NOTE
OPTIONAL BAGGAGE COMPARTMENT LOADING. The bag-
gage compartment is accessible through the main access door on
the left side of the aircraft. It contains approximately 4.2 cubic feet
of space. The baggage compartment has a load limit of 60 pounds
(one (1) pound per square inch), which is a structural limitation
only, and does not infer that C.G. will remain within approved lim-
its. The load shall be secured to tiedown fittings, shifting of the
load in flight could result in structural damage to the baggage com-
partment or in gross weight center of gravity limits being ex-
ceeded. The C.G. shall be computed with the load in the most
adverse position.
Table 6-1. Center of Gravity Limits
Gross Weight
(lb)
Longitudinal C.G. Limit Lateral C.G. Limit
(Sta.-in.) (B.L.-in.)
Forward Aft (+) Right, (-) Left
2230 94.1 96.0 +2.4 - .9
1950 92.8 98.8 + 3.7 - 2.2
1750 & below 92.0 101.0 + 4.5 - 3.0
NOTE: Forward C.G. limit is 94.1 in. at 2230 lbs varying linearly to
92.0 in. at 1750 lbs and below. Aft C.G. limit is 96.0 in. at 2230 lbs
varying linearly to 101.0 in. at 1750 lbs & below. (Fig. 2-2, Sheet 1)
NOTE: The right lateral C.G. limit varies linearly from a gross weight
of 2230 lbs at buttline 2.4 in. to 1750 lbs & below at buttline 4.5 in.
NOTE: The left lateral C.G. limit varies linearly from a gross weight of
2230 lbs at buttline -.9 in. to 1750 lbs & below at buttline -3.0 in.
Weight and Balance
Pilot's Flight Manual
Schweizer RSG, LLC.
Model 269D Helicopter
6-2
Reissued: 16 Jan 2019
Book 3.indd 140 8/4/19 1:25 PM
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