SY105 Flashcards

(32 cards)

1
Q

Engine operating limits: TO/MAX

Torque, ITT, N1, Np, Oil Pressure, Oil Temperature

A

100%; 820; 104 Max; 100 Max; 90 to 120; 10 to 105

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2
Q

Engine operating limits: IDLE

Torque, ITT, N1, Np, Oil Pressure, Oil Temperature

A

3-8%; 750; 60 to 61 (ground), 67 min (flight); 46 to 50 (ground); 90 min; -40 to 105 (ground), 10 to 105 (flight), 106 to 110 (up to 10 minutes)

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3
Q

Engine operating limits: START

Torque, ITT, N1, Np, Oil Pressure, Oil Temperature

A

N/A, 1000 for 5 sec; N/A; N/A; 200 max; -40 min

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4
Q

Engine operating limits: TRANSIENT

Torque, ITT, N1, Np, Oil Pressure, Oil Temperature

A

131 max (20 sec); 870 (20 sec); 104; 102 (20 sec); 40 to 130; 106 to 110 (10 min)

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5
Q

Propeller Interface Unit receives power from

A

PMU

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6
Q

What does the PIU do?

A

regulates oil pressure to pitch change mechansim

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7
Q

What are the indications of a high start?

A

High/rapidly rising ITT and lower N1

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8
Q

What are your primary and secondary indications of a windmilling engine?

A

Primary: N1
Secondary: Oil pressure

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9
Q

When is an airstart warranted?

A

Three conditions: NO FIRE, FOD, or Frozen

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10
Q

What are initial indications of engine failure?

A

Loss of power and airspeed
Rapid decay in N1, torque, and ITT
Propeller movement toward feather due to loss of oil pressure

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11
Q

FEVER check for Fire in Flight

A
Fluctuating oil pressure, oil temperature, or hydraulic pressure
Excessive turbine temperature
Visual Indications (smoke or flames)
Erratic engine operation
Roughness or Vibration
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12
Q

What is the minimum recommended altitude for airstart procedures?

A

2,000 ft AGL

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13
Q

What are some possible causes of engine failure in-flight?

A

Fuel Starvation
Mechanical Failure
Compressor Stall

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14
Q

What are some possible causes of uncommanded feather?

A

Feather dump solenoid malfunction

Loss of oil pressure to propeller pitch control mechanism

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15
Q

Possible causes of high start

A

PMU failure
FMU failure
Incorrect air/fuel mixture
Low battery

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16
Q

Possible indications of hung start

A

Slow rising ITT
Lower N1
Lower NP

17
Q

Possible causes of hung start

A
PMU failure 
FMU failure 
Incorrect air/fuel mixture 
Ignition system failure 
Starter failure 
Low battery
18
Q

Possible indications of no start

A

No ITT indication
Lower N1
No NP indication
No torque indication

19
Q

Possible causes of no start

A
PMU failure 
FMU failure 
Starter failure 
Ignition system failure 
Incorrect air/fuel mixture
20
Q

Initial Indications of Engine Failure

A

Loss of power and airspeed
Rapid decay of N1, torque, and ITT
MASTER WARN lights and tone
Propeller moves toward feather

21
Q

Accompanying Indications of Engine Failure

A

Rapidly decreasing ITT, NP
Lower-than-normal oil pressure
Engine noise
GEN, FUEL PX, OIL PX, OBOGS FAIL annunciators
Possibly PMU FAIL and CKPT ALT annunciators

22
Q

Possible Causes of Engine Failure

A

Fuel Starvation
Mechanical Failure
Compressor Stall

23
Q

Possible Indications of PMU failure

A

Power step change
PMU FAIL and PMU STATUS annunciators
MASTER WARN light
Aural tone

24
Q

Possible Causes of PMU failure

A

System failure System malfunction

25
Possible Indications of Uncommanded Power Changes/Loss of Power
Reduction in power/thrust Lower than expected fuel flow Uncommanded decrease in N1 High raw ITT (RITT) on AEDD With oil/engine/fuel system contamination, additionally: Power surges Uncontrollable high power
26
Possible Causes of Uncommanded Power Changes/Loss of Power
Engine rollback due to PMU scheduling Oil/engine/fuel system contamination
27
Possible Indications of Uncommanded Feather
``` Rapid loss of power High torque Lower NP Possible PMU FAIL/PMU STATUS annunciators Engine vibration Engine noise ```
28
Possible Causes of Uncommded Feather
Feather dump solenoid malfunction | Loss of oil pressure to propeller pitch control mechanism
29
Possible Indications of Prop Sleeve Touchdown
``` NP fluctuations Increasing torque Decreasing thrust Engine vibrations Possible CHIP detector warning light ```
30
Possible Causes of Prop Sleeve Touchdown
Loss of oil pressure to propeller pitch control mechanism from momentary contact between oil transfer sleeve and propeller shaft
31
Possible Indications of Engine Fire in Flight
FIRE annunciator MASTER WARN light Aural tone ``` Fluctuating oil pressure, oil temperature, or hydraulic pressure Excessive turbine temperature Visual indications (smoke or flames) Erratic engine operation Roughness or vibration ```
32
Possible Causes of Engine Fire in Flight
Fuel or oil leaks | Fire getting outside the engine