Memory Items Flashcards
T/A
3
1) Disengage A/P Disconnect A/T If Req’d
2) Smoothly adjust pitch to satisfy TA
3) Fly planned lateral path
T/A - Climb in Landing Config
6
1) Disengage the A/P and disconnect A/T
2) Maximum thrust
3) FLAPS 20
4) Smoothly adjust pitch to satisfy RA
5) Follow planned lateral path
6) Positive rate – call GEAR UP
Upset -Nose High
6
1) Disengage A/P and disconnect A/T
2) Apply as much as full nose down elevator.
3) Apply appropriate nose down stabilizer trim.
4) Reduce thrust.
5) Roll (adjust bank angle) to obtain a nose down pitch rate.
6) Complete the recovery:
- when approaching the horizon, roll to wings level
- check airspeed and adjust thrust
- establish pitch attitude.
Upset - Nose Low
4
1) Disengage autopilot and disconnect autothrottle.
2) Recover from stall, if required.
3) Roll in the shortest direction to wings level (unload and roll if bank angle is more than 90 degrees).
4) Recover to level flight:
- apply nose up elevator
- apply nose up trim, if required
- adjust thrust and drag as required.
GPWS
7
1) Call “FIREWALL”.
2) Disengage autopilot & autothrottle
3) Aggressively apply maximum* thrust.
4) Simultaneously roll wings level and rotate to an initial pitch attitude of 20°.
5) Retract speedbrakes.
6) If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet.
7) Do not change gear or flap configuration until terrain separation is assured.
Stall
7
1) Simultaneously call “STALL” and :
2) SMOOTHLY APPLY NOSE DOWN ELEVATOR to reduce the angle of attack until buffet or stick shaker stops.
3) For high thrust settings, it may be necessary to reduce thrust.
4) When out of stall (stall indications have stopped): ROLL WINGS LEVEL*.
5) INCREASE THRUST SMOOTHLY AS REQUIRED.
In case of one engine inoperative, progressively compensate the thrust asymmetry with rudder.
6) CHECK SPEEDBRAKES RETRACTED.
7) MAINTAIN EXISTING GEAR AND FLAP CONFIGURATION.
Windshear - Manual Flight
7
1) Call “WINDSHEAR TOGA” and disconnect autopilot.
2) Push either TO/GA switch.
3) Aggressively apply maximum* thrust.
4) Disconnect autothrottle(s).
5) Simultaneously roll wings level and rotate toward an initial pitch attitude of 15°.
6) Retract speedbrakes.
7) Follow flight director TO/GA guidance (if available).
Windshear - Autopilot On
5
1) Call “WINDSHEAR TOGA”
2) Push either TO/GA switch.**
3) Verify TO/GA mode annunciation.
4) Verify thrust advances to GA power.
5) Retract speedbrakes.
Engine Fail in Cruise
6
1) Request ENG OUT to be selected on the FMC ACT CRZ page.
2) Ensure VNAV engaged
3) Set the EO cruise altitude in the MCP altitude window and call “EXECUTE”
4) Confirm that the thrust reference changes to CON and the autothrottle maintains MCT.
5) Initiate turn with HDG/TRK SEL (if required).
6) Call “CHECKLIST ENGINE FAILURE”
ABORTED ENGINE START / ENGINE AUTOSTART
1
FUEL CONTROL switch - CUTOFF
DUAL ENG FAIL/STALL
2
1) FUEL CONTROL switched (both) - CUTOFF, then RUN
2) RAM AIR TURBINE switch - Push and hold for 1 second
ENGINE LIMIT EXCEED / ENGINE SURGE
2
1) A/T ARM switch - OFF
2) Thrust Lever - Retard until message blanks or idle
VOLCANIC ASH
5
1) TURN - Consider 180˚turn, descending
2) Autothrottle disconnect switch - PUSH
3) Thrust levers (both) - IDLE (If conditions allow)
4) OXYGEN MASKS - ON (If required)
5) CREW COMMUNICATIONS - ESTABLISH
SMOKE OR FIRE FROM LITHIUM BATTERY
2
1) If necessary transfer control to the flight crew member seated on the opposite side of the fire.
2) PA “BACKUP TO THE FLIGHT DECK” x 2
SMOKE, FIRE or FUMES
2
1) OXYGEN MASKS - ON, 100%
2) CREW COMMUNICATIONS - ESTABLISH
STABILIZER
2
1) STAB cutout switches (both) - CUTOUT
2) Do not exceed current airspeed
AIRSPEED UNRELIABLE
3
1) Disconnect Autopilot and Autothrottle
2) F/D switches (both) - OFF
3) Set the following:
Flaps extended
10˚ and 85% N1
Flaps retracted
4˚ and 70% N1
Turbulence
2
1) Seatbelts ON
2) Speed
FL250 and above M84/310 kts
Below FL250 290 kts
-40→+3ºC visible moisture during TAXI:
RUNUP 40%N1 for 5secs./60min (50% w/vibes)
> 25%=Contam NO T/O if:
> 4” LT DRY SNOW
> 2” PKD DRY SNOW
> ½” WET SNOW, SLUSH or ST. WATER
LANDING DISTANCE CALC.
8
1) Over Max Landing Weight
2) Tail wind
3) Shorter than 9300 ft.
4) Less than autobrake 2
5) Airport elevation > 2000 ft.
6) Temperature > 30 C
7) Runway is contaminated
8) Abnormality affecting landing
After Landing
12
- Strobe and landing lights
- Chrono - Start timing
- Engine ANTI-ICE - AUTO or ON
- WXR Radar - OFF
- F/D switches OFF
- ISFD - Reset
- Autobrakes selector OFF
- Speedbrake Lever - DOWN
- Flaps Up
- Stab Trim – 5.0
- TCAS – XPDR or STBY
- APU – START
Shutdown Scan (6)
1) Transponder STBY / 1000
2) Hydraulics - OFF
3) Fuel Pumps - OFF
4) Packs - OFF
5) Lower Resirc Fan - OFF
6) Status - Check
Before T/O Checklist “TAKE OFF DATA”
“V1\_\_\_,V2\_\_\_” “LNAV ARMED, VNAV ARMED” “\_\_\_FEET” (Cleared or SID ALT) “\_\_\_DEGREES” (Runway or SID HDG) “RUNWAY \_\_\_”
Hold Speed North America At/Below 6000’
200 kts
Hold Speed North America Above 6000’ to 14000’
230
Hold Speed above 14000
265
Mod to Sev Icing Engines below 70% N1
Idle then 70% one at a time every 15 mins
Cat II RVR
A:1200
B:600
CAT III Fail Passive (LAND 2)
RVR 600 (175m)
RA 50ft
CAT III Fail Operational (LAND 3)
RVR 150 or 50m
RA 0 AH 100
Localizer Available when:
18 nm
120 degrees
Pointers proper position
If conducting an automatic landing (ILS only), at 1500 FT RA:
Confirm autoland status and verify the FLARE and ROLLOUT modes are armed.
