31-04. MASS AND BALANCE DETAILS OF AIRCRAFT
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1. From the attached data sheet, what is the forward CG limit for an aircraft with a mass of 3.500 Ib?

2. Longitudinal CG location is normally expressed:
3. What is the centre of gravity position of the aircraft in the diagram, given:
Left main: 1.620 kg
Right main: 1.632 kg
Nose: 640 kg

4. From the medium range twin jet data sheet give the distance of body station 727F from the front spar:

5. An aircraft may be weighed: