Maneuvers Flashcards

1
Q

Approach to stall recovery - PF

A

Initiate recovery: Hold column firmly, disengage A/P & A/T, nose down to reduce AoA until buffet or stick shaker stops (nose down elevator trim)
Continue recovery: Roll shortest direction to wings level, thrust levers as needed, retract speedbrakes, do not change gear/flaps configuration (during liftoff off with flaps up, call flaps 1)
Complete recovery: Check airspeed and adjust thrust, establish pitch attitude, return to desired flight path, re-automate

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2
Q

Approach to stall recovery - PM

A

Monitor altitude and airspeed
Verify all required actions have been done and call out omissions
Call out any trend toward terrain contact
Set flap lever as directed

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3
Q

Overweight landings

A

Normal procedures and techniques for approach and landing
- If stopping distance is a concern, reduce landing weight as much as possible
- At high gross weights and non-normals requiring flaps 25, brake energy limits likely exceeded
- Use longest available runway considering wind and slope
- Do not carry excess airspeed on final, particularly OEI or other non-normal

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4
Q

Overweight autolands

A

Not recommended - systems may not be adequate to task
If required (i.e. CAT III):
- Touchdown may be beyond normal touchdown zone - allow for additional landing distance
- Touchdown may be at higher than normal sink rates - possible to exceed structural limits
- Plan for go-around if autoland performance unsatisfactory

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5
Q

Rejected takeoff criteria below 80 kts

A

Master caution
System failure
Unusual noise or vibration
Tire failure
Abnormally slow acceleration
Takeoff configuration warning
Fire or fire warning
Engine failure
Predictive wind shear
Airplane unsafe or unable to fly

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6
Q

Rejected takeoff criteria 80 kts to V1

A

Fire or fire warning
Engine failure
Predictive wind shear warning
Airplane unsafe or unable to fly

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7
Q

Rejected takeoff

A

Simultaneously close thrust levers, disconnect autothrottle, and apply max brakes/verify RTO operation.
- If RTO selected, monitor performance and BPT apply max manual if AUTOBRAKES message shows
Raise speedbrake lever
Apply maximum reverse on symmetrical engines
Continue max braking until certain aircraft will stop on runway
Field length permitting, bring reverse thrust levers to to idle reverse detent by taxi speed

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8
Q

Rejected takeoff cleanup

A

Review brake cooling schedule (performance in flight)
Consider:
- Possibility of fuse plugs melting
- Need to clear the runway
- Requirement for remote parking
- Wind direction in case of fire
- Alerting fire department
- Not setting parking brake unless evacuation is necessary
- Advising ground crew of hot brake hazard
- Advising those on board to remain seated or evacuate
- Completion of NNC for conditions that caused the RTO

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9
Q

Ground proximity warning

A

Disengage autopilot/autothrottle
Aggressively apply maximum thrust
Roll wings level and pitch to initial pitch attitude of 20’
Retract speedbrakes
If terrain impact remains a threat, continue pitch to PLI, stick shaker, or initial buffet

  • Do not change configuration until terrain separation is assured
  • Monitor RADALT for sustained or increasing terrain separation
  • When clear of terrain, slowly decrease pitch attitude and accelerate
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10
Q

TCAS RA

A

Disconnect A/P & A/T
Adjust pitch to satisfy RA command
Follow planned lateral flight path unless visual contact with traffic requires other action

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11
Q

Climb TCAS RA in landing configuration

A

Disengage A/P & A/T
Advance thrust levers to maximum thrust and call “Flaps 20”
Adjust pitch to satisfy RA command
Follow planned lateral path unless visual contact requires other action
After positive rate of climb established, call “gear up”

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12
Q

Upset recovery - nose high

A

A/P & A/T - off
Apply nose down elevator and trim as required
Reduce thrust
Roll to obtain a nose down pitch rate

When approach horizon - wings level
Check airspeed and adjust thrust
Establish pitch attitude

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13
Q

Upset recovery - nose low

A

A/P & A/T - off
Recover from stall if needed
Roll the shortest direction to wings level (if AoB is more than 90’, unload wings then roll)
Nose up elevator and trim as required
Adjust thrust and drag as needed

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14
Q

Wind shear escape maneuver - manual flight

A

A/P - off
Push TO/GA switch
A/T - off
Apply maximum thrust
Roll wings level and pitch to 15’
Retract speedbrakes
Follow FD TO/GA guidance if available

Do not change configuration
Monitor vertical speed and altitude
Do not attempt to regain lost airspeed until clear of wind shear

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15
Q

Wind shear escape maneuver - automatic flight

A

Press TO/GA
Verify TO/GA mode annunciation
Verify thrust advances to GA power
Retract speedbrakes
Monitor system performance

Do not change configuration
Monitor vertical speed and altitude
Do not attempt to regain lost airspeed until clear of wind shear

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16
Q

V1 cut

A

Maintain directional control with rudder and aileron
Initiate rotation at VR, but pitch to 2 - 3’ below normal, 12-13’ at 1/2 deg/sec slower rate
Maintain minimum V2 - after liftoff, FD provides proper pitch guidance.
Climb at V2 to V2 + 10