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Command Prep > Memory Items > Flashcards

Memory Items Flashcards

1
Q

FMC FAIL?

A
  • If flying an approach that has an RNP alerting requirement:

Initiate a go-around unless a visual approach can be flown

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2
Q

UNABLE RNP?

A

on a procedure or airway that has an RNP alerting requirement:

select an alternate procedure or airway. During an approach, initiate a go- around unless a visual approach can be flown

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3
Q

ENGINE FIRE

or

Engine severe Damage or seperation

A
  • A/T ARM switch - OFF
  • Thrust Lever (affected side) - confirm - IDLE
  • FUEL CONTROL switch (afected side) - Confirm - CUTOFF
  • Engine Fire Switch (affected side) - Confirm - Pull
  • IF the engine fire warning light is illuminated:

Engine fire switch affected side - Rotate to the stop and hold for one second

IF after 30 seconds the engine fire warning light stays illuminated:

Engine fire switch (affected side) - Rotate to the other stop and hold for one

second

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4
Q

Engine Limit or Surge or Stall

A
  • A/T ARM switch - OFF
  • Thrust lever (affected side) - Confirm - Retard until engine indications

stay within limits or the thrust

is at idle

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5
Q

Dual Engine Failure

A
  • ENG START selectors (both) - FLT
  • Thrust levers (both) - Idle
  • FUEL CONTROL switches (both) - CUTOFF, then RUN
  • If engine appears stalled or EGT approaces the standby Engine Indicator placard limit:

FUEL CONTROL switch (affected side) - Confirm - CUTOFF then RUN

IF engine appears stalled again or EGT approaches the standby engine

indicator placard limit, repeat as needed.

—————————————————————————————————————————-NOTE:

  • start APU asap
  • ABV 30000’ maintain 240kts minimum
  • 30000’ and below use 220kt minimum
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6
Q

Aborted Engine Start

A
  • FUEL CONTROL switch (affected side) - CUTOFF
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7
Q

CABIN ALTITUDE

or

Rapid Depressurization

A
  • Oxygen Masks and regulators - ON, 100%
  • Establish crew communications
  • If ocupants in main cargo compartment:

MAIN CARGO ALERT switch - Push

  • Check the cabin altitude and rate
  • If the cabin is uncontrollable:

Without delay, descend to the lowest safe altitude of 10000’ which ever is

higher.

To descend:

  • Move the thrust levers to idle
  • Extend the speedbrakes
  • If structual integrity is in doubt, limit airspeed and avoid high maneuvering

loads.

  • Descend at VMO/MMO
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8
Q

Airspeed Unrelible

A
  • Autopilot disengage switch - Push
  • A/T ARM switch - OFF
  • F/D switches (both) - OFF
  • set the following gear up pitch attidude and thrust:
    • Flaps extended - 10º and 80% N1
    • Flaps up - 4 º and 75% N1

NOTE:

The following are reliable;

  • Attitude
  • N1
  • Ground speed
  • Radio altitude
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9
Q

Runway slope?

A

+/- 2%

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10
Q

Max operating altitude?

A

43100’

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11
Q

Max takeoff and landing altitude

A

8400’ pressure altitude

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12
Q

Max takeoff and landing tail wind component

A

15kts

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13
Q

Turbulent air penetration speed?

A

290kts/.78M

250kts below 10000’

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14
Q

RVSM altimeter cross check limitations

A
  • 200’ in flight
  • on the ground differences =
    • sea level = FO-CAPT = 40’ FO or CAPT and feild elevation = 75’
    • 5000’ = 45’ = 75’
    • 10000 = 50’ = 75’
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15
Q

Max Taxi weight?

Max Takeoff weight?

Max landing weight?

Max Zero fuel weight?

A
  • 187 333 Kg
  • 186 880 Kg
  • 147 871 Kg
  • 140 160 Kg
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16
Q

Crosswind limitaions?

Dry runway?

Wet?

Standing water/slush?

snow no melting?

Ice no melting?

Reported RVR 200m or less (wet or dry)?

Reported vis between 200m-350m (wet or dry)?

Autoland?

