Normal Climb; Before Landing - Rotax CESSNA 150 Manual

Airplane flight
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Converted with kit
NS402S with ROTAX 912 S3 and
HOFFMANN HO-V352F/170FQ+10
SHORT FIEL TAKE OFF
1)
Flaps ............................................................... 10°
2)
carburetor heat ............................................... cold (forward)
3)
Brakes ............................................................ apply
4)
Propeller control .............................................. max. RPM
5)
Throttle ........................................................... Full open (forward)
6)
Brakes ............................................................ release
7)
Elevator control ............................................... 50-55mph (43-48kts) list the nose wheel
Note– lifting the nosewheel below 50mph (44kts) can extend the takeoff run.
8)
Airspeed ......................................................... 60mph (52kts), then select airspeed from
9)
Flaps ............................................................... retract slowly after reaching safe altitude
10) el. Fuel pump .................................................. off
11) Suction (If venturi installed) ............................. check (3.0 bis 5.4 in.Hg.)

NORMAL CLIMB

1)
Airspeed ..................................... 75-80mph (65-70 Kts)
NOTE. If the climb is performed with maximum climb rate, use the speeds given in
section 5 in the table "Maximum climb speeds".
2)
Throttle ........................................ Full open
3)
Propeller control ........................... 2260 rpm
CRUISE (RECOMMENDED)
1)
Engine speed ............................... 1700 to 2260 rpm
Throttle ........................................ See section 5 – cruise power settings
2)
3)
Elevator trim ................................ adjust

BEFORE LANDING

Carb heat ..................................... Cold (forward) – apply full heat if conditions are prone
1)
2)
el. Fuel pump ............................... on
3)
Airspeed ...................................... 65-75mph (55-65kts)
4)
Wing flaps .................................... as required (airspeed below 100mph (87kts)
5)
Airspeed ...................................... 60-70mph (50-60kts) (flaps down)
Airplane Flight Manual
Cessna F150L
section 5
and airspeed
to carb ice
Nr. 160
4-5
Page:
Revision 1

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F150l series

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