Penny Guide

Question 1

Ground evacuation

Answer 1

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

Question 2

Engine fire shutdown

Answer 2

Fire handle- pull
Agent - discharge, as required
Engine start switch - stop

Question 3

Hyds system press lo/loss/leak

Answer 3

Eng pump switches (affct system)-off
Suction boost pump (affct system)-off

Question 4

Windshear/GCAS/twas/pull up

Answer 4

Takeoff power-set
Aircraft attitude-wings level, nose up
Radar alt, airspeed, sink rate- call out

Question 5

Rapid decompression

Answer 5

Oxygen—normal, 100%, on

Question 6

Eng fail below refusal speed

Answer 6

Aborted takeoff procedure- perform

Question 7

Eng fail after refusal speed

Answer 7

Takeoff—continue
Directional control—maintain
Aircraft attitude—rotate to target pitch

Question 8

Fire/smoke/fumes

Answer 8

Crew/passengers-notify
Oxygen-emergency, 100%, on

Question 9

Aborted takeoff

Answer 9

Abort—announce
Power levers—Gnd idle
Brakes and nose wheel steering- as required

Question 10

Four engine flameout

Answer 10

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

Question 11

Apu fire

Answer 11

Apu fire handle—pull
Agent—discharge if required

Question 12

Hose rapid trail (110)

Answer 12

Rapid trail-announce

Question 13

Broken hose

Answer 13

Broken hose/breakaway—announce
Hydraulic pwr LSK-off
Master pwr LSK-off

Question 14

Wing fire

Answer 14

Cross feed switches (all)—CLSD
Transfer from switches (all) — off
ISO valve (affected wing) — CLOSE
Nac shutoff switches (affct wing)-Close

Question 15

Critical field length

Answer 15

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

Question 16

Critical engine failure speed

Answer 16

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.

Question 17

Critical engine failure speed is based on:

Answer 17

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

Question 18

Refusal speed

Answer 18

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.