FORMAT_NAME
:DD173                                                                   25550  
DISTRIBUTION
:CF:  AMSAT-R-E, AMSAT-D-SAF, AMSAT-WA, SFAE-AV, AMSAT-D-WAU,
:AMSAT-D-SLNO(RAAF), AMSAT-I-LOS(AOC), AMSAT-D-SS, AMSAT-D-SLNO(IS)
DRAFTERS_NAME
:KEN SCHNAARE, EQUIPMENT SPECIALIST
DRAFTERS_OFFICE
:AMSAT-R-X, X2999
RELEASERS_NAME
:NORBERT R. KNIEPP, X217
SPECIAL_INSTRUCTIONS
:MINIMIZE CONSIDERED
PAGE_OF
:        
DTG
:101430Z
MONTH
:APR
YEAR
:97
PRECEDENCE_ACTION
:PP
PRECEDENCE_INFO
:PP
CLASS
:UUUU
FL12A_DUMMY
:
SPECAT
:     
LMF
:AA
CIC
:ZYUW
OMI
:            
BOOK
:NO 
MSG_HANDLING
:                                                                
FROM
:CDRATCOM ST LOUIS MO//AMSAT-R-X//
TO
:AIG 8881
:AIG 9004
:AIG 8708
:AIG 9042
:AIG 7515
:AIG 7471
:AIG 12124
:DCM APMO OZARK AL//DCMDE-AOA//
:USDAO NICOSIA CY//11 CAB LNO//
:CDROSAC EASTERN REGION FT MCPHERSON GA//ANAV-ER//
:CDR4THBN228THAVN SOTO CANO HO//AVN-AMO//
:CDR160TH SOAR FT CAMPBELL KY//AOAV-SI//
:CDRBGAD RICHMOND KY//SIOBG-GC//
:CDRCBDCOM ABERDEEN PROVING GROUND MD//AMSCB-OP/OPA//
:CDRUSAGAPG ABERDEEN PROVING GROUND MD//STEAP-PF-V//
:NAVTESTPILOTSCH PATUXENT RIVER MD//55TP90A//
:NAVTESTWINGLANT PATUXENT RIVER MD//55TW91A/55TW96A/
:    55TP01A//
:RAYTHEON RANGE SYSTEMS ENGINEERING KWAJALEIN MH//PAT2//
:CDR WHITE SANDS MISSILE RANGE NM//STEWS-NRS-AA-MQA//
:USCS CNAC OKLAHOMA CITY OK//AMI//
:CDRDPG DUGWAY UT//STEDP-AVN//
:USDOCO LANDSOUTHEAST IZMIR TU//AV//
:CDROSAC WESTERN REGION FT HOOD TX//ANAV-WR//
:DPRO BELL HELICOPTER FORT WORTH TX//DCMDS-RBOB/RBP//
:CDROSAC FT BELVOIR VA//OSAC-OS/OSAC-CM//
INFO
:TSM ATK HEL FT RUCKER AL//ATZQ-TSM-A//
:CDRUSARDSG CANBERRA AS//AMXIP-AS//
:129RQG MOFFETT FLD CA//MAQ//
:129RQS MOFFETT FLD CA//DOV//
:HSL FOUR ONE NORTH ISLAND CA
:HQAFSPC PETERSON AFB CO//LGM//
:CDRMDW WASHINGTON DC//ANLG-LS//
:FAA NATIONAL HQ WASHINGTON DC//AIR-100//
:FBI WASHINGTON DC//PASS TO AVIATION SUPERVISOR//
:HQ USAF WASHINGTON DC//AQQU//
:SEC STATE WASHINGTON DC//NEA/MFO//
:US CUSTOMS SERVICE WASHINGTON DC//AVIATION
:    OPERATIONS//
:41RQS PATRICK AFB FL//CC//
:301RQS PATRICK AFB FL//SE//
:16OG HURLBURT FIELD FL//CC//
:AFSOC HURLBURT FIELD FL//DOT/DOVR/LGMA/SE//
:CDR AMC EUROPE SECKENHEIM GE//AMXEU-L-AAH-MFT-E//
:HQ PACAF HICKAM AFB HI//DO/LGM//
:NAVSURFWARCENDIV CRANE IN//80PM1/805/8052//
:HQ AMC SCOTT AFB IL//LG/LGF/LGQ/DO/DOT/DOV/DOX//
:33RQS KADENA AB JA//DO/LG//
:CDR FT BRAGG NC//AFZA-GT-OM//
:48RQS HOLLOMAN AFB NM//MA//
:66RQS NELLIS AFB NV//MA//
:CUSALAO FT BLISS TX//AMXLA-T-BL/DEPT OF JUSTICE
:    INS BORDER PATROL//
:304RQS PORTLAND IAP OR//SE//
:DIR OTSA FT BLISS TX//CSTE-OT//
:CDRIIICORPS FT HOOD TX//SFAE-AV-AAH-MFT-H//
:CDRUSARDSG LONDON UK//AMXSN-UK-SE//
:PROJ MGR NVEO FT BELVOIR VA//SFAE-IEW-NV//
:COMNAVSAFCEN NORFOLK VA//113/111/122//
:PMSW VHFS WARRENTON VA//SFAE-IEW-SG//
XMT
:ODC CANBERRA AS
:USDAO DHAKA BG
:USDAO RANGOON BM
:USCINCPAC REP PHNOM PENH CB
:USDAO COLOMBO CE
:USDAO SUVA FJ
:OMADP JAKARTA ID
:DSA NEW DELHI IN
:AMEMBASSY ANTANANARIVO MA
:AMEMBASSY PORT LOUIS
:SAO KUALA LUMPUR MY
:AMEMBASSY KATHMANDU NP//POL-MIL//
ACCT
:
TEXT
:UNCLAS
THIS IS PART 1 OF 2
SUBJECT - AVIATION SAFETY ACTION MESSAGE, MAINTENANCE MANDATORY,
RCS CSGLD-1860(R1), ALL U.S. ARMY AIRCRAFT, REVISION TO UPDATED
INFORMATION ON NIGHT VISION GOGGLES (GEN97-ASAM-04) (TB 1-1500-
346-20 WILL SUPERSEDE THIS MESSAGE, TB 1-1500-346-20, DTD 26 JAN
96. TB 1-1500-346-20 IS EFFECTIVE UNTIL RESCINDED OR SUPERSEDED).
NOTE - THIS IS AN AVIATION SAFETY ACTION MESSAGE 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 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
RETRANSMISSION TO COMMANDER, ATCOM, ATTN - AMSAT-R-X (SOF
COMPLIANCE OFFICER).
1.  PRIORITY CLASSIFICATION - N/A.
2.  TASK/INSPECTION SUSPENSE DATE - N/A.
3.  REPORTING COMPLIANCE SUSPENSE DATE - N/A.
4.  SUMMARY OF PROBLEM -
     A.  THE PURPOSE OF THIS MESSAGE IS TO PROVIDE CONSOLIDATED
AND UPDATED INFORMATION ON AVIATION NVG MESSAGES.  IT IS NOT
INTENDED TO REPLACE ANY PUBLICATION. THIS MESSAGE DOES NOT
ADDRESS NVGS USED FOR GROUND OPERATIONS.
