Apollo FOX - Page 27

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3.1.5.8 Climb
- throttle max. cont. power, max. 5500 r.p.m.
- airspeed 100 - 110 km/h IAS
- engine instruments within limits
3.1.5.9 Cruise Flight
- bring the aircraft into horizontal flight
- throttle 4000 - 5000 r.p.m.
- airspeed 110 - 150 km/h IAS
- engine instruments within limits
3.1.5.10 Descent
- throttle increased idle
- airspeed 110 km/h IAS
- engine instruments within limits
CAUTION
At long final and when descending from a considerable height, it is not
advisable to reduce the engine throttle control to minimum. In such
case the engine becomes undercooled and a loss of power occurs.
When descending, apply increased idle so that engine instrument
indications stay within the limits for normal use.
3.1.5.11 Downwind
- throttle 3500 - 4500 r.p.m.
- airspeed 110 km/h IAS
- engine instruments within limits
- fuel check fuel quantity
-safety belts tighten
- base leg and before final space check of free space
- at base leg and before final space check free space