A weight and balance computation must be accomplished prior to
flight. Ballast, if required, must be carried.
NOTE: Ballast may be carried in the stowage area behind the seats.
Ballast may consist of lead shot, sand bags or similar material ade-
quately contained and secured.
Maximum weight in the stowage area behind each outboard seat is
50 pounds each side.
This helicopter is limited to operation in accordance with this section
and the approved loading information given in Section VI, Weight
and Balance Data.
2-8. CENTER OF GRAVITY (CG ENVELOPE)
The datum line is 100.0 inches forward of the main rotor hub
centerline.
Forward CG limit is 94.1 inches at 2230 pounds varying linearly to
92.0 inches at 1750 pounds and below. Aft CG limit is 96.0 inches
at 2230 pounds varying linearly to 101.0 inches at 1750 pounds &
below (Fig. 2-2, Sheet 1).
Lateral “+” CG is right of the aircraft centerline; lateral “-” CG is
left of the aircraft centerline when looking forward (Fig. 2-2, Sheet
2).
The right lateral CG limit varies linearly from a gross weight of
2230 lbs at buttline 2.4 inches to 1750 pounds & below at buttline
4.5 inches.
The left lateral CG limit varies linearly from a gross weight of 2230
lbs at buttline -.9 inches to 1750 lbs & below at buttline -3.0 inches.
Limitations
Pilot's Flight Manual
Schweizer RSG, LLC.
Model
269D
Helicopter
2-6
Reissued:
16
Jan 2019
FAA Approved
Book 3.indd 54
8/4/19 1:25 PM