         B.  THE UPDATED INFORMATION IN THIS MESSAGE IS
ORGANIZED INTO TWO PARTS AS FOLLOWS:
PARAGRAPH         SUBJECT
8A   NVG MAINTENANCE TRAINING
8B   GM-6 GOGGLES
8C   COMMERCIAL NVGS
8D   AN/AVS-6 (ANVIS)
8E   AN/AVS-7 (ANVIS HUD)
8F   BATTERY AND POWER PACK ASSEMBLY (BATTERY PACK)
8G   TEST SETS
8H   MODIFICATION WORK ORDERS (MWO)
8I   LIGHTING
8J   PHYSICAL SECURITY
8K   MISCELLANEOUS INFORMATION
       C.  THIS MESSAGE AND THE FOLLOWING MESSAGES/TBS ARE
CURRENT AND SHALL BE COMPLIED WITH UNTIL EXPIRED AS NOTED:
(1)  CDRUSAAVNC MESSAGE 032330Z JAN 91, SUBJECT - NIGHT VISION
GOGGLE SCANNING AND CREW COORDINATION ERRORS. THIS MESSAGE
EXPIRES WHEN THE INFORMATION IS INCLUDED IN THE NEXT REVISION OF
TC 1-204, DTD DEC 88.
          (2)  CDRATCOM MESSAGE 052130Z NOV 92, SUBJECT
CORRECTION OF OBVIOUS ERRORS IN DA PAM 738-751, 15 JUN 92, USERS
MANUAL FOR THE ARMY MAINTENANCE MANAGEMENT SYSTEM. THIS MESSAGE
WILL EXPIRE WITH THE UPDATE TO DA PAM 738-751.
          (3)  TB 1-1500-350-30, 26 FEB 96, SUBJECT - USE OF DUAL
VISOR ON SPH-4B AVIATOR'S HELMET AND RELATED INFORMATION.  THIS
TB IS EFFECTIVE UNTIL RESCINDED OR SUPERSEDED.
          (4)  TB 1-1500-348-30, SUBJECT - AVIATION NIGHT VISION
GOGGLE MAINTENANCE DOCUMENTATION, DTD 29 DEC 95. THIS TB IS
EFFECTIVE UNTIL RESCINDED OR SUPERSEDED.   THIS INFORMATION WILL
BE INCLUDED IN NEXT UPDATE OF DA PAM 738751.
          (5)  CDRUSAAVNC MESSAGE 191537Z FEB 97, SUBJECT
AVIATOR'S NIGHT VISION IMAGING SYSTEM (ANVIS) MAINTENANCE
QUALIFICATION TRAINING GUIDANCE.
           (6)  CDRATCOM MESSAGE SUBJECT - MAINTENANCE
INFORMATION MESSAGE DTG 130229Z SEP 96, AN/AVS-7 ANVIS/HUD 4RNAD-
5025.
5.  END ITEMS - THIS TB COVERS THE AN/AVS-6, AN/AVS-7, AND GM-6,
AS WELL AS NECESSARY SUPPORT EQUIPMENT.
6.  ASSEMBLY COMPONENTS TO BE INSPECTED - N/A.
7.  PARTS TO BE INSPECTED - N/A.
8.  NVG PROCEDURES/INFORMATION -
     A.  NVG MAINTENANCE TRAINING - NEW EQUIPMENT TRAINING (NET)
FOR THE AN/AVS-6 ANVIS HAS BEEN COMPLETED. MAINTENANCE TRAINING
PROCEDURES FOR AN/AVS-6 SHALL BE
ACCOMPLISHED IAW MESSAGE IN PARA 3 AND 4 (CDRUSAAVNC MESSAGE
191537Z FEB 97). DUE TO THE RAPID RESTRUCTURING OF THE ARMY,
QUALIFIED PERSONNEL (WHO HAVE TRAINING DOCUMENTED FROM APPROVED
SOURCES) RETAIN THEIR QUALIFICATION TO REPAIR/SERVICE/MAINTAIN
AN/AVS-6 ANVIS REGARDLESS OF MOS REVISIONS.  THE COMMANDER MUST
STILL DESIGNATE THAT INDIVIDUAL AS THE ANVIS MAINTAINER IAW AR
750-1.
     B.  GM-6 NVGS - GM-6 NIGHT VISION GOGGLES ARE NO LONGER
AUTHORIZED FOR AVIATION USE.  GM-6 NIGHT VISION GOGGLES SHOULD BE
TURNED IN IAW SUPPLY PROCEDURES.  CONTACT YOUR LOCAL CECOM
AVIONICS LAR, OR MR. STEVE BORMAN, DSN 2364064/2814, OR
COMMERCIAL 910/396-4064/2814 FOR ASSISTANCE.
     C.  COMMERCIAL NVGS - COMMERCIAL NVGS, (INCLUDING
PROCURED GSA CATALOGUED GOGGLES AND SPARE PARTS) ARE NOT
AUTHORIZED FOR AVIATION USE.  THESE NONSTANDARD NVGS AND PARTS
HAVE NOT BEEN ADEQUATELY TESTED FOR MILITARY USE (ELECTROMAGNETIC
INTERFERENCE, ETC).
     D.  AN/AVS-6 (ANVIS) -
         (1)  NEWLY FIELDED ANVIS THAT FAIL EITHER THE SERVICE
UPON RECEIPT OF MATERIAL INSPECTION OR FAIL PRIOR TO THE
EXPIRATION OF THE WARRANTY MUST BE REPORTED ON A PRODUCT QUALITY
DEFICIENCY REPORT (PQDR), SF 368.  THE PQDR MUST BE PROCESSED
THROUGH THE LOCAL CECOM AVIONICS LAR AND TRANSMITTED TO CDR,
CECOM.  THIS WILL ENSURE THE UNITSUBMITTING THE PQDR WILL RECEIVE
CREDIT FOR THAT ANVIS.
         (2)  MODIFICATION OF AN/AVS-6 (V2) (NSN 5855-01-
138-4748) BINOCULARS TO AN/AVS-6 (V1) (NSN 5855-01-138-4749)
VERSION BY REPLACEMENT OF THE PAS IS NOT AUTHORIZED.
          (3)  INSTALLATION OF THE LIGHT INTERFERENCE FILTER
(LIF), NSN 5855-01-379-1410, ON AN/AVS-6 IS MANDATORY, IAW
PROCEDURES CONTAINED IN PAR 2-12, AND FIGURE 2-24 OF TM 115855-
263-10.  AN/AVS-6 WITHOUT THIS MODIFICATION WILL NOT BE USED.
UNIT MAINTAINERS SHALL DOCUMENT THE INSTALLATION OF THE NEW LIF
ON DA FORM 2408-15, HISTORICAL RECORD. POC IS GLEN NOWAK, DSN 654-
3453 OR COMMERCIAL 703/704-3453.
          (4)  NEW ANVIS SYSTEMS THAT ARE CURRENTLY BEING
MANUFACTURED HAVE ENHANCEMENTS WHICH INCLUDE A NEW 25 MM
EYEPIECE, DUAL INTERPUPILLARY DISTANCE (IPD) ADJUSTMENTS,
INCREASED FORE/AFT ADJUSTMENT, INCREASED TILT AND IMPROVED TUBE
PERFORMANCE.  THESE ENHANCED SYSTEMS CAN BE MIXED IN THE SAME
COCKPIT AS OLDER VERSION ANVIS SYSTEMS OR ANVIS SYSTEMS THAT HAVE
BEEN UPGRADED WITH ANY OF THE ENHANCEMENTS.
          (5)  THE ANVIS EYEPIECE TUBE RETAINER, NSN 5855-01151-
4226, MATERIAL HAS BEEN CHANGED FROM PLASTIC TO METAL. BOTH
MATERIALS ARE APPROVED FOR USE.
