Mahindra GIPPSAERO GA8-TC 320, Operating Handbook

Page: 101 / 148

C01-01-08 01 Aug 2011 Page 6-17
Section 6
Weight & Balance /
Model GA8-TC 320 Equipment List
GA8 / GA8-TC 320 SERIES LOADING ENVELOPE CHART - FREIGHTER CONFIGURATION (METRIC)
WEIGHT (kg) ARM (mm) MOMENT (kg.mm)
Row 1
X
965 mm
=
Zone 1A
X
1524 mm
=
Zone 1B
X
1968 mm
=
Zone 1C
X
2861 mm
=
Combined Zone 1
Max: 680 kg
Zone 2
Max: 113 kg
X
3763 mm
=
Aft Luggage Bin
Max: 22 kg
X
4623 mm
=
ZERO FUEL
(Sum of Weight Column) (Sum of Moment Column)
ZERO FUEL CENTRE OF GRAVITY
- Division of Zero Fuel Moment
by Zero Fuel Weight
Take-Off Fuel
X
1715 mm
=
TAKE-OFF
Max: 1814 kg (Sum of Zero Fuel Weight & Take-Off Fuel)
TAKE-OFF CENTRE OF GRAVITY
- Division of Take-Off Moment
by Take-Off Weight
Trip Fuel
LANDING
- Deduct Trip Fuel from Take-Off Weight
Max: 1814 kg
Aircraft Basic
Weight, Arm &
Moment.
Centre of Gravity Location (mm)
W
eight (kg)
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
1900
2000
1000 1050 1100 1150 1200 1250 1300 1350 1400 1450 1500 1550 1600 1650 1700 1750 1800
Series1
Centre of Gravity Envelope
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
1900
2000
1000 1050 1100 1150 1200 1250 1300 1350 1400 1450 1500 1550 1600 1650 1700 1750 1800
Series1
900
1000
1100
1200
1300
1400
1500
1600
1700
1800
1900
2000
1000 1050 1100 1150 1200 1250 1300 1350 1400 1450 1500 1550 1600 1650 1700 1750 1800
Series1
(Sum of Zero Fuel Moment & Take-Off Fuel Moment)