APU FIRE
(Proceed to APU 01-1)
Uncommanded Yaw Motion
(Proceed to AVNC 02-18)
Unreliable Airspeed
If Climb or Go-Around is required:
4. Pitch/N1 ….. 15 DEGREES/TO FROM SL TO 15,000 FT 10 DEGREES/CLB ABOVE 15,000 FT
5. Airplane Configuration ….. FLAPS 20/GEAR UP FOR GO AROUND FLAPS 0/GEAR UP ONCE CLIMBING
CAUTION: Respect stall warning/stick shacker and stick pusher.
(Proceed to AVNC 02-20)
Rejected Takeoff
Simultaneously:
1. Takeoff …..DISCONTINUE immediately.
2. Thrust levers …… IDLE
3. Wheel brakes ….. APPLY MAX BRAKING until safe stop.
4. FLIGHT SPOILER ….. MAX
5. Operating thrust reverser(s) ….. APPLY MAX consistent with directional control.
(Proceed to OTHER 13-2)
L(R) ENGINE FIRE (In Flight)
OR
Severe Engine Damage (In Flight)
After takeoff and at a safe altitude:
Affected engine:
9. Thrust lever ….. CONFIRM and IDLE
10. Thrust lever ….. CONFIRM and SHUT OFF
11. ENG FIRE PUSH ….. PRESS IN
12. BOOST PUMP ….. PRESS OUT
L(R) ENGINE FIRE stays on (after 10 seconds):
13. BOTTLE ARMED ….. PRESS and hold to discharge.
L(R) ENGINE FIRE stays on (after additional 30 seconds):
14. Other BOTTLE ARMED ….. PRESS and hold to discharge.
(Proceed to ENG 05-1)
L(R) ENGINE FIRE (On Ground)
OR
Severe Engine Damage (On Ground)
(Proceed to ENG 05-3)
Double Engine Failure
(ENG 05-15)
L(R) JETPIPE OVHT
Affected engine:
1. Thrust lever ….. CONFIRM and RETARD slowly until message goes out.
(Proceed to ENG 05-7)
Post-Shutdown Engine Tail pipe Fire
Affected Engine:
1. Dry motor ….. ACCOMPLISH until ITT is reduced below 150°C or starter limit.
(Proceed to ENG 05-42)
L(R) REV UNLOCKED
In flight, on affected engine:
3. Thrust lever ….. CONFIRM and IDLE
4. THRUST REVERSER, EMER STOW ….. PRESS IN
“L(R) REV UNLOCKED” will stay on.
5. Airspeed ….. 200 KIAS maximum.
(Proceed to ENG 05-11)
ENGINE
Affected engine:
1. Thrust lever ….. CONFIRM and RETARD until engine responds and ITT is below limit range.
(Proceed to ENG 05-4)
Uncommanded Acceleration
On ground, affected engine:
1. Thrust lever ….. CONFIRM and IDLE then SHUT OFF.
In flight, affected engine:
2. Thrust lever ….. CONFIRM and IDLE Check engine response.
(Proceed to ENG 05-44)
CABIN ALT
(Proceed to ENVR 06-4)
Emergency Descent
(Proceed to ENVR 06-13)
Ditching or Forced Landing Imminent
(Proceed to F-LDG 08-2)
Emergency Evacuation
Pilot:
1. PARKING BRAKE ….. SET
2. Evacuation ….. COMMAND
3. GND SPOILERS ….. DISARM
4. FLIGHT SPOILER lever ….. RETRACT
5. Thrust levers ….. SHUTOFF
6. APU, LH and RH ENG FIRE PUSH ….. PRESS IN
7. BATT MASTER ….. OFF
to prevent CVR erasure.
Copilot: On EVACUATION command
8. ATC ….. NOTIFY on condition and intention to evacuate.
9. Both PACKs ….. PRESS OUT
10. EMER DEPRESS ….. PRESS IN
11. EMER LTS ….. ON
(Proceed to F-LDG 08-1)
EMER PWR ONLY
OR
Loss of All Normal Electrical Power
If ADG did not deploy:
1. ADG manual deploy handle ….. PULL
and leave extended.
On airplanes 5301 to 5407:
2. ADG manual deploy handle ….. PULL for at least 1 sec, the stow.)
When ADG power is established:
4. STAB TRIM, CH 2 ….. PRESS TO ENGAGE
5. Engine instruments ….. VERIFY N1, N2 & ITT.
(Proceed to ELEC 04-1)
Stabilizer Trim Runaway
(Proceed to FCTL 07-24)
Uncommanded Flap Extension
If above VFE
At a safe altitude
1. Autopilot ….. DISCONNECT
2. Thrust levers ….. IDLE
3. FLIGHT SPOILER lever ….. SELECT As required up to MAX.
4. Airspeed ….. REDUCE Until less than VFE.
(Proceed to FCTL 07-27)
Stall Recovery
MLG BAY OVHT
(Proceed to GEAR 08-2)
Asymmetric Braking / Loss of Braking
If loss of directional control or braking is observed:
1. Wheel brakes ….. RELEASE momentarily.
2. ANTI-SKID ….. OFF
3. Wheel brakes ….. RE-APPLY as required.
(Proceed to GEAR 10-12)
Smoke / Fire / Fumes
(Proceed to SMK 14-1)
Aileron / Elevator Jam