Discover the remarkable Cessna 401, a light twin-engine aircraft that revolutionized corporate aviation in the late 1960s. This comprehensive guide explores its specifications, performance capabilities, and historical significance in the world of general aviation.
Overview of the Cessna 401
The Cessna 401 emerged as a groundbreaking light twin-engine aircraft during its production run from 1966 to 1972. This versatile aircraft established itself as a preferred choice for corporate transport and utility operations, accommodating six to eight passengers comfortably.
The aircraft’s distinctive features included:
- Four oval windows for enhanced visibility
- Compact nose design for aerodynamic efficiency
- Wingtip fuel tanks for extended range
- Pressurized cabin for passenger comfort
- Retractable landing gear for improved performance
Introduction to the Cessna 401
The Cessna 401 filled a crucial niche in the general aviation market, offering an impressive blend of performance and comfort. Its pressurized cabin and short-field capability made it exceptionally versatile, while its design reflected Cessna’s commitment to expanding its twin-engine aircraft lineup.
Design and Features of the Cessna 401
The aircraft’s design excellence manifested through several key features:
- Three-bladed, reversible constant-speed propellers
- Spacious pressurized cabin with flexible seating configurations
- Large windows for superior visibility
- Strategic wingtip fuel tank placement
- Advanced aerodynamic design for optimal performance
Specifications and Performance of the Cessna 401
Technical Specifications
| Specification | Measurement |
|---|---|
| Engine Power (each) | 300 horsepower (Continental TSIO-520-E) |
| Maximum Takeoff Weight | 6,300 pounds (2,858 kg) |
| Empty Weight | 3,674 pounds (1,667 kg) |
| Wingspan | 39 feet 9 inches (12.12 m) |
| Length | 33 feet 8 inches (10.26 m) |
| Height | 11 feet 7 inches (3.53 m) |
Performance Metrics
| Performance Aspect | Capability |
|---|---|
| Maximum Speed | 227 knots (420 km/h) |
| Cruise Speed | 209 knots (387 km/h) |
| Range | 1,102 nautical miles (2,041 km) |
| Service Ceiling | 26,180 feet (7,980 m) |
| Rate of Climb | 1,610 feet per minute (8.18 m/s) |
Variants of the Cessna 401
The Cessna 401’s evolution through its production span showcased Cessna’s commitment to continuous improvement. Each variant introduced refinements to enhance performance and capabilities.
Cessna 401A and 401B
- Cessna 401A (1969) – Featured initial improvements to performance and comfort
- Cessna 401B (1970-1972) – Represented the pinnacle of the 401 series with advanced features
- Both variants maintained the popular six to eight-seat configuration
- Continued the legacy of performance and utility that defined the original model
- Eventually succeeded by the more advanced Cessna 402B
History and Development of the Cessna 401
The Cessna 401 emerged as a pivotal aircraft in the light twin-engine market during the mid-1960s. Developed as part of Cessna’s strategic expansion into corporate and utility aviation, this aircraft was engineered to meet increasing demands for efficient, comfortable transportation suitable for both short-haul and cross-country flights.
Production commenced in 1966, introducing a new chapter in Cessna’s light twin-engine portfolio. The aircraft’s meticulous design offered an optimal balance of performance, comfort, and utility, making it particularly attractive to business travelers and charter operators with its six to eight-passenger capacity.
Development Background
Building upon the success of its predecessor, the Cessna 411, the 401 represented a more refined and efficient design. The development team focused on creating a smaller, lighter aircraft that would be more accessible to a broader range of pilots and operators while maintaining high performance standards.
- Pressurized cabin for enhanced comfort
- Retractable landing gear for improved aerodynamics
- Wingtip fuel tanks for extended range
- Innovative design features for superior performance
- Enhanced accessibility for pilots and operators
Operational History
During its production run from 1966 to 1972, the Cessna 401 significantly influenced general aviation’s landscape. The aircraft achieved remarkable success among corporate flight departments, charter operators, and private owners, offering impressive capabilities with its 227-knot maximum speed and 1,102-mile range.
The 401’s impact extended beyond performance metrics, establishing new standards for comfort and efficiency in the light twin-engine category. Its success laid the groundwork for future models, particularly the 402 Businessliner, and its enduring presence in today’s used aircraft market testifies to its exceptional design and capabilities.
Cost and Ownership of the Cessna 401
The Cessna 401, particularly the 401B model, represents a significant investment in the light twin-engine aircraft market, with current market values averaging approximately $138,772. This initial price varies based on factors such as condition, flight hours, avionics upgrades, and maintenance history.
Total Cost of Ownership
Annual ownership costs for the Cessna 401A model average $34,323.12, encompassing various essential expenses for safe and efficient operation.
| Fixed Cost Component | Annual Amount |
|---|---|
| Annual Inspection | $3,020.00 |
| Hangar/Tie-down Fees | $840.00 |
| Weather Service Subscriptions | $604.89 |
| Insurance | $3,132.78 |
| Refurbishment/Modernization | $645.08 |
| Depreciation | $3,347.11 |
Additional variable costs include fuel consumption, regular maintenance, and potential engine overhauls for the twin Continental TSIO-520-E engines. Prospective owners should also consider pilot training expenses and possible avionics upgrades to meet current airspace requirements.