Aircraft › SOCATA › MS890 / Rallye 235 Series › RALLYE 235 A
The RALLYE 235 A is a model in the MS890 / Rallye 235 Series family. It is described here as a Single-engine low-wing piston aircraft.
SOCATA RALLYE 235 A specifications
| Manufacturer | SOCATA |
|---|---|
| Model | RALLYE 235 A |
| Aircraft type | Single-engine low-wing piston aircraft |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.A.379 |
SOCATA RALLYE 235 A weights and capacities
SOCATA RALLYE 235 A engine and configuration
| Engine | Lycoming · O-540-B4B5 · 235 hp · @ 2,575 rpm |
|---|
Certified weight limits and applicability
| normal category | Takeoff 2,645 lb · Landing 2,513 lb · normal category |
|---|---|
| utility-category maneuvers | Takeoff 2,204 lb · Landing 2,204 lb · utility-category maneuvers |
Fuel capacity and configuration
| Fuel | 73.97 gal total · 71.33 gal usable |
|---|
Baggage and loading applicability
| Baggage | 99 lb maximum |
|---|
SOCATA RALLYE 235 A history and development
RALLYE 235 A is a certificated member of the MS890 / Rallye 235 Series family. This model is listed under EASA TCDS EASA.A.379 - MS890 / Rallye 235 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.
SOCATA RALLYE 235 A 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 SOCATA model or suffix.
SOCATA RALLYE 235 A 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.
SOCATA RALLYE 235 A 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 SOCATA 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 RALLYE 235 A calculator.
Reference sources
EASA: EASA Type Certificate Data Sheet EASA.A.379, Issue 07, 24 April 2026