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TEXT
:UNCLAS
SUBJECT - AVIATION SAFETY ACTION MESSAGE, MAINTENANCE MANDATORY,
RCS CSGLD-1860(R1), ALL H-47 AIRCRAFT, INSPECTION OF FLIGHT AND
UTILITY BOOST HYDRAULIC CONTROL MODULES, CH-47-01-ASAM-08
(TB 1-1520-240-20-138)
                              NOTE
THIS IS AN AVIATION SAFETY ACTION MESSAGE 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
POWER, PRESSURE, AND RETURN CONTROL MODULE ASSEMBLIES TO ENSURE
SHUT-OFF DIAPHRAGM HARDWARE IS INSTALLED IAW CH-47-01-ASAM-08 (TB
1-1520-240-20-138) AT THE NEXT SCHEDULED INSPECTION BUT NLT 50
FLIGHT HOURS FROM THE DTG OF THIS MESSAGE."  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 50 FLIGHT HOURS FROM THE DTG OF
THIS MESSAGE.  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 -
        (1)  AIRCRAFT IN AVUM, AVIM, OR DEPOT LEVEL MAINTENANCE -
COMMANDERS AND FACILITY MANAGERS WILL NOT ISSUE AIRCRAFT UNTIL
THEY ARE IN COMPLIANCE WITH THIS MESSAGE.
        (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) - COMPLY NLT 28
FEBRUARY 2002.
    E.  COMPONENT/PARTS IN STOCK AT ALL LEVELS (DEPOT AND OTHERS)
INCLUDING WAR RESERVES - N/A.
2.  TASK/INSPECTION SUSPENSE DATE - COMPLETE THE INSPECTION IAW
PARAGRAPH 8 AT THE NEXT SCHEDULED INSPECTION BUT NLT 50 FLIGHT
HOURS FROM THE DTG OF THIS MESSAGE.
3.  REPORTING COMPLIANCE SUSPENSE DATE - REPORT COMPLIANCE IAW
PARA 14A(1) NLT 30 AUGUST 2001.
4.  SUMMARY OF PROBLEM -
    A.  A DEFICIENCY REPORT INVESTIGATION IDENTIFIED THAT A POWER
CONTROL MODULE WAS MISSING ITS SHUT-OFF DIAPHRAGM HARDWARE.
    B.  FOR MANPOWER/DOWNTIME AND FUNDING IMPACTS SEE PARA 12.
    C.  THE PURPOSE OF THIS MESSAGE IS TO REQUIRE A ONE TIME
INSPECTION OF ALL H-47 POWER, PRESSURE AND RETURN CONTROL MODULES
TO ENSURE PROPER INSTALLATION OF SHUT-OFF DIAPHRAGM HARDWARE.
5.  END ITEMS TO BE INSPECTED - ALL H-47 AIRCRAFT.
6.  ASSEMBLY COMPONENTS TO BE INSPECTED -
  NOMENCLATURE                      PART NO.
MODULE ASSEMBLY                   145H1201-6 (2 PLCS)
POWER CONTROL F.C. - CH-47D
MODULE ASSEMBLY                   145H1551-4, -5
PRESSURE CONTROL UTILITY - CH-47D
RETURN CONTROL                    145H1601-4
MODULE ASSEMBLY
7.  PARTS TO BE INSPECTED -
  NOMENCLATURE         PART NO.               NSN
SPRING, REMOVAL      AB-3255-12D21     5360-00-968-8403
SCREW, RETAINING     AA-3258-12D9      5305-00-781-4005
DIAPHRAGM, SHUT-OFF  AC-3255-12D7      1650-01-029-5333
8.  INSPECTION PROCEDURES -
    A.  PREPARE AIRCRAFT FOR SAFE GROUND MAINTENANCE.
    B.  FOR THE FLIGHT HYDRAULIC SYSTEM, REMOVE POWER CONTROL
MODULE FILTERS (4 PLACES) PER TASK 7-33 OF REFERENCE 13.B (CH/MH-
47D), AND TASK 7-38 OF REFERENCE 13.C (MH-47E).
        1.  VISUALLY INSPECT FOR SHUT-OFF DIAPHRAGM AND REMOVAL
SPRING HARDWARE. REFERENCE FIGURE 218 OF REFERENCE 13.D (CH/MH-
47D) ITEMS 27, 28 AND 31 AND FIGURE 7-19 OF REFERENCE 13.E (MH-
47E) ITEMS 27, 28 AND 31. A MIRROR TOOL MAY BE REQUIRED TO
INSPECT FOR ITEMS 28 AND 31 (RETAINING SCREW AND SHUT-OFF
DIAPHRAGM).
