ACM-115 W & B (STUDY QUESTIONS) Flashcards

(54 cards)

1
Q

6-1
It is the responsibility of the ________ who makes a repair or alteration to change the aircraft ______ and ______ paperwork.

A

Aircraft Maintenance Technician
Weight
Balance

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2
Q

6-1
The paperwork must reflect the new computations for _____ and _____ and indicate the aircraft is ______ ______ ______.

A

weight
balance
safe to fly

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3
Q

6-2
What does Basic Empty Weight include? (5)

A
  1. Aircraft Weight
  2. Ballast - Fixed
  3. Equipment - (Optional / special)
  4. Fluids:
    a. Oil
    b. Hydraulic fluid
    c. Other fluids required for normal operation of aircraft systems
  5. Fuel - Unusable
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4
Q

6-2
What does Basic Empty Weight NOT include?

A
  1. Potable Water
  2. Lavatory precharge water
  3. Engine injection water
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5
Q

6-2
What is the term for Basic Empty Weight used prior to March 1, 1978?

A

Licensed Empty Weight

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6
Q

6-2
What does Licensed Empty Weight NOT include?

A

Full engine oil
(Only includes weight of undrainable oil)

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7
Q

6-2
What sources should you consult to obtain all information regarding weight and balance data for a particular aircraft? (5)

A
  1. Flight Manual
  2. Limitations
  3. Specifications
  4. Type Certificate Data Sheets
  5. Weight and Balance Report
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8
Q

6-2
Define Standard Empty Weight.

A

Weight of an aircraft without optional equipment obtained from aircraft manufacturer.

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9
Q

6-2
What are Standard Weights used to compute the weight of? (5)

A
  1. Baggage
  2. Crew
  3. Fuel
  4. Oil
  5. Water
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10
Q

6-2
List the weight for the following items:
1. AVGAS
2. TURBINE FUEL
3. LUBRICATING OIL
4. WATER
5. CREW & PASSENGERS

A
  1. 6 lbs. p/gal
  2. 6.7 lbs. p/gal
  3. 7.5 lbs. p/gal
  4. 8.35 lbs. p/gal
  5. 170 lbs. p/person
  6. 190 lbs. for utility / aerobatic aircraft
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11
Q

6-2
What does Payload include the weight of?

A
  1. Flight crew
  2. Passengers
  3. Cargo
  4. Baggage
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12
Q

6-2
Define Useful Load

A

Difference between maximum takeoff weight and basic empty weight

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13
Q

6-2
What weights does useful load include?

A
  1. Payload
  2. Usable fuel
  3. Full operating fluids
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14
Q

6-2
Define Usable Fuel

A

Fuel available for the flight

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15
Q

6-2
Define Unusable Fuel

A

Quantity of fuel that cannot be safely used during flight.

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16
Q

6-2
Define Zero Fuel Weight

A

Operational weight of the aircraft including payload but excluding fuel load.

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17
Q

6-3
Define Maximum Ramp Weight

A

Maximum weight approved for ground operations

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18
Q

6-3
Define Maximum Takeoff Weight

A

Maximum weight approved for the start of the takeoff roll

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19
Q

6-3
Define Maximum Landing Weight

A

Maximum allowable weight at which an aircraft can be landed

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20
Q

6-3
Weight limitations are necessary to guarantee the _____ _____ of an airplane, as well as enable the pilot to predict _____ _____ accurately.

A

structural integrity
aircraft performance

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21
Q

6-3
Define Scale Weight
Includes the weight of all items on the scales including:

A

Reading taken from the scales:
1. Aircraft
2. Chocks
3. Jacks

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22
Q

6-3
Define Tare Weight
The weight of these items must be deducted from the _____ _____ to obtain the actual or _____ _____.

A

weight of all items on the scales that are not part of the aircraft.
Scale Weight
Net Weight

23
Q

6-3
How many aircraft is the manufacturer required to weigh?

24
Q

6-3
When must a general aviation aircraft be weighed and a new set of records computed?

A

When weight & balance records are lost and cannot be duplicated from any source.

