MEMORY ITEMS Flashcards
ABORTED ENGINE START L,R
FUEL CONTROL SWITCH (affected side)………………. CUTOFF
— - - - - - - - - - - - - - - - - - - - - - - - - - - —
AIRSPEED UNRELIABLE
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
CABIN ALTITUDE
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.
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[] 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
DUAL ENGINE FAIL/STALL
1 FUEL CONTROL switches (both) . . . . . . . . . . . . . . . . . .CUTOFF, then RUN
2 RAM AIR TURBINE switch . . . . . . . Push and hold for 1 second
ENG AUTOSTART L,R
FUEL CONTROL switch (affected side)……CONFIRM…..CUTOFF
ENG LIMIT EXCEED
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
ENG SURGE L,R
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
SEVERE DEMAGE
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
FIRE ENGINE
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
STABILIZER
1 STAB cutout switches (both) . . . . . . . . . CUTOUT
2 Do not exceed the current airspeed