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C-12 U1 V2 > Limits > Flashcards

Limits Flashcards

1
Q

Torque Limitations

Normal Operating Range-

A

20-100

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2
Q

Torque Limitations

Maximum-

A

100

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3
Q 
Torque Limitations
Max Transient (\_\_ secs)-
A

123 for 5 seconds

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4
Q

Torque Limitations

Max w/Prop > 2000 RPM-

A

81

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5
Q

Torque Limitations

Max w/Prop < 1600 RPM-

A

49

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6
Q

Torque Limitations

Max w/Oil Press < 85 PSI-

A

49

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7
Q 
Propeller Tachometer (N2) RPM
Normal Operating Range-
A

1600-2000

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8
Q 
Propeller Tachometer (N2) RPM
Maximum-
A

2000

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9
Q 
Propeller Tachometer (N2) RPM
Max Transient (\_\_ Secs)-
A

2200 for 5 seconds

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10
Q 
Propeller Tachometer (N2) RPM
Max Reverse (\_\_ min)-
A

1900 for 1 minute

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11
Q

Turbine Gas Temperature (TGT) -C

Normal Operating Range-

A

400-800 Celsius

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12
Q

Turbine Gas Temperature (TGT) -C

Takeoff and Max Continuous-

A

800 Celsius

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13
Q

Turbine Gas Temperature (TGT) -C

Normal Climb/ Cruise-

A

770 Celsius

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14
Q 
Turbine Gas Temperature (TGT) -C
Max Reverse (\_\_\_ Minute)-
A

750 for 1 minute

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15
Q 
Turbine Gas Temperature (TGT) -C
Max Start (\_\_\_ Secs)-
A

1000 Celsius 5 seconds

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16
Q

Turbine Gas Temperature (TGT) -C

Max LO Idle-

A

750 Celsius

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17
Q 
Turbine Tachometer (N1) Speed
Takeoff and Max continuous-
A

101.5

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18
Q 
Turbine Tachometer (N1) Speed
Transient (\_\_ Secs)-
A

102.6 for 10 seconds

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19
Q 
Turbine Tachometer (N1) Speed
Max Below -48 Celsius-
A

100.1

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20
Q 
Turbine Tachometer (N1) Speed
LO Idle ( Minimum)
A

56

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21
Q

Oil Pressure PSI

Normal below 21,000 feet-

A

100-135

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22
Q

Oil Pressure PSI

Caution below 21,000 feet

A

85-100

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23
Q

Oil Pressure PSI

Normal Above 21,000 feet

A

85-135

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24
Q 
Oil Pressure PSI
Low Idle (MIN)
A

60

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25
Q

Oil Temperature Celsius

Takeoff and Max Continuous-

A

0 to 99

26
Q

Oil Temperature Celsius

Starting-

A

-40

27
Q

Oil Temperature Celsius

Low Idle-

A

-40 to 99

28
Q

Oil Temperature Celsius

Transient (___ Secs)

A

99 to 104 for 5 seconds

29
Q 
Pneumatic Pressure (PSI)
Normal Operating Range-
A

12-20

30
Q 
Pneumatic Pressure (PSI)
Max-
A

20

31
Q

Starter Limitations-

A

40 seconds on, 60 seconds off
40 seconds on, 60 seconds off
40 seconds on, then 30 minutes off

32
Q 
Airspeed Limitations (KIAS)
(Vmo)-
A

Max Allowable- 260

33
Q 
Airspeed Limitations (KIAS)
(Va)-
A

Max Design Maneuvering- 181

34
Q 
Airspeed Limitations (KIAS)
(Vb)-
A

Turbulence Penetration- 170

35
Q 
Airspeed Limitations (KIAS)
(Vf)-
A

Max (flaps APPCH)- 199

36
Q 
Airspeed Limitations (KIAS)
(Vfe)-
A

Max (flaps FULL)- 157

37
Q 
Airspeed Limitations (KIAS)
(Vmc)-
A

Min Single Engine Control- 86

38
Q 
Airspeed Limitations (KIAS)
(Vyse)-
A

Best rate of climb S/E @ 12,500lbs- 121

39
Q 
Airspeed Limitations (KIAS)
minimum airspeed for sustained icing conditions-
A

140

40
Q 
Airspeed Limitations (KIAS)
maximum airspeed for effective windshield anti-icing -
A

226

41
Q

Propeller Deicer Ammeter

Normal Operating Range from-

A

14-18 Amperes

42
Q

Cabin Altimeter and Differential Pressure

Normal Range to Max-

A

0- 6.1

43
Q

Airplane

Max Ramp weight (LBS)-

A

14,090

44
Q

Airplane

Max Gross Take0ff Weight-

A

14,000

45
Q

Airplane

Max Landing Weight-

A

12,500

46
Q

Airplane

Max Zero Fuel Weight-

A

11,000

47
Q

Brake Deice System shall not be operated, except to test, at ambient temperatures above ____ Celsius.

A

15

48
Q

Maintain___ % N1 of higher during simultaneous operation of the brake deice and surface deice.

A

85

49
Q

Max G loading at 12,500 and below

Wings UP -/+

A

-1.27 to +3.17

50
Q

Max G loading at 12,500 and below

Wings Down -/+

A

-1.27 to +2.0

51
Q

Fuel Limitations

No Takeoff Range:

A

0 to 265 lbs

52
Q

Fuel Limitations

Max Fuel Imbalance:

A

1,000 lbs

53
Q

Fuel Limitations

Max altitude for aircraft operations is ______ feet.

A

31,000 feet

54
Q

The aircraft shall not be operated when the ambient temperatures are warmer than International Standard Atmosphere (ISA) +___ at SL to 25,000 feet or ISA +____ above 25,000 feet PA.

A

37 Celsius and 31 Celsius

55
Q

Ice Vanes shall be extended for operations in ambient temperature of ___ or below when flight free of visible moisture cannot be assured.

A

+5 Celsius

56
Q

Engine ice vanes shall be retracted at ____ and above for flight operations.

A

+15 Celsius

57
Q

Minimum FAT for operation of deicing boots shall be ___ Celsius.

A

-40 Celsius

58
Q

Maximum Crosswind Component is ____ kts at 90 degrees.

A

25 knots

59
Q

The pitot heat is limited to ___ minutes during ground Operations.

A

15 minutes

60
Q

Hydraulic Landing Gear cycles, a complete retraction and extension are limited to :

A

1 every 5 minutes for a total of 6 cycles followed by a 15 minute cool-down period.

61
Q

Icing Limitations-

Typical

A
  1. Unexplained 30 % increase of torque needed to maintain airspeed in level flight
  2. A cumulative 2 or more inches of Ice accumulation on the wing.
  3. Unexplained decrease of 15 KIAS
  4. Unexplained deviation between the pilot and co-pilot airspeed Indicators.
62
Q

Icing Limitations-

Severe

A

Use of autopilot is prohibited if any of the visual cues to typical icing condition exist.

C-12 U1 V2 (2 decks)

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