1.1 AIRCRAFT . . . 1−1 1.1.1 Aircraft Weight . . . 1−1 1.1.2 Cockpit . . . 1−1 1.1.3 Electronic Nomenclature . . . 1−2 1.1.4 Technical Directives . . . 1−2 1.1.5 Block Numbers . . . 1−2
CHAPTER 2 SYSTEMS
2.1 AIR INLET CONTROL SYSTEM (AICS) . . . 2−1 2.1.1 Normal AICS Operations . . . 2−1 2.1.2 AICS Test . . . 2−1 2.1.3 AICS Failure Modes of Operation . . . 2−4 2.1.4 AICS Anti−Ice . . . 2−9 2.2 ENGINE . . . 2−9 2.2.1 Engine Control . . . 2−11 2.2.2 Variable Exhaust Nozzle . . . 2−16 2.3 FATIGUE ENGINE MONITORING SYSTEM . . . 2−18 2.3.1 FEMS Functional Description. . . 2−18 2.3.2 FEMS Operation . . . 2−21 2.3.3 FEMS and OBC. . . 2−21 2.4 ENGINE FUEL SYSTEM . . . 2−21 2.4.1 Motive Flow Fuel Pump . . . 2−21 2.4.2 Engine Fuel Boost Pump. . . 2−21 2.4.3 Main Fuel Pump . . . 2−21 2.4.4 Main Engine Control. . . 2−21 2.4.5 Afterburner Fuel Pump . . . 2−23 2.4.6 Afterburner Fuel Control. . . 2−23 2.5 THROTTLES . . . 2−23 2.5.1 Throttle Control Modes. . . 2−23 2.6 ENGINE BLEED AIR . . . 2−27 2.6.1 Engine Anti−Ice . . . 2−27 2.6.2 Environmental Control System Leak Detection. . . 2−29 2.7 ENGINE COMPARTMENT VENTILATION . . . 2−30 2.7.1 Engine In−Flight Ventilation . . . 2−30 2.7.2 Engine Ground Ventilation . . . 2−30
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2.8 ENGINE IGNITION SYSTEM . . . 2−30 2.8.1 Main High−Energy Ignition. . . 2−30 2.8.2 Afterburner Ignition . . . 2−32 2.8.3 Backup Ignition. . . 2−32 2.9 ENGINE STARTING SYSTEM . . . 2−32 2.9.1 External Airstart . . . 2−32 2.9.2 Engine Crank. . . 2−32 2.9.3 Crossbleed Start. . . 2−34 2.9.4 Airstarts . . . 2−34 2.10 ENGINE OIL SYSTEM . . . 2−34 2.10.1 Oil Cooling . . . 2−35 2.10.2 Oil Pressure Indicators . . . 2−35 2.10.3 OIL HOT Caution Lights . . . 2−35 2.11 ENGINE INSTRUMENTS . . . 2−35 2.11.1 Engine RPM Indicator. . . 2−35 2.11.2 Exhaust Gas Temperature Indicator . . . 2−35 2.11.3 Fuel Flow Indicator . . . 2−37 2.11.4 Engine Instrument Group BIT . . . 2−37 2.11.5 Engine Instrument Group Self−Test . . . 2−37 2.11.6 Engine Oil Pressure Indicator . . . 2−37 2.11.7 Exhaust Nozzle Position Indicator . . . 2−37 2.11.8 Engine Monitor Display Format . . . 2−37 2.11.9 MFD Engine Caution Legends . . . 2−38 2.11.10 Engine Stall/Overtemperature Warning . . . 2−38 2.12 FIRE DETECTION SYSTEM . . . 2−39 2.12.1 Fire Detection Test . . . 2−40 2.13 FIRE EXTINGUISHING SYSTEM . . . 2−40 2.13.1 Fire Extinguisher Pushbuttons . . . 2−40 2.13.2 Fire Extinguisher Advisory Lights . . . 2−40 2.13.3 Fire Extinguisher Test . . . 2−40 2.14 AIRCRAFT FUEL SYSTEM . . . 2−40 2.14.1 Fuel Tankage . . . 2−42 2.14.2 Fuel Quantity System . . . 2−42 2.14.3 Engine Feed. . . 2−43 2.14.4 Fuel Transfer . . . 2−50 2.14.5 Fuel Quantity Balancing . . . 2−54 2.14.6 Fuel Transfer/Feed During Single−Engine Operation. . . 2−54 2.14.7 Fuel Dump. . . 2−55 2.14.8 Internal Tank Pressurization and Vent . . . 2−56 2.14.9 Fueling and Defueling. . . 2−56 2.14.10 In−Flight Refueling . . . 2−57 2.14.11 Hot Refueling . . . 2−58 2.14.12 Automatic Fuel Electrical Controls . . . 2−59 2.15 ELECTRICAL POWER SUPPLY SYSTEM . . . 2−59 2.15.1 Normal Electrical Operation . . . 2−59
