Memory Items

Question 1

L (R) REV DEPLOYED

Answer 1

Affected thrust lever….. Confirm and IDLE

Question 2

ENGINE OVERSPD

Answer 2

Affected thrust lever….. Confirm and IDLE

Question 3

Uncommanded acceleration

Answer 3

Affected thrust lever….. Confirm and IDLE

Question 4

NO STRTR CUTOUT (In Flight)

APU or Cross Bleed Start

Answer 4

Affected ENG STOP……. STOP

Question 5

L (R) STRT VLV OPEN (In flight)

Answer 5

Affected ENG STOP……. STOP

Question 6

NO STRTR CUTOUT (On ground)

APU or Cross Bleed Start

Answer 6

Affected ENG STOP……. STOP

Question 7

L (R) STRT VLV OPEN (In flight)

APU or Cross Bleed Start

Answer 7

Affected ENG STOP……. STOP

Question 8

Loss of ALL AC Power (ADG Not Operative)

Answer 8

ADG Manual deploy handle…… Pull

Question 9

Aileron System Jammed

Answer 9

Autopilot…………. Disengage

Aileron Controls (Both)……………. Release pressure

ROLL DISC…………… Confirm then PULL AND TURN to lock

Airplane control……………. Transfer to pilot with operative aileron

Question 10

Elevator System Jammed

Answer 10

Autopilot…………………. Disengage

Elevator Controls (Both)………………. Release pressure

PITCH DISC………………. Confirm then PULL AND TURN to lock

Airplane control……………… Transfer to pilot with operative elevator

Question 11

Rudder System Jammed

Answer 11

YAW DAMPER DISC………………. Select

Rudder Pedals……………….. Overpower

Question 12

Stabilizer trim runaway

Answer 12

Control wheel……………………Assume manual control and override runaway

STAB TRIM DISC……………..Select

Question 13

Cabin Alt (Red)

Answer 13

Oxygen masks……….. Don and set to 100%

Crew Communication………… Establish

Question 14

Excessive Asymmetry or Loss of Braking (During landing)

Answer 14

Wheel brakes………….. Release momentarily

ANTI SKID…………… OFF

Wheel brakes………….. Re-apply as required

Question 15

Configuration warning

Answer 15

Takeoff…………. Discontinue immediately

Question 16

Rejected Takeoff

Answer 16

Simultaneously:
Thrust Levers………….. IDLE

Wheel brakes………….. Maximum until safe stop

Thrust reversers on operating engine(s)…………….. Maximum consistent with directional control

Question 17

Double Engine Failure

Answer 17

CONT IGNITION switch…………….. ON

Airspeed………… No less than 240 KIAS

Question 18

Unreliable Airspeed in Flight

Answer 18

Autopilot………………. Disconnect

Flight Directors………….. Deselect

Use ISI for pitch reference

• If initial take-off climb or go-around is required:

Pitch/N1……………. 10 degrees/TOGA from SL-15,000’

or
5 degrees/CLB above 15,000’

Question 19

Engine Failure in Climb during ALTS CAP, (V) ALTS CAP, or (V) ALTV CAP

Answer 19

Autopilot (if engaged)………… Disconnect

Pitch attitude…………… Adjust to maintain the required single engine operating airspeed.