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:AIG 8881
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:CDRUSARDSG CANBERRA ACT AS//AMXIP-AS//
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:UNCLAS
SUBJECT - SAFETY OF FLIGHT MESSAGE, TECHNICAL, RCS CSGLD-1860(R1),
ALL H-47 SERIES AIRCRAFT, UNGROUNDING REQUIREMENTS FOR AIRCRAFT
WITH INCORRECTLY INSTALLED DROOP STOPS, CH-47-01-03
(TB 1-1520-240-20-137).
NOTE
THIS IS A SAFETY OF FLIGHT MESSAGE ISSUED IAW AR 95-1, CHAPTER 6,
1 SEP 97. THIS MESSAGE HAS NOT BEEN TRANSMITTED TO UNITS SUBORDINATE
TO ADDRESSEES. ADDRESSEES SHALL 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, PARA 6-6A, MACOM COMMANDERS MAY AUTHORIZE TEMPORARY
EXCEPTION FROM SOF 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
AIRCRAFT IAW CH-47-01-03 (TB 1-1520-240-20-137) PRIOR TO NEXT
ENGINE START (ROTORS TURNING) BUT NLT 23 FEB 01." 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 FACILITY -
(1) AIRCRAFT IN AVUM, AVIM OR DEPOT - SAME AS PARA 1A.
(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 - SAME AS PARA 1A.
D. MAINTENANCE TRAINERS (CATEGORY A AND B) - SAME AS PARA 1A.
E. COMPONENT/PARTS IN STOCK AT ALL LEVELS (DEPOT AND OTHERS)
INCLUDING WAR RESERVES -
(1) WHOLESALE STOCK - N/A
(2) RETAIL STOCK - REPORT RECEIPT OF THIS MESSAGE IAW
PARAGRAPH 14C(2). 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.
COMMANDERS WILL ENSURE THE MATERIAL CONDITION TAGS OF ALL ITEMS IN
ALL CONDITION CODES LISTED IN PARAGRAPHS 6 AND 7 ARE ANNOTATED TO
READ CH-47-01-03 (TB 1-1520-240-20-137), INSPECTION OF DROOP STOP NOT
COMPLIED WITH." DISPOSE OF DISCREPANT MATERIAL IAW PARAGRAPH 10.
REPORT COMPLIANCE WITH THIS MESSAGE IAW PARAGRAPH 14D(2).
F. 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 AND
CORRECTION PROCEDURES IAW PARAGRAPHS 8 AND 9 PRIOR TO NEXT ENGINE
START (ROTORS TURNING) BUT NLT 23 FEB 01.
3. REPORTING COMPLIANCE SUSPENSE DATE - REPORT COMPLIANCE IAW
PARA 14A NLT 22 FEB 01
4. SUMMARY OF PROBLEM -
A. WHILE CONDUCTING AN ACCIDENT INVESTIGATION, INCORRECTLY
INSTALLED DROOP STOPS WERE DISCOVERED. SAFETY OF FLIGHT MESSAGE
CH-47-01-02 WAS ISSUED CALLING FOR A ONE TIME INSPECTION ON
FORWARD AND AFT DROOP STOPS FOR PROPER INSTALLATION.
B. MANPOWER/DOWNTIME AND FUNDING IMPACTS - SEE PARA 12.
C. THE PURPOSE OF THIS MESSAGE IS TO -
(1) IDENTIFY AN ADDITIONAL AUTHORIZED AFT DROOP STOP
CONFIGURATION.
(2) PROVIDE INSTRUCTIONS FOR CORRECTING THOSE AIRCRAFT
WHICH HAVE THEIR DROOP STOPS INSTALLED INCORRECTLY.
