AEROPRAKT-32 Pilot Operating Handbook
A32-iS-129-POH
25
C.G. position for the maximum take-off weight:
Item
Weight,
kg/lbs
×
CG arm,
m/inch
=
Moment,
kg×m/lbs×inch
Empty airplane
348.8/769.1
×
1.615/63.6
=
563.5/48 914
Crew (2×78.0 kg)
156.0/344.0
×
1.663/65.5
=
259.4/22 521
Baggage
30.0/66.2
×
2.320/91.3
=
69.6/6 042
Fuel (2×45 l)
64.8/142.9
×
1.960/77.2
=
127.0/11 026
Total:
599.6/1 322.1
1019.5/88 503
X
CG
= Total moment / Total weight
=
1.700/66.9
Note
: X
CG
must be between 1.529 m and 1.780 m (19% and 37% MAC) as shown in
6.2 Installed equipment list
This subsection contains a table with the list of the installed optional equipment affecting
weight and balance of the aircraft. It is responsibility of the aircraft owner/operator that any
such equipment installed in the aircraft after the date of its manufacture is listed in the table
below.
No.
Equipment description and Part No.
Weight, kg CG arm, m
Содержание A32-iS-129-POH
Страница 26: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 26 No Equipment description and Part No Weight kg CG arm m...
Страница 36: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 36 Fig 10 Brake control system...
Страница 41: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 41 Fig 13 Wiring diagram of A 32 electrical system main...
Страница 47: ...AEROPRAKT 32 Pilot Operating Handbook A32 iS 129 POH 47 Fig 19 Recovery system...