SAMPLE
4-6
Document No.:
Z601XLFMEN
Date of Issue:
12/2002
Revision:
4.4.7 Climb
1. Best rate-of-climb speed - 130 km/h (70 KIAS)
2. Throttle
- Max. take-off power
(max. 5800 rpm for 5 minutes)
- Max. cont.power 5500 rpm
3. Trim
- trim the airplane
4. Instruments
- oil temperature and pressure, cylinder
temperature within limits
CAUTION
If the cylinder head temperature or oil temperature exceed their limits,
reduce the climb angle to decrease airspeed and thus fulfil the limits.
4.4.8 Cruise
Refer to Section 5, for recommended cruising regimes.
4.4.9 Descent
1. Optimum glide speed
- 120 km/h (65 KIAS)
CAUTION
It is not advisable to reduce the engine throttle control lever to minimum on
final approach and when descending from very high altitude. In such cases
the engine becomes undercooled and a loss of power may occur. Descent
at increased idle at 3000 rpm, speed between 120-140 km/h IAS (65-76
KIAS) and check that the engine instruments indicate values within
permitted limits.
4.4.10 Before
landing
1. Approach speed
- 120 km/h (65 KIAS)
2. Throttle
-
as
needed
3. Wing flaps
- extend as needed
4. Trim
-
tail
heavy
5. Fuel
-
check
quantity
