Aircraft › Aviat › Pitts Special Series › S-2A
The S-2A is a model in the Pitts Special Series family. It is described here as a Aviat Pitts Special Series aircraft; exact model-specific configuration requires source verification.
Aviat S-2A specifications
| Manufacturer | Aviat |
|---|---|
| Model | S-2A |
| Aircraft type | Aviat Pitts Special Series aircraft; exact model-specific configuration requires source verification |
| Certification | FAA A8SO |
Aviat S-2A weights and capacities
Aviat S-2A engine and configuration
| earlier approved configuration | Lycoming · IO-360-A1A · 200 hp · @ 2,700 rpm · earlier approved configuration |
|---|---|
| S/N 1001, 2001 and up | Lycoming · AEIO-360-A1A · 200 hp · @ 2,700 rpm · S/N 1001, 2001 and up |
| S/N 2206 and up | Lycoming · AEIO-360-A1E · 200 hp · @ 2,700 rpm · S/N 2206 and up |
Certified weight limits and applicability
| normal category | Takeoff 1,575 lb · normal category |
|---|---|
| acrobatic category | Takeoff 1,500 lb · acrobatic category |
Fuel capacity and configuration
| Fuel | 24 gal total · 23 gal usable |
|---|
Baggage and loading applicability
| Baggage | 20 lb maximum |
|---|
Aviat S-2A history and development
S-2A is a member of the Aviat Pitts Special Series family. This page identifies the model, family relationship and available certification context. Model-specific technical values that have not yet been verified from an approved or manufacturer source remain explicitly marked as unverified technical values rather than being inferred from related aircraft.
Aviat S-2A fuel capacity
exact model-specific fuel capacity and usable fuel, where applicable, have not yet been verified from the applicable approved source.
Aviat S-2A model applicability and configuration
Verify the exact model designation, serial number, installed propulsion, equipment and approved operating configuration against the applicable certification or manufacturer record and the individual aircraft documentation.
Aviat S-2A weight and balance
Use the exact model and serial-number loading data together with the individual aircraft's approved weight-and-balance documentation. No payload or baggage limit is inferred from a related model. The exact model-specific maximum takeoff weight and loading limits remains unverified until verified from the applicable approved source. Operational calculations must use the individual aircraft's current empty weight or mass, CG, station data 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 S-2A calculator.
Reference sources
FAA: FAA Type Certificate Data Sheet A8SO, Revision 21