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Payload vs. Range
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Range
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En route
Fuel burned
Direct cost
Fuel cost
Tanks run dry about past before at this burn.
Mission Profile
- High-Performance
- Complex
- High-Altitude
- Pressurization
- Multi-Engine
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
- Cessna 340 – the smaller pressurised cabin twin one rung below the 421C. Compare
- Cessna 414 Chancellor – the mid-size pressurised 400-series twin between the 340 and the 421. Compare
- Cessna 402 – the unpressurised utility and commuter sibling on the same 400-series lineage. Compare
- Cessna 425 Conquest I – the PT6A turboprop developed from the 421 airframe, the next step up in capability and cost. Compare
Technical Specifications
Dimensions & Weights
- 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.
Similar to the Cessna 421C Golden Eagle
Similar PistonsCessna 340
Cessna 402
Cessna 404 Titan
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Rockwell Commander 685
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