Boeing MFF

Question 1

FIRE ENG L,R

FIRE ENG 1, 2, 3, 4

Answer 1

1 A/T ARM swithch (affected side )…OFF (777)
2 Thrust lever (affected engine) . . . .Confirm. . . . Idle
3 FUEL CONTROL switch (affected engine) . . . . Confirm. . . . . . .. . CUTOFF
3 Engine fire switch (affected engine) . . . . . . . . . . . Confirm. . . . . . . . . Pull
4 If the FIRE ENG message stays shown:
Engine fire switch (affected
engine) . . . . . . . Rotate to the stop and hold for 1 second
If after 30 seconds the FIRE ENG message stays shown:
Engine fire switch (affected engine). . . . .Rotate to the other stop and hold for 1 second

Question 2

ABORTED ENGINE START

Answer 2

FUEL CONTROL switch (Affected Eng) …. CUTOFF

Question 3

AIRSPEED UNRELIABLE

IAS DISAGREE

Answer 3

1 Check pitch attitude and thrust for phase of flight

2 If pitch attitude or thrust are not normal for the phase of flight:
Autopilot disengage switch . . . . . . . Push
Autothrottle disconnect switch . . . . .Push
F/D switches (both) . . . . . . . . . . . . . .OFF
Establish normal pitch attitude and thrust setting for the phase of flight.

Question 4

CABIN ALTITUDE

Answer 4

1 Don the oxygen masks.
2 Establish crew communications.
3 Check the cabin altitude and rate. Verify
that the packs are on and the outflow
valves are closed.
4 If the cabin altitude is uncontrollable:
SUPRNMRY or PAX OXY switch . . . .  Push
to ON and hold for 1 second
Without delay, descend to the lowest
safe altitude or 14,000 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 5

DUAL ENGINE FAIL/STALL

Answer 5

FUEL CONTROL switches (both) ..CUTOFF then RUN

RAM AIR TURBINE switch …Push and hold for 1 second

Question 6

ENG AUTOSTART L, R

ENG 1, 2, 3, 4 AUTOSTART

Answer 6

FUEL CONTROL switch (affected engine) . . . . . CUTOFF

Question 7

ENG LIM/SURGE/STALL L, R (777)

ENG 1, 2, 3, 4 LIM EXCEED (747-8)

Answer 7

A/T ARM swithch (affected side )…OFF (777)
Thrust lever (affected engine) . . . . Confirm. . .. Retard until the ENG LIM EXCEED message
blanks 747-8 or indications stay within limits on 777, or the thrust lever is at idle

Question 8

ENG LIM/SURGE/STALL (747)

Answer 8

A

Question 9

ENG SVR DAMAGE/SEP L, R

Eng Svr Damage/Sep 1, 2, 3, 4

Answer 9

1 A/T ARM switch (affected side )…OFF (777)
2 Thrust lever (affected engine) . . . . Confirm. . . . Idle
3 FUEL CONTROL switch (affected
engine) . . . . . Confirm. . . . . . CUTOFF
4 Engine fire switch (affected engine) . . . . . . . Confirm. . . . . . . . . . Pull

Question 10

SMOKE, FIRE OR FUMES

Answer 10

Don the oxygen masks.

Question 11

STABILIZER (777)

STAB TRIM UNSCHD (747)

Answer 11

STAB cutout switches (both) … CUTOUT

Do not exceed the current airspeed

Question 12

a

Answer 12

A

Question 13

APPROACH TO STALL RECOVERY OR STALL RECOVERY

Answer 13

A

Question 14

REJECTED TAKE-OFF

Answer 14

Simultaneously:
Call “STOP”
Close Thrust Levers and disengage autothrottles
Verify operation of RTO autobrakes or apply maximum manual wheel brakes
If RTO autobrakes is selected:
Monitor system performance and apply manual wheel brakes if the AUTOBRAKE message is displayed or deceleration is not adequate
Apply the maximum amount of reverse thrust consistent with conditions
If AUTO speedbrake fails:
Raise speedbrake lever
Continue maximum braking until certain the airplane will stop on the runway

