUT DOWN AND THE FLIGHT CONTROL SYSTEMS ARE BEING POWERED BY EITHER THE APU THROUGH THE PTU PUMP OR A GROUND POWER UNIT. THEREFORE, THE FAILURE POSES NO SAFETY OF FLIGHT CONDITION. AFTER COMPLIANCE WITH THIS ASAM, DO NOT CONTROL SUBSTITUTE/CANNIBALIZE FROM THE MODULES IDENTIFIED IN PARA 8C. C. TO ELIMINATE THE PROBLEM, THE VALVE HAS BEEN REDESIGNED TO REPLACE THE THREE-PIECE ASSEMBLY (RIVET, WASHER, AND POPPET) WITH A ONE-PIECE POPPET. THERE ARE TWO LOCATIONS WHERE THE POWER CONTROL MODULE P/N AE-A620-14 (145H1201-5) OR P/N AE-A620-15 (145H1201-6) IS USED ON THE AIRCRAFT. EACH POWER CONTROL MODULE HAS THREE CHECK VALVES. HOWEVER, ONLY THE CHECK VALVE THAT IS INSTALLED INTO THE PORT MARKED "FLT CONT PUMP" CAN CAUSE THE ABOVE PROBLEM. IF ANY OF THE OTHER FOUR(4) CHECK VALVES FAIL, THE RIVET BECOMES TRAPPED OR LODGED IN THE HYDRAULIC SYSTEM WITHOUT CAUSING ANY DAMAGE OR FAILURE OF OTHER COMPONENTS. D. FOR MANPOWER/DOWNTIME AND FUNDING IMPACTS SEE PARA 12. E. THE PURPOSE OF THIS MESSAGE IS TO REPLACE THE OLD THREE- PIECE CONFIGURATION OF THE 4C3074 CRISSAIR CHECK VALVE WITH THE CURRENT IMPROVED ONE-PIECE DESIGN, REVISION D. P/N 4C3074, REVISION D, CAN BE IDENTIFIED BY FOUR(4) SHALLOW FLAT BOTTOM HOLES THAT ARE FILLED WITH WHITE PAINT. THE HOLES ARE EQUALLY SPACED 90 DEGREES APART AROUND THE BODY ASSEMBLY. ALSO, "REV D" IS MARKED ON THE BODY ASSEMBLY. THE DESIGNS PRIOR TO REVISION D DO NOT HAVE FOUR(4) SHALLOW FLAT BOTTOM HOLES FILLED WITH WHITE PAINT ON THE BODY ASSEMBLY, OR THE "REV D" MARKING. 5. END ITEMS TO BE INSPECTED - ALL CH-47D, MH-47D, AND MH-47E AIRCRAFT. 6. ASSEMBLY COMPONENTS TO BE INSPECTED - NOMENCLATURE PART NO. NSN MODULE ASSEMBLY, 145H1201-5 1650-01-145-8575 POWER CONTROL (AE-A620-14) MODULE ASSEMBLY, 145H1201-6 N/A POWER CONTROL (AE-A620-15) 7. PART TO BE INSPECTED - NOMENCLATURE PART NO. NSN CHECK VALVE 4C3074 4820-01-118-3009 8. INSPECTION PROCEDURES - A. PREPARE AIRCRAFT FOR SAFE GROUND MAINTENANCE. B. LOCATE THE NO.1 POWER CONTROL MODULE ASSEMBLY (REFER TO TM 55-1520-240-23P, FIGURE 206, ITEM 26 OR TM 1-1520-252-23P, FIGURE 7-7, ITEM 28) AND NO. 2 POWER CONTROL MODULE ASSEMBLY (REFER TO TM 55-1520-240-23P, FIGURE 215, INDEX 19 OR TM 1-1520-252-23P, FIGURE 7-16, ITEM 19). C. IF NECESSARY REMOVE THE CRISSAIR, INC. P/N 4C3074 CHECK VALVES FROM POWER CONTROL MODULE ASSEMBLIES FROM THE PORTS MARKED "FLT CONT PUMP" ONLY (REFER TO TM 55-1520-240-23, TASK 7-54.1 OR TM 1-1520-252-23, TASK 7-66). NOTE ONLY THE CRISSAIR, INC. P/N 4C3074 CHECK VALVE INSTALLED IN THE PORT MARKED "FLT CONT PUMP" OF THE POWER CONTROL MODULE ASSEMBLIES CITED IN PARA 6 ABOVE NEED TO BE REPLACED. THE OTHER TWO VALVES IN THE ASSEMBLIES ARE "ON CONDITION" REPLACEMENT ITEMS. NOTE THE CRISSAIR, INC. P/N 4C3074 CHECK VALVES INSTALLED IN THE FOLLOWING COMPONENTS DO NOT NEED TO BE REPLACED AS THEY ARE "ON CONDITION" REPLACEMENT ITEMS: NOMENCLATURE PART NUMBER MODULE HOUSING ASSEMBLY 145HS551-4 (AE-A620-33D1A) MODULE HOUSING ASSEMBLY 145HS601-4 (AE-A620-23D1A) D. VISUALLY INSPECT THE P/N 4C3074 CHECK VALVES FOR FOUR(4) SHALLOW FLAT BOTTOM HOLES FILLED WITH