Memory Items Flashcards

1
Q

GLIDESLOPE INTERCEPT FROM ABOVE

A

Ensure LOC capture within 1/2 Scale prior to descent below cleared or FAF altitude.

APP ………. Arm
Landing Configuration ………. Establish

MCP Altitude ………. Set 1,000’ AAL
MCP V/S ………. 1000-1500 fpm

IF GS not captured, or approach not stabilised by 1000’ AAL:
- Initiate Go-Around

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2
Q

ENGINE FAILURE DRIFTDOWN

A

Autothrottle (if engaged) ………. Disengage
Thrust Lever (operating engine) ………. Set CON Thrust
MCP Altitude ………. Set MAX EO ALT
MCP Speed ………. Set EO Target Speed

At EO Target Speed:
LVL CHG ………. Engage
HDG (if required) ………. Turn

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3
Q

REACTIVE WINDSHEAR WARNING (AUTOMATIC)

A

“WINDSHEAR, WINDSHEAR, WINDSHEAR”

“WINDSHEAR, TOGA”

TO/GA ………. Push
Verify GA Thrust
Verify TOGA mode annunciation

Speedbrakes ………. Retract
Monitor system performance

DO NOT change Flap or Gear Configuration until out of windshear.

Maintain wings level to maximize climb gradient, unless a turn is required for obstacle clearance.

Monitor vertical speed and altitude.

Do not attempt to regain lost airspeed until out of windshear.

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4
Q

REACTIVE WINDSHEAR WARNING (MANUAL)

A

“WINDSHEAR, WINDSHEAR, WINDSHEAR”

“WINDSHEAR, TOGA”

Autopilot ………. Disengage
TO/GA ………. Push
Max Thrust ………. Aggressively Apply
Autothrottle ………. Disengage

Roll Wings Level and Rotate to initial pitch 15°.

Speedbrakes ………. Retract
Follow Flight Director TO/GA guidance

DO NOT change Flap or Gear Configuration until out of windshear.

Maintain wings level to maximize climb gradient, unless a turn is required for obstacle clearance.

Monitor vertical speed and altitude.

Do not attempt to regain lost airspeed until out of windshear.

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5
Q

PREDICTIVE WINDSHEAR AHEAD (APPROACH)

A

“GO AROUND, WINDSHEAR AHEAD”

Windshear Escape Maneuver or normal Go-Around.

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6
Q

PREDICTIVE WINDSHEAR WARNING (TAKEOFF)

A

“WINDSHEAR AHEAD, WINDSHEAR AHEAD”

Before V1 ………. Reject Takeoff
After V1 ………. Windshear Escape Maneuver

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7
Q

PREDICTIVE WINDSHEAR CAUTION

A

“MONITOR RADAR DISPLAY”

Maneuver as needed to avoid windshear

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8
Q

TCAS RA, for climb in landing config

A

Autopilot ………. Disengage
Autothrottle ………. Disengage

Advance thrust levers forward to ensure max thrust is attained and call for Flaps 15°.

Smoothly adjust pitch and thrust to satisfy the RA command.

Follow planned lateral flight path unless visual contact with traffic which requires other action.

Positive Rate ………. Gear Up

Attempt to establish visual contact.

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9
Q

TCAS RA

A

Autopilot ………. Disengage
Autothrottle ………. Disengage

Smoothly adjust pitch and thrust to satisfy the RA command.

Follow planned lateral flight path unless visual contact with traffic which requires other action.

Attempt to establish visual contact.

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10
Q

TCAS TA

A

“I HAVE CONTROL, ALL LIGHTS ON”

Look for traffic using the navigation display aa a guide.

If traffic is sighted, maneuver if needed.

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11
Q

GPWS WARNING

A

“PULL UP, FULL THRUST”

Autopilot ………. Disengage
Autothrottle ………. Disengage
Maximum Thrust ………. Aggressively Apply
Roll Wings Level & Rotate initial pitch 20°.

Speedbrakes ………. Retract

If terrain remains a threat, continue rotation up to the pitch limit indicator or stick shaker or initial buffet.

Do not change gear or flap configuration until clear of terrain

Clear of Terrain ………. Recover

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12
Q

GPWS CAUTION

A

Correct Flight Path,
Airplane Configuration,
or Airspeed

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13
Q

REJECTED TAKEOFF

A

Thrust Levers ……….. Close
Autothrottle ………. Disengage

Maximum Braking ………. Verify RTO autobrake or apply Manual brake
Speedbrake Lever ………. Raise
Reverse Thrust ………. Maximum as needed

Continue max braking until certain A/C can stop.

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14
Q

APPROACH TO STALL or STALL RECOVERY

A

Control Column ………. Hold Firmly
Autopilot (if engaged) ……….. Disengage
Autothrottle (if engaged) ……….. Disengage

Smoothly apply nose down elevator to reduce AOA until buffet or stick shaker stops.
Nose down trim may be needed.

Roll in the shortest direction to wings level if needed

Thrust Lever ………. Advance as needed
Speedbrakes ………. Retract

Do not change gear or flap configurationn, except during liftoff, if flaps are up, call for Flaps 1.

Required flight path ………. Recover

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15
Q

RUNAWAY STABILISER

A

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 Stabiliser Trim ………. Reduce control colum forces

IF Runaway Stops after the autopilot is disengaged:
- DO NOT re-engage autopilot or autothrottle.

IF runaway continues after autopilot disengaged:
- STAB TRIM Cutout Switches (both) ………. CUTOUT

IF runaway continues:
- Stabiliser Trim Wheel ………. Grasp and hold

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16
Q

LOST OF THRUST ON BOTH ENGINES

A

ENGINE START Switches (both) ………. FLT
Engine Start Levers (both) ………. CUTOFF

When EGT decreases:
Engine Start Levers (both) ………. IDLE detent

IF EGT reaches Redline or no increase in EGT within 30 seconds:
- Engine Start Levers (affected engine) ….. “Confirm” ….. CUTOFF, then IDLE detent

IF EGT reaches Redline or no increase in EGT within 30 seconds:
- Repeat as necessary.

17
Q

ENGINE OVERHEAT

A

Autothrottle (if engaged) ………. Disengage
Thrust Lever (affected engine) …… “Confirm” ….. Close

IF the ENG OVERHEAT light stays illuminated:
- Go to the ENGINE FIRE or SEV DAMAGE or SEPARATION checklist

18
Q

ENGINE LIMIT or SURGE or STALL

A

Autothrottle (if engaged) ………. Disengage

Thrust Lever (affected engine) ………. Retard until Engine Indications stay within limits or Thrust Lever is closed.

19
Q

ENGINE FIRE or SEV DAMAGE or SEPARATION

A

Autothrottle (if engaged) ………. Disengage
Thrust Lever (affected engine) ….. “Confirm” ….. Close
Engine Start Lever (affected engine) ….. “Confirm” ….. CUTOFF
Engine Fire Switch (affected engine) ….. “Confirm” ….. Pull
(To manually unlock, press override and pull.)

IF the Engine Fire Switch or ENG OVERHEAT light is illuminated:
- Engine Fire Switch (affected engine) ………. Rotate and hold for 1 sec

20
Q

CONFIGURATION WARNING

A

Assure correct AC takeoff or landing configuration.

21
Q

EMERGENCY DESCENT

A

Announce Emergency Descent.
PF advise cabin crew on PA.
PM advise ATC and obtain local QNH.

Passenger Signs ON.

Without delay, descend to lowest safe altitude or 10,000’.

ENGINE START Switches (both) ………. CONT
Thrust Levers (both) ………. minimum or as needed for AI
Speedbrake ………. FLIGHT DETENT

IF structural integrity is in doubt, limit speed, otherwise:
- Set target speed Mmo/Vmo.

22
Q

APU FIRE

A

APU Fire Switch ….. “Confirm” ….. Pull, Rotate & hold 1 sec

APU Switch ………. OFF

23
Q

ABORTED ENGINE START

A

Engine Start Lever (affected engine) ………. CUTOFF

24
Q

CABIN ALT WARNING OR RAPID DEPRESSURISATION

A

Don O2 masks & set 100%
Establish crew communications

Pressurisation Mode Selector ………. MAN
Outflow Valve ………. CLOSE until fully closed

IF cabin alt uncontrollable:
- PASS SIGNS ………. ON
- PASS OXYGEN ………. ON

Go to EMERGENCY DESCENT Checklist

25
**AIRSPEED UNRELIABLE**
Autopilot (if engaged) .......... Disengage Autothrottle (if engaged) .......... Disengage FD (both) .......... OFF Set GEAR UP Pitch & Thrust: IF FLAPS extended .......... 10 and 80% IF FLAPS UP .......... 4 and 75%