Good To Know

Question 1

TO/GA on Ground Above 80 Knots

Answer 1

LNAV/VNAV disarmed
FD shows
Does not remove thrust derate
Thrust FMA stays HOLD

Question 2

TO/GA After Liftoff

Answer 2

Pitch&roll TO/GA
Flight director shows it off
THR REF set

Question 3

FLAP LIMIT

Answer 3

1 - 250
5 - 230
15 - 215
20 - 210
25 - 180
30 - 170

Question 4

TO/GA Armed

Answer 4

Flaps not up
GS captured

Question 5

Pulling Engine Fire Switch

Answer 5

Fuel valves close
Hydraulic pumps depressurized
Hydraulic fluid shuts off
Trips GEN off
Fire bottles ARM
Close engine anti ice valve
Removes power from thrust reverser

Question 6

Wing span
Min 180 turn width

Answer 6

60.1
788-42.2
789-47

Question 7

APU Fire Switch Pulled

Answer 7

Closes fuel valve
APU shuts down
Air inlet door closes
Trips off APU GEN
Shuts down APU
Arms APU bottle extinguisher
** bottle will discharge automatically after 15 sec

Question 8

TERR colors

Answer 8

Green - 2000 to 1000 below.
Dense Green - 1000 to 500 below.
Yellow- 500 below to 1000 above.
Dense Yellow- 1000 to 2000 above.
Red - greater than 2000 above.
Yellow - caution 40-60 sec impact.
Red - warning 20-30 sec impact.

Question 9

Predictive windshear

Answer 9

To be

Question 10

TCA RA

Answer 10

Climb - not below 1000ft, descent 1200ft, increase descent 1650ft
Descent - below 1000ft,

Question 11

Engine Out cruise PAVE

Answer 11

P-plan
A-access
E-enter
V-verify

Question 12

Engine

If OAT is above 40°C

Answer 12

Do not attempt to start both engine at the same time

Question 13

Engine warm up requirements:

Engine cool down

Answer 13

• Run the engines for at least 5 minutes

• Use a thrust setting normally used for taxi operations

• Engine oil temperature must be above the lower amber band before takeoff

• Run the engines for at least 5 minutes

Question 14

Oceanic in flight contingencies

Answer 14

Min 30 turn L or R
Offset 5nm
Attempt ATC clearance
Maintain FL as possible
ACAS
Exterior light on
Alert other aircraft on EMG FRQ
ALT + 500ft

Question 15

Atlantic WX deviation

Answer 15

ATC clearance
Visual + ACAS
Exterior lights ON
Report EMG FRQ
Up to 5nm maintain ALT
More than 5nm: SAND
South of track Ascend
North of track Descend

Resume clearance ALT within 5nm

Question 16

Items required “CONFIRM”

Answer 16

Autothrottle arm switch
Engine thrust lever
Fuel control switch
Engine or APU fire switch
Cargo fire arm switch
Generator drive disconnect switch

Question 17

Recommended Max LDW for one engine INOP G/A

Answer 17

230t

Question 18

Minimum T/O Fuel (OMA)

Answer 18

15t

Question 19

TO/GA available in flight

Answer 19

In flight, TO/GA is armed when flaps are out of up or glideslope is captured.

Question 20

Autothrottle stall protection

Answer 20

speed is less than an FMC calculated value for one second, and
• thrust is below reference thrust limit, and
• airplane barometric altitude is 400 feet above the airport on takeoff or airplane altitude is above 100 feet RA on approach

Question 21

Flaps up maneuvering speed

Answer 21

VREF 30 + 80

Question 22

Minimum command speed on approach

Answer 22

Auto land - VREF +5
Manual landing with autothrottle - VREF + 5 to Max +10
No autothrottle - half headwind component + full gust (Max + 15)
Direct head 50%, 45 degrees 35%…

Question 23

Severe Turbulence

Answer 23

Pax signe - ON
Flaps extension should be delayed as possible
During climb or descent us of VS is recommended
In cruise, it may be necessary to disconnect autothrottle
Set TPR at or slightly above the magenta line
Do not make sudden large control inputs

Question 24

flight control system provides rudder input

Answer 24

Above 65knt

Question 25

Speed reduction

Answer 25

For planning purposes, it requires approximately 80 seconds and 9 NM to decelerate from 330 to 250 knots in level flight without speedbrakes
Speedbrakes reduce time and distance by 60%

Question 26

Go-Around

Answer 26

TO/GA
Flaps 20
Positive rate - gear up
200’ AP-AT
At 400’ - LNAV-missed approach ALT
1000’ speed bug - flaps up
after flap retraction - FLCH or VNAV
CLB thrust
After takeoff checklist

Question 27

Fuel capacity

Answer 27

Wing 16.9 (9-16.77)
Main 67.9

Question 28

Engine

Answer 28

The airplane is powered by two Rolls-Royce Trent 1000J engines. The engines are rated at 73,800 pounds of takeoff thrust each.

Question 29

Electrically powered in addition to traditional systems

Answer 29

Engine start
Pressurization
Brakes
Stabilizer
Wing anti-ice

Question 30

Fuel Jettison

Answer 30

Fuel in center tank - 1360 kg/min
Center tank empty - 570 kg/min

Question 31

Time after shutdown to allow cool off to unpowered the airplane

Answer 31

10min with 2 sources
22min with 1 source

Question 32

Cargo compartment allowed to carry live animals

Answer 32

Forward cargo compartment
Bulk cargo compartment

Question 33

Slap liver position they extend or retract only the slats

Answer 33

0-1
20-25

Question 34

Hydraulic systems Powered items

Answer 34

LEFT
- flight controls / spoilers
- left engine thrust reverser

RIGHT
- flight controls / spoilers
- right engine thrust reverser

CENTER
- flight control / spoilers
- landing gear actuation
- leading edge slats
- nose gear steering
- trailing edge flaps

Question 35

Typical TPR

Answer 35

789
Europe 180-200t 52%-72%

USA or East Asia. 210-250t 72%-87%

Question 36

Emergency descent

Answer 36

30 turn, 5nm

China and India: 90 turn, China 25nm, India 15nm
Seychelle islands: 45 turn

Question 37

Landing performance must be assessed

Answer 37

The landing performance is in doubt; or

• Conditions are significantly less favourable than those presumed at time of dispatch; or

• The runway is contaminated; or

• LDA is less than 8,000 ft.

Question 38

PA announcements during emergency

Answer 38

No evacuation expected- 2 cabin chime

Evacuation expected-
2 min before landing “ צוות לסיים הכנות ולשבת לנחיתה “ + 2 cabin chime
40-5 seconds before landing - “ עבור לתנוחת חרום/ brace for landing “