Standard Operating Procedures
L410 UVP-E20
Document No.:
SOP-L410-0
Page BB -2
Rev: 0
Date: Jul 17
Prepared by: TRI
Checked by: TM
WEIGHT AND BALANCE LOADING FOR
19 PASSENGER CONFIGURATION
Payload
(kg)
Arm (m) Moment (kg.m)
F.S. Forward baggage (max.100 kg)
-1.333
F.S. CREW seats
0.103
F.S. Seat Row 1
1.235
F.S. Seat Row 2
1.995
F.S. Seat Row 3
2.755
F.S. Seat Row 4
3.515
F.S. Seat Row 5
4.275
F.S. Seat Row 6
5.035
F.S. Seat Row 7
5.785
F.S. AFT baggage (max.100 kg)
6.650
TOTAL PAYLOAD AND MOMENT
EMPTY WEIGHT AND MOMENT
ZERO FUEL WEIGHT AND MOMENT
MAX. ALLOWABLE FUEL MAIN TANKS
3.13
MAX. ALLOWABLE FUEL TIP TANKS
2.67
ACT.FUEL MAIN TANKS
3.13
ACT.FUEL TIP TANKS
2.67
TAKE OFF WEIGHT AND MOMENT
14.11
FUELBURN MAIN TANKS
3.13
FUELBURN TIP TANKS
2.67
LANDING WEIGHT AND MOMENT
36.92
Take-Off
Landing
CENTRE OF GRAVITY AFT LIMIT
CENTRE OF GRAVITY FWD LIMIT
ACTUAL CENTRE OF GRAVITY POSITION
Summary of Contents for L410 UVP-E20
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