Aircraft › Piper › PA-28R / PA-28RT Arrow › PA-28RT-201
The Piper PA-28RT-201 Arrow IV is a four-seat, retractable-tricycle-gear member of the PA-28 Arrow family 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.
Piper PA-28RT-201 Weight and Balance Calculator →
Piper PA-28RT-201 specifications
| Manufacturer | Piper |
|---|---|
| Model | PA-28RT-201 |
| Production years | 1979–1982 |
| Aircraft type | Four-seat retractable-gear piston single |
| Seats | 4 |
| Engine | Lycoming IO-360-C1C6 |
| Power | 200 hp at 2700 rpm |
| Propeller | McCauley or Hartzell constant-speed |
| Landing gear | Retractable tricycle |
| Certification | FAA 2A13 |
Piper PA-28RT-201 weights and capacities
| Maximum takeoff weight | 2,750 lb |
|---|---|
| Maximum landing weight | 2,750 lb |
| Standard fuel capacity | 77 gal total / 72 gal usable |
| Maximum baggage | 200 lb combined |
Piper PA-28RT-201 history and development
The PA-28RT-201 Arrow IV followed the Arrow III generation and is associated with the 1979–1982 period.
Piper maintains separate Arrow IV operating-document groups, while FAA Type Certificate Data Sheet 2A13 defines the model's certified configuration and serial-number applicability.
Piper PA-28RT-201 certification and applicability
| FAA type certificate | 2A13 |
|---|---|
| Catalog production period | 1979–1982 |
| Model name | Arrow IV |
Piper PA-28RT-201 fuel capacity
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 PA-28RT-201 model applicability and configuration
Operating limitations and weight and balance data must match the individual PA-28RT-201 aircraft, its serial number, equipment, supplements and approved modifications.
Piper Arrow IV vs Turbo Arrow IV
| Specification | Arrow IV | Turbo Arrow IV |
|---|---|---|
| Model | PA-28RT-201 | PA-28RT-201T |
| Engine | Lycoming IO-360-C1C6 | Continental TSIO-360-FB |
| Induction | Normally aspirated | Turbocharged |
| Power | 200 hp | 200 hp |
| Maximum takeoff weight | 2,750 lb | 2,900 lb |
The normally aspirated Arrow IV and Turbo Arrow IV use different engine families. Both are rated at 200 hp in the configurations represented here, while the turbocharged model has a higher certificated maximum takeoff weight.
Piper PA-28RT-201 weight and balance
PA-28RT-201 weight and balance calculations must use the individual aircraft's current basic empty weight and moment or arm together with the approved model-specific loading limits.
The source-linked WBcalc configuration represents a 2,750 lb maximum takeoff weight and 72 U.S. gallons of usable fuel.
Open Piper PA-28RT-201 Weight and Balance Calculator →
Piper PA-28RT-201 frequently asked questions
What engine does the Piper PA-28RT-201 Arrow IV use?
The PA-28RT-201 uses the Lycoming IO-360-C1C6 rated at 200 hp at 2,700 rpm.
What is the maximum takeoff weight of the PA-28RT-201 Arrow IV?
The source-linked configuration represented here has a maximum takeoff weight of 2,750 lb.
How much usable fuel does the Arrow IV hold?
The source-linked configuration represented here uses 72 U.S. gallons of usable fuel from 77 gallons total capacity.
What is the difference between the Arrow IV and Turbo Arrow IV?
The PA-28RT-201 uses a normally aspirated Lycoming IO-360-C1C6, while the PA-28RT-201T uses a turbocharged Continental TSIO-360-FB. Both are rated at 200 hp in the configurations represented here.
Reference sources
FAA: Type Certificate Data Sheet 2A13, Model PA-28RT-201
WBcalc source-linked calculator dataset: piper/pa-28rt-201-arrow-iv
Related PA-28R / PA-28RT Arrow models
- Piper PA-28R-201 - 1977–2009
- Piper PA-28RT-201T