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:UNCLAS
SUBJECT - AVIATION SAFETY ACTION MESSAGE, MAINTENANCE MANDATORY,
RCS CSGLD-1860(R1), ALL H-47 SERIES AIRCRAFT, FORWARD AND AFT
ROTOR HUB LIGHTENING HOLE INSPECTIONS, CH-47-01-ASAM-03
(TB 1-1520-240-20-131)
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
ROTOR HUB LIGHTENING HOLES IAW CH-47-01-ASAM-03 (TB 1-1520-240-
131) WITHIN THE NEXT 10 FLIGHT HOURS, BUT NLT 23 NOV 00." 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 23 NOV 00. 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 DEPOT MAINTENANCE - DEPOT COMMANDERS WILL NOT
ISSUE AIRCRAFT UNTIL THEY ARE IN COMPLIANCE WITH THIS MESSAGE.
C. AIRCRAFT UNDERGOING MAINTENANCE - COMMANDERS AND FACILITY
MANAGERS WILL NOT ISSUE AIRCRAFT UNTIL THEY ARE IN COMPLIANCE
WITH THIS MESSAGE.
D. AIRCRAFT IN TRANSIT -
(1) SURFACE/AIR SHIPMENT - WITHIN 10 FLIGHT HOURS OR 14
DAYS OF ARRIVAL.
(2) FERRY STATUS -
(A) INSPECT AT FINAL DESTINATION WITHIN 10 FLIGHT
HOURS OR 14 DAYS OF ARRIVAL.
(B) BOEING WILL INSPECT DD 250 AIRCRAFT PRIOR TO
THOSE AIRCRAFT DEPARTING FOR FERRY TO FINAL DESTINATION.
E. MAINTENANCE TRAINERS (CATEGORY A AND B) - COMPLY NLT 8
MARCH 2001.
F. 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 PARAGRAPHS 6
AND 7 ARE ANNOTATED TO READ: "CH-47-01-ASAM-03, (TB 1-55-1520-
240-131), ROTOR HUB LIGHTENING HOLE INSPECTIONS NOT COMPLIED
WITH."
G. COMPONENTS/PARTS IN WORK (DEPOT LEVEL AND OTHERS) - DEPOT
AND OTHER MAINTENANCE ACTIVITY COMMANDERS WILL ENSURE ITEMS
LISTED IN PARAGRAPHS 6 AND 7 ARE NOT ISSUED UNTIL THEY ARE IN
COMPLIANCE WITH THIS MESSAGE.
2. TASK/INSPECTION SUSPENSE DATE - COMPLETE THE INSPECTION IAW
PARAGRAPH 8 WITHIN THE NEXT 10 FLIGHT HOURS BUT NLT 23 NOV 00 AND
REPORT IAW PARA 14B.
3. REPORTING COMPLIANCE SUSPENSE DATE - REPORT COMPLIANCE IAW
PARA 14A NLT 5 DEC 00.
4. SUMMARY OF PROBLEM -
A. A CATEGORY I DEFICIENCY REPORT WAS RECEIVED WHICH
REVEALED CRACKS EXTENDING FROM THE LIGHTENING HOLES IN THE
VERTICAL WEB AREA OF THE ROTOR HEAD CENTER HUB. WHEN DISCOVERED,
THESE CRACKS WERE GREATER THAN ONE INCH IN LENGTH. FURTHER
INVESTIGATION REVEALED THE CRACKS WENT UNDISCOVERED DURING
SEVERAL PHASED MAINTENANCE VISUAL INSPECTIONS. RESEARCH REVEALED
THREE OTHER ROTOR HUBS THAT HAVE BEEN FOUND WITH SIMILAR CRACKS.
B. FOR MANPOWER/DOWNTIME AND FUNDING IMPACTS SEE PARA 12.
C. THE PURPOSE OF THIS MESSAGE IS TO REQUIRE AN INITIAL
VISUAL, RECURRING VISUAL, AND RECURRING EDDY CURRENT INSPECTION
OF THE VERTICAL WEB LIGHTENING HOLE AREAS OF ALL ROTOR HUBS
IDENTIFIED IN PARAGRAPH 7 OF THIS MESSAGE.
