Aircraft › Cessna › 414 Chancellor › 414A
The Cessna 414A Chancellor is a model in the 414 Chancellor family. It is described here as a Six-to-eight-seat pressurized twin-engine piston aircraft. FAA type-certificate reference: A7CE.
Cessna 414A specifications
| Manufacturer | Cessna |
|---|---|
| Model | 414A |
| Aircraft type | Six-to-eight-seat pressurized twin-engine piston aircraft |
| Seats | 8 |
| Landing gear | Retractable tricycle |
| Certification | FAA A7CE |
Cessna 414A weights and capacities
| Maximum ramp weight | 6,785 lb |
|---|---|
| Maximum takeoff weight | 6,750 lb |
| Maximum landing weight | 6,750 lb |
| Standard fuel capacity | 213.4 gal total |
A7CE lists nose, cabin and aft baggage compartments with individual limits; the total is not a single interchangeable station.
Cessna 414A engine and configuration
| Engine | Continental · 310 hp each · @ 2,700 rpm |
|---|
Baggage and loading applicability
| Baggage | A7CE lists nose, cabin and aft baggage compartments with individual limits; the total is not a single interchangeable station. |
|---|
Cessna 414A history and development
The 414A Chancellor is a substantially revised branch of the 414 family. FAA A7CE lists Continental TSIO-520-N or TSIO-520-NB engines for early aircraft and TSIO-520-NB for later serial numbers, rated at 310 hp each. Maximum ramp weight is 6,785 lb, maximum takeoff and landing weight is 6,750 lb, and maximum zero-fuel weight is 6,515 lb. Total fuel capacity is 213.4 gallons, with usable quantity varying by serial-number group.
Cessna 414A fuel capacity
Standard total fuel: 213.4 U.S. gallons. A7CE lists 102 or 103 usable gallons per wing depending on serial number, giving 204 or 206 gallons usable total.
Cessna 414A model applicability and configuration
This page is specific to the 414A and preserves the A7CE serial-number distinction in usable fuel. Do not substitute 414 fuel or weight data. Check serial number, POH/AFM revision, installed equipment and current weight-and-balance records.
Cessna 414A weight and balance
Maximum ramp weight: 6,785 lb. Maximum takeoff weight: 6,750 lb. Maximum landing weight: 6,750 lb. Maximum zero fuel weight: 6,515 lb. A7CE lists nose, cabin and aft baggage compartments with individual limits; the total is not a single interchangeable station. Maximum ramp weight is 6,785 lb, takeoff and landing weight 6,750 lb, and zero-fuel weight 6,515 lb. Multiple baggage compartments must be evaluated separately. Usable fuel is serial-number dependent within the 213.4-gallon system. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Cessna 414A Chancellor calculator.
Cessna 414A frequently asked questions
What is the maximum takeoff weight of the Cessna 414A Chancellor?
The represented maximum takeoff weight is 6,750 lb.
Reference sources
FAA: Type Certificate Data Sheet A7CE - Cessna 411 / 411A / 414 / 414A / 425