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:CDRUSARDSG CANBERRA AS//AMXIP-AS//
:ARGENTINE AIR ATTACHE FMS WASHINGTON DC
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:CDRBGAD RICHMOND KY//SIOBG-GC//
:USDAO RABAT MO//AF//
:ODC THE HAGUE NL//AVIATION SAFETY//
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:CDRUSASAC NEW CUMBERLAND PA//AMSAC-SALO-UK//
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:SAO SINGAPORE SN//AVIATION SAFETY//
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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.
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