AIRCREW WEAPONS DELIVERY MANUAL (NONNUCLEAR) B-52/AGM-158 JASSM

Transcription

1 AIRCREW WEAPONS DELIVERY MANUAL (NONNUCLEAR) B-52/AGM-158 JASSM USAF SERIES B-52/AGM-158 JASSM THE BOEING COMPANY F C-0002 F D-0066 AIRCRAFT WEAPONS This manual contains unverified procedures. Refer to the validation/verification status page(s) prior to performing any operation or maintenance procedure. THIS PUBLICATION IS INCOMPLETE WITHOUT CLASSIFIED SUPPLEMENT T.O. 1B-52H SEE T.O. 0-1-CD-1 FOR CURRENT STATUS OF FLIGHT MANUALS, SAFETY SUPPLEMENTS, OPERATIONAL SUPPLEMENTS, AND FLIGHT CREW CHECKLISTS. COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTION OF ALL AIR FORCE PERSONNEL CLEARED FOR OPERATION OF SUBJECT AIRCRAFT. DISTRIBUTION STATEMENT E Distribution authorized to the Department of Defense Components only, due to Direct Military Support, 29 October Other requests shall be referred to 327 BMSG/EN, Tinker AFB, OK WARNING This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App et seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive HANDLING AND DESTRUCTION NOTICE Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document. Demil code D. PUBLISHED UNDER AUTHORITY OF THE SECRETARY OF THE AIR FORCE 1 DECEMBER 2003 CHANGE 3 1 JUNE 2006

2 Technical orders are normally distributed promptly after printing. Date(s) shown on the title page (lower right corner) are for identification only. These are not distribution dates. Processing time sometimes causes distribution to only appear to have been delayed. LIST OF EFFECTIVE PAGES NOTE: INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES. The portion of the text affected by the changes is indicated by a vertical line in the outer margins of the page. Dates of issue for original and changed pages are: Original 0 1 Dec 03 Change 1 1 Dec 04 Change 2 1 Jul 05 Change 3 1 Jun 06 TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 256 CONSISTING OF THE FOLLOWING: Page Change Page Change Page Change Page Change No. No. No. No. No. No. No. No. * Title *A... 3 V/VS-1 V/VS-7 Added... 2 V/VS-8 Blank Added * Flyleaf Flyleaf 2 Blank i ii iii *iv Blank * Blank * * A 1-30F Added * * * * * A 1-52G Added H Blank Added * A Added * 1-62B 1-62D * * A 1-68D Added * * Blank * * Blank * Blank * * Blank * * * Blank * * * 7-20A 7-20B * 7-20C 7-20D Deleted * Blank A Added B Blank Added * A 7-68D Added Blank Glossary-1 Glossary Index-1 Index Index-4 Blank CURRENT ABBREVIATED CHECKLIST AGM-158 JASSM Abbreviated Flight Crew Checklist T.O. 1B-52H CL-1 1 Dec 03 Change 3-1 Jun 06 Upon receipt of the second and subsequent changes to this technical order, personnel responsible for maintaining this publication in current status will ascertain that all previous changes have been received and incorporated. Action should be taken promptly if the publication is incomplete. *The asterisk indicates pages changed, added, or deleted by the current change. ADDITIONAL COPIES OF THIS PUBLICATION MAY BE OBTAINED BY USAF ACTIVITIES IN ACCORDANCE WITH T.O A Change 3 USAF

3 WARNING This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs and Performance of unverified procedures may result in injury to personnel or damage to equipment. TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE T.O. NO. BASIC DATE CHANGE NO. DATE PTO CHANGE NO. DATE T.O. 1B-52H DEC 03 CHANGE 2-1 JUL 2005 AMI DATA ELEMENT DATE VALIDATED VALIDATION METHOD DATE VERIFIED VERIFICATION METHOD REMARKS (A) (B) (B) TCTO Listings (P, PG iv) 1 Mar 04 A Offensive Avionics System (OAS) Interface (P, PG 1-11 ) 1 Mar 04 A Weapon Control Panel Interface (P, PG 1-11 ) 1 Mar 04 A Missile Data Flow (Typical) (F: 1-4, PG 1-13) 1 Mar 04 A Weapon Control Panel (F: 1-5, 2 /2, PG 1-15) 1 Mar 04 A JASSM IKB Commands (F: 1-9, 1/2, PG 1-19) 1 Mar 04 A JASSM IKB Commands (F: 1-9, 2/2, PG 1-20) 1 Mar 04 A Weapon Jettison (P, PG 1-22) 1 Mar 04 A AJCP Commanded Jettison (P, PG 1-22) 1 Mar 04 A Pilot s Bmb Bay & Missile Jett Contrl Switch Commanded Jett (P, PG1-25) 1 Mar 04 A JASSM SMO Software (P, PG 1-27) 1 Mar 04 A SMO MFD Displays (P, PG ) 1 Mar 04 A Prime Mission Data (P, PG 1-28) 1 Mar 04 A Weapon Supervision Menu (CF-5) (P, PG 1-30) 1 Dec 04 A PART SIM Mode Command (CF-51) (P, PG 1-30) 1 Dec 04 A FULL SIM Mode Command (CF-52) (P, PG 1-30) 1 Dec 04 A JASSM Supervision Menu (CF-57) (P, PG 1-30A) 1 Mar 04 A JASSM Control Function (CF) Commands (F: 1-16, PG 1-30B) 1 Mar 04 A CF Menu (F: 1-17, 1/2, PG 1-30C) 15 Mar 04 A CF Menu (F: 1-17, 2/2, PG 1-30D) 15 Mar 04 A Weapon Supervision Menu (CF-5) (F: 1-18, 1/2, PG 1-30E) 15 Mar 04 A LEGEND: (A) DATA ELEMENT: (S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE (B) VALIDATION OR VERIFICATION METHOD: (P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP) V/VS-1

