GsPilot

1/30

Question ID: 101416

Basic Empty Mass 5300 kg
Dry Operating Mass 5500 kg
Zero Fuel Mass 5980 kg
Take-off Mass 7980 kg
What is the Useful Load (UL)?

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A

2000 kg

B

2680 kg

C

480 kg

D

2480 kg

2/30

Question ID: 101202

Consider a conventional aircraft with three wheels

The nose jack is located 161 inches aft of the datum

The main wheel jacks are located 775 inches aft of the datum

After weighing the following results are reported nose jack 2 300 lb each main wheel jack 19 300 lb

What is the basic empty mass of the aircraft and the center of gravity from the datum?

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A

BEM 21 600 lb, CG 709.6 in

B

BEM 40 900 lb, CG 722.3 in

C

BEM 21 600 lb, CG 0.71 in

D

BEM 40 900 lb, CG 740.5 in

3/30

Question ID: 101530

Using the graph, and given the following parameters, what is the loaded Centre of Gravity of this aircraft?

BEM 1100 kg

Moment 3.10.

Front pax 150 kg

Rear pax 200 kg

Fuel 200 kg

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A

3.10 m

B

2.98 m

C

3.01 m

D

2.94 m

4/30

Question ID: 101248

The mass and center of gravity of an aircraft must be established by actual weighing?

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A

By the owner operator before the first flight of the day

B

By the engineers before commencing service

C

By the pilot on entry of aircraft into service

D

By the operator prior to initial entry of aircraft into service

5/30

Question ID: 101492

An aircraft has a loaded mass of 5 500 lbs. The CG is 22 inches aft of the datum. A passenger, mass 150 lbs, moves aft from row 1 to row 3 a distance of 70 inches. What will be the new position of the CG (assuming all dimensions aft of the datum)?

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A

23.9 inches

B

26.3 inches

C

22.9 inches

D

21.1 inches

6/30

Question ID: 101200

If nose wheel moves aft during gear retraction, how will this movement affect the location of the center of gravity (cg) on the aircraft?

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A

The cg location will change, but the direction cannot be told the information given

B

It will not affect the cg location

C

It will cause the cg to move aft

D

It will cause the cg to move forward

7/30

Question ID: 101562

Given:
Basic Empty Mass = 5300 kg
Dry Operating Mass = 5500 kg
Zero Fuel Mass = 5980 kg
Take-off Mass = 7980 kg

What is the traffic load?

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A

2000 kg

B

2480 kg

C

2680 kg

D

480 kg

8/30

Question ID: 101402

The Zero Fuel Mass and the Dry Operating Mass?

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A

Differ by the value of the Traffic Load mass

B

Differ by the sum of the mass of usable fuel plus Traffic Load mass

C

Are the same value

D

Differ by the mass of usable fuel

9/30

Question ID: 101440

A mass of 500 kg is loaded at a station which is located 10 meters behind the present center of gravity and 16 meters behind the datum. The moment for that mass used in the loading manifest is (Assume g=10 m/s 2)?

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A

130000 Nm

B

80000 Nm

C

50000 Nm

D

30000 Nm

10/30

Question ID: 101534

Given the following
Maximum structural take-off mass 48000 kg
Maximum structural landing mass 44000 kg
Maximum zero fuel mass 36000 kg
Taxi fuel 600 kg
Contingency fuel 900 kg
Alternate fuel 800 kg
Final reserve fuel 1100 kg
Trip fuel 9000 kg
The actual TOM can never be higher than

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A

48400 kg

B

47800 kg

C

53000 kg

D

48000 kg

11/30

Question ID: 101152

The Maximum Zero Fuel Mass (MZFM)? Select 3 options from the below

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A

Is calculated for a maximum load factor of +3.5g

B

Is based on the maximum permissible bending moment at the wing root

C

Is a regulatory limitation

D

Is defined under the assumption that fuel is consumed from the inner wing tanks first

E

Is defined under the assumption that fuel is consumed from the outer wing tanks first

12/30

Question ID: 101469

Without the crew, the mass and longitudinal CG position of the aircraft are 6 000 kg and 4.70 m?

The mass of the pilot 90kg
The mass of the copilot 100kg
The mass of the flight engineer 80kg
With the crew, the mass and longitudinal CG position of the aircraft are?

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A

6270 kg and 5.012 m

B

6270 kg and 4.796 m

C

6270 kg and 4.61 m

D

6270 kg and 4.594 m

13/30

Question ID: 101175

In cruise flight, a center of gravity moving aft will?

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A

Decrease longitudinal static stability

B

Not change the maneuverability

C

Increase longitudinal static stability

D

Have no effect on longitudinal static stability

14/30

Question ID: 101258

Crew baggage is considered to be?

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A

Bulk load

B

Variable load

C

Palletized load

D

Containerized cargo load

15/30

Question ID: 101302

A pallet having a freight platform which measures 200 cm x 250 cm has a Total Mass of 300 kg.

The pallet is carried on two ground supports each measuring 20 cm x 200 cm. Using the Loading Manual for the transport aeroplane.