5. END ITEMS TO BE INSPECTED - ALL H-47 SERIES AIRCRAFT.
6. ASSEMBLY COMPONENTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
HEAD, ROTARY WING, FORWARD 145R2003-1 1615-01-118-5634
145R2003-3 1615-01-198-7555
145R2003-4 1615-01-184-3875
145R2003-5 1615-01-345-0477
145R2003-6 1615-01-296-9503
145R2003-9 1615-01-314-8863
145R2003-10 1615-01-391-4398
HEAD, ROTARY WING, AFT 145R2004-2 1615-01-115-3607
145R2004-6 1615-01-199-1814
145R2004-8 1615-01-184-3874
145R2004-10 1615-01-312-6833
145R2004-12 1615-01-298-0763
145R2004-18 1615-01-315-3972
145R2004-20 1615-01-391-4399
7. PARTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
FORWARD ROTOR HUB 114R2050-19 N/A
114R2050-21 1615-00-004-8891
114R2050-39 1615-01-246-1341
114R2050-41 1615-01-246-1342
AFT ROTOR HUB 114R2050-20 N/A
114R2050-22 1615-00-004-8889
114R2050-40 1615-01-246-1345
114R2050-42 1615-01-246-1346
8. INSPECTION PROCEDURES -
NOTE
ONLY ROTOR HUBS THAT CONTAIN LIGHTENING HOLES
IN THE VERTICAL WEB AREAS REQUIRE THESE
INSPECTIONS. NOT ALL ROTOR HUBS CONTAIN THESE
LIGHTENING HOLES. SEE PARAGRAPH 7 FOR THE PART
NUMBERS OF AFFECTED ROTOR HUBS.
A. PERFORM RECORDS CHECK AND VISUAL INSPECTION OF MAIN ROTOR
HUBS TO DETERMINE THE PART NUMBERS OF HUBS INSTALLED. IF THE HUB
IS NOT AFFECTED, THE INSPECTION IS COMPLETE FOR THAT AIRCRAFT.
CLEAR THE DA FORM 2408-13-1 ENTRY AND REPORT COMPLIANCE.
B. PREPARE AIRCRAFT FOR SAFE GROUND MAINTENANCE.
C. REMOVE THE LOCKING BEAMS FROM THE HORIZONTAL HINGE PIN
CAPS IAW TM 55-1520-240-23, TASK 5-40 (CH-47D), OR TM 1-1520-252-
23, TASK 5-50 (MH-47E).
D. COMPLETELY CLEAN THE AREA AROUND THE LIGHTENING HOLES
USING ACETONE 0-A-51 OR EQUIVALENT.
E. VISUALLY INSPECT THE AREA SURROUNDING THE LIGHTENING
HOLES FOR CRACKS. ROTOR HUBS THAT ARE FOUND TO HAVE CRACKS ARE
NON-SERVICEABLE. IF CRACKS ARE FOUND PROCEED TO PARAGRAPH 9A.
F. IF NO CRACKS ARE FOUND, REINSTALL THE LOCKING BEAMS IAW
TM 55-1520-240-23, TASK 5-41 (CH-47D), OR TM 1-1520-252-23, TASK
5-52 (MH-47E). PROCEED TO PARAGRAPH 9B FOR RECURRING INSPECTION.
9. CORRECTION PROCEDURES -
A. IF ANY CRACKS ARE FOUND IN THE HUB, THE ROTOR HEAD
ASSEMBLY MUST BE REPLACED WITH A ROTOR HEAD ASSEMBLY THAT IS IN
COMPLIANCE WITH THIS ASAM.
(1) PREPARE AIRCRAFT FOR SAFE GROUND MAINTENANCE.
(2) REMOVE THE ROTOR HEAD ASSEMBLY IAW TM 55-1520-240-
23, TASK 5-8 (CH-47D), OR TM 1-1520-252-23, TASK 5-9 (MH-47E).
(3) REFER TO PARAGRAPH 10B FOR REQUISITION INSTRUCTIONS
FOR REPLACEMENT PARTS.
NOTE
ENSURE THAT THE REPLACEMENT ROTOR HEAD IS IN
COMPLIANCE WITH THIS ASAM PRIOR TO INSTALLATION.
(4) INSTALL THE REPLACEMENT ROTOR HEAD ASSEMBLY IAW TM
55-1520-240-23, TASK 5-9 (CH-47D), OR TM 1-1520-252-23, TASK 5-10
(MH-47E).
(5) REFER TO PARAGRAPH 10D FOR DISPOSITION INSTRUCTIONS
FOR NON-COMPLIANT PARTS.
NOTE
COMPLETION OF EDDY CURRENT INSPECTIONS
DEPEND ON THE AVAILABILITY OF PROBES. THE
PROBES ARE BEING SENT TO NDI PERSONNEL WHO
ACTUALLY SUPPORT CH-47 AIRCRAFT ONLY.
CONTACT YOUR NDI SUPPORT TECHNICIAN. THE
50 HOUR VISUAL INSPECTIONS WILL CONTINUE
UNTIL PROBES ARE AVAILABLE.
