Cessna T210N Turbo Centurion weight & balance

Data source

POH Section 2 Weight Limits and Center of Gravity Limits (p. 2-7); Section 6, Figure 6-3 Loading Arrangements, Figure 6-5 Sample Loading Problem, Figure 6-7 Center of Gravity Moment Envelope, Figure 6-8 Center of Gravity Limits (pages 17-144 of t210n__poh__1982.pdf) · version type

• Station arms as printed in Figure 6-3 Loading Arrangements (p. 6-8): pilot and front passenger 37 (Sta 34 to 46), center passengers 71 (Sta 61 to 77), aft passengers or baggage on the folded aft seat 101, baggage on the wheel well 117, baggage aft of the wheel well 138 (baggage area centres); usable fuel 43.0.
• The aft baggage wall (approximately Sta 152) can be used as a reference for locating baggage.
• Baggage limits: 120 lb fwd of wheel well, 50 lb on wheel well, 200 lb aft of wheel well; combined on + aft of wheel well max 200 lb; combined all three areas max 240 lb.
• Maximum ramp weight 4016 lb. Takeoff above 3800 lb requires fuel burn-off to 3800 lb before landing (dashed takeoff-only area).
• Envelope from the printed CG limits: forward 37.0 in at 3000 lb or less, straight line to 43.9 in at 4000 lb (42.5 in at 3800 lb computed on that line); aft 53.0 in at 3800 lb or less, straight line to 52.0 in at 4000 lb. Lower edge 2000 lb is the chart's bottom, not a stated limit. Gear extended.
• Fuel: 87 gal usable standard tanks at 6 lb/gal; total tank capacity not printed on these pages (max set to usable). Reduced fuel option 64 gal. Unusable fuel 3 gal (18 lb at 38.0 in) is included in basic empty weight.
• Typical empty is the sample airplane (2362 lb, moment 99.5) from Figure 6-5; use your aircraft's actual weight and balance record.
• Read from the POH by ZuluCheck; the two machine readings disagreed (the second took the 3800 lb landing envelope as the top) and this was settled by reading the POH pages by hand; verify against your own manual.

For reference only. The aircraft’s approved flight manual and weighing report are the final authority.