B777 Recalls

Question 1

Aborted Engine Start L, R

Answer 1

Condition: On the ground, an aborted engine start is
needed.
1 FUEL CONTROL switch
(affected side) . . . . . . . . . . . . . . . . . . . CUTOFF

Question 2

Airspeed Unreliable

Answer 2

Condition: Airspeed or Mach indications are suspected
to be unreliable. (Items which can indicate
unreliable airspeed are listed in the
Additional Information section.)
Objective: To identify a reliable airspeed indication, if
possible, or to continue the flight using the
Flight With Unreliable Airspeed table in the
Performance Inflight chapter.
1 Autopilot disengage 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 degrees and 85% N1
Flaps up . . . . . . . . . . .4 degrees and 70% N1

Question 3

[] CABIN ALTITUDE

Answer 3

Condition: Cabin altitude is excessive.
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, critical fuel scenario altitude, or 10,000
feet, whichever is higher.
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

Question 4

Dual Eng Fail/Stall

Answer 4

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

Question 5

[] ENG AUTOSTART L, R

Answer 5

Condition: During a ground start, one of these occurs:
•Autostart did not start the engine
•Fuel control switch is in RUN at low engine
RPM with the autostart switch OFF
1 FUEL CONTROL switch
(affected side) . . . . . . . . . . . . . . . . . . . CUTOFF

Question 6

Eng Lim/Surge/Stall L, R

Answer 6

Condition: One or more of these occur:
•Engine indications are abnormal
•Engine indications are quickly nearing or
show an exceedance
•Abnormal engine noises are heard,
possibly with airframe vibration
•There is no response to thrust lever
movement or the response is abnormal
•Flames in the engine inlet or exhaust are
reported
1 A/T ARM switch
(affected side) . . . Confirm . . . . . . . . . . . . . OFF
2 Thrust lever
(affected side) . . . Confirm . . . . . . . .Retard until
engine indications
stay within limits or
the thrust lever is at idle

Question 7

Eng Svr Damage/Sep L, R

Answer 7

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

Question 8

[] FIRE ENG L, R

Answer 8

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

Question 9

[] STABILIZER

Answer 9

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.

Question 10

Windshear

Answer 10

MANUAL FLIGHT
• Disengage autopilot
• Push either TO/GA switch
• Aggressively apply maximum* thrust
• Disconnect autothrottle(s)
• Simultaneously roll wings level and
rotate toward an initial pitch attitude
of 15°
• Retract speedbrakes
• Follow flight director TO/GA
guidance (if available)**

AUTOMATIC FLIGHT
• Push either TO/GA switch***
• Verify TO/GA mode annunciation
• Verify GA* thrust
• Retract speedbrakes
• Monitor system performance****

MANUAL OR AUTOMATIC FLIGHT
• Do not change gear or flap
configuration until windshear is no
longer a factor
• Monitor vertical speed and altitude
• Do not attempt to regain lost airspeed
until windshear is no longer a factor

Question 11

GPWS Warning

Answer 11

• Disengage autopilot
• Disconnect autothrottle(s)
• Aggressively apply maximum* thrust
• Simultaneously roll wings level and rotate
to an initial pitch attitude of 20°
• Retract speedbrakes
• If terrain remains a threat, continue rotation
up to the pitch limit indicator or stick
shaker or initial buffet
• Do not change gear or flap configuration
until terrain separation is assured
• Monitor radio altimeter for sustained or
increasing terrain separation
• When clear of the terrain, slowly decrease
pitch attitude and accelerate