At 69% power at 8,000 ft, the Cessna 182S Skylane trues 133 KTAS on 11.6 gal/hr. Every other published setting is in the table below — not a single brochure number.
Textron Lycoming IO-540-AB1A5, 230 BHP at 2400 RPM.
Cross-checked against the POH for this model
Verified against the POH for this variant. Always fly your own aircraft’s POH — equipment and modifications change the numbers.
Specs: Cessna 182S Information Manual P/N 182SIM §2/§5 — verify against your aircraft's POH
Cruise data: POH Figure 5-9 Cruise Performance, Section 5 (sheets 1-10)
True airspeed and fuel flow at every published power setting. 3,100 lb, recommended lean mixture, cowl flaps closed. Maximum cruise power is 80% MCP; powers above that are printed for interpolation only. For best economy, operate at peak EGT.
| Power | RPM | MP | KTAS | gal/hr |
|---|---|---|---|---|
| 0 ft pressure altitudestandard temp 15°C | ||||
| 82%not recommended | 2400 | 26.0 | 134 | 13.7 |
| 77% | 2400 | 25.0 | 131 | 13 |
| 73% | 2400 | 24.0 | 127 | 12.3 |
| 69% | 2400 | 23.0 | 124 | 11.6 |
| 64% | 2400 | 22.0 | 121 | 10.9 |
| 60% | 2400 | 21.0 | 117 | 10.3 |
| 55% | 2400 | 20.0 | 113 | 9.7 |
| 83%not recommended | 2300 | 27.0 | 134 | 13.9 |
| 79% | 2300 | 26.0 | 132 | 13.2 |
| 75% | 2300 | 25.0 | 129 | 12.5 |
| 70% | 2300 | 24.0 | 126 | 11.9 |
| 66% | 2300 | 23.0 | 123 | 11.2 |
| 62% | 2300 | 22.0 | 119 | 10.6 |
| 58% | 2300 | 21.0 | 115 | 10 |
| 54% | 2300 | 20.0 | 111 | 9.4 |
| 80% | 2200 | 27.0 | 132 | 13.3 |
| 76% | 2200 | 26.0 | 129 | 12.7 |
| 72% | 2200 | 25.0 | 126 | 12.1 |
| 68% | 2200 | 24.0 | 124 | 11.5 |
| 64% | 2200 | 23.0 | 121 | 10.9 |
| 60% | 2200 | 22.0 | 117 | 10.3 |
| 56% | 2200 | 21.0 | 113 | 9.7 |
| 52% | 2200 | 20.0 | 109 | 9.2 |
| 76% | 2100 | 27.0 | 130 | 12.7 |
| 72% | 2100 | 26.0 | 127 | 12.1 |
| 68% | 2100 | 25.0 | 124 | 11.5 |
| 64% | 2100 | 24.0 | 121 | 11 |
| 61% | 2100 | 23.0 | 117 | 10.4 |
| 57% | 2100 | 22.0 | 114 | 9.9 |
| 53% | 2100 | 21.0 | 111 | 9.4 |
| 72% | 2000 | 27.0 | 127 | 12.1 |
| 68% | 2000 | 26.0 | 124 | 11.5 |
| 65% | 2000 | 25.0 | 122 | 11 |
| 61% | 2000 | 24.0 | 118 | 10.5 |
| 58% | 2000 | 23.0 | 115 | 10 |
| 54% | 2000 | 22.0 | 111 | 9.5 |
| 50% | 2000 | 21.0 | 108 | 9 |
| 2,000 ft pressure altitudestandard temp 11°C | ||||
| 80% | 2400 | 25.0 | 135 | 13.4 |
| 75% | 2400 | 24.0 | 131 | 12.7 |
| 71% | 2400 | 23.0 | 128 | 12 |
| 67% | 2400 | 22.0 | 125 | 11.3 |
| 62% | 2400 | 21.0 | 120 | 10.6 |
| 58% | 2400 | 20.0 | 117 | 10 |
| 81%not recommended | 2300 | 26.0 | 136 | 13.6 |
| 77% | 2300 | 25.0 | 132 | 12.9 |
| 73% | 2300 | 24.0 | 129 | 12.2 |
| 68% | 2300 | 23.0 | 126 | 11.6 |
| 64% | 2300 | 22.0 | 123 | 10.9 |
| 60% | 2300 | 21.0 | 119 | 10.3 |
| 56% | 2300 | 20.0 | 115 | 9.7 |
| 78% | 2200 | 26.0 | 133 | 13.1 |
| 74% | 2200 | 25.0 | 130 | 12.4 |
