Piper PA-32-260 Cherokee Six weight and balance and performance calculator
Calculate the weight and balance of the Piper PA-32-260 Cherokee Six 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-32-260 Cherokee Six is a model of the Piper PA-32; built 1965–1978.
* MTOW, sea level, 15 °C, no wind – BriefingPal result from the POH data
Calculate the Piper PA-32-260 Cherokee Six 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-32-260 Cherokee Six key figures
| Maximum takeoff mass (MTOW) | 1,542 kg (3,400 lb) |
|---|---|
| Typical empty mass (POH sample) | 774 kg (1,706 lb) |
| Usable fuel | 83 US gal (314 L) |
| Total fuel capacity | 84 US gal (318 L) |
| Fuel type | AVGAS |
| Useful load with full fuel | 543 kg (1,196 lb) |
| Maximum baggage | 45 kg (100 lb) |
| Demonstrated crosswind | 15 kt |
| Best rate of climb speed Vy | 91 KIAS |
| Service ceiling | 16,500 ft |
| Built | 1965–1978 |
| Loading stations | front seats, rear seats, baggage compartment, hat shelf / rear baggage, fuel |
Empty mass and useful load depend on your aircraft – its weighing report applies.
Piper PA-32-260 Cherokee Six 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 | 325 m (1,060 ft) | 495 m (1,630 ft) | 305 m (1,000 ft) | 195 m (630 ft) |
| 5,000 ft, 25 °C (density altitude ≈ 7,300 ft) | 740 m (2,430 ft) | 1,175 m (3,850 ft) | – | – |
Hot and high, the Piper PA-32-260 Cherokee Six needs about 136 % more distance to clear 50 ft than at sea level. Calculate density altitude →
Piper PA-32-260 Cherokee Six climb and cruise
| Rate of climb at sea level | Time / fuel to 6,500 ft | Cruise TAS at 6,500 ft | Fuel flow |
|---|---|---|---|
| 860 fpm | 10 min / 3.2 US gal | 121 kt | 10.4 US gal/h (39 L/h) |
MTOW, ISA, default power setting of the POH cruise table (≈55 % power).
How to do the Piper PA-32-260 Cherokee Six 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-32-260 Cherokee Six. 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-32-260 Cherokee Six compared with the other Piper PA-32 models
| Model | MTOW | Usable fuel | Takeoff over 50 ft* | Cruise TAS* |
|---|---|---|---|---|
| Piper PA-32-260 Cherokee Six | 1,542 kg | 83 US gal | 495 m | 121 kt |
| Piper PA-32-301T Turbo Saratoga | 1,633 kg | 102 US gal | 660 m | 144 kt |
* MTOW, sea level, 15 °C / 6,500 ft, ISA – BriefingPal result from the POH data.
Piper PA-32-260 Cherokee Six – frequently asked questions
What is the MTOW of the Piper PA-32-260 Cherokee Six?
The maximum takeoff mass of the Piper PA-32-260 Cherokee Six is 1,542 kg (3,400 lb) according to the POH.
How much usable fuel does the Piper PA-32-260 Cherokee Six carry?
83 US gal (314 L) usable (total capacity 84 US gal (318 L)). With the typical POH empty mass and full fuel, about 543 kg (1,196 lb) remain for people and baggage.
How long is the takeoff distance of the Piper PA-32-260 Cherokee Six?
At MTOW, sea level, 15 °C and no wind the ground roll is about 325 m (1,060 ft) and the distance over 50 ft about 495 m (1,630 ft). At 5,000 ft and 25 °C it grows to about 1,175 m (3,850 ft). The calculator above gives the value for your conditions.
How do I calculate the CG of the Piper PA-32-260 Cherokee Six?
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-32-260 Cherokee Six POH (front seats, rear seats, baggage compartment, hat shelf / rear baggage, fuel) and checks the CG against the envelope.
How does the Piper PA-32-260 Cherokee Six differ from other Piper PA-32 models?
BriefingPal has 2 Piper PA-32 models on file. Compared with them the Piper PA-32-260 Cherokee Six has the lowest MTOW (1,542 kg (3,400 lb)), 83 US gal (314 L) usable fuel and a takeoff distance over 50 ft of 495 m (1,630 ft) at MTOW.
Is the Piper PA-32-260 Cherokee Six 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-32-260 Cherokee Six (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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