5. END ITEMS TO BE INSPECTED - ALL H-47 SERIES AIRCRAFT.
6. ASSEMBLY COMPONENTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
FORWARD ROTOR HEAD 145R2003-ALL N/A
AFT ROTOR HEAD 145R2004-ALL N/A
7. PARTS TO BE INSPECTED -
NOMENCLATURE PART NO. NSN
DROOP STOP, FWD 114R2063-7 1615-00-967-9759
DROOP STOP, AFT 114R2087-2 1615-00-941-8730
DROOP STOP, AFT 114R2087-3 1615-01-199-1785
PITCH SHAFT 114R2088-7 1615-00-757-7115
PITCH SHAFT 114R2088-14 3040-00-919-1356
PITCH SHAFT 114R2088-15 1615-01-111-4313
PITCH SHAFT 114R2088-16 3040-01-105-1431
PITCH SHAFT 234R2088-1 1615-01-205-3921
PITCH SHAFT 234R2088-2 3040-01-206-3925
8. INSPECTION PROCEDURES -
A. INSPECT THE AIRCRAFT DA FORM 2408-13-1 FOR A RED //X//
ENTRY WHICH STATES, "AIRCRAFT GROUNDED IAW SOF CH-47-01-02 FOR
IMPROPERLY INSTALLED DROOP STOP(S)." IF THIS WRITE-UP EXISTS,
PROCEED TO PARAGRAPH 9 FOR CORRECTION PROCEDURES.
NOTE
FOR A DESCRIPTION OF THE INSPECTION REQUIREMENTS OF
THIS MESSAGE, REFER TO THE FOLLOWING WEBSITE -
HTTP://SAFETY.ARMY.MIL/MESSAGES/DROOPSTOPUPDATE.HTML
B. AIRCRAFT WHICH DO NOT HAVE THE ABOVE RESTRICTION ARE NOT
AFFECTED BY THIS MESSAGE AND RED //-// MAY BE CLEARED FOR FLIGHT
AND COMPLIANCE WITH THIS MESSAGE WILL BE NOTED.
9. CORRECTION PROCEDURES
A. PREPARE AIRCRAFT FOR SAFE GROUND MAINTENANCE.
WARNING
NUMEROUS CASES OF IMPROPER STENCILING OF THE DROOP
STOPS HAVE BEEN IDENTIFIED. THEY RANGE FROM IMPROPER
MARKING, TO MISSING/UNREADABLE STENCILING. THE
CORRECT DROOP STOP INSTALLATION AT THIS TIME SHALL BE
IDENTIFIED BY THE CHAMFERED EDGE OF THE DROOP STOP
FACING THE RADIUS OF THE PITCH SHAFT DROOP STOP BOSS.
SEPARATE INSTRUCTIONS WILL BE PROVIDED BY THE CH-47
PMO CUSTOMER SERVICE DEPARTMENT CONCERNING THE
REQUIREMENT TO PROPERLY MARK THE DROOP STOPS.
B. IF THE RED //X// ENTRY IDENTIFIED IN 8A ABOVE WAS REQUIRED
DUE TO THE FORWARD DROOP STOPS BEING INCORRECTLY INSTALLED, REMOVE
AND REPLACE ROTOR HEAD ASSEMBLY IAW REF 13B TASK 5-8 AND 5-9, REF 13C
TASK 5-9 AND 5-10.
C. IF THE RED //X// ENTRY IDENTIFIED IN 8A ABOVE WAS REQUIRED
DUE TO THE AFT DROOP STOPS NOT MEETING THE CONFIGURATION REQUIREMENTS
IDENTIFIED IN CH-47-01-02, PARAGRAPH 8C(1) (I.E. THE DROOP STOP DOES
NOT HAVE THE TWO ADDITIONAL OUTBOARD HOLES REQUIRED FOR DROOP STOP
SHIELD), INSPECT AS FOLLOWS TO DETERMINE IF THE 114R2087-2 STOP WHICH
IS AN AUTHORIZED CONFIGURATION IS INSTALLED. THE 114R2087-2 AFT
DROOP STOP HAS TWO CHAMFERED EDGES, BUT ONLY TWO HOLES USED FOR DROOP
STOP INSTALLATION. THE TWO HOLE/TWO CHAMFER AFT DROOP STOP
CONFIGURATION (PART NUMBER 114R2087-2) IS AUTHORIZED AND MUST BE
INSTALLED CORRECTLY. THE SIDE WITH THE MOUNTING HOLES SHALL HAVE THE
CHAMFER UPWARD IN THE RADIUS OF THE PITCH SHAFT DROOP STOP BOSS.
D. IF THE RED //X// ENTRY IDENTIFIED IN 8A ABOVE WAS REQUIRED
DUE TO AFT DROOP STOPS BEING INCORRECTLY INSTALLED, PERFORM THE
FOLLOWING -
(1) REMOVE INCORRECTLY INSTALLED DROOP STOP IAW REF 13B,
TASK 5-48 (CH/MH-47D) AND REF 13C, TASK 5-59 (MH-47E). THE DROOP
STOP, BOLTS AND WASHERS SHALL BE DISPOSED OF AND NOT REUSED.
