Systems Flashcards

1
Q

What is the fuselage made out of and what type of construction is it?

A

CFRP, a semi monocoque construction

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2
Q

What are the wings made out of and what construction are they?

A

CFRP + GFRP, they are a semi monocoque construction

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3
Q

What are the ailerons, flaps, elevator and rudder made from and what design are they?

A

They are made from CFRP + GFRP, sandwich construction

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4
Q

Each wing is F….. S….. and has a main and rear ….

A

Fail safe - Front and rear spar -

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5
Q

What is the firewall made from and how is it designed?

A

It is made from fire resistant matting and stainless steel cladding. The stainless steel cladding has a layer of fire resistant matting over it on the engine side. Which separates it from the rest of the structure.

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6
Q

What is the fuel tank made from? Is it just one tank?

A

Aluminium fuel tank with 3 sections

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7
Q

Total fuel quantity? Total usable? Max fuel imbalance?

A

52 gallons 50 gallons 5 gallons

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8
Q

How does the canopy attach to the fuselage?

A

It attaches to a roll over bar, the roll over bar then forms the construction of the cockpit. Canopy has a forward hinge mechanism.

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9
Q

What prevents anything jamming in the control columns?

A

Gaiters

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10
Q

Are the front seats adjustable or removable?

A

Front seats are removable and the rear seats are adjustable via a locking pin

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11
Q

In the event of a crash what frequencies will the ELT transmit on and for how long the will it transmit? What setting does it need to be on to do this and are there any others methods of activate it?

A

VHF, UHF and satellite frequencies for up to 72 hours. Needs to be set to arm, however can be manually activated

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12
Q

How are the ailerons and rudder operated?

A

They are operated via control rods and control cables

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13
Q

What are the ailerons and are do they have a trim tab

A

Conventional ailerons - trim tab on left which is fixed to adjust trim has to be done on ground by engineers by bending the tab

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14
Q

Electrical trim - explain?

A

Electrical trim switch that comprises of a servo motor connected to the electric trim wheel

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15
Q

What type of switch is the trim switch - how does it work and what does this help guard against?

A

Dual pole Must press both switches at same time for trim If only one switch is pressed for 3 seconds or more then it won’t trim and it will make a PT annunciation show on the auto pilot - prevents against trim runaway

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16
Q

How does the elevator stick limiting system work?

A

The amount of elevator deflection available changes in certain configurations. The system does this by sensing the position of the power levers and flaps. When flaps are landing and power levers are at more than 20% the backstop limit is decreased. Full elevator deflection is regained when flaps are retracted or power less than 20%.

17
Q

What is full elevator deflection and what can in be reduced to? How is it reduced?

A

Full elevator deflection is 15.5% This can be reduced to 13% when landing flaps are retracted and more than 20% power is on This is done by an electrically actuated control stop

18
Q

When does the stick limit caution annunciate?

A

If the system malfunctions and/or there is full deflection with land flap and power more than 20%. Or if there is not full movement when landing flap is retracted.

19
Q

How do the flaps work?

A

The flaps are electric Control rods are moved by electric actuators

20
Q

What happens if the flap selector over runs the electric motor?

A

This will draw a high current from the motor and cause the circuit breaker to pop caused by the motor stalling

21
Q

How is the rudder operated

A

The rudder is operated by control cables

22
Q

Stall warning system - What is the type of stall warner on the DA42? How does it work?

A

Electrical flapper device fitted to the left hand leading edge. Known as a lift detector vane. Works by activating a warning if the angle of attack exceeds a set value. As the AoA increases the stagnation point moves down on the leading edge. At low AoA This then keeps the flapper in its down position. However at Larger AoA the stagnation point moves down and aft behind the flapper switch which then causes the airflow to push the flapper switch up. Used to symbolise a high AoA cannot warn for the approach of the stall! But symptoms of the stall are large AoA

23
Q

Is the DA42 approved for flight into icing conditions?

A

Approved for flight into known conditions: * No FZRA/FZDZ * De-icing system must be serviceable and fluid at least 3/4 full * Must not depart with ICE, frost or snow adhering to wings, propellers, ctrl sfcs, windscreen or any system necessary for flight

24
Q

Describe the obstacle colour legend on the G1000

25
Describe the G1000 schematic
26
Describe the L/G extension process
* 3 actuators extend the gear assisted by springs * Springs hold down-lock hooks engaged * Gear held down by down-locks and hydraulic pressure.
27
Describe the L/G retraction process
* Hydraulic pressure directed to both sides of actuators * Fluid flows from extension side, gear retracts * Inadvertent retraction prevented by squat switches * Gear held up by hydraulic pressure