Aircraft › Piper › PA-32R / PA-32RT Lance / Saratoga SP › PA-32R-300
The Piper PA-32R-300 is a model in the PA-32R / PA-32RT Lance / Saratoga SP family. It is described here as a Six-seat low-wing retractable-gear piston single.
Piper PA-32R-300 specifications
| Manufacturer | Piper |
|---|---|
| Model | PA-32R-300 |
| Aircraft type | Six-seat low-wing retractable-gear piston single |
| Landing gear | Retractable tricycle |
| Certification | FAA A3SO |
Piper PA-32R-300 weights and capacities
| Maximum takeoff weight | 3,600 lb |
|---|
Piper PA-32R-300 engine and configuration
| Configuration 1 | Lycoming · IO-540-K1A5D · 300 hp · @ 2,700 rpm |
|---|---|
| S/N 32R-7680141 through 32R-7880068 | Lycoming · IO-540-K1G5D · 300 hp · @ 2,700 rpm · S/N 32R-7680141 through 32R-7880068 |
Fuel capacity and configuration
| Fuel | 98 gal total · 94 gal usable |
|---|
Baggage and loading applicability
| Baggage | 200 lb maximum |
|---|
Piper PA-32R-300 history and development
Piper PA-32R-300 is a certificated member of the Piper PA-32R Lance / Saratoga SP family. Certification for this model is listed under Type Certificate Data Sheet A3SO - Piper PA-32R / PA-32RT series. This family spans model-specific changes in engine installation, maximum weight, fuel capacity, landing-gear or seaplane configuration, and approved equipment. This page retains the certification identity and encyclopedia context without transferring unresolved numerical values from another Piper suffix.
Piper PA-32R-300 fuel capacity
exact model-specific fuel capacity / usable fuel has not yet been verified from the applicable FAA type-certificate section, approved flight manual, or manufacturer data. Do not infer it from a neighboring Piper model or suffix.
Piper PA-32R-300 model applicability and configuration
Verify exact model designation, serial number, installed engine or engines, fuel system, landing-gear or seaplane configuration, and approved equipment against the applicable FAA record and aircraft documentation.
Piper PA-32R-300 weight and balance
Use the exact model/serial-number loading data and the individual aircraft's approved weight-and-balance record. No baggage limit is inferred from a related Piper model. The exact model-specific maximum takeoff weight / gross weight remains unverified until the applicable approval section is verified. Operational loading must use the aircraft-specific empty weight, CG, station arms and limitations. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Piper PA-32R-300 calculator.
Reference sources
FAA: FAA Type Certificate Data Sheet A3SO