Limitations Oil, Fuel, Alt ect

Question 1

Maximum Cabin Pressure Differential

Answer 1

6.6 psi

Question 2

Altitudes (maximums) Normal Operations

Answer 2

35,000 ft.

Question 3

Altitudes (maximums) Yaw Damp Inoperative: Single Strake

Answer 3

17,000 ft

Question 4

Altitudes (maximums)Yaw Damp Yaw Damp Inoperative: Dual Strakes

Answer 4

No Limit

Question 5

Altitudes (maximums) Aviation gas Both standby Fuel Pumps Operative

Answer 5

31,000 ft.

Question 6

Altitudes (maximums) Aviation gas Both Either Standby Fuel Pump Inoperative:

Answer 6

20,000 ft.

Question 7

Altitudes (maximums) Aviation gas No crossfeed capability

Answer 7

above 20,000 ft.

Question 8

Electrical
Engine Starter

Answer 8

40 sec ON: 60 sec OFF: 40 sec ON: 60 sec OFF: 40 sec ON: 30 min OFF.

Question 9

Generator Load In flight: Below 31,000 ft:

Answer 9

100%

Question 10

Generator Load In flight: above 31000ft

Answer 10

88%

Question 11

Usable quantity:

Answer 11

Total 544 gallons / 3645 lbs.

Question 12

Main (per wing):

Answer 12

193 gallons / 1293 lbs

Question 13

Auxiliary (per wing):

Answer 13

79 gallons / 529 lbs

Question 14

Imbalance:

Answer 14

1000 lbs

Question 15

Crossfeed:

Answer 15

Only permitted with one engine inoperative.

Question 16

Yellow Arc:

Answer 16

Takeoff prohibited with less than 265 lbs of fuel in each wing.

Question 17

Auxiliary Fuel:

Answer 17

Do not put any fuel into the auxiliary tanks unless the main tanks are full.

Question 18

Powerplant/Propeller
Torque (ft-lbs)
 Transient:

Answer 18

2750 (5 sec)

Question 19

Powerplant/Propeller
Torque (ft-lbs)
All Other:

Answer 19

2230 - 2275 (up to 7 min)

Question 20

N1 (%) Idle:

Answer 20

61 minimum

Question 21

N 1 All Other:

Answer 21

101.5

Question 22

N1 Transient:

Answer 22

102.6 10 seconds

Question 23

n2 prop rpm idle

Answer 23

1180 minimum

Question 24

n2 prop rpm reverse

Answer 24

1900

Question 25

n2 prop rpm transient

Answer 25

2200 <5 seconds

Question 26

n2 prop rpm all other

Answer 26

2000-2040 (7min)

Question 27

Landing Gear cycle

Answer 27

Cydes (1 up - 1 down) are limited to one every 5 min for a total of 6 cycles, followed by a 15 min cool-down.

Question 28

Load factor (g’s): flaps UP

Answer 28

+3.17 / -1.27

Question 29

Load factor (g’s): flaps down

Answer 29

+ 2.00 / 0.00.

Question 30

Maximum Operating Air temperature limits
Sea level to 25,000 ft pressure altitude:

Answer 30

ISA +37

Question 31

Maximum Operating Air temperature limits
Above 25,000 ft pressure altitude:

Answer 31

ISA +31

Question 32

Oil Temperature (°C) starting
starting
takeoff
Max cont
transient

Answer 32

-40
0-99
0-99
0-104
99-104 limited to 5 min

Question 33

Minimum airspeed for sustained flight in icing:

Answer 33

140 kts

Question 34

Sustained flight in icing conditions with flaps extended is

Answer 34

prohibited

Question 35

Deice Boots: Minimum temperature for operation

Answer 35

-40c

Question 36

Engine Anti-ice: ENGINE ANTI-ICE switches should be ON below

Answer 36

5°C when operating in visible moisture.

Question 37

ENGINE ANTI-ICE switches should be OFF above

Answer 37

15°C for takeoff.

Question 38

Propeller Deice: Green Arc:(amp?)

Answer 38

18-24a

Question 39

Rudder Boost: Must be

Answer 39

operational for all flights.

Question 40

ADC 1 and 2 must be

Answer 40

operational for takeoff.

Question 41

AHRS 1 and 2 must

Answer 41

be operational for takeoff.

Question 42

The pilot PFD and MFD must be

Answer 42

operational for takeoff.

Question 43

Autopilot Minimum use heights (AGL):

Answer 43

Engagement after takeoff: 400 ft.
 Cruise: 1000 ft.
 Approach: 79 ft.

Question 44

Generator Load on the ground

Answer 44

85% max