          (6)  A NEW AN/AVS-6 VISOR HOUSING IS PRE-DRILLED TO
ACCEPT THE ANVIS MOUNT.  THE MOUNTING KIT, ANVIS (NSN 5340-01-390-
8872) IS SHOWN IN TM 1-8415-216-12&P.  THE MOUNTING SCREWS, P/N
MS51957-12, FURNISHED WITH THE KIT MUST BE USED BECAUSE THE OLD
FLUSH HEAD SCREWS COULD SCRATCH THE VISORS.
     E.   AN/AVS-7 (ANVIS HUD) -
          (1) THE ANVIS/HUD OPTICAL UNIT SUPPORT CLAMPS, WHEN
INSTALLED ON THE ANVIS MONOCULAR, ARE PERMANENT.  UNIT
MAINTAINERS SHALL DOCUMENT THE INSTALLATION OF THE UNIT SUPPORT
CLAMPS ON DA FORM 2408-15, HISTORICAL RECORD.
          (2) UNITS ARE AUTHORIZED TO MODIFY THE FOAM INSERT OF
THE ANVIS CARRYING CASE TO ACCEPT ANVIS WITH OPTICAL UNIT SUPPORT
CLAMP INSTALLED.
          (3) UNITS REQUIRING ADDITIONAL ANVIS HUD PARTS CAN
ORDER THEM USING THE FOLLOWING NSNS:
LEFT STRAP (RETAINING), P/N 125268, NSN 5340-01-393-9379 RIGHT
STRAP, P/N 125267-001, NSN 5340-01-393-9378
BOTTOM CLAMP (LEFT AND RIGHT), P/N 125269-001, NSN 5340-01393-
9380 SCREW, CAP (SHORT), P/N MS 16995-2B, NSN 5305-00409-4438,
SCREW, CAP (LONG), P/N MS 16995-3B, NSN 5305-00470-5988, WRENCH,
HEX, 5/64 INCH NSN 5120-00-729-6392.
          (4)  INSTALLATION OF THE ANVIS/HUD DU REQUIRES REMOVAL
OF THE STANDARD ANVIS NECK CORD ASSEMBLY, TO FACILITATE EGRESS
FROM THE AIRCRAFT IN THE EVENT OF AN EMERGENCY.  AN ADDITIONAL
(REMOVABLE) NECK CORD ASSEMBLY IS PROVIDED WITH THE ANVIS HUD.
THIS CORD MUST BE REMOVED FROM THE ANVIS WHEN THE ANVIS/HUD IS
INSTALLED, AND MUST BE REPLACED PRIOR TO FLYING WITH THE BASIC
ANVIS.  THE ASSEMBLY CONSISTS OF A NECK CORD (STRAP, WEBBING),
P/N 125302, NSN 5340-01-396-1746 AND BARREL FASTENER (CYLINDER),
P/N 125301, NSN 5340-01-393-4890. THIS NECK CORD CAN ALSO BE USED
TO REPLACE THE LANYARD USED ON ANY STANDARD ANVIS SYSTEM.
                           WARNING:
  IT HAS BEEN REPORTED THAT NYLON CORDS/BOOT LACES HAVE BEEN USED
AS ANVIS NECK CORDS.  USE OF ANY NYLON CORD AS AN ANVIS NECK CORD
IS UNAUTHORIZED, AS IT MAY PRESENT A SEVERE BURNING HAZARD IN THE
EVENT OF A FIRE.
          (5)  CURRENT TECHNICAL MANUALS SUPPORTING THE AN/AVS-7
(ANVIS HUD) ARE AS FOLLOWS:
               (A)  TM 11-5855-300-10, OPERATORS MANUAL FOR HEADS
UP DISPLAY AN/AVS-7 (NSN 5855-01-350-0349), DTD 1 AUG 94
               (B)  TM 11-5855-300-23 AND P, AVIATION UNIT

AND INTERMEDIATE MAINTENANCE MANUAL INCLUDING REPAIR PARTS AND
SPECIAL TOOLS LIST, HEADS UP DISPLAY AN/AVS-7 (NSN 585501-350-
0349), DTD 1 DEC 94.
       F.  BATTERY AND POWER PACK ASSEMBLY (BATTERY PACK)
INFORMATION -
          (1)  ANVIS CLIP-ON POWER SOURCE - PM NV/RSTA IS IN THE
PROCESS OF PROVIDING, AS INITIAL ISSUE, A NEW POWER SOURCE, WHICH
WILL BE AN ADDITIONAL AUTHORIZED ITEM.  THIS POWER SOURCE,
UTILIZING TWO AA ALKALINE BATTERIES, ALLOWS USERS TO OPERATE THE
ANVIS WITHOUT THE NEED FOR THE AVIATORS HELMET (MOUNT).  THIS
ITEM WILL FACILITATE TESTING WITH THE TS-4348, AND WILL ASSIST
AIRCREW MEMBERS DURING ESCAPE & EVASION.  THE BATTERIES SHOULD BE
TESTED EVERY SIX MONTHS.
          (2)  BATTERIES AUTHORIZED FOR ANVIS ARE BA-5567/U
LITHIUM BATTERY AND (1.5 VOLT) AA ALKALINE BATTERY.  NO OTHER
BATTERIES (NICAD, MERCURY, CARBON, ANY RECHARGEABLE, ETC) ARE
AUTHORIZED FOR USE WITH THE ANVIS.  THE NSN FOR THE (1.5 VOLT) AA
ALKALINE BATTERIES HAVE CHANGED. THE AA ALKALINE BATTERIES CAN BE
ORDERED IN PACKAGES OF 24 EACH
UNDER THE FOLLOWING NSNS FOR THE QUANTITY DESIRED:  NSN 613500-
985-7845 FOR QTYS 1-36, NSN 6135-01-382-9206 FOR QTYS 3774, NSN
6135-01-382-9208 FOR QTYS 75 AND UP.  THE ARMY RESEARCH
LABORATORY POINT OF CONTACT IS MR. FEE LEUNG AT COMMERCIAL
908/427-4735 OR DSN 987-4735.
                         NOTE
AA LITHIUM BATTERIES (3.6 VOLTS), NSN 6135-01-301-8776 ARE NOT
AUTHORIZED.
          (3)  AUTHORIZED REPAIR OF ANVIS BATTERY PACK AND CAP
LANYARDS ASSEMBLY IS LIMITED TO THE REPAIR OF THE SHIELDED CABLE,
IAW TB 1-1500-350-30.  NO OTHER MAINTENANCE IS AUTHORIZED.
     G.  TEST SETS -
          (1)  TS-4348/UV AND TS-3895A/UV TEST SETS REQUIRE
CALIBRATION EVERY 12 MONTHS.  CALIBRATIONS ARE TRACKED WITH DA
LABEL 80 THAT IS ATTACHED TO THE BODY.  UPON INITIAL ISSUE, TURN
THE ITEMS INTO LOCAL TMDE FOR CALIBRATION (PRIOR TO USE).
          (2)  TS-3895/UV (NOT THE "A" VERSION) TEST SET DOES NOT
REQUIRE CALIBRATION. DA LABEL 80 MUST BE STAMPED WITH "CNR"
(CALIBRATION NOT REQUIRED) AND AFFIXED TO THE MAIN PLATE.