4 WARNING This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs and Performance of unverified procedures may result in injury to personnel or damage to equipment. TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE T.O. NO. BASIC DATE CHANGE NO. DATE PTO CHANGE NO. DATE T.O. 1B-52H DEC 03 CHANGE 2-1 JUL 2005 AMI DATA ELEMENT DATE VALIDATED VALIDATION METHOD DATE VERIFIED VERIFICATION METHOD REMARKS (A) Weapon Supervision Menu (CF-5) (F: 1-18, 2/2, PG 1-30F) 15 Mar 04 A Classified Data Erase Command (CF-575) (P, PG 1-31) 1 Mar 04 A JASSM Auto Targeting Mode (CF-580) (P, PG 1-31) 1 Mar 04 A Missile Tgt Assign(Manual Targeting) Display (CF-586) (P, PG 1-31) 1 Mar 04 A JASSM Supervision Menu (CF-57) (F: 1-18, 1/2, PG 1-32) 15 Mar 04 A JASSM Supervision Menu CF-57 (F: 1-18, 2/2, PG 1-33) 1 Mar 04 A JASSM Targeting Menu (CF-58) (F: 1-20, 1/2, PG 1-34) 1 Mar 04 A JASSM Targeting Menu (CF-58) (F: 1-20, 2/2, PG 1-35) 1 Mar 04 A Missile Target Assignment Display (CF-586) (F: 1-21, 1/3, PG 1-36) 1 Mar 04 A Missile Target Assignment Display (CF-586) (F: 1-18, 2/3, PG 1-37) 1 Mar 04 A Missile Target Assignment Display (CF-586) (F: 1-18, 3/3, PG 1-38) 1 Mar 04 A Direct Target Definition Display (CF-588,n) (P, PG 1-39) 1 Mar 04 A Retarget-All Command (CF589) (P, PG 1-41) 1 Mar 04 A Direct Tgt Definition Disp (CF-588,n) (P, 1-22, 2/4, PG 1-43) 1 Mar 04 A CF-62 SMO Menu (P, PG 1-46) 1 Mar 04 A CF-65 Data Record (P, PG 1-46) 1 Mar 04 A CF-67 Shutdown (P, PG 1-47) 1 Mar 04 A CF-68 ECU Power Override (P, PG 1-47) 1 Mar 04 A CF-69A & CF-69B ACU Shutdown (P, PG 1-47) 1 Mar 04 A FCP Supervision Menu (CF-6) (F: 1-23, 1/2, PG 1-48) 1 Mar 04 A FCP Supervision Menu (CF-6) (F: 1-23, 2/2, PG 1-49) 1 Mar 04 A (B) (B) LEGEND: (A) DATA ELEMENT: (S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE (B) VALIDATION OR VERIFICATION METHOD: (P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP) V/VS-2

5 WARNING This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs and Performance of unverified procedures may result in injury to personnel or damage to equipment. TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE T.O. NO. BASIC DATE CHANGE NO. DATE PTO CHANGE NO. DATE T.O. 1B-52H DEC 03 CHANGE 2-1 JUL 2005 AMI DATA ELEMENT DATE VALIDATED VALIDATION METHOD DATE VERIFIED VERIFICATION METHOD REMARKS (A) SMO Load Menu (CF-62) (F: 1-24, PG 1-50) 1 Mar 04 A Mission Supervision Menu (P, PG 1-51) 15 Mar 04 A B-52 Mission Data Load Command (P, PG 1-51) 1 Dec 04 A Weapon Group Load Display (CF-82A, CF-82C)(P, PG 1-52) 1 Mar 04 A Mission Supervision Menu (F: 1-25, 1/2, PG 1-52A) 15 Mar 04 A Mission Supervision Menu (F: 1-25, 2 /2, PG 1-52B) 15 Mar 04 A B-52 Mission Data Load Display (CF-81)(F: 25A, 1/2, PG 1-52C) 15 Mar 04 A B-52 Mission Data Load Display (CF-81)(F: 25A, 2/2, PG 1-52D) 1 Mar 04 A Wpn Grp Load Menu (F: 1-25B, 1/2, PG 1-52E) 1 Mar 04 A Wpn Grp Load Menu (F: 1-25B, 2/2, PG 1-52F) 1 Mar 04 A Targeting Completion Command (CF-DD) (P, PG 1-52G) 1 Mar 04 A Direct Target Copy Command (CF-Dn) (P, PG 1-52G) 1 Mar 04 A Format (FRMT) Displays (P, PG 1-56) 1 Mar 04 A JASSM Status & Inventory Display (FRMT-7)(P, PG 1-56) 1 Mar 04 A JASSM Status & Invent Disp w/ Sel Sta Status (FRMT-7xy)(P, PG 1-57) 1 Mar 04 A Weapon Assignment Data Display (P, PG 1-57) 1 Mar 04 A Stores Inventory Summary Display (FRMT-77)(P, PG 1-57) 1 Mar 04 A JASSM Format Commands (F: 1-28, PG 1-57) 1 Mar 04 A JASSM FRMT (Format) Menu (F: 1-29, 1/2, PG 1-58) 1 Mar 04 A JASSM FRMT (Format) Menu (F: 1-29, 2/2, PG 1-59) 1 Mar 04 A PME Status Display (FRMT-6) (F: 1-30, 1/2, PG 1-60) 1 Mar 04 A (B) (B) LEGEND: (A) DATA ELEMENT: (S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE (B) VALIDATION OR VERIFICATION METHOD: (P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP) V/VS-3

