1 - General Knowledge Flashcards

1
Q

Aspiration type?

driveshaft type?

how is it cooled?

Engine layout?

Fuel injection?

How many cylinders?

A

Normally Aspirated
- Not turbo/super charged

Direct Drive
-no belt, motor is directly spinning prop

air cooled

horizontally opposed
- flat engine, so cylinders on each side

fuel injected
- no primer!

four cylinder
- 2 on each side of engine horizontally opposed

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2
Q

What is horsepower rating and engine speed?

A

HP: 180 rated BHP

engine speed: 2700 RPM

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3
Q

What are the approved fuel grades (and their colours)?

A

100LL grade aviation fuel
-Blue

100 Grade aviation fuel
-Green

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4
Q

What is the total fuel capacity?

Total usable fuel capacity?

A

56 US Gallons is total capacity

53 US Gallons is total usable

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5
Q

After the first 50 hour oil break in period, what oil should be used?

A

MIL-L-22851 or SAE j1899 Aviation Grade Ashless Dispersant Oil

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6
Q

What is the Sump and Total oil capacity?

A

Sump: 8 US Quarts
- depression in bottom of engine to use as a bit of a reserve

Total: 9 US Quarts

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7
Q

What is the maximum Takeoff and landing weight for both categories (normal/utility)?

A

Both maximum takeoff and landing weight are the same at:

Normal: 2550 lbs
Utility: 2200 lbs

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8
Q

What are the loading conditions to be in the utility category?

A

Rear seat and baggage compartment must be empty.

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9
Q

Roughly, what are the standard airplane weights?

Empty weight:
Maximum useful load, Normal
Maximum useful load, Utility

A

the standard airplane weights:

Empty weight: 1663 lbs
Max useful load, Normal: 895 lbs
Max useful load, utility: 545

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10
Q

What is KTAS?

A

Knots true airspeed, meaning it is the airspeed relative to undisturbed air - or KCAS corrected for altitude and temperature

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11
Q

What is KCAS?

A

Knots calibrated airspeed, so that is indicated airspeed corrected for position and instrument error.

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12
Q

When it KCAS equal to KTAS?

A

Well, KTAS is just KCAS corrected for deviance from standard of altitude and temperature. Therefore, KTAS will equal KCAS in standard atmosphere at sea level (15C & 29.92inHg)

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13
Q

Define and state following V speeds:

Va:

Vfe:

Vno:

Vne:

Vs

Vso

Vx

Vy

A

Va:
- Maneuvering speed (max abrupt movements)

Vfe:
- Max flap extended speed

Vno:
- Max structural cruising speed (can only be exceeded with caution in smooth air)

Vne:
- Never exceed speed

Vs
-Stalling speed

Vso
- stalling speed in landing config at most forward centre of gravity

Vx
- Best Angle-of-Climb (highest alt in shortest distance)

Vy
-Best rate-of-climb (highest alt in shortest time)

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14
Q

Difference between RPM and static RPM

A

Static RPM is engine speed attained during a full throttle engine runup when on the ground and stationary

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15
Q

What is MAP (Manifold Absolute Pressure)?

A

Measured in inHG (same as altimeter), the the Manifold Absolute Pressure is the absolute pressure measured in the engine induction system

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16
Q

What is the course datum?

A

The course datum is the compass reference combined with the course deviation to provide lateral autopilot control when tracking a nav signal

17
Q

What is the reference datum?

A

This an imaginary line slicing the plane vertically like a cucumber. It’s a point which all horizontal distances are measured from for balance purposes

18
Q

What is the station?

A

This is a location somewhere on the fuselage which serves as a reference to measure the distance from the reference datum

19
Q

What is an arm in W&B?

A

Arm is just the horizontal distance from an item’s centre of gravity and it’s reference datum

20
Q

What is the moment in W&B?

A

The moment of an item is just it’s weight x it’s arm.

21
Q

Obviously you can’t balance every item on a stick to find C.G. So how do you calculate it’s distance from the reference datum?

A

The centre of gravity’s distance from reference datum can be calculated by doing this:

total moment / total weight of plane

22
Q

Define what the standard empty weight is?

Basic empty weight?

A

Standard empty weight is plane with unusable fuel, full operating fluids, and full engine oil

Basic empty weight is standard empty weight plus any optional equipment

23
Q

Define useful load

A

useful load = ramp weight - basic empty weight

24
Q

What is MAC (Mean Aerodynamic Chord)?

A

Chord of an imaginary rectangular airfoil having the same pitching moments throughout the flight range as that of the actual wing.

So think of an imaginary box being drawn around the wing to perfectly fit it. The MAC is the line that goes right through the middle as if it was just a box wing.