WHITE PAINT. THE HOLES ARE EQUALLY SPACED 90 DEGREES APART AROUND THE VALVE BASE. ALSO, THE MARKING "REV D" IS MARKED ON THE BODY ASSEMBLY. E. IF THERE ARE FOUR(4) HOLES FILLED WITH WHITE PAINT AND/OR "REV D" IS MARKED ON THE VALVE BASE, THE VALVE IS THE IMPROVED REVISION D ONE-PIECE DESIGN AND THE INSPECTION IS COMPLETE. REINSTALL THE CHECK VALVES (REFER TO TM 55-1520-240-23, TASK 7-54.2 OR TM 1-1520-252-23, TASK 7-67) AND RECORD AND REPORT COMPLIANCE WITH THIS ASAM IN ACCORDANCE WITH PARA 14 BELOW. F. IF THE VALVE IS NOT THE IMPROVED REVISION D ONE-PIECE DESIGN AS DESCRIBED ABOVE, PROCEED TO PARA 9. 9. CORRECTION PROCEDURES - A. REQUISITION REPLACEMENT P/N 4C3074, REVISION D, CHECK VALVES. B. INSTALL CHECK VALVES IN ACCORDANCE WITH THE INSTRUCTIONS IN TM 55-1520-240-23, TASK 7-54.2 OR TM 1-1520-252-23, TASK 7-67. C. REPORT COMPLIANCE WITH THE ABOVE IN ACCORDANCE WITH PARA 14B BELOW. 10. SUPPLY/PARTS AND DISPOSITION - A. PARTS REQUIRED - ITEMS CITED IN PARA 7 ABOVE MAY BE REQUIRED TO COMPLY WITH THIS ASAM. B. REQUISITIONING INSTRUCTIONS - REQUISITION REPLACEMENT PARTS THROUGH NORMAL SUPPLY CHANNELS USING NORMAL SUPPLY PROCEDURES. ALL REQUISITIONS SHALL USE PROJECT CODE XDC PER THIS MESSAGE. NOTE PROJECT CODE XDC IS REQUIRED TO TRACK AND ESTABLISH A DATA BASE OF STOCK FUND EXPENDITURES INCURRED BY THE FIELD AS A RESULT OF SOF/ASAM ACTIONS. C. BULK AND CONSUMABLE MATERIALS - N/A. D. DISPOSITION - MULTILATE IAW TM 1-1500-328-23. E. DISPOSITION OF HAZARDOUS MATERIAL - N/A. 11. SPECIAL TOOLS, JIGS AND FIXTURES REQUIRED - N/A. 12. APPLICATION - A. CATEGORY OF MAINTENANCE - AVIM. AIRCRAFT DOWNTIME WILL BE CHARGED TO AVIM. B. TIME REQUIRED - (1) INSPECTION: 1 MANHOUR USING 1 PERSON. (2) REPLACEMENT: 6 MANHOURS USING 2 PERSONS. (3) TOTAL OF 3 HOURS DOWNTIME FOR ONE END ITEM. C. ESTIMATED COST IMPACT OF STOCK FUND ITEMS TO THE FIELD - $ 123.05 FOR CHECK VALVE P/N 4C3074 NSN 4820-01-118-3009. 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 55-1520-240-23-6. 13. REFERENCES - A. TM 55-1520-240-23-6. B. TM 55-1520-240-23P. C. TM 1-1520-252-23. D. TM 1-1520-252-23P. 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, DATA FAX OR E-MAIL TO COMMANDER, ATCOM, ATTN: AMSAT-R-X (SOF COMPLIANCE OFFICER), PER AR 95-3. DATA FAX NUMBER IS DSN 693-2064 OR COMMERCIAL 314/263-2064. E-MAIL ADDRESS IS "AMSATRXS (AT SIGN) EMH4.STL.ARMY.MIL". THE REPORT WILL CITE THIS ASAM 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) - INSPECTION AND REPORTS WILL BE COMPLETED NO LATER THAN 7 DAYS AFTER TASK/INSPECTION SUSPENSE DATE. UNITS HAVE 90 DAYS FROM TIME SUSPECT CHECK VALVES ARE LOCATED ON AIRCRAFT TO REPLACE THEM. THIS ALLOWS ORDER, SHIP AND REPLACEMENT TIME. C. REPORTING COMPLIANCE SUSPENSE DATE (SPARES) - (1) MATERIEL IN RETAIL STORAGE - REPORT RECEIPT OF THIS MESSAGE BY E-MAIL OR DATA FAX TO THE LOGISTICAL POINT OF CONTACT LISTED IN PARAGRAPH 16B WITHIN 5 WORKING DAYS FROM THE DATE OF THIS MESSAGE. (2) MATERIEL IN WHOLESALE DEPOT STORAGE - REPORT RECEIPT OF THIS MESSAGE BY E-MAIL OR DATA FAX TO THE WHOLESALE MATERIEL (SPARES) POINT OF CONTACT