Standard Operating Procedures
L410 UVP-E20
Document No.:
SOP-L410-0
Page BB -4
Rev: 0
Date: Jul 17
Prepared by: TRI
Checked by: TM
PAYLOAD AND FUEL MOMENT FOR 19 PASSENGER CONFIGURATION
Moments listed are kg.m for weights located as shown
Payload weight
(kg)
20
40
60
80
100
120
140
160
180
200
220
240
260
280
300
F.S. 0.103 m Crew
seats
2.1
4.1
6.2
8.2
10.3
12.4
14.4
16.5
18.5
20.6
22.7
-
-
-
-
F.S. 1.235 m seat
Row 1
24.7
49.4
74.1
98.8
123.5
148.2
172.9
197.6
222.3
247.0
271.7 296.4 321.1 345.8 370.5
F.S. 1.995 m seat
Row 2
39.9
79.8
119.7
159.6
199.5
239.4
279.3
319.2
359.1
399.0
438.9 478.8 518.7 558.6 598.5
F.S. 2.755 m seat
Row 3
55.1
110.2
165.3
220.4
275.5
330.6
385.7
440.8
495.9
551.0
606.1 661.2 716.3 771.4 826.5
F.S. 3.515 m seat
Row 4
70.3
140.6
210.9
281.2
351.5
421.8
492.1
562.4
632.7
703.0
773.3 843.6 913.9 984.2 1,054.5
F.S. 4.275 m seat
Row 5
85.5
171.0
256.5
342.0
427.5
513.0
598.5
684.0
769.5
855.0
940.5 1,026.0 1,111.5 1,197.0 1,282.5
F.S. 5.035 m seat
Row 6
100.7
201.4
302.1
402.8
503.5
604.2
704.9
805.6
906.3 1,007.0
-
-
-
-
-
F.S. 5.785 m seat
Row 7
115.7
231.4
347.1
462.8
578.5
694.2
809.9
925.6 1,041.3 1,157.0
-
-
-
-
-
Baggage weight (lb)
10
20
30
40
50
60
70
80
90
100
110
120
130
140
150
F.S. -1.333 m Forward -13.3
-26.7
-40.0
-53.3
-66.7
-80.0
-93.3
-106.6 -120.0 -133.3
-
-
-
-
-
Baggage
F.S. 6.650 m Aft
Baggage
66.5
133.0
199.5
266.0
332.5
399.0
465.5
532.0
598.5
665.0
731.5
798.0 864.5 931.0 997.5
Fuel weight (lb)
100
200
300
400
500
600
700
800
900
1,000
F.S. 3.134 m Fuel
Main
313.4 626.8
940.2 1,253.6 1,567.0 1,880.4 2,193.8 2,507.2 2,820.6 3,134.0
F.S. 2.674 m Fuel Tip 267.4 534.8
802.2
-
-
-
-
-
-
-
WARNING
IT IS THE RESPONSIBILITY OF THE PILOT TO MAKE SURE THAT THE AIRPLANE IS
LOADED CORRECTLY. OPERATION OUTSIDE OFPRESCRIBED WIEGHT AND BALANCE
LIMITATIONS COULD RESULT INAN ACCIDENT AND SERIOUS FATAL INJURY.
Summary of Contents for L410 UVP-E20
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