BRM Aero Bristell S-LSA weight & balance
POH figures for the type
- MTOW600 kg
- Typical empty356.1 kg
- Typical empty CG375.86 mm
Envelope chart. Takeoff 476 kg at 398.8 mm.
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PEOPLE
BAGGAGE
FUEL
EMPTY MASS · YOUR AIRCRAFT
Typical for the type, 356.1 kg at 375.86 mm. Edit it to your aircraft’s own, from its weighing report.
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Data source
AOI SLSA-AOI-2-8-0-AU Section 1.5 (p.1-8), Section 6.2.1.1-6.2.1.3 (pp.6-4 to 6-6), Section 6.3 Permitted payload range (p.6-7) (pages 20-79 of bristell-slsa__aoi__slsa-aoi-2-8-0-au-rev1.pdf) · version type
- No CG envelope chart is printed; only forward limit 341.8 mm (25% MAC) and rearward limit 478.5 mm (35% MAC) with MTOW 600 kg. The envelope is a rectangle; its lower mass bound (356.1 kg) is this aircraft's empty weight, not a printed limit.
- MAC = 1367.0 mm.
- Baggage maxima (behind seats 15 kg, wing lockers 40 kg total, front locker 10 kg) are taken from the maximum values used in the permitted payload table (6.3); no explicit structural placard limits are printed on these pages. Verify against cockpit placards.
- Wing lockers are given as a single combined station at arm 630 mm; per-side limit not stated on these pages.
- Fuel density 0.725 kg/L derived from the payload table (20 L = 14.5 kg); not stated explicitly.
- Fuel: 120 L total, 119 L usable (Section 1.5).
- Front locker is optional equipment.
- Empty weight 356.1 kg at 375.86 mm (27.5% MAC) is for S/N 320/2018 weighed 2.1.2018; use the current weighing report.
- No maximum landing, zero fuel weight, or minimum pilot weight printed on these pages.
- 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 kg | Arm mm | Moment kg·mm/1000 |
|---|---|---|---|---|
| Empty aircraft | 356 | 375.9 | 133.8 | |
| Pilot | 80 | 600.0 | 48.0 | |
| Passenger | 0 | 600.0 | 0.0 | |
| Baggage - behind seats | 0 | 1400.0 | 0.0 | |
| Baggage - front locker (optional) | 0 | -300.0 | 0.0 | |
| Baggage - wing lockers | 0 | 630.0 | 0.0 | |
| Fuel tanks | 55 L | 40 | 200.0 | 8.0 |
| Zero fuel | 436 | 417.0 | 181.8 | |
| Takeoff | 476 | 398.8 | 189.8 |
AOI SLSA-AOI-2-8-0-AU Section 1.5 (p.1-8), Section 6.2.1.1-6.2.1.3 (pp.6-4 to 6-6), Section 6.3 Permitted payload range (p.6-7) (pages 20-79 of bristell-slsa__aoi__slsa-aoi-2-8-0-au-rev1.pdf). For reference only; the aircraft’s flight manual and weighing report are the final authority. https://zulucheck.com/wb/type/brm-bristell-slsa/
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