Tecnam P2008 - 3.3 Weight and Balance

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3.3 Weight and Balance
In order to compute the weight and balance of this aircraft, we have provided the following loading charts. This will reduce
the amount of math you need. To compute weight and balance use the formula:
Weight * Arm = Moment.
Pilot & Passenger
Fuel Baggage
Weight
(lbs)
Moment
(lbs x in)
Weight
(lbs)
Moment
(lbs x in)
Gallons
Weight
(lbs)
Moment
Weight
(lbs)
Moment
(lbs x in)
10
748
260
19448
1
6,26
544
5
476
20
1496
270
20196
2
12,52
1089
10
952
30
2244
280
20944
3
18,78
1633
15
1427
40
2992
290
21692
4
25,04
2178
20
1903
50
3740
300
22440
5
31,3
2722
25
2379
60
4488
310
23188
6
37,56
3267
30
2855
70 5236 320 23936 7 43,82 3811 35 3331
80
5984
330
24684
8
50,08
4355
40
3806
90
6732
340
25432
9
56,34
4900
44
4187
100
7480
350
26180
10
62,6
5444
110
8228
360
26928
11
68,86
5989
120
8976
370
27676
12
75,12
6533
130
9724
380
28424
13
81,38
7078
140
10472
390
29172
14
87,64
7622
150
11220
400
29920
15
93,9
8166
160
11968
410
30668
16
100,16
8711
170
12716
420
31416
17
106,42
9255
180
13464
430
32164
18
112,68
9800
190 14212 440 32912 19 118,94 10344
200
14960
450
33660
20
125,2
10889
210
15708
460
34408
21
131,46
11433
220
16456
470
35156
22
137,72
11978
230
17204
480
35904
23
143,98
12522
240
17952
490
36652
24
150,24
13066
250
18700
500
37400
25
156,5
13611
26
162,76
14155
Meter
Inches
PAX 1.900 74,80
FUEL
2.209
86,97
BAGGAGE
2.417
95,16
To compute weight and balance: