Pelegrin Tarragon, Руководство по эксплуатации и полетной документации для пилотов

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Pilots Operating Handbook
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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).