6 WARNING This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs and Performance of unverified procedures may result in injury to personnel or damage to equipment. TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE T.O. NO. BASIC DATE CHANGE NO. DATE PTO CHANGE NO. DATE T.O. 1B-52H DEC 03 CHANGE 2-1 JUL 2005 AMI DATA ELEMENT DATE VALIDATED VALIDATION METHOD DATE VERIFIED VERIFICATION METHOD REMARKS (A) PME Status Display (FRMT-6) (F: 1-30, 2/2, PG 1-61) 1 Mar 04 A JASSM Status & Inventory Display (FRMT-7)(F: 1-31, 1/6, PG 1-62) 1 Mar 04 A JASSM Status & Inventory Display (FRMT-7)(F: 1-31, 2/6, PG 1-62A) 1 Mar 04 A JASSM Status & Inventory Display (FRMT-7)(F: 1-31, 3/6, PG 1-62B) 1 Mar 04 A JASSM Status & Inventory Display (FRMT-7)(F: 1-31, 4/6, PG 1-62C) 1 Mar 04 A JASSM Status & Inventory Display (FRMT-7)(F: 1-31, 5/6, PG 1-62D) 1 Mar 04 A JASSM Status & Inventory Display (FRMT-7)(F: 1-31, 6/6, PG 1-63) 1 Mar 04 A JASSM Stat & Invent Disp w/ Sel Sta Status (F: 1-32, 2/5, PG 1-65) 1 Mar 04 A JASSM Stat & Invent Disp w/ Sel Sta Status (F: 1-32, 3/5, PG 1-66) 1 Mar 04 A JASSM Stat & Invent Disp w/ Sel Sta Status (F: 1-32, 4/5, PG 1-67) 1 Mar 04 A JASSM Stat & Invent Disp w/ Sel Sta Status (F: 1-32, 5/5, PG 1-68) 1 Mar 04 A Weapon Assignment Data Display (F: 1-32A, 1/2, PG 1-68A) 1 Mar 04 A Weapon Assignment Data Display (F: 1-32A, 2/2, PG 1-68B) 1 Mar 04 A Stores Inventory Display (F: 1-32B, Sheet 1/2, PG 1-68C) 1 Mar 04 A Stores Inventory Display (F: 1-32B, Sheet 2/2, PG 1-68D) 1 Mar 04 A Weapon Summary Display (P, PG 1-70) 1 Mar 04 A Weapon Summary Display (F: 1-34, 1/3, PG 1-71) 1 Mar 04 A Weapon Summary Display (F: 1-34, 2/3, PG 1-72) 1 Mar 04 A Weapon Summary Display (F: 1-34, 3/3, PG 1-73) 1 Mar 04 A Program Display (PRGM) (F: 1-36, 3/6, PG 1-77) 1 Mar 04 A Program Display (PRGM) (F: 1-36, 4/6, PG 1-78) 1 Mar 04 A (B) (B) LEGEND: (A) DATA ELEMENT: (S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE (B) VALIDATION OR VERIFICATION METHOD: (P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP) V/VS-4

7 WARNING This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs and Performance of unverified procedures may result in injury to personnel or damage to equipment. TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE T.O. NO. BASIC DATE CHANGE NO. DATE PTO CHANGE NO. DATE T.O. 1B-52H DEC 03 CHANGE 2-1 JUL 2005 AMI DATA ELEMENT DATE VALIDATED VALIDATION METHOD DATE VERIFIED VERIFICATION METHOD REMARKS (A) General (Procedures) (P, PG 2-3) 1 Mar 04 A After Engine Start (P, PG 2-7) 1 Mar 04 A MIssile Power Application (P, PG ) 1 Mar 04 A Post Strike/ Abort Procedures (P, PG 2-22) 1 Mar 04 A Selective Jettison Using WCP/SMO (P, PG 3-3) 1 Mar 04 A Selective Jettison Using AJCP (P, PG 3-4) 1 Mar 04 A Emergency Jettison (P, PG 3-5) 1 Mar 04 A Telemetry Power Off Command (CF-57B) (Test Only)(P, PG 4-3) 1 Mar 04 A MIssion Planning Considerations (P, PG 6-7) 1 Mar 04 A OAS/JASSM Operation (P, PG 7-3) 1 Mar 04 A WCE Power Application (P, PG 7-7) 1 Mar 04 A Missile Power Application (P, PG 7-8) 1 Mar 04 A Missile and Ejector Status (P, PG ) 1 Mar 04 A Launch Point Target Number (P, PG 7-12) 1 Mar 04 A Missile GPS Alignment Quality (P, PG 7-12) 1 Mar 04 A JASSM Status & Inventory Display (FRMT-7)(F: 7-4, PG 7-14) 1 Mar 04 A Missile Mission Data and Targeting (P, PG 7-17) 1 Mar 04 A Missile Targeting Methods (P, PG 7-17) 1 Mar 04 A Automatic Targeting (P, PG 7-17) 1 Mar 04 A JASSM Tgt Assign (Manual Targeting) Disp(CF-586)(F: 7-6, 1/2, PG 7-19) 1 Dec 04 A Direct Target Definition Disp(CF-586) (F: 7-7, 2/2, PG 7-20A) 1 Dec 04 A (B) (B) LEGEND: (A) DATA ELEMENT: (S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE (B) VALIDATION OR VERIFICATION METHOD: (P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP) V/VS-5

8 WARNING This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs and Performance of unverified procedures may result in injury to personnel or damage to equipment. TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE T.O. NO. BASIC DATE CHANGE NO. DATE PTO CHANGE NO. DATE T.O. 1B-52H DEC 03 CHANGE 2-1 JUL 2005 AMI DATA ELEMENT DATE VALIDATED VALIDATION METHOD DATE VERIFIED VERIFICATION METHOD REMARKS (A) Missile/Tgt Assign (Man Targeting) Data Entry Proced (P, PG 7-23) 1 Mar 04 A Automatic Launch Determination (P, PG 7-46) 1 Mar 04 A Missile Jettison (P, PG 7-50) 1 Mar 04 A Simulation Capabilities (P, PG 7-51) 1 Mar 04 A Simulated Missile Loadout (P, PG 7-51) 1 Mar 04 A Simulated Targeting Operations (P, PG 7-51) 1 Mar 04 A Simulated WCE Responses (P, PG 7-51) 1 Mar 04 A Simulated Ranging (P, PG 7-51) 1 Mar 04 A SMO Termination (P, PG 7-52) 1 Mar 04 A SMO Restart (P, PG 7-52) 1 Mar 04 A JASSM Master Faults (F: 7-19, 1/17, PG 7-53) 1 Dec 04 A JASSM Master Faults (F: 7-19, 2/17, PG 7-54) 1 Mar 04 A JASSM Master Faults (F: 7-19, 3/17, PG 7-55) 1 Mar 04 A JASSM Master Faults (F: 7-19, 4/17, PG 7-56) 1 Dec 04 A JASSM Master Faults (F: 7-19, 5/17, PG 7-57) 1 Mar 04 A JASSM Master Faults (F: 7-19, 6/17, PG 7-58) 1 Dec 04 A JASSM Master Faults (F: 7-19, 7/17, PG 7-59) 1 Mar 04 A JASSM Master Faults (F: 7-19, 8/17, PG 7-60) 1 Dec 04 A JASSM Master Faults (F: 7-19, 9/17, PG 7-61) 1 Dec 04 A JASSM Master Faults (F: 7-19, 10/17, PG 7-62) 1 Mar 04 A JASSM Master Faults (F: 7-19, 11/17, PG 7-63) 1 Dec 04 A (B) (B) LEGEND: (A) DATA ELEMENT: (S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE (B) VALIDATION OR VERIFICATION METHOD: (P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP) V/VS-6