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2.15.2 Electrical Power Distribution . . . 2−61 2.15.3 Degraded Electrical Operation . . . 2−62 2.16 HYDRAULIC POWER SUPPLY SYSTEMS . . . 2−69 2.16.1 Flight and Combined Systems . . . 2−69 2.16.2 Hydraulic Power Distribution . . . 2−72 2.16.3 Outboard Spoiler System . . . 2−73 2.16.4 Backup Flight Control System . . . 2−73 2.17 PNEUMATIC POWER SUPPLY SYSTEMS. . . 2−77 2.17.1 Normal Canopy Control . . . 2−77 2.17.2 Auxiliary Canopy Open Control . . . 2−77 2.17.3 Emergency Gear Extension. . . 2−77 2.18 MISSION COMPUTER SYSTEM . . . 2−77 2.18.1 Aircrew Interface . . . 2−77 2.18.2 Operational States . . . 2−79 2.18.3 Aircraft Master Modes . . . 2−79 2.19 STANDARD CENTRAL AIR DATA COMPUTER . . . 2−79 2.19.1 Standard Central Air Data Computer Tests . . . 2−79 2.20 WING−SWEEP SYSTEM . . . 2−82 2.20.1 Wing−Sweep Performance. . . 2−82 2.20.2 Wing−Sweep Modes . . . 2−83 2.20.3 Wing−Sweep Interlocks . . . 2−87 2.20.4 Wing−Sweep System Test . . . 2−87 2.21 FLAPS AND SLATS . . . 2−89 2.21.1 Flap and Slat Controls. . . 2−89 2.21.2 Flap and Slat Operation. . . 2−93 2.22 SPEEDBRAKES . . . 2−95 2.22.1 Speedbrake Operation . . . 2−95 2.23 FLIGHT CONTROL SYSTEMS . . . 2−97 2.23.1 Longitudinal Control . . . 2−97 2.23.2 Integrated Trim System. . . 2−97 2.23.3 Lateral Control . . . 2−102 2.23.4 Spoiler Control . . . 2−105 2.23.5 Yaw Control. . . 2−107 2.23.6 Direct Lift Control . . . 2−109 2.24 DIGITAL FLIGHT CONTROL SYSTEM . . . 2−109 2.24.1 Stability Augmentation System . . . 2−110 2.24.2 Voltage Monitoring . . . 2−125 2.24.3 Autopilot . . . 2−125 2.24.4 Pilot Relief and Guidance Modes . . . 2−126 2.24.5 DFCS Test . . . 2−129 2.24.6 DFCS Control Panel Fault Reporting . . . 2−131 2.25 LANDING GEAR SYSTEMS . . . 2−132 2.25.1 Landing Gear Handle . . . 2−132 2.25.2 Main Landing Gear . . . 2−133
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2.25.3 Nose Landing Gear . . . 2−133 2.25.4 Landing Gear Normal Operation . . . 2−135 2.25.5 Emergency Gear Extension. . . 2−136 2.26 WHEELBRAKE SYSTEM. . . 2−136 2.26.1 Brake Characteristics . . . 2−138 2.26.2 Normal Braking. . . 2−138 2.26.3 Antiskid . . . 2−138 2.26.4 Auxiliary Brake. . . 2−140 2.26.5 BRAKES Warning Light. . . 2−140 2.26.6 Parking Brake . . . 2−140 2.26.7 Wheel Antirotation . . . 2−141 2.27 NOSEWHEEL STEERING SYSTEM . . . 2−141 2.27.1 Nosewheel Steering Control . . . 2−141 2.27.2 Nosewheel Centering . . . 2−143 2.27.3 Shimmy Damping . . . 2−143 2.28 NOSEGEAR CATAPULT SYSTEM . . . 2−143 2.28.1 Nose Strut Kneel . . . 2−143 2.28.2 Launch Bar . . . 