Aircraft › Piper › PA-22 Tri-Pacer / Colt / Caribbean › PA-22-135
The Piper PA-22-135 is a model in the PA-22 Tri-Pacer / Colt / Caribbean family. It is described here as a High-wing piston single.
Piper PA-22-135 specifications
| Manufacturer | Piper |
|---|---|
| Model | PA-22-135 |
| Aircraft type | High-wing piston single |
| Landing gear | Model-specific tricycle, seaplane or approved configuration |
| Certification | FAA 1A6 |
Piper PA-22-135 weights and capacities
| Maximum takeoff weight | 1,950 lb |
|---|---|
| Standard fuel capacity | 36 gal total |
Piper PA-22-135 engine and configuration
| Engine | Lycoming · O-290-D2 · 135 hp · @ 2,600 rpm |
|---|
Baggage and loading applicability
| baseline approved baggage limit | 50 lb maximum · baseline approved baggage limit |
|---|---|
| when the applicable placard/AFM approval is installed | 100 lb maximum · when the applicable placard/AFM approval is installed |
Piper PA-22-135 history and development
Piper PA-22-135 belongs to the Piper PA-22 Tri-Pacer / Colt / Caribbean family certificated under FAA Type Certificate Data Sheet 1A6. The family spans several horsepower ratings and landplane/seaplane configurations. Exact engine, maximum-weight and fuel values are intentionally not inferred from another PA-22 suffix.
Piper PA-22-135 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-22-135 model applicability and configuration
Verify the exact model designation, serial number, engine, landing-gear/float configuration and fuel installation against the applicable FAA certificate and approved aircraft documentation.
Piper PA-22-135 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-22-135 calculator.
Reference sources
FAA: FAA Type Certificate Data Sheet 1A6