REMOS GX NXT weight & balance

Data source

POH Section 2.19 (Operating Limitations p. 2-9); Section 6.2 Station Definitions, 6.5 Operating Weights and Loading, 6.6 Weight and Balance Chart, 6.7, 6.8 Calculation Example (pp. 6-3 to 6-8) (pages 21-101 of gx-nxt__poh__104176-rev03-2017-12.pdf) · version type

• Manual prints both metric and imperial values; metric (kg, mm) used here. Imperial: seats 8.3 in, baggage 37.4 in, fuel 37.8 in, CG limits 9.6-16.3 in, MTOW 1,320 lb.
• Maximum fuel is given only as a mass: 57 kg (126 lb); tank volume in litres is not printed. At the stated 0.72 kg/L this is about 79 L; verify against the fuel system section.
• Max baggage in each bin: 2 kg (4.4 lb); no arm is given for the bins.
• Envelope is a simple rectangle: CG 245-415 mm at any weight up to 600 kg; minimum airborne weight 'not limited'. No separate maximum landing or zero-fuel mass is printed.
• Crew: minimum 1 occupant (pilot in command), maximum 2 occupants; PIC normally seated on the left. No per-seat maximum printed.
• Typical empty (305 kg at 318 mm) is from the calculation example only; the manual says not to use it for flight preparation; use the individual aircraft weight and balance report.
• The calculation example uses 215 mm for occupants while the station table gives 210 mm; 210 mm is used here.
• Fuel density stated: 0.72 kg/L = 6 lb/gal. Calculate CG at take-off and at landing 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.