Aircraft › Piper › PA-32 Cherokee Six / Saratoga › PA-32-300
The Piper PA-32-300 is a model in the PA-32 Cherokee Six / Saratoga family. It is described here as a Low-wing piston single.
Piper PA-32-300 specifications
| Manufacturer | Piper |
|---|---|
| Model | PA-32-300 |
| Aircraft type | Low-wing piston single |
| Landing gear | Fixed tricycle |
| Certification | FAA A3SO |
Piper PA-32-300 weights and capacities
| Maximum takeoff weight | 3,400 lb |
|---|
Piper PA-32-300 engine and configuration
| Configuration 1 | Lycoming · IO-540-K1A5 · 300 hp · @ 2,700 rpm |
|---|---|
| approved serial-number configuration | Lycoming · IO-540-K1G5 · 300 hp · @ 2,700 rpm · approved serial-number configuration |
Fuel capacity and configuration
| S/N 32-15, 32-21, 32-40000 through 32-40974, and 32-7140001 through 32-7840202 | 84 gal total · S/N 32-15, 32-21, 32-40000 through 32-40974, and 32-7140001 through 32-7840202 |
|---|---|
| S/N 32-7940001 through 32-7940290 | 98 gal total · 94 gal usable · S/N 32-7940001 through 32-7940290 |
Baggage and loading applicability
| Baggage | 200 lb maximum |
|---|
Piper PA-32-300 history and development
Piper PA-32-300 is a certificated member of the PA-32 Cherokee Six / Saratoga family. This model is listed under FAA TCDS A3SO - PA-32 Cherokee Six / Saratoga series. The family contains model-specific differences in propulsion, maximum weight, fuel system, landing gear, cabin or mission equipment. preserves the model and certification identity while model-specific values that have not been verified remain unverified values.
Piper PA-32-300 fuel capacity
exact model-specific fuel capacity / usable fuel has not yet been verified from the applicable certification record, approved flight manual, or manufacturer data. Do not infer it from a neighboring Piper model or suffix.
Piper PA-32-300 model applicability and configuration
Verify exact model designation, serial number, installed engine or engines, fuel system, landing gear and approved equipment against the applicable certification record and individual aircraft documentation.
Piper PA-32-300 weight and balance
Use exact model/serial-number loading data and the individual aircraft's approved weight-and-balance record. No baggage or payload 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-32-300 calculator.
Reference sources
FAA: FAA Type Certificate Data Sheet A3SO