Memory Items

Question 1

FMC FAIL?

Answer 1

• If flying an approach that has an RNP alerting requirement:

Initiate a go-around unless a visual approach can be flown

Question 2

UNABLE RNP?

Answer 2

on a procedure or airway that has an RNP alerting requirement:

select an alternate procedure or airway. During an approach, initiate a go- around unless a visual approach can be flown

Question 3

ENGINE FIRE

or

Engine severe Damage or seperation

Answer 3

• A/T ARM switch - OFF
• Thrust Lever (affected side) - confirm - IDLE
• FUEL CONTROL switch (afected side) - Confirm - CUTOFF
• Engine Fire Switch (affected side) - Confirm - Pull
• IF the engine fire warning light is illuminated:

Engine fire switch affected side - Rotate to the stop and hold for one second

IF after 30 seconds the engine fire warning light stays illuminated:

Engine fire switch (affected side) - Rotate to the other stop and hold for one

second

Question 4

Engine Limit or Surge or Stall

Answer 4

• A/T ARM switch - OFF
• Thrust lever (affected side) - Confirm - Retard until engine indications

stay within limits or the thrust

is at idle

Question 5

Dual Engine Failure

Answer 5

• ENG START selectors (both) - FLT
• Thrust levers (both) - Idle
• FUEL CONTROL switches (both) - CUTOFF, then RUN
• If engine appears stalled or EGT approaces the standby Engine Indicator placard limit:

FUEL CONTROL switch (affected side) - Confirm - CUTOFF then RUN

IF engine appears stalled again or EGT approaches the standby engine

indicator placard limit, repeat as needed.

—————————————————————————————————————————-NOTE:

• start APU asap
• ABV 30000’ maintain 240kts minimum
• 30000’ and below use 220kt minimum

Question 6

Aborted Engine Start

Answer 6

• FUEL CONTROL switch (affected side) - CUTOFF

Question 7

CABIN ALTITUDE

or

Rapid Depressurization

Answer 7

• Oxygen Masks and regulators - ON, 100%
• Establish crew communications
• If ocupants in main cargo compartment:

MAIN CARGO ALERT switch - Push

• Check the cabin altitude and rate
• If the cabin is uncontrollable:

Without delay, descend to the lowest safe altitude of 10000’ which ever is

higher.

To descend:

• Move the thrust levers to idle
• Extend the speedbrakes
• If structual integrity is in doubt, limit airspeed and avoid high maneuvering

loads.

• Descend at VMO/MMO

Question 8

Airspeed Unrelible

Answer 8

• Autopilot disengage switch - Push
• A/T ARM switch - OFF
• F/D switches (both) - OFF
• set the following gear up pitch attidude and thrust:
  
  • Flaps extended - 10º and 80% N1
  • Flaps up - 4 º and 75% N1

NOTE:

The following are reliable;

• Attitude
• N1
• Ground speed
• Radio altitude

Question 9

Runway slope?

Answer 9

+/- 2%

Question 10

Max operating altitude?

Answer 10

43100’

Question 11

Max takeoff and landing altitude

Answer 11

8400’ pressure altitude

Question 12

Max takeoff and landing tail wind component

Answer 12

15kts

Question 13

Turbulent air penetration speed?

Answer 13

290kts/.78M

250kts below 10000’

Question 14

RVSM altimeter cross check limitations

Answer 14

• 200’ in flight
• on the ground differences =
  
  • sea level = FO-CAPT = 40’ FO or CAPT and feild elevation = 75’
  • 5000’ = 45’ = 75’
  • 10000 = 50’ = 75’

Question 15

Max Taxi weight?

Max Takeoff weight?

Max landing weight?

Max Zero fuel weight?

Answer 15

• 187 333 Kg
• 186 880 Kg
• 147 871 Kg
• 140 160 Kg

Question 16

Crosswind limitaions?

Dry runway?

Wet?

Standing water/slush?

snow no melting?

Ice no melting?

Reported RVR 200m or less (wet or dry)?

Reported vis between 200m-350m (wet or dry)?

Autoland?

Answer 16

Dry = 35Kt/ 35kt

Wet = 25kt/25kt

standing water/ slush = 15kt takeoff / 12kt landing

snow not melting = 15kt takeoff / 30 kt landing

ice not melting = 15kt takeoff / 12kt landing

200m or less = 10kts/10kts

200m-350m = 15kt takeoff

< 550m = 15kt landing

autoland = 15kts

note:

• inclusive of gusts
• reduce by 5kts if assy on contaminated or wet runways
• Take off and land on untreated now should only be attempted if no melting present.
• use rolling takeoff procedure if x-winf is greater than 20kts

Question 17

what is the lowest height the autopilot can be engaged after takeoff?

Answer 17

200’

Question 18

wind limits for autolands?

Answer 18

• 25kt head
• 15kt tail
• 15 kt x-wind

Question 19

Engine RPM limitations?

Answer 19

• N1 = low pressure rotor = 117.5%
• N2 high pressure rotor = 112.5%

Question 20

Engine EGT limitations?

Answer 20

• Takeoff = 960º = 5 min
• Max continuous = 925º = continuous
• Starting = 870º = max transient for 40 sec

= 750º = unlimited

Question 21

Minimum inflight fuel tank temperature?

Answer 21

• 3º above the freezing temperature of fuel

Question 22

Can you have center tank fuel without full main tanks?

Answer 22

• Yes,
• can contain upto 10000 kg of fuel without full main tanks provided the center tank fuel weight and the actual zero fule weight does not exceed the maximum zero fuel weight, and the center of gravity limits are observed.

Question 23

Max altitude with flaps extended?

Answer 23

20000’

Question 24

Approach to stall recovery?