| 70% | 2200 | 24.0 | 127 | 11.8 |
| 66% | 2200 | 23.0 | 124 | 11.2 |
| 62% | 2200 | 22.0 | 120 | 10.6 |
| 58% | 2200 | 21.0 | 117 | 10 |
| 54% | 2200 | 20.0 | 113 | 9.4 |
| 74% | 2100 | 26.0 | 130 | 12.4 |
| 70% | 2100 | 25.0 | 128 | 11.8 |
| 66% | 2100 | 24.0 | 125 | 11.3 |
| 63% | 2100 | 23.0 | 121 | 10.7 |
| 59% | 2100 | 22.0 | 118 | 10.2 |
| 55% | 2100 | 21.0 | 114 | 9.6 |
| 51% | 2100 | 20.0 | 110 | 9.1 |
| 70% | 2000 | 26.0 | 128 | 11.8 |
| 67% | 2000 | 25.0 | 125 | 11.3 |
| 63% | 2000 | 24.0 | 121 | 10.8 |
| 59% | 2000 | 23.0 | 118 | 10.2 |
| 56% | 2000 | 22.0 | 115 | 9.7 |
| 52% | 2000 | 21.0 | 111 | 9.2 |
| 4,000 ft pressure altitudestandard temp 7°C | ||||
| 82%not recommended | 2400 | 25.0 | 139 | 13.8 |
| 78% | 2400 | 24.0 | 135 | 13 |
| 73% | 2400 | 23.0 | 132 | 12.3 |
| 69% | 2400 | 22.0 | 129 | 11.6 |
| 64% | 2400 | 21.0 | 124 | 10.9 |
| 60% | 2400 | 20.0 | 121 | 10.3 |
| 79% | 2300 | 25.0 | 136 | 13.3 |
| 75% | 2300 | 24.0 | 133 | 12.6 |
| 71% | 2300 | 23.0 | 130 | 11.9 |
| 66% | 2300 | 22.0 | 126 | 11.2 |
| 62% | 2300 | 21.0 | 123 | 10.6 |
| 58% | 2300 | 20.0 | 119 | 10 |
| 76% | 2200 | 25.0 | 134 | 12.7 |
| 72% | 2200 | 24.0 | 131 | 12.1 |
| 68% | 2200 | 23.0 | 128 | 11.5 |
| 64% | 2200 | 22.0 | 124 | 10.9 |
| 60% | 2200 | 21.0 | 121 | 10.3 |
| 56% | 2200 | 20.0 | 116 | 9.7 |
| 72% | 2100 | 25.0 | 132 | 12.2 |
| 68% | 2100 | 24.0 | 129 | 11.6 |
| 65% | 2100 | 23.0 | 125 | 11 |
| 61% | 2100 | 22.0 | 122 | 10.4 |
| 57% | 2100 | 21.0 | 118 | 9.9 |
| 53% | 2100 | 20.0 | 114 | 9.3 |
| 69% | 2000 | 25.0 | 129 | 11.6 |
| 65% | 2000 | 24.0 | 125 | 11 |
| 61% | 2000 | 23.0 | 122 | 10.5 |
| 58% | 2000 | 22.0 | 118 | 10 |
| 54% | 2000 | 21.0 | 115 | 9.5 |
| 6,000 ft pressure altitudestandard temp 3°C | ||||
| 76% | 2400 | 23.0 | 136 | 12.7 |
| 71% | 2400 | 22.0 | 133 | 12 |
| 67% | 2400 | 21.0 | 128 | 11.3 |
| 62% | 2400 | 20.0 | 125 | 10.6 |
| 57% | 2400 | 19.0 | 120 | 10 |
| 73% | 2300 | 23.0 | 134 | 12.2 |
| 68% | 2300 | 22.0 | 130 | 11.6 |
| 64% | 2300 | 21.0 | 127 | 10.9 |
| 60% | 2300 | 20.0 | 122 | 10.3 |
| 55% | 2300 | 19.0 | 118 | 9.7 |
| 70% | 2200 | 23.0 | 132 | 11.8 |
| 66% | 2200 | 22.0 | 128 | 11.2 |
| 62% | 2200 | 21.0 | 124 | 10.6 |
| 57% | 2200 | 20.0 | 120 | 10 |
| 53% | 2200 | 19.0 | 116 | 9.4 |
| 66% | 2100 | 23.0 | 128 | 11.3 |
| 63% | 2100 | 22.0 | 125 | 10.7 |
| 59% | 2100 | 21.0 | 121 | 10.1 |
| 55% | 2100 | 20.0 | 117 | 9.6 |
| 51% | 2100 | 19.0 | 113 | 9 |
| 63% | 2000 | 23.0 | 126 | 10.8 |
| 59% | 2000 | 22.0 | 122 | 10.2 |
| 56% | 2000 | 21.0 | 118 | 9.7 |
| 52% | 2000 | 20.0 | 114 | 9.2 |
| 48% | 2000 | 19.0 | 109 | 8.7 |
| 8,000 ft pressure altitudestandard temp -1°C | ||||
| 69% | 2400 | 21.0 | 133 | 11.6 |
| 64% | 2400 | 20.0 | 129 | 10.9 |
| 59% | 2400 | 19.0 | 124 | 10.3 |
| 55% | 2400 | 18.0 | 119 | 9.6 |
| 66% | 2300 | 21.0 | 131 | 11.2 |
