B737-NG Memory Items

Question 0

ENGINE OVERHEAT

Answer 0

1) Autothrottle (if engaged) ……………… Disengage

2) Thrust lever
(affected engine) ……..Confirm… Close

3) IF the ENG OVERHEAT light stays illuminated:
- Go to the ENGINE FIRE or Engine Severe Damage or Separation Checklist on page 8.2

Question 1

Engine Fire
or
Engine Severe Damage 
or 
Separation

Answer 1

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
To Manually unlock the engine fire switch, press the override and pull

5) IF the engine fire switch or ENG OVERHEAT light stays illuminated:

  Engine Fire Switch ........... Rotate to the stop and hold for 1 sec.

IF after 30 sec the engine fire switch or ENG OVERHEAT  light stays
illuminated

  Engine Fire Switch ........Rotate to the other stop and hold for 1 sec

Question 2

Loss of Thrust on Both Engines

Answer 2

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 950˚C or there is no increase in EGT within 30 sec.

     Engine Start Levers 
     (affected engine)......Confirm................ CUTOFF
                                                     Then IDLE Detent

IF EGT again reaches 950˚C or there is no increase in EGT within 30 sec., repeat as needed.

Question 3

Engine Limit or Surge or Stall

Condition: One or more of these occur:

     - Engine indications are unusual
     - Engine indications are rapidly approaching or exceeding limits
     - Unusual engine noises are heard
     - There is no response to thrust lever movements.

Objective:
- To attempt to recover normal engine operations or shut down
the engine if recovery is not possible

Answer 3

1) Autothrottle (if enganged) …………………….. Disengage

2) Thrust lever
(affected engine)………Confirm………………. Retard until
indications stay
within limits or
the thrust lever
is closed

Question 4

APU Fire

Condition: Fire is detected in the APU

Answer 4

1) APU Fire Switch ……………Confirm………. Pull, Rotate to the
stop and hold for 1
sec.

2) APU Switch ……………………………………… OFF

Question 5

Aborted Engine Start
(without Automatic Ignition)

Condition: During a ground start, an abort engine start condition occurs.

Objective: To shut down the engine and motor it.

Answer 5

1) Engine Start Lever (affected engine) ………………. CUTOFF

Question 6

Takeoff Configuration

Condition:

On the ground, the intermittent cabin altitude/configuration warning horn sounds and the TAKEOFF CONFIG lights (if installed and operative) illuminate when advancing the thrust levers to takeoff thrust.

Answer 6

1) Assure correct airplane takeoff configuration.

Question 7

Overspeed

Condition:
Airspeed is more than Vmo/Mmo (340kias/M.82)

Answer 7

1) Reduce thrust and , if needed, adjust attitude to

reduce airspeed to less than Vmo/Mmo

Question 8

Warning Horn - CABIN ALTITUDE

Condition:
In flight, an intermittent horn sounds and the CABIN ALTITUDE lights (if installed and operative) illuminate, when the cabin altitude is at or above 10,000 feet

Answer 8

1)  If the intermittent warning horn sounds and the CABIN 
   ALTITUDE lights (if installed and operative) illuminate in 
   flight:

  Don the oxygen masks and set the regulators to 100%

  Establish crew communications.

-Go to the CABIN ALTITUDE WARNING or RAPID
DEPRESSURIZATION checklist on page 2.1-

Question 9

Warning Horn - TAKEOFF CONFIGURATION

Condition:
On the ground, an intermittent horn sounds and the TAKEOFF CONFIG lights (if installed and operative) illuminate, when the takeoff configuration is not correct during takeoff.

Answer 9

1) If the intermittent warning horn sounds and the TAKEOFF CONFIG lights
(if installed and operative) illuminate on the ground:

Assure correct airplane takeoff configuration

Question 10

Warning Horn - LANDING CONFIGURATION

Condition:
In flight, a steady horn sound when the landing configuration is not correct.

Answer 10

1) If the steady warning horn sounds in flight

  Assure correct airplane landing configuration

Question 11

CABIN ALTITUDE WARNING
or
RAPID DEPRESSURIZATION

Condition: One or more of these occur:
- A cabin altitude exceedance
- In flight, the intermittent cabin altitude/configuration warning horn sounds
and the CABIN ALTITUDE lights (if installed and operative) illuminate

Answer 11

1) Don oxygen masks and set regulators to 100%
2) Establish crew communications
3) Pressurization mode selector ………………………….MAN
4) Outflow VALVE switch …………………………………….. Hold in Close
until outflow valve
indicates fully closed
5) If cabin altitude is not controllable:
Passenger signs …………………………………………….. ON

IF the cabin altitude exceeds or is expected to exceed 14,000 ft:
PASS OXYGEN switch ........................................... ON

-Go to the Emergency Descent checklist on page 0.1-

Question 12

Airspeed Unreliable

Condition:
The pitch attitude is not consistent with the phase of flight, altitude, thrust and weight, or noise or low frequency buffeting is experienced.

Objective:
To establish the normal pitch attitude and thrust setting for the phase of flight.

Answer 12

1) Adjust the airplane attitude and thrust.
Maintain airplane control.
2) PROBE HEAT switches …………………………………….Check ON
3) Cross check the MACH/AIRSPEED indicators.

Question 13

Emergency Descent

Condtion: One or more of these occur:

• Cabin altitude cannot be controlled when the airplane is above 14,000 feet
• A rapid descent is needed

Answer 13

1) Announce the emergency descent.
The Captain will advise the cabin crew, on the PA system, of the impending rapid
descent. The first officer will advise ATC and obtain the area altimeter setting.
2) Passenger signs …………………………………………… ON
3) WITHOUT DELAY, descend to the lowest
safe altitude or 10,000 feet, whichever is
higher.
4) ENGINE START switches (both) ………………….. CONT
5) Thrust levers (both) ………………………………………. Reduce Thrust to
minimum or as needed
for anti-ice
6) Speedbrake …………………………………………………… FLIGHT DETENT

     *If structural integrity is in doubt, limit speed as much as possible 
      and avoid high maneuvering loads.*

7) Set target speed to Mmo/Vmo.

Question 14

Runaway Stabilizer

Condition: Uncommanded stabilizer trim movement occurs continuously

Answer 14

1) Control Column ……………………………… Hold Firmly
2) Autopilot (if engaged) …………………… Disengage

         Do NOT re-engage the autopilot.

         Control airplane pitch attitude manually with
         control column and main electric trim as needed.

3) IF the runaway STOPS: Done

4) IF the runaway CONTINUES:
STAB TRIM CUTOUT
switches (both) …………………………. CUTOUT

        IF the runaway CONTINUES:
        Stabilizer Trim Wheel .................... Grasp and hold