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Safety of Flight CH-47-02-04 |
UNCLASSIFIED
MSG DTG 071545Z FEB 02
FROM CDRAMCOM, REDSTONE ARSENAL, AL //AMSAM-SF-A//
SUBJECT - SAFETY OF FLIGHT TECHNICAL, RCS CSGLD-1860(R1), H-47,
INSPECTION OF FWD PIVOTING ACTUATOR TO SWASHPLATE ATTACHMENT
HARDWARE FOR PROPER INSTALLATION, CH-47-02-04 (TB 1-1520-240-20-
145).
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/6-14A, 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 ENTRY ON THE DA FORM 2408-13-1. ENTER A RED HORIZONTAL
DASH //-// STATUS SYMBOL WITH THE FOLLOWING STATEMENT: "INSPECT
THE FORWARD PIVOTING ACTUATOR UPPER ATTACHMENT BEARING IAW CH-47-
02-04 (TB 1-1520-240-20 -145) PRIOR TO NEXT FLIGHT. CLEAR THE
RED HORIZONTAL DASH //-// ENTRY WHEN THE PROCEDURES IAW PARA 8
AND 9 ARE COMPLETED. 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 -
NOTE
FOR AIRCRAFT AWAY FROM HOME STATION: AFTER VISUAL
INSPECTION FOR RESIDUE, AND/OR SWASHPLATE DAMAGE,
CHECK FOR LOOSENESS WITH HYDRAULIC POWER APPLIED.
HAVE HELPER MOVE THRUST CONTROL UP AND DOWN AND
OBSERVE THE ACTUATOR TO SWASHPLATE CONNECTION FOR
LOOSENESS OR PLAY. IF RESIDUE, AND/OR SWASHPLATE
DAMAGE, AND/OR LOOSENESS IS DETECTED, THIS SAFETY OF
FLIGHT MESSAGE PROCEDURE SHALL BE PERFORMED AT THE
AIRCRAFT'S PRESENT LOCATION. IF RESIDUE, AND/OR
SWASHPLATE DAMAGE, AND/OR LOOSENESS IS NOT DETECTED,
THIS MESSAGE AUTHORIZES A ONE TIME FLIGHT, WITH
INTERMEDIATE STOPS, TO RETURN TO THE NEAREST SECURED
MAINTENANCE FACILITY/HOME STATION.
(1) SURFACE/AIR SHIPMENT - SAME AS PARA 1A.
(2) FERRY STATUS - SAME AS PARA 1A.
D. MAINTENANCE TRAINERS (CATEGORY A AND B) - INSPECT THE
FORWARD PIVOTING ACTUATOR UPPER ATTACHMENT BEARING IAW CH-47-02-
04 (TB 1-1520-240-20 -145) NLT 8 JUN 02.
E. 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 PARAGRAPH
10. REPORT COMPLIANCE WITH THIS MESSAGE IAW PARAGRAPH 14C(2) NLT
22 FEB 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 - PRIOR TO NEXT FLIGHT BUT NLT
22 FEB 02.
3. TAMMS REPORTING COMPLIANCE SUSPENSE DATE - REPORT COMPLIANCE
IAW PARA 14A(1) NLT 12 FEB 02.
4. SUMMARY OF PROBLEM -
A. A QUALITY DEFICIENCY REPORT HAS BEEN RECEIVED FROM THE
FIELD DOCUMENTING THAT THE WRONG BEARING WAS INSTALLED IN THE
FORWARD PIVOTING ACTUATOR UPPER ATTACHMENT. THE APPARENT CAUSE
WAS AN ERROR IN THE PARTS MANUAL; WHILE THIS WRONG BEARING FITS
PROPERLY IN THE ACTUATOR, ITS INNER DIAMETER IS TOO LARGE FOR THE
MATING BOLT.
B. 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 FORWARD PIVOTING ACTUATOR UPPER ATTACHMENT
BEARINGS FOR THE PROPER PART.