9 WARNING This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs and Performance of unverified procedures may result in injury to personnel or damage to equipment. TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE T.O. NO. BASIC DATE CHANGE NO. DATE PTO CHANGE NO. DATE T.O. 1B-52H DEC 03 CHANGE 2-1 JUL 2005 AMI DATA ELEMENT DATE VALIDATED VALIDATION METHOD DATE VERIFIED VERIFICATION METHOD REMARKS (A) JASSM Master Faults (F: 7-19, 12/17, PG 7-64) 1 Dec 04 A JASSM Master Faults (F: 7-19, 13/17, PG 7-65) 1 Dec 04 A JASSM Master Faults (F: 7-19, 14/17, PG 7-66) 1 Mar 04 A JASSM Master Faults (F: 7-19, 15/17, PG 7-67) 1 Mar 04 A JASSM Master Faults (F: 7-19, 16/17, PG 7-68) 1 Dec 04 A JASSM Master Faults (F: 7-19, 17/17, PG 7-68A) 1 Dec 04 A JASSM Advisories (F: 7-20, 2/3, PG 7-68C) 1 Dec 04 A JASSM Advisories (F: 7-20, 3/3, PG 7-68D) 1 Dec 04 A JASSM Status Messages (F: 7-21, PG 7639) 1 Mar 04 A Safe Release Advisories (F: 7-22, PG 7-69) 1 Mar 04 A (B) (B) LEGEND: (A) DATA ELEMENT: (S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE (B) VALIDATION OR VERIFICATION METHOD: (P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP) V/VS-7/(V/VS-8 blank)

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11 STATUS OF SAFETY AND OPERATIONAL SUPPLEMENTS T.O. 1B-52H This supplement status page is based on information available to the manual editor as of the date of this publication. The information may not be current as it must be updated by any subsequent supplement status pages and by reference to T.O. 0-1-CD-1. SUPPLEMENTS IN THIS CHANGE Number Date Short Title Section Affected OUTSTANDING SUPPLEMENTS Number Date Short Title Section Affected SS-1(I) 30 September 03 Recycle Weapon Power After Targeting II, VII SS-4(I) 27 January 06 JASSM Launch Criteria II, V, VI Change 3 Flyleaf-1/(Flyleaf-2 blank)

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13 Table of Contents SECTION I DESCRIPTION 1-1 SECTION II NORMAL AIRCREW PROCEDURES 2-1 SECTION III EMERGENCY AIRCREW PROCEDURES 3-1 SECTION IV SUPPLEMENTARY DATA 4-1 SECTION V OPERATING LIMITATIONS 5-1 SECTION VI MISSION PLANNING 6-1 SECTION VII SYSTEMS OPERATION 7-1 GLOSSARY GLOSSARY 1 ALPHABETICAL INDEX INDEX 1 i

14 INTRODUCTION SCOPE. This manual provides aircrews with descriptive and procedural information required for delivery of the AGM-158 Joint Air-To-Surface Standoff Missile (JASSM) from B-52H aircraft modified with Integrated Conventional Stores Management System (ICSMS), and the Standoff Weapon Stores Management Overlay loaded. CHECKLISTS. Abbreviated checklists for the procedures given in this manual are contained in a stand alone Weapon Delivery Checklist. This checklist is identified by a T.O. number that is identical to that of the applicable weapon delivery manual except for the addition of the letters CL (checklist). ARRANGEMENT. This manual is divided into seven sections as follows: Section I, DESCRIPTION Locates, identifies, and functionally describes the weapon and aircraft components which directly concern the aircrew in the control and delivery of the JASSM. Section II, NORMAL AIRCREW PROCEDURES Contains partially illustrated amplified checklists for performance of normal aircrew weapon delivery procedures from preflight through after landing and procedures applicable in the event a mission is aborted. Section III, EMERGENCY AIRCREW PROCEDURES Contains weapon jettison procedures. No attempt is made to regulate or define conditions under which the mission will be aborted. Section IV, SUPPLEMENTARY DATA Contains information on operational test systems. Section V, OPERATING LIMITATIONS Contains important weapon and weapon system limitations that must be taken into account during planning and accomplishment of a mission. Section VI, MISSION PLANNING Contains information on transportation of dangerous material, inflight emergency notification, and inflight mission data changes that can be accomplished by the flightcrew. Section VII, SYSTEMS OPERATION Contains additional material regarding the operation of the aircraft, JASSM systems. Theory of guidance system operation, guidance performance, and malfunction analysis are included. PRECEDENCE. Compliance with procedures herein is mandatory. In all instances, only those operations which are within the scope of the current applicable safety rules may be performed. SAFETY POLICIES. The procedures in this manual reflect the latest applicable rules and policies. Aircrew compliance with these procedures and policies is mandatory. Mission planning shall provide maximum protection to friendly and neutral areas consistent with operational requirements. Selection of launch point and type of maneuver shall be guided by the possible effect upon friendly or neutral areas of a missile guidance or control system failure. Since launch point and type of maneuver are sufficiently flexible to allow for inflight decisions, aircrews shall be briefed concerning the potential disaster hazard to friendly or neutral areas. ii Change 2

