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BE300 Study Guide > Limitations > Flashcards

Limitations Flashcards

1
Q

Maneuvering Speed (Va)

A

184 KIAS

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2
Q

Maximum Flap Extension/Extended Speed (VFE)

A 
Approach (APP) 202 KIAS
Full Down (DN) 158 KIAS
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3
Q

Maximum Landing Gear Operating Speed (VLO)

A

Extension 184 KIAS

Retraction 166 KIAS

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4
Q

Maximum Landing Gear Extended Speed (VLE)

A

184 KIAS

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5
Q

Maximum Operating Speed (VMO)

A

Sea Level to 21,000 feet 263 KIAS

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

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6
Q 
Stalling Speed (VSO)
Maximum weight, flaps down, idle power
A

81 KIAS

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7
Q 
Stalling Speed (VS1)
Maximum weight, flaps approach, idle power
A

89 KIAS

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8
Q 
Stalling Speed (VS1)
Maximum weight, flaps up, idle power
A

96 KIAS

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9
Q

Blue Line

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

A

125 KIAS

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10
Q

Maximum ITT °C

Starting _______

A

Starting 1000 °C

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11
Q

Maximum ITT °C

Idle _______

A

Idle 750 °C

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12
Q

Maximum ITT °C

Takeoff _______

A

Takeoff 820 °C

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13
Q

Maximum ITT °C

Max Cruise _______

A

Max Cruise 820 °C

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14
Q

Maximum ITT °C

Max Reverse _______

A

Max Reverse 760 °C

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15
Q

Gas Generator RPM % N1

Takeoff _______

A

Takeoff 104%

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16
Q

Gas Generator RPM % N1

Max Cruise _______

A

Max Cruise 104%

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17
Q

Oil Temperature Limits

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

A

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

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18
Q

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

A

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

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19
Q

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

A

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

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20
Q

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

A

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

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21
Q

Starter Limits

A

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

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22
Q

Starter limits
ITT _______
Oil Pressure _______
Oil Temperature _______

A

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

23
Q

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

A
  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)
24
Q

Usable fuel (Gallons x 6.7 = pounds)

Total quantity _______ (gallons)
_______ (pounds)

A

Total quantity 539 (gallons)

3611 (pounds)

25
Q

Usable fuel (Gallons x 6.7 = pounds)

Each main tank fuel system _______ (gallons)
_______ (pounds)

A

Each main tank fuel system 190 (gallons)

1273 (pounds)

26
Q

Usable fuel (Gallons x 6.7 = pounds)

Each auxiliary fuel tank _______ (gallons)
_______ (pounds)

A

Each auxiliary fuel tank 79.5 (gallons)

533 (pounds)

27
Q

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

A

300 pounds

28
Q

Fuel Cross feed

Permitted only for what circumstance?

A

One engine inoperative

29
Q

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

A

265 lbs

30
Q

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

A

10 hours

31
Q

Propeller rotational speed limits

Minimum idle speed _______

A

Minimum idle speed 1050 rpm

32
Q

Propeller autofeather

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

A

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

33
Q

Pneumatic Pressure Gauge

Green Arc (Normal Operating Range)

A

12 to 20 psi

34
Q

Maximum Operating Altitude Limit for Normal Operation

A

35,000 feet

35
Q

Maximum Operating Altitude with Yaw Damper Inoperative

A

17,000 feet with Dual Aft Strakes

36
Q

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

A

ISA + 37°C

37
Q

Maximum cabin pressure differential

A

6.6 psi

38
Q

Rudder boost must be operational for

A

all flights

39
Q

Landing Gear cycle limits

Limited to ____ every ____ for a total of ____, followed by a ____ cool down period

A

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

40
Q

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

A

15°C

41
Q

Minimum ambient temperature for operation of deicing boots

A

-40°C

42
Q

Minimum airspeed for sustained icing flight

A

140 knots

43
Q

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

A

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

44
Q

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

A

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

45
Q

Maximum demonstrated crosswind component

A

20 knots

46
Q

Maximum demonstrated tailwind component

A

10 knots

47
Q

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

A

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

48
Q

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

A

Nav and Localizer Less than 90°

Back Course 70°

49
Q

Maximum ramp weight

A

15,100 lbs

50
Q

Maximum take-off weight

A

15,000 lbs

51
Q

Maximum landing weight

A

15,000 lbs

52
Q

Maximum zero-fuel weight

A

12,500 lbs

53
Q

Maximum weight in baggage compartment

A

550 lbs

54
Q

Maximum allowable weight on airstair door

A

1 person

BE300 Study Guide (3 decks)

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