Range Map

Origin:

• nm at current load

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Payload vs. Range

Configure weights
Occupants
lb + lbs / pax

gal

Fuel on board

lbs

Extra weight

nm

Range

Available Range / nm
Mission capable. Aircraft can handle the current load with full fuel tanks.
Fuel capacity reduced by gallons ( 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

Used market Only available used
204
KTAS
Cruise Speed
1,099
nm
Max Range
30,800
ft
Service Ceiling
8
Occupants
1118
lbs
Wet Payload
Endorsements & ratings:
  • High-Performance
  • Complex
  • High-Altitude
  • Multi-Engine

Estimated Ownership Costs

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About the Cessna 414A Chancellor

Type certificated 1978

Overview

The Cessna 414A Chancellor is a pressurised, cabin-class piston twin built from 1978 to 1985, the refined evolution of the original 414 that first flew in 1968. Cessna positioned it as the step up for owners moving out of unpressurised twins like the 310 or the 402: a flat-floor pressurised cabin, club seating, and cabin-class comfort in a piston airframe running on avgas rather than Jet-A.

The 414A introduced a longer-span bonded wet wing (retiring the earlier model’s wing-locker tanks), a stretched nose for baggage and avionics, and 310 hp Continental TSIO-520-N engines. For the GA buyer it occupies a specific niche: the most attainable entry into pressurised cabin-class flying, below the larger 421 Golden Eagle and the turboprop Conquest, but a clear step above the unpressurised 402 on the same airframe lineage.

Key Features for GA Buyers

  • Pressurised cabin. Pressurisation holds the cabin near 10,000 ft into the low flight levels, the feature that defines the type and separates it from the 402.
  • Cabin-class comfort. Flat-floor cabin with club seating for six, a side airstair door, and an optional belted lavatory, with cross-country range around 1,100 nm with reserves on 213 gallons usable.
  • Avgas economics. Two turbocharged TSIO-520 engines burn about 34 GPH combined at 75 percent cruise for roughly 205 KTAS in the high teens, without the acquisition premium of a turbine.
  • Honest twin performance. A 1,580 fpm climb and a 30,800 ft service ceiling, with a single-engine ceiling near 19,800 ft that is genuinely useful for the mission.

Trade-offs

  • Wing spar AD. The Cessna 400-series twins are subject to a recurring wing-spar inspection airworthiness directive. Compliance history is the first item to verify on any pre-purchase; an aircraft without a documented spar-inspection program is a financial unknown.
  • Turbocharged maintenance. The TSIO-520 turbo system, intercoolers, and pressurisation plumbing demand disciplined upkeep. Cylinders, turbochargers, and exhaust components are recurring cost centres, and hourly maintenance reserves run high for a piston aircraft.
  • TBO and overhaul. TBO is 1,400 hours on early -N engines and 1,600 on the improved -NB, with overhauls around $33,000 per engine. Two engines plus pressurisation make this a genuinely expensive piston twin to own.
  • Annual cost reality. A realistic annual inspection on a well-kept 414A runs near $9,000, and total annual ownership at low utilisation sits in the $55,000 to $65,000 range. Deferred-maintenance examples cost considerably more to bring current.

See Also

  • Cessna 340 – the smaller pressurised cabin-class twin, the natural step below the 414. Compare
  • Cessna 402 – the unpressurised 400-series sibling on the same airframe lineage, favoured for commuter and utility roles. Compare
  • Cessna Conquest II – the turboprop step-up for owners outgrowing piston-twin economics. Compare

Technical Specifications

Dimensions & Weights

Wingspan 44.2 ft
Height
11.5 ft
Length
36.4 ft
Parking area (ft2)
2243.88 ft2
Max Takeoff Weight
6,750 lbs
Max Landing Weight
6,750 lbs
Useful Load
2,396 lbs
Fuel Capacity
213 gal

Performance

Cruise Speed
204 KTAS
Never-Exceed (VNE)
Source: third-party reference 237 KIAS
Max Structural Cruise (VNO)
Source: third-party reference 203 KIAS
Approach Speed
95 KIAS
Stall, Clean (VS1)
82 KIAS
Range
1099 NM
Service Ceiling
30,800 ft
Rate of Climb
1580 fpm

Engines

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Sources

Where the figures on this page come from. Cessna 414A Chancellor specifications are traced to published references; estimated values are flagged inline next to the figure.

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External Media

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