Models / Bartels Joseph / LANCAIR EVOLUTION / N427LE Aircraft record N427LE 2009 Bartels Joseph LANCAIR EVOLUTION Deregistered Unclaimed Source: FAA, updated Oct 20, 2026 This N-number isn't registered right now. Below is its last known registration, canceled Feb 26, 2018.
Safety record in brief: 1 NTSB accident (destroyed damage, Aug 2015) · 2 ADs may apply
NTSB events 1 destroyed, 2015 ADs may apply 2 confirm with A&P Service reports 0 since 1995
Registration FAA Aircraft Registry · Oct 20, 2026
Last registered owner Unmanned Systems INC
Owner type Corporation
City, state Redmond, OR
Certificate issued Apr 14, 2015
Canceled Feb 26, 2018
Airworthiness Experimental · Research and Development, Crew Training, Market Survey
Airworthiness date Dec 22, 2014 We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine FAA Registry + type data Airframe
Manufacturer Bartels Joseph
Model LANCAIR EVOLUTION
Year 2009
Serial number EVO-002
Aircraft type Fixed wing single engine
Category Land
Certification Not Type Certificated
Seats 4
Engines 1
Max takeoff weight Up to 12,499 lb
Kit Lancair Intl Inc Evolution
Mode S code A5169F Engine
Make and model P&W Canada Pt6a-135a
Type Turbo-prop
Power 750 hp Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history Ownership history from FAA records 2015 – 2018 Unmanned Systems INC Redmond, OR Individual owners are shown by city and state only.
Safety record NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026 NTSB events (1)
Accident · destroyed Aug 14, 2015 · Pacific Ocean, PO The pilot's incapacitation for reasons that could not be determined because the airplane was not recovered from the ocean.
Damage Destroyed
Injuries Fatal
Report WPR15LA242 From NTSB records; matched by N-number. Read NTSB report (search CAROL for WPR15LA242)
ADs published since 1998 that may apply (2) These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
AD Subject Effective Applies to 2012-09-10 Pratt & Whitney Canada Turboprop Engines May 23, 2012 Engine (PT6A-135A)Only with: Engines with power section maintenance involving first stage sun gear or planet gear replacement since December 22, 2008, and with TAATI PMA first stage sun gears P/N E3028456 or E3037304, or planet gear sets P/N E3101455-02 or E3101525-02 installed. 2002-23-13 Pratt & Whitney Canada PT6A Series Turboprop Engines Dec 31, 2002 Engine (PT6A-135A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed.
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (0) No Service Difficulty Reports found for this airframe since 1995.
Sources FAA Aircraft Registry Registration, owner city and state, airframe, engine updated Oct 20, 2026 NTSB accident and incident database Accidents and incidents since 1982 updated Oct 15, 2026 FAA Airworthiness Directives (Federal Register) ADs published since 1998 updated Oct 20, 2026 FAA Service Difficulty Reports Reports since 1995 updated Oct 16, 2026 Request owner name removal Report an error in this record