Penny Guide Flashcards
Ground evacuation
Parking brake-set
Tower-notify
Pressurization- EMER DEPRESS
Exits- open (as required)
Fire handles for all eng and APU-pull
Crew/passengers- notify to evacuate aircraft
Engine fire shutdown
Fire handle- pull
Agent - discharge, as required
Engine start switch - stop
Hyds system press lo/loss/leak
Eng pump switches (affct system)-off
Suction boost pump (affct system)-off
Windshear/GCAS/twas/pull up
Takeoff power-set
Aircraft attitude-wings level, nose up
Radar alt, airspeed, sink rate- call out
Rapid decompression
Oxygen—normal, 100%, on
Eng fail below refusal speed
Aborted takeoff procedure- perform
Eng fail after refusal speed
Takeoff—continue
Directional control—maintain
Aircraft attitude—rotate to target pitch
Fire/smoke/fumes
Crew/passengers-notify
Oxygen-emergency, 100%, on
Aborted takeoff
Abort—announce
Power levers—Gnd idle
Brakes and nose wheel steering- as required
Four engine flameout
Aircraft attitude- adjust to maintain 15-25%NG
Power levers-flt idle
Crossfeed switches-CLSD
No 2 & 3 eng start switches- stop start release
No 1 & 4 eng start switches- stop start release
Apu fire
Apu fire handle—pull
Agent—discharge if required
Hose rapid trail (110)
Rapid trail-announce
Broken hose
Broken hose/breakaway—announce
Hydraulic pwr LSK-off
Master pwr LSK-off
Wing fire
Cross feed switches (all)—CLSD
Transfer from switches (all) — off
ISO valve (affected wing) — CLOSE
Nac shutoff switches (affct wing)-Close
Critical field length
Total runway distance required to accelerate on all engines to critical engine failure speed,experience engine failure, then continue the takeoff or stop within the same distance.
Must be no greater than the length of runway available
Critical engine failure speed
Based on CFL, defined as the speed to which the aircraft can accelerate, lose an engine, and then either continue the takeoff w/ the remaining engines or stop in the same total runway distance.
Critical engine failure speed is based on:
Two engines (symmetrical power) in reverse, one engine in ground idle, one prop idle, one prop feathered, and max braking with anti skid operative or inoperative
Refusal speed
Based on runway available and is defined as the maximum speed to which the aircraft can accelerate with engines at takeoff then stop within the remainder of runway available with two engines in reverse, one engine in ground idle, one propeller feathered and max anti skid braking.
