Limitations

Question 1

Minimum width for a 180 turn?

Answer 1

24.3m

Question 2

Max ZFW

Answer 2

61,688kg

Question 3

Max Landing weight

Answer 3

65,317kg

Question 4

Overall length?

Answer 4

39.5m

Question 5

Max Operating Speed

Answer 5

340 kts

Question 6

Overall height?

Answer 6

12.5m

Question 7

Max operating Mach?

Answer 7

0.82

Question 8

AC indications with IDG online?

Answer 8

115v +/- 5v 400hz +/-10

Question 9

Voltage on DC busses?

Answer 9

28v, normal battery range 22-30v

Question 10

Fuel tank main capacity (each)

Answer 10

3915kg

Question 11

Centre tank capacity

Answer 11

13,066kg

Question 12

Total fuel tank capacity?

Answer 12

20,896kg

Question 13

Max/min fuel temp

Answer 13

+49/ -43 or fuel waxing temp +3c

Question 14

What fuel in centre tank means main tanks are full?

Answer 14

453kgs

Question 15

When will a LOW fuel alert display?

Answer 15

453kgs (alert extinguishes at 567kg)

Question 16

Config Fuel alert display?

Answer 16

Centre tank is greater than 726kg
Engines operating with centre pumps off or low pressure

Question 17

How many fuel measuring sticks are fitted to the a/c?

Answer 17

6 in each main tank and 4 in centre tank

Question 18

Dual channel approach requires:

Answer 18

2 A/P’s, flaps 30/40 deg, 25kt headwind, x-wind 20kts, tailwind 15kts unless flap 30 (12kts)

Question 19

White bug on takeoff speed select?

Answer 19

V2 +15

Question 20

White bug on App speed select?

Answer 20

Vref +20

Question 21

Upper amber band shows

Answer 21

When flaps are up 1.3G high speed buffet (40deg bank)

Question 22

Lower amber band?

Answer 22

Below 20,000ft 1.3G stick shaker
Above 20,000ft 1.3G low speed buffet

Question 23

Fuel imbalance number?

Answer 23

453kgs (goes at 91kg)

Question 24

Landing gear extension speed

Answer 24

270kts/ 0.82M

Question 25

Landing gear retraction speed

Answer 25

235kts

Question 26

Landing gear extended speed

Answer 26

320kts

Question 27

System A Hydraulic fluid quantity

Answer 27

21 litres

Question 28

Hydraulic system B quantity?

Answer 28

30 litres

Question 29

Minimum fuel in tank to allow ground running of an electric pump?

Answer 29

760kg

Question 30

Winglet clearance from ground?

Answer 30

3.9m

Question 31

X-wind limit

Answer 31

33kts

Question 32

Cabin begins to pressurise?

Answer 32

Lift off

Question 33

When is Eng anti ice turned on?

Answer 33

Part of before taxi cx list

Question 34

For a ground service, ground service switch is on?

Answer 34

Fwd flight attendant panel

Question 35

Accessory gearbox receives drive from?

Answer 35

N2 motor

Question 36

The amber ‘LE transit flaps are:

Answer 36

Inhibited when autoslats are operating in flight

Question 37

The supplemental and storage database has space for

Answer 37

40 navaids and 6 airfields

Question 38

FMC ‘buffet advisory’

Answer 38

Current conditions result in a manoeuvre margin less than required

Question 39

When will config alert extinguish?

Answer 39

Less than 363kg in centre tank

Question 40

The Standby hydraulic system powers the

Answer 40

Leading edge devices, rudder thrust reversers and alt yaw damper

Question 41

Landing gear transfer unit

Answer 41

Ensures system B can raise the gear with the loss of system A

Question 42

Minimum fuel on the ground for an electric motor driven hydraulic pump?

Answer 42

760kgs in that tank

Question 43

Amber display source annunciation

Answer 43

DEU 1/2 has failed

Question 44

MTOW

Answer 44

74,990 kg

Question 45

MTOW

Answer 45

75,216 kg

Question 46

Hyd system B pressurises the number 1 hyd pump why?

Answer 46

Redundancy if you lose an engine

Question 47

Elec & Hyd pumps for the engine at the same pressure?

Answer 47

Yes but volume 6x amount

Question 48

Predictive wind shear

Answer 48

1800’

Question 49

Predictive Alert for wind shear

Answer 49

1200’

Question 50

How do EEC take inputs or what?

Answer 50

Sensed flight conditions and bleed air demand

Question 51

What protection does EEC provide?

Answer 51

Over speed N1 & N2 protection

Question 52

Any EGT Redline flight protection

Answer 52

No

Question 53

What conditions for RTO

Answer 53

On ground, anti skid and auto brake system operational, wheel speed less than 60kts, thrust levers idle

Question 54

Overwings exits auto lock

Answer 54

3/4 doors shut, either engine running, thrust levers advance

Question 55

Dc power lost does emerg stay locked

Answer 55

No on ground

Question 56

V speeds entered on

Answer 56

Takeoff page 1

Question 57

Sustainable idle speed

Answer 57

50% N2

Question 58

Stabilised Engine

Answer 58

59%

Question 59

Oil temperature in amber band

Answer 59

45 mins

Question 60

RF comes on at

Answer 60

76%

Question 61

When is nose wheel unresponsive?

Answer 61

Gear pins are still in

Question 62

Tiller movement

Answer 62

78 deg

Question 63

Rudder turn

Answer 63

7 deg

Question 64

Pitch bar move up on take off speed?

Answer 64

60 kts

Question 65

What speed does a/t change from n1 in take off?

Answer 65

84kts

Question 66

When can Vnav be engaged?

Answer 66

LE Flaps

Question 67

TE bypass closes because of skew can TE be repositioned?

Answer 67

Yes Alt flap system, no protection though

Question 68

What’s the LE high lift devices

Answer 68

4 LE flaps, 8 LE Slats per Aircaft 12

Question 69

A/T LIMIT’

Answer 69

FMC not providing N1 limit values, degraded N1 limit value

Question 70

How much rudder authority do you have above 135kts?

Answer 70

25%

Question 71

STS system speed limits

Answer 71

100kts - 0.6M