REMOS GX weight & balance

Data source

Flughandbuch REMOS GX Standard Cockpit, Abschnitt 2.15 (Schwerpunktlage und Massen), Abschnitt 6.1 Wägung, 6.2 Beladeplan, 6.3 Berechnungsbeispiel (pages 18-19, 72-74 of gx-std-ul__poh__fhb-ul-rev06.pdf) · version type

• No CG envelope chart is printed; only flight CG limits 245 mm to 430 mm independent of mass and MTOW 472.5 kg. Envelope given as a rectangle; the lower mass edge (0 kg) is not a printed limit.
• Baggage max 25 kg applies to ROTAX 912 ULS (100 PS); with ROTAX 912 UL2 (80 PS) baggage max is 10 kg. Check your engine variant.
• Storage compartments (Ablagefächer): max 2 kg each; no arm printed, not included as stations.
• Fuel is entered as mass (kg) at arm 960 mm; tank volume, usable fuel and fuel density are not printed on these pages.
• Pilot and passenger share one 'Insassen' arm of 210 mm; no per-seat maximum or minimum pilot mass printed.
• Typical empty mass 295 kg at 330 mm is from the sample calculation (Berechnungsbeispiel), use your aircraft's actual weighing report.
• Minimum crew one pilot, pilot seat left (right only with primary instruments on right side).
• 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.