ORIGINAL NATOPS FLIGHT MANUAL NAVY MODEL AV- -8B/TAV- -8B 161573 AND UP AIRCRAFT THE AIRCRAFT INDOCTRINATION NORMAL PROCEDURES FLIGHT CHARACTERISTICS EMERGENCY PROCEDURES ALL-WEATHER OPERATION COMMUNICATION WEAPONS SYSTEMS FLIGHT CREW COORDINATION NATOPS EVALUATION PERFORMANCE DATA 3 4 5 6 7 8 9 10 11 INDEX & FOLDOUTS 15 MARCH 2008 1 (Reverse Blank) A1-AV8BB-NFM-000 DISTRIBUTION STATEMENT C — Distribution authorized to U.S. Government Agencies and their contractors to protect publications required for official use or for administrative or operational purposes only, 15 March 2008. Other requests for this document shall be referred to Commander, Naval Air Systems Command (PMA--257), 47123 Buse Rd, Bldg 2272, Patuxent River, MD 20670--1547. DESTRUCTION NOTICE — For unclassified, limited documents, destroy by any method that will prevent disclosure of contents or reconstruction of the document. ISSUED BY AUTHORITY OF THE CHIEF OF NAVAL OPERATIONS AND UNDER THE DIRECTION OF THE COMMANDER, NAVAL AIR SYSTEMS COMMAND. 2 1 THIS PUBLICATION IS INCOMPLETE WITHOUT A1-AV8BB- -NFM- -400. PROCEDURES THIS PUBLICATION SUPERSEDES NAVAIR A1-AV8BB- -NFM- -000 DATED 01 SEPTEMBER 2006 AND CHANGE 1 - - 23 APRIL 2007. 0801LP1082212 A1-AV8BB-NFM-000 ORIGINAL 3/(4 blank) DEPARTMENT OF THE NAVY NAVAL AIR SYSTEMS COMMAND RADM WILLIAM A. MOFFETT BUILDING 47123 BUSE ROAD, BLDG 2272 PATUXENT RIVER, MD 20670-1547 15 March 2008 LETTER OF PROMULGATION 1. The Naval Air Training and Operating Procedures Standardization (NATOPS) Program is a positive approach toward improving combat readiness and achieving a substantial reduction in the aircraft mishap rate. Standardization, based on professional knowledge and experience, provides the basis for development of an efficient and sound operational procedure. The standardization program is not planned to stifle individual initiative, but rather to aid the Commanding Officer in increasing the unit’s combat potential without reducing command prestige or responsibility. 2. This manual standardizes ground and flight procedures but does not include tactical doctrine. Compliance with the stipulated manual requirements and procedures is mandatory except as authorized herein. In order to remain effective, NATOPS must be dynamic and stimulate rather than suppress individual thinking. Since aviation is a continuing, progressive profession, it is both desirable and necessary that new ideas and new techniques be expeditiously evaluated and incorporated if proven to be sound. To this end, Commanding Officers of aviation units are authorized to modify procedures contained herein, in accordance with the waiver provisions established by OPNAV Instruction 3710.7, for the purpose of assessing new ideas prior to initiating recommendations for permanent changes. This manual is prepared and kept current by the users in order to achieve maximum readiness and safety in the most efficient and economical manner. Should conflict exist between the training and operating procedures found in this manual and those found in other publications, this manual will govern. 