A

Dry = 35Kt/ 35kt

Wet = 25kt/25kt

standing water/ slush = 15kt takeoff / 12kt landing

snow not melting = 15kt takeoff / 30 kt landing

ice not melting = 15kt takeoff / 12kt landing

200m or less = 10kts/10kts

200m-350m = 15kt takeoff

< 550m = 15kt landing

autoland = 15kts

note:

  • inclusive of gusts
  • reduce by 5kts if assy on contaminated or wet runways
  • Take off and land on untreated now should only be attempted if no melting present.
  • use rolling takeoff procedure if x-winf is greater than 20kts
17
Q

what is the lowest height the autopilot can be engaged after takeoff?

A

200’

18
Q

wind limits for autolands?

A
  • 25kt head
  • 15kt tail
  • 15 kt x-wind
19
Q

Engine RPM limitations?

A
  • N1 = low pressure rotor = 117.5%
  • N2 high pressure rotor = 112.5%
20
Q

Engine EGT limitations?

A
  • Takeoff = 960º = 5 min
  • Max continuous = 925º = continuous
  • Starting = 870º = max transient for 40 sec

= 750º = unlimited

21
Q

Minimum inflight fuel tank temperature?

A
  • 3º above the freezing temperature of fuel
22
Q

Can you have center tank fuel without full main tanks?

A
  • Yes,
  • can contain upto 10000 kg of fuel without full main tanks provided the center tank fuel weight and the actual zero fule weight does not exceed the maximum zero fuel weight, and the center of gravity limits are observed.
23
Q

Max altitude with flaps extended?

A

20000’

24
Q

Approach to stall recovery?

A

INITIATE THE RECOVERY:

  • hold the controll column firmly
  • Discontect autopilot and autothrottle
  • smoothly apply nose down elevator to reduce the angle of attack until stick shaker stops. nose down elevator may be needed.

CONTINUE THE RECOVERY:

  • roll in the shortest direcction to wings level
  • advance thrust levers as needed
  • retract speedbrakes
  • do not change gear or flap configuration, except
    • during liftoff, iff flaps are UP call for flaps 1

COMPLETE THE RECOVERY:

  • Check airspeed and adjust thrust as needed
  • Establish pitch attitude
  • Return to desired flight path
  • re-engage the autopilot and autothrottle if desired
25
Q

GPWS response?

A

CAUTION = corect the flight path or the airplane configuration

WARNING =

Pilot Flying

  • disconnect the autopilot
  • disconnect the autothrottle
  • aggressivly appluy max thrust, simultaneously roll wings level and rotate to an initial pitch attitude of 20º
  • retract speedbrakes
  • 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 terrain speration is assured
  • monitor radio altimeter for sustained or increasing terrain seperation
  • when clear of terrain slowly decrease pitch attitude and accelerate
  • After the recovery manouver is complete, the aircrafts position together with the minimum safe altitude (MSA) or lowest safe altitude (LSALT)must be crossed checked

Pilot monitoring

  • Verify max thrust
  • Verify all required actions have been completed and call out any omissions
  • Monitor vertical speed and altitude (radio altitude for terrain seperation and barometric altitude for a minimum safe altitude)
  • call out any trend toward terrain contact.
  • After the recovery manouver is complete, the aircrafts position together with the minimum safe altitude (MSA) or lowest safe altitude (LSALT)must be crossed checked
26
Q

TCAS TA?

A
  • Look for any conflicting traffic using display as a guide. Call out any conflicting traffic.
  • If traffic is sighted, manouver if needed.

Note:

Manouvres based soley on a TA may result in reduced seperation and are not recomended.

27
Q

TCAS RA?

A
  • If manouvering is required. disengage the autopilot and autothrottle.
  • smoothly adjust pitch and thrust to satisfy the RA command.
  • follow the planned lateral flight path unless visual contact with the conflicting trafic requires other action
  • Attempt to establish visual contact. Call out any conflicting traffic

NOTE:

A DESCEND RA issued below 1000’ AGL should not be followed.

The pilot has 5 seconds to make the controlled .25g pitch change required

Following an increased strength or reversed corrective RA, the new target vertical speed must be attained within 2.5 seconds.

28
Q

Climb RA in landing configuration?

