RV6Awb
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RV6Awb
Product catalog summary
Introduction: This document provides a quick reference for the weight and balance data of the RV-6A aircraft. It is important to note that this chart is not a substitute for the complete information found in Section 14 of the Builder’s Manual.
Key Cautions:
- The Gross Weight is determined by the builder, who acts as the manufacturer.
- Aerobatic flight should not be conducted at weights greater than 1375 lbs or at CG locations outside the aerobatic CG limit.
Specifications:
- Datum: 60 inches forward of the wing leading edge.
- Design C.G. Range: 15%-29% of wing chord or between 68.7-76.8 inches aft of datum.
- Recommended Gross Weight: 1650 lbs.
- Aerobatic Gross Weight: 1375 lbs.
- Aerobatic CG Limit: 26.5% of chord or 75.3 inches aft of datum.
Arms:
- Fuel: 70.00 inches aft of datum.
- Pilot/Passenger: 87.40 inches aft of datum.
- Baggage: 117.00 inches aft of datum.
Procedure for Determining Empty CG:
- Level the aircraft longitudinally and laterally using the longerons in the cabin area as the level reference.
- Weigh the airplane with the canopy closed, full oil, and empty fuel tanks.
- Enter the weights and distances from the datum (arm) in the provided chart.
- Multiply weight by arm to obtain moment.
- Divide the total moment by the weight to determine the empty CG.
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Catalog excerpts
ARMS Fuel Pilot/Passenger Baggage DETERMINING EMPTY CG Level the aircraft longitudinally and laterally using the longerons in the cabin area as the level reference. Weigh the airplane with the canopy closed, full oil and the fuel tanks empty. Enter the weights and distances from the datum (arm) in the chart below. Multiply weight by arm to obtain moment. Divide the total moment by the weight to determine the empty CG.
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