PS-POH-1-1-11 SECTION 4
NORMAL PROCEDURES
P
P
S
S
-
-
2
2
8
8
C
C
r
r
u
u
i
i
s
s
e
e
r
r
Date: 2011-09-01
4-9 Rev. No.: -
WARNING
Takeoff is prohibited if:
• Engine is running unsteadily, roughly or with vibrations
• Engine instrument values are beyond operational limits
• Aircraft systems (e.g. brakes, flight controls or avionics) working incorrectly
• Crosswind velocity exceeds permitted limits
(see Section 5 Performance, 5.7 Demonstrated wind performance)
4.5 Climb
1. THROTTLE - MAX
(max. 5,800 rpm for max. 5 min,
max. continuous power 5,500 rpm)
2. Airspeed - V
x
= 55 KIAS
- V
y
= 62 KIAS
3. Trims - as necessary
4. Engine gauges - oil temperature, oil pressure and
CHT within limits
CAUTION
If the cylinder head temperature or oil temperature and/or coolant temperature
approaches or exceeds limits, reduce the climb angle to increase airspeed and
possibly return within limits. If readings do not improve, troubleshoot causes other
than high power setting at low airspeed.
4.6 Best angle of climb speed (V
x
):
55 KIAS
4.7 Best rate of climb speed (V
y
):
62 KIAS
4.8 Cruise
Refer to Section 5, for recommended cruising figures.
4.9 Descend
1. Optimum glide speed - 60 KIAS
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