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
236
KTAS
Cruise Speed
950
nm
Max Range
24,000
ft
Service Ceiling
11
Occupants
2,058
lbs
Wet Payload
Endorsements & ratings:
  • High-Performance
  • Complex
  • Multi-Engine
Piper PA-31T Cheyenne, representative of the PA-31T3 T-1040, which mates a stretched Chieftain fuselage to the Cheyenne's PT6A turboprops, at Tobalaba Airport, Santiago, October 2012. Photo: Aeroprints.com, CC BY-SA 3.0.
Piper PA-31T Cheyenne, representative of the PA-31T3 T-1040, which mates a stretched Chieftain fuselage to the Cheyenne's PT6A turboprops, at Tobalaba Airport, Santiago, October 2012. Photo: Aeroprints.com, CC BY-SA 3.0.

Estimated Ownership Costs

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About the Piper PA-31T3-500 T-1040

Type certificated 1982 Source: FAA Type Certificate Data Sheet

Overview

The Piper PA-31T3-500 T-1040 is a rare commuter turboprop developed in the early 1980s by mating the unpressurised fuselage of the Chieftain with the wings, tail, and PT6A-11 engines of the Cheyenne I. Piper certified the type in 1982 and built only 24 airframes through 1984, targeting the third-level commuter airline market that needed turbine reliability without the cost or complexity of a pressurised cabin.

The design rationale was specific: short-haul feeder routes typically run under 200 miles, where pressurisation adds weight and cost without operational benefit. The result is an 11-passenger turboprop with a useful load above 3,800 lbs, capable of operating from 3,000 ft strips and burning Jet A. Most units served regional carriers like Bar Harbor Airlines and Sunbird Airlines before the deregulation era reshaped commuter aviation. That commuter history still names the airplane’s buyer: a regional feeder, cargo, or jump operator who wants PT6A turbine reliability and an eleven-seat, 3,800-pound load over short feeder legs, and who has no use for a pressurised cabin to fly them.

Key Features for GA Buyers

  • Payload Utility: Without pressurisation equipment, the T-1040 carries an exceptional useful load (3,800 lbs+), making it well suited to cargo, jump operations, or high-density passenger configurations.
  • Turbine Reliability: Pratt & Whitney Canada PT6A-11 engines deliver 500 shp per side with 3,600 hr standard TBO, significantly more reliable and longer-running than the piston Chieftain’s Lycoming TIO-540s.
  • Cabin Volume: The stretched Chieftain fuselage seats up to 11 in commuter configuration, or holds substantial cargo with seats removed and an optional belly pod fitted.
  • Short-Field Capability: Wing loading and engine power yield landing distances under 2,200 ft, opening regional fields that jet operators cannot serve.

Trade-offs

  • Unpressurised: Service ceiling is 24,000 ft but most operations run between 10,000 and 14,000 ft, leaving the aircraft below most weather rather than above it.
  • Rarity: With only 24 built, type-specific parts and experienced maintenance are increasingly difficult to source. Many components are shared with the Cheyenne I and Chieftain, but unique hybrid items have no aftermarket.
  • Fuel Burn: Cruise burn near 66 GPH erodes the economic case for low-utilization private operators.
  • Limited Resale Market: The combination of small fleet size, commuter-spec interiors, and aging avionics keeps the secondary market narrow.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 41 ft
Height
13 ft
Length
37 ft
Parking area (ft²2)
2,129 ft²
Max Takeoff Weight
9,000 lbs
Max Landing Weight
9,000 lbs
Useful Load
3,800 lbs
Fuel Capacity
260 gal

Performance

Cruise Speed
236 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 230 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 230 KIAS
Approach Speed
90 KIAS
Stall, Clean (VS1)
86 KIAS
Range
950 NM
Service Ceiling
24,000 ft
Rate of Climb
1600 fpm
Takeoff over 50 ft obstacle
2,650 ft
Landing over 50 ft obstacle
2,150 ft

Engines

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Sources

Where the figures on this page come from. Piper PA-31T3-500 T-1040 specifications are traced to published references; estimated values are flagged inline next to the figure.

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