At 74% power at 8,000 ft, the Cessna 182Q Skylane trues 143 KTAS on 12.7 gal/hr. Every other published setting is in the table below — not a single brochure number.
Continental O-470-U, 230 BHP at 2400 RPM.
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: C182Q POH §2 Fig. 2-1/2-2, §3, §4 p.4-3 — KIAS. TCDS 3A13 is the certificate basis only; it publishes no stall, climb or glide speeds. Vne/Vno/Vs0/Vs1 here are lower/higher than the 1979-model printing (179/143/45/48) — conservative, and pending an owner decision on which 182Q printing this entry declares
Cruise data: POH Figure 5-7 Cruise Performance, Section 5 (sheets 1-6)
True airspeed and fuel flow at every published power setting. 2,950 lb, recommended lean mixture, cowl flaps closed. For best fuel economy at 65% power or less, operate at the leanest mixture giving smooth operation, or at peak EGT if an EGT indicator is installed.
| Power | RPM | MP | KTAS | gal/hr |
|---|---|---|---|---|
| 2,000 ft pressure altitudestandard temp 11°C | ||||
| 74% | 2400 | 22.0 | 135 | 12.6 |
| 69% | 2400 | 21.0 | 132 | 11.8 |
| 65% | 2400 | 20.0 | 128 | 11.1 |
| 60% | 2400 | 19.0 | 124 | 10.3 |
| 75% | 2300 | 23.0 | 136 | 12.8 |
| 70% | 2300 | 22.0 | 133 | 12 |
| 66% | 2300 | 21.0 | 129 | 11.3 |
| 62% | 2300 | 20.0 | 125 | 10.5 |
| 70% | 2200 | 23.0 | 133 | 12 |
| 66% | 2200 | 22.0 | 129 | 11.3 |
| 62% | 2200 | 21.0 | 126 | 10.6 |
| 58% | 2200 | 20.0 | 122 | 9.9 |
| 66% | 2100 | 23.0 | 129 | 11.2 |
| 62% | 2100 | 22.0 | 126 | 10.5 |
| 58% | 2100 | 21.0 | 122 | 9.9 |
| 54% | 2100 | 20.0 | 118 | 9.3 |
| 50% | 2100 | 19.0 | 114 | 8.7 |
| 46% | 2100 | 18.0 | 109 | 8.1 |
| 4,000 ft pressure altitudestandard temp 7°C | ||||
| 76% | 2400 | 22.0 | 139 | 13 |
| 71% | 2400 | 21.0 | 136 | 12.1 |
| 66% | 2400 | 20.0 | 132 | 11.3 |
| 62% | 2400 | 19.0 | 128 | 10.6 |
| 76% | 2300 | 23.0 | 140 | 13.1 |
| 72% | 2300 | 22.0 | 136 | 12.3 |
| 68% | 2300 | 21.0 | 133 | 11.5 |
| 63% | 2300 | 20.0 | 129 | 10.8 |
| 72% | 2200 | 23.0 | 136 | 12.3 |
| 68% | 2200 | 22.0 | 133 | 11.6 |
| 64% | 2200 | 21.0 | 129 | 10.9 |
| 59% | 2200 | 20.0 | 126 | 10.2 |
| 55% | 2200 | 19.0 | 121 | 9.5 |
| 67% | 2100 | 23.0 | 133 | 11.5 |
| 63% | 2100 | 22.0 | 129 | 10.8 |
| 59% | 2100 | 21.0 | 126 | 10.1 |
| 55% | 2100 | 20.0 | 121 | 9.5 |
| 51% | 2100 | 19.0 | 117 | 8.9 |
| 47% | 2100 | 18.0 | 112 | 8.3 |
| 43% | 2100 | 17.0 | 107 | 7.8 |
| 6,000 ft pressure altitudestandard temp 3°C | ||||
| 77% | 2400 | 22.0 | 143 | 13.3 |
| 73% | 2400 | 21.0 | 139 | 12.4 |
| 68% | 2400 | 20.0 | 136 | 11.6 |
| 64% | 2400 | 19.0 | 132 | 10.8 |
| 74% | 2300 | 22.0 | 140 | 12.6 |
| 69% | 2300 | 21.0 | 137 | 11.8 |
| 65% | 2300 | 20.0 | 133 | 11.1 |
| 60% | 2300 | 19.0 | 129 | 10.3 |
| 69% | 2200 | 22.0 | 137 | 11.9 |
| 65% | 2200 | 21.0 | 133 | 11.1 |
| 61% | 2200 | 20.0 | 129 | 10.4 |
| 57% | 2200 | 19.0 | 125 | 9.7 |
| 65% | 2100 | 22.0 | 133 | 11.1 |
| 61% | 2100 | 21.0 | 129 | 10.4 |
| 53% | 2100 | 19.0 | 121 | 9.2 |
