AEROPRAKT-32 Pilot Operating Handbook
A32-103-POH
62
touching the ground before the other. During the landing roll the nose wheel shall be kept
lifted as long as possible and the heading shall be maintained using the rudder pedals.
Immediately before the nose wheel is finally touching the ground the rudder pedals shall
be set neutral in order to prevent the side load on the nose leg.
Total time of crosswind takeoff and landing training
– 30 minutes. Number of flights – 1.
Number of landings
– 6.
9.8.9 Flights with imitated engine failure
The emergency procedures in case of engine failure are described in the sections
. When imitating the engine failure it is recommended to reduce the engine RPM to
idle. While doing that it should be kept in mind that sink rate with the engine stopped is by
100 fpm higher than that with the engine at idle because of the remaining propeller thrust.
Special attention shall be paid to maintaining the airspeed. The imitated engine failures
shall be done at every leg of the airfield circuit.
Total time of imitated engine failure training
– 30 minutes. Number of flights – 1. Number of
landings
– 4.
9.9 Airplane Owner Feedback to Manufacturer
To ensure continued operational safety of the airplane the airplane owner(s) must keep in
contact with the airplane manufacturer and report all issues associated with the
operational safety of the airplane to the airplane manufacturer. The Feedback Form for
operational safety reporting is contained in the Aircraft Maintenance Manual.
Besides airplane owner(s) must inform the airplane manufacturer about the changes in
their address or airplane ownership rights. No particular form for that is prescribed.
Information about the change of address or airplane ownership rights may be delivered to
the airplane manufacturer in writing by fax or e-mail. This information must be accurate
and sufficiently detailed for keeping contact between the airplane manufacturer and owner.
Содержание A32-103-POH
Страница 25: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 25 No Equipment description and Part No Weight kg CG arm m...
Страница 29: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 29 Fig 3 Fuel system schematic...
Страница 36: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 36 Fig 10 Engine pre start mixture control...
Страница 38: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 38 Fig 12 Brake control system...
Страница 43: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 43 Fig 15 Wiring diagram of A 32 electrical system main...
Страница 48: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 48 Fig 21 Wiring diagram for installation of PTT buttons...
Страница 50: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 50 Fig 22 Recovery system...
