777 > Maneuvers > Flashcards

Maneuvers Flashcards

(13 cards)

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1
Q

NADP 1 climb

A

Climb at V2 + 15
At 1500’ reduce to climb thrust
Accelerate to V2 + 25
At 3000’ retract flaps on schedule

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2
Q

NADP 2 climb

A

Initial climb accelerate at V2 + 15 to V2 + 25

At accelerate height or flap retraction altitude (normally 1000’) retract the flaps and accelerate to 250 or climb speed

At initial flap retraction or 1500 feet if there is a speed restriction, set climb thrust.

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3
Q

Go-around profile

A 
Initiate:
TO/GA, Flaps 20 (5 SE)
Verify go-around altitude
Verify or adjust thrust as needed
Positive rate - gear up
Limit bank angle to 15 degrees if airspeed is below minimum maneuver speed.

For a manual go-around:

  • Rotate manually
  • Select or verify go-around thrust
  • Engage autopilot as needed

Above 400’:
Select or verify roll mode
Verify MA altitude set in MCP
Verify route tracking

Acceleration Height:
Select speed for planned flap setting or 2 engines select VNAV (Optional).
If VNAV used set speed intervene.
Retract flaps on schedule

After planned flaps are set and at or above the selected flaps speed
2 engines:
Verify CLB thrust
Verify that the missed approach altitude is captured
After TO checklist
SE:
Select FLCH
Verify CON thrust
Verify the MA alt is captured
After TO checklist
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4
Q

Normal Takeoff

A

Manually advance thrust to stabilize
Push TO/GA

Takeoff roll
Set takeoff thrust by 80 kts
Monitor airspeed
Maintain light forward pressure

Positive rate - gear up

50’ LNAV engaged (within 2.5 nm)

400’ RA
Select or verify roll mode
Verify VNAV engaged

Initial climb speed V2 + 15

Thrust reduction (normally 1500’)
CLB thrust
V2 + 15 to V2 + 25

Acceleration height flap retraction altitude (normally 3000’)
Retract flaps on schedule

Flaps up
• Verify CON thrust (1 engine)
• Select and execute ENG OUT
(1 engine)
• Do the NNC (as needed)
• Do the After Takeoff checklist
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5
Q

Instrument Approach using VNAV

A

On vectors:
HDG SEL
pitch mode as needed

Enroute to fix:
L - arm LNAV or other roll mode
V - select VNAV
S - Select speed intervention as desired
A - If not cleared for approach: set lowest transition altitude or ATC assigned
If cleared for approach and established on a published segment between IAF and FAF: Set DA OR MDA

Approaching intercept heading:
Flaps 5

Intercept heading
Verify RNP
ARM LNAV or select appropriate roll mode

Inbound no later than 2 nvm from FAF:
Gear down, flaps 20, arm speedbrakes

Descent to DA or MDA:
Landing flaps
Landing checks
Verify crossing altitude and cross check altimeter
Monitor VNAV path

300’ below MA altitude:
Set MA altitude in MCP

AT DA or MDA:
Disengage A/P no lower than 200’ AGL

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6
Q

Instrument Approach using V/S or FPA

A

On radar vectors:

  • HDG SEL
  • Pitch mode (as needed)

Enroute to the fix:

  • LNAV or other roll mode
  • VNAV or other pitch mode

Approaching intercept heading:
- Flaps 5

Intercept heading:
- Arm LNAV or select other roll mode

No later than 2 nm from FAF and after ALT is engaged:

  • Set MDA
  • Gear Down
  • Flaps 20 (optional landing flaps 1 engine)
  • Arm speedbrakes

Descent to MDA:

  • Landing flaps (2 engine, optional 1 engine)
  • Set V/S or FPA
  • Do the landing checklist

Approximately 300’ above MDA:
- Set missed approach altitude

At MDA:
- Disengage A/P in accordance with regulatory requirements

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7
Q

Instrument Approach using RNAV (RNP) AR

A

On radar vectors:

  • HDG SEL
  • Pitch mode (as needed)

Enroute to the fix:

  • LNAV or other roll mode
  • VNAV or other pitch mode

Before being established on final approach course:
- Position flaps as needed to comply with applicable regulatory airspeed requirements.

Intercept heading:
- Arm or verify LNAV

No later than 2 nm from FAF:

  • Verify ALT, VNAV PATH, or VNAV ALT annuciated
  • Set DA
  • Select or verify VNAV
  • Speed intervention
  • Gear Down
  • Flaps 20 (optional landing flaps 1 engine)
  • Arm speedbrakes

Descent to DA:

  • Landing flaps (2 engine, optional 1 engine)
  • Do the landing checklist
  • At the FAF verify the crossing altitude matches the charted value within 100’

300’ below missed approach altitude:
- Set missed approach altitude

At DA:
- Disengage A/P in accordance with regulatory requirements

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8
Q

Circling Approach

A

If a missed approach is needed at any time while circling, make an initial climbing turn toward the landing runway and intercept the missed approach course.

