Cessna T206H Turbo Stationair weight & balance
POH figures for the type
- MTOW3600 lb
- MLM3600 lb
- Typical empty2314 lb
- Typical empty CG36.95 in
Envelope chart. Takeoff 2729 lb at 37.8 in.
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PEOPLE
BAGGAGE
FUEL
EMPTY MASS · YOUR AIRCRAFT
Typical for the type, 2314 lb at 36.95 in. Edit it to your aircraft’s own, from its weighing report.
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Data source
POH Section 2 Weight Limits and Center of Gravity Limits (p. 2-8); Section 6, Figures 6-3, 6-4, 6-5, 6-8 and 6-9 (pages 22-212 of t206h-g1000-gfc700__poh__2007.pdf) · version type
- Maximum ramp weight 3617 lb (includes 14 lb fuel allowance for start, taxi and runup).
- Envelope taken from Section 2 text and Figure 6-9: forward limit 33.0 in at 2500 lb or less, straight line to 42.5 in at 3600 lb; aft limit 49.7 in at all weights. The 1900 lb lower edge is the bottom of the moment envelope chart (Figure 6-8), not a printed limit.
- Fuel: 87 gal usable standard (reduced fuel 64 gal option also listed); total tank capacity not given on these pages. Fuel arm FS 46.5, 6 lb/gal.
- Seat arms are for average occupant; occupant CG range: front 32-43, center 69-79, aft 94-100 in.
- Baggage area FS 109-145 limited to 180 lb; floor loading not to exceed 200 lb/sq ft.
- Cargo areas A, B, C apply only with seats removed; maximum cargo loads depend on tiedowns used and W&B limits.
- Optional cargo pack (FS 10-84) max 300 lb; arm depends on item position (Figures 6-5, 6-6) and is not included as a station.
- Sample empty weight arm computed from printed moment 85.5 lb-in/1000 at 2314 lb; use your airplane's actual basic empty weight and moment.
- 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 | 2314 | 37.0 | 85.5 | |
| Pilot (FS 32-43) | 175 | 37.0 | 6.5 | |
| Front passenger (FS 32-43) | 0 | 37.0 | 0.0 | |
| Center passengers (FS 69-79) | 0 | 70.0 | 0.0 | |
| Aft passengers (FS 94-100) | 0 | 100.0 | 0.0 | |
| Baggage / Cargo D (FS 109-145) | 0 | 127.0 | 0.0 | |
| Fuel (usable, standard 87 gal) | 40 USG | 240 | 46.5 | 11.2 |
| Cargo A, seats removed (FS 10-50) | 0 | 33.0 | 0.0 | |
| Cargo B, seats removed (FS 50-84) | 0 | 67.0 | 0.0 | |
| Cargo C, seats removed (FS 84-109) | 0 | 96.0 | 0.0 | |
| Zero fuel | 2489 | 37.0 | 92.0 | |
| Takeoff | 2729 | 37.8 | 103.1 |
POH Section 2 Weight Limits and Center of Gravity Limits (p. 2-8); Section 6, Figures 6-3, 6-4, 6-5, 6-8 and 6-9 (pages 22-212 of t206h-g1000-gfc700__poh__2007.pdf). For reference only; the aircraft’s flight manual and weighing report are the final authority. https://zulucheck.com/wb/type/cessna-t206h/
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