          (3)  FOR MAINTENANCE GUIDANCE OR CALIBRATION ON TS
3895A/UV,  TS-3895/UV, OR TS-4348/UV CONTACT U.S. ARMY TMDE
ACTIVITY, AMXTM-LM-AMR, MR. ED COPELAND AT DSN 788-2698 OR
COMMERCIAL 205/842-2698, FAX 205/876-3070 OR PM-NVEO, GLEN NOWAK
AT DSN 654-3453, COMMERCIAL 703/704-3453, FAX 703/7043449.
                         NOTE
DURING CREWMEMBER PRE-OPERATIONAL CHECKS, THE TS-4348/UV MAY BE
UTILIZED AS AN OPTIONAL CHECK, TO ASSIST IN EVALUATING IMAGE
INTENSIFIER RESOLUTION AND CLARITY.  OPERATE THE TEST SET IAW TM
11-5855-238-10 (DTD 15 MAY 93), TM 11-5855-263-10 (DTD 1 MAR 94)
OR TM 11-5855-299-12 AND P (DTD 15 MAR 92).
          (4)  TS-3895A/UV AND TS-3895/UV REQUIRE AN ANNUAL
OPTICAL CHECK USING COLLIMATION ATTACHMENT AND DIOPTER SCOPE IAW
TM 11-5855-264-14.  DOCUMENT THE ANNUAL INSPECTION IAW DA PAM 738-
750 AND SCHEDULE THE ANNUAL INSPECTION WITH A DD FORM 314.
          (5)  TM 11-5855-264-14, PAGE 5-7, ITEM NUMBER 3, TABLE
5-1:  DELETE THE VOLTAGE VERIFICATION CHECK ONLY FOR THE TS-
3895A/UV FROM THE AVIM, DS/GS ANNUAL MAINTENANCE SCHEDULE.
          (6)  THE USE OF THE RADIOMETRIC TEST SET
(INTERFEROMETER, NSN 5860-01-178-5837) AFTER REPLACING THE TS-
3895A/UV PC BOARD BOX ASSEMBLY OR THE RETICLE LENS
ASSEMBLY AT AVIM, DS/GS IS NO LONGER REQUIRED.  AFTER REPLACING
THESE ITEMS, SEND THE TS-3895A/UV TO TMDE FOR CALIBRATION.
          (7)  THE CORRECT NSN AND P/N FOR THE TS-3895A, GOGGLE
CONNECTOR CABLE (POWER), IS NSN 5855-01-151-4212, AND P/N
5003265.
          (8)  CECOM IS CONDUCTING A RETROFIT PROGRAM TO REPLACE
THE TS-3895/UV, NSN 6625-01-134-7146  WITH THE TS3895A/UV, 6625-
01-301-6894.  REPAIR PARTS ARE NO LONGER AVAILABLE FOR THE TS-
3895/UV. CONTACT CECOM ITEM MANAGER MR. CHRISTOPHER DELOATCH, DSN
992-4797/98 OR COMMERCIAL 908/532-4797/98.  EMAIL IS DELOATCH (AT
SIGN) MME-V4 (AT SIGN) USACECOMDMM.
     H.   MODIFICATION WORK ORDERS (MWO) -
           (1)  THE FOLLOWING MWOS MUST BE APPLIED TO
AIRCRAFT PRIOR TO NVG OPERATIONS. (AIRCRAFT WITH NVG COMPATIBLE
COMPONENTS THAT HAVE BEEN REPLACED SINCE INITIAL APPLICATION OF
MWO AND DO NOT MEET INTERIOR LIGHTING REQUIREMENTS MUST ELIMINATE
THE EFFECTS OF RED OR WHITE LIGHTING IAW PARA 8I(1)).
               (A)  UH-60A AND UH-60L - AIRCRAFT S/N 8524462 AND
SUBSEQUENT ARE AUTHORIZED FOR NVG USE WHEN DELIVERED WITH
EXCEPTIONS LISTED BELOW.  AIRCRAFT S/N 8524461 AND PRIOR ARE
REQUIRED TO HAVE MWO 55-1520-237-50-20 INSTALLED FOR NVG USE.
AIRCRAFT 85-24745 THRU 85-24750, 8525511, AND 85-25512 ARE
REQUIRED TO HAVE MWO 55-1520-237-5020 INSTALLED FOR NVG USE. (ALL
AIRCRAFT ARE REQUIRED TO COMPLY WITH UH-60-94-ASAM-01.  RED
LIGHTING FROM PDU AND CDU IS FILTERED AND NVG COMPATIBLE.)
               (B)  UH-1H/V - CONCURRENT INSTALLATION OF MWO
551520-210-50-7 AND MWO 55-1520-210-50-11 IS REQUIRED FOR NVG
USE.  OTHERWISE, INSTALLATION OF MWO 55-1520-210-50-10 OR MWO 55-
1520-210-50-12 IS REQUIRED FOR NVG USE.  AIRCRAFT

ARE ALSO REQUIRED TO COMPLY WITH ASAM UH-1-97-ASAM-02 WHICH
REMOVES OBSCURING PAINT OR TAPE APPLIED BY THE AFOREMENTIONED
MWOS.
                         NOTE
UH-1H/V AIRCRAFT WHICH HAVE THE AN/ARC-186 RADIO AND/OR THE
AN/ARC-164 UHF RADIO INSTALLED MUST HAVE THE LIGHTING TO THE
CONTROL DISABLED UNTIL NVG COMPATIBLE LIGHTING FOR THE CONTROL IS
AVAILABLE.  PROCEDURES FOR THIS IS AS FOLLOWS:
                    (1)  IF THE C-10604/ARC-186 OR THE C-
10606/ARC-186 IS INSTALLED AS A RESULT OF MWO 55-1520-210-5014,
DISABLE THE CONTROL HEAD LIGHTING WIRE BY REMOVING TERMINAL LUG
FOR WIRE NUMBER ARC186-19A22 FROM TB12, PIN 3. CAP AND STOW WIRE
FOR FUTURE USE.  THIS WIRE MAY BE RECONNECTED WHEN THE CONTROL IS
MODIFIED WITH NVG COMPATIBLE LIGHTING.
                    (2)  IF THE C-10604 OR THE C-10606 IS NOT
INSTALLED VIA USE OF AN MWO (I.E. AN/ARC-186 RADIO IS LOCATED IN
THE REAR OF THE AIRCRAFT, RIGHT SIDE, ON TOP OF THE PREVIOUSLY
INSTALLED RT-857/ARC-134 RADIO MOUNT), DISABLE THE CONTROL HEAD
WIRE BY REMOVING TERMINAL LUG FOR WIRE NUMBER ARC134-35A20 FROM
TB12, PIN 2.  CAP AND STOW THE WIRE FOR FUTURE USE.  THIS WIRE
MAY BE RECONNECTED WHEN THE CONTROL IS MODIFIED WITH NVG
COMPATIBLE LIGHTING.
                    (3)  IF THE RT-1354/ARC-186 (RED LIGHTING) IS
INSTALLED IN LIEU OF THE AN/ARC-115, THE LIGHTING MUST BE
DISABLED BY CUTTING WIRE NUMBER ARC 1153A22 GOING TO PIN C OF THE
AN/ARC-115 RADIO CONNECTOR P1151. CAP AND STOW THE WIRE FOR
FUTURE USE.  THIS WIRE MAY BE RECONNECTED WHEN THE RADIO IS
MODIFIED WITH NVG COMPATIBLE LIGHTING.