LISTED IN PARAGRAPH 16C WITHIN 5 WORKING DAYS FROM THE DATE OF THIS MESSAGE. D. TASK/INSPECTION REPORTING SUSPENSE DATE (SPARES) - (1). MATERIAL IN WHOLESALE DEPOT STORAGE - REPORT COMPLIANCE WITH THIS ASAM TO THE WHOLESALE MATERIEL POINT OF CONTACT (SPARES) LISTED IN PARAGRAPH 16C WITHIN 5 WORKING DAYS FROM THE DATE OF THIS MESSAGE. IF REQUIRED PROVIDE AN ESTIMATE OF THE COST REIMBURSABLE FUNDING REQUIRED TO MOVE THE ITEMS LISTED IN PARA 6 AND 7 ABOVE TO A WORK AREA, UNPACK THE MATERIEL, REPACK THE MATERIEL AFTER INSPECTION BY ATCOM INSPECTORS, AND TO RETURN THE MATERIEL TO STORAGE. REPORT THE QUANTITY, BY ORIGINAL SERVICEABLE CONDITION CODE, OF ALL MATERIAL PLACED IN CONDITION CODE //J//. REPORT BY E-MAIL OR DATA FAX AND PROVIDE LOCAL POINT OF CONTACT. (2) MATERIAL IN RETAIL STORAGE - REPORT COMPLIANCE WITH THIS ASAM BY E-MAIL OR DATA FAX AND PROVIDE LOCAL POINT OF CONTACT TO THE LOGISTICAL POINT OF CONTACT IN PARAGRAPH 16B WITHIN 5 WORKING DAYS FROM THE DATE OF THIS MESSAGE. REPORT THE QUANTITY INSPECTED BY CONDITION CODE, AND THE RESULTING CONDITION CODE. REPORT THE QUANTITY OF ALL MATERIEL REQUIRING MUTILATION. PLACE THESE ITEMS IN CONDITION CODE //D// AND PROVIDE COPIES OF SHIPPING DOCUMENTS TO WHOLESALE MATERIEL POINT OF CONTACT LISTED IN PARAGRAPH 16C. E. THE FOLLOWING FORMS ARE APPLICABLE AND ARE TO BE COMPLETED IN ACCORDANCE WITH DA PAM 738-751, 15 JUN 92 - (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. 15. WEIGHT AND BALANCE - N/A. 16. POINTS OF CONTACT - A. TECHNICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. ROBERT A. LAWYER, AMSAT-R-ECC, DSN 693-3820 OR COMMERCIAL 314/263-3820, AND FAX IS DSN 693-1485 OR COMMERCIAL 314/263-1485. B. LOGISTICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. NORM HUSTON, AMCPM-CH-L, DSN 693-1415 OR COMMERCIAL 314/263-1415, AND FAX IS DSN 693-1485 OR COMMERCIAL 314/263-1485. C. WHOLESALE MATERIEL POINT OF CONTACT (SPARES) FOR THIS MESSAGE IS MR. HAL BARNES, AMSAT-I-SACA, DSN 693-6031 OR COMMERCIAL 314/263-6031, AND FAX IS DSN 693-6022 OR COMMERCIAL 314/263-6022. D. FORMS AND RECORDS POINT OF CONTACT FOR THIS MESSAGE IS MS. ANN WALDECK, AMSAT-I-MDM, DSN 490-2318 OR COMMERCIAL 314/260- 2318. E. SAFETY POINT OF CONTACT FOR THIS MESSAGE IS MR. JIM WILKINS, AMSAT-R-X, DSN 693-2258 OR COMMERCIAL 314/263-2258. F. FOREIGN MILITARY SALES (FMS) RECIPIENTS REQUIRING CLARIFICATION OF ACTION ADVISED BY THIS ASAM SHOULD CONTACT CW5 JAY NANCE OR MR. RON VAN REES, AMSAT-D-S, DSN 693-7844/3216 OR COMMERCIAL 314/263-7844/3216. G. AFTER HOURS CONTACT ATCOM COMMAND OPERATIONS CENTER (COC), DSN 693-2066/7 OR COMMERCIAL 314/263-2066/7. .............................................................................................................................................................................................................................................................................................................................................................................................................................................................................