At 72% power at 8,000 ft, the Cessna 182T Skylane trues 139 KTAS on 12.5 gal/hr. Every other published setting is in the table below — not a single brochure number.
Nav III. Cruise data at 3,100 lb, recommended lean mixture, cowl flaps closed.
Published POH values for a standard production model
These are the manufacturer’s published figures, not cross-checked against an individual airframe. Always verify against your aircraft’s own POH before flight.
Specs: 182T Information Manual §2/§4 — verify against your aircraft's POH
Cruise data: POH 182TPHAUS-00, Figure 5-9 Cruise Performance, Section 5 (sheets 1-11) — copy 182TPHAUS-04, S/N 18281780
True airspeed and fuel flow at every published power setting. Applies to: Nav III. 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 | ||||
| 81%not recommended | 2400 | 25.0 | 136 | 14 |
| 76% | 2400 | 24.0 | 133 | 13.2 |
| 71% | 2400 | 23.0 | 130 | 12.4 |
| 67% | 2400 | 22.0 | 127 | 11.7 |
| 62% | 2400 | 21.0 | 122 | 11.1 |
| 58% | 2400 | 20.0 | 118 | 10.4 |
| 82%not recommended | 2300 | 26.0 | 137 | 14.2 |
| 78% | 2300 | 25.0 | 135 | 13.4 |
| 73% | 2300 | 24.0 | 132 | 12.7 |
| 69% | 2300 | 23.0 | 128 | 12 |
| 65% | 2300 | 22.0 | 124 | 11.4 |
| 60% | 2300 | 21.0 | 120 | 10.8 |
| 56% | 2300 | 20.0 | 116 | 10.2 |
| 83%not recommended | 2200 | 27.0 | 137 | 14.4 |
| 79% | 2200 | 26.0 | 135 | 13.6 |
| 75% | 2200 | 25.0 | 133 | 12.9 |
| 71% | 2200 | 24.0 | 130 | 12.3 |
| 66% | 2200 | 23.0 | 126 | 11.7 |
| 62% | 2200 | 22.0 | 122 | 11.1 |
| 58% | 2200 | 21.0 | 119 | 10.5 |
| 54% | 2200 | 20.0 | 114 | 9.9 |
| 79% | 2100 | 27.0 | 135 | 13.7 |
| 75% | 2100 | 26.0 | 133 | 13 |
| 71% | 2100 | 25.0 | 130 | 12.4 |
| 67% | 2100 | 24.0 | 127 | 11.8 |
| 63% | 2100 | 23.0 | 123 | 11.2 |
| 59% | 2100 | 22.0 | 120 | 10.6 |
| 55% | 2100 | 21.0 | 116 | 10.1 |
| 51% | 2100 | 20.0 | 111 | 9.6 |
| 75% | 2000 | 27.0 | 133 | 13 |
| 71% | 2000 | 26.0 | 130 | 12.4 |
| 67% | 2000 | 25.0 | 127 | 11.8 |
| 64% | 2000 | 24.0 | 124 | 11.3 |
| 60% | 2000 | 23.0 | 120 | 10.7 |
| 56% | 2000 | 22.0 | 117 | 10.2 |
| 53% | 2000 | 21.0 | 112 | 9.7 |
| 49% | 2000 | 20.0 | 108 | 9.2 |
| 2,000 ft pressure altitudestandard temp 11°C | ||||
| 83%not recommended | 2400 | 25.0 | 140 | 14.4 |
| 79% | 2400 | 24.0 | 138 | 13.6 |
| 74% | 2400 | 23.0 | 134 | 12.8 |
| 69% | 2400 | 22.0 | 131 | 12.1 |
| 65% | 2400 | 21.0 | 126 | 11.4 |
| 60% | 2400 | 20.0 | 122 | 10.7 |
| 80% | 2300 | 25.0 | 139 | 13.9 |
| 76% | 2300 | 24.0 | 136 | 13.1 |
| 71% | 2300 | 23.0 | 133 | 12.4 |
| 67% | 2300 | 22.0 | 128 | 11.7 |
| 62% | 2300 | 21.0 | 124 | 11.1 |
| 58% | 2300 | 20.0 | 120 | 10.5 |
| 81%not recommended | 2200 | 26.0 | 139 | 14.1 |
| 77% | 2200 | 25.0 | 137 | 13.3 |