                    (4)  IF THE AN/ARC-51BX UHF RADIO OR THE C-
9682B/ARC-164 HAVEQUICK CONTROL IS INSTALLED, DISABLE LIGHTING
WIRE BY CUTTING WIRE NO. L122A20 GOING TO PIN P OF
THE C-6287ARC-51BX OR C-9682B/ARC-164 CONTROL CONNECTOR N0.
P3801.
                    (5)  IF THE C-9682C/ARC-164 HAVEQUICK CONTROL
OR THE C-11721/ARC-164 CONTROL IS INSTALLED, THE LIGHTING MAY BE
ENABLED BY RECONNECTING WIRE NO. L122A20 GOING TO PIN P OF RADIO
CONNECTOR P3801.
                    (6)  IF THE PANEL MOUNT ARC 164 RADIO(RT
1518C) IS INSTALLED WITH NVG COMPATIBLE LIGHTING, LIGHTING TO THE
RADIO MAY BE ACTIVATED BY COMPLETING THE CONNECTION OF WIRE NO.
ARC 164-3A22 FROM THE ARC 164 RADIO CONNECTOR NO. P1, PIN C TO
TB12, PIN 1.  IF THE LIGHTING IS NOT NVG COMPATIBLE, THE LIGHING
MUST BE DISABLED BY DISCONNECTING WIRE NO. ARC 164-3A22 FROM TB
12, PIN 1.  SEE PARAGRAPH H2 BELOW FOR AVIONICS APPROVED FOR NVG
USE.
                    (7)  USE OF THE ID-2192A/ARN-124 INDICATOR IS
AUTHORIZED FOR NVG MISSIONS IN THE UH-1H/V AIRCRAFT.
               (C)  OH-58A - MWO 55-1520-228-50-31 IS REQUIRED TO
BE INSTALLED FOR NVG USE.
               (D)  OH-58C - MWO 55-1520-228-50-32 IS REQUIRED TO
BE INSTALLED FOR NVG USE.
               (E)  OH-58D KIOWA WARRIOR - ALL AIRCRAFT ARE
ACCEPTABLE/SAFE FOR NVG USE FROM PRODUCTION AND RETROFIT LINES.
USE OF THE ANVIS DISPLAY SYMBOLOGY SYSTEM OPTICAL DISPLAY
ASSEMBLY IS AUTHORIZED. NO MWO IS REQUIRED.
               (F)  CH-47D - CH-47D AIRCRAFT ARE AUTHORIZED FOR
NVG USE WHEN DELIVERED WITH THE EXCEPTION OF AIRCRAFT S/N 84-
24187 AND PRIOR WHICH ARE REQUIRED TO HAVE MWO 551520-240-50-3
INSTALLED.
                         NOTE
AIRCRAFT S/N 81-23381 THRU 81-23384 ARE NOT AUTHORIZED FOR NVG
USE.
               (G)  AH-1S - MWO 55-1520-234-50-1 AND MWO 55-1520-
234-50-4 ARE REQUIRED TO BE INSTALLED FOR NVG USE.            (H)
AH-1E, F AND P - MWO 55-1520-236-50-4
AND MWO 55-1520-236-50-5 ARE REQUIRED TO BE INSTALLED FOR NVG
USE.
            (2)  UPDATE ON ANVIS BLUE-GREEN LIGHTING
UPGRADE/MODIFICATION KITS FOR AVIONIC COMPONENTS


:UNCLAS
PART 2 OF 2
               (A)  MWOS HAVE BEEN APPROVED AND PROCUREMENT
ACTION INITIATED FOR ANVIS LIGHTING UPGRADE/MODIFICATION LIGHTING
KITS ON AVIONICS COMPONENTS LISTED BELOW.  ALL KITS WILL BE
AVAILABLE AFTER 1 APR 96, THROUGH THE NORMAL REQUISITIONING
PROCESS.  LISTED ITEMS HAVE BEEN IDENTIFIED AS THE PRIMARY
AVIONICS COMPONENTS REQUIRING ANVIS BLUEGREEN LIGHTING
MODIFICATION/UPGRADE:
AVIONICS COMPONENT/LRU  ANVIS LIGHTING       ESTIMATED MANHOURS
                         MOD KIT NSN     (LOCATION FOR KIT
INSTALLATION)
CP-1252/ASN-128          N/A            10 (DEPOT ONLY)
DOPPLER RADAR
AN/ARC-164          1680-01-342-6491    3 (AVIM) UHF/AM
RADIO
RT-1354/ARC-186     1680-01-342-6490    3 (AVIM) VHF/AM
RADIO
C-10604/ARC-186     1680-01-342-6492    3 (AVIM) VHF/AM
RADIO
C-10606/ARC-186     5821-01-209-0109    3 (AVIM) VHF/AM
RADIO CONTROL
RT-1285/APX-100     1680-01-342-6489    6 (AVIM)
TRANSPONDER/IFF
RT-1296/APX-100     1680-01-342-6488    6 (AVIM)
TRANSPONDER/IFF
C-10533/APX-100     1680-01-342-6487    6 (AVIM)
TRANSPONDER/IFF
AN/ARC-114 VHF/FM   1680-01-342-6494    3 (AVIM) RADIO
ID-2192/ARN-124 DME 1680-01-407-4440    3 (AVIM)
C-7392A/ARN-89 ADF  6210-01-230-0531    1/2 (AVUM)
C-10048/ARN-123 VOR/ILS  N/A            5 (DEPOT ONLY)
C-6533/ARC INTERCOM 6210-01-230-9106    AVUM/AVIM
(SEE TM)
               (B)  WITH THE EXCEPTION OF THE CP-1252/ASN128, ALL
ANVIS LIGHTING UPGRADE/MODIFICATION KIT MWOS CAN BE INSTALLED AT
THE AVIM LEVEL.  ALL ASSETS FOR THE ABOVE COMPONENTS/LRUS ARE NOW
BEING ISSUED WITH NVG COMPATIBLE LIGHTING.
               (C)  THE C7392A/ARN-89 ADF (NSN 6210-01-2300531,
P/N EGD-0929-1) AND THE C-6533/ARC INTERCOM (NSN 621001-230-3109,
P/N EGD-0929-5) REQUIRE ONLY A FILTER CHANGE TO BECOME NVG
COMPATIBLE.  THIS MODIFICATION CAN BE DONE AT THE AVUM/AVIM LEVEL
IAW THE APPLICABLE TM.
               (D)  CECOM ANVIS LIGHTING KIT POC IS MR. ROBERT
MANSFIELD, DSN 992-3800, COMMERCIAL 908/532-3800, EMAIL MANSFIEL
(AT SIGN) DOIM6.MONMOUTH.ARMY.MIL OR MR. DWIGHT DEATHERAGE, DSN
992-1626, COMMERCIAL 908/532-1626, EMAIL DEATHERA (AT SIGN)
DOIM6.MONMOUTH.ARMY.MIL.
               (E)  CECOM POC FOR ANVIS LIGHTING ENGINEERING
SUPPORT OR DATA IS MR. JOHN SANTAMATIA, DSN 992- 3652, COMMERCIAL
908/532-3652, EMAIL SANTAMR (AT SIGN) DOIM6.MONMOUTH.ARMY.MIL.
     I.  LIGHTING -
           (1)  RED OR WHITE LIGHTING -  RED OR WHITE
LIGHTING OF ANY RADIO CONTROL, SWITCH PANEL, INSTRUMENT, MASTER
CAUTION LIGHT, ETC. MUST BE TAPED, FILTERED, TURNED OFF, ETC. TO
ELIMINATE EFFECTS OF RED OR WHITE LIGHTING PRIOR TO CONDUCTING
NVG OPERATIONS.
