737 manuvers Flashcards
GPWS
- Disconnect autopilot.
- Disconnect autothrottle.
- Aggressively apply maximum* thrust.
- Simultaneously roll wings level and rotate to an initial pitch attitude of 20°.
- Retract speedbrakes.
- If terrain remains a threat, continue rotation up to the pitch limit indicator (if available) or stick shaker or initial buffet.
- Do not change gear or flap configuration until terrain separation is
assured. - Monitor radio altimeter for sustained or increasing terrain separation.
- When clear of terrain, slowly decrease pitch attitude and accelerate.
TCAS RA
- 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 traffic requires other action.
TCAS RA During landing required climb
- Disengage the autopilot and autothrottle.
- Advance thrust levers forward to ensure maximum thrust is attained
- Call for FLAPS 15.
- Smoothly adjust pitch to satisfy the RA command. Follow the planned lateral flight path unless visual contact with
the conflicting traffic requires other maneuvers. - Verify a positive rate of climb on the altimeter and call “GEAR UP.”
Upset recovery conditions
- Pitch attitude greater than 25 degrees nose up, or
- Pitch attitude greater than 10 degrees nose down, or
- Bank angle greater than 45 degrees, or
- Flying at airspeeds inappropriate for the conditions.
Upset recovery - High nose recovery
• Disconnect autopilot and autothrottle
• Apply as much as full nose-down elevator
• Apply appropriate nose down stabilizer 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.
Upset recovery - nose down recovery
• Disconnect autopilot and autothrottle • Recover from stall, if required • Roll in shortest direction to wings level (unload and roll if bank angle is more than 90 degrees) • Recover to level flight: - Apply nose up elevator - *Apply nose up trim, if required - Adjust thrust and drag as required.
Wind sheer During TO
Predictive:
Caution - “monitor radar display” maneuver as required
Warning - “windsheer ahead” before V1 reject TO
after V1 normal rotate and perform escape maneuver
Real WS:
Near V1 - continue rotate at Vr max and perform escape maneuver
After V1 before Vr - continue until 2000 ft end of RWY rotate and escape maneuver
WS during final
Predictive “go around, WS ahead” - perform escape or normal GO AROUND
WS - siren x 2 + “windsheer x 3” - perform escape maneuver
Windshear warning manual maneuver
- Disconnect autopilot.
- Press either TO/GA switch.
- Aggressively apply maximum thrust
- Disconnect autothrottle.
- Simultaneously roll wings level and rotate toward an initial pitch attitude of 15°.
- Retract speedbrakes.
- Follow flight director TO/GA guidance (if available)
- Do not change flap or gear 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.
Windshear warning Autopilot maneuver
- Press either TO/GA switch
- Verify TO/GA mode annunciation.
- Verify GA thrust.
- Retract speedbrakes.
- Monitor system performance
- Do not change flap or gear 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.
Rejected Takeoff Conditions
Prior to 80 knots, the takeoff should be rejected for any of the following:
• activation of the master caution system
• system failure(s)
• unusual noise or vibration
• tire failure
• abnormally slow acceleration
• takeoff configuration warning
• fire or fire warning
• engine failure
• predictive windshear warning
• if a side window opens
• if the airplane is unsafe or unable to fly.
Above 80 knots and prior to V1, the takeoff should be rejected for any off the following
• fire or fire warning
• engine failure
• predictive windshear warning
• if the airplane is unsafe or unable to fly
Rejected Takeoff
Announce REJECT and:
Without delay simultaneously:
1. Close the thrust levers
2. disengage the autothrottles and
3. apply maximum manual wheel brakes or verify operation of RTO autobrake.
4. Raise SPEED BRAKE lever.
5. Apply reverse thrust up to the maximum amount consistent with
conditions. Continue maximum braking until certain the airplane will stop on the runway.
Reject Takeoff after Airplane Stop
- Perform procedures as required.
- Review Brake Cooling Schedule for brake cooling time and precautions (refer to Performance Inflight Chapter.)
- Consider the following:
The possibility of wheel fuse plugs melting
The need to clear the runway
The requirement for remote parking
Wind direction in case of fire
Alerting fire equipment
Not setting the parking brake unless passenger evacuation is necessary
Advising the ground crew of the hot brake hazard
Advising passengers of the need to remain seated or evacuate
Completion of Non-Normal checklist (if appropriate) for conditions which caused the RTO.
ENG FAIL IN CLIMB
HDG SEL BANK 15 SPD VZF PW CONT mayday EFP
ENG FAIL IN CRUISE
A/T DISCONNECT N1 CONT FMC ENG OUT PAGE SET ENG OUT ALT ENG OUT SPD LVL CHG MAYDAY NNC AT CRZ LVL ENG OUT LRC FUEL & TIME