3. Checklists and other pertinent extracts from this publication necessary to normal operations and training should be made and carried for use in naval aircraft. S. R. EASTBURG Rear Admiral, United States Navy By direction of Commander, Naval Air Systems Command A1-AV8BB-NFM-000 ORIGINAL 5/(6 blank) INTERIM CHANGE SUMMARY The following Interim Changes have been cancelled or previously incorporated into this manual. INTERIM CHANGE NUMBER(S) REMARKS/PURPOSE 1 thru 33 Previously incorporated The following Interim Changes have been incorporated into this Change/Revision. INTERIM CHANGE NUMBER(S) REMARKS/PURPOSE 34 192005Z MAR 07 Crosswind Component Calculation 35 202004Z JUN 07 Landing Gear EP/EAAS 36 102006Z DEC 07 Emergency DC Wiring AFC--481 Interim Changes Outstanding — To be maintained by the custodian of this manual. INTERIM CHANGE NUMBER ORIGINATOR/DATE (or DATE/TIME GROUP) PAGES AFFECTED REMARKS/PURPOSE 37 242006Z NOV 08 18--5(18--6 Blank) CHP 18 OCF Procedure Correction 38 052015 Z FEB 0 9 9--17/18 RendezvousTechnique A1-AV8BB- -NFM- -000 ORIGINAL 9-20 PAGE INSERTED TO ALLOW USE OF “A” PAGE P 052015Z FEB 09 FM COMNAVAIRSYSCOM PATUXENT RIVER MD//4.0P// TO ALL HARRIER AIRCRAFT ACTIVITIES COMNAVAIRFOR SAN DIEGO CA//N421A// AIRTEVRON THREE ONE CHINA LAKE CA//51J000D/51J00MD// COMFLOAN MARISTAT INFO COMNAVSAFECEN NORFOLK VA//11// COMNAVAIRSYSCOM PATUXENT RIVER MD//4.0P/4.1/5.0F/4.6.3.3// VMAT TWO ZERO THREE//CO/OPSO/NATOPS/MO// FLTREADCEN EAST CHERRY PT NC//AV8FST// PEOTACAIR PATUXENT RIVER MD//PMA-257/PMA-257SP/PMA-257IT// AJEMA//NINTHSQUADRON// GRUPAER GROTTAGLIE COMMARFORCOM//ALD/G-6/DSS// COMMAFORPAC//ALD/G-6/DSS// CG FIRST MAW//ALD/G-6/DSS// CG SECOND MAW//ALD/G-6/DSS// CG THIRD MAW//ALD/G-6/DSS// MAG TWELVE//CO/OPSO/MO/DSS// MAG THIRTEEN//CO/OPSO/MO/DSS// MAG FOURTEEN//CO/OPSO/MO/DSS// VMA 211//CO/OPSO/MO/DSS// VMA 214//CO/OPSO/MO/DSS// VMA 223//CO/OPSO/MO/DSS// VMA 231//CO/OPSO/MO/DSS// VMA 311//CO/OPSO/MO/DSS// VMA 513//CO/OPSO/MO/DSS// VMA 542//CO/OPSO/MO/DSS// MSGID/GENADMIN,USMTF,2007/COMNAVAIRSYSCOM PATUXENT RIVER// SUBJ/AV-8B AIRCRAFT NATOPS PUBLICATIONS INTERIM CHANGE// REF/A/MSGID:EML/COMMARFORCOM/26JAN2009// REF/B/MSGID:DOC/NAVAIR/09SEP2008// REF/C/MSGID:DOC/NAVAIR/15MAR2008// NARR/REF (A) IS COG CONCURRENCE. REF (B) IS AIRS 2008-165. REF (C) IS AV-8B A1-AV8BB-NFM-000 NATOPS FLIGHT MANUAL DTD 15 NOV 2008.// GENTEXT/REMARKS/1. THIS MESSAGE IS ISSUED IN RESPONSE TO REFS (A) AND (B). THIS MESSAGE ISSUES INTERIM CHANGE (IC) NUMBER 38 TO REF (C). 2. SUMMARY. A. THIS MESSAGE ISSUES NEW PARA 9.1.7.4, RENDEZVOUS TECHNIQUE, ADDRESSING USE OF NOZZLES TO CONTROL CLOSURE RATE, TO REF (C). B. REPLACEMENT PAGES CONTAINING THESE CHANGES FOR DOWNLOADING AND INSERTION INTO REF (C) WILL BE ATTACHED TO THIS INTERIM CHANGE MESSAGE WHEN IT IS POSTED ON THE NATEC AND AIRWORTHINESS WEBSITES (SEE LAST PARA BELOW). 