Drills/Limitations Flashcards
Airspeed Unreliable
1 Autopilot disconnect switch . . . . . . . . . . . . Push
2 A/T ARM switches (both) . . . . . . . . . . . . . . . OFF
3 F/D switches (both). . . . . . . . . . . . . . . . . . . OFF
4 Set the following gear up pitch attitude and thrust:
Flaps extended . . . . . . . . . . . 10° and 85% N1
Flaps up. . . . . . . . . . . . . . . . .4° and 70% N1
Oceanic Diversion - All Engine
Condition: An emergency diversion is required while in
oceanic airspace but altitude can be
maintained.
1 Initiate applicable drills and time critical checklists.
2 Declare emergency and request clearance.
3 Choose one:
If clearance obtained:
Proceed per clearance.
If clearance unavailable:
Turn at least and offset as follows:
OCA - 30degrees L/R - offset 5NM
China - 30degrees R - offset 5NM
Russia - 30degrees R - offset 16.2NM
When established on the offset, +/- 500 ft.
Oceanic Diversion - Engine Out
Condition: One of these occurs in oceanic airspace:
- Engine Flameout
- Engine loss of thrust
- Intentional in-flight shutdown or thrust
reduction
1 Initiate applicable drills and time critical checklists.
2 Declare emergency and request clearance.
3 Choose one:
If clearance obtained:
Proceed per clearance.
Go to step 4
If clearance unavailable:
Turn at least and offset as follows:
OCA - 30degrees L/R - offset 5NM
China - 30degrees R - offset 5NM
Russia - 30degrees R - offset 16.2NM
Minimize descent until established on
the offset.
When established on offset, descend to
below FL290 and maintain +/-500 ft.
FD DOOR AUTO UNLOCK
FD DOOR ACCESS selector . . . . . . Rotate to DENY
and hold for 1 second
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.
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Aborted Engine Start L, R
Condition: On the ground, an aborted engine start is
needed.
1 FUEL CONTROL switch
(affected side) . . . . . . . . . . . . . . . . . . . CUTOFF
Dual Eng Fail/Stall
Condition: Engine speed for both engines is below idle.
1 FUEL CONTROL switches
(both) . . . . . . . . . . . . . . . . . . CUTOFF, then RUN
2 RAM AIR TURBINE switch . . . . . . . Push and hold
for 1 second
- - - - - - - - - - - - - - - - - - - - - - -
Set airspeed above 270
APU selector (If APU available)…………..START, then ON
ENG AUTOSTART L, R
Condition: Autostart did not start the engine.
1 FUEL CONTROL switch
(affected side) . . . . Confirm. . . . . . . . . CUTOFF
ENG LIMIT EXCEED L, R
Condition: An engine limit exceedance occurs.
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
Condition: An engine surge or stall that requires crew
action is detected.
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
- - - - - - - - - - - - - - - - - - - - - - -
Eng Svr Damage/Sep L, R
Condition: One or more of these occur:
•Airframe vibrations with abnormal engine
indications
•Engine separation
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
- - - - - - - - - - - - - - - - - - - - - - -
Volcanic Ash
Condition: Volcanic ash is suspected when one or more
of these occur:
•A static discharge around the windshield
•A bright glow in the engine inlets
•Smoke or dust on the flight deck
•An acrid odor
Objective: To exit the ash cloud and restart engines if
1 Exit the volcanic ash as quickly as possible.
Consider a 180 degree turn. Consider a descending
turn.
2 Autothrottle disconnect switch . . . . . . . . . . Push
This step reduces possible engine damage or
flameout, or both, by decreasing EGT.
3 Thrust Levers ……………IDLE (if conditions permit)
4 Don the oxygen masks and smoke goggles, if
needed.
5 Establish crew communications, if needed.
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FIRE ENG L, R
Condition: Fire is detected in the 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
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STABILIZER
Condition: One of these occurs:
•Stabilizer movement without a signal to
trim
•The stabilizer is failed
1 STAB cutout switches (both). . . . . . . . . . CUTOUT
2 Do not exceed the current airspeed.
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ETOPS Diversion times/distances
330KTS S/E
60 458nm 75 (Benign) 549nm 120 878nm 138 1010nm 180 1317nm 207 1515nm
