Range Map

Origin: · two fingers to move map

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1

Tank-dry, where fuel runs out at catalogue's stored cruise burn.

Excludes reserves: range beyond the dashed circle requires a leaner cruise than what we store. Great-circle, still air, book cruise. Estimates only: always verify against the POH.

Payload vs. Range

Occupants:

Fuel on board

Cargo

nm

Range

Cargo is additional payload after occupants and baggage.
full tanks
Available Range / nm
Mission capable. This load flies with full fuel.
Fuel reduced by . left aboard for nm range.
Over max payload by . At this load it cannot lift a single occupant.

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Mission Profile

Used market Only available used
241
KTAS
Cruise Speed
1,197
nm
Max Range
30,200
ft
Service Ceiling
10
Occupants
922
lbs
Wet Payload
Endorsements & ratings:
  • High-Performance
  • Complex
  • High-Altitude
  • Pressurization
  • Multi-Engine
Cessna 421C Golden Eagle (N100L) at Daytona Beach International Airport, January 2025. Photo: ZLEA, CC BY-SA 4.0.
Cessna 421C Golden Eagle (N100L) at Daytona Beach International Airport, January 2025. Photo: ZLEA, CC BY-SA 4.0.

Estimated Ownership Costs

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About the Cessna 421C Golden Eagle

Type certificated 1975

Overview

The Cessna 421C Golden Eagle is a pressurised, cabin-class piston twin, the largest and most powerful of Cessna’s pressurised 400-series at 375 horsepower per side. For many owners it is the top of Cessna’s piston-twin line, the last rung before its own turboprop development. Two geared, turbocharged Continental GTSIO-520-L engines drive the propellers through reduction gearing, holding propeller speed low for reduced noise and vibration in a quiet, flat-floor cabin that seats six to eight in club comfort and is certificated for up to ten. It cruises near 240 knots, reaches a 30,200-foot service ceiling, and carries a useful load around 2,200 pounds over distances beyond 1,000 nm. The C-model, built from 1976 to 1985 on FAA type certificate A7CE, traded the earlier 421B’s wingtip tanks for a bonded wet wing and added trailing-link landing gear; the type is finite and out of production today.

Within Cessna’s twin line the 421C sits a clear step above the smaller Cessna 340 and the mid-size Cessna 414 Chancellor, and just below its own turboprop development, the Cessna 425 Conquest I, with which it shares much of the airframe. Most buyers weigh it against entry-level turboprops and the unpressurised twins beneath it: the 421C gives up turbine simplicity and dispatch reliability, but answers with a comparable cabin and ceiling on piston, avgas economics. It makes the most sense for an owner who needs genuine pressurised, all-weather transport for six to eight people and has the budget and the maintenance discipline to keep a geared, turbocharged twin healthy.

Key Features for GA Buyers

  • A quiet, cabin-class interior. The reduction-geared engines let the propellers turn slowly while the engines themselves spin fast, holding noise and vibration down in a flat-floor cabin seating six to eight.
  • Real load over real distance. At 7,450 lb gross the 421C carries a useful load around 2,200 lb and will move a meaningful cabin load more than 1,000 nm.
  • Pressurised and high-flying. A pressurised cabin and a 30,200-foot service ceiling let it cruise in the flight levels, over much of the weather that keeps unpressurised twins lower; airframe de-ice is available for the rest.
  • Trailing-link landing gear. The C-model’s trailing-link mains absorb an imperfect touchdown gracefully, a detail owner-pilots routinely single out.

Trade-offs

  • Demanding geared engines. The Continental GTSIO-520 is complex and costly to overhaul, and it asks for deliberate handling, no abrupt throttle reductions, to protect its reduction gearbox.
  • High fuel burn and a short TBO. Combined fuel flow runs near 47 gph, and the GTSIO-520’s 1,600-hour TBO arrives often; direct operating cost lands close to an entry turboprop without the turbine’s longevity.
  • Light-jet maintenance exposure. Pressurisation, hydraulic gear, turbochargers, and de-ice push annual budgets well beyond a normally-aspirated light twin, and real-world 421C annuals often run $15,000 to $20,000 once those systems are kept current.
  • A finite, out-of-production fleet. Production ended in 1985, so parts and 400-series expertise draw on a fixed, slowly shrinking pool, and a thorough pre-buy and a known type shop matter more than usual.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 44 ft
Height
12 ft
Length
37 ft
Parking area (ft²2)
2,278 ft²
Max Takeoff Weight
7,450 lbs
Max Landing Weight
7,200 lbs
Useful Load
2,200 lbs
Fuel Capacity
213 gal

Performance

Cruise Speed
241 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 240 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 201 KIAS
Approach Speed
98 KIAS
Stall, Clean (VS1)
86 KIAS
Range
1197 NM
Service Ceiling
30,200 ft
Rate of Climb
350 - 1940 fpm
Takeoff over 50 ft obstacle
2,323 ft
Landing over 50 ft obstacle
2,293 ft

Engines

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Sources

Where the figures on this page come from. Cessna 421C Golden Eagle specifications are traced to published references; estimated values are flagged inline next to the figure.

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