V-speeds, cruise performance, fuel, and weights, digitized from the POH for planning and study.
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Piper PA-28R-200 Arrow preflight numbers at a glance: max gross weight 2650 lb, typical useful load 1010 lb, 48 gal usable fuel, cruise up to about 145.1 KTAS (POH figure at 8000 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 | Lycoming IO-360-C1C (200 HP) |
| Propeller | Hartzell HC-C2YK-1BF/F7690A |
| Max gross weight | 2650 lb |
| Empty weight (typical) | 1640 lb |
| Useful load (typical) | 1010 lb |
| Usable fuel | 48 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 | 56 kt | Stall, landing configuration |
| VS1 | 62 kt | Stall, clean configuration |
| VX | 83 kt | Best angle of climb |
| VY | 87 kt | Best rate of climb |
| VA | 114 kt | Design maneuvering speed (at max gross) |
| VFE | 109 kt | Max flaps extended |
| VNO | 148 kt | Max structural cruising |
| VNE | 186 kt | Never exceed |
| Best glide | 91 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) | RPM | TAS (kt) | Fuel (GPH) |
|---|---|---|---|
| 2000 | 2100 | 134.1 | 8.9 |
| 2000 | 2400 | 138 | 10 |
| 2000 | 2600 | 140.6 | 10.8 |
| 4000 | 2100 | 135.6 | 8.7 |
| 4000 | 2400 | 139.5 | 9.8 |
| 4000 | 2600 | 142.1 | 10.6 |
| 6000 | 2100 | 137.1 | 8.6 |
| 6000 | 2400 | 141 | 9.7 |
| 6000 | 2600 | 143.6 | 10.5 |
| 8000 | 2100 | 138.6 | 8.4 |
| 8000 | 2400 | 142.5 | 9.6 |
| 8000 | 2600 | 145.1 | 10.3 |
Standard-day (ISA) rows shown, sampled across the POH table for readability; the FlightDecide app carries the full digitized table, including non-standard temperatures.
Book figures at 2650 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 | 1100 ft |
| Takeoff over a 50 ft obstacle | 1595 ft |
| Landing ground roll | 530 ft |
| Landing over a 50 ft obstacle | 900 ft |
| Rate of climb | 830 fpm |
See how density altitude stretches these distances on a hot day.
Common QuestionsPer the POH cruise table, up to about 145.1 KTAS at 8000 ft on a standard day, burning roughly 10.3 GPH at that setting. Typical everyday cruise settings run slower and leaner; see the table above.
48 gallons usable. At a high-cruise burn of 10.3 GPH that is roughly 4.7 hours to dry tanks. Plan with reserves, never to zero.
About 1010 lb for a typically equipped example (2650 lb max gross minus a typical empty weight of 1640 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 186 kt and VNO (max structural cruising) is 148 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: Piper PA-28R-200 Arrow Pilot's Operating Handbook, Piper Aircraft Corporation Data synced from the FlightDecide aircraft library on 2026-07-17.