| 73% | 2200 | 24.0 | 134 | 12.6 |
| 69% | 2200 | 23.0 | 130 | 12 |
| 64% | 2200 | 22.0 | 126 | 11.4 |
| 60% | 2200 | 21.0 | 122 | 10.8 |
| 56% | 2200 | 20.0 | 118 | 10.2 |
| 77% | 2100 | 26.0 | 137 | 13.4 |
| 73% | 2100 | 25.0 | 134 | 12.7 |
| 69% | 2100 | 24.0 | 131 | 12.1 |
| 65% | 2100 | 23.0 | 127 | 11.5 |
| 61% | 2100 | 22.0 | 123 | 10.9 |
| 57% | 2100 | 21.0 | 119 | 10.4 |
| 53% | 2100 | 20.0 | 115 | 9.8 |
| 73% | 2000 | 26.0 | 134 | 12.7 |
| 69% | 2000 | 25.0 | 131 | 12.1 |
| 66% | 2000 | 24.0 | 127 | 11.5 |
| 62% | 2000 | 23.0 | 124 | 11 |
| 58% | 2000 | 22.0 | 120 | 10.5 |
| 54% | 2000 | 21.0 | 116 | 10 |
| 51% | 2000 | 20.0 | 112 | 9.4 |
| 4,000 ft pressure altitudestandard temp 7°C | ||||
| 81%not recommended | 2400 | 24.0 | 142 | 14 |
| 76% | 2400 | 23.0 | 139 | 13.2 |
| 72% | 2400 | 22.0 | 135 | 12.5 |
| 67% | 2400 | 21.0 | 131 | 11.7 |
| 62% | 2400 | 20.0 | 126 | 11.1 |
| 83%not recommended | 2300 | 25.0 | 143 | 14.3 |
| 78% | 2300 | 24.0 | 140 | 13.5 |
| 74% | 2300 | 23.0 | 137 | 12.8 |
| 69% | 2300 | 22.0 | 133 | 12.1 |
| 65% | 2300 | 21.0 | 128 | 11.4 |
| 60% | 2300 | 20.0 | 124 | 10.7 |
| 79% | 2200 | 25.0 | 141 | 13.7 |
| 75% | 2200 | 24.0 | 138 | 13 |
| 71% | 2200 | 23.0 | 134 | 12.3 |
| 66% | 2200 | 22.0 | 130 | 11.7 |
| 62% | 2200 | 21.0 | 126 | 11 |
| 58% | 2200 | 20.0 | 122 | 10.4 |
| 75% | 2100 | 25.0 | 138 | 13 |
| 71% | 2100 | 24.0 | 135 | 12.4 |
| 67% | 2100 | 23.0 | 131 | 11.8 |
| 63% | 2100 | 22.0 | 127 | 11.2 |
| 59% | 2100 | 21.0 | 123 | 10.6 |
| 55% | 2100 | 20.0 | 119 | 10.1 |
| 71% | 2000 | 25.0 | 135 | 12.4 |
| 68% | 2000 | 24.0 | 131 | 11.8 |
| 64% | 2000 | 23.0 | 128 | 11.3 |
| 60% | 2000 | 22.0 | 124 | 10.7 |
| 56% | 2000 | 21.0 | 120 | 10.2 |
| 52% | 2000 | 20.0 | 115 | 9.7 |
| 6,000 ft pressure altitudestandard temp 3°C | ||||
| 79% | 2400 | 23.0 | 143 | 13.6 |
| 74% | 2400 | 22.0 | 139 | 12.8 |
| 69% | 2400 | 21.0 | 135 | 12.1 |
| 65% | 2400 | 20.0 | 130 | 11.4 |
| 60% | 2400 | 19.0 | 126 | 10.7 |
| 76% | 2300 | 23.0 | 141 | 13.1 |
| 71% | 2300 | 22.0 | 137 | 12.4 |
| 67% | 2300 | 21.0 | 133 | 11.7 |
| 62% | 2300 | 20.0 | 128 | 11 |
| 58% | 2300 | 19.0 | 123 | 10.4 |
| 73% | 2200 | 23.0 | 138 | 12.6 |
| 69% | 2200 | 22.0 | 134 | 12 |
| 64% | 2200 | 21.0 | 130 | 11.3 |
| 60% | 2200 | 20.0 | 126 | 10.7 |
| 56% | 2200 | 19.0 | 121 | 10.1 |
| 69% | 2100 | 23.0 | 135 | 12.1 |
| 65% | 2100 | 22.0 | 131 | 11.5 |
| 61% | 2100 | 21.0 | 127 | 10.9 |
| 57% | 2100 | 20.0 | 122 | 10.3 |
| 53% | 2100 | 19.0 | 118 | 9.8 |
| 66% | 2000 | 23.0 | 132 | 11.5 |
| 62% | 2000 | 22.0 | 128 | 11 |
| 58% | 2000 | 21.0 | 123 | 10.4 |
| 54% | 2000 | 20.0 | 119 | 9.9 |
| 50% | 2000 | 19.0 | 114 | 9.4 |