25
6-3 What secondary times should a general aviation aircraft be weighed?
1. After making major alterations that affect the weight & balance 2. Periodically to account for accumulation of dirt, greases and other trapped debris.
26
6-4 Define Aircraft Center of Gravity
point along an aircraft's longitudinal axis
27
6-4 Define CG Range
The distance between the limits between the most forward and rearward CG limits
28
6-4 For light aircraft, the CG is expressed in terms of _____ from a predetermined _____ _____.
inches reference point
29
6-4 A part of the certification procedure for an airplane is to determine that its weight and balance are within the _____ _____, and this information is furnished with the aircraft as part of its _____ _____.
allowable limits operations manual
30
6-4 What are characteristics of an overloaded aircraft?
1. Higher-than-normal speed to generate lift for flight. 2. More runway for takeoff 3. Reduces acceleration during takeoff roll adding to total takeoff distance. 4. Reduction in climb performance 5. Service Ceiling decreased
31
6-4 What are the characteristics of a Forward CG?
1. Nose heavy 2. Longer takeoff distance 3. Higher stall speeds
32
6-4 What are the characteristics of a Rear CG?
1. More dangerous than forward CG 2. Tail heavy 3. Unstable in pitch, regardless of speed 4. Stabilator effectiveness decreases
33
6-4 Define Datum
Imaginary vertical plane from which all horizontal measurements are taken with the aircraft in a level flight attitude.
34
6-4 The reference datum sits at a _____ angle to the aircraft's _____ axis.
right longitudinal
35
6-4 All items are listed in the Aircraft Specifications or TCDS referenced as ______ from the datum
inches
36
6-19 Define Basic Empty Weight
Weight of the aircraft, any optional or standard equipment, fixed ballast, unusable fuel and full operating fluids. The starting point for the computation of weight and balance.
37
6-19 What are the standard weights for: 1. Gallon of Gas 2. Gallon of Oil 3. Gallon of water
1. 6 lbs. 2. 7.5 lbs. 3. 8.35 lbs.
38
6-19 Define Payload
Weight of the flight crew, passengers and cargo or baggage
39
6-19 Define Center of Gravity
Point along an aircraft's longitudinal axis at which an aircraft's weight is concentrated.
40
6-19 Define CG range
Distance between forward and aft CG limits
41
6-19 Define Datum
An imaginary vertical plane from which all horizontal measurements are taken with the aircraft in level flight attitude.
42
6-19 List where weight and balance information for a specific aircraft is located:
1. TCDS 2. Approved Airplane Flight Manual 3. Manufacturer's Maintenance Manual 4. Aircraft Specifications
43
6-19 Define MAC Define LEMAC Define TEMAC
1. Mean Aerodynamic Chord - Chord drawn through the center of the wing plan area. 2. Leading edge of MAC 3. Trailing edge of MAC
44
6-20 Weight and Balance records are one of the ______ records for the aircraft.
Permanent
45
6-20 If the Weight and Balance records for an aircraft are lost or destroyed, the aircraft must be _____.
reweighed
46
6-20 The _____ is an imaginary vertical plane from which all horizontal measurements are taken for balance purposes.
Datum
47
6-20 The horizontal distance that an item of equipment is located from the datum is called the _____.
Arm
48
6-20 The _____ _____ _____ of an object is the point about which the object would balance if it were suspended from that point.
Center of Gravity
49
6-20 The _____ weight of an aircraft is the maximum authorized weight of the aircraft and its contents.
Maximum
50
6-20 The weight of an aircraft and engine, with all of the items of operating equipment which have fixed locations installed is known as the _____ weight.
Empty
51
6-20 The _____ _____ of an aircraft is its empty weight subtracted from its maximum allowable gross takeoff weight.
Useful load
52
6-20 How much fuel is considered to be part of the empty weight of an aircraft?
Unusable
53
6-20 The product of the weight of an item times its distance from the datum is the _____.
Moment
54
6-20 To find the balance point, divide the total _____ by the total _____.
Moment weight