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031 Mass & Balance

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Refer to figure.

You are about to depart for a domestic commercial flight, with an aircraft having a capacity of 2

flight crew members and 10 passengers. As part of your pre-flight calculations, you need to compute

the Traffic Load in accordance with standard passenger and baggage masses as defined in the annex. What is the Traffic Load, given the following information?

Flight crew: 2

Male passengers: 2

Female passengers: 3

Baggage: 6 pieces, with a total mass of 63 kg

Hand baggage: 3 pieces

Standard mass for a flight crew member: 85 kg

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Refer to figure.

Cross-check the information contained in the load/trim sheet of a Medium Range Jet Commercial Air Transport (MRJT) aeroplane. Which of the following masses/loads is correctly computed?

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Refer to figure.

A turboprop aeroplane having 36 passenger seats operates a domestic Commercial Air Transport flight carrying a rugby team of 28 sportsmen. Each of these players has one checked baggage and the average mass of these people is 115 kg. Determine the mass of the Traffic Load for this flight.

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If an aeroplane lands below its Max Structural Landing Mass, but above its Performance Limited

Landing Mass for the arrival airfield:

1) It might not have sufficient runway length to stop safely.

2) Tyre temperature limits could be exceeded.

3) It will increase structural fatigue.

4) Physical damage might be suffered as a result of the extra mass.

5) A go-around might not be achievable.

The combination regrouping all the correct statements is:

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Given:

Dry Operating Mass: 29 800 kg

Maximum Take-Off Mass: 52 400 kg

Maximum Zero-Fuel Mass: 43 100 kg

Maximum Landing Mass: 46 700 kg

Trip fuel: 4 000 kg

Fuel quantity at brakes release: 8 000 kg

The maximum traffic load is:

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Given the following information, what will be the expected Landing Mass at the destination?

Maximum structural take-off mass: 8 600 kg

Maximum structural landing mass: 8 600 kg

Zero Fuel Mass: 6 500 kg

Taxi Fuel: 15 kg

Contingency fuel: 110 kg

Alternate fuel: 600 kg

Final Reserve Fuel: 130 kg

Trip Fuel: 970 kg

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During dispatch calculations, you want to calculate the maximum possible Traffic Load and carry as

a minimum 13 800 kg of Block Fuel.

Determine the Allowed Traffic Load for your flight, given:

Allowed Take-off Mass: 71 240 kg

Maximum Zero Fuel Mass: 56 380 kg

Dry Operating Mass: 40 561 kg

Actual Traffic Load: 14 367 kg

Taxi Fuel: 274 kg

Assume NO restrictions on the Landing Mass.

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Determine the mass that must be entered into the loading chart for a fuel load of 170 litres, given: Fuel density: 0.78 kg/l

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What will be the effect on the longitudinal static stability, if the Centre of Gravity (CG) is located behind the aft CG limit?

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What is a possible consequence of loading an aircraft incorrectly so that the Centre of Gravity is positioned ahead of

the forward limit?

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