REMOS GX Aviator weight & balance

Data source

POH Section 2.19 (Operating Limitations 2-9); Section 6.2, 6.5, 6.6, 6.7, 6.8 (pages 6-3, 6-6 to 6-8) (pages 21-101 of gx-aviator__poh__104177-rev07-2017-12.pdf) · version type

• Manual prints both metric and imperial values; metric (kg/mm) used here. Imperial: CG limits 9.6-16.3 in, MTOW 1,320 lb, seats 8.3 in, baggage 37.4 in, fuel 37.8 in.
• Maximum fuel is given only as a mass: 57 kg (126 lb); tank volume and usable fuel are not printed on these pages, so fuel max is left null. Fuel density stated as 0.72 kg/L = 6 lb/gal.
• Baggage: 30 kg max in baggage compartment; additionally max 2 kg in each bin (bin arms not given).
• Minimum airborne weight 'not limited'; envelope drawn as a rectangle from 0 to 600 kg between 245 mm and 415 mm.
• Calculation example uses 215 mm for occupants, while the station table gives 210 mm; 210 mm used. Example imperial weights also inconsistent (e.g. 70 kg shown as 175 lb).
• Typical empty is the calculation example only (305 kg at 318 mm); manual says not to use it for flight preparation - use the individual aircraft weight and balance report.
• No maximum landing, zero fuel, per-seat or minimum pilot weights printed. Minimum crew 1, maximum 2 occupants; pilot in command normally on the left.
• 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.