IAC Flashcards
L(R) ENG FIRE Msg or Severe Engine Damage , in Flight
At a safe altitude, affected engine:
1) Thurst Lever - Confirm & Idle
2) Thrust Lever - Confirm & Shut Off
3) Engine Fire Push - Confirm & Select
4) Fuel Boost Pump - Confirm & Off
After 10s and fire warning persists:
5) Affected engine Bottle - Select to Discharge
After another 30s and fire warning still persists:
6) Other engine Bottle - Select to Discharge
Double Engine Failure
1) IGNITION CONT - ON*
2) Airspeed - 240 KIAS Minimum*
maintain airspeed until ready to restart engines.
L(R) REV UNLOCKED Msg
1) Affected thrust lever - Confirm & IDLE*
2) Affected THRUST REVERSER EMER STOW - Select*
UNCOMMANDED ACCELERATION/ENGINE OVERSPEED Msg, in flight
1) Affected thrust lever - Confirm & IdleCheck engine response
L(R) JETPIPE OVHT Msg
1) Thrust Lever - Confirm & Retard
slowly until warning message goes out
APU FIRE Msg (in flight)
1) APU FIRE PUSH - Select
after 5 s and fire warning persists:
2) APU BOTTLE - SELECT to discharge
SMOKE REMOVAL
1) O2 masks / smoke goggles - ON, 100%*
2) Crew and cabin communication - Establish*
CABIN ATL Msg or Emergency Descent Procedure
1) O2 masks - DON, set to 100%*
2) Crew Communications - Establish*
3) NO SMKG and SEAT BELTS signs - ON
4) Descent - INITIATE to 10,000ft or lowest safe altitude
5) Thrust Levers - IDLE
6) Flight Spoilers - DEPLOY
Aileron System Jammed
1) Autopilot - DISENGAGE*
2) Aileron Controls (both) - Release Pressure *
3) ROLL DISC - PULL & TURN to lock*
4) Airplane control - TRANSFER to pilot with operative aileron.
Elevator System Jammed
1) Autopilot - DISENGAGE*
2) Elevator Controls (both) - Release Differential Pressure *
3) PITCH DISC - PULL & TURN to lock*
4) Airplane control - TRANSFER to pilot with operative elevator.
Rudder System Jammed
1) YAW DAMPER DISC - SELECT
2) Rudder pedals - OVERPOWER
Stabilizer Trim Runaway
1) Control column - Assume manual control* and override runaway.
2) Both STAB TRIM DISC switches - PRESS, HOLD & RELEASE *
Uncommanded Yaw Motion
1) Controls - Assume manual control* and counter aircraft motion using control yoke inputs *
2) YAW DAMPER, DISC - SELECT* to disconnect both yaw dampers
Loss of All AC Power?
Extra credit: what happens electrically when this handle is pulled?
1) ADG manual deploy handle - PULL
The battery bus is directly tied into the DC ESS bus when WOW. This allows the ESS bus to remain powered when the ADG spools down on landing.
This allows the following to remain powered:
Thrust reversers (both) • Right oil pressure indicator • Fuel system control • Fuel gravity crossflow • Pressurization controllers (1 and 2) and control panel • 10TH stage isolation valve • Cargo bay air-conditioning shut-off valves • Pilot’s PFD, MFD, EFIS control • Avionic cooling controller (1) • AHRS FAN 1 • NAV 1, ADF 1, and ATC 1 • Radio tuning unit 1 • EFIS, dimming panel 1 • Bleed air leak test • Spoiler electronic control system 1 and 2 (PWR 3) • Stall protection, right channel • Horizontal Stabilizer Trim Control Unit (HSTCU) channel 2 • Left standby wing anti-icing • Left window heater controller • Left static and ADS controller heaters • Cockpit voice recorder • Instruments flood lights • Emergency lights
BRAKE OVHT Msg
1) Airspeed - NOT MORE THAN 250 KIAS
2) LDG GEAR lever - DN
MGL Bay OVHT Msg
1) Airspeed - NOT MORE THAN 250 KIAS
2) LDG GEAR Lever - DN
Ditching or Forced Landing Imminent
1) L and R Packs - Select both OFF
2) EMER DEPRESS - ON
Just before contact:
3) EMER DEPRESS - SELECT OFF
Engine Hot Start
1) Affected thrust lever - SHUT OFF*
2) IGNITION - OFF
3) Dry motor - ACCOMPLISH
until ITT is reduced below 120*C or starter limit, whichever comes first
N2 Stagnation
1) Affected thrust lever - SHUT OFF*
2) IGNITION - OFF
3) Dry motor until ITT is reduced below 120*C or starter limit, whichever comes first
No Lightoff
1) Affected thrust lever - SHUT OFF*
2) IGNITION - OFF
3) Dry motor until starter time limit.
Interrupted Start
1) Affected thrust lever - SHUT OFF*
2) IGNITION - OFF
3) Dry motor until ITT is reduced below 120*C or starter limit, whichever comes first
NO STRTR CUTOUT Msg -or-Engine Starter Fails to Cut Out
1) Affected ENG START - STOP* Starter fails to cut out - or- NO STARTER CUTOUT caution message persists: (YES) 2) Normal operations - CONTINUE (NO) 2) Affected engine - SHUTDOWN 3) Affected 10th STAGE BLEED - CLOSED 4) APU LCV - CLOSED, if applicable 5) External Air source - OFF, if applicable
Engine is still motoring: (YES) 6) Other Engine - SHUTDOWN (NO) 6) No further action Required.
L(R) ENG FIRE Msg or Severe Engine Damage, On Ground
Note: Attempt to face the airplane into the wind.
1) PARKING BRAKE - ON Affected Engine: 2) Thrust Lever - SHUT OFF 3) ENG FIRE PUSH - SELECT 4) L and R FUEL BOSST PUMPs - SELECT both OFF
After 10s and fire warning persists:
5) Both engine BOTTLEs - SELECT to discharge
After 30s and fire warning persists:
6) Passenger Evacuation procedure - AS REQUIRED
APU FIRE Msg, On Ground
1) APU FIRE PUSH - SELECT
After 5s and fire warning persists:
2) APU BOTTLE - SELECT, to discharge
After 30s and fire warning persists:
(YES)
3) Passenger Evacuation procedure - AS REQUIRED