Question 15

GROUND PROXIMITY CAUTION

Answer 15

A

Question 16

GROUND PROXIMITY WARNING

Answer 16

A

Question 17

TCAS TA

Answer 17

Look for traffic using traffic display as a guide. Call out any conflicting traffic
If traffic is sighted: Maneuver if needed

Question 18

TCAS RA, EXCEPT A CLIMB IN LANDING CONFIGURATION

Answer 18

If maneuvering is required:
Disengage the autopilot and autothrottle
Smoothly adjust pitch and thrust to satisfy the RA command
Follow the planned lateral flight path unless visual contact with the conflicting traffic requires other action

Attempt to establish visual contact. Call out any conflicting traffic

Question 19

TCAS RA, CLIMB IN LANDING CONFIGURATION

Answer 19

Disengage the autopilot and autothrottle
Advance thrust levers forward to ensure maximum thrust is attained (PM-Verify maximum thrust set) and call for FLAPS 20. (PM-Position flap lever to 20 detent)
Smoothly adjust pitch to satisfy the RA command
Follow the planned lateral flight path unless visual contact with the conflicting traffic requires other action

After a positive rate of climb established, call for GEAR UP
( PM- Verify a positive rate of climb on the altimeter and Select landing gear lever to UP)

Question 20

UPSET RECOVERY, NOSE HIGH

Answer 20

Recognize and confirm the situation.
• Disconnect autopilot and autothrottle
• Apply as much as full nose down elevator
• Apply appropriate nose down stabilizer trim
• Reduce thrust
• Roll (adjust bank angle) to obtain a nose down pitch rate
• Complete the recovery:
when approaching the horizon, roll to wings level
check airspeed and adjust thrust establish pitch attitude

Question 21

UPSET RECOVERY, NOSE LOW

Answer 21

Recognize and confirm the situation.
• Disconnect autopilot and autothrottle
• Recover from stall, if required
• Roll in the shortest direction to wings level (unload and roll if bank angle is more than 90 degrees)*
• Recover to level flight:
• apply nose up elevator
• apply nose up trim, if required*
• adjust thrust and drag as required

Question 22

PREDICTIVE WINDSHEAR CAUTION

Answer 22

For predictive windshear caution alert: (“MONITOR RADAR DISPLAY” aural)
If a windshear encounter is anticipated, engage the autopilot (if not already engaged).
Maneuver as required to avoid the windshear

Question 23

PREDICTIVE WINDSHEAR WARNING DURING TAKE-OFF ROLL

Answer 23

“WINDSHEAR AHEAD, WINDSHEAR AHEAD” aural
• Prior to V1: Reject take-off
• After V1: Perform the Windshear Escape Maneuver.
If windshear is encountered prior to V1:
– There may not be sufficient runway remaining to stop if an RTO is initiated at V1.
– At VR, rotate at a normal rate toward a 15 degree pitch attitude.

When airborne:
Perform the Windshear Escape Maneuver.
If windshear is encountered near the normal rotation speed and airspeed stagnates or suddenly decreases:
– There may not be sufficient runway left to accelerate back to normal take-off speed.
– Ensure maximum thrust is set.
– Initiate a normal rotation at least 2000 feet before the end of the runway even if airspeed is low.
– Higher than normal attitudes may be required to lift off in the remaining runway.

Question 24

PREDICTIVE WINDSHEAR WARNING DURING APPROACH

Answer 24

“GO-AROUND, WINDSHEAR AHEAD” aural

Call “Go-around” and perform a normal go-around.

If windshear is encountered:
Perform the windshear escape maneuver.

Question 25

WINDSHEAR ESCAPE MANEUVER

Answer 25

Autopilot Available
• Press either TO/GA switch*
• Follow FD commands if AP not engaged
• Verify TO/GA mode annunciation
• Verify thrust advances to GA Thrust
• Retract speedbrakes
• Engage Autopilot (if not already engaged)
• Monitor system performance

Manual Flight
• Press either TO/GA switch
• Aggressively apply maximum thrust
• Verify TO/GA mode annunciation
• Disconnect autothrottle
• Simultaneously roll wings level and rotate toward an initial pitch attitude of 15°
• Retract speedbrakes
• Follow flight director TO/GA guidance if available

Question 26

ENG 1, 2, 3, 4 SURGE (747-8)

Answer 26

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

Question 27

Engine

Answer 27

a