B. IF NO CRACKS ARE FOUND, PERFORM THE INSPECTION PROCEDURE
DESCRIBED IN PARAGRAPH 8 EVERY 50 FLIGHT HOURS. AN EDDY CURRENT
INSPECTION IS REQUIRED PRIOR TO INSTALLATION AND AT NEXT PHASED
INSPECTION INTERVAL AND EVERY PHASED INSPECTION INTERVAL
THEREAFTER. ONCE THE AIRCRAFT REACHES A PHASED INSPECTION
INTERVAL AND THE EDDY CURRENT INSPECTION IS PERFORMED, THE 50
HOUR VISUAL INSPECTION IS NO LONGER REQUIRED.
10. SUPPLY/PARTS AND DISPOSITION -
A. PARTS REQUIRED - ITEMS CITED IN PARAGRAPHS 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) "X0D" (X-RAY-ZERO-DELTA).
NOTE
PROJECT CODE "X0D" 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 - ACETONE, TECHNICAL, P/N
0-A-51, NSN 6810-00-184-4796.
D. DISPOSITION - DISPOSE OF REMOVED PARTS/COMPONENTS USING
NORMAL SUPPLY PROCEDURES. ALL TURN-IN DOCUMENTS MUST INCLUDE
PROJECT CODE (CC 57-59) "X0D" (X-RAY-ZERO-DELTA). NON-COMPLIANT
HUBS WILL BE SCRAPPED AT DEPOT LEVEL ONLY.
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 MAINTENANCE. REPORT AIRCRAFT NON-MISSION
CAPABLE MAINTENANCE (NMCM) WHILE UNDERGOING INSPECTION AND
CORRECTION IAW THIS MESSAGE.
B. ESTIMATED TIME REQUIRED -
(1) FOR INITIAL AND RECURRING 50 HOUR VISUAL INSPECTION -
(A) TOTAL OF 2 MAN-HOURS USING 1 PERSON.
(B) TOTAL OF 2 HOURS DOWNTIME FOR ONE END ITEM.
(2) FOR EDDY CURRENT INSPECTION -
(A) TOTAL OF 2 MAN-HOURS USING 1 PERSON.
(B) TOTAL OF 2 HOURS DOWNTIME FOR ONE END ITEM.
(3) FOR ROTOR HEAD REPLACEMENT:
(A) TOTAL OF 80 MAN-HOURS USING 8 PERSONS.
(B) TOTAL OF 10 HOURS DOWNTIME FOR ONE END ITEM.
C. ESTIMATED COST IMPACT TO THE FIELD -
NOMENCLATURE PART NO. NSN COST EA.
HEAD, ROTARY WING, FWD 145R2003-10 1615-01-391-4398 $167,729
HEAD, ROTARY WING, AFT 145R2004-20 1615-01-391-4399 $167,729
TOTAL COST PER AIRCRAFT (IF BOTH HUBS HAVE CRACKS) = $335,458
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 AS NOTED
BELOW 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 - ADD THE
FOLLOWING REQUIREMENT TO CONDITIONAL INSPECTIONS - "EDDY CURRENT
INSPECTION OF HUBS WITH LIGHTENING HOLES IS REQUIRED. PRIOR TO
INSTALLATION, INSPECT THE AREA SURROUNDING THE VERTICAL WEB".
(2) TM 1-1520-252-23 AVIATION UNIT AND AVIATION
INTERMEDIATE MAINTENANCE MANUAL, MH-47E HELICOPTER - ADD THE
FOLLOWING REQUIREMENT TO CONDITIONAL INSPECTIONS - "EDDY CURRENT
INSPECTION OF HUBS WITH LIGHTENING HOLES IS REQUIRED. PRIOR TO
INSTALLATION, INSPECT THE AREA SURROUNDING THE VERTICAL WEB".
(3) TM 55-1520-240-PM, CH-47D HELICOPTER PHASED
MAINTENANCE CHECKLIST. THE FOLLOWING STATEMENT SHALL BE ADDED TO
AREA #6, AFT ROTOR AND PYLON, AND AREA #7, FORWARD ROTOR, CROWN,
AND TUNNEL, "PERFORM EDDY CURRENT INSPECTION OF AREA SURROUNDING
THE VERTICAL WEB LIGHTENING HOLES ON ROTOR HUBS THAT CONTAIN SUCH
LIGHTENING HOLES". THIS INSPECTION SHALL BE REQUIRED AT EACH
PHASED MAINTENANCE INTERVAL.
