Aircraft › Piper › PA-28R / PA-28RT Arrow › PA-28R-201T
The Piper PA-28R-201T Turbo Arrow III is a four-seat, retractable-tricycle-gear PA-28 variant powered by a turbocharged Continental TSIO-360 engine rated at 200 hp.
FAA certification data distinguish this turbocharged model from the normally aspirated PA-28R-201 Arrow III and assign it a 2,900 lb maximum takeoff weight.
Piper PA-28R-201T specifications
| Manufacturer | Piper |
|---|---|
| Model | PA-28R-201T |
| Aircraft type | Four-seat turbocharged retractable-gear piston single |
| Seats | 4 |
| Engine | Continental TSIO-360-F / TSIO-360-FB |
| Power | 200 hp at 2575 rpm |
| Landing gear | Retractable tricycle |
| Certification | FAA 2A13 |
Piper PA-28R-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-28R-201T history and development
FAA Type Certificate Data Sheet 2A13 identifies the PA-28R-201T as the Turbo Arrow III and records its original model approval on November 2, 1976.
Piper publication catalogs identify separate Turbo Arrow III documentation groups, including early aircraft and later production serial-number ranges.
Piper PA-28R-201T certification and applicability
| FAA type certificate | 2A13 |
|---|---|
| FAA model approval | November 2, 1976 |
| Model name | Turbo Arrow III |
Piper PA-28R-201T fuel capacity
FAA TCDS 2A13 lists 77 U.S. gallons total fuel capacity for the PA-28R-201T.
A universal usable-fuel quantity is not asserted on this page. Use the applicable POH or AFM for the aircraft's usable fuel, unusable fuel and loading data.
Piper PA-28R-201T model applicability and configuration
The PA-28R-201T spans more than one documentation and serial-number group. The exact engine installation, propeller, equipment and operating limits must be confirmed against the aircraft's approved documentation.
Turbo Arrow III vs normally aspirated Arrow III
| Specification | Turbo Arrow III | Arrow III |
|---|---|---|
| Model | PA-28R-201T | PA-28R-201 |
| Engine | Continental TSIO-360-F / 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 III replaces the normally aspirated Lycoming installation of the PA-28R-201 with a turbocharged Continental TSIO-360 installation while retaining a 200 hp rating.
Piper PA-28R-201T weight and balance
PA-28R-201T weight and balance calculations must use the current basic empty weight and moment or arm and the approved loading data for the specific aircraft.
FAA certification data list a 2,900 lb maximum takeoff weight and 2,912 lb maximum ramp weight for the configuration represented in the technical reference data.
Piper PA-28R-201T frequently asked questions
What engine does the PA-28R-201T Turbo Arrow III use?
FAA certification data list the Continental TSIO-360-F or TSIO-360-FB, rated at 200 hp at 2,575 rpm.
What is the maximum takeoff weight of the Turbo Arrow III?
FAA certification data list a maximum takeoff weight of 2,900 lb for the PA-28R-201T.
How much fuel does the PA-28R-201T hold?
FAA TCDS 2A13 lists 77 U.S. gallons total fuel capacity. Usable fuel should be confirmed from the POH or AFM applicable to the individual aircraft.
Is the PA-28R-201T the same as the PA-28R-201?
No. The PA-28R-201T is the turbocharged Turbo Arrow III with a Continental TSIO-360 installation, while the PA-28R-201 uses a normally aspirated Lycoming IO-360.
Reference sources
FAA: Type Certificate Data Sheet 2A13, Model PA-28R-201T
Related PA-28R / PA-28RT Arrow models
- Piper PA-28R-201 - 1977–2009
- Piper PA-28RT-201T