Power Plant Limitations Flashcards

1
Q

ITT in Start

A

816C

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2
Q

ITT in G.I. (Feather)

A

805c

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3
Q

ITT in G.I. (Run)

A

805c

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4
Q

ITT and Time for Normal Takeoff

A

816C 5 Min (also applies to FLEX)

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5
Q

ITT and Time for Max Takeoff

A

852C 5 Min (also applies to FLEX)

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6
Q

ITT Max Continuous (OEI)

A

832C

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7
Q

Power (PU) Limited to ___PU when oil temp is below____

A

30 PU below 45C

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8
Q

Max Power Units Normal Takeoff

A

100 PU for 5 Min (also applies to FLEX) consult AFM 5.2 for engine bleeds and anti-ice.

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9
Q

Max Power Units Max Takeoff

A

111 PU for 5 Min (also applies to FLEX)

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10
Q

Max Continuous Power Units (OEI)

A

100 PU

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11
Q

Max Engine RPM % in GI (Feather)

A

72%

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12
Q

Max Engine RPM % in GI (Run)

A

72%

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13
Q

Max Engine RPM % in Normal Takeoff

A

100% (also applies to FLEX)

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14
Q

Max Engine RPM % in Max Takeoff

A

100% (also applies to FLEX)

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15
Q

Max Continuous Engine RPM% (OEI)

A

100%

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16
Q

Max Prop RPM in GI (RUN)

A

770 RPM

17
Q

Max Prop RPM Normal Takeoff

A

1100 RPM (also applies to FLEX)

18
Q

Max Prop RPM Maximum Takeoff

A

1100 RPM (also applies to FLEX)

19
Q

Max Prop RPM MAX CONTINUOUS (OEI)

A

1100 RPM

20
Q

Engine Oil Pressure Range GI (Feather)

A

35-100 PSI

21
Q

Engine Oil Pressure Range GI (RUN)

A

35-100 PSI

22
Q

Engine Oil Pressure Range Normal Takeoff

A

40-90 PSI

23
Q

Engine Oil Pressure Range Max Takeoff

A

40-90 PSI

24
Q

Engine Oil Pressure Range Max Continuous

A

40-90 PSI

25
Q

Propeller Oil Pressure Range GI (Feather)

A

15-210 PSI

26
Q

Propeller Oil Pressure Range GI (RUN)

A

110-210 PSI

27
Q

Propeller Oil Pressure Range Normal Takeoff

A

170-210 PSI

28
Q

Propeller Oil Pressure Range Max Takeoff

A

170-210 PSI

29
Q

Propeller Oil Pressure Range Max Continuous

A

170-210 PSI

30
Q

Oil Temp Range all Conditions (GI Feather/Run, Normal Takeoff, Max Takeoff, Max Continuous)

A

45-88C up to 93C for FIVE MIN

31
Q

Oil Pressure can increase to ___PSI for a max of ___ Min ___Sec when performing initial start and warmup.

A

250 PSI for 2 MIN 30 SEC when preforming initial start and warmup.

32
Q

Engine Start Attempts Limit

A

5 attempts in succession, engine must be allowed to stop completely between attempts, then rest for 60 seconds before the next attempt.

33
Q

After reaching the max engine start attempt of __ the engine must be allowed to cool for ____ MIN

A

After reaching the max engine start attempts of 5 the engine must be allowed to cool for 20 minuets, then the entire start sequence (up to 5 attempts with 60 seconds in between) may be repeated.

34
Q

The engine shall be motored for _____ sec after a failed start with no light off

A

45 seconds after a failed start with no light off

35
Q

What start must be aborted manually?

A

Hung

36
Q

The start switch must not be reactivated under what conditions (in air and on the ground)

A

NG above 0% on the ground or 29% in flight.

37
Q

Max ITT for start is _______ if operational or safety considerations require an engine to be started immediately in flight…

A

210C, consult the INFLIGHT ENGINE START ENVELOPE

38
Q

If starting the engine with a ground air starting source (Huffer Cart) the unit must be able to provide____ PSIA in all ambient conditions and ____flow.

A

30 PSIA in all ambient conditions
Flow requirements vary with temp and the appropriate
chart must be consulted.