AV-8B Harrier IIDCS WORLD Startup Checklist · 123 steps
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U.S. Marine Corps / Wikimedia CommonsPublic Domain
AttackCold War
AIRCRAFT BRIEF
The McDonnell Douglas AV-8B Harrier II is a single-engine, V/STOL (Vertical/Short Takeoff and Landing) ground-attack aircraft operated by the U.S. Marine Corps. Entering service in 1985, it can operate from amphibious assault ships, austere forward bases, and even road strips. Its Rolls-Royce Pegasus engine with four rotating nozzles allows it to transition between hovering like a helicopter and flying like a conventional jet.
SPECIFICATIONS
manufacturerMcDonnell Douglas / BAe (now Boeing)
first Flight1981
roleV/STOL attack aircraft
crew1 pilot
engines1x Rolls-Royce F402-RR-408 Pegasus (23,500 lbf)
max Speed1,065 km/h (575 kts)
range2,200 km (1,200 nmi)
ceiling50,000 ft
weight14,061 kg (MTOW — STO)
PHS 1 — Electrical / Pre-Start7 steps
| 01 | Throttle | OFF | |
| 02 | Parking Brake | SET | |
| 03 | Nozzle LeverNOTE: Nozzles pointing aft for conventional flight. | FULL AFT (0°) | |
| 04 | Battery Switch | ON | |
| 05 | External Power | CONNECT (if available) | |
| 06 | Generator | ON | |
| 07 | Fuel Shutoff | ON |
PHS 2 — Engine Start7 steps
| 01 | H2O Mode Switch | OFF | |
| 02 | Engine Start ButtonNOTE: Pegasus engine starts — monitor JPT. | PRESS | |
| 03 | JPT (Jet Pipe Temp)WARNING: JPT must not exceed 675°C during start. Abort if exceeded. | MONITOR | |
| 04 | RPM | MONITOR — Rising | |
| 05 | ThrottleCAUTION: Advance to IDLE only after RPM indication. | IDLE (when RPM >15%) | |
| 06 | Engine Stabilize | CHECK — ~55% RPM at idle, JPT below 500°C | |
| 07 | External Power | DISCONNECT |
PHS 3 — Post-Start / Systems10 steps
| 01 | Generator | VERIFY ON | |
| 02 | Hydraulic Pressure | CHECK — Normal | |
| 03 | Flight ControlsNOTE: Nozzles at 0° for control check. | CYCLE — Stick and rudder | |
| 04 | Reaction Control SystemNOTE: RCS provides control authority in hover/VSTOL. | CHECK — Verify puffers | |
| 05 | Nozzle LeverCAUTION: Verify nozzles move smoothly through full range. | CYCLE — Check nozzle rotation | |
| 06 | Flaps | CHECK — Cycle and return | |
| 07 | Speed Brake | CHECK — Extend and retract | |
| 08 | Trim | SET — Takeoff | |
| 09 | NWS | ON | |
| 10 | Anti-Skid | ON |
PHS 4 — INS / Avionics14 steps
| 01 | INS KnobNOTE: Full alignment ~8 minutes. Carrier align available. | GND ALIGN | |
| 02 | INS Status | MONITOR — Wait for NAV ready | |
| 03 | INS Knob | NAV (when aligned) | |
| 04 | HUD | ON — Brightness as required | |
| 05 | MPCD / MFD | ON | |
| 06 | ODU (Option Display Unit) | CHECK | |
| 07 | Radar (APG-65)NOTE: Allow warm-up time. | STBY | |
| 08 | RWR (ALR-67) | ON | |
| 09 | CMDS (ALE-39) | ON — Set program | |
| 10 | IFF / Transponder | SET | |
| 11 | Radios (UHF / VHF) | SET frequencies | |
| 12 | TACAN | SET channel | |
| 13 | Altimeter | SET — Field elevation | |
| 14 | DMT (Dual Mode Tracker) | ON (if targeting pod equipped) |
PHS 5 — Before Taxi8 steps
| 01 | Canopy | CLOSE & LOCK | |
| 02 | Ejection SeatWARNING: Verify canopy locked. | ARM | |
| 03 | VSTOL Master ModeNOTE: Select STO or VSTOL mode as required. | SET (for vertical/short takeoff) | |
| 04 | FlapsNOTE: Set for short takeoff — STOL flap setting. | STO position | |
| 05 | Trim | SET — 0° rudder, 0° aileron, 4° nose down | |
| 06 | Taxi Light | ON | |
| 07 | Anti-Collision Light | ON | |
| 08 | Parking Brake | RELEASE |
PHS 6 — Taxi5 steps
| 01 | NWS | CHECK responsive | |
| 02 | Taxi Speed | SAFE — max 10 kts | |
