Aircraft › Cessna › 411 › 411A
The Cessna 411A is a model in the 411 family. It is described here as a Six-to-eight-seat pressurized twin-engine piston aircraft. FAA type-certificate reference: A7CE.
Cessna 411A specifications
| Manufacturer | Cessna |
|---|---|
| Model | 411A |
| Aircraft type | Six-to-eight-seat pressurized twin-engine piston aircraft |
| Seats | 8 |
| Landing gear | Retractable tricycle |
| Certification | FAA A7CE |
Cessna 411A weights and capacities
| Maximum takeoff weight | 6,500 lb |
|---|---|
| Maximum landing weight | 6,500 lb |
| Standard fuel capacity | 175 gal total / 170 gal usable |
350 lb nose baggage station plus separate cabin/aft limits
Cessna 411A engine and configuration
| Engine | Continental · GTSIO-520-C · 340 hp each · @ 2,400 rpm |
|---|
Baggage and loading applicability
| Baggage | 350 lb nose baggage station plus separate cabin/aft limits |
|---|
Cessna 411A history and development
Cessna 411A is certificated under FAA A7CE with two Continental GTSIO-520-C engines, each rated at 340 hp at 2,400 propeller rpm. Takeoff and landing maximum weight is 6,500 lb. The standard fuel system totals 175 U.S. gallons with 170 usable. The 411 and 411A share the same basic engine, weight and fuel figures but differ in serial-number range and baggage-station details, so they remain separate model references.
Cessna 411A fuel capacity
Standard total fuel: 175 U.S. gallons. Standard usable fuel: 170 U.S. gallons. A7CE defines two 51-gallon tip tanks with 50 usable each plus two 36.5-gallon wing tanks with 35 usable each.
Cessna 411A model applicability and configuration
This page reflects the certificated base model under A7CE. Seating layouts, propellers, optional equipment and baggage arrangements vary. Match the serial number and installed configuration to the current equipment list and approved flight manual.
Cessna 411A weight and balance
Maximum takeoff weight: 6,500 lb. Maximum landing weight: 6,500 lb. 350 lb nose baggage station plus separate cabin/aft limits Maximum takeoff and landing weight is 6,500 lb. The airplane uses several baggage stations rather than one combined baggage compartment; each published station limit and arm must be respected when computing weight and balance. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Cessna 411A calculator.
Cessna 411A frequently asked questions
What engine does the Cessna 411A use?
The engine listed for this model is Continental GTSIO-520-C.
What is the maximum takeoff weight of the Cessna 411A?
The represented maximum takeoff weight is 6,500 lb.
How much usable fuel does the Cessna 411A carry?
The represented standard usable fuel capacity is 170 U.S. gallons.
Reference sources
FAA: Type Certificate Data Sheet A7CE - Cessna 411 / 411A / 414 / 414A / 425