15 REFERENCES. The following publications, available to using commands, should be used to gain more comprehensive information on subjects referred to in this technical order: 1B-52H-1 Flight Manual 1B-52H-1-1 Flight Manual - Appendix 1, Performance Data 1B-52H-1-12 Radar Navigator s/navigator s Manual 1B-52H-1-13 Electronic Warfare Officer s Manual 1B-52H-2-31GA-1 General Aircraft/Bomb Release System B-52H 1B-52H Nonnuclear Munitions Loading Procedures 1B-52H Aircrew Weapon Delivery Manual (Nonnuclear) B-52 1B-52H Aircrew Weapon Delivery Manual (Nonnuclear) B-52/AGM-154 JSOW 1B-52H B-52H/AGM-158 Aircrew Weapons Delivery Manual Classified Supplement 1B-52H Aircrew Weapon Delivery Manual (Nonnuclear) B-52/AGM-86C/D 1B-52H-5 Basic Weight Checklist and Loading Data B-52H 1-1M-34 Aircrew Weapons Delivery Manual (Nonnuclear) JMEM Joint Munition Employment Manual SAFETY AND OPERATIONAL SUPPLEMENTS. Information involving flightcrew safety and directly pertaining to the information contained herein will be promptly forwarded to you by Safety Supplements issued against this manual. Safety Supplements covering loss of life will get to you in 48 hours by message (called Interim Safety Supplements) and those concerning serious damage to equipment within 15 days by mail (in a formal printed form). Operational information not involving safety but of an urgent nature will be forwarded to you by Operational Supplements issued against this manual. These will be forwarded by message (interim) or by mail (formal), depending on the urgency of the information. Interim supplements are normally replaced by formal printed supplements at an early date. Formal printed supplements are identified by red letters SS for safety supplements and black letters OS for operational supplements printed around the borders of the pages. The currency of safety and operational supplements affecting your manual can be determined by referring to the Weekly Index of Bomber Aircraft Safety Supplements (T.O. 0-1-CD-1). The title block of each supplement and the title page of this manual should also be checked to determine the effect they may have on existing supplements. You must remain constantly aware of the status of all supplements current supplements must be complied with, but there is no point in restricting your operation by complying with a replaced or rescinded supplement. As a further aid a supplement summary is included in this manual, following the A pages, for both safety and operational supplements: however, this summary can only be as current as this manual. Safety and operational supplements will be filed in accordance with Section VI of the Air Force Technical Order System, T.O WARNINGS, CAUTIONS, AND NOTES. The following definitions apply to Warnings, Cautions, and Notes found throughout the manual. Operating procedures, techniques, etc, which could result in personal injury or loss of life if not carefully followed. Operating procedures, techniques, etc, which could result in damage to equipment if not carefully followed. NOTE An operating procedure, technique, etc, which is considered essential to emphasize. Change 2 iii

16 SHALL, WILL, SHOULD, and MAY. The following definitions apply to the words: SHALL or WILL SHOULD MAY The instructions or procedures prefaced by shall or will are mandatory. Normally used to indicate a preferred but nonmandatory method of accomplishment. An acceptable or suggested means of accomplishment. CHANGE SYMBOLS. Changes to existing material and addition of new material are indicated by one of three types of symbols determined by the nature of the material affected. Text material utilized a vertical line in the margin adjacent to the affected area. New illustrations (figures) utilize a vertical line in the outer margin of the page. Line drawings use a miniature pointing hand to highlight the affected area. Change symbols are not used for blank space resulting from deletions, indexes, and tabular data where changes cannot be identified, relocation of material, or correction of minor inaccuracies unless such correction changes the meaning. RESPONSIBLE AGENCY. Every effort is made to keep this manual current. Review conferences with operating personnel and a constant review of reports assure inclusion of the latest data in this manual. Comments, corrections, and questions regarding this manual should be submitted on AF Form 847 through the local standardization/evaluation unit and routed to 327 BMSG/EN, 3001 Staff Drive Suite 2AF193A, Tinker AFB, Oklahoma RETROFIT CODING. The following code symbols along with the word Less are used to distinguish information related to aircraft that have the described retrofit change incorporated from that which is applicable to aircraft not yet retrofitted. This list contains only TCTO s currently active. Those known to be completed are not included. SYMBOL T.O. NO. TITLE CS 1B-52H-753 1B-52H-756 Installation of Global Positioning System (GPS) on B-52H Aircraft (ECP 0109) Installation of Integrated Conventional Stores Management System (ICSMS) on B-52H Aircraft (ECP 0109) [AMI] 1B-52H-830 Replacement of Ballistics Computer Set AN/AYQ-10 and Inertial Navigation System AN/ASN-136 on B-52H Aircraft. iv Change 3

17 Description section I table of contents page PART 1 B-52/AGM-158 JASSM SYSTEM DESCRIPTION 1-3 B-52/JASSM WEAPON SYSTEM 1-3 B-52 CARRIER EQUIPMENT 1-3 JOINT AIR-TO-SURFACE STANDOFF MISSILE (JASSM) 1-3 JASSM SUSPENSION SYSTEM 1-7 JASSM COVER 1-7 PART 2 OFFENSIVE AVIONICS SYSTEM 1-11 OFFENSIVE AVIONICS SYSTEM (OAS) INTERFACE 1-11 OAS/WEAPON SYSTEM RELATED CONTROLS AND DISPLAYS 1-11 WEAPON JETTISON 1-22 PART 3 JASSM SMO SOFTWARE 1-27 SMO MFD DISPLAYS 1-27 RELEASE ADVISORY DISPLAY 1-27 PRIME MISSION DATA 1-29 CONTROL FUNCTION (CF) DISPLAYS 1-29 FORMAT (FRMT) DISPLAYS 1-56 PROGRAM (PRGM) DISPLAYS /(1-2 blank)

