CPL Skills Test - Aircraft Knowledge Flashcards

1
Q

Landing gear - Fluid used?

A

MIL-H-5606

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Landing gear - Purpose of pressure switch?

A

Tells system when gear is up and pressurised, turns off hydraulic pump

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

Landing gear - Gear down mechanism?

A

Gravity and hydraulics

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Landing gear - Gear up mechanism?

A

Hydraulics

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Landing gear - Up limit?

A

Turns off gear unsafe light after gear has been retracted

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Landing gear - Downlock switch?

A

Turns the 3 green lights on

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

Landing gear - Squat switch?

A

Acts as weight off wheels indicator (left gear), should not be touching on the ground

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Landing gear - When does alarm go off?

A

Flaps 25, no gear
Below 13’ manifold, no gear
No gear on ground

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Landing gear - Emergency extension?

A

Emergency valve opens, 1800 PSI

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Landing gear - Nose wheel steering?

A

30 degrees each way

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Brakes - type and reservoir?

A

Single disc hydraulic on man gears. Reservoir under engine cowling

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

Flaps - Stages and type?

A

Flaps 10 - Plain
Flaps 25/40 - Slotted

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Stabilator - Design and purpose?

A

Anti-servo trim tab to prevent overcontrol and to give positive feel

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Ailerons - Type?

A

Differential ailerons to minimise adverse law

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Intakes - Locations and purposes?

A

Intake below landing light - Environmental systems, air heated through shroud around exhaust for cabin and window defrost.
Intake to right of prop - Engine cooling entering towards lower portions of cylinder 2 and 4

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Fuel system - Components?

A

Fuel selector
Fuel filter
Electric boost pump
Engine driven fuel pump
Servo Regulator
Flow Dividers
Fuel injectors
Throttle

17
Q

Fuel system - Electric boost pump purpose?

A

Provides fuel pressure for priming and as backup to engine driven pump

18
Q

Fuel system - Engine driven pump function and purpose?

A

Diaphragm pump, converts rotary motion from accessory case to linear motion through cam

19
Q

Fuel system - Servo regulator purpose?

A

Measures amount of fuel flowing to injectors. First point of control inside the servo regulator is the fuel control unit which is attached

20
Q

Fuel system - Throttle operation?

A

Throttle opens and closes the butterfly valves which controls how much air is going through the filter and induction manifold.

21
Q

Fuel system - Amounts?

A

77 gal total (38.5 in each)
72 gal usable (36 in each)
Tabs - 50 gal (25 in each)

22
Q

Fuel system - Burn?

A

12.7 gal/hr 65% power @ 2500RPM

23
Q

Induction system - alternate air source?

A

Door that functions automatically when primary source is obstructed, can also be operated manually

24
Q

Engine - layout and information?

A

Horizontally opposed, 4 cylinder, direct drive, fuel injected

200HP @2700RPM

Oil between 6-8 quarts (Skyborne standard)

25
Airframe - MTOW
2750lbs
25
Controllable pitch prop - Components and function?
Prop governor - Speeder spring and flyweights control flow of oil into hub via valve Overspeed - Flyweights go out, spring and pilot valve moves up, allowing more oil to entry the hub to make pith more course. Torque requirement increases, RPM decreases
26
Electrics -Battery and alternator?
24V battery, 28V alternator
27
Pitot static system - Locations and use?
Pitot tube under left wing, static pressure sensed by button vents on both sides of fuselage. Used for ASI, altitude, and VSI Alternate static
28
Pitot static system - Alternate sources
Alternate static inside cockpit, left of pilot seat
29
Airspeeds - Vs1/Vs?
Vs1 - 55 Vs - 60
30
Airspeeds - Vx, Vy?
Vx - Gear Down - 72 Vx - Gear up - 78 Vy - Gear down - 78 Vy - Gear up - 90
31
Airspeeds - Vg?
Vg - 79
32
Airspeeds - Vle
Vle - Retract - 107 Vle - Extend - 129
33
Airspeeds - Vfe, Va
Vfe - 103 Va - 118
34
Airspeeds - Vno, Vne?
Vno - 146 Vne - 183