3. THE REPLACEMENT PAGES IMPACT THE FOLLOWING NATOPS FLIGHT MANUAL. THE REPLACEMENT PAGE PACKAGE INCLUDES THE FOLLOWING PAGES: A. REF (C) (AV-8B NFM-000) PAGES 5/(6 BLANK), 9-17, 9-18, 9- 18A/(B BLANK). B. TO ENSURE THE PDF PAGES PRINT TO SCALE: SELECT PRINT AND VIEWING PRINT SETUP WINDOW, ENSURE "NONE" IS SELECTED IN THE PAGE SCALING DROPDOWN. 4. POINTS OF CONTACT: A. AV-8B NATOPS PROGRAM MANAGER: (1) MAJ JOHN ROUNTREE, VMAT-203, (252) 466-4863 EXT 3151, DSN 582-4863 EXT3151, E-MAIL JOHN.D.ROUNTREE(AT)USMC.MIL. B. NAVAIR POCS: (1) MARTY SCANLON, NATOPS IC COORDINATOR, TEL DSN 757-6045 NAVAIR 052015Z FEB 09 Page 1 of 2 A1-AV8BB-NFM-000 IC 38 NAVAIR 052015Z FEB 09 Page 2 of 2 A1-AV8BB-NFM-000 IC 38 OR COMM (301) 757-6045, EMAIL: MARTIN.SCANLON(AT)NAVY.MIL (2) LTCOL JASON MADDOCKS, PMA-257 APMSE, (301) 757-5458, DSN 757-5458, E-MAIL JASON.MADDOCKS(AT)NAVY.MIL (3) KRISTIN SWIFT, AIR-4.0P, NATOPS CHIEF ENGINEER, (301) 995-4193, DSN 995-4193, E-MAIL KRISTIN.SWIFT(AT)NAVY.MIL. (4) AIRWORTHINESS GLOBAL CUSTOMER SUPPORT TEAM, TEL: 301-757-0187, EMAIL: NAVAIR_4.0P_IFC@NAVY.MIL. 5. THIS MESSAGE WILL BE POSTED ON THE NATEC WEBSITE, WWW.MYNATEC.NAVAIR.NAVY.MIL WITHIN 48 HOURS OF RELEASE. NEW NATOPS IC MESSAGES MAY BE FOUND IN TWO PLACES ON THIS WEBSITE: A. IN THE NATOPS IC DATABASE FOUND UNDER THE TMAPS OPTION. B. IN THE AFFECTED PUBLICATIONS(S) JUST AFTER THE IC SUMMARY PAGE. IF THE IC MESSAGE INCLUDES REPLACEMENT PAGES, THEY WILL BE ADDITIONALLY PLACED WITHIN THE MANUAL AND REPLACED PAGES DELETED. MESSAGES ARE NORMALLY POSTED IN THE DATABASE BEFORE APPEARING IN THE PUBLICATION. THIS MESSAGE WILL ALSO BE POSTED ON THE AIRWORTHINESS WEBSITE, AIRWORTHINESS.NAVAIR.NAVY.MIL. IF UNABLE TO VIEW THIS MESSAGE ON EITHER THE NATEC OR AIRWORTHINESS WEBSITES, INFORM THE NATOPS GLOBAL CUSTOMER SUPPORT TEAM AT (301) 342-3276, DSN 342-3276, OR BY EMAIL AT NATOPS(AT)NAVY.MIL. C. INFORMATION REGARDING THE AIRWORTHINESS PROCESS, INCLUDING A LISTING OF ALL CURRENT INTERIM FLIGHT CLEARANCES, NATOPS AND NATIP PRODUCTS ISSUED BY NAVAIR 4.0P, CAN BE FOUND AT OUR WEBSITE: AIRWORTHINESS.NAVAIR.NAVY.MIL. D. E-POWER FOLDER 851943, TRACKING NUMBER 33118.// Kristin Swift, NATOPS Chief Engineer, 4.0P, 02/05/2009 P 242006Z NOV 08 FM COMNAVAIRSYSCOM PATUXENT RIVER MD//4.0P// TO ALL HARRIER AIRCRAFT ACTIVITIES COMNAVAIRFOR SAN DIEGO CA//N421A// AIRTEVRON THREE ONE CHINA LAKE CA//51J000D/51J00MD// COMFLOAN MARISTAT INFO COMNAVSAFECEN NORFOLK VA//11// COMNAVAIRSYSCOM PATUXENT RIVER MD//4.0P/4.1/5.0F/4.6.3.3// VMAT TWO ZERO THREE//CO/OPSO/NATOPS/MO// FLTREADCEN EAST CHERRY PT NC//AV8FST// PEOTACAIR PATUXENT RIVER MD//PMA-257/PMA-257SP/PMA-257IT// AJEMA//NINTHSQUADRON// GRUPAER GROTTAGLIE COMMARFORCOM//ALD/G-6/DSS// COMMAFORPAC//ALD/G-6/DSS// CG FIRST MAW//ALD/G-6/DSS// CG SECOND MAW//ALD/G-6/DSS// CG THIRD MAW//ALD/G-6/DSS// MAG TWELVE//CO/OPSO/MO/DSS// MAG THIRTEEN//CO/OPSO/MO/DSS// MAG FOURTEEN//CO/OPSO/MO/DSS// VMA 211//CO/OPSO/MO/DSS// VMA 214//CO/OPSO/MO/DSS// VMA 223//CO/OPSO/MO/DSS// VMA 231//CO/OPSO/MO/DSS// VMA 311//CO/OPSO/MO/DSS// VMA 513//CO/OPSO/MO/DSS// VMA 542//CO/OPSO/MO/DSS// MSGID/GENADMIN,USMTF,2007/COMNAVAIRSYSCOM/4.0P// SUBJ/AV-8B AIRCRAFT PRELIMINARY NATOPS PUBLICATIONS INTERIM CHANGE /SAFETY OF FLIGHT// REF/A/MSGID:EML/COMMARFORCOM/20NOV2008// REF/B/MSGID:DOC/NAVAIR/19NOV2008// REF/C/MSGID:DOC/NAVAIR/15MAR2008// NARR/REF (A) IS COG CONCURRENCE. REF (B) IS AIRS 2008-228. REF (C) IS AV-8B A1-AV8BB-NFM-000 NATOPS FLIGHT MANUAL DTD 15 NOV 2008.// GENTEXT/REMARKS/1. THIS MESSAGE IS ISSUED IN RESPONSE TO REFS (A) AND (B). THIS MESSAGE ISSUES INTERIM CHANGE (IC) NUMBER 37 TO REF (C). 2. SUMMARY. A. THIS MESSAGE ISSUES AND ADMIN CORRECTION TO PAGE 18-5, PARA 18-20-2, IMMEDIATE ACTION ITEMS FOR OUT OF CONTROL FLIGHT/ SPIN/FALLING LEAF RECOVERY PROCEDURES. B. REPLACEMENT PAGES CONTAINING THESE CHANGES FOR DOWNLOADING AND INSERTION INTO REF (C) WILL BE ATTACHED TO THIS INTERIM CHANGE MESSAGE WHEN IT IS POSTED ON THE NATEC AND AIRWORTHINESS WEBSITES (SEE LAST PARA BELOW). 3. THE REPLACEMENT PAGES IMPACT THE FOLLOWING NATOPS FLIGHT MANUAL. THE REPLACEMENT PAGE PACKAGE INCLUDES THE FOLLOWING PAGES: A. REF (C) (AV-8B NFM-000) PAGES 5/(6 BLANK) AND 18-5/(18-6 BLANK). B. TO ENSURE THE PDF PAGES PRINT TO SCALE: SELECT PRINT AND VIEWING PRINT SETUP WINDOW, ENSURE "NONE" IS SELECTED IN THE PAGE SCALING DROPDOWN. 4. POINTS OF CONTACT: A. AV-8B NATOPS PROGRAM MANAGER: (1) MAJ MICHAEL HUNTING, VMAT-203, (252) 466-2638, DSN NAVAIR 242006Z NOV 08 Page 1 of 2 A1-AV8BB-NFM-000 IC 37 NAVAIR 242006Z NOV 08 Page 2 of 2 A1-AV8BB-NFM-000 IC 37 582-2638, E-MAIL MICHAEL.HUNTING(AT)USMC.MIL B. NAVAIR POCS: (1) MARTY SCANLON, NATOPS IC COORDINATOR, TEL DSN 757-6045 OR COMM (301) 757-6045, EMAIL: MARTIN.SCANLON(AT)NAVY.MIL (2) LTCOL JASON MADDOCKS, PMA-257 APMSE, (301) 757-5458, DSN 757-5458, E-MAIL JASON.MADDOCKS(AT)NAVY.MIL (3) KRISTIN SWIFT, AIR-4.0P, NATOPS CHIEF ENGINEER, (301) 995-4193, DSN 995-4193, E-MAIL KRISTIN.SWIFT(AT)NAVY.MIL. (4) AIRWORTHINESS GLOBAL CUSTOMER SUPPORT TEAM, TEL: 301-757-0187, EMAIL: NAVAIR_4.0P_IFC@NAVY.MIL. 5. THIS MESSAGE WILL BE POSTED ON THE NATEC WEBSITE, WWW. NATEC.MIL WITHIN 48 HOURS OF RELEASE. NEW NATOPS IC MESSAGES MAY BE FOUND IN TWO PLACES ON THIS WEBSITE: A. IN THE NATOPS IC DATABASE FOUND UNDER THE TMAPS OPTION. B. IN THE AFFECTED PUBLICATIONS(S) JUST AFTER THE IC SUMMARY PAGE. IF THE IC MESSAGE INCLUDES REPLACEMENT PAGES, THEY WILL BE ADDITIONALLY PLACED WITHIN THE MANUAL AND REPLACED PAGES DELETED. MESSAGES ARE NORMALLY POSTED IN THE DATABASE BEFORE APPEARING IN THE PUBLICATION. THIS MESSAGE WILL ALSO BE POSTED ON THE NATOPS WEBSITE, AIRWORTHINESS.NAVAIR.NAVY.MIL. IF UNABLE TO VIEW THIS MESSAGE ON EITHER THE NATEC OR AIRWORTHINESS WEBSITES, INFORM THE NATOPS GLOBAL CUSTOMER SUPPORT TEAM AT (301) 342-3276, DSN 342-3276, OR BY EMAIL AT NATOPS(AT)NAVY.MIL. C. INFORMATION REGARDING THE AIRWORTHINESS PROCESS, INCLUDING A LISTING OF ALL CURRENT INTERIM FLIGHT CLEARANCES, NATOPS AND NATIP PRODUCTS ISSUED BY NAVAIR 4.0P, CAN BE FOUND AT OUR WEBSITE: AIRWORTHINESS.NAVAIR.NAVY.MIL. D. EPOWER FOLDER NUMBER 848143, TRACKING NUMBER 32809.