Cessna U206F Stationair weight & balance
POH figures for the type
- MTOW3600 lb
- Typical empty1975 lb
- Typical empty CG35.24 in
Envelope chart. Takeoff 2390 lb at 35.0 in.
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PEOPLE
BAGGAGE
FUEL
EMPTY MASS · YOUR AIRCRAFT
Typical for the type, 1975 lb at 35.24 in. Edit it to your aircraft’s own, from its weighing report.
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Data source
Owner's Manual Section 4, pages 4-4 to 4-11: Sample Loading Problem (4-6), Loading Arrangements (4-7), Loading Graph (4-8), Center of Gravity Moment Envelope (4-9), Internal Cabin Dimensions (4-10) (pages 50-57 of u206f__poh__n9554g.pdf) · version type
- Envelope is drawn as weight vs moment/1000; vertices read at moments 62 and 82 (forward, at 1900 and 2500 lb), 152 and 179 (at 3600 lb), 94 (aft, at 1900 lb) and converted to arm = moment/weight. Chart bottom is 1900 lb, not necessarily a minimum weight. Verify readings against the original chart.
- Maximum weight 3600 lb taken from the top of the envelope and the sample loading total; no separate landing or ramp weight printed.
- Fuel arm not printed; 47.9 in derived from the sample (480 lb = 80 gal at 6 lb/gal, moment 23.0). Standard tanks 63 gal usable, long range tanks 80 gal usable; total tank capacity not printed. Set usable to 80 if long range tanks are installed.
- Oil: 12 qts (22 lb) at moment -0.4 (no oil filter), 13 qts (24 lb) at moment -0.5 with optional oil filter; arm derived from moment. The licensed empty weight on your airplane's data sheet normally includes oil (sample empty weight 1975 lb at moment 69.6 excludes it).
- Seat arms are for average occupants; the ranges in parentheses give fore/aft limits of occupant c.g.
- Cargo areas A-D apply to the seats-removed cargo arrangements I-III; maximum cargo depends on tie-downs used and c.g. limits; floor loading max 200 lb/sq ft.
- Optional cargo pack (Sta. 10 to 84) max 300 lb; its arm is on a page 4-12 diagram not included here.
- Baggage area IV max 120 lb.
- 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 | 1975 | 35.2 | 69.6 | |
| Pilot (Sta. 34 to 48) | 175 | 37.0 | 6.5 | |
| Copilot (Sta. 34 to 48) | 0 | 37.0 | 0.0 | |
| Center passengers (Sta. 69 to 79) | 0 | 70.0 | 0.0 | |
| Aft passengers (Sta. 92 to 100) | 0 | 100.0 | 0.0 | |
| Baggage, arrangement IV (Sta. 109 to 145) | 0 | 127.0 | 0.0 | |
| Cargo A (Sta. 10 to 50, seats removed) | 0 | 33.0 | 0.0 | |
| Cargo B (Sta. 50 to 84, seats removed) | 0 | 67.0 | 0.0 | |
| Cargo C (Sta. 84 to 109, seats removed) | 0 | 96.0 | 0.0 | |
| Cargo D (Sta. 109 to 145) | 0 | 127.0 | 0.0 | |
| Fuel (standard 63 gal usable; long range 80 gal usable) | 30 USG | 180 | 47.9 | 8.6 |
| Engine oil (12 qts = 22 lb, no oil filter) | 10 USG | 60 | -18.2 | -1.1 |
| Zero fuel | 2210 | 33.9 | 75.0 | |
| Takeoff | 2390 | 35.0 | 83.6 |
Owner's Manual Section 4, pages 4-4 to 4-11: Sample Loading Problem (4-6), Loading Arrangements (4-7), Loading Graph (4-8), Center of Gravity Moment Envelope (4-9), Internal Cabin Dimensions (4-10) (pages 50-57 of u206f__poh__n9554g.pdf). For reference only; the aircraft’s flight manual and weighing report are the final authority. https://zulucheck.com/wb/type/cessna-u206f/
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