Aquila A212 weight & balance

Data source

POH FM-AT01-1010-104 Section 2.6/2.7 (p. 2-6), Section 6.2-6.4 (pp. 6-3, 6-4, 6-8, 6-9) (pages 22-108 of a212-at01-200a__afm__fm-at01-1010-104-200a-dvfr-a01.pdf) · version type

• Manual also gives metric values: MTOW/MLW 750 kg, baggage 40 kg at 1.3 m, seats 0.484 m (forward) / 0.580 m (aft), fuel 0.325 m, CG limits 0.427-0.523 m, fuel density 0.72 kg/L, usable fuel 100 L.
• Seats are adjustable: arm 19.1 in with seat fully forward, 22.8 in fully aft; interpolate for intermediate positions. Stations set to forward position here - adjust for actual seat position.
• CG limits are printed as constant 16.8 in (fwd) and 20.6 in (aft) up to MTOW; the CG envelope chart 6.4.3 (page 6-10) was not provided. Lower mass bound of the envelope (1116 lb) is the sample empty weight, not a printed limit.
• Total fuel tank capacity not printed on these pages; usable fuel 26.5 USG and unusable fuel 2.74 USG (10.4 L) are given.
• Sample empty weight 1116 lb with CG 17.58 in from the weighing example (19620 in-lb); table 6.4.2 lists example DSL as 17.3 in - inconsistency in manual. Use the actual aircraft's weighing report.
• No minimum pilot weight, maximum per seat, maximum ramp or zero fuel weight printed.
• 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.