Calculate how much mass may be added to, or must be off loaded from, the pallet in order for the load intensity to match the maximum permitted distribution load intensity for lower deck forward cargo compartment?

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A

285.5 kg may be added

B

28.5 kg must be off loaded

C

28.5 kg may be added

D

158.3 kg must be off loaded

16/30

Question ID: 101451

For the transport aeroplane the Moment (Balance) Arm (B.A.) for the forward hold centroid is?

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A

421.5 inches

B

257 inches

C

314.5 inches

D

367.9 inches

17/30

Question ID: 101176

What are the effects on stability and controllability of a CG behind the aft limit? Longitudinal stability?

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A

And controllability is increased

B

Is increased and controllability is reduced

C

Is reduced and controllability is increased

D

And controllability is reduced

18/30

Question ID: 101261

The actual Take-off Mass is equivalent to?

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A

Dry Operating Mass plus take-off fuel and the Traffic Load

B

Dry Operating Mass plus the take-off fuel

C

Actual Zero Fuel Mass plus the Traffic Load

D

Actual Landing Mass plus the take-off fuel

19/30

Question ID: 101303

The maximum floor loading for a cargo compartment in an aeroplane is given as 750 kg per square meter. A package with a mass of 600 kg is to be loaded. Assuming the pallet base is entirely in contact with the floor, which of the following is the minimum size pallet that can be used?

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A

40 cm Ã-300 cm

B

30 cm Ã-200 cm

C

30 cm A-300 cm

D

40 cm Ã-200 cm

20/30

Question ID: 101435

Dry Operating Mass (DOM) 3500lbs
Takeoff fuel 500lbs
Passenger Mass 400lbs
Cargo + baggage 1 250lbs
Maximum structural TOM 5850lbs
Performance limited TOM 5200lbs
To bring the TOM into the regulated TOM limits the Traffic Load (TL) must be reduced by?

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A

250 lbs

B

200 lbs

C

450 lbs

D

650 lbs

21/30

Question ID: 101540

Assume Aircraft actual mass 4750 kg Centre of gravity at station 115.8

What will be the new position of the center of gravity if 100 kg is moved from the station 30 to station 120?

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A

Station 117.69

B

Station 118.33

C

Station 118.25

D

Station 120.22

22/30

Question ID: 101141

A pilot is taking-off from an airport with a light aircraft which has a maximum structural take-off mass of 3 250 lb and 25 lb of taxi fuel can be added. It is a hot summer day and the maximum all up mass (MAUM) is 3 100 lb. What is the maximum ramp mass in these conditions?

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A

3250 lb

B

3100 lb

C

3125 lb

D

3275 lb

23/30

Question ID: 101463

The interval between 2 fleet mass evaluations must not exceed?

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A

24 months

B

12 months

C

48 months

D

36 months

24/30

Question ID: 101489

The planned Take-off Mass of an aeroplane is 180 000 kg, with its center of gravity located at 31% MAC (Mean Aerodynamic Chord) Distance from reference point to leading edge = 14 m
Length of MAC = 4.6 m.
Shortly prior to engine start, the local staff informs the crew that an additional load of 4 000 kg must be loaded in cargo 1 (located at 2.73 m aft of the reference point) After loading this cargo, the new center of gravity location will be?

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A

25%

B

34%

C

28%

D

37%

25/30

Question ID: 101263

The Dry Operating Mass (DOM) includes?

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A

Crew and crew baggage, catering, removable passenger service equipment, potable water and lavatory chemicals

B

Unusable fuel and reserve fuel

C

Fuel and passengers’ baggage and cargo

D

Passengers baggage and cargo

26/30

Question ID: 101332

The Zero Fuel Mass of an aeroplane is always?

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A

The Take-off Mass minus the wing fuel mass

B

The Take-off Mass minus the mass of take-off fuel

C

The Take-off Mass minus the fuselage fuel mass

D

The Maximum Take-off Mass minus the take-off fuel mass

27/30

Question ID: 101158

The principle of the index method is?

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A

To round all values for easier and much faster calculation

B

To refer all the items of an aircraft to a position which is called BA (Balance Arm)

C

To calculate the center of gravity position (CG) and stabilizer trim setting without calculating the load sheet

D

To divide high magnitude moments by a constant and thereby simplify calculations by decreased values

28/30

Question ID: 100292

Determine the ZFM and the Useful load, given:

BEM: 1799 lbs

Pilot: 125 lbs

Front seat pax: 150 lbs

Rear seat pax: 110 lbs

Fwd baggage compartment: 175 lbs

Aft baggage compartment: 100 lbs

Flight crew equipment: 120 lbs

Block fuel: 90 USG

Taxi Fuel: 3 USG

Trip Fuel: 50 USG

Fuel density: 6lb/USG

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A

ZFM is 2579 lbs and the Useful load is 1075 lbs

B

ZFM is 2561 lbs and the Useful load is 1075 lbs

C

ZFM is 2561 lbs and the Useful load is 1057 lbs

D

ZFM is 2579 lbs and the Useful load is 1057 lbs

29/30

Question ID: 101179

Overloading has the following effects on performance?