(2) VISUALLY INSPECT THE AFT ROTOR HEAD ASSEMBLY AS FOLLOWS -
(A) PITCH SHAFT BOSS DROOP STOP MOUNTING HOLES FOR
EVIDENCE OF ELONGATION OR SCORING. NO ELONGATION OR SCORING IS
ALLOWED. INSPECT PER REFERENCE 13.E, PARAGRAPH 3-22. HOLE DIAMETER
SHALL NOT EXCEED 0.287 INCHES.
(B) PITCH SHAFT DROOP STOP BOSS RADIUS FOR EVIDENCE
OF DROOP STOP CONTACT. NO PAINT DAMAGE OR DENTING IN THE RADIUS
AREA IS ALLOWED.
(C) EVIDENCE OF CONTACT BETWEEN THE IMPROPERLY
INSTALLED DROOP STOP AND THE HUB WEB. NO EVIDENCE OF CONTACT
SHALL BE PERMITTED.
(D) IF DAMAGE IS FOUND ON THE PITCH SHAFT OR HUB,
THE ROTOR HEAD IS CONSIDERED UNSERVICEABLE AND MUST BE REMOVED
AND REPLACED IAW REF 13B TASK 5-8 AND 5-9, REF 13C TASK 5-9 AND 5-10.
(3) IF PITCH SHAFT AND HUB ARE UNDAMAGED, INSTALL DROOP
STOP USING NEW STOP, BOLTS, AND WASHERS IAW REF 13B, TASK 5-48
(CH/MH-47D) AND REF 13C TASK 5-59 (MH-47E). INSTALL WITH
CHAMFERED EDGE IN THE RADIUS OF THE PITCH SHAFT DROOP STOP BOSS.
E. SUBMIT A CATEGORY I DEFICIENCY REPORT FOR ALL UNSERVICEABLE
ROTOR HEAD ASSEMBLIES REMOVED VIA THIS MESSAGE.
F. AFTER COMPLETION OF ABOVE CORRECTIVE PROCEDURES THE RED //X//
ENTRY AND THE RED //-// ENTRY MAY BE CLEARED AND COMPLIANCE WITH THIS
MESSAGE NOTED.
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) "X1A" (X-RAY-ONE-ALPHA).
NOTE
PROJECT CODE "X1A" 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 - DISPOSE OF REMOVED PARTS/COMPONENTS USING
NORMAL SUPPLY PROCEDURES. ALL TURN-IN DOCUMENTS MUST INCLUDE PROJECT
CODE (CC 57-59) "X1A".
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. REPORT AIRCRAFT NON-MISSION CAPABLE MAINTENANCE
(NMCM) WHILE UNDERGOING INSPECTION AND CORRECTION IAW THIS MESSAGE.
B. ESTIMATED TIME REQUIRED -
(1) TIME REQUIRED TO COMPLETE INSPECTION - TOTAL OF 1
MAN-HOUR USING 1 PERSON.
(2) TIME REQUIRED FOR DROOP STOP REPLACEMENT -
(A) TOTAL OF 8 MAN-HOURS USING 2 PERSONS.
(B) TOTAL OF 4 HOURS DOWNTIME FOR ONE END ITEM.
(3) TIME REQUIRED FOR ROTOR HEAD REPLACEMENT -
(A) TOTAL OF 30 MAN-HOURS USING 5 PERSONS.
(B) TOTAL OF 6 HOURS DOWNTIME FOR ONE END ITEM.
C. ESTIMATED COST IMPACT TO THE FIELD -
NOUN PART NO./NSN QTY COST EA. TOTAL
ROTOR HEAD, 145R2004-20 1 $167,729.00 $167,729.00
AFT 1615-01-391-4399
ROTOR HEAD, 145R2003-10 1 $167,729.00 $167,729.00
FWD 1615-01-391-4398
BOLT NAAS624H7 12 $7.50 $90.00
5306-00-862-8202
DROOP STOP, 114R2087-3 3 $134.12 $402.36
AFT 1615-01-199-1785
DROOP STOP, 114R2063-7 3 $27.95 $83.85
FWD 1615-00-967-9759
WASHER BACW10DH-C4 12 $0.21 $2.52
5310-01-143-6570
MAXIMUM COST PER AIRCRAFT $335,458.00
(THIS COST IS THE MAXIMUM COST PER AIRCRAFT. IF THE ROTOR HEAD
IS REPLACED, THE ADDITIONAL PARTS LISTED ABOVE ARE INCLUDED WITH
THE ROTOR HEAD)
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 AND TM 1-1520-252-23 WILL BE
UPDATED 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.
