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
183
KTAS
Cruise Speed
900
nm
Max Range
18,500
ft
Service Ceiling
4
Occupants
580
lbs
Wet Payload
Endorsements & ratings:
  • High-Performance
  • Complex
Aero Commander 200D (N898LF) at EAA AirVenture 2016 — Photo: TimothyMN, CC BY-SA 4.0
Aero Commander 200D (N898LF) at EAA AirVenture 2016 — Photo: TimothyMN, CC BY-SA 4.0

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

Technical Specifications

Dimensions & Weights

Wingspan 30 ft
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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