Piper PA-28R-201

The Piper PA-28R-201 Arrow III is a four-seat, low-wing, retractable-tricycle-gear piston single powered by the Lycoming IO-360-C1C6 rated at 200 hp.

The source-linked configuration represented here has a maximum takeoff weight of 2,750 lb and 72 U.S. gallons of usable fuel.

The PA-28R-201 Arrow III followed the PA-28R-200 series and is associated with the 1977–2009 period.

Piper documentation separates PA-28R-201 publication groups by production and serial-number range, while FAA Type Certificate Data Sheet 2A13 defines the certified model applicability.

FAA certification data list 77 U.S. gallons total fuel capacity. The source-linked WBcalc configuration represents 72 U.S. gallons of usable fuel.

Piper documentation divides PA-28R-201 aircraft into serial-number-specific publication groups. Operating limits, equipment and weight and balance data must therefore be matched to the individual aircraft.

The normally aspirated PA-28R-201 Arrow III and turbocharged PA-28R-201T Turbo Arrow III share the Arrow III generation designation but use different engine families and have different certificated maximum weights.

PA-28R-201 weight and balance calculations must use the individual aircraft's current basic empty weight and moment or arm together with its applicable approved loading limits.

The source-linked WBcalc configuration represents a 2,750 lb maximum takeoff weight, 72 U.S. gallons usable fuel and the model-specific loading stations and CG envelope.