Limits

Question 0

Max operating alt

Answer 0

42000

Question 1

Max slope

Answer 1

2%

Question 2

Max takeoff and landing alt

Answer 2

13500

Question 3

Max takeoff and landing tailwind

Answer 3

15 kts

Question 4

Turbulent air pen speed

Answer 4

290 or 0.78M, whichever is less

Question 5

No latitudes greater than

Answer 5

87 degrees

Question 6

Max altimeter difference for RVSM

Answer 6

200’

Question 7

Max altimeter difference at sea level

Answer 7

40’

Question 8

Max difference between altimeter and field elevation

Answer 8

75’

Question 9

Do not operate WX radar within

Answer 9

50’ of personnel or fuel

Question 10

Max taxi weight

Answer 10

256000 lbs

Question 11

Max takeoff weight

Answer 11

255,000 lbs

Question 12

Max landing weight

Answer 12

210,000 lbs

Question 13

Max zero fuel weight

Answer 13

187,400 lbs

Question 14

Max cabin differential

Answer 14

8.6 +- 0.05

Question 15

Max cabin differential during climb

Answer 15

8.6 +- 0.10

Question 16

Max cabin differential for takeoff and land

Answer 16

0.125

Question 17

Equipment cooling for more than 20 min at 34-40C.

Answer 17

One forward and one aft door open OR one AC pack

Question 18

Equipment cooling for more than 20 min at 41-49C

Answer 18

One AC pack

Question 19

Equipment cooling for more than 20 min at more than 49C

Answer 19

Two AC packs

Question 20

After takeoff, autopilot not below

Answer 20

200’

Question 21

No autopilot below 100’ at fields above

Answer 21

8400

Question 22

Max Autoland headwind or crosswind

Answer 22

25

Question 23

Max Autoland tailwind

Answer 23

15

Question 24

Use CONT ignition in

Answer 24

Severe turbulence

Question 25

Max fuel temp

Answer 25

49C

Question 26

Min fuel temp

Answer 26

Higher of 3 degrees above freeze or -45C

Question 27

With less than full wing tanks and zero fuel limits applied, how much fuel can be in center tank

Answer 27

2000 lbs

Question 28

Transfer of aux fuel shall begin before center tank reaches

Answer 28

39,300 lbs

Question 29

Before aux fuel transfer

Answer 29

Flaps must be retracted

Question 30

APU starter duty cycle

Answer 30

3 starts in 60 min (5 min cooling between each)

Question 31

Max altitude for flaps

Answer 31

20,000’

Question 32

IRU alignment must not be attempted

Answer 32

Above 78 degrees N or S

Question 33

GPWS terrain display prohibited within

Answer 33

15 NM of an airport not in the database

Question 34

SDS hazard zone

Answer 34

230’ from tail

Question 35

Ground operating of SDS limited to 30 min with

Answer 35

Temp above 44F

Question 36

SDS operating envelope

Answer 36

45,000’

-54C to plus 55C

Question 37

SDS max maneuver rates

Answer 37

10 degrees per sec roll, pitch, or yaw