Aquila A211 GX weight & balance

Data source

POH/AFM FM-AT01-1010-103 Section 2.6-2.7 (p. 2-6), Section 6.4.1 Loading Graph (p. 6-8), Table 6.4.2 Weight and Moment Determination (p. 6-9), 6.4.4 (p. 6-11) (pages 22-103 of a211gx-at01-100c__afm__fm-at01-1010-103-100c-dvfr-a09.pdf) · version type

• Seats are adjustable: arm 19.1 in (0.484 m) seat forward to 22.8 in (0.580 m) seat aft. 21 in is the middle position used by the MVP-50P-AQ; interpolate for the actual seat position.
• Chart 6.4.3 (Approved C.G. Range and Moment Limits) was not among the pages provided. The envelope is built from the Section 2.7 limits: forward 16.8 in (0.427 m), aft 20.6 in (0.523 m), with no weight dependency printed. The lower mass bound of 1116 lb is only the example empty weight, not a printed limit.
• Fuel tank total and usable capacity are not printed on these pages. The 6-9 example uses 159 lb usable (26.5 USG / 100 L). Unusable fuel of 2.74 USG (10.4 L) is included in the empty weight.
• Fuel density is printed as 6.01 lb/USG (0.72 kg/L).
• Baggage maximum is 88.2 lb (40 kg).
• Typical empty weight of 1116 lb at 17.3 in is the manual's example (moment 19309 in-lb). Use the actual aircraft's weighing report.
• Metric equivalents are printed: MTOW 750 kg; arms 0.484/0.580 m seats, 1.3 m baggage, 0.325 m fuel.
• 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.