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031 Mass & Balance
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The total mass limit of a light twin is equal to 3 200 lb. The pilot weighs 200 lb and the combined mass of the passengers and their baggages is 650 Ib. Assuming a Dry Operating Mass of 1 742 Ib, how much fuel can be loaded?
Refer to figure
During dispatch, you perform the Mass and Balance calculations. Given the following information, calculate the Take-Off Mass CG in Inches aft of the datum. Basic Empty Mass: 2 635 Ib Basic Empty Mass Moment: 204 397.5 in.Ib Front Seat Occupant's Mass: 93 lb Front Seat Occupant's Arm: 78 in Aft Seat Occupant's Mass: 186 Ib Aft Seat Occupant's Arm: 119 in Block Fuel: 850 Ib Taxi Fuel: 320 lb
An aeroplane has a Basic Empty Mass of 1000 kg, located at station 92.
The pilot's mass is 80 kg, located at station 100.
The fuel mass is 120 kg, located at station 130.
The length of the MAC is 60 inches, 0% MAC is at station 80.
What is the centre of gravity location of the loaded aeroplane in % MAC?
Refer to figure.
The centre of gravity of an aeroplane is at 25% of the Mean Aerodynamic Chord. This means that the centre of gravity of the aeroplane is situated at 25% of the length of:
What are the effects on stability and controllability of a CG behind the aft limit? Longitudinal stability..
Before departure for a flight, the load controller presents to you cargo documents for boxes containing spare parts. These boxes have a total mass of 4500 kg. If you accept all the boxes, given the following information, what will be the Underload/Overload?
Allowed Take-Off Mass: 76720 kg
Maximum Zero Fuel Mass: 62731 kg
Operating Mass: 58799 kg
Actual Zero Fuel Mass: 55063 kg
Actual Traffic Load (without the boxes): 12563 kg
Take-off fuel: 16299 kg
Disregard changes in fuel due to the increase in Total Mass.
Consider no restrictions on structural limits and Allowed Landing Mass.
Refer to figure.
Using CAP 696 Figure 4.3 determine the moment change when flaps are retracted from 40° to 15°.
Refer to figure… A commercial Air transport flight is scheduled with a planned Dry operating mass (DOM) of 35350 Kg and the associated Dry Operating Index (DOl) is 47. If one instructor pilot is added in the flight deck and 150 kg of catering are offloaded from the aft galley, the new DOM and DOI are respectively...