Pilots Operating Handbook
45/76
YL-MFG
Revision 7, Issue 1
4/6/2016
Loading Table 1 (Sample Problem with Very FWD CG)
ITEM DESCRIPTION
WEIGHT
CG ARM
MOMENT
1 Basic empty weight
404
3.515
1418.88
2 Fuel (@ 0.72 kg/l)
- Standard fuel 85l max.
64
3.492
223.49
- Reduced fuel, e.g., 60l
3.492
3 Pilot
95
3.488
331.36
4 Passenger
-
4.272
-
5 Baggage
17
4.955
84.24
6 Ramp Weight
580
3.548
2057.97
7 Fuel for start, taxi, run-up
-5
3.492
-17.45
8 Take-Off Weight
575
3.549
2040.52
9 Trip fuel
-10
3.492
-34.9
10 Landing Weight
565
3.550
2005.62
This sample forward loading problem puts the sample airplane to the forward limit of the CG range
(3.50-3.76m).
Loading Table 2 (Sample Problem with Very AFT CG)
ITEM DESCRIPTION
WEIGHT
CG ARM
MOMENT
1 Basic empty weight
404
3.515
1418.88
2 Fuel (@ 0.72 kg/l)
- Standard fuel 85l max.
3.492
- Reduced fuel, e.g., 50l
35
3.492
122.22
3 Pilot
62
3.488
216.26
4 Passenger
80
4.272
341.76
5 Baggage
4.955
6 Ramp Weight
581
3.613
2099.12
7 Fuel for start, taxi, run-up
-5
3.492
-17.46
8 Take-Off Weight
576
3.614
2081.66
9 Trip fuel
-25
3.492
-87.30
10 Landing Weight
551
3.620
1994.36
This sample extreme aft loading problem puts the sample airplane well within the CG range (3.50-
3.76m).