// Kristin Swift, NATOPS Chief Engineer, 4.0P, 11/24/2008 A1-AV8BB-NFM-000 ORIGINAL 7 Summary of Applicable Technical Directives Information relating to the following technical directives has been incorporated into this manual. Change Number ECP Number Description Visual Identification Effectivity ASC--020 0102 Improves high speed roll rate None AV--8B (P)162942 and up (R)161573 thru 162746 AYC--836 Lucus--08 Mk 4 GTS/APU operational performance enhancement None No aircraft effectivity AFC--286 AYC--873 141 Throttle grip modification None AV--8B (P)163659 and up (R)161573 thru 163519 AFC--287 85R1 Dual airspeed/altitude sensor arming incorp & removal of external initiated canopy fracturing system arming None AV--8B (P)163659 and up (R)161573 thru 163519 — 145 Voice warning None AV--8B (P)163519 and up TAV--8B (P)163856 and up — 177 Landing gear blow down bottle gas change Identification plate installed on bottle AV--8B (P)163659 and up TAV--8B (P)163856 and up — 162 Part 1 Provisions for incorporation of F402--RR--408 engine 15 sec caution light threshold for short lift dry is 684 5 º vice 687 5 º TAV--8B (P)164113 and up AFC--253 075R1C2 Modification of data storage unit installation Mount swings forward for removal and installation of DSU AV--8B (P)163677 and up (R)163176 thru 163676 A1-AV8BB-NFM-000 ORIGINAL 8 Change Number ECP Number Description Visual Identification Effectivity AFC--328 217 Incorporation of two batteries for emergency backup power Emergency battery/switch on left canopy sill and on left console AV--8B (R)161573 thru 164150 TAV--8B (R)162747 thru 164542 AFC--332 231 Redundant DECS enable switch Switch aft left console above fuel shutoff handle AV--8B (P) 164139 and up (R)161573 thru 164135 TAV--8B (P)164540 and up (R)162747 thru 164138 — 162C3 Add F402--RR--408 engine ENG ID --408 -- Identification displayed on ENG display AV--8B (P)164116 and up ASC--043 DO 30 Incorporates OMNIBUS VII mission computer OFP MC OFP 91--D0FE040K AV--8B (R)161573 thru 163852 TAV--8B (R)162747 thru 164542 — 129C/C3 Adds new head up display Wider field of view HUD AV--8B (P)163853 and up — 170C1 Power distribution redesign Changes in circuit breaker panels AV--8B (P)163853 and up — 161C1/C2 Adds 100% LERX provisions Forward ram air intakes moved AV--8B (P)163853 and up — 134C1/ C3/C4 Production night attack installation Additional MPCD, night vision compatible main instrument panel AV--8B (P)163853 and up — 143C1C2 Stores management system enhancement None AV--8B (P)163853 and up — 161 Adds upward firing dispensing system Four additional dispensers near top of rear fuselage AV--8B (P)163853 and up A1-AV8BB-NFM-000 ORIGINAL 9 Change Number ECP Number Description Visual Identification Effectivity ASC--053 226 Incorporates OMNIBUS VI+ mission computer OFP MC OFP 90--N0FE030P AV--8B (P)163853 and up — 199C1 Night attack enhancements An IR source on the HUD video camera AV--8B (P)163853 and up — 200R1 Production incorporation of AN/ APG--65 radar and wiring provisions for smart weapons Radar switch on miscellaneous switch panel AV--8B (P)164549 and