                         NOTE
EFFECTS OF LIGHTING FROM NONSTANDARD EQUIPMENT MUST BE ELIMINATED
IAW THE ABOVE PARAGRAPH PRIOR TO CONDUCTING NVG
OPERATIONS, UNLESS THE APPLICABLE AIRWORTHINESS RELEASE (AWR)
CLEARLY AUTHORIZES THE USE OF LIGHTING FROM NONSTANDARD EQUIPMENT
DURING NVG OPERATIONS.
          (2)  SUPPLEMENTAL LIGHTING -
               (A)  SUPPLEMENTAL LIGHTING IS DEFINED AS
ADDITIONAL INTERIOR LIGHTING WHICH MAY CONSIST OF LIP LIGHTS (MIC
LIGHTS), FINGER LIGHTS, FLASHLIGHTS WITH FILTERS AND OTHER
SIMILAR DEVICES.  LIP/MIC LIGHTS AND FINGER LIGHTS DO NOT FULFILL
THE FLASHLIGHT REQUIREMENT OF AR 95-1.
               (B)  NEW ITEMS - PM SOLDIER HAS DEVELOPED, TESTED
AND APPROVED THE FOLLOWING NEW ITEMS :
FINGER LIGHT, NSN 6230-01-357-2175
MICLIGHT, NSN 6240-01-362-4902
FLASHLIGHT FILTER, (1.715 INCH), NSN 6230-01-369-1658
FLASHLIGHT FILTER, (1 INCH), NSN 6230-01-369-1659
FLASHLIGHT FILTER, (0.895 INCH), NSN 6230-01-369-1657
               (C)   IF THE ABOVE ARE NOT AVAILABLE, THE USE
OF SUPPLEMENTAL LIGHTING WHICH PASSES THE EVALUATION OF PARAGRAPH
8I(2)(D) BELOW IS AUTHORIZED. THE SPECIFIC LIGHTING
CONFIGURATIONS AUTHORIZED BY UNIT COMMANDERS MUST BE DEFINED IN
UNIT SOPS. ADDITIONALLY, UNIT COMMANDERS MUST ENSURE CREWMEMBERS
RECEIVE INSTRUCTION IN THE USE OF AUTHORIZED SUPPLEMENTAL
LIGHTING INCLUDING FLASHLIGHT FILTERS. AS A MINIMUM, THE
FOLLOWING TRAINING MUST BE ADDRESSED AND DOCUMENTED:
                    (1)  OPERATION AND USE OF LIGHTING
                    (2)  CAUTIONS/WARNINGS ASSOCIATED WITH THE
LIGHTING
                    (3)  DEMONSTRATE DEGRADATION OF NVG
PERFORMANCE CAUSED BY SUPPLEMENTARY LIGHTS
                    (4)  VERIFY KNOWLEDGE OF USE.
                         NOTE
FLASHLIGHTS WITH RED OR WHITE LIGHT MAY NOT BE USED EXCEPT
FOR GROUND OPERATIONS OR IN THE CARGO COMPARTMENT OF UH-1, UH-60
OR CH-47 AIRCRAFT, AT THE DISCRETION OF THE PILOT IN COMMAND.
          (D)  SUPPLEMENTAL LIGHTING DEGRADATION EVALUATION -
A METHOD FOR EVALUATING THE EFFECTS OF SUPPLEMENTAL
LIGHTING WITH ANVIS IS AS FOLLOWS:
                    (1)  AT NIGHT, IN AN AIRCRAFT LOCATED IN AN
AREA OF LOW AMBIENT LIGHT (LANDING ZONE, ETC), WITH INTERIOR
LIGHTING SET FOR NVG OPERATIONS, AND WITH ANVIS PREPARED FOR USE,
POSITION A REFLECTIVE MATERIAL (MAP SHEET, NOTE CARD, VINYL
CHECKLIST, ETC.) AT READING DISTANCE FROM YOUR EYES
(APPROXIMATELY 12 TO 18 INCHES).
                    (2)  SHINE THE SUPPLEMENTAL LIGHT ONTO THE
MATERIAL.  WITH THE UNAIDED EYE, LOOK AT THE RESULTANT REFLECTION
CAST ON THE WINDSCREEN.
                    (3)  OBSERVE THIS SAME REFLECTION THROUGH THE
ANVIS.  AN ACCEPTABLE SUPPLEMENTAL LIGHT SOURCE WILL ALLOW ANVIS
AIDED VISION THROUGH THE REFLECTION.  THE REFLECTION CAN EVEN
DISAPPEAR.
                    (4)  IF THE REFLECTION BLOCKS ANVIS AIDED
VISION, THIS LIGHT SOURCE SHOULD BE DEEMED UNACCEPTABLE.
     F.  LASER POINTERS -
          (1)  THE USE OF LASER POINTERS IN THE COCKPIT OF ARMY
AIRCRAFT IS PROHIBITED.  LASER POINTERS MAY ONLY BE USED IN THE
CARGO COMPARTMENT OF UH-1, UH-60 OR CH-47 AIRCRAFT, AT THE
DISCRETION OF THE PILOT IN COMMAND.  THE PILOT IN COMMAND SHOULD
INCLUDE THE USE OF LASER POINTERS IN THE CREW AND PASSENGER
BRIEFING.
                            WARNING:
USERS SHOULD BE AWARE THAT ANY LASER CAN PERMANENTLY OR
TEMPORARILY DEGRADE THE PERFORMANCE OF NVGS IF USED
IMPROPERLY.  ANY LASER THAT IS NOT A CLASS 1 LASER DEVICE HAS THE
POTENTIAL TO CAUSE DIRECT DAMAGE TO THE EYE. TESTING IS CURRENTLY
BEING ACCOMPLISHED TO ASSIST IN THE  SELECTION AND DEVELOPMENT OF
PROPER OPERATING PROCEDURES FOR SAFELY ALLOWING THE USE OF THESE
DEVICES IN NVG AVIATION OPERATIONS.
          (2)  UNIT COMMANDERS WILL (IF APPLICABLE) DEVELOP SOP'S
REGARDING THE SAFE USE OF LASER POINTERS DURING NVG HELICOPTER
MISSIONS.  GUIDANCE REGARDING HAZARDS ASSOCIATED WITH TACTICAL
LASER POINTERS IS AVAILABLE FROM THE U.S ARMY CENTER FOR HEALTH
PROMOTION AND PREVENTIVE MEDICINE, DSN 5843932 OR COMMERCIAL
410/671-3932 OR EMAIL "MCHBDSL (AT SIGN) AEHA1.APGEA.ARMY.MIL".
GENERAL GUIDANCE REGARDING THE SAFE USE OF LASERS IS AVAILABLE IN
THE FOLLOWING VIDEOTAPES:
               (A)  TVT-20-835, GUIDELINES FOR LASER SAFETY
               (B)  TVT-20-854, SAVPIN 705980DA, LASERS IN
COMBAT AND TRAINING
               (C)  TVT-20-855, SAVPIN 705981DA, LASERS, THE NEW
THREAT.