2−145 2.28.3 Holdback Fitting . . . 2−145 2.29 ARRESTING HOOK SYSTEM . . . 2−145 2.29.1 Arresting Hook Operation . . . 2−145 2.30 ENVIRONMENTAL CONTROL SYSTEM . . . 2−148 2.30.1 ECS Air Sources . . . 2−148 2.30.2 Cockpit Air−Conditioning . . . 2−151 2.30.3 Electronic Equipment Cooling . . . 2−152 2.30.4 Pressurization . . . 2−152 2.30.5 Windshield Air and Anti−Ice . . . 2−154 2.30.6 Gun−Gas Purging . . . 2−154 2.30.7 Degraded ECS Operation . . . 2−154 2.31 OXYGEN SYSTEM . . . 2−157 2.31.1 On−Board Oxygen Generating System (OBOGS) . . . 2−157 2.31.2 Backup Oxygen System (BOS). . . 2−159 2.31.3 BOS Pressure Indicator . . . 2−160 2.31.4 Emergency Oxygen Supply. . . 2−160 2.32 PITOT−STATIC SYSTEM . . . 2−160 2.32.1 Pitot−Static Heat . . . 2−160 2.33 CONTROL AND DISPLAY SYSTEM . . . 2−161 2.33.1 Display Types . . . 2−161 2.33.2 Display Processors . . . 2−169 2.33.3 System Operation . . . 2−169 2.33.4 Heads−Up Display (HUD) . . . 2−169 2.33.5 Multistatus Indicator (MSI). . . 2−170 2.33.6 Multifunction Displays (MFD) . . . 2−174 2.33.7 Cursor Controls . . . 2−174 2.33.8 Displays, Formats, and Symbology . . . 2−176 2.33.9 MFD Formats . . . 2−197
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2.34 DATA ENTRY UNIT . . . 2-242 2.34.1 Data Entry Unit Operating Modes . . . 2-242 2.34.2 DEU Menu Pages . . . 2-248 2.35 FLIGHT INSTRUMENTS . . . 2-248 2.35.1 Standby Attitude Indicator . . . 2-248 2.35.2 Standby Airspeed Indicator. . . 2-250 2.35.3 Standby Altimeter . . . 2-250 2.35.4 AN/APN-194(V) Radar Altimeter System . . . 2-250 2.35.5 Vertical Velocity Indicator . . . 2-251 2.35.6 Standby Compass . . . 2-251 2.35.7 Clock . . . 2-251 2.36 ANGLE-OF-ATTACK SYSTEM . . . 2-251 2.36.1 AOA Test . . . 2-251 2.36.2 AOA Indicator . . . 2-251 2.36.3 AOA Indexer . . . 2-251 2.36.4 Approach Lights . . . 2-251 2.37 CANOPY SYSTEM . . . 2-254 2.37.1 Canopy Operation . . . 2-255 2.38 EJECTION SYSTEM . . . 2-256a 2.38.1 Ejection Seat . . . 2-258 2.38.2 Command Ejection Lever . . . 2-263 2.38.3 Ejection Initiation . . . 2-263 2.38.4 Seat Operation After Ejection. . . 2-265 2.39 LIGHTING SYSTEM . . . 2-265 2.39.1 Exterior Lights . . . 2-265 2.39.2 Interior Lights . . . 2-268 2.39.3 Warning and Indicator Lights . . . 2-269 2.40 STORES MANAGEMENT SYSTEM/JETTISON . . . 2-278 2.40.1 SMS Weapons Replaceable Assemblies . . . 2-278 2.40.2 Multistatus Indicator (MSI). . . 2-279 2.40.3 Stores Jettison Modes . . . 2-279 2.41 MISCELLANEOUS EQUIPMENT . . . 2-283 2.41.1 Boarding Ladder . . . 2-283 2.41.2 Nose Radome . . . 2-283 2.41.3 Systems Test and System Power Ground Panel . . . 2-283 2.41.4 External Baggage Container (CNU-188/A) . . . 2-284 CHAPTER 3 — SERVICING AND HANDLING
3.1 SERVICING DATA. . . 3-1 3.1.1 Ground Refueling . . . 3-1 3.1.2 Engine Oil . . . 3-4 3.1.3 Integrated Drive Generator Oil . . . 3-4 3.1.4 Hydraulic Systems. . . 3-4 3.1.5 Pneumatic Systems . . . 3-8
