Range 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
182
KTAS
Cruise Speed
1,412
nm
Max Range
22,500
ft
Service Ceiling
7
Occupants
962
lbs
Wet Payload
Endorsements & ratings:
  • High-Performance
  • Complex
  • Multi-Engine
Aero Commander 560 (N2775B) at Kingman, March 2022. Photo: Duncan Kirk, CC BY 4.0.
Aero Commander 560 (N2775B) at Kingman, March 2022. Photo: Duncan Kirk, CC BY 4.0.

Estimated Ownership Costs

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About the Aero Commander 560

Type certificated 1957 Source: FAA Type Certificate Data Sheet

Overview

The Aero Commander 560E is a 1957 cabin-class twin piston, the mature geared-engine member of Ted Smith’s original Aero Design and Engineering Commander twin family. It seats up to seven (one pilot plus six passengers), rides on retractable tricycle landing gear, and shares the family’s signature high-wing layout with the spar passing above the cabin. Two Lycoming GO-480-C/G geared engines of 295 hp each drive three-blade Hartzell constant-speed feathering propellers, and the 223 US gal fuel system gives the type genuine cross-country range for a 1950s light twin.

The 560 line evolved quickly. The base 560 entered production in 1954 with 250 hp Lycoming GO-435 engines, a 44 ft wing, and a 6,000 lb MTOW. The 560A followed in 1955 with revised systems and a longer fuselage. The 560E, certified in 1957 and the canonical airframe for this record, added 30-inch wing tip extensions, a reinforced landing gear, an outboard fuel system, and the 295 hp GO-480-C/G installation, which together lifted MTOW to 6,500 lb. The later 560F continued the formula at the same horsepower before North American Rockwell’s acquisition pushed the family toward the simpler, ungeared 500-line variants and ultimately the Shrike Commander. About 93 Model 560Es were built; the line is certificated under FAA Type Certificate 6A1 and remains supported today by Twin Commander Aircraft LLC, the current TC holder.

What distinguishes the 560E in market terms is the combination of stand-up cabin, generous fuel, and the period distinction of serving as an Eisenhower-era presidential transport in the form of the VC-3. In airframe character it is over-engineered to military standards, slow by modern light-twin reckoning, and quietly capable on long legs.

Key Features for GA Buyers

  • Cabin-class twin layout. Stand-up cabin volume, club-style seating for seven, and a flat unobstructed floor courtesy of the over-cabin wing carry-through, uncommon at this weight class.
  • Long legs on the standard fuel system. 223 US gal of fuel and the geared 295 hp GO-480s yield roughly 1,400 nm of range with reserve at economy cruise, real cross-country capability for the era.
  • High service ceiling. 22,500 ft published gives meaningful over-the-weather margin for an unpressurised 1950s twin, with oxygen the practical limit on prolonged altitude work.
  • Robust airframe and gear. Built to military standards under Ted Smith’s design philosophy; main gear rated to roughly twice aircraft weight, and the type has a reputation for durability that has carried it well into a seventh decade of service.
  • Active TC holder support. Twin Commander Aircraft LLC continues to maintain parts, manuals, an AOG line, and an authorized service center network under TC 6A1, an unusually live support footprint for a 1950s airframe.

Trade-offs

  • Geared GO-480 economics. The geared Lycomings are more complex and more expensive to overhaul than the carbureted O-540 and IO-540 engines on the later 500-line variants; budget accordingly for top and major intervals.
  • Slower than its peers. 182 KTAS at 70% power and 10,000 ft sits roughly 20 kt below a Baron, Cessna 310, or Aerostar of comparable era; the 560E trades cruise speed for cabin and load.
  • Recurring spar inspection. A three-year wing inspection driven by mid-1990s spar cap corrosion ADs runs in the 9,000 to 11,000 USD range, and lower spar cap replacement, when needed, can exceed the value of older airframes.
  • Unreliable fuel gauging. The single-sump system is forgiving in concept but the original gauges have been implicated in fuel-related accidents; budget for an electronic fuel totalizer at acquisition.
  • Variant confusion in market data. Listings, broker spec sheets, and even some published aircraft references freely conflate 560, 560A, 560E, and 560F figures; verify the specific airframe’s serial number, engine fitment, and weight schedule against TCDS 6A1 before trusting any quoted performance number.
  • Unpressurised. The cabin is not pressurised; useful cruise altitudes with passengers in comfort fall well below the 22,500 ft ceiling, and any sustained altitude work requires supplemental oxygen.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 50 ft
Height
14 ft
Length
35 ft
Parking area (ft²2)
2,388 ft²
Max Takeoff Weight
6,500 lbs
Useful Load
2,300 lbs
Fuel Capacity
223 gal

Performance

Cruise Speed
Source: manufacturer figure 182 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 234 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 182 KIAS
Approach Speed
83 KIAS
Stall, Clean (VS1)
66 KIAS
Range
1412 NM
Service Ceiling
22,500 ft
Rate of Climb
1450 fpm
Takeoff over 50 ft obstacle
1,452 ft
Landing over 50 ft obstacle
1,500 ft

Engines

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Sources

Where the figures on this page come from. Aero Commander 560 specifications are traced to published references; estimated values are flagged inline next to the figure.

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