A102 Aircraft Systems Flashcards

1
Q

DA 20 Components

A

FUSELAGE
WINGS
COCKPIT
EMPENNAGE
FLIGHT CONTROLS
LANDING GEAR
POWERPLANT (Eng + Prop)

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2
Q

Describe Fuselage

A

The fuselage is the body of the aircraft. The
DA20C-1 has a GFRP-fuselage of semi-monocoque (reinforced shell) construction.

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3
Q

Describe the Wings

A

Wings are the primary lift generating
component of an aircraft. The GFRP-wings
are of semi-monocoque sandwich construction
and contain a CFRP-spar for strength. The
ailerons and flaps are made from CFRP and
are attached to the wings using stainless steel
and aluminum hinges.

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4
Q

Describe the Cockpit

A

2xFixed Position Seats
Dual Stick, Single Throttle
Adjustable rudder pedals
(Everything painted red goes forward)

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5
Q

Describe the Empennage

A

The tail of the fuselage and includes the vertical and horizontal stabilizers

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6
Q

Describe the primary flight controls

A

Ailerons, Rudder, Elevators

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7
Q

How are the Rudders controlled?

A

By cable from the pedals themselves to the rudder

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8
Q

Describe the Flaps

A

Slotted flaps for landing and take-off
Operated by an electric flap actuator
3 position switch: Cruise, T/O, and LDG

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9
Q

Describe Trim

A

The electrically operated trim system balances the elevator forces for different air speeds.

“Pitch-Power-Trim”

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10
Q

Describe the Landing Gear

A

Fixed tricycle ldg gear
Aluminum spring main landing gear struts
60° free castering nose wheel mounted to a tubular strut.
The manual brake pedals operate hydraulic disk brakes on the main wheels.

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11
Q

Describe the Powerplant

A

BOTH Eng and Prop
Continental IO-240-B engine. Fuel injected, 4-cylinder, 4-stroke engine with horizontally opposed, air cooled cylinders and heads, with a displacement of 239.8 cu.in. (3.9 liters).
Propeller drive is direct from the crankshaft.

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12
Q

Describe 4-Cycle Eng Operation

A

Converting fuel into mechanical energy.
These strokes are called intake, compression, power, and exhaust.

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13
Q

Spark plugs per cylinder

A

2

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14
Q

Total Number of Spark Plugs

A

8

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15
Q

Describe Eng Baffles

A

2 Types: Inlet (upper) and Outlet (lower) Baffles
During cold months, baffles used to allow quicker engine warm up and limit cooling to keep engine temps in optimum range

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16
Q

Describe the Eng Controls

A

The Mixture, Throttle and Alternate Air Control levers

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17
Q

Mixture Lever

A

Right lever with red cylindrical handle and integral lock
out lever.
Mixture Lever full forward = Full Rich
Mixture Lever full aft = Idle Cutoff

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18
Q

Describe the Prop

A

Sensenich W69
Two Blade
Wood Construction
Plastic Laminate
Fixed Pitch
Direct Drive
Diameter: 5 ft 9 in

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19
Q

Describe how a prop works

A

2 ways:
The propeller has a camber like a wing to produce lift in the forward direction

The propeller is twisted to change the angle of attack from the hub to the tip.

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20
Q

DA20 Flight Instruments

A

Airspeed Indicator
Attitude Indicator
Altimeter
Turn Coordinator
Heading Indicator
Vertical Speed Indicator
Magnetic Compass

21
Q

ID the Engine Instruments

A

Cylinder Head Temp (CHT)
Exhaust Gas Temp (EGT)
Fuel Pressure
Fuel Quantity
Oil Temp
Oil Pressure
Ammeter
Voltmeter

22
Q

Where is the CHT Measured from?

A

Left rear cylinder

23
Q

Where is the EGT Measured from?

A

Left rear exhaust pipe

24
Q

Where is the Fuel Pressure measured from?

A

Fuel distribution manifold

25
Q

Oil Temp for Full Power Operation?

A

100 F

26
Q

What is the Ammeter?

A

Indicates current flowing b/w the battery and main bus
When the needle is indicating a + , the battery is receiving a charge, a - would be opposite

27
Q

What is a Voltmeter

A

Indicates the voltage on the main bus.
Indicates about 14 volts when the generator is on-line.

28
Q

What is the function of the Oil System?

A

The engine oil system performs several functions to include:
* Lubrication of the engine’s moving parts.
* Cooling the engine by reducing friction.
* Removing heat from the cylinders.
* Providing a seal between the cylinder walls and pistons.
* Carrying away contaminants which cleans the engine.

29
Q

When would you add a quart of oil?

A

When it is measuring less that 4.5 quarts.

30
Q

What material is the fuel tube?

A

Brass

31
Q

How many fuel pumps?

A

2

32
Q

How many are electrically driven?

A

1

33
Q

What gas do we use?

A

100LL (blue in color)
- DA20 can run on 100 as well

34
Q

Where does Cabin Heat come from?

A

Heated around the exhaust manifold

35
Q

3 Components of the Pnuematic system?

A

Engine Induction Air
Alternate Air
Cabin Heat/Defrost Air

36
Q

How many ignition systems are in the DA20?

A

2

37
Q

How many Magnetos are there in the ignition system?

A

2 (left and right)

38
Q

Major Components of Electrical System?

A

Battery/Alternator - Electrical Wiring - Electrical Bus - Circuit Breakers - Electrical Equipment

39
Q

Alternator Volts/Amps?

A

14 volts, 40 Amps

40
Q

Battery Volts/Amps?

A

12 volts / 20 Amps

41
Q

Brake System Source?

A

Hydraulic Reservoirs
One behind each pedal
Holds 0.5 Liters each

42
Q

Where are the Landing & Taxi Lights located?

A

Left Wing

43
Q

Where is the Pitot Static Tube located?

A

Left Wing on the bottom

44
Q

What is the Static system connected to?

A

Airspeed, Altimeter, VSI, Mode C Transponder

45
Q

Vacuum System is connected to what?

A

Attitude and Heading Indicator

46
Q

Warning Indicators?

A

GEN
CANOPY
START
EPU

47
Q

What is both the Pitot and Static system connected to?

A

Airspeed Indicator

48
Q

When does the stall warning sound?

A

5 knots before a stall