B737Ng Memory Items

Front 1

ENGINE FIRE or SEVERE DAMAGE OR SEPARATION

Back 1

Condition: one or more of the following occur: engine fire warning, airframe vibrations with unusual engine indications, engine separation

1. AUTOTHROTTLE...DISENGAGE

2. THRUST LEVER (AFFECTED ENGINE)....CONFIRM...CLOSE

3. ENGINE START LEVER (AFFECTED ENGINE)...CONFIRM...CUTOFF

4.ENGINE FIRE SWITCH... ...CONFIRM...PULL
(to manually unlock the engine fire switch, press the override and pull)

5. IF THE ENGINE FIRE SWITCH OR ENGINE OVERHEAT LIGHT STAYS ILLUMINATED:
ENGINE FIRE SWITCH...ROTATE TO THE STOP AND HOLD FOR 1 SECOND

IF AFTER 30 SECONDS THE ENGINE FIRE SWITCH OR ENG OVERHEAT STAYS ILLUMINATED:
ENGINE FIRE SWITCH...ROTATE TO THE OTHER STOP AND HOLD FOR 1 SECOND

Front 2

ENGINE OVERHEAT

Back 2

condition: an overheat is detected in the engine

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 SEVERE DAMAGE OR SEPARATION CHECKLIST

Front 3

LOSS OF THRUST ON BOTH ENGINES

Back 3

condition: both of these occur:
-both engines have a loss of thrust
-both ENG FAIL alerts show

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 950C or there is no increase in EGT within 30 sec:
ENGINE START LEVER (affected engine )...CONFIRM...CUTOFF, THEN IDLE DETENT
If EGT again reaches 950C or there is no increase in EGT within 30 sec, repeat as needed.

Front 4

ENGINE LIMIT OR SURGE OR STALL

Back 4

condition: one or more of the following 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 movement
objective: to attempt to recover normal engine operation or shut down the engine if recovery is not possible

1. AUTOTHROTTLE (if engaged)...DISENGAGE
2. THRUST LEVER (affected engine)...CONFIRM...RETARD UNTIL INDICATIONS STAY WITHIN LIMITS OR THRUST LEVER IS CLOSED

Front 5

APU FIRE

Back 5

condition: fire is detected in the APU

1. APU FIRE SWITCH...CONFIRM..PULL, ROTATE TO THE STOP, AND HOLD FOR 1 SECOND
2. APU SWITCH...OFF

Front 6

ABORTED ENGINE START

Back 6

(without automatic ignition)
condition: during a ground start, an abort engine start condition occurs.
objective: to shut down the engine and motor it

1. ENGINE START LEVER (affected engine)...CUTOFF

Front 7

TAKEOFF CONFIGURATION

Back 7

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 configuration.

1. ASSURE CORRECT AIRPLANE TAKEOFF CONFIGURATION

Front 8

OVERSPEED

Back 8

condition: airspeed is more than VMO/MMO

1. REDUCE THRUST AND, IF NEEDED, ADJUST ATTITUDE TO REDUCE AIRSPEED TO LESS THAN VMO/MMO.

Front 9

WARNING HORN- CABIN ALTITUDE OR CONFIGURATION

Back 9

condition: one of these occurs
- in flight an intermittent horn sounds and the CABIN ALTITUDE lights illuminate, when the cabin altitude is at or above 10,000ft
-on the ground, an intermittent horn sounds and the TAKEOFF CONFIG lights illuminate, when the takeoff configuration is not correct during takeoff.
-in flight, a steady horn sounds when the landing configuration is not correct

1. if the intermittent warning horn sounds and the CABIN ALTITUDE lights 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

2. IF the intermittent warning horn sounds and the TAKEOFF CONFIG lights illuminate on the ground:
-ASSURE CORRECT AIRPLANE TAKEOFF CONFIGURATION

3. If the steady warning horn sounds in flight:
ASSURE CORRECT AIRPLANE LANDING CONFIGURATION

Front 10

CABIN ALTITUDE WARNING OR RAPID DEPRESSURIZATION

Back 10

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 illuminate

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 thr the cabin is expected to exceed 14,000 feet :
-PASSENGER OXYGEN SWITCH...ON

Go to EMERGENCY DESCENT CHECKLIST

Front 11

AIRSPEED UNRELIABLE

Back 11

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

1. ADJUST THE AIRPLANE ATTITUDE AND THRUST. MAINTAIN AIRPLANE CONTROL
2. PROBE HEAT SWITCHES....ON
3. CROSS CHECK MACH/AIRSPEED INDICATORS

Front 12

EMERGENCY DESCENT

Back 12

condition: one or more of these occcur:
-cabin altitude can not be controlled when the airplane is above 14,000 feet
-a rapid descent is needed

1. ANNOUNCE THE EMERGENCY DESCENT.
THE CAPTAIN WILL ADVISE THE CABIN CREW, ON THE PA SYSTEM, OF 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 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 TO MMO/VMO

Front 13

RUNAWAY STABILIZER

Back 13

condition: uncommanded stabilizer trim movement occurs continously

1. CONTROL COLUMN...HOLD FIRMLY
2. AUTOPILOT (if engaged)...DISENGAGE
-DO NOT reengage the autopilot.
-CONTROL AIRPLANE PITCH ATTITUDE MANUALLY WITH CONTROL COLUMN AND MAIN ELECTRIC TRIM AS NEEDED.
3. IF THE RUNAWAY STOPS: End of Procedure
4. IF THE RUNAWAY CONTINUES:
-STAB TRIM CUTOUT SWITCHES (both)...CUTOUT
-IF THE RUNAWAY CONTINUES:
-STABILIZER TRIM WHEEL...GRASP AND HOLD

END OF PROCEDURE