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19 PART 1 - B-52/AGM-158 JASSM SYSTEM DESCRIPTION B-52/JASSM WEAPON SYSTEM The B-52 Joint Air to Surface Standoff Missile (JASSM) weapon system consists of a Conventional Enhancement Modification (CEM) modified B-52 with OAS, and the JASSM. The B-52 aircraft has the capability of releasing 12 JASSM missiles, six from each Heavy Stores Adapter Beam (HSAB) mounted on an Integrated Conventional Stores Management System (ICSMS) external pylon. B-52 CARRIER EQUIPMENT The offensive avionics system (OAS) controls power application, programming, and launch of missiles. The OAS also provides signal processing, storage avionics, control and display panels, missile supervision, regulated dc power conversion, and monitors environmental control equipment in the aircraft. The OAS interfaces with the carrier electrical sources, and panel lighting. Primary missile control and monitor is provided through the OAS weapon control panel (WCP), integrated keyboard (IKB) and the multifunction displays (MFD). The B-52, when configured for JASSM carriage and release, is equipped with the following equipment: OAS Hardware; OAS Software, including the Joint Air-To-Surface Standoff Missile Stores Management Overlay (JASSM SMO); and Less [AMI] the pilots moving map display, which depicts both the In-Range and In-Zone Launch Acceptability Regions (LARs) for the JASSM. For information on the pilots moving map display see GPS IU/TACAN EMULATION in T.O. 1B-52H-1. JOINT AIR-TO-SURFACE STANDOFF MISSILE (JASSM) anti-jam capability is also provided to ensure robust performance. The no-seeker mission option provides excellent performance against soft targets using GPS/Inertial guidance to target impact. The seeker is employed against targets requiring high impact precision. The no-seeker mission option can be used in a GPS/Inertial terminal guidance mode. The JASSM is trapezoidal in cross section. The fuselage is constructed from composite shells of a sandwiched foam core construction. An internal hardback assembly and several bulkheads provide structural strength. A pair of folding lugs with 30 inch spacing is provided for mating to the ejector rack. Flight surfaces (wings) are stowed in a folded location under the fuselage and are pyrotechnically deployed after launch. A single vertical tail surface assists in steering control. The vertical tail surface is stowed in a folded position and is also pyrotechnically deployed after launch. Electrical connection to the B-52 is made via a MIL-STD-1760 cable interface through the missile umbilical connector just aft of the rear launch lug. After release, pyrotechnics are fired to deploy both the flight surfaces and the vertical tail. Propulsion is provided by a liquid fueled (JP-10) Teledyne 370 series turbojet engine. JASSM uses a 1000-pound class WDU-42/B warhead with a FMU-156B fuze. The aircraft MIL- STD-1760 cable connection to the missile umbilical is the only electrical connection to the missile. All missile arming and flight transition actions are electronically controlled within the missile after missile release. No other lanyards or release devices are required between the host aircraft and the JASSM. JASSM physical characteristics are as follows: The AGM-158A JASSM, figure 1-1, is an airlaunched, medium range autonomous cruise missile. JASSM is designed as a launch and leave weapon system, in that once launched, the missile will navigate to and engage its planned target with no further control communication from the launching aircraft or other command agency. The use of the Infrared (IR) seeker in the nose of the missile is optional based on target requirements. The missile uses a tightly coupled Global Positioning System (GPS) aided Inertial Navigation System (INS) for mid-course and terminal area navigation. A GPS Length Width Height Lug Spacing Wing Span (fully deployed) Engine Weight Seeker Guidance Warhead 168 inches 24.9 Inches 20.4 Inches 30 inches 120 inches Teledyne 370 series Turbojet 2250 pounds Infrared GPS/Inertial WDU-042 One Thousand Pound Class Change 3 1-3

20 Joint Air to Surface Standoff Missile (JASSM) Figure

21 FUSELAGE The fuselage has a pointed nose with a trapezoidal cross section. Two covers close out the bottom of the fuselage. The forward cover encloses the IR seeker, Inertial Measuring Unit (IMU), Missile Control Unit (MCU), warhead and the wing section, while fitting around the forward inlet lips; the aft cover encloses the propulsion section and aft fuel tank and test instrumentation kit areas. The fabricated skins are constructed of stiffened foam cores contained between composite panels. The bulkheads consist of a superframe assembly and 2 conventional frames. The superframe assembly supports the launch lug, ejector and sway brace loads, and missile retention. The aft lower bridge encloses the warhead below the aft lug. The main superframe and the wing carry-through are fabricated from stainless steel. The superframe assembly is split horizontally to allow the installation of the warhead late in the assembly process. The composite forward frame provides stiffness. The engine/ tail frame secures the engine to the upper fuselage, the vertical fin actuator and the vertical fin root. WINGS The missile has two deployable wings. The wings have a constant chord and thickness except at the wing fuselage intersection where the upper wing surface transitions to a flat surface for the wing pivot integration. Mechanical latches hold the wings next to the missile fuselage until launch to prevent flutter during captive carriage. The wings are deployed in a two step process, using a twostage pyrotechnic actuator. The wings are commanded to extend to 75 degrees when clear of the launch aircraft. This first deployment position increases pitch stability to aid separation from the host aircraft. The wings move from 75 degrees to a 45 degree sweep position for cruise when initial pitch stability is achieved. The 45 degree sweep position aids longitudinal stability and contributes a large dihedral effect. The wing deployment mechanism connects both the left and right wings to ensure symmetrical deployment. An elevon located on the outer portion of each wing provides pitch and roll control. The elevons are not effective until the wings are deployed to 45 degrees. Roll control is provided by differential elevon deflections and pitch control by symmetrical deflection. Electro-mechanical actuators mounted inside the wing spars drive the elevons. VERTICAL TAIL The vertical tail is constructed similar to the wings. Prior to launch the tail is folded over 135 degrees and held in place by a mechanical latch. After launch a pyrotechnic actuator located in the folded tail fires to erect and latch the tail. The entire vertical tail pivots on a metallic shaft for yaw control. The electro-mechanical rotary yaw actuator is located inside the aft fuselage. The Bomb Impact Assessment (BIA) antenna is located in the vertical fin. BLOW OFF WEDGES Two expendable wedges are located on the underside of each aft strake and held in place by pyrotechnic retention pins. The wedges insure the missile makes a clean separation from the aircraft and are jettisoned from the missile after a fixed delay following launch. Wedge separation occurs after wings are deployed. WARHEAD The WDU-42/B warhead provides the hard target penetration, detonation, and blast/fragmentation damage capabilities for the JASSM. The warhead consists of the loaded case, containing PBX(AF)-757 insensitive munition fill, and an FMU-156/B fuze. The warhead is capable of penetrating and defeating hardened underground facilities as well as destroying soft targets. Arming power is provided only from the JASSM engine alternator. The FMU-156/B is a programmable fuze. The fuze is installed in the aft well of the warhead case and secured with a retaining ring. The FMU-156/B modes of operation are BIT, arm, impact fire and command fire. The command fire delay times are instantaneous, 10, 15 20, 30, 40, 50 and 120 milliseconds. Fuze settings are established during mission planning and can be changed in flight. FUEL SYSTEM Fuel (JP-10) is carried in four fuselage fuel tanks made of aluminum. The fuel system distributes fuel from the tanks to the engine, transfers fuel between tanks, and vents the tanks during filling. The fuel tanks are pressurized by engine bleed air during missile powered flight. Fuel from the tanks is fed to the fuel pump where pressure is boosted to the pressure level required by the engine for engine start. 1-5

