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B737 Memory Items > Drills and Procedures > Flashcards

Drills and Procedures Flashcards

AOM transmittal 24

1
Q

Rejected Takeoff

(“I Wills”)

A

“I Will’s” for continued takeoff, rejected takeoff and ground incident

(AOM 1.04.02 P46 or 1.04.06 P1-2)

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2
Q

Ground Incident

A

Following rejected takeoff, emergency landing, or other ground incident:

  1. If an immediate evacuation is not required, I will PA, “Remain seated. Remain seated.”
  2. If urgent contact with the In-Charge is required, I will PA “In-Charge Flight Attendant call (or report to) the flight deck.”
  3. If an evacuation is required I will call, “Checklist, Passenger Evacuation.”
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3
Q

Engine Fire / Failure / Severe Damage / Separation at or above V1

(“I Wills”)

A

“I Wills” for engine fail, fire, or severe damage after V1

(AOM 1.02.10 P5-7 or 1.04.02 P47-48)

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4
Q

Engine Inoperative Cruise Driftdown

A
  1. “Disengage autothrottle, set max continuous thrust.”
  2. “Set Engine Out on ECON CRZ page.”
  3. Set driftdown altitude and speed
  4. Slow to driftdown speed and select LVL CHG.
  5. All exterior lights on
  6. Advise ATC
  7. “Checklist, Engine Failure”
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5
Q

Rapid Depressurization and Emergency Descent

(“I Wills”)

A

“I Wills “ for rapid depressurization and emergency descent

(AOM 1.02.10 P12-14 or 1.04.02 P49-50)

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6
Q

Trafffic Avoidance (TA)

A
  1. Look for traffic using trafic display as a guide. Call out any conflicting traffic.
  2. If trafic is sighted, maneuver if needed.

Note: Maneuvers based solely on a TA may result in reduced separation and are not recommended.

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7
Q

Traffic Avoidance (RA)

A
  1. If maneuvering is required, PF disengage autopilot and autothrottle. Smoothly adjust pitch and thrust to satisfy RA command. Follow lateral flight path unless visual contact with conflicting traffic
  2. PM verify actions and notify ATC “Air Canada XXX, TCAS RA.”

*If in landing configuration, set max thrust and call “Flaps 15.” Verify positive rate and call “Positive rate” “Gear up.”

*WARNING: do not follow DESCEND RA issued below 1000 ft AGL

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8
Q

Define “Upset”

A

Any time the airplane is diverting from the intended airplane state

  • Pitch attitude greater than 25° nose up
  • Pitch attitude greater than 10° nose down
  • Bank angle greater than 45°
  • Within pitch and bank parameters but flying at air speeds inappropriate for the conditions
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9
Q

Nose High Recovery

A
  1. Recognize and confirm the situation (nose high and increasing, airspeed decreasing rapidly)
  2. Disengage autopilot and autothrottle
  3. Apply up to full nose-down elevator and appropriate nose down stabilizer trim
  4. Reduce thrust
  5. Roll to obtain nose down pitch rate (45º to 60°), using small rudder input only if required
  6. Recover
    a. Approaching the horizon, roll wings level
    b. Check airspeed and adjust thrust
    c. Establish pitch attitude

PM verifies required actions and calls out attitude, airspeed and altitude throughout the recovery.

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10
Q

Nose Low Recovery

A
  1. Recognize and confirm the situation (nose low and decreasing, airspeed rapidly increasing)
  2. Disengage autopilot and autothrottle
  3. Recover from stall, if required (nose down, reduce thrust)
  4. Roll in shortest direction to wings level (unload and roll if bank angle is more than 90°)
  5. Recover to level flight
    a. Apply nose up elevator
    b. Apply nose up trim, if required
    c. Adjust thrust and drag as required

PM verifies required actions and calls out attitude, airspeed and altitude throughout the recovery

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11
Q

GPWS Warning

A
  • “PULL UP”
  • “OBSTACLE OBSTACLE PULL UP”
  • “TERRAIN TERRAIN PULL UP”
  1. “Firewall”
  2. Disengage autopilot
  3. Disengage autothrottle
  4. Aggressively apply maximum thrust
  5. Simultaneously roll wings level and pitch to 20° nose up
  6. Retract speedbrakes
  7. If terrain contact imminent, continue to pitch up to limit indicator, respecting stick shaker or buffet
  8. Leave gear and flap configuration until terrain separation assured
  9. Both pilots monitor RAD ALT, and PM calls out any trend toward terrain contact
  10. When clear of terrain, slowly decrease pitch, accelerate and assess
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12
Q

Approach to Stall or Stall Recovery

A
  1. “Stall”
  2. Hold the control column firmly
  3. Disengage autopilot and autothrottle
  4. Smoothly apply nose down elevator until buffet or stick shaker stops
  5. Roll in shortest direction to wings level
  6. Advance thrust levers as needed
  7. Retract speedbrakes
  8. Do not change gear or flap configuration EXCEPT during liftoff, if flaps are up, call “Flaps 1”
  9. Complete recovery
    a. check airspeed and thrust
    b. establish pitch
    c. return to desired flight path
  10. Re-engage autopilot and autothrottle if desired
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13
Q

