Limitations

Question 1

Maximum landing tailwind component is _____ kts.

Answer 1

15

Question 2

Maximum takeoff tailwind component is _____ kts.

Answer 2

15

Question 3

Maximum operating altitude is ______.

Answer 3

41000

Question 4

Maximum takeoff and landing altitude is _____.

Answer 4

8400

Question 5

Maximum Turbulence Penetration airspeed is ______.

Answer 5

280 KIAS / .76M

Question 6

With engine bleed air switches ______ do not operate the air-conditioning packs in _______ for takeoff, approach or landing.

Answer 6

ON / HIGH

Question 7

Engine TAI must be ON when icing conditions exist or anticipated, except during climb or cruise below ______.

Answer 7

-40 degrees SAT

Question 8

Do not engage the autopilot below _______ AGL on takeoff.

Answer 8

1000

Question 9

For single channel ILS operation during approach the autopilot shall not remain engaged below _____ feet AGL.

Answer 9

50

Question 10

For manually flown HGS AIII approach the autopilot shall not remain engaged below ______ AGL.

Answer 10

500

Question 11

Use of aileron trim with autopilot engaged is ______.

Answer 11

prohibited

Question 12

Operate the engines for a minimum of ______ minutes prior to takeoff.

Answer 12

3

Question 13

Operate engines at or near idle (taxi thrust acceptable) for a minimum of _______ minutes prior to shutdown.

Answer 13

3

Question 14

Maximum time limit for Takeoff Thrust assuming normal takeoff with both engines operating is ______ minutes.

Answer 14

5

Question 15

Maximum time limit for Takeoff Thrust in the event of loss of engine thrust during takeoff is ______ minutes.

Answer 15

10

Question 16

ENGINE START Switches must be in the CONT position for ________. (Select all that apply)

Answer 16

1) takeoff
2) landing
3) anti-ice operation

Question 17

Maximum start EGT is _____ degrees

Answer 17

725

Question 18

ENGINE START Switches must be in get FLT position for ________.

Answer 18

operation in severe turbulence

Question 19

Minimum start pressure at sea level is _______ psi.

Answer 19

30

Question 20

Engine Starter Duty Cycle (normal starts) - limit each start attempt to a maximum of _______.

Answer 20

2 minutes

Question 21

Intentional use of reverse thrust in flight is ________.

Answer 21

prohibited

Question 22

Maximum altitude for APU operation with electrical loads only is _____ feet.

Answer 22

41000

Question 23

Maximum altitude for APU operation with bleed loads only is ______ feet.

Answer 23

17000

Question 24

Maximum operating altitude for the APU is ______ feet.

Answer 24

41000

Question 25

Maximum altitude for APU operation with both bleed and electrical loads is ______ feet.

Answer 25

10000

Question 26

Close the APU bleed valve when ______. (Select ALL correct)

Answer 26

1) ground air connected and Isolation Valve open
2) Engine No. 1 Bleed Valve open with No. 1 engine running.
3) Isolation Valve and Engine No. 2 Bleed Valve open with Engine No. 2 running

Question 27

Maximum flap extension altitude is ______ feet.

Answer 27

20000

Question 28

Do not deploy speed brakes in flight at radio altitudes less than ______ feet.

Answer 28

1000

Question 29

Random fuel imbalance must not exceed ______ lbs for taxi, takeoff, flight or landing.

Answer 29

1000

Question 30

(Ground operation) DO NOT turn Center Tank Fuel pumps ON unless center tank fuel quantity exceeds _____ lbs, except when refueling or transferring fuel.

Answer 30

1000

Question 31

Operating Electric Hydraulic Pumps on the ground requires a minimum of ______ lbs of fuel in the respective tank.

Answer 31

1675