Systems Limitations

Question 1

Max. Relief diff. Pressure during taxi, TO, and Lndg.

Answer 1

Must not exceed 1.0 psi

Question 2

Air data system.

Must both air data computers be operational for TO?

Answer 2

YES

Question 3

Air data system.

For RVSM

Answer 3

ADC source coupled to the active autopilot must be same as coupled ATC transponder during RVSM flight

If alternate static source is selected, airplane must not be operated in RVSM airspace

Question 4

Can pilot and copilot select alternate static source simultaneously?

Answer 4

No

Question 5

Operation of auto pilot is prohibited at altitudes below

Answer 5

200 feet AGL

Question 6

VOR approaches are not permitted with flaps set to

Answer 6

0

Question 7

Is the auto pilot approved for continued approach following engine failure on final approach?

Answer 7

No

Question 8

Maximum flap angle for single-engine auto pilot approach

Answer 8

20° with Vref +10 K TS

Question 9

Use of LNAV mode is not permitted when what is selected?

Answer 9

Lasertrak

Question 10

For takeoff and landing with cowl and/or wing anti-ice systems on. What applies to the bleed air system?

Answer 10

10 stage bleed air valves must be closed

Question 11

Air and press. Structural limitation

Max. Relief diff pressure in flight

Answer 11

9.20 psi

Question 12

AC Generator load limitation

Each Main Generator (0-35,000ft.)

Answer 12

30Kva

Question 13

AC Generator load limitation

Each Main Generator (35,000 and above)

Answer 13

25 KVA

Question 14

APU Generator load limitation

Answer 14

30

Question 15

Maximum load on TRU 1 or TRU 2

Answer 15

100 amps

Question 16

Maximum continuous load on essential TRU 1 and essential TRU 2 combined

Answer 16

75 amps

Question 17

If TRU one and TRU two loads are inadvertently exceeded on the ground

Answer 17

The nose bay doors must be open for 10 minutes prior to taxi for take off

Question 18

Flight with flaps extended is prohibited above

Answer 18

15,500

Question 19

Flight with spoilers extended is prohibited below

Answer 19

300 feet AGL

Question 20

Maximum permissible fuel in balance between the contents of the main fuel tanks

Answer 20

800 pounds

Question 21

Take off with up to 500 pounds of fuel in the auxiliary tank is permitted provided there is at least how much fuel in each wing tank and no fuel in the tail tank

Answer 21

1500 pounds of fuel in each wing tank

Question 22

Maximum usable fuel quantity is**

Answer 22

Left main tank, 4909 pounds
Right main tank, 4909 pounds
Fuselage tanks, ????
Total, ??? B

Question 23

Fuel jettison must not be initiated when tail tank quantity is below

Answer 23

30 pounds

Question 24

Thrust reverse above 60% N1 is not permitted at airspeeds below

Answer 24

60 kts.

Question 25

Maximum Crosswind component approved for use of reverse thrust is

Answer 25

24 kts.

Question 26

Taxi light must be switched off whenever the airplane is stationary in excess of

Answer 26

10 minutes

Question 27

Maximum nose wheel tire pressure

Answer 27

151 PSI +5-0% on the ground