Minimum Descent Altitude:

  • Select ALT HOLD (as needed)
  • Set missed approach altitude
  • Select HDG SEL / HDG HOLD or TRK SEL / TRK HOLD

Configuration at MDA:

  • Gear Down
  • Flaps 20 (landing flaps optional)
  • Speedbrakes armed

Before starting turn to base:

  • Landing flaps (if not previously selected)
  • Do the landing checklist

Intercepting landing profile:

  • Disengage A/P
  • on VNAV glide path of a visual approach path indicator, and on centerline with wings level no later than 300’ AGL.
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9
Q

Visual Traffic Pattern

A

Entering downwind:
- Flaps 5

Before starting the turn to base:

  • Gear down
  • Flaps 20
  • Arm speedbrakes
  • Start descent as needed
  • Start turn about 2.5 nm from the end of the runway

Base:

  • Landing flaps (2 engine, optional 1 engine)
  • Do the landing checklist
  • By 1000’ AGL stabilized on profile

On VNAV glide path or on glide path of a visual approach path indicator, and on centerline with wings level no later than 300’ AGL. Should be 2 - 2.5 nm from the end of the runway.

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10
Q

Touch and Go Landing

A

Touchdown:
- Target, minimum 1000’

After touchdown - touch and go:

  • Maintain runway alignment (PF)
  • Flaps 20 (PM)
  • Reset stabilizer trim (PM)
  • Check speedbrakes down (PM)
  • Thrust Levers vertical (PF)
  • Go around thrust (PF)

Rotate:
- Vref

Climb:
- Vref + 15 to 25

Crosswind:
- Flaps 5

Entering downwind:

  • Flaps 5
  • After takeoff checklist
  • Descent checklist (check or set AUTOBRAKE selector off)

Stabilized on downwind:
- Approach checklist

Before starting the turn to base:

  • Gear down
  • Flaps 20
  • Arm speedbrakes
  • Start descent as needed
  • Start turn about 2.5 nm from the end of the runway

Base:

  • Landing flaps (2 engine, optional 1 engine)
  • Do the landing checklist
  • By 1000’ AGL stabilized on profile

On VNAV glide path or on glide path of a visual approach path indicator, and on centerline with wings level no later than 300’ AGL. Should be 2 - 2.5 nm from the end of the runway.

  • No autobrakes, spoilers, or rev thrust
  • After touchdown PF calls “Flaps 20, reset trim” (~ 7 units)
  • Standup throttles — about 2” off idle detent (double click A/T disconnect button to disable warning)
  • PM calls “flaps and trim reset”
  • Manually advance throttles toward max
  • Pattern altitude 1500’ AGL
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11
Q

Balked landing after touchdown

A

If a go-around is initiated after touchdown but before thrust reverser selection:

  • Disengage the A/P and disconnect the A/T, while smoothly advancing the thrust levers to go-around thrust (the configuration warning siren sounds due to the landing flap configuration).
  • Verify the speedbrakes retract and autobrakes disarm.
  • Maintain landing flap configuration and smoothly rotate toward 15° go-around pitch attitude at no less than Vref.
  • Once airborne, push the TO/GA switch. This will activate the F/D go-around mode and re-engage the A/T in the THR mode.
  • When safely airborne with a positive rate of climb, continue the go-around and missed approach procedures as described in the FCOM/QRH.
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12
Q

Approach to Stall or Stall Recovery

A
  • Do not use F/D commands during recovery
  • If autopilot response is unacceptable, disengage
  • If autothrottle response is unacceptable, disengage

PM:

  • Monitor altitude and airspeed
  • Verify all required action have been completed and call out any omissions
  • Call out any trend toward terrain contact
  • Initiate recovery by smoothly applying nose down elevator until buffet or stick shakers stops.
  • Roll in shortest direction to wings level (if needed)
  • Advance thrust levers (as needed)
  • Retract speedbrakes
  • Do not change gear or flap configuration except: during liftoff, if flaps are up, call for flaps 1
  • Check airspeed and adjust thrust as needed, establish pitch attitude, return to desired flight path
  • Re-engage A/P and A/T, if desired
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13
Q

GPWS Warning

A

PM:

  • Assure maximum thrust
  • Verify all actions have been completed and call out any omissions
  • Monitor vertical speed and altitude
  • Callout any trend toward terrain contact

PF:

  • Disengage autopilot and autothrottle
  • Aggressively apply max thrust
  • Simultaneously roll wings level and rotate to 20° pitch attitude
  • Retract speedbrakes
  • If terrain is still a threat continue rotation up to pitch limit indicator or stick shakers
  • Do not change gear or flap configuration
  • Monitor radio altimeter for sustained or increasing terrain separation
  • When clear of the terrain, slowly decrease pitch attitude and accelerate
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