                             NOTE
            FOR THE CH/MH-47D (REF. 13.D, FIGURE 218),
            THE PART NUMBER IN THE PARTS LIST FOR ITEM
            27 IS INCORRECT. THE PART NUMBER SHOULD BE
            AB-3255-12D21 INSTEAD OF AA-3255-12D21.
                             NOTE
            FOR THE CH/MH-47D, DISREGARD THE REFERENCE
            TO FIGURES 223 AND 227 IN THE LISTING FOR
            ITEM NUMBER 24.
                             NOTE
            FOR THE MH-47E, DISREGARD THE REFERENCE TO
            FIGURES 7-24 AND 7-28 IN THE LISTING FOR
            ITEM NUMBER 24.
                             NOTE
            WITH THE EXCEPTION NOTED IN PARA 12D
            CONCERNING PREFORMED PACKING, THESE PARTS
            ARE IDENTICAL FOR EACH FLIGHT HYDRAULIC SYSTEM
            MODULE INSTALLATION.
        2.  IF SHUT-OFF DIAPHRAGM HARDWARE WAS INSTALLED,
REINSTALL FILTER IAW TASK 7-34 OF REFERENCE 13.B (CH/MH-47D) AND
TASK 7-39 OF REFERENCE 13.C (MH-47E).
    C.  FOR THE UTILITY HYDRAULIC SYSTEM PRESSURE CONTROL MODULE,
REMOVE FILTER PER TASK 7-156 OF REFERENCE 13.B (CH/MH-47D), AND
TASK 7-181 OF REFERENCE 13.C (MH-47E).
        1.  VISUALLY INSPECT FOR SHUT-OFF DIAPHRAGM AND REMOVAL
SPRING HARDWARE. REFERENCE FIGURE 223 OF REFERENCE 13.D (CH/MH-
47D), ITEMS 37, 38 AND 41 AND REFERENCE FIGURE 7-24 OF REFERENCE
13.E (MH-47E), ITEMS 37, 38 AND 41. A MIRROR TOOL MAY BE REQUIRED
TO INSPECT FOR ITEMS 38 AND 41 (RETAINING SCREW AND SHUT-OFF
DIAPHRAGM).
                             NOTE
            FOR THE CH/MH-47D(REF. 13.D, FIGURE 223),
            THE PART NUMBER IN THE PARTS LIST FOR ITEM 37
            IS INCORRECT. THE PART NUMBER SHOULD BE
            AB-3255-12D21 INSTEAD OF AA-3255-12D21.
        2.  IF SHUT-OFF DIAPHRAGM HARDWARE WAS INSTALLED,
REINSTALL FILTER IAW TASK 7-157 OF REFERENCE 13.B (CH/MH-47D) AND
TASK 7-182 OF REFERENCE 13.C (MH-47E).
    D.  FOR THE UTILITY HYDRAULIC SYSTEM RETURN CONTROL MODULE,
REMOVE FILTER PER TASK 7-194 OF REFERENCE 13.B (CH/MH-47D), AND
TASK 7-224 OF REFERENCE 13.C (MH-47E).
        1.  VISUALLY INSPECT FOR SHUT-OFF DIAPHRAGM AND REMOVAL
SPRING HARDWARE.  REFERENCE FIGURE 227 OF REFERENCE 13.D (CH/MH-
47D), ITEMS 31, 32 AND 35 AND REFERENCE FIGURE 7-28 OF REFERENCE
13.E (MH-47E), ITEMS 31, 32 AND 35. A MIRROR TOOL MAY BE REQUIRED
TO INSPECT FOR ITEMS 32 AND 35 (RETAINING SCREW AND SHUT-OFF
DIAPHRAGM).
                             NOTE
            FOR THE CH/MH-47D (REF.13.D, FIGURE 227),
            THE PART NUMBER IN THE PARTS LIST FOR ITEM
            31 IS INCORRECT. THE PART NUMBER SHOULD BE
            AB-3255-12D21 INSTEAD OF AA-3255-12D21.
                             NOTE
            WITH THE EXCEPTION NOTED IN PARA 12D
            CONCERNING PREFORMED PACKING, THESE PARTS
            ARE IDENTICAL FOR EACH UTILITY HYDRAULIC SYSTEM
            MODULE INSTALLATION.
        2.  IF SHUT-OFF DIAPHRAGM HARDWARE WAS INSTALLED,
REINSTALL FILTER IAW TASK 7-195 OF REFERENCE 13.B (CH/MH-47D) AND
TASK 7-225 OF REFERENCE 13.C (MH-47E).
    E.  IF SHUT-OFF DIAPHRAGM HARDWARE IS INSTALLED ON ALL FOUR
MODULES, (SIX FILTERS) THE RED HORIZONTAL DASH //-// MAY BE
CLEARED.