B. TM 55-1520-240-23
C. TM 1-1520-252-23
D. SOF CH-47-01-02
E. TM 1-1500-204-23-9
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, 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 MISSION
DESIGN SERIES AND SERIAL NUMBERS OF AIRCRAFT IN NUMERICAL ORDER.
B. TASK/INSPECTION REPORTING SUSPENSE DATE (AIRCRAFT) -
UPON COMPLETION OF THE INSPECTION/CORRECTION PROCEDURES,
COMMANDERS WILL FORWARD A PRIORITY MESSAGE TO THE LOGISTICS POINT
OF CONTACT IN PARAGRAPH 16B. THE REPORT WILL CITE THIS MESSAGE,
DATE OF INSPECTION, DATE OF CORRECTION, AIRCRAFT SERIAL NUMBER,
AIRCRAFT HOURS, AND RESULTS OF THE INSPECTION/CORRECTION.
INSPECTION/CORRECTION AND REPORTS WILL BE COMPLETED NO LATER THAN
14 DAYS AFTER COMPLETION OF CORRECTIVE ACTION.
C. REPORTING MESSAGE RECEIPT (SPARES) -
(1) MATERIAL IN WHOLESALE DEPOT STORAGE - N/A.
(2) MATERIAL IN RETAIL STORAGE - COMMANDERS AND FACILITY
MANAGERS WILL REPORT RECEIPT OF THIS MESSAGE BY E-MAIL OR DATAFAX TO
THE LOGISTICAL POINT OF CONTACT LISTED IN PARAGRAPH 16B NLT 22
FEB 01. PROVIDE LOCAL POINT OF CONTACT.
D. TASK/INSPECTION REPORTING SUSPENSE DATE (SPARES).
(1) MATERIAL IN WHOLESALE DEPOT STORAGE - N/A.
(2) MATERIAL IN RETAIL STORAGE - COMMANDERS AND FACILITY
MANAGERS WILL REPORT COMPLIANCE WITH THIS MESSAGE TO THE LOGISTICAL
POINT OF CONTACT IN PARAGRAPH 16B NLT 1 MAR 01 REPORT THE QUANTITY
INSPECTED BY CONDITION CODE AND THE RESULTING CONDITION CODE. REPORT
BY E-MAIL OR DATAFAX AND PROVIDE LOCAL POINT OF CONTACT.
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
FORWARD AND AFT ROTOR HEADS.
(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 2410, COMPONENT REMOVAL AND REPAIR/OVERHAUL
RECORD (ONLY IF ROTOR HEAD OR PITCH SHAFT IS REMOVED OR REPLACED).
(7) DD FORM 1577-2/DD FORM 1577-3, UNSERVICEABLE
(REPARABLE) TAG/LABEL - MATERIEL (COLOR GREEN). ANNOTATE REMARKS
BLOCK WITH "UNSERVICEABLE IAW CH-47-01-03 (TB 1-1520-240-20-137)".
15. WEIGHT AND BALANCE - N/A.
16. POINTS OF CONTACT -
A. TECHNICAL POINT OF CONTACT IS LARRY WIESCHHAUS, AMSAM-
RD-AE-I-P-C, DSN 897-3341 OR (256) 313-3341, DATAFAX IS 256-313-4348.
E-MAIL IS "LARRY.WIESCHHAUS@REDSTONE.ARMY.MIL".
B. LOGISTICAL POINT OF CONTACT IS BILL OLSON , SFAE-AV-CH-L,
DSN 897-3379 OR (256) 313-3379, DATAFAX IS 256-313-4348. E-MAIL IS
"WILLIAM.OLSON@PEOAVN.REDSTONE.ARMY.MIL".
C. WHOLESALE MATERIAL POINT OF CONTACT (SPARES) IS MS. GERI
REDDY, AMSAM-MMC-AV-CA, DSN 897-1511 OR (256) 313-1511, DATAFAX
IS DSN 897-1106. E-MAIL IS "GERI.REDDY@REDSTONE.ARMY.MIL".
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. 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. 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) CW5 JOSEPH L. WITTSTROM, SECURITY ASSISTANCE
MANAGEMENT, AMSAM-SA, DSN 897-0410 OR (256) 313-0410. EMAIL IS
"JOSEPH.WITTSTROM@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 "RONNIE.SAMMONS@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.
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