(4) TM 1-1520-252-PM, MH-47E/AWC HELICOPTER PHASED
MAINTENANCE CHECKLIST. THE FOLLOWING STATEMENT SHALL BE ADDED TO
AREA #6, AFT ROTOR AND PYLON, AND AREA #7, FORWARD ROTOR, CROWN,
AND TUNNEL, "PERFORM EDDY CURRENT INSPECTION OF AREA SURROUNDING
THE VERTICAL WEB LIGHTENING HOLES ON ROTOR HUBS THAT CONTAIN SUCH
LIGHTENING HOLES". THIS INSPECTION SHALL BE REQUIRED AT EACH
PHASED MAINTENANCE INTERVAL.
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.
D. TM 55-1520-240-PM, CH-47D HELICOPTER PHASED MAINTENANCE
CHECKLIST.
E. TM 1-1520-252-PM, MH-47E/AWC HELICOPTER PHASED
MAINTENANCE CHECKLIST.
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 MISSION DESIGN SERIES (MDS) 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. 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 MDS AND SERIAL NUMBERS OF AIRCRAFT IN
NUMERICAL ORDER.
B. TASK/INSPECTION REPORTING SUSPENSE DATE (AIRCRAFT) -
UPON COMPLETION OF INSPECTION, COMMANDERS WILL FORWARD A PRIORITY
MESSAGE TO THE LOGISTIC POC 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 23 NOV
00.
C. REPORTING MESSAGE RECEIPT (SPARES) - N/A.
D. TASK/INSPECTION REPORTING SUSPENSE DATE (SPARES).
(1) MATERIEL IN WHOLESALE DEPOT STORAGE - N/A.
(2) MATERIEL IN RETAIL STORAGE - 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 2408-5-1, EQUIPMENT MODIFICATION RECORD
(MAIN ROTOR HEAD, MAIN ROTOR HUB).
(2) DA FORM 2408-13, AIRCRAFT STATUS INFORMATION
RECORD.
(3) DA FORM 2408-13-1, AIRCRAFT INSPECTION AND
MAINTENANCE RECORD.
(4) DA FORM 2408-15, HISTORICAL RECORD FOR AIRCRAFT.
(5) DA FORM 2408-16, AIRCRAFT COMPONENT HISTORICAL
RECORD.
(6) DA FORM 2408-18, EQUIPMENT INSPECTION LIST.
NOTE
ULLS-A UNITS WILL USE AN "800" INSPECTION NUMBER
FOR THE 50 HOUR MAIN ROTOR HEAD VISUAL INSPECTION.
(7) DA FORM 2410, COMPONENT REMOVAL AND REPAIR/
OVERHAUL RECORD. (ONLY IF MAIN ROTOR HEAD IS REMOVED/REPLACED.
(8) DD FORM 1574/DD FORM 1574-1, SERVICEABLE TAG/LABEL -
MATERIEL (COLOR YELLOW). ANNOTATE REMARKS BLOCK WITH "INSPECTED
SERVICEABLE IAW CH-47-01-ASAM-03 (TB 1-1520-240-20-131)."
(9) DD FORM 1577-2/DD FORM 1577-3, UNSERVICEABLE
(REPARABLE) TAG/LABEL - MATERIEL (COLOR GREEN). ANNOTATE REMARKS
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 897-3377 OR (256) 313-3377,
DATAFAX IS DSN 897-4348 OR (256) 313 4348. E-MAIL IS
"STEVE.PROSISE@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-RE-FF 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. RANDALL RUSHING (SAIC), AMSAM-SF-A,
DSN 897-2092 OR (256) 313-2092, DATAFAX IS DSN 897-2111 OR (256)
313-2111. E-MAIL IS "RANDALL.RUSHING@REDSTONE.ARMY.MIL".
(2) ALTERNATE - MR. RUSS 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) CW5 JOSEPH L. WITTSTROM, SECURITY ASSISTANCE
MANAGEMENT, AMSAM-SA, DSN 897-0410 OR (256) 313-0410. EMAIL IS
"WITTSTROMJL@REDSTONE.ARMY.MIL".
(2) MR. RONNIE W. SAMMONS, AMSAM-SA-CS-NF, DSN 897-0408
OR (256) 313-0408. DATAFAX IS DSN 897-0411 OR (256) 313-0411.
EMAIL IS "SAMMONSRW@REDSTONE.ARMY.MIL".
G. AFTER HOURS CONTACT THE AMCOM COMMAND OPERATIONS CENTER
(COC) DSN 897-2066/7 OR (256) 313-2066/7. HUNTSVILLE, AL IS GMT
MINUS 6 HRS.