Cessna 303 Crusader
Piston • twin engine • Low Wing • Retractable gear
Range Visualization
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Payload vs. Range
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Default: 190 lbs (FAA standard)
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Mission Profile
- High-Performance
- Complex
- Multi-Engine
About the Cessna 303 Crusader
Overview
The Cessna 303 Crusader is a light cabin-class piston twin produced from 1981 to 1986. It was Cessna’s last new piston twin design, conceived as a modern replacement for the ageing 310 and 320 Skyknight in the mid-six-seat owner-flown segment. Power comes from two Continental TSIO-520-AE engines of 250 hp each, mounted in nacelles outboard of the relatively narrow fuselage.
The Crusader arrived at the worst possible moment in the cabin-twin market. By 1981, fuel prices, rising insurance costs, and the cratering of the corporate piston-twin market were already pushing buyers either down to single-engine high-performance pistons or up to entry-level turboprops. Cessna built approximately 315 Crusaders before discontinuing the line, leaving it one of the rarer and more obscure cabin twins in the GA fleet today.
For the modern buyer who finds one in good condition and at a fair price, the Crusader is a credible aeroplane: docile handling, a roomy cabin for its class, modest operating costs by twin standards, and the simple maintenance discipline that comes with an unpressurised airframe. The narrow buyer pool means values are stable but liquidity is poor.
Key Features for GA Buyers
- Modern airframe. The 303 is one of the youngest piston-twin designs in the GA fleet. Wing structure, fuel system, and avionics bay all reflect early 1980s engineering rather than 1960s carryover.
- Manageable operating cost. Two 250 hp turbocharged Continentals burn roughly 24 to 26 GPH at cruise. That is materially less than a Cessna 340 or Baron 58, putting the Crusader in reach for buyers who want twin redundancy on a piston budget.
- Cabin and visibility. The fuselage is wide enough for proper club seating in the back, and the airstair door is a meaningful comfort upgrade over earlier Cessna twins. Forward visibility is strong; the engines are well clear of the pilot’s sight line.
- Docile handling. The 303 has the most benign single-engine handling of any Cessna piston twin, with a published V_mc that gives the pilot meaningful margin. Owners and instructors consistently report it is the easiest of the Cessna twins to land.
- Unpressurised simplicity. No pressurisation means no recurring leak inspections, no door-seal replacement cycles, and no associated systems training burden.
Trade-offs
- Rarity and parts. With only ~315 built and production ended in 1986, finding a 303 specialist for systems work can require travel. Aircraft-specific parts may need to be sourced through the Cessna Pilots Association or via salvage.
- Single-source engines. The TSIO-520-AE is a relatively low-volume Continental variant. Major-overhaul cost is comparable to other 520 series, but parts lead times can stretch when shop demand is high.
- Performance compromise. 196 KTAS cruise and a 1,020 nm range are fine for the design’s mission but are unimpressive next to the contemporary 340 (229 KTAS, 1,400 nm) at not much higher acquisition cost.
- Resale liquidity. The buyer pool is narrow. Selling a 303 typically takes longer than selling an equivalent 340 or Baron, and the price spread between asking and selling can be wide.
See Also
- Cessna 320 Skyknight – the predecessor concept the 303 was meant to replace; the 320 sits one generation back in Cessna’s piston-twin lineage. Compare
- Cessna 335 – the unpressurised 340 sibling from the same era; a step-up in cabin size and performance for not much more money. Compare
- Cessna 340 – the pressurised cabin twin; the segment-defining Cessna twin of the era. Compare
- Beech Baron 55 – the closest direct competitor; lighter, faster, with a vastly larger buyer pool and parts network. Compare
- Beech 76 Duchess – the Duchess is a step-down lighter twin; relevant for buyers using the cabin-twin segment as a step up from a trainer multi. Compare
Technical Specifications
Dimensions
- Wingspan
- 39.0 ft
- Length
- 30.4 ft
- Height
- 13.3 ft
- Parking area (ft2)
- 1734.6 ft2
Weights
- Max Takeoff Weight
- 5,150 lbs
- Max Landing Weight
- 3,605 lbs
- Useful Load
- 1,845 lbs
- Fuel Capacity
- 153 gal
Performance
- Cruise Speed
- 196 KTAS
- Never-Exceed (Vne)
- 216 KIAS
- Max Structural Cruise (Vno)
- 175 KIAS
- Approach Speed
- 90 KIAS
- Stall, Clean (Vs1)
- 69 KIAS
- Range
- 1020 NM
- Service Ceiling
- 25,000 ft
- Rate of Climb
- 1480 fpm
- Takeoff over 50 ft obstacle
- 2,200 ft
- Landing ground roll
- 2,350 ft
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