    F.  AFTER INSPECTION IS COMPLETE AND IT IS DISCOVERED THAT
SHUT-OFF DIAPHRAGM HARDWARE IS NOT INSTALLED ON ONE OR MORE OF
THE FOUR MODULES (SIX FILTERS), CLEAR THE ORIGINAL RED DASH //-//
ENTRY AND ENTER THE FOLLOWING RED //X// ENTRY ON THE DA FORM
2408-13-1: "XXXXX CONTROL MODULE ASSEMBLY DIAPHRAGM HARDWARE
MISSING."  PROCEED TO PARAGRAPH 9 FOR CORRECTION PROCEDURES.
9.  CORRECTION PROCEDURES -
                             NOTE
            CONTACT THE LOGISTICS POC LISTED AT PARA 16B
            FOR INSTRUCTIONS TO MAKE A SPECIAL TOOL TO
            SIMPLIFY INSTALLATION AND ILLUSTRATED INSTALLATION
            INSTRUCTIONS.
     A.  FOR FLIGHT HYDRAULIC SYSTEM MODULE NUMBERS 1 AND/OR 2,
IF THE DIAPHRAGM HARDWARE IS MISSING, REQUISITION AND INSTALL
DIAPHRAGM HARDWARE LISTED IN PARAGRAPH 12D ALONG WITH THE FILTER
IAW TASK 7-34 OF REFERENCE 13.B (CH/MH-47D) AND TASK 7-39 OF
REFERENCE 13.C (MH-47E). REFERENCE FIGURE 218 OF REFERENCE 13.D
(CH/MH-47D) AND FIGURE 7-19 OF REFERENCE 13.E (MH-47E).
     B.  FOR THE UTILITY HYDRAULIC SYSTEM PRESSURE CONTROL
MODULE, IF THE DIAPHRAGM HARDWARE IS MISSING, REQUISITION AND
INSTALL DIAPHRAGM HARDWARE LISTED IN PARAGRAPH 12D ALONG WITH THE
FILTER IAW TASK 7-157 OF REFERENCE 13.B (CH/MH-47D) AND TASK 7-
182 OF REFERENCE 13.C (MH-47E). REFERENCE FIGURE 223 OF REFERENCE
13.D (CH/MH-47D) AND FIGURE 7-24 OF REFERENCE 13.E (MH-47E).
     C.  FOR THE UTILITY HYDRAULIC SYSTEM RETURN CONTROL MODULE,
IF THE DIAPHRAGM HARDWARE IS MISSING, REQUISITION AND INSTALL
DIAPHRAGM HARDWARE LISTED IN PARAGRAPH 12D ALONG WITH THE FILTER
IAW TASK 7-195 OF REFERENCE 13.B (CH/MH-47D) AND TASK 7-225 OF
REFERENCE 13.C (MH-47E). REFERENCE FIGURE 227 OF REFERENCE 13.D
(CH/MH-47D) AND FIGURE 7-28 OF REFERENCE 13.E (MH-47E).
     D. ONCE SHUT-OFF DIAPHRAGM HARDWARE IS INSTALLED, TAKE A
SPECIAL HYDRAULIC FLUID SAMPLE AND TURN IT INTO THE SERVICING
AOAP LABORATORY.  THE AIRCRAFT RED //X// STATUS MAY BE CLEARED
UPON VERIFICATION OF A GOOD SAMPLE BY THE AOAP LABORATORY.
10.  SUPPLY/PARTS AND DISPOSITION -
     A.  ITEMS CITED IN PARAGRAPH 12D MAY BE REQUIRED TO REPLACE
MISSING ITEMS.
     B.  REQUISITIONING INSTRUCTIONS - REQUISITION REPLACEMENT
PARTS USING NORMAL SUPPLY PROCEDURES.  ALL REQUISITIONS SHALL USE
PROJECT CODE (CC 57-59) "X0X", "X-RAY-ZERO-X-RAY".
                              NOTE
            PROJECT CODE "X0X", "X-RAY-ZERO-X-RAY"
            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 - N/A.
     E.  DISPOSITION OF HAZARDOUS MATERIAL - N/A.
11.  SPECIAL TOOLS AND FIXTURES REQUIRED - DRAWINGS TO FABRICATE
SPECIAL TOOLS SHALL BE OBTAINED FROM THE LOGISTICAL POINT OF
CONTACT LISTED IN PARAGRAPH 16.B.
12.  APPLICATION -
     A.  CATEGORY OF MAINTENANCE - AVUM: AIRCRAFT DOWNTIME WILL
BE CHARGED TO AVUM.  REPORT AIRCRAFT NON-MISSION CAPABLE
MAINTENANCE (NMCM) WHILE UNDERGOING INSPECTION AND CORRECTION IAW
THIS MESSAGE.
