Limitations

Question 1

Maneuvering Speed (Va)

Answer 1

184 KIAS

Question 2

Maximum Flap Extension/Extended Speed (VFE)

Answer 2

Approach (APP) 202 KIAS
Full Down (DN) 158 KIAS

Question 3

Maximum Landing Gear Operating Speed (VLO)

Answer 3

Extension 184 KIAS

Retraction 166 KIAS

Question 4

Maximum Landing Gear Extended Speed (VLE)

Answer 4

184 KIAS

Question 5

Maximum Operating Speed (VMO)

Answer 5

Sea Level to 21,000 feet 263 KIAS

21,000 to 35,000 feet 263-194 KIAS

Question 6

Stalling Speed (VSO)
Maximum weight, flaps down, idle power

Answer 6

81 KIAS

Question 7

Stalling Speed (VS1)
Maximum weight, flaps approach, idle power

Answer 7

89 KIAS

Question 8

Stalling Speed (VS1)
Maximum weight, flaps up, idle power

Answer 8

96 KIAS

Question 9

Blue Line

One-Engine-Inoperative Best Rate-of-Climb Speed

Answer 9

125 KIAS

Question 10

Maximum ITT °C

Starting _______

Answer 10

Starting 1000 °C

Question 11

Maximum ITT °C

Idle _______

Answer 11

Idle 750 °C

Question 12

Maximum ITT °C

Takeoff _______

Answer 12

Takeoff 820 °C

Question 13

Maximum ITT °C

Max Cruise _______

Answer 13

Max Cruise 820 °C

Question 14

Maximum ITT °C

Max Reverse _______

Answer 14

Max Reverse 760 °C

Question 15

Gas Generator RPM % N1

Takeoff _______

Answer 15

Takeoff 104%

Question 16

Gas Generator RPM % N1

Max Cruise _______

Answer 16

Max Cruise 104%

Question 17

Oil Temperature Limits

Minimum _______
Maximum _______
Limited to a max of 10 mins _______

Answer 17

Minimum -40°C
Maximum +110°C
Limited to a max of 10 mins between 99°C and 110°C

Question 18

External Power Limits
Set to ____ - ____ volts
Minimum of ____ momentarily
And ____ continuously

Answer 18

Set to 28.0 – 28.4 volts
Minimum of 1000 amps momentarily
And 300 amps continuously

Question 19

Maximum sustained generator load is limited as follows:
In flight:
Sea level to 34,000 feet _______
Above 34,000 feet _______

Answer 19

In flight:
Sea level to 34,000 feet 100%
Above 34,000 feet 95%

Question 20

Maximum sustained generator load is limited as follows:
Ground operation:
N1 62% to 70% _______
N1 70% to 100% _______

Answer 20

Ground operation:
N1 62% to 70% 75%
N1 70% to 100% 100%

Question 21

Starter Limits

Answer 21

30 seconds On, 5 minutes Off,
30 seconds On, 5 minutes Off,
30 seconds On, 30 minutes Off,

Question 22

Starter limits
ITT _______
Oil Pressure _______
Oil Temperature _______

Answer 22

ITT 1000 °C (5 sec)
Oil Pressure 0 to 200 psi
Oil Temperature -40 °C (min)

Question 23

What are the three limitations on the use of aviation gasoline?

Answer 23

1. Operation is limited to 150 hours between engine overhauls.
   2 .Operation is prohibited if either standby fuel pump is inoperative.
2. Cross feed capability is required for flight above 20,000 feet pressure altitude (FL200)

Question 24

Usable fuel (Gallons x 6.7 = pounds)

Total quantity _______ (gallons)
_______ (pounds)

Answer 24

Total quantity 539 (gallons)

3611 (pounds)

Question 25

Usable fuel (Gallons x 6.7 = pounds) Each main tank fuel system _______ (gallons) _______ (pounds)

Answer 25

Each main tank fuel system 190 (gallons) | 1273 (pounds)

Question 26

Usable fuel (Gallons x 6.7 = pounds) Each auxiliary fuel tank _______ (gallons) _______ (pounds)

Answer 26

Each auxiliary fuel tank 79.5 (gallons) | 533 (pounds)

Question 27

What is the maximum allowable fuel imbalance between the wing fuel system?

Answer 27

300 pounds

Question 28

Fuel Cross feed Permitted only for what circumstance?

Answer 28

One engine inoperative

Question 29

Do not take off if fuel quantity gauges indicate in yellow arc or indicate less than ____ lbs of fuel in each wing system

Answer 29

265 lbs

Question 30

Operating with the Low Fuel Pressure Annunciators is limited to how many hours?

Answer 30

10 hours

Question 31

Propeller rotational speed limits Minimum idle speed _______

Answer 31

Minimum idle speed 1050 rpm

Question 32

Propeller autofeather Must be operable for ____ and must be armed for ____, ____, ____, and ____.

Answer 32

Must be operable for all flights and must be armed for takeoff, climb, approach and landing.

Question 33

Pneumatic Pressure Gauge Green Arc (Normal Operating Range)

Answer 33

12 to 20 psi

Question 34

Maximum Operating Altitude Limit for Normal Operation

Answer 34

35,000 feet

Question 35

Maximum Operating Altitude with Yaw Damper Inoperative

Answer 35

17,000 feet with Dual Aft Strakes

Question 36

Maximum OAT Limit sea level to 25,000 feet pressure altitude

Answer 36

ISA + 37°C

Question 37

Maximum cabin pressure differential

Answer 37

6.6 psi

Question 38

Rudder boost must be operational for

Answer 38

all flights

Question 39

Landing Gear cycle limits Limited to ____ every ____ for a total of ____, followed by a ____ cool down period

Answer 39

Limited to one every 5 minutes for a total of 6 cycles, followed by a 15 minute cool down period

Question 40

Brake deice (if installed) is not to be operated above

Answer 40

15°C

Question 41

Minimum ambient temperature for operation of deicing boots

Answer 41

-40°C

Question 42

Minimum airspeed for sustained icing flight

Answer 42

140 knots

Question 43

Left and Right Engine Anti-Ice shall be ____ for operation in ambient temperatures of ____ or below when ____________ cannot be assured.

Answer 43

shall be on for operation in ambient temperatures of +5°C or below when flight free of visible moisture cannot be assured.

Question 44

Left and Right Engine Anti-Ice shall be ____ for _____ in ambient temperatures of above ____.

Answer 44

shall be off for takeoff operations in ambient temperatures of above +10°C.

Question 45

Maximum demonstrated crosswind component

Answer 45

20 knots

Question 46

Maximum demonstrated tailwind component

Answer 46

10 knots

Question 47

Autopilot Minimum engage height after takeoff _______ Minimum use height during cruise _______ Minimum use height during approach _______ Minimum use height during steep approach _______

Answer 47

Minimum engage height after takeoff 400 feet AGL Minimum use height during cruise 1000 feet AGL Minimum use height during approach 79 feet AGL Minimum use height during steep approach 160 feet AGL

Question 48

Autopilot What are the maximum coupled intercept angles? Nav and Localizer _______ Back Course _______

Answer 48

Nav and Localizer Less than 90° | Back Course 70°

Question 49

Maximum ramp weight

Answer 49

15,100 lbs

Question 50

Maximum take-off weight

Answer 50

15,000 lbs

Question 51

Maximum landing weight

Answer 51

15,000 lbs

Question 52

Maximum zero-fuel weight

Answer 52

12,500 lbs

Question 53

Maximum weight in baggage compartment

Answer 53

550 lbs

Question 54

Maximum allowable weight on airstair door

Answer 54

1 person