AEROPRAKT A-32L, Руководство по эксплуатации для пилотов

Страница: 15 / 60

AEROPRAKT-32L Pilot Operating Handbook A32L-FO-POH
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 (68 mph, 59 kts) — PULL YOKE GENTLY to recover from
diving.
Do not 4g and 230 km/h (143 mph, 124 kts)!
WARNING: Intentional spinning in A-32L is prohibited!
NOTE: In level flight and during turn stall warning is assured by the aerodynamic
characteristics of A-32L — gentle shaking of the airplane and yoke due to the starting
airflow separation.
3.2.14 Inadvertent icing encounter
5. Abandon icing build-up area.
6. 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.
7. Airspeed indicator readings — IGNORE.
8. In level flight — SET THROTTLE to 4000-4500 rpm.
9. Altitude — MAINTAIN.
10. In descent — SET THROTTLE to IDLE.
11. Sink rate — SET to 3 m/s (600 ft/min).
12. 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.
13. IGNORE altimeter, VSI and ASI readings.
14. Airplane attitude — CONTROL by the position of the horizon line with relation to the
wings and engine cowling.
15. Airspeed and vertical speed — CONTROL using throttle.
16. Follow PRECAUTIONARY LANDING procedure, see section 3.2.6.
1 5