22 ENGINE A Teledyne turbojet powers the vehicle. The flush lower surface mounted inlet has full line of sight blockage. The nozzle also provides for an ejector flow to aid engine compartment cooling. A pyrotechnic cartridge starts the engine. The engine has a variable throttle for optimal cruise or airspeed control to meet the time on target requirement. AIR DATA SYSTEM The air data system is composed of an Air Data Probe (ADP), one Flush Static Port (FSP), and related sensor cards as part of the avionics package. The air data system is equipped with anti-ice heaters on both the ADP and FSP. Weapon (115VAC) power for missile loaded locations applies warmup power to these heaters. Warm-up time may take up to 13 minutes depending on ambient temperature. The heaters remain on as long as 115 VAC power is applied. Temperatures for these heaters can reach 250 degrees F. Heaters are on during any WIU operations. Without proper warm-up time, icing can degrade the missile pitot-static system such that mission failure could occur. Ensure the JASSM heater power is applied (WIU ON) at least 15 minutes prior to launch. If icing conditions are encountered prior to 15 minutes of heater operation, then a minimum warm-up time of 30 minutes is required prior to launch. AVIONICS The JASSM Avionics consists of the Missile Control Unit (MCU), Seeker Assembly, JASSM Anti-jam Global Positioning System Receiver (JAGR or JAGR- S), and associated antennas. The seeker assembly consists of the gimbaled IR imaging sensor and IMU. Missile Control Unit (MCU) The MCU provides electrical power distribution along with centralized communication, timing, control and processing for the operation of the missile, and generates telemetry data. Its functional elements consist of a squib and power distribution CCA, a system interface and processing CCA, and actuator control CCA; and air data transducer assembly; a BIA transmitter; and an Electromagnetic Interference (EMI) filter assembly. IR Seeker Assembly The IR seeker assembly consists of a dual axis lineof-sight gimbal assembly, a sensor assembly; optics, reference wheel assembly; a squib activated gas bottle for cooling the sensor to cryogenic temperatures; and an Inertial Measurement Unit (IMU). The IMU is attached to the seeker assembly to ensure dynamic alignment. JASSM Anti-Jam Global Positioning System Receiver (JAGR) and JAGR-S Selective Availability Anti-Spoofing Module (SAASM) The JAGR provides the MCU with GPS measurement data computed from GPS satellite data collected in a jamming environment. Critical functions performed by the JAGR include: acceptance of initialization data, acceptance of inertial aiding data from the MCU, receiving GPS satellite and jammer signals from the antenna, minimization of the jammer to GPS signal ratios, satellite selection, GPS receiver control, computation of GPS data, and BIT. The JASSM Anti-Jam GPS Receiver-SAASM (JAGR- S) is a high fidelity Anti-Jam GPS receiver. It achieves its Anti-Jam performance through the integration of a multi-channel analog RF Front End, the implementation of Space-Time Adaptive signal processing algorithms in digital nuller/front beamformer electronics and GPS measurement algorithms in a digital receiver back-end. The JAGR-Ss critical task is to provide GPS satellite line-of-sight (LOS) Range and Delta-range measurements to the Navigation functions algorithms in the MCU. In order to provide these measurements, the JAGR-S receives Position, Time and Velocity Initialization data and inertial aiding data from the MCU and tracks GPS satellite signals from the GPS satellite through a Controllable Radiation Pattern (CRPA) antenna. In the case of operation in a jamming environment, the digital beamformer/nuller adaptively and dynamically nulls signals in the direction of the jammers while simultaneously steering multiple higher gain producing signal reception beams in the known directions of the GPS satellites. This provides interference-free LOS measurements to the MCU s navigation function. Bomb Impact Assessment (BIA) System The BIA system s primary function is to transmit missile terminal engagement status and missile health data just prior to target impact. The transmitter provides 25 watts of output power and is capable of transmitting data at 2400 Bps rate to a line-of-sight airborne platform such as the RC-135 (RIVET JOINT) aircraft. The BIA transmitter is connected to an antenna mounted in the tail for tactical operation. The BIA begins sending repeated messages approximately 10 seconds prior to impact. 1-6 Change 1

23 JASSM SUSPENSION SYSTEM JASSMs are carried externally on CEM modified wing pylon weapon suspension assemblies which are attached to the wing pylon adapter. Up to 6 JASSMs can be carried on each B-52 wing pylon. Figure 1-2 illustrates the JASSM suspension system. Each suspension assembly consists of the following: Stub Pylon (Modified Wing Pylons) Heavy Stores Adapter Beam (HSAB) MAU-12 Ejector Racks (6 JASSM) The HSAB is attached to the stub pylon on each wing and houses the wire harnesses for missile control and release. The adapter beam has provisions for carrying 6 JASSMs on stations 1, 2, 3, and 6, 7, 8. The MAU-12 ejector rack (figure 1-3) is used to suspend and release the missiles. Each rack is equipped with two hooks and four sway braces which hold and support the missile. Two ejector feet, one near each hook between each pair of sway braces, ejects the missile when release is commanded. The rack has provisions for a ground safety lockpin and an inflight safety lock. An extension has been added to the rack which contains the umbilical restraint. This restraint is a cable which holds the umbilical cable in position to help ensure a clean missile separation when the missile is released. Electrical circuits to the inflight safety lock are available but not used. Therefore, a bolt with nut is installed in the inflight safety lockout pin hole of each MAU-12 rack. The ground safety lockpin is used to prevent operation of the racks while on the ground. JASSM COVER The missile is covered with an environmental cover, whenever it is outside the shipping and storage container, which includes when loaded on external stores stations for ground alert and other extended periods. The environmental cover serves to protect air data probe ports, static ports, and engine openings from dirt, debris and any other hazards that may be the result of poor environmental conditions. The environmental cover is required, due to warranty considerations. The effects of environmental contamination on weapon reliability and accuracy are unknown. 1-7

24 Heavy Stores Adapter Beam JASSM Configuration Figure

25 MAU-12 Ejector Rack With Extension 1 INFLIGHT SAFETY LOCKOUT PIN 2 QUICK RELEASE PIN 3 LANYARD CHANNEL 4 QUICK RELEASE PIN 5 UMBILICAL RESTRAINT A HOLE 6 UMBILICAL RESTRAINT B HOLE 7 UMBILICAL RESTRAINT C HOLE 8 CAMLOCK FASTENER 9 LEFT PLATE ASSEMBLY 10 FORWARD CABLE LANYARD 11 UMBILICAL CABLE LANYARD 12 CENTER CHANNEL ASSEMBLY Figure /(1-10 blank)

