Aircraft › Cessna › 205 / 206 / 207 › 210-5A (205A)
The Cessna 210-5A (205A) is a model in the 205 / 206 / 207 family. It is described here as a Six-seat high-wing piston single. FAA type-certificate reference: 3A21.
Cessna 210-5A (205A) specifications
| Manufacturer | Cessna |
|---|---|
| Model | 210-5A (205A) |
| Production years | 1964 |
| Aircraft type | Six-seat high-wing piston single |
| Seats | 6 |
| Landing gear | Fixed tricycle |
| Certification | FAA 3A21 |
Cessna 210-5A (205A) weights and capacities
| Maximum takeoff weight | 3,300 lb |
|---|---|
| Standard fuel capacity | 65 gal total / 63.4 gal usable |
FAA 3A21 refers to model-specific approved weight-and-balance data for baggage loading.
Cessna 210-5A (205A) engine and configuration
| Engine | Continental · IO-470-S · 260 hp |
|---|
Baggage and loading applicability
| Baggage | FAA 3A21 refers to model-specific approved weight-and-balance data for baggage loading. |
|---|
Cessna 210-5A (205A) history and development
The cataloged production period is 1964.
Cessna 210-5A (205A) is the fixed-gear utility/passenger derivative historically marketed as the Cessna 205. FAA 3A21 identifies it by the certification designation 210-5 / 210-5A. The model uses the Continental IO-470-S rated at 260 hp, a 3,300 lb maximum weight and 65 U.S. gallons total / 63.4 usable fuel. Its six-seat fixed-gear configuration distinguishes it from the retractable 210 models even though it remains on the same type certificate.
Cessna 210-5A (205A) fuel capacity
Standard total fuel: 65 U.S. gallons. Standard usable fuel: 63.4 U.S. gallons.
Cessna 210-5A (205A) model applicability and configuration
Use the certification designation and serial number when matching a Cessna 205 to FAA 3A21. The aircraft may be marketed as 205/205A while the TCDS identifies 210-5/210-5A.
Cessna 210-5A (205A) weight and balance
Maximum takeoff weight: 3,300 lb. FAA 3A21 refers to model-specific approved weight-and-balance data for baggage loading. Maximum weight is 3,300 lb. Use the current aircraft empty weight, CG and approved loading stations for operation. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Cessna 210-5A (205A) calculator.
Cessna 210-5A (205A) frequently asked questions
What engine does the Cessna 210-5A (205A) use?
The engine listed for this model is Continental IO-470-S.
What is the maximum takeoff weight of the Cessna 210-5A (205A)?
The represented maximum takeoff weight is 3,300 lb.
How much usable fuel does the Cessna 210-5A (205A) carry?
The represented standard usable fuel capacity is 63.4 U.S. gallons.
Reference sources
FAA: Type Certificate Data Sheet 3A21, Revision 50 - Cessna 210 series
Related 205 / 206 / 207 models
- Cessna 206 - 1964