Memory Items

Question 1

Operating Pressure Altitude

Maximum

Answer 1

41,000 feet

Question 2

Maximum Takeoff/Landing Tailwind Component

Answer 2

15 knots

Question 3

Recommended Severe Turbulence Penetration Speed

Answer 3

Cruise: TURB N1 setting from cruise page

Climb and descent: 280 knots/.76 Mach

Question 4

Takeoff Crosswind Component (knots)

Runway Condition Code: 6 (Dry)

Answer 4

34 Blended Winglet

33 Split Scimitar Winglet

Question 5

Landing Crosswind Component (knots)

Runway Condition Code: 6 (Dry)

Answer 5

40 Blended Winglet

37 Split Scimitar Winglet

Question 6

Takeoff Crosswind Component (knots)

Runway Condition Code: 5 (Wet, Damp, Frost, 1/8” or less Water, Slush, dry/wet snow)

Answer 6

25 Blended Winglet

25 Split Scimitar Winglet

Question 7

Landing Crosswind Component (knots)

Runway Condition Code: 5 (Wet, Damp, Frost, 1/8” or less Water, Slush, dry/wet snow)

Answer 7

40 Blended Winglet

37 Split Scimitar Winglet

Question 8

ICING CONDITIONS EXIST ON THE GROUND AND FOR TAKEOFF WHEN:

Answer 8

Outside air temperature: 10 degrees C or below
And
Visible moisture in any form is present
or
While operating on ramps, taxiways, or runways where snow, standing water, or slush may be ingested by the engines or freeze on the engines, nacelles, or engine sensor probes.

Question 9

ICING CONDITIONS EXIST IN FLIGHT WHEN:

Answer 9

Total air temperature: 10 degrees C or below
And
Visible moisture in any form is present

Question 10

Engine ignition must be selected to ….. prior to and during engine anti-ice operation

Answer 10

CONT

Question 11

AUTOPILOT MINIMUM ENGAGEMENT HEIGHT

on takeoff or missed approach, do not engage autopilot below:

Answer 11

400 feet AGL

Question 12

Minimum altitude for use of Autopilot on Approach

Answer 12

ILS/GLS coupled approaches (no Autoland): 50 feet AGL

Non-Precision approaches: 50 feet below MDA/DA

Question 13

Do not use LVL CHG on final approach below….

Answer 13

1000 feet AFE

Question 14

APU FIRE

Answer 14

1. APU fire switch… Confirm…Pull, rotate, & hold
   Rotate to the stop and hold for 1 second.
2. APU switch……OFF

Question 15

LOSS OF THRUST IN BOTH ENGINES

Answer 15

1. ENGINE START switches (both)……FLT
2. Engine start levers (both)……CUTOFF
3. When EGT decreases: Engine start levers (both)…… IDLE detent

Question 16

ENGINE FIRE OR ENGINE SEVERE DAMAGE OR SEPARATION

Answer 16

1. Autothrottle (if engaged)……. Disengage

2. Thrust Lever (affected engine)…Confirm……Close

Question 17

ENGINE OVERHEAT

Answer 17

1. Autothrottle (if engaged)……. Disengage

2. Thrust Lever (affected engine)…Confirm……Close

Question 18

ENGINE LIMIT OR SURGE OR STALL

Answer 18

1. Autothrottle (if engaged)……Disengage
2. Thrust lever(affected engine)…..Confirm….Retard
   Until engine indications stay within limits or the thrust lever is closed

Question 19

ENGINE START-ABORTED START

Answer 19

1. Engine start lever (affected engine) ….CUTOFF

Question 20

AIRSPEED UNRELIABLE

Answer 20

1. Autopilot (if engaged)……Disengage
2. Autothrottle (if engaged) ……Disengage
3. Flight Director switches (both)……OFF
4. Set the following gear up pitch attitude and thrust:
   Flaps extended……10degrees and 80%N1
   Flaps up……4degreea and 75%N1

Question 21

SMOKE, FIRE, OR, FUMES

Answer 21

1. Oxygen masks and regulators……..On, 100%

2. Crew communications (as needed) ……Establish

Question 22

CABIN ALTITUDE WARNING OR RAPID DEPRESSURIZATION/EMERGENCY DESCENT

Answer 22

1. Oxygen masks and regulators ………On, 100%
2. Crew communications……Establish
3. Seatbelt sign…………………..On

Question 23

FLIGHT DECK DOOR EMER ACTIVE LIGHT/AUTOMATIC UNLOCK

Answer 23

JAMCO Flight Deck Door
1. Flight deck door HARD LOCK switch……Push

BOEING Flight Deck Door
1. FLT DK DOOR lock selector ……Rotate to DENY and hold for 1 second

Question 24

RUNAWAY STABILIZER

Answer 24

1. Control Column……Hold firmly
2. Autopilot (if engaged)……Disengage
3. Autothrottle (if engaged)……Disengage
4. Control column and thrust levers…..Control airplane pitch attitude and airspeed
5. Main electric stabilizer trim….Reduce control column forces
6. Choose one:
   * The runaway stops after the autopilot is disengaged: Do not re-engage the autopilot or autothrottle

• The runaway continues after the autopilot is disengaged:
  STAB TRIM CUTOUT
  switches (both)…….CUTOUT

If the runaway continues:
Stabilizer trim wheel …..Grasp and hold

Question 25

Rejected T/O considerations in the HIGH Speed regime

Answer 25

Engine failure
Any Fire indication
Unsafe/unable to fly
PWS warning or caution