V-speeds, cruise performance, fuel, and weights, digitized from the POH for planning and study.
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Piper PA-44-180 Seminole preflight numbers at a glance: max gross weight 3800 lb, typical useful load 1266 lb, 108 gal usable fuel, cruise up to about 162 KTAS (POH figure at 2000 ft, standard day). All figures below come from the FlightDecide curated aircraft library, digitized from the published POH/AFM. Use them for planning and study, and confirm against the POH for your specific serial number before flight.
| Engine | 2x Lycoming O-360-A1H6 (180 HP each) |
| Propeller | Hartzell HC-M2YR-2/C8045A-6 |
| Max gross weight | 3800 lb |
| Empty weight (typical) | 2534 lb |
| Useful load (typical) | 1266 lb |
| Usable fuel | 108 gal |
Knots indicated (KIAS) unless the POH states otherwise. Speeds vary by model year and serial; the placarded speeds and your POH govern.
| Speed | Value | Meaning |
|---|---|---|
| VS0 | 55 kt | Stall, landing configuration |
| VS1 | 57 kt | Stall, clean configuration |
| VX | 82 kt | Best angle of climb |
| VY | 88 kt | Best rate of climb |
| VXSE | 82 kt | Best angle of climb, single engine |
| VYSE | 88 kt | Best rate of climb, single engine |
| VA | 135 kt | Design maneuvering speed (at max gross) |
| VFE | 111 kt | Max flaps extended |
| VNO | 169 kt | Max structural cruising |
| VNE | 202 kt | Never exceed |
| VMC | 56 kt | Min control, one engine inoperative |
| Best glide | 88 kt | Best glide speed |
Transcribed from the POH cruise tables. True airspeed and fuel flow depend on altitude, power setting, temperature, and leaning technique.
| Pressure alt (ft) | MP (inHg) | % power | TAS (kt) | Fuel (GPH) |
|---|---|---|---|---|
| 2000 | 21.7 | 55 | 138 | 17.4 |
| 2000 | 24.2 | 65 | 152 | 20.4 |
| 2000 | 25.9 | 75 | 162 | 23.4 |
| 4000 | — | 75 | 162 | 23.4 |
| 5000 | 23.2 | 65 | 152 | 20.4 |
| 5500 | — | 55 | 138 | 17.4 |
| 6000 | — | 75 | 162 | 23.4 |
| 8000 | 20 | 55 | 138 | 17.4 |
| 8000 | — | 65 | 152 | 20.4 |
| 12,000 | — | 55 | 138 | 17.4 |
Book figures at 3800 lb, 0 ft pressure altitude, 15 °C. Real-world technique, wind, surface, and density altitude move these substantially, so apply your own margin (many pilots use 1.5× the book number) and run the numbers for the actual conditions.
| POH figure | Distance |
|---|---|
| Takeoff ground roll | 1400 ft |
| Takeoff over a 50 ft obstacle | 1950 ft |
| Landing ground roll | 590 ft |
| Landing over a 50 ft obstacle | 1350 ft |
| Rate of climb | 1340 fpm |
See how density altitude stretches these distances on a hot day.
Common QuestionsPer the POH cruise table, up to about 162 KTAS at 2000 ft on a standard day, burning roughly 23.4 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.
108 gallons usable. At a high-cruise burn of 23.4 GPH that is roughly 4.6 hours to dry tanks. Plan with reserves, never to zero.
About 1266 lb for a typically equipped example (3800 lb max gross minus a typical empty weight of 2534 lb). Your aircraft's actual empty weight and CG come from its own weight-and-balance records. Always use those, not type averages.
VNE (never exceed) is 202 kt and VNO (max structural cruising) is 169 kt. Full V-speed table above; verify against the POH for your serial.
Check today's wind against your personal crosswind maximum.
See what heat and elevation do to these takeoff and climb numbers.
Fold these numbers into a structured preflight decision.
FlightDecide ships this aircraft as a built-in profile: it computes your fuel, weight and balance, and takeoff/landing performance for the actual conditions, scores 8 risk categories against your personal minimums, and explains the result in plain language.
Get FlightDecide on the App StoreReference data for planning and study: approximate, and not a substitute for the FAA-approved AFM/POH for your specific aircraft, an official weather briefing, or your judgment as pilot in command (14 CFR 91.3). Source: PA-44-180 Seminole POH, Piper Aircraft Corporation | FD-215: cruise re-digitized on POH axis (best_power, medium conf), fuel total both-engines for twins. Data synced from the FlightDecide aircraft library on 2026-07-17.