| 49% | 2100 | 18.0 | 116 | 8.6 |
| 45% | 2100 | 17.0 | 110 | 8 |
| 8,000 ft pressure altitudestandard temp -1°C | ||||
| 74% | 2400 | 21.0 | 143 | 12.7 |
| 70% | 2400 | 20.0 | 139 | 11.9 |
| 65% | 2400 | 19.0 | 135 | 11.1 |
| 60% | 2400 | 18.0 | 131 | 10.3 |
| 71% | 2300 | 21.0 | 140 | 12.1 |
| 66% | 2300 | 20.0 | 137 | 11.3 |
| 62% | 2300 | 19.0 | 132 | 10.6 |
| 58% | 2300 | 18.0 | 128 | 9.9 |
| 67% | 2200 | 21.0 | 137 | 11.4 |
| 63% | 2200 | 20.0 | 133 | 10.7 |
| 58% | 2200 | 19.0 | 129 | 10 |
| 54% | 2200 | 18.0 | 124 | 9.3 |
| 63% | 2100 | 21.0 | 133 | 10.7 |
| 59% | 2100 | 20.0 | 129 | 10 |
| 54% | 2100 | 19.0 | 124 | 9.4 |
| 50% | 2100 | 18.0 | 120 | 8.8 |
| 46% | 2100 | 17.0 | 114 | 8.2 |
| 10,000 ft pressure altitudestandard temp -5°C | ||||
| 71% | 2400 | 20.0 | 143 | 12.2 |
| 67% | 2400 | 19.0 | 139 | 11.4 |
| 62% | 2400 | 18.0 | 135 | 10.6 |
| 57% | 2400 | 17.0 | 130 | 9.8 |
| 68% | 2300 | 20.0 | 140 | 11.6 |
| 64% | 2300 | 19.0 | 136 | 10.9 |
| 59% | 2300 | 18.0 | 131 | 10.1 |
| 55% | 2300 | 17.0 | 126 | 9.4 |
| 64% | 2200 | 20.0 | 137 | 11 |
| 60% | 2200 | 19.0 | 132 | 10.2 |
| 56% | 2200 | 18.0 | 128 | 9.6 |
| 51% | 2200 | 17.0 | 123 | 8.9 |
| 60% | 2100 | 20.0 | 133 | 10.3 |
| 56% | 2100 | 19.0 | 128 | 9.6 |
| 52% | 2100 | 18.0 | 123 | 9 |
| 48% | 2100 | 17.0 | 118 | 8.4 |
| 44% | 2100 | 16.0 | 111 | 7.8 |
| 12,000 ft pressure altitudestandard temp -9°C | ||||
| 64% | 2400 | 18.0 | 139 | 10.9 |
| 59% | 2400 | 17.0 | 133 | 10.1 |
| 54% | 2400 | 16.0 | 128 | 9.4 |
| 50% | 2400 | 15.0 | 121 | 8.7 |
| 61% | 2300 | 18.0 | 135 | 10.4 |
| 56% | 2300 | 17.0 | 130 | 9.7 |
| 52% | 2300 | 16.0 | 125 | 9 |
| 47% | 2300 | 15.0 | 118 | 8.3 |
| 57% | 2200 | 18.0 | 131 | 9.8 |
| 53% | 2200 | 17.0 | 126 | 9.2 |
| 49% | 2200 | 16.0 | 120 | 8.5 |
| 44% | 2200 | 15.0 | 113 | 7.9 |
| 54% | 2100 | 18.0 | 127 | 9.3 |
| 49% | 2100 | 17.0 | 121 | 8.7 |
| 45% | 2100 | 16.0 | 115 | 8.1 |
Carbureted 230 HP with constant-speed prop. Uses CARB HEAT. 1979+ has wet-wing fuel system (88 gal) vs earlier bladder tanks (75 gal).
FlightKit holds the digitized POH takeoff and landing tables for the Cessna 182Q Skylane, interpolated for your actual weight, pressure altitude, temperature and wind in the app.
At 74% power at 8,000 ft pressure altitude, the Cessna 182Q Skylane trues 143 KTAS according to C182Q POH §2 Fig. 2-1/2-2, §3, §4 p.4-3 — KIAS. TCDS 3A13 is the certificate basis only; it publishes no stall, climb or glide speeds. Vne/Vno/Vs0/Vs1 here are lower/higher than the 1979-model printing (179/143/45/48) — conservative, and pending an owner decision on which 182Q printing this entry declares. The full table below publishes 104 power settings across 6 altitudes.
12.7 gal/hr at 74% power at 8,000 ft. Fuel flow varies with altitude and power setting — the table below gives the published figure for every combination.
176 KIAS — Never Exceed.
2950 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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