up AFC--326 180R1 Incorporation of provisions for ATHS Addition of circuit breaker AV--8B (R)164548 thru 165006 AFC--326 PART 3 180R1 Incorporation of provisions for ATHS Addition of circuit breaker AV--8B (R)163853 thru 164547 180R2 Production incorporation of the ATHS Addition of circuit breaker AV--8B (P)165384 and up AFC--354 REV A 168C1 Incorporation of GPS provisions and mini tacan Addition of circuit breaker AV--8B (R)163853 thru 164547 TAV--8B (R)164113 thru 164542 AFC--354 PART 2 168C1 Incorporation of GPS provisions and mini tacan Addition of circuit breaker AV--8B (R)161573 thru 163852 TAV--8B (R)162963 thru 163861 AFC--354 PART 3 168C1 Incorporation of GPS provisions and mini tacan Addition of circuit breaker AV--8B (R)164549 thru 165383 168C1R1 Production incorporation of GPS provisions and mini tacan Addition of circuit breaker AV--8B (P)165384 and up 161C3 Production incorporation of 100% LERX 100% LERX installed AV--8B (P)163853 thru 164121 200C2 Radar remanufacture for AV--8B Same as radar aircraft AV--8B (P)165305 and up A1-AV8BB-NFM-000 ORIGINAL 10 Change Number ECP Number Description Visual Identification Effectivity AFC--368 RAMEC-- 13--91 Radar altimeter power distribution Changes in circuit breaker panels AV--8B (P)164549 and up AV--8B (R)163853 thru 164547 TAV--8B (R)164113 thru 164542 AFC--370 19R1 MIL--W--81381 wiring replacement Addition of circuit breakers AV--8B (R)161573 thru 163852 TAV--8B (R)162747 thru 163861 AFC--391 251R1 Production incorporation of Pilot Selectable Hi/Lo Gain Nose Wheel Steering (NWS) Addition of NWS light on caution/ advisory panel AV--8B (P)165354 and up AFC--392 254 Incorporation of provisions for IGVC Digital Electronic Control (IDEC) None AV--8B (P)165354 and up (R)161573 thru 165312 TAV--8B (R)162747 thru 164542 AFC--394 256 Jet Pipe Temperature modification None AV--8B (P)165354 and up (R)161396 thru 165312 TAV--8B (R)162747 thru 164542 ASC--76 NWC-- RJW-- 014D-- 5310 Incorporates Omnibus 7.1 MC OFP 96--D0FE060C AV--8B (R) 161573 thru 163852 TAV--8B (R)162747 thru 164542 A1-AV8BB-NFM-000 ORIGINAL 11 Change Number ECP Number Description Visual Identification Effectivity AFC--395 257 Uninterupted power to DECU Addition of circuit breakers AV--8B (P)165354 and up (R)163853 thru 165312 TAV--8B (R)164113 thru 164542 ASC--78 JSSA--01 Incorporates Omnibus C1 MC OFP 96--C0FE060L AV--8B (P)163853 and up AFC--393 255R1 Incorporates DFC and FCEM DFC OFP 75A870731-- AV--8B (P)165391 and up (R)161397 thru 165390 TAV--8B (R)164113 thru 164542 AFC--409 JSSA--01 Incorporates ARC--210 Radio New Radio Set Control Panel AV--8B (P)165384 and up (R) 163853 thru 165383 AFC--420 270R1 Incorporates MIL--STD--1760 Wiring Added Circuit Breakers AV--8B (P)165413 and up (R) 163853 thru 165412 AFC--422 CHPT-- 029 Incorporates 8mm Video Recorder 8mm Video Recorder AV--8B (P) 165422 and up (R) 161573 thru 165421 TAV--8B (R)162747 thru 164542 AFC--373 246 Incorporation of Pyrotechnic Canopy Restraint Addition of SMDC thruster on forward canopy aft arch