Aero Commander 200
Piston • single engine • Low Wing • Retractable gear
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About the Aero Commander 200
Overview
The Aero Commander 200 is the final production form of the Meyers 200, a hand-built, high-performance four-seat single developed by Al Meyers from the late 1940s. The design reached its definitive configuration as the 200D in 1965, when the IO-470 was replaced by the Continental IO-520-A and the wings received flush riveting — producing an honest 183-knot cruise from a 285 HP normally-aspirated engine. Aero Commander (a division of North American Rockwell) acquired the type certificate in 1966 but ceased production in 1968, unable to manufacture the hand-fitted steel-tube and aluminium composite structure economically. Only 135 were built in total across all variants; fewer than 100 remain flying. The type has one of the most remarkable accident records in GA — Aviation Consumer’s 35-year search found only 20 accidents across the entire fleet.
Key Features for GA Buyers
- Exceptional speed: 183 knots at 75% power from a 285 HP IO-520-A. Faster than contemporary V-tail Bonanzas and roughly 10 knots ahead of the Cessna 210 Centurion of the same era.
- Steel-tube structure: The fuselage and wing carry-through are framed in 4130 chrome-moly steel running from firewall to aft cabin and crosswise through the gear attachment points. This structure is credited with the type’s outstanding accident survivability record.
- Safety record: Arguably the best of any comparable GA single. No recorded gear-up landings, no loss-of-control on rollout, no VFR-into-IMC — across 35 years of fleet history.
- Wraparound cabin windows: Near-360-degree visibility from a raised canopy section; a distinctive and practical design feature.
- Engine accessibility: The IO-520-A installation allows the engine to swing out for maintenance access, similar to the Jacobs installation in the Cessna 195.
- Upgrade path: Earlier 200A/B/C models can be brought to effective D specification via IO-520-A STC. IO-550 upgrades are also available.
Trade-offs
- Effective two-place cross-country machine: Full fuel (80 gal) and full seats is not realistic. Aero Commander completed testing to raise gross weight to 3,350 lbs but never submitted the paperwork to the FAA.
- Fuel system complexity: Four tanks, one gauge. Fuel mismanagement is one of only two recurring accident causes across the entire fleet history. Requires disciplined fuel management on every flight.
- Parts and maintenance: Out of production since 1968. Landing gear components in particular can be difficult to source. The composite steel-tube/aluminium structure requires a mechanic familiar with the type.
- Tiny fleet: Fewer than 100 flying examples worldwide means a thin resale market, limited type-specific maintenance expertise outside of the owner community, and elevated insurance costs relative to more common types.
- Insurance: Low-volume vintage retractable with a bespoke structure — expect elevated premiums and scrutiny of pilot experience.
See Also
- Beechcraft Bonanza V35B — direct contemporary; similar speed, more common, retractable gear, flat engine
- Beechcraft Bonanza A36 — later straight-tail variant; more payload flexibility
- Cessna 210 Centurion — higher-volume alternative; slower but better parts availability
- Interceptor 400 — turboprop derivative of the same airframe; only two built
Technical Specifications
Dimensions
- Wingspan
- 30.0 ft
- Length
- 24.0 ft
- Height
- 7.0 ft
Weights
- Max Takeoff Weight
- 3,000 lbs
- Max Landing Weight
- 3,000 lbs
- Useful Load
- 1,060 lbs
- Fuel Capacity
- 80 gal
Performance
- Cruise Speed
- 183 KTAS
- Range
- 900 NM
- Service Ceiling
- 18,500 ft
- Rate of Climb
- 1400 fpm
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