MEMORY ITEMS Flashcards

1
Q

ABORTED ENGINE START L,R

A

FUEL CONTROL SWITCH (affected side)………………. CUTOFF
— - - - - - - - - - - - - - - - - - - - - - - - - - - —

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2
Q

AIRSPEED UNRELIABLE

A

A/P disconnect switch………….PUSH

A/T ARM switches (both)……..OFF

F/D switches (both)……………..OFF

Set the following gear up and pitch attitude and trust:

FLAP EXTENDED…….10* AND 85%N1
FLAP UP…………………4* AND 70 N1

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3
Q

CABIN ALTITUDE

A

1 Don the oxygen masks.

2 Establish crew communications.

3 Check the cabin altitude and rate.

4 If the cabin altitude is uncontrollable:

PASS OXYGEN switch . . . . . . . Push to ON and hold for 1 second

Without delay, descend to the lowest safe altitude or 10,000 feet, whichever is higher.

Caution! Autopilot and flight director descent near Vmo/Mmo may result in overspeed excursions due to wind and temperature changes. Pilot intervention via FLCH speed or manually flown pitch adjustment may be necessary to remain below Vmo/Mmo.

▼ Continued on next page ▼

[] CABIN ALTITUDE

Condition: Cabin altitude is excessive.

To descend: •Move the thrust levers to idle •Extend the speedbrakes •If structural integrity is in doubt, limit airspeed and avoid high maneuvering loads •Descend at Vmo/Mmo

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4
Q

DUAL ENGINE FAIL/STALL

A

1 FUEL CONTROL switches (both) . . . . . . . . . . . . . . . . . .CUTOFF, then RUN

2 RAM AIR TURBINE switch . . . . . . . Push and hold for 1 second

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5
Q

ENG AUTOSTART L,R

A

FUEL CONTROL switch (affected side)……CONFIRM…..CUTOFF

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6
Q

ENG LIMIT EXCEED

A

1 A/T ARM switch (affected side) . . . . .Confirm . . . . . . . . . . . OFF

2 Thrust lever (affected side) . . . . .Confirm . . . . . .Retard until ENG LIMIT EXCEED message blanks or the thrust lever is at idle

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7
Q

ENG SURGE L,R

A

1 A/T ARM switch (affected side) . . . . . . Confirm. . . . . . . . . . OFF

2 Thrust lever (affected side) . . . . .Confirm . . . . . .Retard until the ENG SURGE message blanks or the thrust lever is at idle

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8
Q

SEVERE DEMAGE

A

1 A/T ARM switch (affected side) . . . . . . . . . . Confirm . . . . . . OFF

2 Thrust lever (affected side) . . . . . . . . . . Confirm . . . . . . Idle

3 FUEL CONTROL switch (affected side) . . . . . . . . . . Confirm . . . CUTOFF

4 Engine fire switch (affected side) . . . . . . . . . . Confirm . . . . . . Pull

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9
Q

FIRE ENGINE

A

1 A/T ARM switch (affected side) . . . . . . . . . .Confirm . . . . . . OFF

2 Thrust lever (affected side) . . . . . . . . . .Confirm . . . . . . Idle

3 FUEL CONTROL switch (affected side) . . . . .Confirm . . . CUTOFF

4 Engine fire switch (affected side) . . . . . . . . . .Confirm . . . . . . Pull

5 If the FIRE ENG message stays shown:

Engine fire switch (affected side) . . . . . . . . . . Rotate to the stop and hold for 1 second

If after 30 seconds, the FIRE ENG message stays shown:

Engine fire switch (affected side). . . . . . . . . .Rotate to the other stop and hold for 1 second

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10
Q

STABILIZER

A

1 STAB cutout switches (both) . . . . . . . . . CUTOUT

2 Do not exceed the current airspeed

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