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BOLDFACE / OPS LIMITS Flashcards

1
Q
  1. ENGINE FIRE ON THE GROUND
A
  1. CONDITION LEVERS – FUEL CUTOFF
  2. FIRE HANDLE – PULL
  3. STARTER SWITCH – AS REQUIRED
  4. FIRE EXTINGUISHER – AS REQUIRED
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2
Q
  1. ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF
A
  1. POWER – MAXIMUM
  2. GEAR – UP
  3. PROPELLER – FEATHER
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3
Q
  1. CABIN FIRE, SMOKE, OR FUMES ELIMINATION or LOSS OF PRESSURIZATION (ABOVE 13,000 FEET)
A
  1. OXYGEN – 100% AND ON (ALL)
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4
Q

Torque Percent:
Takeoff
___ %

Note 3:
These values are limited to ____ minutes.

A

100%

Note 3:
These values are limited to 5 minutes.

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5
Q

Torque Percent:
Emer Cont
___ %

Note 4:
Cruise torque values vary with altitude and temperature.

A

100%

Note 4:
Cruise torque values vary with altitude and temperature.

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6
Q

Torque Percent:
Max Cont
___ %

Note 4:
Cruise torque values vary with altitude and temperature.

A

100%

Note 4:
Cruise torque values vary with altitude and temperature.

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7
Q

Torque Percent:
Transient
___ %

Note 7:
These values are time limited to ____ seconds.

A

123%

Note 7:
These values are time limited to 5 seconds.

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8
Q

Note 1. Torque limit applies within range of 1600-2000 prop RPM (N2). Below 1600 RPM, torque is limited to _____%.

A

49%

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9
Q

Maximum Observed TGT °C
Takeoff
___°C

Note 3:
These values are limited to ____ minutes.

A

750 °C

Note 3:
These values are limited to 5 minutes.

Note 11:
For TGT in excess of 750°C, refer to Engine Over Temperature Limits chart.

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10
Q

Maximum Observed TGT °C
Emer Cont
___°C

A

750 °C

Note 11:
For TGT in excess of 750°C, refer to Engine Over Temperature Limits chart.

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11
Q

Maximum Observed TGT °C
Max Cont
___°C

A

725 °C

Note 11:
For TGT in excess of 750°C, refer to Engine Over Temperature Limits chart.

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12
Q

Maximum Observed TGT °C
Low Idle
___ °C

Note 6:
High TGT at ground idle may be corrected by reducing ______ and/or increasing ____.

A

660 °C

Note 6:
High TGT at ground idle may be corrected by reducing “LOAD” and/or increasing “N1”.

Note 11:
For TGT in excess of 750°C, refer to Engine Over Temperature Limits chart.

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13
Q

Maximum Observed TGT °C
Starting
___°C

Note 7:
These values are time limited to ____ seconds.

A

1000 °C

Note 7:
These values are time limited to 5 seconds.

Note 11:
For TGT in excess of 750°C, refer to Engine Over Temperature Limits chart.

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14
Q

Maximum Observed TGT °C
Transient
___°C

A

850 °C

Note 11:
For TGT in excess of 750°C, refer to Engine Over Temperature Limits chart.

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15
Q

Maximum Observed TGT °C
Max Reverse
___°C

Note 9:
This operation is time limited to ____ minute.

A

750 °C

Note 9:
This operation is time limited to 1 minute.

Note 11:
For TGT in excess of 750°C, refer to Engine Over Temperature Limits chart.

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16
Q

Gas Generator RPM N1 %
Takeoff
___ %

Note 3:
These values are limited to ____ minutes.

A

101.5%

Note 3:
These values are limited to 5 minutes.

Note 10:
For every 5.6°C below -48°C ambient temperature, reduce maximum allowable N1 by 1.6%.

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17
Q

Gas Generator RPM N1 %
Emer Cont
___ %

A

101.5%

Note 10:
For every 5.6°C below -48°C ambient temperature, reduce maximum allowable N1 by 1.6%.

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18
Q

Gas Generator RPM N1 %
Max Cont
___ %

A

101.5%

Note 10:
For every 5.6°C below -48°C ambient temperature, reduce maximum allowable N1 by 1.6%.

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19
Q

Gas Generator RPM N1 %
High Idle
Note 5:
At approximately ___% N1.

A

Note 5:
At approximately 70% N1.

Note 10:
For every 5.6°C below -48°C ambient temperature, reduce maximum allowable N1 by 1.6%.

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20
Q

Gas Generator RPM N1 %
Low Idle
___ %

A

60% (min)

Note 10:
For every 5.6°C below -48°C ambient temperature, reduce maximum allowable N1 by 1.6%.

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21
Q

Gas Generator RPM N1 %
Transient
___ %

Note 8:
These values are time limited to ____ seconds.

A

102.6%

Note 8:
These values are time limited to 10 seconds.

Note 10:
For every 5.6°C below -48°C ambient temperature, reduce maximum allowable N1 by 1.6%.

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22
Q

Gas Generator RPM N1 %
Max Reverse
___ %

Note 9:
This operation is time limited to ____ minute.

A

88%

Note 9:
This operation is time limited to 1 minute.

Note 10:
For every 5.6°C below -48°C ambient temperature, reduce maximum allowable N1 by 1.6%.

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23
Q

Prop RPM N2
Takeoff
___ RPM

Note 3:
These values are limited to ____ minutes.

A

2000 RPM

Note 3:
These values are limited to 5 minutes.

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24
Q

Prop RPM N2
Emer Cont
___ RPM

25
Q

Prop RPM N2
Max Cont
___ RPM

26
Q

Prop RPM N2
Low Idle
___ RPM

Note 13:
Operation between ____ and ____ propeller RPM is permissible only with prop feathered.

A

1150 RPM (min)

Note 13:
Operation between 0 and 450 propeller RPM is permissible only with prop feathered.

27
Q

Prop RPM N2
Transient
___ RPM

Note 7:
These values are time limited to ____ seconds.

A

2200 RPM

Note 7:
These values are time limited to 5 seconds.

28
Q

Prop RPM N2
Max Reverse
____ RPM

Note 9:
This operation is time limited to ____ minute.

A

1900 RPM

Note 9:
This operation is time limited to 1 minute.

29
Q

Oil Press PSI
Takeoff
___ PSI

Note 2:

Note 3:
These values are limited to ____ minutes.

A

105 to 135 PSI

Note 2:
The minimum oil pressure above 21,000 feet is 85 PSIG. +/- 10 PSIG fluctuations are acceptable. Oil pressure between 60 and 85 PSIG should be tolerated only for the completion of the flight at power settings not to exceed 49% torque. Oil pressure below 60 PSIG are unsafe and require that either the engine be shut down or a landing be made as soon as possible, using the minimum power required to sustain flight.

Note 3:
These values are limited to 5 minutes.

30
Q

Oil Press PSI
Emer Cont
___ PSI

Note 2:

A

105 to 135

Note 2:
The minimum oil pressure above 21,000 feet is 85 PSIG. +/- 10 PSIG fluctuations are acceptable. Oil pressure between 60 and 85 PSIG should be tolerated only for the completion of the flight at power settings not to exceed 49% torque. Oil pressure below 60 PSIG are unsafe and require that either the engine be shut down or a landing be made as soon as possible, using the minimum power required to sustain flight.

31
Q

Oil Press PSI
Max Cont
___ PSI

Note 2:

A

105 to 135

Note 2:
The minimum oil pressure above 21,000 feet is 85 PSIG. +/- 10 PSIG fluctuations are acceptable. Oil pressure between 60 and 85 PSIG should be tolerated only for the completion of the flight at power settings not to exceed 49% torque. Oil pressure below 60 PSIG are unsafe and require that either the engine be shut down or a landing be made as soon as possible, using the minimum power required to sustain flight.

32
Q

Oil Press PSI
Low Idle
___ PSI

Note 2:

A

105 to 135

Note 2:
The minimum oil pressure above 21,000 feet is 85 PSIG. +/- 10 PSIG fluctuations are acceptable. Oil pressure between 60 and 85 PSIG should be tolerated only for the completion of the flight at power settings not to exceed 49% torque. Oil pressure below 60 PSIG are unsafe and require that either the engine be shut down or a landing be made as soon as possible, using the minimum power required to sustain flight.

33
Q

Oil Press PSI
Max Reverse
___ PSI

Note 2:

Note 9:
This operation is time limited to ____ minute.

A

105 to 135

Note 2:
The minimum oil pressure above 21,000 feet is 85 PSIG. +/- 10 PSIG fluctuations are acceptable. Oil pressure between 60 and 85 PSIG should be tolerated only for the completion of the flight at power settings not to exceed 49% torque. Oil pressure below 60 PSIG are unsafe and require that either the engine be shut down or a landing be made as soon as possible, using the minimum power required to sustain flight.

Note 9:
This operation is time limited to 1 minute.

