Piper PA-30 Turbo Twin Comanche

Piston • twin engine • Low 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:
  • Complex
  • High-Altitude
  • Multi-Engine
194
KTAS
Cruise Speed
4
Occupants
1100
nm
Max Range
597
lbs
Wet Payload

Estimated Ownership Costs

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About the Piper PA-30 Turbo Twin Comanche

The Piper PA-30 Turbo Twin Comanche is the ultimate efficiency machine in the light twin category. By pairing a sleek, laminar-flow airframe with two fuel-injected 160 hp Lycoming engines, it achieves cruise speeds that rival much larger twins while burning a fraction of the fuel (roughly 15–17 GPH total). The Turbo models, typically featuring manual RayJay wastegates, allow the aircraft to maintain power up to 24,000 ft, making it a serious high-altitude cruiser.

Key Features for GA Buyers

  • Unmatched Efficiency: Frequently cited as the only twin that makes financial sense compared to high-performance singles, offering a second engine for safety with a ‘nickel budget’ fuel burn.
  • Long Endurance: When equipped with the iconic 15-gallon tip tanks (totaling 120 gallons), this aircraft has a range of over 1,100 nm, capable of crossing half a continent in one hop.
  • Ramp Appeal: Its low-slung stance and pointed nose give it a timeless, sporty look that stands out among mid-century GA designs.

Trade-offs

  • Complex Engine Management: Older Turbo models use manual wastegates, requiring the pilot to manage throttle and wastegate knobs simultaneously during climb to avoid over-boosting.
  • Challenging Landings: Due to the laminar-flow wing and short main gear, it is a notorious ‘floater’ that can reward poor speed control with a punishing ‘thud’ on touchdown.
  • Single-Engine Performance: Like many light twins of its era, single-engine climb is anemic (approx. 200-260 FPM). It requires a proficient pilot who respects its $V_{MC}$ and $V_{SSE}$ speeds.

Featured in our buying guides

Technical Specifications

Dimensions

Wingspan
36.0 ft
Length
25.1 ft
Height
8.2 ft
Parking area (ft2)
1384.6 ft2

Weights

Max Takeoff Weight
3,725 lbs
Max Landing Weight
3,725 lbs
Useful Load
1,317 lbs
Fuel Capacity
120 gal

Performance

Cruise Speed
194 KTAS
Never-Exceed (Vne)
230 KIAS
Max Structural Cruise (Vno)
194 KIAS
Approach Speed
75 KIAS
Stall, Clean (Vs1)
69 KIAS
Range
1100 NM
Service Ceiling
30,000 ft
Rate of Climb
260 - 1460 fpm
Takeoff over 50 ft obstacle
1,590 ft
Landing ground roll
1,900 ft

Engines

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