Windshear Identification

Aural Warnings and Flight Path Deviations

A

Predictive Windshear Aural Warnings
* “WINDSHEAR AHEAD, WINDSHEAR AHEAD”
* “GO AROUND, WINDSHEAR AHEAD”
* “WINDSHEAR, WINDSHEAR, WINDSHEAR”

Flight Path Deviations
* 15 KIAS
* 500 fpm vertical speed
* 5º pitch attitude
* 1 dot displacement from glideslope
* unusual thrust lever position for significant period of time

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14
Q

Windshear Escape Maneuver

A

Prior to V1, reject takeoff

After V1, perform Windshear Escape Maneuver

  1. “Windshear TOGA”
  2. Disengage autopilot
  3. Push TO/GA switch
  4. Aggressively apply maximum thrust
  5. Disengage autothrottle
  6. Roll wings level and rotate toward 15º pitch
  7. Retract speedbrakes
  8. Follow flight director

CAUTION
* Do not change flap or gear configuration until windshear is no longer a factor
* Maintain wing level to maximize climb gradient, unless a turn is required for obstacle clearance
* Do not attempt to regain lost airspeed until all windshear is no longer a factor

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15
Q

Low Energy Definition and Go-Around

All Engines Operating

A

Low-Energy Regime:
* Aircraft descending
* Thrust at or near idle
* Airspeed decreasing
* Height 50 ft or less above runway

Follow normal Go-Around procedure, expect ground contact, and ensure Vref prior to commencing climb.

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16
Q

Go-Around and Missed-Approach

One Engine Inoperative, flap 15

A

From flap 15 landing, use flap 1 — pilot must control yaw. Select max continuous thrust when flaps are retracted.

17
Q

Go-Around and Missed-Approach

One Engine Inoperative, flap 30 and autoland

A

From flap 30 landing, use flap 15

From LAND 3 or LAND 2 autopilot controls yaw until another roll or pitch mode, or altitude capture occurs above 400 AGL.

18
Q

Engine Failure During Go-Around / Missed Approach

A

Perform normal Go-Around and Missed Approach procedures

19
Q

CAB ALT Warning or Rapid Depressurization

A
  1. Don oxygen masks and set regulators to 100%
  2. Establish crew communication
  3. Fasten Belts - ON
  4. PA (if conditions permit) “Attention - Flight Attendants secure the cabin. Passengers take your seats.”
  5. Pressurization mode selector - MAN
  6. Outflow Valve switch - hold in CLOSE until indication shows fully closed
  7. If cabin altitude is uncontrollable:
    a. PASS OXYGEN switch - ON
    b. Go to Emergency Descent checklist
20
Q

Emergency Descent

A
  1. “Emergency Descent”
  2. PA (if not already done) “Attention - Flight Attendants secure the cabin, passengers take your seats.”
  3. Fasten Belts - ON
  4. Without delay, descend to lowest safe or 10,000 feet, whichever is higher:
    a. Move thrust levers to minimum or as needed for anti-ice
    b. Extend speedbrakes to FLIGHT DETENT
    c. If structural integrity is in doubt, limit airspeed and avoid high maneuvering loads
    d. Descend at Vmo/Mmo
  5. Landing Lights - ON
  6. ATC - ADVISE, OBTAIN ALT SETTING
  7. Transponder - 7700
  8. If cabin altitude cannot be controlled: PA “Attention, put on your oxygen masks immediately”
  9. “Checklist, Emergency Descent”
21
Q

Aborted Engine Start

A
  1. Engine start lever (affected engine) - CUTOFF
  2. “Checklist, Aborted Engine Start”
22
Q

Engine Limit or Surge or Stall

A
  1. Autothrottle (if engaged) - DISENGAGE
  2. Thrust Lever (affected engine) - confirm - retard until engine indications within limits or thrust lever closed
  3. “Checklist, Engine Limit or Surge or Stall”
23
Q

Loss of Thrust on Both Engines

A
  1. Engine Start switches (both) - FLT
  2. Engine start levers (both) - CUTOFF
  3. When EGT decreases, Engine Start levers (both) - IDLE detent
  4. If EGT reaches a redline, or there is no increase in EGT within 30 seconds:
    a. Engine start lever (affected engine) - confirm - CUTOFF, then IDLE detent
    b. If EGT again reaches a redline or there is no increase in EGT within 30 seconds, repeat as needed.
  5. “Checklist, Loss of Thrust on Both Engines”
24
Q

APU Fire

A
  1. APU Fire switch - confirm - Pull, rotate to the stop, and hold for 1 second
  2. APU switch - OFF
  3. “Checklist, APU Fire”
25
Q

Engine Overheat

A
  1. Autothrottle (if engaged) - DISENGAGE
  2. Thrust Lever (affected engine) - confirm - CLOSE
  3. If the ENG OVERHEAT light stays illuminated, go to Engine Fire or Engine Severe Damage or Separation checklist
26
Q

