AEROPRAKT-32 Pilot Operating Handbook
A32-060-POH
22
6
Weight and Balance and Equipment List
This section contains information about weight and balance requirements for the safe
operation of the airplane. It is responsibility of the pilot in command to ensure before every
flight that weight and balance of the airplane remains within the specified limits. Failure to
do so may cause deterioration in airplane's flight performance and stability characteristics
and, as consequence, lead to unsafe operation.
6.1 Weight and Balance Chart
This subsection contains weighing and CG location data of the aircraft in configuration
“as
built
”. Any permanent modification of the aircraft configuration (such as replacement,
removal/installation of any parts or/and equipment) essentially affecting those data shall be
accounted for in this weight and balance chart by appropriate revisions of this subsection
data.
Weight readings at: front wheel ............... 143.0 lb.
left wheel .................. 289.5 lb.
right wheel ................ 291.7 lb.
Total empty weight: ...................... 724.2 lb.
Total maximum take-off weight
….1323 lb.
Fig. 2
Empty C.G. position from the datum (engine flange):
𝑥
𝐶𝐺
𝑒𝑚𝑝𝑡𝑦
=
(64.9 × 0.588 + (131.3 + 132.3) × 1.831)
64.9 + 131.3 + 132.3
= 1.585 𝑚.
Содержание A32
Страница 24: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 24 No Equipment description and Part No Weight kg CG arm m...
Страница 28: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 28 Fig 3 Fuel system schematic...
Страница 37: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 37 Fig 12 Brake control system...
Страница 42: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 42 Fig 15 Wiring diagram of A 32 electrical system main...
Страница 43: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 43 Fig 16 Block diagram of Garmin G3X system installation...
Страница 52: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 52 Fig 25 Recovery system...