          (3)  IR BANDPASS FILTERS - THE IR FILTER (PINK LIGHT),
P/N EGD-0931-1 MAY BE INSTALLED ON EITHER THE SINGLE MODE
SEARCHLIGHT OR LANDING LIGHT BASED ON OPERATIONAL REQUIREMENTS AS
DETERMINED BY THE USER.  UNITS ARE AUTHORIZED TO USE THE BULB
WHICH BEST SUITS THEIR OPERATIONAL ENVIRONMENT AND MISSION AS
FOLLOWS:
P/N:       NSN:             VOLTAGE    WATTAGE  CANDLEPOWER
4571      6240-00-690-1094   28.0        150         7,000
4551      6240-00-583-3334   28.0        250        75,000
4553      6240-00-816-4808   28.0        250       300,000
4596      6240-00-577-8450   28.0        250       150,000
4626      6240-00-917-0771   28.0        150         3,000
BEAM SPREAD:
P/N:        HORIZONTAL:          VERTICAL:
4571        80 DEGREES          25 DEGREES
4551        50 DEGREES          10 DEGREES
4553        11 DEGREES          12 DEGREES
4596        11 DEGREES          12 DEGREES
4626        9 DEGREES           40 DEGREES
                         NOTE
MAXIMUM PERMISSIBLE WATTAGE IS 250 WATTS. J.  PHYSICAL SECURITY -
          (1)  UNITS SHOULD USE THE FOLLOWING REFERENCES AND
THEIR LOCAL REQUIREMENTS FOR ANVIS PHYSICAL SECURITY AND
ACCOUNTABILITY:
               (A)  PHYSICAL SECURITY, AR 190-51.
               (B)  UNIT SUPPLY, AR 710-2 AND AR 735-5.
          (2)  FOR FURTHER GUIDANCE, CONTACT THE LOCAL
               PHYSICAL SECURITY MANAGER/OFFICER.
     K.  MISCELLANEOUS INFORMATION -
          (1)  THE LOCK RELEASE BUTTON (SCREW MOUNT
ASSEMBLY) FOR THE VISOR MOUNT MUST BE ORDERED USING P/N MS519573B
(NO NSN ASSIGNED).
          (2)  NVG OPERATIONS IN THE AH-64 AIRCRAFT WILL BE
CONDUCTED IAW THE INTERIM STATEMENT OF AIRWORTHINESS
QUALIFICATION (ISAQ), DTD 29 JUN 94 WITH LATEST ADDITIONS/CHANGES
DTD 29 NOV 94.
          (3)  PROBLEMS HAVE BEEN REPORTED WITH THE METAL CLIP IN
THE SPH-4B ANVIS ATTACHMENT KIT.  PROBLEMS CONCERN THE FACT THAT
THE RETAINING SCREWS THAT SECURE THE CLIP TO THE VISOR LOOSEN
AFTER MINIMUM USE, THE CLIP WILL NOT TIGHTEN ENOUGH TO SECURE THE
NVG CABLE, AND OTHERS. RECOMMEND USING CLAMP LOOP, NSN 5340-00-
434-9596 TO PROPERLY SECURE THE NVG CABLE CONNECTOR TO THE
HELMET.
          (4)  TM 11-5855-263-10, DTD 1 MAR 94, TABLE 2-2, PAGE 2-
11, STEP 13, NOT USABLE IF COLUMN, ADD THE FOLLOWING: "AIRCREW
SHALL CHECK THAT BOTH EYEPIECES ARE IDENTICAL

(EITHER TWO 15 MM EYEPIECES OR TWO 25 MM EYEPIECES)".
          (5)  TM 11-5855-263-10, DTD 1 MAR 94, PAGE 2-40, PARA 2-
6A, OPERATING INSTRUCTIONS, CHANGE THE NOTE TO THE FOLLOWING:
"ANVIS WILL ACCOMMODATE THE USE OF EYEGLASSES."
          (6)  TM 11-5855-263-10, DTD 1 MAR 94, PAGE B-6,
SECTION 3, BASIC ISSUE ITEMS, ILLUSTRATION NO. 6, CHANGE NSN FOR
NECK CORD ASSEMBLY TO READ: NSN 5855-01-149-4106.  THE LENGTH OF
THIS NECK CORD IS 42 INCHES.  AN ADDITIONAL NECK CORD ASSEMBLY IS
AVAILABLE, SEE PARAGRAPH 8E(4) OF THIS MESSAGE.
          (7)  TM 11-5855-263-23 AND P, DTD 15 MAY 95, PAGE 3-35,
PARA 3-16, SETTING COLLIMATION FOR 25 MM EYEPIECE, ADD THE
FOLLOWING ANTI-TAMPER LACQUERS IN THE INITIAL SETUP, UNDER
MATERIALS/PARTS:  NSN 8030-00-408-1137 (GREEN), NSN 8030-01-077-
7674 (WHITE), NSN 8030-01-163-3483 (YELLOW).
          (8)  TM 11-5855-263-23 AND P, DTD 15 MAY 95, PAGE
B-8, SECTION III, TOOLS AND TEST EQUIPMENT REQUIREMENTS, TOOL REF
CODE 13, SOLDERING IRON, ELECTRIC CHANGE NSN TO READ "NSN 3439-01-
183-4632."
          (9)  THE NEW MONOCULAR HOUSING, HOUSING IMAGE
INTENSIFIER, P/N 5009524, NSN 5855-01-380-9669 ON THE ANVIS HAS A
NEW ANTI-WOBBLE ENHANCEMENT.  WHEN REPLACING THE MONOCULAR
HOUSING IN THE PIVOT AND ADJUSTMENT SHELF (PAS), DO NOT REINSTALL
THE FOUR PAS BELLOWS WHEN REASSEMBLING THE SHELF.
          (10)  THE FOLLOWING NEW NSNS ARE AVAILABLE FROM SUPPLY:
SILICON GREASE, NSN 9150-00-145-0161
COMPRESSED AIR REFILL (16 OZ), NSN 6830-01-335-5741
AA FLASHLIGHT, NSN 6230-01-259-4495
ANVIS COMPATIBLE FLASHLIGHT FILTER (WITH BOOT), NSN 6230-01393-
2365.
          (11)  THE ANVIS PURGE DEVICE (JA215008) HAS A
BUILT-IN PRESSURE REGULATOR CALLED A 5 PSI POP-OFF VALVE, P/N B-
4CP2-5.  IF PROBLEMS HAVE BEEN EXPERIENCED, UNITS SHOULD ENSURE
THE POP-UP VALVE IS A P/N B-4CP2-5 AND NOT B4CP2-1 THIS ITEM MAY
BE PURCHASED FROM, NUPRO COMPANY, 4800 EAST 345TH STREET,
WILOUGHBY, OH  44094.  CUSTOMER SERVICE MAY BE REACHED AT 1-216-
951-7100 TO PROVIDE THE LOCAL DISTRIBUTOR IN THE AREA.
          (12)  ANVIS COMPONENTS SUCH AS THE BATTERY PACK AND
VISOR ASSEMBLY DO NOT REQUIRE PMCS UNTIL PLACED INTO SERVICE.
          (13)  THIS IS A CLARIFICATION REGARDING COMPLETION OF
THE PERMANENT MAINTENANCE RECORD FOR THE ANVIS ON DA FORM 2408-
15.  ALL MAINTENANCE REPAIR, SUCH AS INSTALLATION OF THE ENHANCED
PIVOT AND ADJUSTMENT SHELF (PAS), OR REPLACING 15 MM LENS
ASSEMBLIES WITH 25 MM LENS ASSEMBLIES, WILL BE DOCUMENTED BY
TRANSFERRING THE INFORMATION FROM THE MAINTENANCE WORK ORDER TO
THE DA FORM 2408-15.
          (14)  AVIM MAINTENANCE ORGANIZATIONS, UPON COMPLETION
OF THE 180 DAY SERVICE FOR AVIM-OWNED ANVIS SYSTEMS, MUST
DOCUMENT THIS MAINTENANCE ACTION ON A DA FORM 2407-15.
