Limitations

Question 1

Max allowable weight of the acft at the gate?

Answer 1

53,250 lbs

Question 2

Max TOW

Answer 2

53,000 lbs

Question 3

Max ZFW

Answer 3

44,000 lbs

Question 4

Max Landing Weight

Answer 4

47,000 lbs

Question 5

Min OAT for takeoff?

Answer 5

-40 Degrees C

Question 6

Max tailwind for t/o and landing?

Answer 6

10 knots

Question 7

Max alt

Answer 7

FL410

Question 8

Flight must be w/in 45 min of nearest suitable airport under what conditions?

Answer 8

If cargo is carried in cargo compartment.

Question 9

With BTMS operative, min brake cooling time between landing or rejected t/o and subsequent t/o?

Answer 9

15 minutes

Question 10

Max weight in the cargo compartment?

Answer 10

3,500 lbs

Question 11

Max crosswind on a wet runway?

Answer 11

27 knots

Question 12

Max crosswind on contaminated runway w/braking action less than good?

Answer 12

15 knots

Question 13

Max crosswind if the Capt has less than 100 hours PIC in type?

Answer 13

27 knots

Question 14

Max speed to lower landing gear?

Answer 14

250 knots

Question 15

Max speed to raise landing gear?

Answer 15

200 knots

Question 16

Max speed with landing gear extended?

Answer 16

250 knots

Question 17

Vfo for flaps 8?

Answer 17

200 knots

Question 18

Vfo for flaps 20?

Answer 18

200 knots

Question 19

Vfo for flaps 30?

Answer 19

185 knots

Question 20

Vfo for flaps 45?

Answer 20

170 knots

Question 21

Vfe for flaps 8?

Answer 21

215 knots

Question 22

Vfe for flaps 20?

Answer 22

215 knots

Question 23

Max cargo loading weight

Answer 23

3500 lbs

Question 24

Max airport pressure alt for t/o and landing

Answer 24

10,000 ft

Question 25

Max ambient air temp approved for t/o and landing

Answer 25

ISA + 35 degrees C

Question 26

Mx action is required if L(R) COWL A/ICE messages are not extinguished above what N2?

Answer 26

78%

Question 27

The engine cowl anti-ice system must be ON when:

Answer 27

1) When in icing conditions | 2) When ICE is annunciated by the ice detection system

Question 28

T/F Aircraft indicated SAT or TAT may not be used on the ground.

Answer 28

True

Question 29

Maximum runway slope

Answer 29

+/- 2 degrees

Question 30

Minimum flight crew

Answer 30

One pilot and one copilot

Question 31

Engines must be running how many minutes prior to takeoff?

Answer 31

2 minutes

Question 32

Operate engines at IDLE for a minimum of now many minutes prior to shutdown?

Answer 32

2 minutes

Question 33

Taxi-in time with engines below what percent may be included in the two minute cool down period?

Answer 33

80% N2

Question 34

Cold Soak definition

Answer 34

Before the first flight of the day and the aircraft has been at an ambient temp of -30 degrees C or below for more than eight hours.

Question 35

Cold Soak engine start requirements

Answer 35

Motor for 60 seconds AND verify fan rotation.

Question 36

Cold Soak thrust reverser requirements

Answer 36

Actuate thrust reversers until the deploy and stow cycles are less than 5 seconds.

Question 37

Starter Cranking Limits

Answer 37

First Start: one minute on, 10 seconds off

Question 38

Max N2 for starter use

Answer 38

55%

Question 39

Max ITT to initiate all ground starts

Answer 39

120 degrees C

Question 40

L and R main fuel tank max fuel imbalance

Answer 40

800 lbs

Question 41

Minimum fuel quantity for a go-around

Answer 41

450 lbs per wing in a level aircraft

Question 42

APU starting limits using aircraft batteries on the ground or for normal in-flight start

Answer 42

1st Start, 30 seconds 2nd Start, 30 seconds followed by 20 minutes off *A two minutes delay should be observed between cranking attempts to allow for cooling of starter and start contractor and for APU drainage.

Question 43

APU starting limits using ground power

Answer 43

1st start, 15 seconds 2nd start, 15 seconds followed by 20 minutes off *A two minutes delay should be observed between cranking attempts to allow for cooling of starter and start contractor and for APU drainage.

Question 44

Max altitude to use APU bleed air

Answer 44

15,000'

Question 45

APU bleed limit for engine start on the ground

Answer 45

No bleed air extraction limit, but once started, engines thrust must not exceed 70% N2.

Question 46

APU bleed limit for engine start during flight, single engine

Answer 46

APU bleed air extraction for an engine start is not permitted

Question 47

APU bleed limit for engine start during flight during double engine failure

Answer 47

APU bleed air extraction for engine starts is permitted 13,000' and below.

Question 48

Turbulence penetration airspeed

Answer 48

280 KIAS or 0.75 mach, whichever is lower

Question 49

Max speed for windshield wiper operations

Answer 49

220 KIAS

Question 50

Wind limits for takeoff

Answer 50

60 knots or a headwind component of >55 knots

Question 51

(T/F) The ADC source coupled to the active autopilot must be the same as that coupled to the ATC transponder during flight in RVSM airspace

Answer 51

True

Question 52

Max alt to extend flaps

Answer 52

15,000'

Question 53

Min alt (AGL) to extend spoilers

Answer 53

800' AGL

Question 54

Max flap setting to use spoilers

Answer 54

30 degrees

Question 55

Max taxi light operation time when stationary

Answer 55

10 minutes

Question 56

Minimum airspeed to use max reverse thrust

Answer 56

60 KIAS

Question 57

(T/F) Use of the ISI localizer and back course information is prohibited during back course approaches.

Answer 57

True

Question 58

Max ITT allowed during engine start.

Answer 58

900 deg C

Question 59

Max N2 split at idle?

Answer 59

2%