5. END ITEMS TO BE INSPECTED - ALL H-47 AIRCRAFT.
6. ASSEMBLY COMPONENTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
CYLINDER, FWD ACTUATING
DUAL PIVOTING 145H6600-19 1650-01-304-9016
7. PARTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
CYLINDER, ACTUATING DUAL PIVOTING:
BEARING-PLAIN
SELF-ALIGNING 145HS001-1 3120-01-111-0693
PIN, COTTER MS24665-304 5315-00-241-7330
NUT, PLAIN AN320-8 5310-00-176-8112
WASHER, PLAIN NAS1149F0863P 5310-01-396-8392
BOLT ASSY 114R3650-3 1615-00-003-1146
RING ASSY, SWASHPLATE:
RING 414R3351-2 1650-01-438-5361
BUSHING 114R3116-54 3120-01-066-5380
BUSHING, SLEEVE 145R3116-1 3120-01-129-7648
8. INSPECTION PROCEDURES -
A. PREPARE AIRCRAFT FOR SAFE GROUND MAINTENANCE.
B. PER TASK 7-124 OF REFERENCE 13.B (CH-/MH-47D), AND TASK
7-146 OF REFERENCE 13.C (MH-47E), REMOVE FORWARD PIVOTING
ACTUATOR TO SWASHPLATE BOLT.
NOTE
MAINTAINERS WERE INSTALLING AFT PIVOTING ACTUATOR
BEARING IN THE FORWARD ACTUATOR. THE SUSPECTED WRONG
PART IS BEARING P/N 145HS001-2. ITS OUTER
DIAMETER(OD)IS THE SAME AS P/N 145HS001-1, BUT THE
INNER DIAMETER(ID) IS DIFFERENT. THE -2 INNER
DIAMETER IS 0.6250 +.0000/-.0005; THE CORRECT -1
INNER DIAMETER IS 0.5000 +.0000/-.0005.
C. MEASURE INNER DIAMETER OF BEARING ON PIVOTING ACTUATOR AT
SWASHPLATE ATTACHMENT POINT.
(1) IF BEARING ID EQUALS .625 INCHES, PROCEED TO PARA 8D.
(2) IF BEARING EQUALS ID .5 INCHES RECONNECT FORWARD
PIVOTING SERVO CYLINDER PER TASK 7-131 OF REFERENCE 13.B(CH-/MH-
47D), AND TASK 7-154 OF REFERENCE 13.C (MH-47E). INSPECTION IS
COMPLETE. PROCEED TO PARA. 9D.
NOTE
FOR REF. 13.D, FIGURE 244, ITEM NO. 95, AND
REF. E, FIGURE 7-48, ITEM NO. 95, THE PART NO.
LISTING IS INCOMPLETE AND THE USABLE ON CODE (UOC)
IS INCORRECT. THE PART NUMBER(S) AND DESCRIPTION
AND UOC, FOR BOTH REFERENCES, SHOULD READ:
ITEM NO. PART NUMBER DESCRIPTION AND UOC
95 145HS001-1 .BEARING, PLAIN, SELF U/W
FWD PIVOTING ACTUATOR PN 145H6600-19
95 145HS001-2 .BEARING, PLAIN, SELF U/W
AFT PIVOTING ACTUATOR PN 145H6600-20
D. REMOVE FORWARD PIVOTING SERVO CYLINDER PER TASK 7-124 OF
REFERENCE 13.B (CH-/MH-47D), AND TASK 7-146 OF REFERENCE 13.C
(MH-47E).
E. INSPECT THE FOLLOWING SWASHPLATE PARTS FOR CONDITION IN
ACCORDANCE WITH TASK 5-126, REF 13.B (CH-47D, MH-47D), AND TASK
5-180, REF 13.C, (MH-47E);
NOMENCLATURE PART NO.
RING 414R3351-2
BUSHING 114R3116-54
BUSHING, SLEEVE 114R3116-1
(1) IF ANY OF THE PARTS IN 8E ABOVE DO NOT PASS
INSPECTION, PROCEED TO PARA 9A.
(2) IF PARTS PASS INSPECTION, PROCEED TO PARA 9B.
9. CORRECTION PROCEDURES -
A. IF ANY OF THE PARTS IN PARA. 8E ABOVE DO NOT PASS
INSPECTION:
(1) REMOVE THE FORWARD SWASHPLATE ASSEMBLY PER TASK 5-
116, REF. 13.B (CH-47D, MH-47D), AND TASK 5-168, REF. 13.C (MH-
47E).
(2) INSTALL A REPLACEMENT SWASHPLATE ASSEMBLY PER TASKS
5-131 AND 5-132, REF. 13.B (CH-47D, MH-47D), AND TASKS 5-186 AND
5-187, REF. 13.C (MH-47E).
