Engine Fire During Ground Operations.
(Indications: FIRE PUSH annunciator, audible warning, smoke, flames, engine instruments) F.E.V.E.R
- THROTTLES - CUTOFF (PF)
- Engine fire switch - Push (PF)
- Bottle armed switch - Push (PF)
- Accomplish Emergency Ground Egress
Tailpipe Fire on the Ground.
No indications. Motoring the engine will normally blow out excess fuel and prevent fire from spreading. If FIRE PUSH annunciator is illuminated accomplish Engine Fire During Ground Operation checklist
IF A TAILPIPE FIRE OCCURS, PERFORM THE FOLLOWING ACTIONS:
1. Throttles - Cuttle (P)
2. Engine start select switch - As required (P)
3. Engine start button - Push (P)
IF FIRE DOES NOT EXTINGUISH
4. Accomplish Emergency Ground Egress
Nose Gear Steering Failure
Accomplish steering with brake and throttle application. Most likely cause is torque link safety pin not being installed.
Emergency Ground Egress
- Crew and passengers - Advise (P)
- Throttles - CUTOFF (PF)
- Parking brake - As required (P) If hot brakes are suspect, do not set the parking brake.
- Oxygen system ready - Push (CP)
- Ground agency - Notified (PM)
- Batteries (2) - OFF (P/CP)
- Evacuate aircraft (ALL)
Abort
- Throttles - IDLE (PF)
- Wheel brakes - As required (PF)
- Speed brakes - EXT (PM)
Tire Failure During Takeoff
If a tire failure occurs prior to S1, the takeoff should be aborted.
If tire failure occurs after S1, do not retract the landing gear. Do not change flap position. Refer to Tire Failure under LANDING EMERGENCIES.
Engine Failure During Takeoff
Failure occurs at or above S1. Use 5 degrees of bank into the good engine. Use roll trim. Rotate to maintain Vco. Retract gear. Maintain Vco until reaching 400 ft AGL. Accelerate to Vco+10 upon reaching 400 AGL, retract the flaps. At Vco+15, set MCT power and continue climb to 2200 ft AGL or pattern altitude. Accomplish Engine Shutdown or Engine Failure During Flight checklist.
Engine Fire During Flight.
(Indications: ENG FIRE switchlight and aural fire warning
- THROTTLE - IDLE (PF,PM)
IF ENGINE FIRE SWITCHLIGHT REMAINS ILL., L OR R FIRE DET FAIL ILL., FIRE WARNING TEST FAILS, OR FIRE CONDITIONS PERSIST: - THROTTLE - CUTOFF (PF,PM) (OIL PRESS LO, FUEL PRESS LO, ENG EFC OFF AND GEN OFF annunciators will illuminate)
- ENGINE FIRE SWITCH - PUSH (PF/PM)
- BOTTLE ARMED SWITCH - PUSH (PF/PM)
- FIRE DET (affected engine) - TEST (if not previously accomplished) (PM)
- Remaining illuminated bottle armed switch - As required (PF/PM)
Engine Fire During Flight cont…
- Generator reset switch - OFF (PM)
- Ignition - OFF (PM)
- Jet Pump - OFF (PM)
- Boost pump - OFF (PM)
- Engine anti-ice - OFF (PM). Remain in on if in icing conditions
- Bleed air selector - Operating engine (CP)
- Engine sync - OFF (PM)
- ENG EFC switch - OFF (PM)
- Electrical load - Within limits (PM)
- N2 (engine with operating generator) - 58% (minimum) (PF)
- Fuel crossfeed - As required (PM) If fuel crossed is required, the boost pump must be turned on to ensure crossfeed capability
- Land as soon as possible
Engine Failure Autopilot Coupled
Maintain a final approach speed of Vapp+5 knots for autopilot coupled approach.
Rudder boost is provided by the rudder servo of the autopilot. The yaw damper is disabled when the rudder boost is activated.
Engine Shutdown During Flight.
(If the engine is being shutdown with no mechanical difficulty, stabilize ITT at IDLE thrust for 1 minute. If shutdown is caused by mechanical difficulty, no stabilization is required)
- Throttle - CUTOFF (PF,PM) (OIL PRESS LO, FUEL PRESS LO, ENG EFC OFF, and GEN OFF annunciators will illuminate)
- Generator reset switch - OFF (PM)
- Ignition - OFF (PM)
- Jet pump - OFF (PM)
- Boost pump - ON (PM) (The L/R FUEL PRESS LO annunciator will extinguish. Keep boost pump operating to ensure lubrication of the engine-driven high pressure pump)
Engine Shutdown During Flight cont….
- Engine anti-ice switch - OFF (PM) (Remain on if in icing conditions)
- Bleed air selector - Operating engine (CP)
- Engine sync - OFF (PM)
- Engine EFC - OFF (PM)
- Electrical load - Within limits (PM) (Less than 400 amps. 280 amps @ 32,500 ft)
- N2 (engine with operating generator) - 58% (minimum) (PF)
- Fuel crossfeed - As required (PM) If fuel crossed is required, the boost pump must be turned on to ensure crossfeed capability
- Land as soon as possible
Engine Restart. (Pre-Start Check)
(If engine fails to restart, accomplish the Engine Shutdown During Flight checklist. Do not restart an engine with know mechanical difficulties)
- Engine EFC switch - Cycle/ON (PM)
- Throttle - CUTOFF (PF,PM)
- Bleed air selector - Operating engine (CP)
- Boost pump - ON (PM)
- Jet pump - OFF (PM)
- Ignition - ON (PM) (The ignition operation light will not illuminate)
- Engine anti-ice switch - OFF (PM) (Remain ON, if in icing conditions)
- Airspeed and altitude - Within limits (PM)
Engine Restart (Starter Assisted Air Start) (The battery is used regardless of the position the generator reset switch for all inflight starter assisted air starts)
- Engine start selector - Inoperative engine (PM)
- Engine start button - Depress (PM)
- Throttle - IDLE (N2-8% or above) (PM) (The ignition operation light will illuminate)
- Engine instruments - Check (PM)
Engine Restart (Post Start Check)
- Throttle - As required (PF) (Consider limiting use to a minimum)
- Engine start selector - OFF (PM)
- Bleed air selector - NORM (CP)
- Engine anti-ice switch - As required (PM)
- Generator reset switch - RESET then NORM (PM) (L/R/ GEN annunciator will extinguish)
- Ignition - As required (PM) (Set STBY unless condition dictate otherwise)
- Jet pump - As required (PM) (Set to NORM unless conditions dictate otherwise)
- Boost pump - As required (PM) (Set to AUTO unless conditions dictate otherwise)
