AEROPRAKT A32-iS-129-POH, Руководство по эксплуатации для пилотов

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AEROPRAKT-32 Pilot Operating Handbook A32-iS-129-POH
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7. Terrain
– CONTROL.
8. At safe altitude
– PULL YOKE GENTLY to level off.
9. G loads
– DO NOT 4g.
3.2.12 Alternator failure
Follow PRECAUTIONARY LANDING procedure, see section 3.2.6 .
3.2.13 Inadvertent spin
1. Rudder pedals
– FULLY AGAINST ROTATION.
2. Yoke/Stick
– PUSH slightly forward of neutral.
3. Rotation stopped
– rudder pedals NEUTRAL.
4. Speed reached 110 km/h (59 kts)
– PULL YOKE GENTLY to recover from diving.
Do not 4g and 240 km/h (130 kts)!
WARNING: Intentional spinning in A-32 is prohibited!
NOTE: In level flight and during turn stall warning is assured by the aerodynamic
characteristics of A-32
– gentle shaking of the airplane and yoke/stick due to the
starting airflow separation.
3.2.14 Inadvertent icing encounter
1. Abandon icing build-up area.
2. Icing build-up not stopped
– FOLLOW PRECAUTIONARY LANDING procedure, see
section 3.2.6 .
3.2.15 Loss of primary instruments
3.2.15.1 ASI failure due to full pressure line blockage
Signs of the blockage
– airspeed indicator reading either:
- does not change with changing airspeed in level flight or,
- reduces during a steady descent or,
- increases during a steady climb.
1. Airspeed indicator readings
– IGNORE.
2. In level flight
– SET THROTTLE to 4000-4500 rpm.
3. Altitude
– MAINTAIN.
4. In descent
– SET THROTTLE to IDLE.
5. Sink rate
– SET to 3 m/s (600 ft/min).
6. Follow PRECAUTIONARY LANDING procedure, see section 3.2.6 .
3.2.15.2 Altimeter, VSI and ASI failure due to static pressure line blockage
Signs of the blockage:
- altimeter and vertical speed indicator readings do not change with changing altitude or,
- airspeed indicator reading increases during a steady descent or,
- airspeed indicator reading reduces during a steady climb.
1. IGNORE altimeter, VSI and ASI readings.
2. Airplane attitude
– CONTROL by the position of the horizon line with relation to the wings
and engine cowling.