Airplane Flight
Manual Cessna
F
150
L
Nr. 160
Converted with kit
NS402S with ROTAX 912 S3 and
Page:
3-3
HOFFMANN HO-V352F/170FQ+10
Edition 1
RELIGTING THE ENGINE WITH PROPELLER WINDMILLING
as long as the airspeed is not below 62 mph (54kts) the propeller continues on wind milling
1)
Airspeed (IAS) ............................. 70-80 mph (60-70kts)
2)
Prop control ................................. Max. RPM (Forward)
3)
Electrical fuel pump...................... ON
4)
Magneto switch ........................... both
5)
Fuel shut off valve ........................ ON
6)
Throttle ........................................ 2 cm forward
7)
Choke .......................................... Off (in)
If the engine does not start within 10 seconds: Cold start
8)
Throttle ........................................ idle (fully drawn)
9)
Choke .......................................... On (fully drawn)
Reduce engine power to the minimum required and land as soon as possible. Prepare for
engine failure and emergency landing.
RELIGHT OF A STOPPED ENGINE
1)
Electrical load/consumers ............ OFF
2)
Main switch .................................. ON
3)
Prop control ................................. Max. RPM (forward)
4)
Electrical fuel pump...................... ON
5)
Cold start
a.
Throttle ............................ Idle (drawn)
b.
Choke .............................. On
6)
Warm start
a.
Throttle............................. 2 cm forward
b.
Choke .............................. Off (forward)
7)
Magneto switch ............................ Start
Note: Increasing the airspeed to approximately. 125 mph (110kts) the engine can be
cranked. Altitude loss of approx. 1000 ft. / 300 m must be taken into con-
sideration
After successful engine start, check:
1)
Oil pressure ................................. Normal
2)
Choke .......................................... In (forward)
3)
Oil temp ....................................... Normal
4)
Turn on electrical loads as needed, reduce engine power to minimum required, land as
soon as possible, and be prepared for engine failure and emergency landing.
Summary of Contents for CESSNA 150
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