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Flugzeugbau Ventus-2C - Page 92

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SCHEMPP-HIRTH FLUGZEUGBAU GmbH., KIRCHHEIM/TECK
Ventus-2c FLIGHT MANUAL
WEIGHT AND BALANCE LOG SHEET
(Loading chart)
for Ser.-No.:
Date of weighing
18 m
Empty mass
(kg)
15 m
Equipment list dated
18m
Empty mass c/g
position (mm)
aft of datum
15 m
Max. (kg) *)
Seat load
(pilot incl.
parachute)
Min. (kg)
Max. useful load in
fuselage (kg)
Inspector
Signature
Stamp
NOTE
*) Maximum seat load = Maximum useful load in
(Pilot & parachute) fuselage but not more than
110 kg (242.5 lb)
For the determination of water ballast in the wing tanks refer to page 6.2.5.
For the determination of water ballast in the fin tank refer to page 6.2.6 through
6.2.8.
November 2003
Revision -- 6.2.3

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