Airframes, Engines, Propellers, and Aircraft Systems Flashcards

1
Q

What is Flex Temp?

A

It is the assumed temperature used to reduce the thrust of a gas turbine engine.

  • Used to reduce takeoff thrust to the minimum needed for a safe takeoff
  • Allows for less noise and less engine wear
  • Flex temp is the highest ambient temperature allowed at which the aircraft could make a safe takeoff at minimum thrust

Higher flex temp = less performance needed due to good conditions, long runway, light aircraft, etc. (saves the engine!)

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2
Q

Which system(s) are used to operate the de-icing boots?

A

Pneumatic system.

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3
Q

Np represents ___ speed rotation and Ng represents __ speed rotation in a free-turbine type engine.

A

Propeller RPM and gas generator speed.

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4
Q

Weight shift formula:

A

Weight to be shifted / Total weight ÷ Δ CG / distance weight is shifted

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5
Q

Which of the following is taken into account by an aircraft’s manufacturer to determine Vmca?

A

?

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6
Q

In determining whether a turbojet aeroplane used in a commuter operation can be dispatched or a takeoff can be conducted, not more than __% of the reported headwind component or not less than__% of the reported tailwind component shall be taken into account.

A

50, 150

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7
Q

What is the final assurance of a safe takeoff in case of icing conditions?

A
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8
Q

Compared to the axial compressor, the centrifugal compressor:

A

Has a larger frontal area.

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9
Q

In an engine equipped with a turbocharger, the turbocharger compresses the air ___ it is mixed with the fuel. When the outside air is not dense enough, the wastegate valve __, thereby directing exhaust gas to the turbine, which will start to rotate and thus compress the air.

A

Before, closes.

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10
Q

What is the mechanism that prevents the reversing of a turboprop engine aeroplane during a cruise flight?

A

The low (or fine) pitch stop system.

System blocks the use of reverse thrust when props are over a certain value, or in flight.

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11
Q

What devices offer electrical protections to an aircraft’s electrical circuits?

A
  1. Fuse
  2. Generator control unit
  3. Circuit breakers
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12
Q

What causes compressor stalls?

A

A too high angle of attack to the compressor blades.

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13
Q

What is the basic principle of a turbocharger?

A

Increases the DENSITY of air that is supplied to the motor therefore increasing power to engine.

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14
Q

In a turbocharged engine, a waste-gate located in the ___ exhausts gas directly in the atmosphere, bypassing the ___.

A

Exhaust system, turbine wheel.

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15
Q

A flight control system is a system that:

A

Includes the flight direction and autopilot system.

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16
Q

The torque motor of the gyromagnetic remote indicating compass:

A

Makes the directional gyroscope to precess. (A SLAVE HSI)

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17
Q

Viscous hydroplanning occurs when:

A

Aircraft is slow over a thin film of water.

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18
Q

Ground effect is strongest on an aircraft with ___ wings and a ___ wingspan.

A

LOWER wing and HIGHER wingspan; Arrow has better ground affect than cessna!

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19
Q

To avoid tailplane stalling, you should avoid:

A

Exceeding tailplane critical angle of attack by abruptly pushing on control column.

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20
Q

Shock waves form near ____ and cause a ____ motion of the plane.

A

Root, nose down.

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21
Q

When decreasing at a constant CAS, the mach number ______ and the local speed of sound ____.

A

Decreases (like flight sim) and increases (more air = more crap for sound to move through)

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22
Q

Formula for required bank in rate one turn:

A

TAS / 10 + 7 kts

TAS/10 + 5 mph

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23
Q

How is the critical altitude in a turbocharger defined?

A

Wastegate is fully closed & can’t keep the pressure needed for the rated power.

24
Q

Deice fluid should first me applied to:

A

Surfaces that can be seen from the cockpit.

25
Q

What are the differences between TAWS A and B?

A

A has all the features of TAWS B, but also has terrain awareness display, and a fully autonomous GPWS (ground proximity warning system) system.

26
Q

What do TAWS A and B both include?

A
  • Premature descent alerts
  • Attention alerts
  • Indications of imminent contact with ground
27
Q

What id the difference between TAWS and GPWS?

A

TAWS builds on GPWS (GPWS is BASIC). TAWS provides the pilots with an earlier warning.

28
Q

What is V1?

A

Go no-go speed.

ALSO

Critical engine failure recognition speed

29
Q

What is V2?

A

Takeoff safety speed.

30
Q

What is V2min?

A

Minimum takeoff safety speed.

31
Q

What is V3?

A

Flap retraction speed.

32
Q

What is V4?

A

Initial climb speed.

33
Q

What is Vmo?

A

Maximum operating speed.

34
Q

What is a balanced field length?

A

Where takeoff-go distance and takeoff-stop distance are the same.

35
Q

What does it mean when controls are in BETA?

A

When the control pitch is in BETA (a lower power setting than idle), it prevents reverse thrust.

36
Q

Ho can you prevent dynamic hydroplanning?

A
  • Do not land fast
  • Keep your tires inflated
  • Use aerodynamic braking
37
Q

How can you prevent reverted rubber hydroplanning?

A
  • Use light braking to keep maximum weight on your main landing gear
  • DO NOT lock up your wheels (reverted rubber = skidding and locking up the tires!)
38
Q

How can you prevent viscous hydroplanning?

A
  • Do not land fast
  • Keep your tired inflated
  • Use aerodynamic braking
39
Q

Reverted rubber hydroplaning occurs when:

A

Tire locks up, rubber melts, makes water steamy. RUBBER

40
Q

Dynamic hydroplaning occurs when:

A

The water lifts your wheels off the surface of the runway. Occurs when a wedge of water builds up in front of your tires and lifts you up.

41
Q

In BETA range, what controls the prop pitch?

A

The power lever AND mechanical linkage.

42
Q

When taxiing a turboprop in BETA mode, the power lever has direct control over:

A

The propeller PITCH.

43
Q

What is the purpose of the bleed valve?

A

To prevent stall of the compressor.

44
Q

When is it most likely for a compressor stall?

A

During engine start.

45
Q

The best way to respond to the needs of one or more hydraulic systems that require different oil flows to work is to:

A

Operate the VARIABLE DISPLACEMENT hydraulic pump.

46
Q

What does an EPR reading of 1.0 mean?

A

There is no net thrust from the engine.

47
Q

During engine start, the starter turns the:

A

HIGH PRESSURE SPOOL.

48
Q

How does the airspeed indicator react to a blocked pitot tube?

A

Over reads in climb, under reads in descent.

49
Q

How does the airspeed indicator react to a blocked static port?

A

Under reads in climb, over reads in descent.

50
Q

What happens to the air speed indicator if the drain hole and pitot tube are blocked?

A

Airspeed indicator will go off of static information: under read in climb, over read in descent.

51
Q

What is the compass lubber line?

A

The line showing the heading of the aircraft with the compass.

52
Q

Purpose of a bleed valve:

A

To help prevent compressor stall.

53
Q

During BETA, the power lever controlls:

A

Blade angle AND fuel flow (beta plus power range)

54
Q

What is the TIT?

A

Turbine Inlet Temperature

Measurement of temperature before the turbine

55
Q

What is the ITT?

A

Interstage Turbine Temperature

Measures the temeprature between the HI/LO pressure compressor.