Aeroprakt A-32 Vixxen weight & balance

Data source

A32-048-POH Section 6.1, Fig. 2 (p. 22) and C.G. table for maximum take-off weight (p. 23) (pages 7-23 of a-32-vixxen__poh__a32-048-poh.pdf) · version type

• The manual gives only fixed CG limits: XCG must be between 1.529 m and 1.780 m (19% and 37% MAC); no weight-dependent envelope chart is printed. The lower mass bound of the envelope (324.2 kg) is this aircraft's empty weight, not a printed minimum.
• Empty weight 324.2 kg at 1.595 m is from the weighing of serial no. 048 (front wheel 61.5 kg, left 134.6 kg, right 130.0 kg); use your own aircraft's weighing data.
• No maximum seat load, baggage limit, minimum pilot weight, max landing or zero-fuel mass printed on these pages; 2×90 kg crew and 30 kg baggage are only the sample loading.
• Fuel: 2×45 L wing tanks at a single arm of 1.960 m; density 0.72 kg/L derived from the sample (90 L = 64.8 kg). Usable fuel not stated on these pages.
• Seats arm 1.663 m (pilots C.G.); baggage arm 2.320 m.
• 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.