Aircraft › Aviat › A-1 Husky Series › A-1C-200
The A-1C-200 is a model in the A-1 Husky Series family. It is described here as a Aviat A-1 Husky Series aircraft; exact model-specific configuration requires source verification.
Aviat A-1C-200 specifications
| Manufacturer | Aviat |
|---|---|
| Model | A-1C-200 |
| Aircraft type | Aviat A-1 Husky Series aircraft; exact model-specific configuration requires source verification |
| Certification | FAA A22NM |
Aviat A-1C-200 weights and capacities
Aviat A-1C-200 engine and configuration
| Engine | Lycoming · IO-360-A1D6 · 200 hp · @ 2,700 rpm |
|---|
Certified weight limits and applicability
| baseline A-1C-200 | Takeoff 2,200 lb · baseline A-1C-200 |
|---|---|
| S/N 3000+ when increased-gross-weight requirements of A22NM Note 25 are incorporated | Takeoff 2,250 lb · S/N 3000+ when increased-gross-weight requirements of A22NM Note 25 are incorporated |
Fuel capacity and configuration
| Fuel | 52 gal total · 50 gal usable |
|---|
Baggage and loading applicability
| Baggage | 50 lb maximum |
|---|
Aviat A-1C-200 history and development
A-1C-200 is a member of the Aviat A-1 Husky 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 A-1C-200 fuel capacity
exact model-specific fuel capacity and usable fuel, where applicable, have not yet been verified from the applicable approved source.
Aviat A-1C-200 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 A-1C-200 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 A-1C-200 calculator.
Reference sources
FAA: FAA Type Certificate Data Sheet A22NM, Revision 31