Section VI
WEIGHT AND BALANCE DATA
6-1. WEIGHT AND BALANCE CHARACTERISTICS
The weight and balance characteristics of the Schweizer 330
Helicopter are as follows:
Maximum Certified Gross Weight 2230 pounds
Longitudinal Reference Datum 100 inches forward of rotor
centerline (Rotor hub cen-
terline is located at Station
100 (Fig. 6-1 and 6-2).
Center of Gravity Limits:
Lateral “+” is right of centerline; lateral “-” is left of centerline,
when seated in the crew compartment looking forward.
See Fig. 6-3 for longitudinal center of gravity limits.
See Fig. 6-4 for lateral center of gravity limits.
Stowage Area Behind Seats Limited to 50 pounds each
side (Fig. 6-1)
Center of Gravity Locations (Fig. 6-1 and 6-2):
Longitudinal
(Sta. - in.)
Lateral
(B.L.- in.)
Fuel *104.20 See Fig. 6-7
LH Seat 68.60 -21.50
Center Seat 78.60 +1.25
Right Seat 68.60 +23.75
Baggage Compartment** 125.00 -13.23
*For any fuel quantity.
**CG for centered load. See Fig. 6-1 for any non-centered load.
Weight and Balance
Schweizer RSG, LLC.
Model 269D Helicopter
Pilot's Flight Manual
6-1
R
eissued: 16 Jan 2019
Book 3.indd 139 8/4/19 1:25 PM
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