Aircraft › Piper › PA-28R / PA-28RT Arrow › PA-28RT-201T
The Piper PA-28RT-201T Turbo Arrow IV is a four-seat, retractable-tricycle-gear PA-28 variant powered by the turbocharged Continental TSIO-360-FB rated at 200 hp.
FAA certification data list a 2,900 lb maximum takeoff weight and 2,912 lb maximum ramp weight for the model.
Piper PA-28RT-201T specifications
| Manufacturer | Piper |
|---|---|
| Model | PA-28RT-201T |
| Aircraft type | Four-seat turbocharged retractable-gear piston single |
| Seats | 4 |
| Engine | Continental TSIO-360-FB |
| Power | 200 hp at 2575 rpm |
| Propeller | Hartzell constant-speed, 2- or 3-blade approved installations |
| Landing gear | Retractable tricycle |
| Certification | FAA 2A13 |
Piper PA-28RT-201T weights and capacities
| Maximum ramp weight | 2,912 lb |
|---|---|
| Maximum takeoff weight | 2,900 lb |
| Standard fuel capacity | 77 gal total |
| Maximum baggage | 200 lb combined |
Piper PA-28RT-201T history and development
The PA-28RT-201T is identified by Piper as the Turbo Arrow IV and is covered separately from the normally aspirated PA-28RT-201 Arrow IV in Piper operating-document listings.
FAA Type Certificate Data Sheet 2A13 defines the certified Turbo Arrow IV configuration and its serial-number applicability.
Piper PA-28RT-201T certification and applicability
| FAA type certificate | 2A13 |
|---|---|
| Model name | Turbo Arrow IV |
Piper PA-28RT-201T fuel capacity
FAA TCDS 2A13 lists 77 U.S. gallons total fuel capacity for the PA-28RT-201T.
A universal usable-fuel quantity is not asserted here. Use the applicable POH or AFM for the individual aircraft's usable and unusable fuel quantities.
Piper PA-28RT-201T model applicability and configuration
The exact Turbo Arrow IV configuration must be established from the aircraft serial number, approved operating documentation, equipment list, supplements and current weight and balance records.
Turbo Arrow IV vs normally aspirated Arrow IV
| Specification | Turbo Arrow IV | Arrow IV |
|---|---|---|
| Model | PA-28RT-201T | PA-28RT-201 |
| Engine | Continental TSIO-360-FB | Lycoming IO-360-C1C6 |
| Induction | Turbocharged | Normally aspirated |
| Power | 200 hp | 200 hp |
| Maximum takeoff weight | 2,900 lb | 2,750 lb |
The Turbo Arrow IV uses a turbocharged Continental engine in place of the normally aspirated Lycoming installation used by the PA-28RT-201 Arrow IV and carries a higher certificated maximum takeoff weight.
Piper PA-28RT-201T weight and balance
PA-28RT-201T weight and balance calculations must use the individual aircraft's current basic empty weight and moment or arm together with the approved limits applicable to that aircraft.
FAA certification data list a 2,900 lb maximum takeoff weight and 2,912 lb maximum ramp weight. Fuel loading must use the usable-fuel quantity established by the applicable POH or AFM.
Piper PA-28RT-201T frequently asked questions
What engine does the PA-28RT-201T Turbo Arrow IV use?
The PA-28RT-201T uses the Continental TSIO-360-FB rated at 200 hp at 2,575 rpm.
What is the maximum takeoff weight of the Turbo Arrow IV?
FAA certification data list a maximum takeoff weight of 2,900 lb and a maximum ramp weight of 2,912 lb.
How much fuel does the PA-28RT-201T hold?
FAA TCDS 2A13 lists 77 U.S. gallons total fuel capacity. The applicable usable-fuel quantity should be obtained from the aircraft POH or AFM.
Is the Turbo Arrow IV the same as the PA-28RT-201 Arrow IV?
No. The Turbo Arrow IV uses the turbocharged Continental TSIO-360-FB, while the normally aspirated PA-28RT-201 Arrow IV uses the Lycoming IO-360-C1C6.
Reference sources
FAA: Type Certificate Data Sheet 2A13, Model PA-28RT-201T
Related PA-28R / PA-28RT Arrow models
- Piper PA-28R-201T
- Piper PA-28RT-201 - 1979–1982