| 8,000 ft pressure altitudestandard temp -1°C | ||||
| 72% | 2400 | 21.0 | 139 | 12.5 |
| 67% | 2400 | 20.0 | 135 | 11.7 |
| 62% | 2400 | 19.0 | 130 | 11 |
| 57% | 2400 | 18.0 | 124 | 10.3 |
| 69% | 2300 | 21.0 | 137 | 12 |
| 64% | 2300 | 20.0 | 132 | 11.3 |
| 60% | 2300 | 19.0 | 127 | 10.7 |
| 55% | 2300 | 18.0 | 122 | 10.1 |
| 66% | 2200 | 21.0 | 134 | 11.6 |
| 62% | 2200 | 20.0 | 130 | 11 |
| 57% | 2200 | 19.0 | 125 | 10.4 |
| 53% | 2200 | 18.0 | 119 | 9.8 |
| 63% | 2100 | 21.0 | 131 | 11.2 |
| 59% | 2100 | 20.0 | 126 | 10.6 |
| 55% | 2100 | 19.0 | 121 | 10 |
| 50% | 2100 | 18.0 | 116 | 9.4 |
| 60% | 2000 | 21.0 | 127 | 10.7 |
| 56% | 2000 | 20.0 | 123 | 10.1 |
| 52% | 2000 | 19.0 | 118 | 9.6 |
| 10,000 ft pressure altitudestandard temp -5°C | ||||
| 69% | 2400 | 20.0 | 139 | 12.1 |
| 64% | 2400 | 19.0 | 134 | 11.3 |
| 59% | 2400 | 18.0 | 129 | 10.6 |
| 71% | 2300 | 21.0 | 141 | 12.4 |
| 66% | 2300 | 20.0 | 137 | 11.7 |
| 62% | 2300 | 19.0 | 132 | 11 |
| 57% | 2300 | 18.0 | 126 | 10.3 |
| 64% | 2200 | 20.0 | 134 | 11.3 |
| 59% | 2200 | 19.0 | 129 | 10.6 |
| 55% | 2200 | 18.0 | 123 | 10 |
| 61% | 2100 | 20.0 | 130 | 10.8 |
| 56% | 2100 | 19.0 | 125 | 10.2 |
| 52% | 2100 | 18.0 | 120 | 9.7 |
| 58% | 2000 | 20.0 | 127 | 10.4 |
| 54% | 2000 | 19.0 | 122 | 9.8 |
| 50% | 2000 | 18.0 | 116 | 9.3 |
| 12,000 ft pressure altitudestandard temp -9°C | ||||
| 61% | 2400 | 18.0 | 133 | 10.9 |
| 56% | 2400 | 17.0 | 127 | 10.2 |
| 51% | 2400 | 16.0 | 120 | 9.6 |
| 59% | 2300 | 18.0 | 130 | 10.6 |
| 54% | 2300 | 17.0 | 124 | 10 |
| 50% | 2300 | 16.0 | 118 | 9.3 |
| 57% | 2200 | 18.0 | 128 | 10.3 |
| 52% | 2200 | 17.0 | 121 | 9.7 |
| 54% | 2100 | 18.0 | 124 | 9.9 |
| 50% | 2100 | 17.0 | 118 | 9.3 |
| 55% | 2000 | 19.0 | 125 | 10.1 |
| 51% | 2000 | 18.0 | 120 | 9.5 |
| 14,000 ft pressure altitudestandard temp -13°C | ||||
| 53% | 2400 | 16.0 | 125 | 9.8 |
| 48% | 2400 | 15.0 | 117 | 9.1 |
| 51% | 2300 | 16.0 | 122 | 9.6 |
| 49% | 2200 | 16.0 | 119 | 9.3 |
| 47% | 2100 | 16.0 | 115 | 8.9 |
Constant-speed prop, fuel injected (ALT AIR, no carb heat), G1000 avionics
FlightKit holds the digitized POH takeoff and landing tables for the Cessna 182T Skylane, interpolated for your actual weight, pressure altitude, temperature and wind in the app.
At 72% power at 8,000 ft pressure altitude, the Cessna 182T Skylane trues 139 KTAS according to 182T Information Manual §2/§4 — verify against your aircraft's POH. The full table below publishes 176 power settings across 8 altitudes.
12.5 gal/hr at 72% 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 Gross 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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