Zlin Aviation
Section 1
Maintenance Manual Aircraft Maintenance Manual
Issued: 01/02/2006
QAP-AMM-Rev02
Date of latest Revision: 23/01/2013
Page Number: 1-11
MOST REARWARD
Description
Weight
Arm
Moment
Main Landing Gear L
306,25
60,62
18564,875
Main Landing Gear R
306,25
60,62
18564,875
Pilot
170
66.90
11373
Fuel 18 Gallons
108
75,98
8205,84
Passenger
170
99,61
16933,7
Baggage Compartment
45
120,87
5439,15
Parachute
0
144,87
0
Tail Wheel
56
233,46
13073,76
Totals
1161,5
92155,2
Aircraft Gross Weight Limit 1235 lbs
Moment /Weight=CG
79,34
Datum Location-Front face of engine's propeller flange
Acceptable CG Range
74.0 - 80.7
Savage Classic Serial Number 0121
04/10/2007
Method
1. Multiply each item’s weight times its arm in inches to find the moment. Record each on its
respective line.
2. Add all the weights and moments and record each on its respective total line.
3. Divide the total moment by the total weight and the result is the C.G. Index in inches from
the datum line.
4. Determine that the airplane’s Loaded C.G. falls within the applicable limits (Forward C.G.
Limits and Aft C.G. Limits).
