BOLDFACE / OPS LIMITS

Question 1

1. ENGINE FIRE ON THE GROUND

Answer 1

1. CONDITION LEVERS – FUEL CUTOFF
2. FIRE HANDLE – PULL
3. STARTER SWITCH – AS REQUIRED
4. FIRE EXTINGUISHER – AS REQUIRED

Question 2

2. ENGINE FAILURE IMMEDIATELY AFTER TAKEOFF

Answer 2

1. POWER – MAXIMUM
2. GEAR – UP
3. PROPELLER – FEATHER

Question 3

3. CABIN FIRE, SMOKE, OR FUMES ELIMINATION or LOSS OF PRESSURIZATION (ABOVE 13,000 FEET)

Answer 3

1. OXYGEN – 100% AND ON (ALL)

Question 4

Torque Percent:
Takeoff
___ %

Note 3:
These values are limited to ____ minutes.

Answer 4

100%

Note 3:
These values are limited to 5 minutes.

Question 5

Torque Percent:
Emer Cont
___ %

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

Answer 5

100%

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

Question 6

Torque Percent:
Max Cont
___ %

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

Answer 6

100%

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

Question 7

Torque Percent:
Transient
___ %

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

Answer 7

123%

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

Question 8

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

Answer 8

49%

Question 9

Maximum Observed TGT °C
Takeoff
___°C

Note 3:
These values are limited to ____ minutes.

Answer 9

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.

Question 10

Maximum Observed TGT °C
Emer Cont
___°C

Answer 10

750 °C

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

Question 11

Maximum Observed TGT °C
Max Cont
___°C

Answer 11

725 °C

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

Question 12

Maximum Observed TGT °C
Low Idle
___ °C

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

Answer 12

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.

Question 13

Maximum Observed TGT °C
Starting
___°C

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

Answer 13

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.

Question 14

Maximum Observed TGT °C
Transient
___°C

Answer 14

850 °C

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

Question 15

Maximum Observed TGT °C
Max Reverse
___°C

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

Answer 15

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.

Question 16

Gas Generator RPM N1 %
Takeoff
___ %

Note 3:
These values are limited to ____ minutes.

Answer 16

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%.

Question 17

Gas Generator RPM N1 %
Emer Cont
___ %

Answer 17

101.5%

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

Question 18

Gas Generator RPM N1 %
Max Cont
___ %

Answer 18

101.5%

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

Question 19

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

Answer 19

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%.

Question 20

Gas Generator RPM N1 %
Low Idle
___ %

Answer 20

60% (min)

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

Question 21

Gas Generator RPM N1 %
Transient
___ %

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

Answer 21

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%.

Question 22

Gas Generator RPM N1 %
Max Reverse
___ %

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

Answer 22

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%.

Question 23

Prop RPM N2
Takeoff
___ RPM

Note 3:
These values are limited to ____ minutes.

Answer 23

2000 RPM

Note 3:
These values are limited to 5 minutes.

Question 24

Prop RPM N2
Emer Cont
___ RPM

Answer 24

2000 RPM

Question 25

Prop RPM N2 Max Cont ___ RPM

Answer 25

2000 RPM

Question 26

Prop RPM N2 Low Idle ___ RPM Note 13: Operation between ____ and ____ propeller RPM is permissible only with prop feathered.

Answer 26

1150 RPM (min) Note 13: Operation between 0 and 450 propeller RPM is permissible only with prop feathered.

Question 27

Prop RPM N2 Transient ___ RPM Note 7: These values are time limited to ____ seconds.

Answer 27

2200 RPM Note 7: These values are time limited to 5 seconds.

Question 28

Prop RPM N2 Max Reverse ____ RPM Note 9: This operation is time limited to ____ minute.

Answer 28

1900 RPM Note 9: This operation is time limited to 1 minute.

Question 29

Oil Press PSI Takeoff ___ PSI Note 2: Note 3: These values are limited to ____ minutes.

Answer 29

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.

Question 30

Oil Press PSI Emer Cont ___ PSI Note 2:

Answer 30

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.

Question 31

Oil Press PSI Max Cont ___ PSI Note 2:

Answer 31

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.

Question 32

Oil Press PSI Low Idle ___ PSI Note 2:

Answer 32

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.

Question 33

Oil Press PSI Max Reverse ___ PSI Note 2: Note 9: This operation is time limited to ____ minute.

Answer 33

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.

Question 34

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.

Answer 34

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.

Question 35

Oil Temp °C Takeoff ___°C Note 3: These values are limited to ____ minutes.

Answer 35

10 to 99 °C Note 3: These values are limited to 5 minutes.

Question 36

Oil Temp °C Emer Cont ___°C

Answer 36

10 to 99 °C

Question 37

Oil Temp °C Max Cont ___°C

Answer 37

10 to 99 °C

Question 38

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.

Answer 38

-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.

Question 39

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.

Answer 39

-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.

Question 40

Oil Temp °C Starting ___°C

Answer 40

-40 (min) °C

Question 41

Oil Temp °C Transient ___°C Note 3: These values are limited to ____ minutes.

Answer 41

100 to 104 °C Note 3: These values are limited to 5 minutes.

Question 42

Oil Temp °C Max Reverse ___°C Note 9: This operation is time limited to ____ minute.

Answer 42

0 to 99 °C Note 9: This operation is time limited to 1 minute.

Question 43

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

Answer 43

VMO/MMO: 259 KIAS ( .52 Mach)

Question 44

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

Answer 44

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

Question 45

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

Answer 45

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

Question 46

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

Answer 46

VSSE [12,500#]: 117 KIAS

Question 47

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

Answer 47

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

Question 48

Airspeeds: VRA [turbulent air penetration]: ___ KIAS

Answer 48

VRA [turbulent air penetration]: 170 KIAS

Question 49

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

Answer 49

VLE [gear extension or extended]: 181 KIAS

Question 50

Airspeeds: VLO [gear retract]: ___ KIAS

Answer 50

VLO [gear retract]: 163 KIAS

Question 51

Airspeeds: VFE40 [flap extend]: ___ KIAS

Answer 51

VFE40 [flap extend]: 200 KIAS

Question 52

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

Answer 52

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

Question 53

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

Answer 53

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

Question 54

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

Answer 54

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

Question 55

Weights: Max normal ramp: _____ LBS

Answer 55

12,590 lbs

Question 56

Weights: Max normal T/O: _____ LBS

Answer 56

Max normal T/O: 12,500 LBS

Question 57

Weights: Max zero fuel: _____ LBS

Answer 57

Max zero fuel: 10,400 LBS

Question 58

Weights: Max restricted T/O: _____ LBS

Answer 58

Max restricted T/O: 14,000 LBS

Question 59

Weights: Max restricted zero fuel: _____ LBS

Answer 59

Max restricted zero fuel: 11,000 LBS