A

Pilot Flying

  • Disengage the autopilot and discontect the autothrottle.
  • Advance thrust levers full foward to ensure maximum thrust is attained, and
  • call for FLAPS 20
  • smoothly adjust pitch to satisfy RA command
  • follow the planned lateral flight path unless visual contact with the conflicting aircrtaft requires other action
  • Verify positive rate of climb and call GEAR IP
  • Attempt to establish visual contact. Call out any conflicting trafffic

Pilot monitoring

  • Verify maximum thrust is set.
  • position flap lever to 20 detent
  • verify a positive rate of climb on the altimeter and call “POSITIVE RATE”
  • Set landing gear lever to up
29
Q

Nose High Upset recovery?

A

Pilot Flying

  • Recognise and confirm the situation
  • apply as much as full nose down elevator
  • apply appropriate nose down stabiliser trim
  • Reduce thrust
  • Roll (adjust bank angle) to obtain a nose down pitch rate
  • complete the recovery:
    • when approaching the horizon, roll to wings level
    • check airspeed and adjust thrust
    • establish pitch attitude.

Pilot Monitoring

  • Call out attitude, airspeed and altitude throughout the recovery
  • Verify all required actions have been completed and call out any omissions
30
Q

Nose Low Upset Recovery?

A

Pilot Flying

  • Recognise and confirm the situation
  • Disconnect the autopilot and autothrottle
  • Roll in the shortest direction to wings level (unload and roll if bank angle is greater than 90 degrees)
  • REcover to level flight:
    • Apply nose up elevator
    • apply nose up trim, if required
    • adjust thrust and drag as required

Pilot moitoring

  • Call out attitude, airspeed and altitude throughout the recovery
  • Verify all required actions have been completed and call out any omissions
31
Q

Windshear Escape Manoeuvre?

A

Pilot Flying

​MANUAL FLIGHT

  • Disconect autopilot
  • push either go-around switch
  • Aggressively apply maximum thrust
  • Disconnect autothrottle
  • Simultaneously roll wings level and rotate toward an initial pitch attitude of 15 degrees
  • Retract speed brakes
  • Follow flight director GA guidance (if available)

AUTOMATIC FLIGHT

  • Push either go-around switch
  • Verify TO/GA mode annunciation
  • Verify GA thrust
  • Retract speedbrakes
  • Monitor system performance

MANUAL OR AUTOMATIC FLIGHT

  • Do not change gear or flap configuration until windshear is no longer a factor
  • Monitor vertical speed and altitude.
  • do not attempt to regain lost airspeed until windshear is no longer a factor

Pilot Monitoring

  • Verify maximum thrust
  • verify all required actions have bee completed and call out any omissions
  • Verify GA thrust
  • verify all required actions have bee completed and call out any omissions
  • monitor vertical speed and altitude
  • Call out any trend toward terrain contact, descending flight path, or significant airspeed changes.
32
Q

Land impact Drill?

A

Captain

  • complete non-normal checklist ‘evacuation’
  • Check door safe to open
  • take torch
  • commence commands
  • fit saftey harness
  • open door
  • direct evacuation
  • When all assistance rendered, connect inertial real to saftey harness and evacuate through door.
  • Assemble crew away from aircraft assist on ground
  • Door unusable - remain, block, redirect, and reassess

First Officer

  • complete non-normal checklist ‘evacuation’
  • Take torch, NOTOC, loadsheet
  • Commence commands
  • Fit safety harness
  • Cinnect inertia reel to safety harness and evacuate through door
  • Report to emergency services if available
  • Door unusable - remain, block, redirect, and reassess
33
Q

Ditch impact Drill?

A

Captain

  • Complete non-normal checklist ‘ Ditching Preperation’
  • Check door safe to open
  • Fit life jacket and take torch
  • Commence commands
  • Open door
  • Launch rafts, ensure correct inflation
  • Direct evacuation
  • Ensure beacon taken
  • When all assistance rendered, evacuate
  • Door unuseable - remain, block, redirect, reassess

First Officer

  • Complete non-normal checklist ‘ Ditching Preperation’
  • Fit life jacket and take torch
  • Commence commands
  • Assist at door
  • Ensure beacon taken
  • When all assistance rendered, evacuate
  • Door unuseable - remain, block, redirect, reassess

Command Prep (10 decks)

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