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3.2 GROUND HANDLING . . . 3−8 3.2.1 Danger Areas. . . 3−8 3.2.2 Radar Radiation Areas . . . 3−8 3.2.3 Towing Turn Radii and Ground Clearances . . . 3−15 3.2.4 Tiedown Points . . . 3−15 CHAPTER 4 OPERATING LIMITATIONS
4.1 LIMITATIONS . . . 4−1 4.1.1 Engine Limits . . . 4−1 4.1.2 Starter Limits. . . 4−1 4.1.3 Airstart Envelope . . . 4−1 4.1.4 Crosswind Limits . . . 4−1 4.1.5 Ground Operations Limits. . . 4−1 4.1.6 Ejection Seat Operation Limits. . . 4−1 4.1.7 Autopilot Limits . . . 4−1 4.2 AIRSPEED LIMITATIONS . . . 4−1 4.2.1 Maximum Airspeeds . . . 4−5 4.3 ACCELERATION LIMITS . . . 4−5 4.3.1 Cruise Configuration . . . 4−5 4.3.2 Approach Configuration . . . 4−5 4.4 ANGLE−OF−ATTACK LIMITS . . . 4−5 4.4.1 Cruise Configuration . . . 4−5 4.4.2 Approach Configuration . . . 4−10 4.5 MANEUVERING LIMITS . . . 4−10 4.5.1 Approach Configuration . . . 4−10 4.5.2 Cruise Configuration . . . 4−10 4.5.3 Rolling Limits . . . 4−10 4.5.4 Sideslip Limits . . . 4−10 4.5.5 Prohibited Maneuvers . . . 4−10 4.6 SAS LIMITS . . . 4−13 4.7 TAKEOFF AND LANDING FLAP AND SLAT AND TRANSITION LIMITS. . . 4−13 4.7.1 Clean and Symmetric Stores Loading. . . 4−13 4.7.2 External Stores Loading With Up to 66,000 Inch−Pounds (5,500 Foot−Pounds) Asymmetry
(AIM−7 on Stations 1B or 8B equals 63,000 inch−pounds) . . . 4−18 4.7.3 External Stores Loading With Greater Than 66,000 Inch−Pounds (5,500 Foot−Pounds) Asymmetry 4−18 4.8 GROSS WEIGHT LIMITS TAKEOFF, LAUNCH, AND LANDING . . . 4−18 4.9 BARRICADE ENGAGEMENT LIMITS . . . 4−18 4.10 CENTER OF GRAVITY POSITION LIMITS . . . 4−18
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4.11 EXTERNAL STORES AND GUN LIMITS . . . 4−19 4.11.1 280−Gallon External Fuel Tank Limits . . . 4−19 4.11.2 External Baggage Container (CNU−188/A) . . . 4−19 4.11.3 Gun Burst Limits. . . 4−19 4.11.4 Launch Limits . . . 4−19 4.11.5 Jettison Limits . . . 4−20 4.12 BANNER TOWING RESTRICTIONS . . . 4−20 4.13 TACTICAL AIR RECONNAISSANCE POD SYSTEM LIMITATIONS . . . 4−21 4.13.1 Authorized Stores Loading . . . 4−21 4.13.2 Interim AIM−7 as Ballast . . . 4−21 PART II INDOCTRINATION
CHAPTER 5 INDOCTRINATION
5.1 GROUND TRAINING SYLLABUS . . . 5−1 5.1.1 Minimum Ground Training Syllabus . . . 5−1 5.1.2 Waiving of Minimum Ground Training Requirements . . . 5−1 5.2 FLIGHT TRAINING SYLLABUS . . . 5−2 5.2.1 Flightcrew Flight Training Syllabus . . . 5−2 5.2.2 Flightcrew Flight Training Phases . . . 5−2 5.3 OPERATING CRITERIA . . . 5−2 5.3.1 Ceiling/Visibility Requirements . . . 5−2 5.3.2 NATOPS Qualification and Currency Requirements . . . 5−3 5.3.3 Requirements for Various Flight Phases . . . 5−4 5.3.4 Mission Commander . . . 5−4 5.3.5 Minimum Flightcrew Requirements . . . 5−5 5.4 FLIGHT CREWMEMBER FLIGHT EQUIPMENT REQUIREMENTS . . . 5−5 PART III NORMAL PROCEDURES