Memory Items Flashcards
APU FIRE
- APU FIRE………………………………………………………………PUSH
After 5 seconds and APU fire warning persists: - APU Bottle………………………………………………….DISCHARGE
and hold until firex bottle light goes out
CABIN ALT
- Oxygen Masks……………………………………DON, SET 100%
- Crew Communications……………………..Establish
- Passenger Signs……………………………….ON
- Passenger Oxygen……………………………DEPLOY
- Descent………………………………………………INITIATE
to 10,000 feet or lowest safe altitude, whichever is higher - Thrust Levers………………………………………IDLE
- ATS DISC……………………………………………..DEPRESS
- FLIGHT SPOILER lever……………………….MAX
ENGINE OVERSPEED/OVERTEMPERATURE
N1, N2, or ITT readout indicates engine limits being exceeded
- ATS DISC……………………………………………………DEPRESS
Affected engine: - Thrust lever………………………..CONFIRM and RETARD
until engine responds and ITT is below limit range
ENGINE FIRE/SEVERE ENGINE DAMAGE (IN FLIGHT)
Affected engine:
1. ATS DISC………………………………………………….DEPRESS
2. Thrust Lever……………………………CONFIRM and IDLE
3. Thrust Lever…………………CONFIRM and SHUT OFF
4. ENG FIRE………………………………………………………PUSH
5. BOOST PUMP………………………………………………….OFF
If warning persists (after 10 seconds):
6. BOTTLE……………………………………………..DISCHARGE
push and hold until firex bottle light goes out
If warning persists (after additional 30 seconds):
7. Other BOTTLE…………………………………….DISCHARGE
push and hold until firex bottle light goes out
ENGINE FIRE/SEVERE DAMAGE (ON GROUND)
- Parking Brake…………………………………………………..SET
Affected engine: - Thrust Lever…………………………………………SHUT OFF
- ENG FIRE……………………………………………………..PUSH
- BOOST PUMPS…………………………………..BOTH OFF
If warning persists (after 10 seconds): - BOTTLE 1 and BOTTLE 2…………………DISCHARGE
push and hold until firex bottle light goes out.
EMER POWER ONLY
or AC ESS BUS and No Generator on-line
If ADG did not deploy:
1. ADG manual deploy handle………………………..PULL
and leave extended
2. AC ELECTRICAL PAGE…………………………….CHECK
ESS BUS is powered
When ADG power is established:
3. STAB TRIM, CH 2 switch……………………..PRESS IN
4. Engine Instruments………………………………….VERIFY
and check N1, N2, and ITT indications
L (R) JET PIPE OVHT
- ATS DISC……………………………………………..DEPRESS
Affected engine:
2. Thrust lever…………………..CONFIRM and RETARD
slowly until message goes out
MLG BAY OVHT
- Airspeed………………………………..197 KIAS maximum
- LDG GEAR lever……………………………………………..DN
L (R) REV UNLOCKED
- Thrust Lever…………………………CONFIRM and IDLE
- ATS DISC……………………………………………..DEPRESS
- THRUST REVERSER……………………….EMER STOW
L (R) REV UNLOCKED caution message will remain on: - Airspeed……………………………….200 KIAS maximum
Asymmetric Braking/Loss of Braking
If excessive asymmetry or loss of braking is observed:
- Wheel brakes…………………….RELEASE momentarily
- ANTI SKID………………………….OFF
- Wheel brakes…………………….RE-APPLY as required
Ditching or Forced Landing Imminent
- PACKs………………………………….OFF
2. EMER DEPRESS…………………ON prior to 200 feet AGL
Emergency Descent
- Oxygen Masks………………………….Don, SET 100%
- Crew Communication……………..Establish
- Passenger Signs……………………..ON
- Passenger Oxygen………………….DEPLOY
- Descent…………………………………….INITIATE
to 10,000 ft or lowest safe altitude, whichever is higher - Thrust Levers…………………………….IDLE
- ATS DISC……………………………………DEPRESS
- FLIGHT SPOILER Lever…………….MAX
Emergency Evacuation
PILOT
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
7. BATT MASTER…………………………….OFF
to prevent CVR erasure
Emergency Evacuation
CO-PILOT
Copilot on EVACUATION command
8. ATC……………………………………………..NOTIFY
of condition and intention to evacuate
9. PACK’s………………………………………….OFF
10. EMER DEPRESS…………………………ON
11. EMER LTS……………………………………ON
Double Engine Failure
Engine failure indicated by N1, N2, ITT and fuel flow indicators on EICAS
- CONT IGNITION…………………………..ON
2. Airspeed………………………………………240 KIAS minimum
