PT6A-67A Turboprop Engine
The PT6A-67A is a turboprop engine manufactured by Pratt & Whitney Canada, designed for general aviation aircraft with power output under 1,100 kW. It features a free turbine design driving a propeller through a reduction gearbox, classifying under HTS 8411.21.40.00 as an aircraft turbine for turboprop applications.
Import Duty Rates by Country of Origin
Alternative Classifications
This product could be classified differently depending on its characteristics or intended use.
If imported as a replacement power section or module
Parts of turbopropellers, not complete engines, fall under specific parts headings in 8411.91.
If used for marine propulsion rather than aircraft
Same power range but non-aircraft application shifts to other gas turbines excluding aircraft types.
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Import Tips & Compliance
• Obtain FAA or EASA certification documentation to verify airworthiness and power specifications under 1,100 kW
• Include detailed technical specs confirming turboprop design to avoid misclassification as turbojets
• Ensure export licenses from origin country due to ITAR restrictions on aircraft engines
Related Products under HTS 8411.21.40.00
TPE331-10 Turboprop Engine
Honeywell's TPE331-10 is a single-shaft turboprop engine delivering up to 1,000 kW for agricultural and utility aircraft. Its design integrates compressor, turbine, and propeller gearbox specifically for aviation, fitting HTS 8411.21.40.00 criteria for low-power aircraft turbines.
Garrett TPE331-1 Turboprop
The legacy Garrett (now Honeywell) TPE331-1 turboprop powers small aircraft like the Fairchild Merlin with under 1,100 kW output. Classified in HTS 8411.21.40.00 due to its aircraft-specific turboprop configuration and power rating.
Walter M601E Turboprop Engine
GE Aviation's Walter M601E is a compact turboprop for light aircraft like the L-410, rated below 1,100 kW. Its free-power turbine architecture qualifies it under HTS 8411.21.40.00 for aircraft turbopropellers.
Turbomeca Arriel 2D Turboshaft
Safran's Arriel 2D, though primarily turboshaft for helicopters, in low-power aircraft configurations falls under HTS 8411.21.40.00 when certified for fixed-wing turboprop use under 1,100 kW.
Rolls-Royce M250-C40B Turboprop
The Rolls-Royce M250-C40B is a lightweight turboprop variant for UAVs and small aircraft, outputting under 1,100 kW. It meets HTS 8411.21.40.00 for low-power aircraft gas turbines.