     B.  ESTIMATED TIME REQUIRED -
         (1)  TIME TO COMPLETE INSPECTION
              (A)  TOTAL OF 6 MAN-HOURS USING 1 PERSON.
              (B)  TOTAL OF 6 HOURS DOWNTIME FOR ONE END ITEM.
     C.  TIME FOR REPAIR/REPLACEMENT -
         (A)  TOTAL OF 12 MAN-HOURS USING 1 PERSON.
         (B)  TOTAL OF 12 HOURS DOWNTIME FOR ONE END ITEM
     D.  ESTIMATED COST IMPACT TO THE FIELD -
NOMENCLATURE      PART NO./NSN      QTY    COST EA. TOTAL $
FILTER BODY, FL   AA-A620-1D2A       6     505.41   3032.46
                    1650-01-116-4321
FILTER ELEMENT    AC-A620F-5         6     100.82    604.92
                    1650-01-114-6385
SPRING, REMOVAL   AB-3255-12D21      6      17.92    107.52
                    5360-00-968-8403
SCREW, RETAINING  AA-3258-12D9       6       4.47     26.82
                    5305-00-781-4005
BUSHING           AB-3255-12D13      6      43.73    262.38
                    5365-01-029-5334
PACKING, PREFORMED * M83461/1-024    6        .17      1.02
                    5331-01-107-9249
DIAPHRAGM, SHUTOFF AC-3255-12D7      6     140.33    841.98
                    1650-01-029-5333
PACKING, PREFORMED  MS28775-017      6        .08      0.48
                    5331-00-618-1920
SPRING             AA-3255-12D8      6      13.20     79.20
                    5360-00-968-8404
RETAINER           MS28774-132       6        .33      1.98
                    5330-00-848-9128
PACKING, PREFORMED ** M83461/1-132   6        .23      1.38
                    5331-01-146-4563
                                 COST PER MODULE = $4960.15
  * M83461/1-024 AND MS28775-024 PREFORMED PACKING ARE
INTERCHANGEABLE.
  **M83461/1-132 AND MS28775-132 PREFORMED PACKING ARE
INTERCHANGEABLE.
     E.  TB/MWOS TO BE APPLIED PRIOR TO OR CONCURRENTLY WITH THIS
INSPECTION - N/A.
     F.  PUBLICATIONS WHICH REQUIRE CHANGE AS A RESULT OF THIS
INSPECTION - REFERENCES 13.B,C,D,E 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.
13.  REFERENCES -
     A.  DA PAM 738-751, 15 MAR 99.
     B.  TM 55-1520-240-23
     C.  TM 1-1520-252-23
     D.  TM 55-1520-240-23P
     E.  TM 1-1520-252-23P
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 AFFECTED
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 - N/A.
     C.  RETAIL SPARE PARTS/ASSEMBLIES - N/A.
     D.  REPORTING MESSAGE RECEIPT (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.
15.  WEIGHT AND BALANCE - N/A.
16.  POINTS OF CONTACT-
     A.  TECHNICAL POINT OF CONTACT FOR THIS MESSAGE IS MR. MIKE
MOORE, AMSAM-RD-AE-I-P-C, DSN 897-3359 OR (256) 313-3359, DATAFAX
IS EXT. 4348.  E-MAIL IS MIKE.MOORE@PEOAVN.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 POINT OF CONTACT (SPARES) IS MR. PAUL
HUGHES, DSCR-XBD, DSN 695-6328 OR (804) 279-6328, DATAFAX IS DSN
695-5695 OR 804)279-5695.  E-MAIL IS "PHUGHES@DSCR.DLA.MIL".
     D.  FORMS AND RECORDS POINT OF CONTACT FOR THIS MESSAGE IS
MS. ANN WALDECK, AMSAM-MMC-RE-FF DSN 746-5564 OR (256) 876-5564,
DATAFAX IS DSN 746-4904.  E-MAIL IS
"WALDECK-AB@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 -
         (1)  PRIMARY - MR. RONNIE W. SAMMONS, AMSAM-SA-CS-NF,
DSN 897-6656 OR (256) 313-6656.  DATAFAX IS DSN 897-6630 OR (256)
313-6630.  EMAIL IS "RONNIE.SAMMONS@REDSTONE.ARMY.MIL".
         (2)  ALTERNATE - MR. PAUL W. TARR, AMSAM-SA-CS-NF, DSN
897-6861 OR (256) 313-6861.  DATAFAX IS DSN 897-6630 OR (256)
313-6630.  EMAIL IS E-MAIL "TARRPW@REDSTONE.ARMY.MIL".
     G.  AFTER HOURS CONTACT THE AMCOM COMMAND OPERATIONS CENTER
(COC) DSN 897-2066/7 OR (256) 313-2066/7.