Control Rigging
Main Rotor
Collective Pitch, Full Travel, Min-
imum
12° ± 1° (up to down)
Collective Pitch at Down Stop 0.75R 2.5° ± 1.5°
(ground adjustable)
Range of Cyclic Pitch Blade Angle
from Neutral Rigging Position,
Minimum
Forward 8.5° to 9.5°
Aft 9.5° to 10.0°
Left 6.5° to 7.5°
Right 6.0° to 7.0°
Tail Rotor
Range of Blade Pitch Angles (3/4
radius), Minimum
Right Pedal 11° to 13°
(thrust to left)
Left Pedal 27° to 29°
(thrust to right)
Engine
Rolls Royce 250-C20W Gas Tur-
bine Max Rated Power = 420 SHP
INSTALLED LIMITS:
Max. Continuous Power = 220 HP (57.8 PSI Torque)
Max.Take-off Power
(5 min. limit) =
235 HP (61.7 PSI Torque)
Max. Gas Generator = 6,317 RPM (105% N
1
)
Max. Power Turbine = 30,294 (91% N
2
)
Max. Power Output Shaft = 5,475 RPM (@91% N
2
)
General
Pilot's Flight Manual
Schweizer RSG, LLC.
Model 269D Helicopter
1-12
R
eissued: 16 Jan 2019
Book 3.indd 24 8/4/19 1:25 PM
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