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A

Reduced takeoff and landing distance, increased VNE and reduced rate of climb

B

Increased takeoff and landing distance, reduced rate of climb and increased fuel consumption

C

Reduced takeoff and landing distance, increased VNE and increased fuel consumption

D

Increased takeoff and landing distance, increased rate of climb and increased fuel consumption

30/30

Question ID: 101389

If an aircraft weight = 2000 kg and 400 kg of freight is added to a hold 2m aft of the present CG position, the movement of the CG is?

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A

0.33m forward

B

0.4m aft

C

0.4m forward

D

0.33m aft

Question ID: 101416

Basic Empty Mass 5300 kgDry Operating Mass 5500 kgZero Fuel Mass 5980 kgTake-off Mass 7980 kgWhat is the Useful Load (UL)?

A

B

C

D

Question ID: 101202

A

B

C

D

Question ID: 101530

Using the graph, and given the following parameters, what is the loaded Centre of Gravity of this aircraft? BEM 1100 kg Moment 3.10. Front pax 150 kg Rear pax 200 kg Fuel 200 kg

A

B

C

D

Question ID: 101248

The mass and center of gravity of an aircraft must be established by actual weighing?

A

B

C

D

Question ID: 101492

An aircraft has a loaded mass of 5 500 lbs. The CG is 22 inches aft of the datum. A passenger, mass 150 lbs, moves aft from row 1 to row 3 a distance of 70 inches. What will be the new position of the CG (assuming all dimensions aft of the datum)?

A

B

C

D

Question ID: 101200

If nose wheel moves aft during gear retraction, how will this movement affect the location of the center of gravity (cg) on the aircraft?

A

B

C

D

Question ID: 101562

Given:Basic Empty Mass = 5300 kg Dry Operating Mass = 5500 kg Zero Fuel Mass = 5980 kg Take-off Mass = 7980 kg What is the traffic load?

A

B

C

D

Question ID: 101402

The Zero Fuel Mass and the Dry Operating Mass?

A

B

C

D

Question ID: 101440

A mass of 500 kg is loaded at a station which is located 10 meters behind the present center of gravity and 16 meters behind the datum. The moment for that mass used in the loading manifest is (Assume g=10 m/s 2)?

A

B

C

D

Question ID: 101534

Given the followingMaximum structural take-off mass 48000 kgMaximum structural landing mass 44000 kgMaximum zero fuel mass 36000 kgTaxi fuel 600 kgContingency fuel 900 kgAlternate fuel 800 kgFinal reserve fuel 1100 kgTrip fuel 9000 kgThe actual TOM can never be higher than

A

B

C

D

Question ID: 101152

The Maximum Zero Fuel Mass (MZFM)? Select 3 options from the below

A

B

C

D

E

Question ID: 101469

Without the crew, the mass and longitudinal CG position of the aircraft are 6 000 kg and 4.70 m?The mass of the pilot 90kgThe mass of the copilot 100kgThe mass of the flight engineer 80kg With the crew, the mass and longitudinal CG position of the aircraft are?

A

B

C

D

Question ID: 101175

In cruise flight, a center of gravity moving aft will?

A

B

C

D

Question ID: 101258

Crew baggage is considered to be?

Basic Empty Mass 5300 kg
Dry Operating Mass 5500 kg
Zero Fuel Mass 5980 kg
Take-off Mass 7980 kg
What is the Useful Load (UL)?

Using the graph, and given the following parameters, what is the loaded Centre of Gravity of this aircraft?

BEM 1100 kg

Moment 3.10.

Front pax 150 kg

Rear pax 200 kg

Fuel 200 kg

Given:
Basic Empty Mass = 5300 kg
Dry Operating Mass = 5500 kg
Zero Fuel Mass = 5980 kg
Take-off Mass = 7980 kg

What is the traffic load?

Given the following
Maximum structural take-off mass 48000 kg
Maximum structural landing mass 44000 kg
Maximum zero fuel mass 36000 kg
Taxi fuel 600 kg
Contingency fuel 900 kg
Alternate fuel 800 kg
Final reserve fuel 1100 kg
Trip fuel 9000 kg
The actual TOM can never be higher than

Without the crew, the mass and longitudinal CG position of the aircraft are 6 000 kg and 4.70 m?

The mass of the pilot 90kg
The mass of the copilot 100kg
The mass of the flight engineer 80kg
With the crew, the mass and longitudinal CG position of the aircraft are?

Dry Operating Mass (DOM) 3500lbs
Takeoff fuel 500lbs
Passenger Mass 400lbs
Cargo + baggage 1 250lbs
Maximum structural TOM 5850lbs
Performance limited TOM 5200lbs
To bring the TOM into the regulated TOM limits the Traffic Load (TL) must be reduced by?

Assume Aircraft actual mass 4750 kg Centre of gravity at station 115.8

What will be the new position of the center of gravity if 100 kg is moved from the station 30 to station 120?