Answer 24

INITIATE THE RECOVERY:

• hold the controll column firmly
• Discontect autopilot and autothrottle
• smoothly apply nose down elevator to reduce the angle of attack until stick shaker stops. nose down elevator may be needed.

CONTINUE THE RECOVERY:

• roll in the shortest direcction to wings level
• advance thrust levers as needed
• retract speedbrakes
• do not change gear or flap configuration, except
  
  • during liftoff, iff flaps are UP call for flaps 1

COMPLETE THE RECOVERY:

• Check airspeed and adjust thrust as needed
• Establish pitch attitude
• Return to desired flight path
• re-engage the autopilot and autothrottle if desired

Question 25

GPWS response?

Answer 25

CAUTION = corect the flight path or the airplane configuration WARNING = _Pilot Flying_ * disconnect the autopilot * disconnect the autothrottle * aggressivly appluy max thrust, simultaneously roll wings level and rotate to an initial pitch attitude of 20º * 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 speration is assured * monitor radio altimeter for sustained or increasing terrain seperation * when clear of terrain slowly decrease pitch attitude and accelerate * After the recovery manouver is complete, the aircrafts position together with the minimum safe altitude (MSA) or lowest safe altitude (LSALT)must be crossed checked _Pilot monitoring_ * Verify max thrust * Verify all required actions have been completed and call out any omissions * Monitor vertical speed and altitude (radio altitude for terrain seperation and barometric altitude for a minimum safe altitude) * call out any trend toward terrain contact. * After the recovery manouver is complete, the aircrafts position together with the minimum safe altitude (MSA) or lowest safe altitude (LSALT)must be crossed checked

Question 26

TCAS TA?

Answer 26

* Look for any conflicting traffic using display as a guide. Call out any conflicting traffic. * If traffic is sighted, manouver if needed. Note: Manouvres based soley on a TA may result in reduced seperation and are not recomended.

Question 27

TCAS RA?

Answer 27

* If manouvering 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 trafic requires other action * Attempt to establish visual contact. Call out any conflicting traffic _NOTE:_ A DESCEND RA issued below 1000' AGL should not be followed. The pilot has 5 seconds to make the controlled .25g pitch change required Following an increased strength or reversed corrective RA, the new target vertical speed must be attained within 2.5 seconds.

Question 28

Climb RA in landing configuration?

Answer 28

_Pilot Flying_ * Disengage the autopilot and discontect the autothrottle. * Advance thrust levers full foward to ensure maximum thrust is attained, and * call for FLAPS 20 * smoothly adjust pitch to satisfy RA command * follow the planned lateral flight path unless visual contact with the conflicting aircrtaft requires other action * Verify positive rate of climb and call GEAR IP * Attempt to establish visual contact. Call out any conflicting trafffic _Pilot monitoring_ * Verify maximum thrust is set. * position flap lever to 20 detent * verify a positive rate of climb on the altimeter and call "POSITIVE RATE" * Set landing gear lever to up

Question 29

Nose High Upset recovery?

Answer 29

_Pilot Flying_ * Recognise and confirm the situation * apply as much as full nose down elevator * apply appropriate nose down stabiliser 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. _Pilot Monitoring_ * Call out attitude, airspeed and altitude throughout the recovery * Verify all required actions have been completed and call out any omissions

Question 30

Nose Low Upset Recovery?

Answer 30

_Pilot Flying_ * Recognise and confirm the situation * Disconnect the autopilot and autothrottle * Roll in the shortest direction to wings level (unload and roll if bank angle is greater than 90 degrees) * REcover to level flight: * Apply nose up elevator * apply nose up trim, if required * adjust thrust and drag as required _Pilot moitoring_ * Call out attitude, airspeed and altitude throughout the recovery * Verify all required actions have been completed and call out any omissions

Question 31

Windshear Escape Manoeuvre?

Answer 31

_Pilot Flying_ ​_MANUAL FLIGHT_ * Disconect autopilot * push either go-around switch * Aggressively apply maximum thrust * Disconnect autothrottle * Simultaneously roll wings level and rotate toward an initial pitch attitude of 15 degrees * Retract speed brakes * Follow flight director GA guidance (if available) _AUTOMATIC FLIGHT_ * Push either go-around 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 _Pilot Monitoring_ * Verify maximum thrust * verify all required actions have bee completed and call out any omissions * Verify GA thrust * verify all required actions have bee completed and call out any omissions * monitor vertical speed and altitude * Call out any trend toward terrain contact, descending flight path, or significant airspeed changes.

Question 32

Land impact Drill?

Answer 32

_Captain_ * complete non-normal checklist 'evacuation' * Check door safe to open * take torch * commence commands * fit saftey harness * open door * direct evacuation * When all assistance rendered, connect inertial real to saftey harness and evacuate through door. * Assemble crew away from aircraft assist on ground * Door unusable - remain, block, redirect, and reassess _First Officer_ * complete non-normal checklist 'evacuation' * Take torch, NOTOC, loadsheet * Commence commands * Fit safety harness * Cinnect inertia reel to safety harness and evacuate through door * Report to emergency services if available * Door unusable - remain, block, redirect, and reassess

Question 33

Ditch impact Drill?

Answer 33

_Captain_ * Complete non-normal checklist ' Ditching Preperation' * Check door safe to open * Fit life jacket and take torch * Commence commands * Open door * Launch rafts, ensure correct inflation * Direct evacuation * Ensure beacon taken * When all assistance rendered, evacuate * Door unuseable - remain, block, redirect, reassess _First Officer_ * Complete non-normal checklist ' Ditching Preperation' * Fit life jacket and take torch * Commence commands * Assist at door * Ensure beacon taken * When all assistance rendered, evacuate * Door unuseable - remain, block, redirect, reassess