| 03 | Nozzle Lever | CHECK — Full aft (0°) | |
| 04 | Instruments | CHECK during taxi | |
| 05 | Brakes | CHECK |
PHS 7 — Before Takeoff (STO)7 steps
| 01 | Nozzle AngleNOTE: STO nozzle setting for rolling takeoff. | SET — ~50° (short takeoff) | |
| 02 | Water InjectionNOTE: H2O provides additional thrust for takeoff. | SET — TO mode (if required) | |
| 03 | Flaps | STO | |
| 04 | Trim | VERIFY — 4° nose down stabilator | |
| 05 | Fuel Quantity | CHECK — Adequate | |
| 06 | Master Arm | SAFE | |
| 07 | Strobe Lights | ON |
PHS 8 — Takeoff (Short Takeoff)10 steps
| 01 | Lineup on Runway | CENTERLINE | |
| 02 | Brakes | HOLD | |
| 03 | ThrottleNOTE: Nozzles at ~50° provide both lift and thrust. | FULL POWER | |
| 04 | Brakes | RELEASE | |
| 05 | At 80–100 kts | ROTATE — Slight aft stick | |
| 06 | Positive Climb | CONFIRMED | |
| 07 | Landing Gear | UP | |
| 08 | Nozzle LeverCAUTION: Transition smoothly — do not slam nozzles aft. | SLOWLY rotate AFT (0°) | |
| 09 | Flaps | RETRACT (above 180 kts) | |
| 10 | Water Injection | OFF |
PHS 9 — After Takeoff / Climb6 steps
| 01 | Landing Gear | CONFIRM UP | |
| 02 | Nozzles | CONFIRM 0° (full aft) | |
| 03 | Airspeed | ACCELERATE to 300 kts | |
| 04 | Altimeter | CHECK | |
| 05 | Taxi / Landing Lights | OFF | |
| 06 | Climb Altitude | AS ASSIGNED |
PHS 10 — Cruise / Transit7 steps
| 01 | Altitude | AT assigned level | |
| 02 | AirspeedNOTE: Max speed ~575 kts. Cruise ~400 kts. | AS REQUIRED | |
| 03 | Autopilot | ENGAGE (if desired) | |
| 04 | Fuel StateNOTE: Harrier has limited range — watch fuel closely. | MONITOR | |
| 05 | Navigation | CHECK waypoints | |
| 06 | Radar | AS REQUIRED | |
| 07 | RWR / CMDS | MONITOR |
PHS 11 — Descent / Approach9 steps
| 01 | ATIS / Weather | OBTAINED | |
| 02 | Altimeter | SET local QNH | |
| 03 | Airspeed | REDUCE below 300 kts | |
| 04 | Landing Mode | SELECT — VSTOL or conventional | |
| 05 | Nozzle LeverNOTE: Slowly rotate nozzles forward for deceleration. | SET for approach (if VSTOL) | |
| 06 | Landing Gear | DOWN (below 210 kts) | |
| 07 | Flaps | DOWN | |
| 08 | Landing Light | ON | |
| 09 | Master Arm | SAFE |
PHS 12 — Landing (Conventional)5 steps
| 01 | Approach SpeedNOTE: Conventional approach speed. | ~130 kts | |
| 02 | Throttle | IDLE at touchdown | |
| 03 | Nosewheel | LOWER gently | |
| 04 | Braking | APPLY | |
| 05 | NWS | ENGAGE |
PHS 13 — Landing (Vertical)8 steps
| 01 | Nozzle LeverNOTE: Decelerate to hover. | ~80° (braking stop) | |
| 02 | Airspeed | REDUCE to hover — below 40 kts | |
| 03 | Nozzle LeverNOTE: Nozzles straight down for hover. | 90° (full down — hover) | |
| 04 | Throttle | MANAGE — Control descent rate | |
| 05 | RCSCAUTION: Avoid rapid or large control inputs in hover. | ACTIVE — Puffers control attitude | |
| 06 | Descent | SLOW — 2–3 ft/sec max | |
| 07 | Touchdown | GEAR on deck — Level attitude | |
| 08 | Throttle | IDLE after stable on deck |
PHS 14 — After Landing5 steps
| 01 | Nozzle Lever | FULL AFT (0°) | |
| 02 | Flaps | RETRACT | |
| 03 | Radar | STBY | |
| 04 | Transponder | STBY | |
| 05 | Landing Light | OFF |
PHS 15 — Shutdown15 steps
| 01 | Parking Brake | SET | |
| 02 | Radar | OFF | |
| 03 | RWR | OFF | |
| 04 | CMDS | OFF | |
| 05 | Radios | OFF | |
| 06 | TACAN | OFF | |
| 07 | IFF | OFF | |
| 08 | Ejection SeatWARNING: Safe seat before ground crew approach. | SAFE | |
| 09 | Throttle | OFF | |
| 10 | Fuel Shutoff | OFF | |
| 11 | Generator | OFF | |
| 12 | HUD / Displays | OFF | |
| 13 | All Lights | OFF | |
| 14 | Battery | OFF | |
| 15 | Canopy | OPEN |