9.  CORRECTION PROCEDURES - N/A.
10.  SUPPLY/PARTS AND DISPOSITION - N/A.
11.  SPECIAL TOOLS, JIGS AND FIXTURES REQUIRED - N/A.
12.  APPLICATION - N/A.
13.  REFERENCES - THE FOLLOWING TBS AND MESSAGES HAVE EXPIRED:
     A.  TB 1-1520-237-20-139, SUBJECT - H-60, NIGHT VISION
GOGGLE (NVG) COMPATIBILITY REWORK OF MASTER WARNING PANEL
ASSEMBLY.  THIS TB EXPIRED 17 OCT 95.
     B.  TB 1-1520-237-50-139, SUBJECT - H-60, NIGHT VISION
GOGGLE (NVG) COMPATIBILITY REWORK OF MASTER WARNING PANEL
ASSEMBLY.  THIS TB WAS SUPERSEDED BY TB 1-1520-237-20-139.
     C.  TB 1-1500-347-30, SUBJECT:  USE OF THE DUAL VISOR ON THE
SPH-4B, DATED 19 NOV 93.  THIS TB WAS SUPERSEDED BY TB 11500-350-
30.
     D.  TB 1-1500-348-30, SUBJECT:  AVIATION NIGHT VISION
GOGGLE MAINTENANCE DOCUMENTATION, 29 DEC 95.  THIS TB WAS
SUPERSEDED BY TB 1-1500-350-30.
     E.  CDRUSAAVNC MESSAGE, 211300Z DEC 93, SUBJECT AVIATORS
NIGHT VISION IMAGING SYSTEM (ANVIS) MAINTENANCE QUALIFICATION
TRAINING GUIDANCE.  THIS MESSAGE WAS SUPERSEDED BY CDRUSAAVNC
MESSAGE, 041600Z MAR 96, SAB.  THIS MESSAGE HAS BEEN SUPERSEDED
BY CDRUSAAVNC MESSAGE, 191537Z FEB 97, SAB.
14.  RECORDING AND REPORTING REQUIREMENTS - N/A.
15.  WEIGHT AND BALANCE - N/A.
16.  POINTS OF CONTACT -
     A.  PM-NV/RSTA POC IS MR. GLEN NOWAK, SFAE-IEW-NV-L,
DSN 654-3453 OR COMMERCIAL 703/704-3453.  FAX IS 703/7041111,
EMAIL ADDRESS IS GNOWAK (AT SIGN) NVL.ARMY.MIL.
     B.  AVIATION TRAINING BRIGADE POC IS CW5 JAKE STEVENS, OR
SFC MINTZE, ATZQ-ATB-NS, DSN 558-9545/9515 OR COMMERCIAL 334/255-
9545/9515.  FAX IS DSN 558-3532. EMAIL ADDRESS ATZQATBNS (AT
SIGN) RUCKER-EMH4.ARMY.MIL.
     C.  AN/AVS-7 (ANVIS HUD) POC IS MR. DAVID TROXEL, SFAEIEW-
NV, DSN 654-3452 OR COMMERCIAL 703/704-3452.  FAX IS DSN 654-
3449.  EMAIL ADDRESS IS DTROXEL (AT SIGN) NVL.ARMY.MIL.
     D.  CECOM LAR ACTION OFFICER IS MR. STEVE BORMAN, DSN
236-4064/2814, OR COMMERCIAL 910/396-4064/2814.  FAX IS DSN 236-
2240/5509.
     E.  CECOM MAINTENANCE POC IS MR. JOSEPH CATTELONA, DSN 992-
2854 OR COMMERCIAL 908/532-2854.
     F.  CECOM SAFETY POC IS MR. JAY HANRAHAN, AMSEL-SF, DSN 992-
0084, EXT 6406 OR COMMERCIAL 908/532-0084 EXT 6406. EMAIL ADDRESS
         IS HANRAHAN (AT SIGN) DOIM6.MONMOUTH.ARMY.MIL.
     G.  CECOM HAVEQUICK POC FOR THIS MESSAGE IS MR CHRIS
CARDINALE, DSN 992-2969 OR COMMERCIAL 908/532-2969.
     H.  SUPPLEMENTAL LIGHTING AT ATCOM POINT OF CONTACT IS MS.
KELLY JEANNOTTE, AMSAT-R-ESC, DSN 693-1131 OR COMMERCIAL 314/263-
1131.
     I.  SUPPLEMENTAL LIGHTING AND SPH-4B HELMET POC AT PM
SOLDIER IS MR. ED TAYLOR, DSN 654-3845 OR COMMERCIAL 703/7043845.
FAX NUMBER IS DSN 654-3820/3841.  EMAIL ADDRESS IS PMSDR (AT
SIGN) PMSOLDIER.US.NET.
     J.  NGB POC IS CW5 RICK ANDREWS, DSN 327-7759 OR
703/607-7759,  EMAIL ADDRESS IS ANDREWSR@ARNGRCEMH2.ARMY.MIL, OR
CW4 DON BEATTY, EAATS-FTD, DSN 491-8688 OR 717/861-8688.
     K.  PM ACIS POC IS MR. JAMES HOUSER, SFAE-AV-LSE, DSN
693-3574, OR COMMERCIAL 314/263-3574.
     L. USASC POC IS CW5 BOB BROOKS, CSSC-PMA, DSN 558-3969 OR
COMMERCIAL 334/255-3969.  EMAIL ADDRESS IS BROOKSR (AT SIGN)
RUCKER-SAFETY.ARMY.MIL.
     M.  AH-1 AND OH-58A/C POC IS MR. JOHN GUENTHER, AMCPMCO, DSN
693-2565 OR COMMERCIAL 314/263-2565.
     N.  UH-1 POC IS MR. STEVE REIBLING, AMSAT-D-WAU, DSN
693-2138 OR COMMERCIAL 314/263-2138.
     O.  UH-60 POC IS MR. TIM BENSON, SFAE-AV-BH-L, DSN 6930483
OR COMMERCIAL 314/263-0483.
     P.  OH-58D (I) IS MR. JACK VAN KIRK, SFAE-AV-ASH-T, DSN 693-
1369 OR COMMERCIAL 314/263-1369.
     Q.  CH-47D POC IS MR. JIM TUCKER, SFAE-AV-CH-L, DSN 6932065
OR COMMERCIAL 314/263-2065.
     R.  AH-64A POC IS MR. DON WATKINS, AMSAT-R-ESC, DSN 6939949
OR COMMERCIAL 314/263-9949.
     S.  ATCOM SAFETY POC FOR THIS MESSAGE IS MR. BOB BROCK,
AMSAT-R-X, DSN 693-1599 OR COMMERCIAL 314/263-1599. EMAIL ADDRESS
IS AMSATRXS (AT SIGN) EMH4.STL.ARMY.MIL.
     T.  FOREIGN MILITARY SALES (FMS) RECIPIENTS REQUIRING
CLARIFICATION OF ACTION ADVISED BY THIS MESSAGE SHOULD CONTACT
CW5 JAY NANCE/RON VAN REES, AMSAT-D-S, DSN 6937844/3216 OR
COMMERCIAL 314/263-7844/3216.
     U.  AFTER HOURS CONTACT ATCOM COMMAND OPERATIONS CENTER
(COC) AT DSN 693-2066/7 OR COMMERCIAL 314/263-2066/7.