CubCrafters CC11-100 Sport Cub weight & balance

Data source

POH Report SC10000AFM Section 6, para 6.2, Tables 6-3, 6-4 and 6-5 (pages 121-138 of cc11-100-sport-cub__afm__sc10000afm-rev-m.pdf) · version type

• Envelope built from printed CG limits (para 6.2): forward 70.5 in at 1100 lb or less, 73.0 in at 1320 lb, straight-line between; aft 78.5 in at all weights. Figure 6-4 chart was not on the provided pages.
• The lower edge of the envelope (883 lb) is not a printed limit; it is the sample empty weight, used only to close the polygon.
• Aircraft with the optional Extended Cargo Compartment (Table 6-4) use arm 138.40 in with a 60 lb max for the extended compartment instead of 134.40 in / 20 lb.
• Fuel tank capacity, usable fuel and fuel density are not printed on these pages; enter fuel as weight in lb at arm 83.90 in.
• Station arms are printed only as Pilot and Passenger; the passenger arm (96.08 in) is aft of the pilot (71.40 in).
• No separate landing or zero-fuel weight printed; 1320 lb is maximum gross weight.
• Different propellers and tires affect weight and balance; optional equipment must be included. Aircraft with 3X3 landing gear use a different main wheel arm (59.50 in vs 62.50 in) when weighing.
• Typical empty weight is from the sample calculation (Table 6-5); use the actual basic empty weight and CG from the aircraft records.
• Read from the POH by ZuluCheck and checked by a second reading; verify against your own manual.

For reference only. The aircraft’s approved flight manual and weighing report are the final authority.