Cessna 206H Stationair weight & balance
POH figures for the type
- MTOW3600 lb
- MLM3600 lb
- Typical empty2210 lb
- Typical empty CG34.66 in
Envelope chart. Takeoff 2625 lb at 35.9 in.
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PEOPLE
BAGGAGE
FUEL
EMPTY MASS · YOUR AIRCRAFT
Typical for the type, 2210 lb at 34.66 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 22-206 of 206h-g1000-gfc700__poh__2007.pdf) · version type
- Maximum ramp weight 3614 lb; 14 lb fuel allowance for start, taxi and runup.
- Envelope 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. Lowest weight 1900 lb taken from the moment envelope (Figure 6-8, moment/1000 ~62.7 and ~94.4 at 1900 lb, consistent with 33.0 and 49.7 in); Figure 6-9 only plots down to 2200 lb.
- Fuel: 87 USG usable standard; a reduced-fuel option of 64 USG usable is listed. Total tank capacity not printed on these pages. Usable fuel arm FS 46.5, 6 lb/gal.
- Seat arms are for average occupant positions: pilot/front pax range FS 32-43, center FS 69-79, aft FS 94-100.
- Baggage area FS 109-145 max 180 lb, arm 127 is the center of area D; the sample loading problem places its baggage at about FS 110.
- Cargo areas A, B and C (arms 33, 67, 96 to area centers) apply only with seats removed; max cargo is limited by tiedowns and floor loading 200 lb/sq ft.
- Optional cargo pack (FS 10 to 84) max 300 lb; its arm depends on the load location (Figures 6-5/6-6).
- Typical empty arm is computed from the sample loading problem: 76.6 / 2210 × 1000 = 34.66 in. Use your own airplane's basic empty weight and arm.
- 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 | 2210 | 34.7 | 76.6 | |
| Pilot (FS 32 to 43) | 175 | 37.0 | 6.5 | |
| Front passenger (FS 32 to 43) | 0 | 37.0 | 0.0 | |
| Center passengers (FS 69 to 79) | 0 | 70.0 | 0.0 | |
| Aft passengers (FS 94 to 100) | 0 | 100.0 | 0.0 | |
| Baggage / Cargo D (FS 109 to 145) | 0 | 127.0 | 0.0 | |
| Fuel (standard, 87 USG usable) | 40 USG | 240 | 46.5 | 11.2 |
| Cargo A, seats removed (FS 10 to 50) | 0 | 33.0 | 0.0 | |
| Cargo B, seats removed (FS 50 to 84) | 0 | 67.0 | 0.0 | |
| Cargo C, seats removed (FS 84 to 109) | 0 | 96.0 | 0.0 | |
| Zero fuel | 2385 | 34.8 | 83.1 | |
| Takeoff | 2625 | 35.9 | 94.2 |
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 22-206 of 206h-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-206h/
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