Memory Items Flashcards
Operating Pressure Altitude
Maximum
41,000 feet
Maximum Takeoff/Landing Tailwind Component
15 knots
Recommended Severe Turbulence Penetration Speed
Cruise: TURB N1 setting from cruise page
Climb and descent: 280 knots/.76 Mach
Takeoff Crosswind Component (knots)
Runway Condition Code: 6 (Dry)
34 Blended Winglet
33 Split Scimitar Winglet
Landing Crosswind Component (knots)
Runway Condition Code: 6 (Dry)
40 Blended Winglet
37 Split Scimitar Winglet
Takeoff Crosswind Component (knots)
Runway Condition Code: 5 (Wet, Damp, Frost, 1/8” or less Water, Slush, dry/wet snow)
25 Blended Winglet
25 Split Scimitar Winglet
Landing Crosswind Component (knots)
Runway Condition Code: 5 (Wet, Damp, Frost, 1/8” or less Water, Slush, dry/wet snow)
40 Blended Winglet
37 Split Scimitar Winglet
ICING CONDITIONS EXIST ON THE GROUND AND FOR TAKEOFF WHEN:
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.
ICING CONDITIONS EXIST IN FLIGHT WHEN:
Total air temperature: 10 degrees C or below
And
Visible moisture in any form is present
Engine ignition must be selected to ….. prior to and during engine anti-ice operation
CONT
AUTOPILOT MINIMUM ENGAGEMENT HEIGHT
on takeoff or missed approach, do not engage autopilot below:
400 feet AGL
Minimum altitude for use of Autopilot on Approach
ILS/GLS coupled approaches (no Autoland): 50 feet AGL
Non-Precision approaches: 50 feet below MDA/DA
Do not use LVL CHG on final approach below….
1000 feet AFE
APU FIRE
- APU fire switch… Confirm…Pull, rotate, & hold
Rotate to the stop and hold for 1 second. - APU switch……OFF
LOSS OF THRUST IN BOTH ENGINES
- ENGINE START switches (both)……FLT
- Engine start levers (both)……CUTOFF
- When EGT decreases: Engine start levers (both)…… IDLE detent
ENGINE FIRE OR ENGINE SEVERE DAMAGE OR SEPARATION
- Autothrottle (if engaged)……. Disengage
2. Thrust Lever (affected engine)…Confirm……Close
ENGINE OVERHEAT
- Autothrottle (if engaged)……. Disengage
2. Thrust Lever (affected engine)…Confirm……Close
ENGINE LIMIT OR SURGE OR STALL
- Autothrottle (if engaged)……Disengage
- Thrust lever(affected engine)…..Confirm….Retard
Until engine indications stay within limits or the thrust lever is closed
ENGINE START-ABORTED START
- Engine start lever (affected engine) ….CUTOFF
AIRSPEED UNRELIABLE
- Autopilot (if engaged)……Disengage
- Autothrottle (if engaged) ……Disengage
- Flight Director switches (both)……OFF
- Set the following gear up pitch attitude and thrust:
Flaps extended……10degrees and 80%N1
Flaps up……4degreea and 75%N1
SMOKE, FIRE, OR, FUMES
- Oxygen masks and regulators……..On, 100%
2. Crew communications (as needed) ……Establish
CABIN ALTITUDE WARNING OR RAPID DEPRESSURIZATION/EMERGENCY DESCENT
- Oxygen masks and regulators ………On, 100%
- Crew communications……Establish
- Seatbelt sign…………………..On
FLIGHT DECK DOOR EMER ACTIVE LIGHT/AUTOMATIC UNLOCK
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
RUNAWAY STABILIZER
- Control Column……Hold firmly
- Autopilot (if engaged)……Disengage
- Autothrottle (if engaged)……Disengage
- Control column and thrust levers…..Control airplane pitch attitude and airspeed
- Main electric stabilizer trim….Reduce control column forces
- 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
Rejected T/O considerations in the HIGH Speed regime
Engine failure
Any Fire indication
Unsafe/unable to fly
PWS warning or caution
