Airplane Instrument, Engines and Systems Flashcards

You may prefer our related Brainscape-certified flashcards:
1
Q

What is the instrument that is checked while preflighting?

A

Compass

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2
Q

When does the magnetic compass give a reliable indication?

A

In straight and level unaccelerated flight

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3
Q

When does the magnetic compass indicate a turn to the north?

A

When accelerating on a east or west heading

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4
Q

When does the magnetic compass indicate a turn to the south?

A

When decelerating on a east or west heading

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5
Q

During your preflight inspection, you find the pitot tube blocked. What instrument(s) would be affected by this?

A

The airspeed indicator.

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6
Q

What instruments would be affected by a loss of vacuum?

A

Heading indicator and attitude

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7
Q

What should the vacuum gauge read under normal circumstances?

A

PA-28-181: 4.8 to 5.2

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8
Q

What instruments would be affected if your static sources were blocked?

A

altimeter
Airspeed Indicator
Vertical Speed indicator

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9
Q

What would cause your attitude indicator and heading indicator to fail?

A

Loss of vacuum

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10
Q

How much power does the engine have?

A

PA-28-181: 180 BHP Lycoming O-360-A4M

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11
Q

What is the total fuel capacity of the airplane?

A

PA-28-181: 50 gallons

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12
Q

How much usable fuel is on board?

A

PA-28-181: 48 gallons

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13
Q

What octane of fuel is used and what color is the fuel?

A

PA-28-181: 100 Low Lead; light blue

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14
Q

What are you looking for when checking fuel samples?

A

Correct color to verify the correct octane and any water bubbles or other types of contamination

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15
Q

How do the fuel tanks feed the engine?

A

PA-28-181:
The fuel is fed either from the left or right fuel tank as selected by the fuel selector valve in the cockpit. The fuel is pumped through the fuel strainer either by the electric, engine drive, or both fuel pumps. From there it is pumped into the carburetor where it is mixed with air and distributed to the cylinders.

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16
Q

How many fuel draining locations are on the airplne?

A

PA-28-181:

3; two under each wing and 1 in the engine

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17
Q

During preflight, you find a puddle of red fluid around on of the main tires, what does this indicate?

A

This is brake fluid and indicate a lead in the brake system.

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18
Q

What is the oil capacity of the airplane?

A

PA-28-181: 8 quarts

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19
Q

When should the oil be checked and what is the minimum amount of oil that must be in the airplane for flight?

A

PA-28-181:

The oil should be checked before each flight and have at least 6 quarts

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20
Q

What should you do if you find nicks in the propeller?

A

Cancel the flight and have the blades inspected by an A&P mechanic

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21
Q

How much magneto drop is allowed when running up teh engine?

A

PA-28-181: No more than 175 RPM drop on each magneto and no more than 50 RPM difference in between the two mags.

22
Q

What should you do if the oil pressure goes to zero and the temperature starts to rise rapidly?

A

Land as soon as possible and investigate cause. Prepare for power off landing

23
Q

What does it mean when after you have actuated the carburetor heat then the rpm drops and then rises on its own?

A

It means carburetor icing was present

24
Q

What is the first thing you should do if the engine begins to lose rpm and run a little rough?

A

Engage carburetor heat

25
Q

What is the first thing you should do if the engine should quit?

A

Trim for best glide speed 76 KIAS

26
Q

Where does the cabin heat come from

A

The head coming from the engine exhaust

27
Q

How much fuel does this airplane burn per hour in normal cruise?

A

PA-28-181: 9.5g/h at 65% power 117 kts

28
Q

What voltage and amperage does the electrical system have?

A

PA-28-181: 14-volt, 60 Amp

29
Q

What should you do if your load meter indicates an excessive load?

A

PA-28-181:
Most likely faulty voltage regulator

Alt switch off
Bat switch On
Reset alt circuit breaker

Else Alt switch off bat switch as required land as soon as possible. prepare for full electrical failure

30
Q

What should you do if your load meter indicates a lower-than-expected load?

A
PA-28-181:
turn on some equipment and look for load indication
Alt switch off
Check Alt breaker 
Alt switch ON
If power is not restored alt switch off 
reduce electrical load and land as soon as practical
31
Q

What should you do if your low-voltage light illuminates

A

Check load meter to verify inop. alt (zero)

32
Q

What is the gross weight of the airplane?

A

N5676V: Empty weight 1518.25lb + people + baggage + fuel = gross weight

33
Q

What is the empty weight of the airplane?

A

N5676V: 1,518.25 (AC W&B Sheet)

34
Q

Where is the exact empty weight and the empty center of gravity found?

A

The aircraft W&B document inside the aircraft

35
Q

What is the maximum ramp weight?

A

N5676V: 2558.00lb

36
Q

What is the maximum takeoff weight?

A

N5676V: 2550.00lb

37
Q

What is the maximum landing weight?

A

N5676V: 2550.00lb

38
Q

What is the maximum baggage weight?

A

N5676V: 200lb

39
Q

What is the normal cruise RPM?

A

PA-28-181: 2,430

40
Q

What is the minimum octane that is to be used in the airplane?

A

PA-28-181: 100

41
Q

When ground handling the airplane with a towbar, how much can the nose gear be turned right or left?

A

PA-28-181: 20 degres left/right of center

42
Q

What kind of oil is used in the airplane?

A

PA-28-181: Ashless mineral oil - SAE 50 (Aeroshell 100)

SAE 50 but can vary depended on ambient temp.

43
Q

As density altitude increases, what happens to performance?

A

Performance decreases

44
Q

How much air pressure should be kept in the tires?

A

PA-28-181:
Nose Gear: 18 psi
Main Gear: 24 psi

45
Q

How does carburetor ice form?

A

The pressure drop in the venturi causes the air to cool and draw heat away from the surrounding metal of the carburetor venturi. Ice can then collect on the cooled carburetor throat.

46
Q

wingspan of your aircraft

A

35 feet

47
Q

Length of your aircraft

A

24 Feet (23’ 9.6”)

48
Q

Height of your aircraft from the ground

A

7.5 feet (7’ 3.6”)

49
Q

wing square area

A

170 sq ft

50
Q

min turning radius (pivot point to wing tip)

A

30 Feet