Maneuvers Flashcards
NADP 1 climb
Climb at V2 + 15
At 1500’ reduce to climb thrust
Accelerate to V2 + 25
At 3000’ retract flaps on schedule
NADP 2 climb
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.
Go-around profile
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
Normal Takeoff
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
Instrument Approach using VNAV
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
Instrument Approach using V/S or FPA
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
Instrument Approach using RNAV (RNP) AR
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
Circling Approach
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.
Visual Traffic Pattern
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.
Touch and Go Landing
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
Balked landing after touchdown
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.
Approach to Stall or Stall Recovery
- 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
GPWS Warning
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