34
Q

Note 2:
The minimum oil pressure above 21,000 feet is ____ PSIG. +/- ____ PSIG fluctuations are acceptable. Oil pressure between ____ and ____ PSIG should be tolerated only for the completion of the flight at power settings not to exceed ____% torque. Oil pressure below ____ PSIG are unsafe and require that either the engine be shut down or a landing be made as soon as possible, using the minimum power required to sustain flight.

A

Note 2:
The minimum oil pressure above 21,000 feet is 85 PSIG. +/- 10 PSIG fluctuations are acceptable. Oil pressure between 60 and 85 PSIG should be tolerated only for the completion of the flight at power settings not to exceed 49% torque. Oil pressure below 60 PSIG are unsafe and require that either the engine be shut down or a landing be made as soon as possible, using the minimum power required to sustain flight.

35
Q

Oil Temp °C
Takeoff
___°C

Note 3:
These values are limited to ____ minutes.

A

10 to 99 °C

Note 3:
These values are limited to 5 minutes.

36
Q

Oil Temp °C
Emer Cont
___°C

A

10 to 99 °C

37
Q

Oil Temp °C
Max Cont
___°C

A

10 to 99 °C

38
Q

Oil Temp °C
High Idle
___°C

Note 12:
On the ground, increases in oil temp can be countered by placing the CONDITION lever in _______ and/or by turning the nose into the wind.

A

-40 to 99 °C

Note 12:
On the ground, increases in oil temp can be countered by placing the CONDITION lever in “LOW IDLE” and/or by turning the nose into the wind.

39
Q

Oil Temp °C
Low Idle
___°C

Note 12:
On the ground, increases in oil temp can be countered by placing the CONDITION lever in _______ and/or by turning the nose into the wind.

A

-40 to 99 °C

Note 12:
On the ground, increases in oil temp can be countered by placing the CONDITION lever in “LOW IDLE” and/or by turning the nose into the wind.

40
Q

Oil Temp °C
Starting
___°C

A

-40 (min) °C

41
Q

Oil Temp °C
Transient
___°C

Note 3:
These values are limited to ____ minutes.

A

100 to 104 °C

Note 3:
These values are limited to 5 minutes.

42
Q

Oil Temp °C
Max Reverse
___°C

Note 9:
This operation is time limited to ____ minute.

A

0 to 99 °C

Note 9:
This operation is time limited to 1 minute.

43
Q

Airspeeds:
VMO/MMO: ____ KIAS (___ Mach)

A

VMO/MMO: 259 KIAS ( .52 Mach)

44
Q

Airspeeds:
VMCA [12,500#, 0 Flap]: ___ KIAS

A

VMCA [12,500#, 0 Flap]: 91 KIAS

45
Q

Airspeeds:
VYSE [clean/12,500#]: ___ KIAS

A

VYSE [clean/12,500#]: 121 KIAS

46
Q

Airspeeds:
VSSE [12,500#]: ___ KIAS

A

VSSE [12,500#]: 117 KIAS

47
Q

Airspeeds:
VX [clean/12,500#]: ___ KIAS

A

VX [clean/12,500#]: 100 KIAS

48
Q

Airspeeds:
VRA [turbulent air penetration]: ___ KIAS

A

VRA [turbulent air penetration]: 170 KIAS

49
Q

Airspeeds:
VLE [gear extension or extended]: ___ KIAS

A

VLE [gear extension or extended]: 181 KIAS

50
Q

Airspeeds:
VLO [gear retract]: ___ KIAS

A

VLO [gear retract]: 163 KIAS

51
Q

Airspeeds:
VFE40 [flap extend]: ___ KIAS

A

VFE40 [flap extend]: 200 KIAS

52
Q

Airspeeds:
VFE100 [flap extend]: ___ [C], ___ [D] KIAS

A

VFE100 [flap extend]: 146 [C], 157 [D] KIAS

53
Q

Structural:
Max sink rate at touchdown (<12,500): ___ FPM

A

Max sink rate at touchdown (<12,500): 600 FPM

54
Q

Structural:
Max sink rate at touchdown (<14,000): ___ FPM

A

Max sink rate at touchdown (<14,000): 500 FPM

55
Q

Weights:
Max normal ramp: _____ LBS

A

12,590 lbs

56
Q

Weights:
Max normal T/O: _____ LBS

A

Max normal T/O: 12,500 LBS

57
Q

Weights:
Max zero fuel: _____ LBS

A

Max zero fuel: 10,400 LBS

58
Q

Weights:
Max restricted T/O: _____ LBS

A

Max restricted T/O: 14,000 LBS

59
Q

Weights:
Max restricted zero fuel: _____ LBS

A

Max restricted zero fuel: 11,000 LBS

C-12C (4 decks)

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