Limits

Question 1

What is max operating altitude?

Answer 1

43,100 feet

Question 2

Main deck cargo door max wind for operating?

Answer 2

40 knots

Question 3

Main deck cargo door max wind while in the open position?

Answer 3

60 knots

Question 4

Max runway slope?

Answer 4

+/- 2%

Question 5

Max takeoff and landing altitude?

Answer 5

8400 feet pressure altitude

Question 6

Max takeoff and landing tailwind component?

Answer 6

15 knots

Question 7

Contaminated runway max depth of allowable precipitation?

Answer 7

6cm of dry snow, 12mm of standing water, wet snow, slush.

Question 8

Maximum airspeed?

Answer 8

360 knots IAS, 0.86 Mach.

Question 9

Minimum airspeed clean?

Answer 9

Below FL200 VREF 30+80, FL200 and above VREF 30+100

Question 10

Max Alt for flap extension?

Answer 10

20,000 feet

Question 11

Flap 25 landing should be considered if VREF 30 + increments is in excess of………..?

Answer 11

150 knots

Question 12

Takeoff on……………….. is not to be attempted whatever the reported braking action?

Answer 12

Wet ice

Question 13

The minimum braking action for takeoff and landing is?

Answer 13

Poor, medium/poor, medium/poor.

Question 14

To provide bird strike protection do not exceed…………..below…………..feet.

Answer 14

313 knots, 8000 feet.

Question 15

What are the flight manoeuvring load acceleration limits?

Answer 15

Flaps up: +2.5g to -1.0g

Flaps down: +2.0g to 0.0g

Question 16

Turbulent air penetration speed is …………………….., whichever is lower, and ………………… below 10,000 feet.

Answer 16

290 KIAS/0.78 Mach, 250 knots

Question 17

Is it permissible to operate HF radios during refuelling?

Answer 17

No

Question 18

Is it permissible to start the APU during refuelling operations?

Answer 18

No

Question 19

The maximum allowable in-flight difference between captain and first officer altitude displays for RVSM operations is…………..feet.

Answer 19

200

Question 20

Minimum inflight weight is………………..LBS.

Answer 20

168,000

Question 21

The maximum payload on the main cargo deck is………..LBS.

Answer 21

94,000

Question 22

If one fitting of the barrier net is damaged or has been disengaged, or one webbing strap has been cut the total main deck payload should be reduced to………………LBS.

Answer 22

56,400

Question 23

Payload LMCs are restricted to +/- …………LBS, and for fuel +/- ……….LBS.

Answer 23

1100, 4400.

Question 24

Max allowable cabin differential is…………… psi.

Answer 24

9.10

Question 25

Max operating differential during climb is.................psi.

Answer 25

8.6 +/- 0.10

Question 26

Max differential for takeoff and landing is..............psi.

Answer 26

0.125

Question 27

After takeoff the autopilot must not be engaged below ..........feet AGL.

Answer 27

400

Question 28

In an approach using V/S mode, the autopilot must be disengaged at or above............... feet above runway threshold elevation.

Answer 28

300

Question 29

On a single channel ILS approach, disengage the autopilot at not less than.................. feet above runway threshold elevation.

Answer 29

180

Question 30

The autopilot must be....................in severe turbulence.

Answer 30

Disengaged

Question 31

The maximum allowable wind speeds for automatic landing are:- Headwind...............knots, Tailwind................knots, Crosswind............knots.

Answer 31

25, 15, 25.

Question 32

The maximum and minimum glide slope angles for automatic landing are.....................and......................respectively.

Answer 32

3.1 and 2.5

Question 33

For an automatic landing, at least............ autopilots must be engaged and the autoland status annunciations must show...................at and below..................feet.

Answer 33

Two, land 2 or land 3, 600.

Question 34

APU starter duty cycle?

Answer 34

Maximum of 3 consecutive starts or attempts within a 60 minute period.

Question 35

Engine starter duty cycle, normal and extended.

Answer 35

Normal, 5 minutes on followed by half a minute off per minute on. Extended, 2 consecutive 5 minute cycles require a 10 minute cooling period before additional 5 minute cycles.

Question 36

Engine RPM, the maximum N1 for the low pressure compressor rotor is................%. N2 intermediate pressure compressor rotor is............. %

Answer 36

117. 5 | 110. 5

Question 37

Max engine EGT for takeoff is.............C for...............minutes.

Answer 37

940, 5

Question 38

Engine EGT maximum continuous is................C.

Answer 38

895

Question 39

Engine EGT max for starting is..........C maximum transient for.............seconds. And.............C unlimited.

Answer 39

870, 40 seconds | 750

Question 40

Minimum oil pressure is...........PSI.

Answer 40

10

Question 41

Maximum oil temperature for continuous operation is..........C, and for a maximum period of..................minutes is..............C.

Answer 41

160 | 15, 175

Question 42

Minimum oil quantity for despatch is............quarts

Answer 42

17

Question 43

Maximum fuel temperature is................C.

Answer 43

49

Question 44

Minimum fuel temperature is ...................or at least............above fuel freezing point, whichever is higher.

Answer 44

-45C, 3C

Question 45

The maximum fuel weight for the left or right wing tanks is........LBS. max for centre tank is..............LBS.

Answer 45

43,097, 32,367.