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Converted with conversion kit
HOFFMANN HO-V352F/170FQ+10
ELEVATOR TRIM
Movement up:
Movement down:
RUDDER AND FIN
Fin area:
Rudder area:
Movement to the left:
Movement to the right:
LANDING GEAR
Type:
Strut,
Main landing gear:
Distance between main gear wheels and nose gear wheel: 1.46 m
Nose wheel tire and pressure:
Main tires and pressure:
Nose landing gear strut pressure:
POWER PLANT
ENGINE: ROTAX 912S3 100HP (73.5KW)
FUEL:
Normal, Super, Super Plus unleaded, EN 288 at
least 95 RON or avgas 100ll in exceptional
cases.
OIL
Corresponding to opposite table (FIG. 1 - 2)
Use only oils meant for OTTO engines that
comply with API system with "SF" or "SG"
marking
Do not use aircraft engine oil.
Do not use any oil additives.
Airplane Flight Manual
Cessna F150L
NS402S with ROTAX 912 S3 and
10 ° ± 1 °
20 ° ± 1 °
0.83 m2
0.65 m2
23 ° + 0 ° (perpendicular to the axis of rotation) -2°
23 ° + 0 °-2 °
fixed tricycle landing gear
nose gear:
width: 2,32m
5.00 - 5 30 psi (2.109 kg / cm2)
6.00 - 6 21 psi (1.476 kg / cm2)
20 psi (1,406 kg / cm2)
air - oil
Nr. 160
1-4
Page:
Revision 1
FIG 1-2 OIL TABLE
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