REMOS GX nXES weight & balance

Data source

POH Section 2.19-2.20 (Operating Limitations), Section 6.2 Station Definitions, 6.5 Operating Weights and Loading, 6.6 Weight and Balance Chart, 6.7, 6.8 Calculation Example (pages 21-101 of gxnxes__poh__104178-rev03-2017-12.pdf) · version type

• Manual prints both metric and imperial values; metric (kg, mm) used here. Imperial equivalents: MTOW 1,320 lb, CG limits 9.6-16.3 in, 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 volume are not printed on these pages, so fuel max is null.
• Fuel density stated as 0.72 kg/L (6 lb/gal).
• Baggage: max 30 kg in baggage compartment; additionally max 2 kg in each bin (bin arms not given).
• Station table gives seats at 210 mm, but the calculation example uses 215 mm for occupants; 210 mm used here - verify.
• Minimum airborne weight is 'not limited'; envelope is a rectangle from 245 to 415 mm up to 600 kg, lower edge drawn at 0 kg.
• Minimum 1 occupant (pilot in command), maximum 2; no minimum pilot mass printed.
• Typical empty values are from the calculation example only (305 kg at 318 mm); use the aircraft's individual weight and balance report.
• Calculate CG for both take-off and landing fuel states.
• 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.