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

41,000’

Question 4

Maximum takeoff and landing altitude is _____ ft.

Answer 4

8400

Question 5

Maximum Turbulence Penetration airspeed is

Answer 5

280 KIAS/ .76 M

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

Operated 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 _____. (3 answers)

Answer 16

takeoff, landing, anti-ice operation

Question 17

Maximum start EGT is _____ degrees.

Answer 17

725

Question 18

ENGINE START Switches must be in the FLT position for _____.

Answer 18

operation in severe turbulence.

Question 19

Minimum engine 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 is _____ feet.

Answer 22

41,000

Question 23

Maximum altitude for APU operation with bleed loads only is _____feet.

Answer 23

17,000

Question 24

Maximum operating altitude for the APU is _____ feet.

Answer 24

41,000

Question 25

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

Answer 25

10,000

Question 26

Close the APU bleed valve when _____. (3)

Answer 26

Ground air connected and isolation valve open
Engine No 1 Bleed Valve open with No 1 engine running
Isolation Valve and Engine No 2 Bleed Valve open with Engine No 2 running

Question 27

Maximum flap extension altitude if _____ feet.

Answer 27

20,000

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

Minimum fuel temperature is ______ unless actual fuel freeze point is known.

Answer 30

-37 degrees C

Question 31

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

Answer 31

1000

Question 32

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

Answer 32

1675