TAV--8B (R)162747 thru 164542 A1-AV8BB-NFM-000 ORIGINAL 12 Change Number ECP Number Description Visual Identification Effectivity ACC--667 PART 2 16416 Incorporation of personnel parachute Four--Line release sys- tem and over--inflation control line. Addition of personnel parachute riser covers. AV--8B (R)161573 and up TAV--8B (R)162747 thru 164542 AFC--449 303 Incorporation of Electronic Airspeed/Altitude Sensor LEDs on sensor AV--8B (R)161573 and up TAV--8B (R)162747 thru 164542 AFC--464 RAMEC-- 41--03 Modification of DC Emergency Panel Assembly Relocation of W ON W circuit breaker AV--8B (R)163853 and up 285 Incorporation of OC1.2 312 Incorporation of H2.0 AFC--456 306 Incorporation of Advanced Multipurpose Color Display New MPCD AV--8B (R)163853 and up AFC--481 Emergency DC Wiring (P) Production (R) Retrofit Information relating to the following applicable technical directives will be incorporated in a future change. Change Number ECP Number Description Visual Identification Effectivity A1-AV8BB-NFM-000 ORIGINAL 13/(14 blank) RECORD OF CHANGES Record entry and page count verification for each printed change and erratum: Change No. and Date of Change Date of Entry Page Count Verified by (Signature) A1-AV8BB-NFM-000 ORIGINAL 15/(16 blank) LIST OF EFFECTIVE PAGES Effective Pages Page Numbers Original 1 (Reverse Blank) Original 3 (Reverse Blank) Original 5 (Reverse Blank) Original 7 thru 13 (Reverse Blank) Original 15 (Reverse Blank) Original 17 thru 41 (Reverse Blank) Original 43 thru 47 (Reverse Blank) Original 49 thru 65 (Reverse Blank) Original 1-1 thru 1-7 (Reverse Blank) Original 2-1 thru 2-130 Original 3-1 (Reverse Blank) Original 4-1 thru 4-21 (Reverse Blank) Original 67 (Reverse Blank) Original 5-1 thru 5-4 Original 69 (Reverse Blank) Original 6-1 (Reverse Blank) Original 7-1 thru 7-68 Original 8-1 (Reverse Blank) Original 9-1 thru 9-27 (Reverse Blank) Original 10-1 thru 10-38 Original 71 (Reverse Blank) Original 11-1 thru 11-42 Original 73 thru 78 Original 12-1 thru 12-13 (Reverse Blank) Original 13-1 thru 13-4 Original 14-1 thru 14-2 Original 15-1 thru 15-49 (Reverse Blank) Original 16-1 thru 16-12 Original 17-1 thru 17-24 Effective Pages Page Numbers Original 18-1 thru 18-5 (Reverse Blank) Original 19-1 thru 19-2 Original 79 (Reverse Blank) Original 20-1 thru 20-5 (Reverse Blank) Original 21-1 thru 21-2 Original 81 (Reverse Blank) Original 22-1 thru 22-18 Original Original Original 23-1 thru 23--81 (Reverse Blank) 83 (Reverse Blank) 85 (Reverse Blank) Original Original 24-1 thru 24-4 87 (Reverse Blank) Original Original 25-1 thru 25-11 (Reverse Blank) 89 (Reverse Blank) Original Index-1 thru Index-21 (Reverse Blank) Original FO-1 (Reverse Blank) Original FO-2 (Reverse Blank) Original FO-3 (Reverse Blank) Original FO-4 (Reverse Blank) Original FO-5 (Reverse Blank) Original FO-6 (Reverse Blank) Original FO-7 (Reverse Blank) Original FO-8 (Reverse Blank) Original FO-9 (Reverse Blank) Original FO-10 (Reverse Blank) Original FO-11 (Reverse Blank) Original FO-12 (Reverse Blank)