Tecnam P2006T - 3. Weights and C.G.

Page 6 - 7
Section 6 – Weight and balance
WEIGHTS AND C.G.
4
th
Edition, Rev 0
3. WEIGHTS AND C.G.
C.G. position can be defined by means of the chart below.
The pilot is responsible for ensuring the correct useful load loading.
500
200
0
1200
200
160
240
280
320
340
380
420
460
140
180
220
260
300
360
400
440
480
40
80
120
160
40
80
120
160
200
900
1000
1100
40
80
0
0
40
80
31% MAC
16,5% MAC
120
(kg)
(kg
)
(kg) (kg)
C.G.Limits
FUEL MASS
BAGGAGE
FLIGHT MASS
MASS & BALANCE
LOADING CONDITION
23% MAC
88
176 265
353
441
0
0
0
0
88
176 265
353
441
88
176 265
88
176
1984
2204
2425
2645
(lbs)
(lbs)
(lbs)
(lbs)
(lbs)
1180 kg (2600 lbs)
3616
3472
3327
3182
3038
2893
2748
2604
2459
2315
2170
2025
1881
1736
1591
1447
1302
1157
1013
ft lbs
m kg
EMPTY A/C MOMENT TO DATUM
OCCUPANTS
FRONT SEATS
MASS
OCCUPANTS
REAR SEATS
MASS
(kg)
MASS
1230 kg (2712 lbs)
Figure 1
Example
A/C empty mass moment 378 kgm
A/C empty mass 790 kg
Occ. front seats 160 kg
Occ. rear seats 140 kg
Fuel 72kg
Baggage 18 kg
A/C T.O. weight 1180kg