REMOS G-3/600 weight & balance
POH figures for the type
- MTOW1320 lb
- Typical empty670 lb
- Typical empty CG12.5 in
Envelope chart. Takeoff 845 lb at 11.6 in.
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PEOPLE
BAGGAGE
FUEL
EMPTY MASS · YOUR AIRCRAFT
Typical for the type, 670 lb at 12.5 in. Edit it to your aircraft’s own, from its weighing report.
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Data source
POH Section 4, 4.3-4.7 (pages 25-29), CG-Diagram 4.6 (pages 25-29 of g3-600-us-s-lsa__poh__us-slsa-rev03.pdf) · version type
- CG limits printed as 9.6 to 16.3 inches behind R.P.; envelope built as a rectangle from these limits up to MTOW 1320 lb.
- Lower mass bound of 770 lb is only the lowest value on the CG-Diagram axis, not a stated limit.
- Fuel tank capacity and usable fuel are not printed on these pages; examples use up to 20 gallons. Density 6 lb/USG derived from the example (10 gallons = 60 lb).
- No maximum seat or luggage weights printed on these pages; check placards and the limitations section.
- Empty weight 670 lb at 12.5 in is the example only; use the aircraft-specific weight and balance form (page 29).
- The CG-Diagram plots weight vs. total moment (lb-in); its torque axis labels appear inconsistent with the stated arm limits, so the printed 9.6/16.3 in limits were used.
- 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.
| Station | Load | Mass lb | Arm in | Moment lb·in/1000 |
|---|---|---|---|---|
| Empty aircraft | 670 | 12.5 | 8.4 | |
| Pilot seat | 175 | 8.3 | 1.5 | |
| Passenger seat | 0 | 8.3 | 0.0 | |
| Fuel | 0 USG | 0 | 37.8 | 0.0 |
| Luggage | 0 | 37.4 | 0.0 | |
| Zero fuel | 845 | 11.6 | 9.8 | |
| Takeoff | 845 | 11.6 | 9.8 |
POH Section 4, 4.3-4.7 (pages 25-29), CG-Diagram 4.6 (pages 25-29 of g3-600-us-s-lsa__poh__us-slsa-rev03.pdf). For reference only; the aircraft’s flight manual and weighing report are the final authority. https://zulucheck.com/wb/type/remos-g3-600/
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