SECTION 6 – WEIGHT AND BALANCE
6.1
Introduction
This section details the payload range within which the aircraft G - _ _ _ _ may
be safely operated.
6.2
Permitted Cockpit Loads
Whenever the empty weight changes following periodic weight checks,
modification or repair, revised values for the Empty Weight must be entered in
the table below. This table is specific to the aeroplane to which this POH
applies.
Procedures for weighing the aircraft and the calculation method for establishing
the permitted payload range are contained in the Maintenance Manual for the
EV-97 teamEUROSTAR UK.
Maximum Permitted Crew Weight for given Baggage and Fuel Loads, kg.
Date
Empty
weight
kg
Empty
CG
posn.
mm
AOD
FUEL LOAD
Approved
Fuel gauge
1
3/4
1/2
1/4
Date
Signature
Fuel volume
62 litres
47litres
31 litres
15 litres
Fuel weight
45 kg
33kg
22 kg
11 kg
B
A
G
G
A
G
E
max. 15kg
½ = 8 kg
None
max. 15kg
½ = 8 kg
None
max. 15kg
½ = 8 kg
None
max. 15kg
½ = 8 kg
None
POH/EUR/01
Issue 2
Page 34 of 42
Summary of Contents for EV-97 teamEUROSTAR UK
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