Orals - EPC's Flashcards
Asymmetric braking/loss of braking on landing - MUST KNOW FOR ORALS
If excessive asymmetry or loss of braking is observed upon landing…
Wheel brakes - RELEASE MOMENTARILY
ANTI - SKID switch - OFF
Wheel brakes - REAPPLY AS REQUIRED
Refer to GEAR tab for expanded procedure
Engine OVERSPEED
MUST KNOW FOR ORALS
Affected thrust lever - CONFIRM & IDLE
Refer to ENG tab for expanded procedure
T/O Configuration Warning - MUST KNOW FOR ORALS
Takeoff - DISCONTINUE IMMEDIATELY
Refer to WARN tab for expanded procedure
UNCOMMANDED YAW MOTION - MUST KNOW FOR ORALS
Controls - ASSUME MANUAL CONTROL AND COUNTER AIRCRAFT MOTION USING HANDWHEEL INPUTS
Yaw Dampers - SELECT TO DISCONNECT BOTH YAW DAMPERS
CABIN ALTITUDE OR EMERGENCY DESCENTS - MUST KNOW FOR ORALS
Oxygen masks - DON & 100% Crew communications - ESTABLISH NO SMKG and SEAT BLTS sign switches - ON Descent - INITIATE TO 10,000 FEET OR LOWEST SAFE ALTITUDE Thrust levers - IDLE Flight spoilers - DEPLOY
Refer to AIR tab for expanded procedure
STALL RECOVERY - MUST KNOW FOR ORALS
Autopilot - DISENGAGE, IF REQUIRED
Pitch attitude - LOWER NOSE TO REDUCE AOA
Thrust levers - ADVANCE TO MAX POWER, LEVEL WINGS
FLIGHT SPOILER Lever - SELECT TO RETRACT
RAPID DECOMPRESSION - MUST KNOW FOR ORALS
Oxygen masks - DON AND 100%
Crew communications - ESTABLISH
REJECTED TAKEOFF BEFORE ACHIEVING V1 - MUST KNOW FOR ORALS
Simultaneously:
Thrust lever - IDLE
Wheel Brakes - MAXIMUM UNTIL A SAFE STOP
Thrust reverser(s) operating engine(s) - MAXIMUM, CONSISTENT WITH DIRECTIONAL CONTROL
Refer to MISC tab for expanded procedure
L/R Engine Start Abort - MUST KNOW FOR ORALS
Affected Thrust Lever - SHUT OFF
Dry Motor - UNTIL ITT IS REDUCED BELOW 120 degrees, OR START LIMIT WHICHEVER COMES FIRST
Affected engine, ENG STOP switch - STOP
Affected engine start - REPEAT
Engine Hot Start - MUST KNOW FOR ORALS
Affected Thrust Lever - SHUT OFF
Dry Motor - UNTIL ITT IS REDUCED BELOW 120, or STARTER LIMIT, WHICHEVER COMES FIRST
Affected engine, ENG STOP switch - STOP
Refer to ENG tab for expanded procedures
ENGINE FIRE OR SEVERE ENGINE DAMAGE (INFLIGHT)
At a safe altitude, affected engine:
Affected thrust lever………….CONFIRM & IDLE
Affected thrust lever……CONFIRM & SHUTOFF
Affected ENG FIRE PUSH Switch……..CONFIRM & SELECT
Affected FUEL BOOST PUMP Switch…..CONFIRM & OFF
After 10 seconds and fire warning persists:
Affected engine BOTTLE switch……SELECT TO DISCHARGE
After another 30 seconds and fire warning still persists:
Other engine BOTTLE switch……..SELECT TO DISCHARGE
ENGINE FIRE OR SEVERE ENGINE DAMAGE (ON GROUND)
NOTE: Attempt to face the airplane into the wind.
Parking brake………………………………………….ON
Affected thrust lever…………………………………SHUT OFF
Affected ENG FIRE PUSH Switch……………..SELECT
L and R FUEL BOOST PUMP Switches……..OFF
After 10 seconds and fire warning persists:
Both engine BOTTLE Switches………………….SELECT TO DISCHARGE
ENGINE FIRE OR SEVERE ENGINE DAMAGE (Inflight)
At a safe altitude, affected engine:
Affected thrust lever………………………….CONFIRM & IDLE
Affected thrust lever………………………….CONFIRM & SHUTOFF
Affected ENG FIRE PUSH switch……….CONFIRM & SELECT
Affected FUEL BOOST PUMP switch…CONFIRM & OFF
After 10 seconds and fire warning persists:
Affected engine BOTTLE switch………..SELECT TO DISCHARGE
After another 30 seconds and fire warning still persists:
Other engine BOTTLE switch…………….SELECT TO DISCHARGE
Refer to ENG or FIRE tab for expanded procedure
L (R) REVERSER DEPLOYED
Affected thrust lever……………..CONFIRM & IDLE
————- Refer to ENG tab for expanded procedure —————
HYD 1 HI TEMP
L HYD SOV switch……………….CLOSED
HYDRAULIC page………………..CONFIRM L HYD SOV CLOSED
System 1 temperature…………..MONITOR
—————— Refer to HYD tab for expanded procedure ————-