Piper PA-28R-200 Arrow II weight and balance and performance calculator
Calculate the weight and balance of the Piper PA-28R-200 Arrow II online: enter people, baggage and fuel and get the takeoff mass, the CG and whether both are within the limits of the POH – plus the takeoff and landing distance for your airfield, temperature and wind. Free, no sign-up. The Piper PA-28R-200 Arrow II is a model of the Piper PA-28R Arrow; built 1972–1976.
* MTOW, sea level, 15 °C, no wind – BriefingPal result from the POH data
Calculate the Piper PA-28R-200 Arrow II weight, CG and takeoff distance
Your own empty mass (weighing report, optional)
The POH has no standard empty moment for this model – enter the empty mass CG from your weighing report to get the CG.
Leave empty to use the typical POH empty mass. Your aircraft's weighing report is what counts.
Calculated on the BriefingPal server from the POH data. Nothing is stored, no cookie. Planning aid only – the POH/AFM and your weighing report are authoritative.
Piper PA-28R-200 Arrow II key figures
| Maximum takeoff mass (MTOW) | 1,202 kg (2,650 lb) |
|---|---|
| Typical empty mass (POH sample) | 726 kg (1,600 lb) |
| Usable fuel | 48 US gal (182 L) |
| Total fuel capacity | 50 US gal (189 L) |
| Fuel type | AVGAS |
| Useful load with full fuel | 346 kg (762 lb) |
| Maximum baggage | 91 kg (200 lb) |
| Demonstrated crosswind | 17 kt |
| Best rate of climb speed Vy | 87 KIAS |
| Service ceiling | 15,000 ft |
| Built | 1972–1976 |
| Loading stations | front seats, rear seats, baggage compartment, fuel |
Empty mass and useful load depend on your aircraft – its weighing report applies.
Piper PA-28R-200 Arrow II takeoff and landing distance
BriefingPal result from the POH charts at MTOW, no wind, dry paved runway, normal procedure, default flap setting, without safety factor. Use the calculator above for your mass, airfield, temperature and wind.
| Conditions | Takeoff ground roll | Takeoff over 50 ft | Landing over 50 ft | Landing ground roll |
|---|---|---|---|---|
| Sea level, 15 °C | 310 m (1,030 ft) | 555 m (1,830 ft) | 420 m (1,380 ft) | 235 m (770 ft) |
| 5,000 ft, 25 °C (density altitude ≈ 7,300 ft) | 700 m (2,290 ft) | 1,365 m (4,480 ft) | – | – |
Hot and high, the Piper PA-28R-200 Arrow II needs about 146 % more distance to clear 50 ft than at sea level. Calculate density altitude →
Piper PA-28R-200 Arrow II climb and cruise
| Rate of climb at sea level | Time / fuel to 6,500 ft | Cruise TAS at 6,500 ft | Fuel flow |
|---|---|---|---|
| 900 fpm | 9 min / 1.9 US gal | 142 kt | 10.2 US gal/h (39 L/h) |
MTOW, ISA, default power setting of the POH cruise table.
How to do the Piper PA-28R-200 Arrow II weight and balance
- Enter the loadingWeights of pilot, passengers and baggage per station, fuel in litres or US gallons. Each station limit and the MTOW are checked.
- Use your own empty massOptional: enter empty mass and empty CG from the weighing report of your Piper PA-28R-200 Arrow II. Without it the typical POH empty mass is used.
- Check CG and massThe traffic light shows whether the takeoff mass and the CG with and without fuel lie within the envelope of the POH.
- Takeoff and landingElevation, QNH, temperature, wind and runway give the takeoff and landing distance – compared with the runway length if you enter it.
Piper PA-28R-200 Arrow II compared with the other Piper Arrow models
| Model | MTOW | Usable fuel | Takeoff over 50 ft* | Cruise TAS* |
|---|---|---|---|---|
| Piper PA-28R-200 Arrow II | 1,202 kg | 48 US gal | 555 m | 142 kt |
| Piper PA-28RT-201 Arrow IV | 1,247 kg | 72 US gal | 685 m | 142 kt |
| Piper PA-28R-201 Arrow III | 1,247 kg | 72 US gal | 690 m | 118 kt |
| Piper PA-28R-201T Turbo Arrow III | 1,315 kg | 72 US gal | 695 m | 135 kt |
| Piper PA-28R-180 Cherokee Arrow | 1,134 kg | 49 US gal | 710 m | 128 kt |
| Piper PA-28RT-201T Turbo Arrow IV | 1,315 kg | 72 US gal | 705 m | 126 kt |
* MTOW, sea level, 15 °C / 6,500 ft, ISA – BriefingPal result from the POH data.
Piper PA-28R-200 Arrow II – frequently asked questions
What is the MTOW of the Piper PA-28R-200 Arrow II?
The maximum takeoff mass of the Piper PA-28R-200 Arrow II is 1,202 kg (2,650 lb) according to the POH.
How much usable fuel does the Piper PA-28R-200 Arrow II carry?
48 US gal (182 L) usable (total capacity 50 US gal (189 L)). With the typical POH empty mass and full fuel, about 346 kg (762 lb) remain for people and baggage.
How long is the takeoff distance of the Piper PA-28R-200 Arrow II?
At MTOW, sea level, 15 °C and no wind the ground roll is about 310 m (1,030 ft) and the distance over 50 ft about 555 m (1,830 ft). At 5,000 ft and 25 °C it grows to about 1,365 m (4,480 ft). The calculator above gives the value for your conditions.
How do I calculate the CG of the Piper PA-28R-200 Arrow II?
Multiply each mass by its arm, add up the moments and divide by the total mass – the calculator above does this with the stations of the Piper PA-28R-200 Arrow II POH (front seats, rear seats, baggage compartment, fuel) and checks the CG against the envelope.
How does the Piper PA-28R-200 Arrow II differ from other Piper Arrow models?
BriefingPal has 6 Piper Arrow models on file. Compared with them the Piper PA-28R-200 Arrow II has an MTOW of 1,202 kg (2,650 lb) (range 1,134–1,315 kg), 48 US gal (182 L) usable fuel and a takeoff distance over 50 ft of 555 m (1,830 ft) at MTOW.
Is the Piper PA-28R-200 Arrow II weight and balance calculator free?
Yes. The calculator on this page and the BriefingPal app are free and need no account. The app adds route planning, weather, NOTAM, fuel planning and a briefing PDF.
Data source
All figures come from the Pilot's Operating Handbook / Airplane Flight Manual of the Piper PA-28R-200 Arrow II (weight and balance and performance sections) and are computed with the BriefingPal engine – the same calculation as in the app. Planning aid only; the original POH/AFM and the weighing report of your aircraft remain authoritative.
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