Smoke, Fire or Fumes

A
  1. Oxygen masks and smoke goggles - ON, 100%
  2. Crew and cabin communications - ESTABLISH
  3. “Checklist, Smoke, Fire or Fumes”
27
Q

Smoke or Fire from Lithium Battery

A
  1. If necessary, transfer control
  2. PA “Backup to the flight deck. Backup to the flight deck.”
  3. “Checklist, Smoke or Fire from Lithium Battery”
28
Q

Runaway Stabilizer

A
  1. Control column - HOLD FIRMLY
  2. Autopilot (if engaged) - DISENGAGE
  3. Autothrottle (if engaged) - DISENGAGE
  4. Control column and thrust levers - CONTROL AIRPLANE PITCH ATTITUDE AND AIRSPEED
  5. Main Electric Stabilizer trim - REDUCE CONTROL COLUMN FORCES
  6. If the runaway stops after the autopilot is disengaged - DO NOT RE-ENGAGE THE AUTOPILOT or AUTOTHROTTLE
  7. If the runaway continues after the autopilot is disengaged
    a. Stab Trim Cutout switches (both) - CUTOUT
    b. If the runaway continues - Stabilizer trim wheel - GRASP AND HOLD
  8. “Checklist, Runaway Stabilizer”
29
Q

Airspeed Unreliable
(Stick Shaker Deactivation)

A
  1. Autopilot (if engaged) - DISENGAGE
  2. Autothrottle (if engaged) - DISENGAGE
  3. Flight Director switches (both) - OFF
  4. Set the following gear up pitch attitude and thrust:
    a. Flaps extended - 10º and 80% N1
    b. Flaps up - 4º and 75% N1
  5. “Checklist, Airspeed Unreliable”
30
Q

Landing Configuration

A

Assure correct airplane landing configuration

31
Q

Takeoff Configuration

A

Assure correct airplane takeoff configuration

32
Q

Warning Horn (Intermittent) or Warning Light (CAB ALT or T/O CONFIG)

A
  1. If warning occurs in flight above 10,000 feet MSL
    a. Don oxygen masks and set to 100%
    b. Establish crew communications
    c. “Checklist, Cabin Altitude Warning or Rapid Depressurization”
  2. If the warning occurs on the ground when advancing the thrust levers to takeoff thrust:
    a. Assure the correct airplane takeoff configuration.
33
Q

Engine Fire or Engine Severe Damage or Separation

A
  1. Autothrottle (if engaged) - DISENGAGE
  2. Thrust lever (affected engine) - confirm - CLOSE
  3. Engine Start lever (affected engine) - confirm - CUTOFF
  4. Engine Fire switch (affected engine) - confirm - PULL
  5. If the engine fire switch or ENG OVERHEAT light is illuminated:
    a. Engine Fire switch - Rotate to the stop and hold for 1 second
  6. “Checklist, Engine Fire or Engine Severe Damage or Separation”
34
Q

Crew Incapacitation

Recognition and Actions

A

Recognition:

  1. Flight crew member does not respond intelligently to two communications
  2. Flight crew member does not respond to single verbal challenge, and/or a significant deviation from the standard flight profile exists.

Actions:

  1. Non-incapacitated crew member shall assume control and ensure safe flight profile
  2. Autopilot shall be engaged
  3. Non-incapacitated crew member shall request flight attendant or observer to assist.
  4. When aircraft at safe altitude and configuration, secure incapacitated pilot:
    a. Tilt seat back
    b. Move seat full aft and rudders full forward
    c. Move head back
    d. Use shoulder harness as a restraint
    e. When practicable, remove incapacitated flight crew member from seat and replace, if possible, with another flight crew member.
35
Q

Overrun Warning (ORW) - In Air

A

Execute a go-around

36
Q

Overrun Warning (ORW) - On Ground

A

Without delay, the PF shall:

  1. Simultaneously close thrust levers and apply maximum manual wheel brakes
  2. Verify (or deploy) Speed Brakes
  3. Apply reverse thrust up to maximum
  4. Continue maximum braking until certain the airplane can stop on the runway
  5. When stopping is assured, slowly stow thrust reversers by idle taxi

The PM shall:

Verify PF actions and callouts per RTO (max brakes, speed brakes, reverse, “60”)

37
Q

Reasons to Reject Takeoff Prior to 80 KIAS

A
  1. activation of master caution system
  2. system failure(s)
  3. unusual noise or vibration
  4. tire failure
  5. abnormally slow acceleration
  6. take-off configuration warning
  7. fire or fire warning
  8. engine failure
  9. predictive windshear warning
  10. airplane unsafe or unable to fly
38
Q

Reasons to Reject Takeoff After 80 KIAS

A
  1. fire or fire warning
  2. engine failure
  3. predictive windshear warning
  4. airplane unsafe or unable to fly

B737 Memory Items (9 decks)

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