B. REMOVE AND DISCARD P/N 145HS001-2 BEARING PER TASK 7-129
OF REF. B AND TASK 7-151 OF REF. C.
C. USING A 10X MAGNIFYING GLASS, VISUALLY INSPECT THE
FORWARD PIVOTING ACTUATOR TO INCLUDE HOUSING AND BEARING
RETAINERS FOR DAMAGE AND ABNORMAL WEAR. ALSO, CHECK SPECIFICALLY
FOR ROD END HOLE ELONGATION. DIAMETER SHOULD NOT EXCEED 1.1868
INCHES.
(1) IF NO DAMAGE OR ABNORMAL WEAR IS NOTED, INSTALL NEW
145HS001-1 BEARING (INSPECT BEARING ID FOR PROPER DIMENSION) PER
TASK 7-129 OF REF. B AND TASK 7-151 OF REF. C. REINSTALL FORWARD
PIVOTING ACTUATOR (PN 145H6600-19) PER TASK 7-131 OF REF. B. (CH-
47D, MH-47D), AND TASK 7-154 OF REF. C (MH-47E). PROCEED TO PARA
9.D.
(2) IF DAMAGE OR ABNORMAL WEAR EXISTS, REPLACE ACTUATOR
AND INSTALL NEW FORWARD PIVOTING ACTUATOR (PN 145H6600-19) PER
TASK 7-131 OF REF. B. (CH-47D, MH-47D), AND TASK 7-154 OF REF. C
(MH-47E).
WARNING
DO NOT REUSE THE UPPER ATTACHMENT FASTENING
HARDWARE REMOVED IN STEP 9C(1) AND (2) ABOVE.
USE NEW FASTENER HARDWARE:
PIN, COTTER MS24665-304
NUT, PLAIN AN320-8
WASHER, PLAIN NAS1149F0863P
BOLT ASSY 114R3650-3
NOTE
FOR TM 55-1520-240-23P, FIGURE 177,
ITEM NO. 94, THE PART NO. LISTING IS INCORRECT.
THE PART NUMBER SHOULD READ:
ITEM NO. PART NUMBER
94 414R3351-1
D. THE RED HORIZONTAL DASH //-// ENTRY PER PARAGRAPH 1A
WILL BE CLEARED.
10. SUPPLY/PARTS AND DISPOSITION -
NOTE
HQDA-ODCSOPS WILL PRIORITIZE UNITS AND
REPAIR PARTS DISTRIBUTION IN A
SEPARATE, FOLLOW ON MESSAGE.
A. PARTS REQUIRED - ITEMS CITED IN 6 AND 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) "X1N" (X-RAY-ONE-NOVEMBER).
NOTE
PROJECT CODE "X1N" 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 -
NOMENCLATURE PART NUMBER NSN
PIN, COTTER MS24665-304 5315-00-241-7330
NUT, PLAIN AN320-8 5310-00-176-8112
WASHER, PLAIN NAS1149F0863P 5310-01-396-8392
BUSHING 114R3116-54 3120-01-066-5380
BUSHING, SLEEVE 145R3116-1 3120-01-129-7648
D. DISPOSITION - DISPOSE OF REMOVED PARTS/COMPONENTS USING
NORMAL SUPPLY PROCEDURES. ALL TURN-IN DOCUMENTS MUST INCLUDE
PROJECT CODE (CC 57-59) "X1N" (X-RAY-ONE-NOVEMBER).
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 MAINTENANCE. REPORT AIRCRAFT NON-MISSION
CAPABLE MAINTENANCE (NMCM) WHILE UNDERGOING INSPECTION AND
CORRECTION IAW THIS MESSAGE. REPORT AIRCRAFT NON-MISSION CAPABLE
SUPPLY (NMCS) WHILE WAITING FOR PARTS IAW THIS MESSAGE.
B. ESTIMATED TIME REQUIRED -
(1) TIME TO COMPLETE INSPECTION -
(A) TOTAL OF 9 MAN-HOURS USING 3 PERSONS.
(B) TOTAL OF 3 HOURS DOWNTIME FOR ONE END ITEM.
(2) TIME FOR REPAIR/REPLACEMENT -
(A) TOTAL OF 60 MAN-HOURS USING 6 PERSONS.
