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Payload vs. 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
Estimated Ownership Costs
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About the Aero Commander 200
Type certificated 1964 Source: FAA Type Certificate Data Sheet
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 1964, when the IO-470 was replaced by the Continental IO-520-A and the wings received flush riveting, giving 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. Sources cite total production between 122 and 135 across all variants, and fewer than 100 remain flying. The type also carries one of the most remarkable accident records in general aviation: Aviation Consumer’s 35-year review 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, genuinely fast for a normally-aspirated four-seat retractable of the 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. An unusually clean fleet accident record: no recorded gear-up landings, no loss-of-control on rollout, and 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 gallons total, 74 usable) 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 V35B Bonanza – direct V-tail Bonanza contemporary; similar cruise, more common, retractable single. Compare
- Beech Bonanza A36 – later straight-tail Bonanza variant with more payload flexibility. Compare
- Cessna 210 Centurion – higher-volume retractable single contemporary; slower but better parts availability. Compare
- Piper PA-24 Comanche – direct contemporary four-place retractable single with broader market presence. Compare
- Bellanca Viking – vintage retractable single contemporary with wood-and-fabric construction. Compare
Technical Specifications
Dimensions & Weights
- Height
- 7 ft
- Length
- 24 ft
- Parking area (ft²2)
- 1,160 ft²
- Max Takeoff Weight
- Source: FAA Type Certificate Data Sheet 3,000 lbs
- Max Landing Weight
- 3,000 lbs
- Useful Load
- 1,060 lbs
- Fuel Capacity
- Source: FAA Type Certificate Data Sheet 80 gal
Performance
- Cruise Speed
- Source: third-party reference 183 KTAS
- Never-Exceed (VNE)
- Source: FAA Type Certificate Data Sheet 205 KIAS
- Max Structural Cruise (VNO)
- Source: FAA Type Certificate Data Sheet 182 KIAS
- Approach Speed
- 75 KIAS
- Stall, Clean (VS1)
- Source: third-party reference 67 KIAS
- Range
- 900 NM
- Service Ceiling
- 18,500 ft
- Rate of Climb
- 1400 fpm
- Takeoff over 50 ft obstacle
- 1,200 ft
- Landing over 50 ft obstacle
- 1,150 ft
Engine
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Sources
Where the figures on this page come from. Aero Commander 200 specifications are traced to published references; estimated values are flagged inline next to the figure.
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