| 62% | 2300 | 20.0 | 126 | 10.6 |
| 57% | 2300 | 19.0 | 122 | 9.9 |
| 53% | 2300 | 18.0 | 117 | 9.3 |
| 64% | 2200 | 21.0 | 128 | 10.8 |
| 59% | 2200 | 20.0 | 124 | 10.2 |
| 55% | 2200 | 19.0 | 120 | 9.6 |
| 51% | 2200 | 18.0 | 114 | 9 |
| 60% | 2100 | 21.0 | 125 | 10.4 |
| 56% | 2100 | 20.0 | 121 | 9.8 |
| 52% | 2100 | 19.0 | 116 | 9.3 |
| 48% | 2100 | 18.0 | 111 | 8.7 |
| 57% | 2000 | 21.0 | 122 | 9.9 |
| 54% | 2000 | 20.0 | 118 | 9.4 |
| 50% | 2000 | 19.0 | 113 | 8.9 |
| 10,000 ft pressure altitudestandard temp -5°C | ||||
| 66% | 2400 | 20.0 | 133 | 11.2 |
| 62% | 2400 | 19.0 | 128 | 10.6 |
| 57% | 2400 | 18.0 | 123 | 9.9 |
| 64% | 2300 | 20.0 | 131 | 10.9 |
| 59% | 2300 | 19.0 | 126 | 10.2 |
| 55% | 2300 | 18.0 | 121 | 9.6 |
| 61% | 2200 | 20.0 | 128 | 10.5 |
| 57% | 2200 | 19.0 | 124 | 9.9 |
| 53% | 2200 | 18.0 | 118 | 9.3 |
| 58% | 2100 | 20.0 | 125 | 10.1 |
| 54% | 2100 | 19.0 | 120 | 9.5 |
| 50% | 2100 | 18.0 | 114 | 8.9 |
| 55% | 2000 | 20.0 | 122 | 9.6 |
| 51% | 2000 | 19.0 | 116 | 9.1 |
| 48% | 2000 | 18.0 | 110 | 8.6 |
| 12,000 ft pressure altitudestandard temp -9°C | ||||
| 59% | 2400 | 18.0 | 128 | 10.2 |
| 54% | 2400 | 17.0 | 121 | 9.5 |
| 49% | 2400 | 16.0 | 114 | 8.8 |
| 57% | 2300 | 18.0 | 125 | 9.9 |
| 52% | 2300 | 17.0 | 119 | 9.2 |
| 48% | 2300 | 16.0 | 111 | 8.6 |
| 54% | 2200 | 18.0 | 122 | 9.5 |
| 50% | 2200 | 17.0 | 115 | 8.9 |
| 52% | 2100 | 18.0 | 118 | 9.2 |
| 48% | 2100 | 17.0 | 112 | 8.6 |
| 49% | 2000 | 18.0 | 114 | 8.8 |
| 14,000 ft pressure altitudestandard temp -13°C | ||||
| 51% | 2400 | 16.0 | 118 | 9.1 |
| 46% | 2400 | 15.0 | 109 | 8.4 |
| 49% | 2300 | 16.0 | 115 | 8.8 |
| 47% | 2200 | 16.0 | 111 | 8.6 |
| 45% | 2100 | 16.0 | 105 | 8.2 |
High-wing, fuel injected, constant-speed prop — high performance. Distance tables are SHORT FIELD technique (Flaps 20° takeoff, Flaps FULL landing), the only ones the book publishes.
FlightKit holds the digitized POH takeoff and landing tables for the Cessna 182S Skylane, interpolated for your actual weight, pressure altitude, temperature and wind in the app.
At 69% power at 8,000 ft pressure altitude, the Cessna 182S Skylane trues 133 KTAS according to Cessna 182S Information Manual P/N 182SIM §2/§5 — verify against your aircraft's POH. The full table below publishes 174 power settings across 8 altitudes.
11.6 gal/hr at 69% power at 8,000 ft. Fuel flow varies with altitude and power setting — the table below gives the published figure for every combination.
175 KIAS — Never Exceed.
3100 lbs (Max Takeoff Weight).
All aircraft cruise performance data — every published power setting, from the POH.
FlightKit interpolates this table for your actual altitude and temperature, remembers your aircraft, and works offline in the cockpit.
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