(B) TOTAL OF 10 HOURS DOWNTIME FOR ONE END ITEM.
NOTE
MOC AND TEST FLIGHT REQUIRED
C. ESTIMATED COST IMPACT TO THE FIELD -
NOMENCLATURE PART NO./NSN QTY COST EA. TOTAL $
BEARING-PLAN SELF 145HS001-1 1 $28.36 $28.36
-ALIGNING 3120-01-111-0693
BOLT ASSY 114R3650-3 1 $72.95 $72.95
1615-00-003-1146
SERVOCYLINDER 145H6600-19 1 $8603.08 $8603.08
1650-01-304-9016
SWASHPLATE, FWD 145R3551-19 1 $133,378.00 $133,378.00
1615-01-473-4376
MAXIMUM TOTAL COST PER AIRCRAFT = $142.082.39
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 - 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 55-1520-240-23P, FIGURE 244, ITEM NO. 95, THE
PART NO. LISTING IS INCOMPLETE AND THE USABLE ON CODE (UOC) IS
INCORRECT. THE PART NUMBER(S) AND DESCRIPTION AND UOC, SHOULD
READ:
ITEM NO. PART NUMBER DESCRIPTION AND UOC
95 145HS001-1 .BEARING, PLAIN, SELF
U/W FWD PN 145H6600-19
95 145HS001-2 .BEARING, PLAIN, SELF
U/W AFT PN 145H6600-20
2. TM 1-1520-252-23P, FIGURE 7-48, ITEM NO. 95,
THE PART NO. LISTING IS INCOMPLETE AND THE USABLE ON CODE (UOC)
IS INCORRECT. THE PART NUMBER(S) AND DESCRIPTION AND UOC, SHOULD
READ:
ITEM NO. PART NUMBER DESCRIPTION AND UOC
95 145HS001-1 .BEARING, PLAIN, SELF
U/W FWD PN 145H6600-19
95 145HS001-2 .BEARING, PLAIN, SELF
U/W AFT PN 145H6600-20
(3) REFERENCE 13.D, FIGURE 177, ITEM NO. 94, THE PART
NO. LISTING WILL BE CHANGED TO 414R3351-2.
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 EFFECTED
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 -
(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 PARAGRAPH 16B NLT DATE SPECIFIED
IN PARAGRAPH 1E(2). REPORT THE QUANTITY INSPECTED BY CONDITION
CODE AND THE RESULTING CONDITION CODE. REPORT BY E-MAIL OR
DATAFAX 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
(FWD PIVOTING ACTUATOR ).
(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. (ONLY IF SWASHPLATE ASSY OR PIVOTING ACTUATOR IS
REMOVED/REPLACED)
(5) DA FORM 2410, COMPONENT REMOVAL AND REPAIR/OVERHAUL
RECORD. (ONLY IF SWASHPLATE ASSY OR PIVOTING ACTUATOR IS
REMOVED/REPLACED)
(6) DD FORM 1577-2/DD FORM 1577-3, UNSERVICEABLE
(REPARABLE) TAG/LABEL - MATERIEL (COLOR GREEN). ANNOTATE REMARKS
BLOCK WITH "UNSERVICEABLE IAW CH-47-02-04 (TB 1-1520-240-20-145)"
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 DSN 897-4348.
E-MAIL IS "MIKE.MOORE@PEOAVN.REDSTONE.ARMY.MIL".
B. LOGISTICAL POINT OF CONTACT FOR THIS MESSAGE IS 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) N/A.
D. FORMS AND RECORDS POINT OF CONTACT FOR THIS MESSAGE IS
MS. ANN WALDECK, AMSAM-MMC-MA-NM, DSN 746-5564 OR (256) 876-5564,
DATAFAX IS DSN 746-4904.
E-MAIL IS "ANN.WALDECK@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 -
MR. RONNIE W. SAMMONS, AMSAM-SA-CS-NF, DSN 897-6856 OR (256) 313-
6856. DATAFAX IS DSN 897-6630 OR (256) 313-6630.
EMAIL IS "RONNIE.SAMMONS@REDSTONE.ARMY.MIL".
G. AFTER HOURS CONTACT THE AMCOM COMMAND OPERATIONS CENTER
(COC) DSN 897-2066/7 OR (256) 313-2066/7.