Aero Commander 680FP

Piston • twin engine • High Wing • Retractable gear

Range Visualization

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Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

Endorsements & ratings:
  • High-Performance
  • Complex
  • High-Altitude
  • Pressurization
  • Multi-Engine
160
KTAS
Cruise Speed
7
Occupants
1200
nm
Max Range
1562
lbs
Wet Payload

Estimated Ownership Costs

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About the Aero Commander 680FP

Overview

The Aero Commander 680FP, marketed as the Pressurized Commander, is the pressurized non-stretched member of the 680F airframe family, certificated in 1964 under FAA Type Certificate 1A1. It sits in the cabin-class piston-twin segment, sharing the high-wing layout, retractable tricycle gear, and twin Lycoming IGSO-540 geared-and-supercharged powerplants common to the late-piston Aero Commander line. With a 5.0 psi pressurization differential, the 680FP gave 1960s owner-flown and corporate operators a way to cruise above weather in a piston twin without stepping up to the cost or runway demands of an early turbine.

The airframe is the same fuselage cross-section and wing as the 680F, with reinforced structure and pressurization plumbing replacing the unpressurized cabin. Production was modest – the variant overlapped with the stretched, unpressurized 680FL Grand Commander, and Aero Commander effectively asked buyers to choose between volume and altitude comfort. Most surviving 680FPs are now in the hands of operators who specifically want pressurization in this airframe class and have access to a shop comfortable with the IGSO-540.

For a GA buyer evaluating one today, the 680FP is a niche acquisition. The cabin is comfortable, the systems are 1960s-typical (engine-driven pressurization source, mechanical controls), and the mission envelope – mid-200s KTAS in the high teens to low 20s – is genuinely useful for regional business travel. The economics are dominated by the powerplants and the pressurization system, both of which reward disciplined ownership and punish deferred maintenance.

Key Features for GA Buyers

  • Pressurized cabin in a piston twin. Roughly 5.0 psi differential allows a 10,000 ft cabin near the mid-20s service ceiling – a comfort tier most piston twins do not reach.
  • Cabin-class layout with airstair door. Seven-place cabin with a center aisle and walk-in entry; meaningfully more space and easier loading than light cabin twins of the same era.
  • High-wing visibility and ramp presence. Unobstructed sightlines for passengers, simple wing-mounted fuel architecture, and an iconic profile that retains owner appeal.
  • Capable useful load. Roughly 2,900 lb useful load on an 8,500 lb MTOW supports realistic four-to-six-occupant trips with bags and IFR fuel reserves.
  • Twin Commander-supported type lineage. The Twin Commander Aircraft organization remains active in supporting the broader Commander line; parts and tribal knowledge for the airframe systems are still reachable through that channel.

Trade-offs

  • IGSO-540 powerplant complexity. Geared, supercharged Lycoming sixes demand specific operating technique and overhaul shops with current experience; both are scarcer and more expensive than parallel-valve TIO-540 equivalents.
  • Pressurization adds a maintenance domain. Door seals, outflow valves, and structural fatigue items are inspection items the unpressurized 680FL does not carry – a real annual-cost delta that should be modeled, not assumed away.
  • Modest production run, thin parts pool. The 680FP was built in small numbers relative to the 680FL Grand Commander and 500-series siblings; some airframe-specific parts require fabrication or salvage sourcing.
  • Modest cruise efficiency for the operating cost. True airspeeds in the mid-200s KTAS at high power settings come at IGSO-540 fuel burns; a Beech King Air 90 in the same mission is faster, simpler to operate, and better supported, at a higher acquisition price.
  • Cabin volume trades against pressurization. The 680FL gives meaningfully more cabin length without pressurization at the same MTOW class – buyers should be honest about whether the mission actually requires pressurized flight or whether the stretched cabin is the better answer.

See Also

Technical Specifications

Dimensions

Wingspan
49.0 ft
Length
36.8 ft
Height
14.5 ft
Parking area (ft2)
2466.2 ft2

Weights

Max Takeoff Weight
8,500 lbs
Useful Load
2,900 lbs
Fuel Capacity
223 gal

Performance

Cruise Speed
160 KTAS
Never-Exceed (Vne)
187 KIAS
Approach Speed
97 KIAS
Stall, Clean (Vs1)
75 KIAS
Range
1200 NM
Service Ceiling
28,000 ft
Rate of Climb
500 - 1000 fpm

Engines

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