Beech 18 (Turbo)

Turboprop • twin engine • Low Wing • Retractable gear

Range Visualization

Origin: · click map to move · nm at current load

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
  • Multi-Engine
  • Instrument
222
KTAS
Cruise Speed
8
Occupants
1000
nm
Max Range
524
lbs
Wet Payload

Estimated Ownership Costs

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About the Beech 18 (Turbo)

Overview

The Beech 18-Turbo is a turboprop conversion of the Beech 18 airframe, most commonly associated with Volpar Aircraft’s Super Turbo 18 program. Volpar replaced the original Pratt & Whitney R-985 radials with two 705 hp Garrett AiResearch TPE-331-1-101B turboprops, flat-rated to 605 hp, and added the Volpar MkIV tricycle landing gear conversion. The result preserved the Twin Beech’s heavy-hauling cabin while modernising powerplant, ground handling, and dispatch reliability.

Key Features for GA Buyers

  • Turbine reliability on a vintage cabin. Garrett TPE-331 turboprops eliminate the magneto, carb-ice, and cylinder-temperature complexity of the R-985 radials, while the cabin retains the Twin Beech’s 6-8 seat utility configuration.
  • Tricycle gear handling. The Volpar MkIV nosewheel conversion removes the demanding ground-handling profile of the original taildragger, opening the type to a wider pilot population.
  • Operational pedigree. Air America operated 14 Volpar conversions during the Vietnam War; civilian freight operators kept Volpar Turbo 18s in revenue service through the 1980s, demonstrating durability under hard utility use.

Trade-offs

  • Conversion-population type. Volpar built a finite number of conversions; airframe availability is limited and parts support depends on a small specialist community.
  • Fuel burn vs payload. Turboprop performance comes at higher fuel-flow than modern equivalents; the 318-gallon fuel system is needed to deliver the published 1,000 nm range, leaving useful load constrained at full fuel.
  • Period airframe. The underlying structure remains a 1937-design Beech 18: spar inspections, corrosion management, and parts that depend on a vintage supply chain are part of the ownership profile, even with the modern powerplant.

See Also

Technical Specifications

Dimensions

Wingspan
46.0 ft
Length
37.5 ft
Height
9.7 ft
Parking area (ft2)
2380.0 ft2

Weights

Max Takeoff Weight
10,286 lbs
Max Landing Weight
9,772 lbs
Useful Load
2,655 lbs
Fuel Capacity
318 gal

Performance

Cruise Speed
222 KTAS
Never-Exceed (Vne)
243 KIAS
Max Structural Cruise (Vno)
196 KIAS
Approach Speed
100 KIAS
Stall, Clean (Vs1)
77 KIAS
Range
1000 NM
Service Ceiling
26,000 ft
Rate of Climb
1400 - 1710 fpm

Engines

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