Cessna 401

Piston twin engine • Low Wing • Retractable gear

Range Visualization

Origin:

nm at current load

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Payload vs. Range

Configure weights

Default: 190 lbs

Default: 30 lbs

Occupants
lbs lbs / pax

Fuel on board

Extra weight

Range

Available Range / nm
Mission capable. Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required. You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight. Reduce payload by lbs to safely operate this aircraft.
Extra weight is the additional payload available with your selected passengers.

Mission Profile

Endorsements & ratings:
  • • High-Performance
  • • Complex
  • • High-Altitude
  • • Multi-Engine
179
KTAS
Cruise Speed
8
Occupants
nm
Max Range
-
lbs
Wet Payload
• Used market

Estimated Ownership Costs

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About the Cessna 401

Overview

The Cessna 401 is the executive-configured member of Cessna’s 400-series light cabin twin, built from 1966 to 1972 on FAA type certificate A7CE. It shares its airframe, systems, and turbocharged Continental TSIO-520-E engines with the Cessna 402; the two differ mainly in cabin fit-out, the 401 sold as a six-to-eight-seat corporate transport and the 402 as a utility and commuter hauler. Unpressurised and avgas-fuelled, it offered cabin-class room and twin-engine capability below the price of the pressurised 340 and 414. Cessna folded the 401 into the continuing 402 line after 1972, so the type is a finite, out-of-production fleet today.

Key Features for GA Buyers

  • Cabin-class room without the pressurisation bill. A flat-floor six-to-eight-seat cabin and an airstair door give the 401 a corporate-transport feel at a lower acquisition and maintenance cost than the pressurised cabin twins on the same airframe lineage.
  • Turbocharged altitude capability. Two turbocharged Continental TSIO-520-E engines hold power into the teens, useful for terrain and weather, with oxygen aboard.
  • Shared 402 support base. Because the 401 and 402 share the airframe and engines, parts, shop knowledge, and type expertise draw on the much larger 402 fleet.

Trade-offs

  • Wing-spar AD. Like the rest of the Cessna 400-series twins, the 401 is subject to the recurring wing-spar inspection airworthiness directive; documented compliance history is the first pre-purchase item.
  • Unpressurised at altitude. The cabin is not pressurised, so the altitudes where the turbocharged engines are most efficient require supplemental oxygen for everyone aboard.
  • Turbocharged maintenance, finite fleet. Two turbocharged engines, their exhaust and turbo systems, and a short five-year production run mean disciplined upkeep and a thinner parts sub-market than the long-lived 402.

See Also

  • Cessna 402 – the utility and commuter sibling on the identical A7CE airframe; the volume model of the pair. Compare
  • Cessna 340 – the pressurised cabin-class step up for owners who want a sea-level cabin in the flight levels. Compare
  • Cessna 310 – the lighter six-seat Cessna twin one rung below the 400-series. Compare

Technical Specifications

Dimensions & Weights

Wingspan 44.2 ft
Height
11.4 ft
Length
36.4 ft
Parking area (ft2)
2243.88 ft2
Max Takeoff Weight
6,850 lbs
Max Landing Weight
6,850 lbs
Fuel Capacity
206 gal

Performance

Cruise Speed
179 KTAS
Never-Exceed (Vne)
Source: FAA Type Certificate Data Sheet 231 KIAS
Max Structural Cruise (Vno)
Source: FAA Type Certificate Data Sheet 200 KIAS
Approach Speed
83 KIAS
Stall, Clean (Vs1)
64 KIAS
Service Ceiling
26,900 ft

Engines

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Sources

Where the figures on this page come from. Cessna 401 specifications are traced to published references; estimated values are flagged inline next to the figure.

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See how the Cessna 401 stacks up against similar aircraft

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