Fam 2 Flashcards

1
Q

Np, Nr, torque oddities

A

If you see any fluctuations in Np, Nr, or torque treat it with EMIF

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2
Q

Single engine conditions establish

A

Level wings, check airspeed (accel or deccel to bucket speed ~ 70 kias)

Check IVISI…. can you maintain level flight???

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3
Q

What causes a compressor stall?

A

Aerodynamic disturbance of smooth airflow pattern through the engine

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4
Q

Compressor stall indications

A

Spiking TGT, hang-up or drop in Ng, loss of power, noises (like banging)

**inverse relationship between TGT and Torque (high high TGT because air is not flowing through for cooling or to produce engine power to produce torque)

**Inverse relationship between TGT and Ng (high temp because no air to cool and low Ng because no air to turn turbines)

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5
Q

Compressor stall

A
  1. Emif - perform
  2. Pcl (malfunctioning engine) - idle

Note: if the Ng decay re-light feature attempts to relight the engine, subsequent compressor stalls may occur and damage to the engine. A yaw kick may be experienced each time the engine relights. The engine must be manually shutdown

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6
Q

Spiking/fluctuations (torque or TGT) can be the result of

A

Engine electronic circuitry or component failures

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7
Q

Spiking is

A

Instantaneous increase of an engine instrument

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8
Q

Fluctuations may be indicative

A

Of contaminated fuel

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9
Q

What may be an indication before power loss

A

Audible power surges with engine q/tgt spiking/fluctuations

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10
Q

Indications of an impending high-speed shaft failure include

A

Medium to high frequency vibrations

Or a “howl” accompanying thr vibration

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11
Q

LDS malfunction

A

Connection to HMU

Check during first takeoff: malfunction if torque are split

In stable hover: malfunction if torque are matched

Also in start up checklist

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12
Q

LDS malfunction warning

A

During low power or autorotative descents with an engine LDS malfunction, Np/Nr may rise rapidly and activate Np overspend protection (120%)

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13
Q

Engine air restart may be attempted any time after shutdown if

A

No indication of mechanical malfunction or engine fire potential

Meaning if engine failure accompanied by an explosion or unusual noise indicates damage to the engine. There is a possibility that any attempt to restart the engine may result in a fire. Under such circumstances, do not try to restart the engine unless it is needed to maintain level fligjt

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14
Q

How much altitude is required approximately for a dual engine restart

A

Approximately 5000 ft

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15
Q

In the event of an alternator failure, (engine air restart note)

A

The Ng signal may be unavailable (because the sensor is mounted on the alternator).

Engine start will not be possible without AC power to provide power to ignition exciter

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16
Q

Oil filter bypass caution

A

Non memory

Consideration may be given to restarting the engine if required for landing

17
Q

Engine chip or engine oil px low

A

Non memory

18
Q

Engine oil px low can be triggered by:

A
  • Ng greater than 70% AND engine oil px less than 26 psi

- engine oil px less than 20 psi

19
Q

The engine oil pressure cations and engine oilntemp cautions are triggered by (sensor(s))

A

The vertical instrument

Therefore cautions and gauge indications cannot be used as secondary indications for each other

20
Q

Eng hot caution

A

TGT > 949°C (max)

21
Q

ENG OIL HOT

A

Engine oil temp > 150°C

22
Q

ENG OIL PRESS HI

A

Engine oil px > or = 120psi

23
Q

Max gross weight for auto

A

19 500#

24
Q

Auto altitudes in agl and speed kias

A

500’/80 straight in auto

500’/95-100 max glide auto

800’/80 for 90 auto

1000’/80 for 180 auto

25
Q

Autoo @ 200’ agl

A

Flare, allow Nr to build to 105-110%

26
Q

DNE what angle of nose up in auto

A

35°

27
Q

In auto @ 60’agk

A

Rock and pull

28
Q

Recover auto by

A

20’ agl/15-20kgs

29
Q

Auto wave off criteria

A

In descent: Nr exceeds 110%; not over rwy by 300’agl; not aligned with rwy by 300’agl

At flare (100’): airspeed < 75 kias

During flare/recovery: aircraft balloons 50’ +; excessive lateral drift and/or sink rate, recovery not initiated by 60’, tail slide indications(>35° and low airspeed)

30
Q

Hit checks shall

A

Be conducted while aircraft is on deck