Aquila A211 weight & balance

Data source

POH/AFM FM-AT01-1010-101 Section 2.7, 2.8; Section 6.2, 6.4.1, 6.4.2 (Table Weight and Moment Determination) (pages 22-98 of a211-at01-100a__afm__fm-at01-1010-101-100a-dvfr-a09.pdf) · version type

• Seats are adjustable: arm is 19.1 in (0.484 m) with seat fully forward and 22.8 in (0.580 m) with seat fully aft. Stations are set to the forward position; interpolate for the actual seat position (seat aft is behind the 20.6 in aft CG limit).
• CG limits from Section 2.8: forward 16.8 in (0.427 m), aft 20.6 in (0.523 m), not weight-dependent on these pages. The chart 6.4.3 (Approved CG Range and Moment Limits) page was not provided; envelope drawn as a rectangle. The lower mass bound 1116 lb is only the example empty weight, not a printed limit.
• Fuel density 6.01 lb/US gal (0.72 kg/L) as printed. Tank capacity and usable fuel are not stated on these pages; the example uses 26.5 US gal usable. Unusable fuel 2.74 US gal (10.4 L) is included in empty weight.
• Maximum baggage 88.2 lb (40 kg).
• Typical empty weight is the weighing example (1116 lb, 17.34 in); use the actual aircraft's weighing report.
• Manual also gives metric values (kg, 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.