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27 PART 2 - OFFENSIVE AVIONICS SYSTEM OFFENSIVE AVIONICS SYSTEM (OAS) INTERFACE Less [AMI] The B-52 Integrated Conventional Stores Management System (ICSMS) provides OAS control for release of JASSM. The ICSMS operational computer program consists of a Ground Maintenance Computer Program (GMCP) and Flight Computer Program (FCP). The GMCP is not discussed. The FCP consists of the Flight Management System (FMS) and JASSM Stores Management Overlay (JASSM SMO). For further information regarding ICSMS and basic SMO functions, refer to INTEGRATED CONVENTIONAL STORES MANAGEMENT SYSTEM, T.O. 1B-52H Less [AMI] The JASSM SMO software controls JASSM functions. The Navigation and Weapon Delivery (NAWD) ACU executes the navigation and weapon delivery functions for the SMO. The Controls and Displays (CAD) ACU executes the controls and displays function along with a majority of the BIT (Built In Test) processing. [AMI] The B-52 OAS provides control for programming and release of JASSM. The operational computer program consists of a Ground Maintenance Computer Program (GMCP) and Flight Computer Program (FCP). The GMCP is not discussed. The FCP consists of the Flight Management System (FMS), Common Stores Processing (CSP), and JASSM Stores Management Overlay (JASSM SMO). For further information regarding OAS and basic SMO functions, refer to T.O. 1B-52H [AMI] The OAS provides the capability for controlling and monitoring more than one type of weapon system at a time. This is accomplished by the CSP and loading multiple weapon SMOs. Currently, only the CALCM SMO may be loaded with the JASSM SMO. With the CALCM and JASSM SMOs loaded, MIU/WIU power, environmental conditioning and monitor capabilities are available to all the CALCM and JASSM weapons. However, all other weapon functions are available only to those weapons controlled by the Primary SMO. [AMI] If the JASSM SMO is not the Primary SMO, only WIU power, heating and monitoring functions (FRMT 7A, 7C and 77) are available for the missiles. [AMI] If the JASSM SMO is not the Primary SMO and a mission planned JASSM launch point is 30 minutes away, a JASSM EVENT advisory message will be displayed. [AMI] If the JASSM SMO is not the Primary SMO and a mission planned JASSM launch point is 25 minutes away, a JASSM EVENT master fault will be displayed. OAS/WEAPON SYSTEM RELATED CONTROLS AND DISPLAYS Operator controls and displays for weapon release system control are located at the pilots and navigators stations. The munitions consent panel is located at the pilots station. The Weapon Control Panel (WCP), OAS Power Control Panel (OAS PCP), keyboards, MFD, and computer control panel are located at the navigators station. See figure 1-4 for OAS/weapon data flow. Weapon Control Panel The Weapon Control Panel (WCP) (figure 1-5), located on the navigator s front panel, provides controls for missile power application, missile power removal, missile jettison, or missile abort. Missiles are selected with the LOCATION (LP and RP) and STATION (1, 2, 3, 6, 7, 8, and ALL) switches. The WCP station switches are enabled only when one or both pylon locations have been selected. If no location is selected when either the ALL station switch or an individual station switch has been selected, the advisory message LOCATION?? will be displayed on each MFD. If the bay location is selected the advisory B: LOCATION will be displayed on each MFD. If an invalid station (4 or 5) is selected, the advisory Less [AMI] STATION??, [AMI] JASSM STATION?? will be displayed on each MFD. NOTE [AMI] With JASSM designated as the Primary SMO (CF-62x), all JASSM weapon functions are available. The JASSM can be powered, aligned, monitored, targeted, ranged, launched and jettisoned (through OAS). Change

28 WEAPON CONTROL PANEL ABNORMAL PROCEDURES An advisory WCP on the MFD indicates malfunction on the WCP. The operator will use CF-E (figure 1-26) to back up actions accomplished on the WCP. This will allow the operator to work around certain failures of the WCP and OAS PCP. NOTE With a total WCP failure prior to accomplishing hardwired function, (LOCK-UN- LOCK) missile release is not possible. CF-E may be used in conjunction with an operational WCP and OAS PCP to operate the system. The operators may use keyboard entries to perform functions mechanized on these panels at any time regardless of the panels go/no-go status. The OAS will treat the keyboard command as if it had originated from the WCP or OAS PCP. The lock-unlock function is not available on the CF-E backup. The display is laid out in basically the same arrangement as the panel. To accomplish a backup action for the malfunctioning panel switch, the operator enters CF-E and the symbols associated with the switch on the keyboard in the same sequence that normal switch operation would occur. See CF-E this section for further discussion of the CF-E functions. Pilot s Munitions Consent Panel The pilot s munitions consent panel (figure 1-6) contains the PREARM-OFF and LOCK-UNLOCK switches. The panel provides unlock consent for powering the weapon ejectors. The PREARM function of the pilot s switch is not used with JASSM. The LOCK-UNLOCK switch is guarded in the LOCK position. OAS Power Control Panel The OAS Power Control Panel (PCP) (figure 1-7) located on the navigators front panel provides power control for the OAS and the WIU (Weapon Interface Unit). All legends are backlighted green when power is on. The MIU switches which command power to the WIU are alternate action pushbuttons and will remain latched if the WIU loses power or is shut down by the OAS. The light in the switch is software controlled and will go out when WIU power is removed regardless of switch position. To reapply power to the WIU when they have been shut down by other than the operator, the switch must be pressed and released to reset the switch and then pressed a second time to reapply WIU power. If PCP switches malfunction, the navigator or radar navigator can select CF-E which provides a display of the PCP switches. Keyboard The keyboards (figure 1-8) located at the navigator s and radar navigator s stations, provide interface with the control of the OAS and weapon system. The keyboard and MFD provide operator interface with the missiles through the selection of format (FRMT), control function (CF), program (PRGM), and modify (MDFY) commands. The selection of FRMT results in the display of a specific OAS and missile data presentation on the selected MFD. Control function selection results in display of a specific OAS data display or initiates the entry into a specific operating mode. If WCP switches malfunction, the navigator or radar navigator can select CF-E which provides a display of the WCP switches and the MIU power switches. IKB commands associated with the JASSM are listed in figure 1-9. MULTIFUNCTION DISPLAYS The multifunction display (MFD) (figure 1-10) is a CRT display unit. The MFD displays scan converted radar video, electro-optical viewing system (EVS) video, and alphanumeric mission data. Two MFDs are located at the navigator s station and two at the radar navigator s station. MFD DISPLAY FIGURES In the MFD display figures in this T.O., the items modifiable by the operator or the SMO are represented in the display explanations as lower case (non-capital) letters. The labels which are not modifiable are presented in all capital letters Change 2