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Schweizer 269C-1 - Page 37

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Rotor Blade Pitch Displacements (cont) Eng lish Met ric
Tail rotor blade
Collective pitch at 3/4 radius
Full left pedal (thrust to
right)
+ 25° to + 27°
Full right pedal (thrust to
left)
- 11° to - 13°
Control Stick and Pedal
Movements
Collective stick (full down to
full up)
10 in. 254 mm
Throttle angle, twist grip
(full closed to full open)
130°
Cyclic control stick (full
forward to full aft)
15 in. 381 mm
Cyclic control stick (full left
to full right)
16 in. 406 mm
Directional control pedals
(full forward to full aft)
8 in. 203 mm
Engine General Data
Powerplant (Carbureted):
Type Lycoming Hor i zon tally Op posed
Designation HO-360-C1A
Cylinders 4
Horsepower 180 hp at 2700 rpm
Powerplant (Fuel Injected):
Type Lycoming Hor i zon tally Op posed
Designation HIO-360-G1A
Cylinders 4
Horsepower 180 hp at 2700 rpm
General
Pilot's Flight Manual
Reissued: 16 Jan 2019 1-11
SCHWEIZER
Model 269C-1 Helicopter
CSP book 2..indd 37 8/4/19 12:53 PM

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