- Registered owner
- Edwards William J
- Location
- Mccall, ID
- Owner type
- Individual
- Serial number
- EVO-011
- Year built
- 2009
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Experimental, amateur built
- Airworthiness date
- March 3, 2026
- Certificate issued
- December 7, 2009
- Expires
- April 30, 2029
- Mode S code
- AB28AD
- Kit
- Lancair Intl Inc EVOLUTION
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 4
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1997 | 1 |
|---|---|
| 2002 | 1 |
| 2012 | 1 |
| 2014 | 1 |
Information bulletins that may apply · 1
Advisory, not mandatory.
Engine · Pratt & Whitney Canada PT6A-135A
SAIB NE-12-04Turbine/ Turboprop Engine: Reduction GearboxNTSB investigations
No NTSB investigations matched to N818SJMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Edwards William J EVOLUTION aircraft
FAA incident reports
No FAA accident or incident reports matched to N818SJMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Edwards William J EVOLUTION aircraft
Reports on N818SJ not matched to an aircraft · 2
They name N818SJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Incident 19960617025169IDoug DC981 · El Paso, TXNarrative: on June 17, 1996, at approximately 1245 MDT, sunjet flight 610, a DC-9-81, enroute from long beach, CA. To dallas/ft. worth, diverted to El Paso, TX due to an engine oil pressure problem. The crew reported the right engine oil pressure light came…Incident 19940812031749IDoug DC981 · Dallas-Ft Worth, TXLoud bang,NR2 engine lost power. Returned. Contained turbine failure.
Service difficulty reports
No reports matched to N818SJGeneral aviation reporting is voluntary. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Reports on Edwards William J EVOLUTION aircraft
Reports on N818SJ not matched to an aircraft · 11
They name N818SJ, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 97ZZZX2971Apu · failedFLIGHT CREW REPORTED APU INOPERABLE. APU PLACED ON MEL 49-1. UPON INVESTIGATION, MX DISCOVERED APU FAILED. APU REMOVED/DEACTIVATED PER MM 49-10-00 ON 4-30-97. DAMAGE NOTED: GEAR CASE HOUSING CRACKED AROUND ENTIRE MOUNTING FLANGE (AT COMPRESSOR PLENUM)SDR 97ZZZX1120Seat Track · corrodedCORRODED SEAT TRACKS UNDER GALLEYS. FOUND DURING CPCP INSPECTION. SEAT TRACK SECTION REPLACED. SUBMITTER STATED SPECIAL ATTENTION TO SEALING AREA, UNDER GALLEY AND MAINTAINING ENVIRONMENTAL SEAL BETWEEN C-CHECKS.SDR 97ZZZX1119Seat Track · corrodedCORRODED SEAT TRACKS UNDER GALLEYS. FOUND DURING CPCP INSPECTION. SEAT TRACK SECTION REPLACED. SUBMITTER STATED SPECIAL ATTENTION TO SEALING AREA, UNDER GALLEY AND MAINTAINING ENVIRONMENTAL SEAL BETWEEN C-CHECKS.
STCs that may be installed · 8
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · Pratt & Whitney Canada PT6A-135A
STC SE00002ENInstructions for Continued Airworthiness for the PT6A-34, -34AG, -34B, -36, -114, -114A, -116, -135, and -135A engine models that define specific maintenance tasks and their associated maintenance schedules, and that are used as a supplement to the applicable Pratt & Whitney Canada manuals.STC SE00014ENInstallation of the Pratt & Whitney Engine Services, Inc. CrossCheck Engine Monitor Kit P/N HUMS-K-071-1, Rev. A on the specified PT6A engine models and kit P/N HUMS-K-071-2 on the specified A250 engine models.STC SE00020ENInstallation of the Pratt & Whitney Engine Services, Inc. TrendCheck/ TrendCheck Plus Engine Monitor Kit P/N TREND-K-010-1STC SE02357NYInstallation of the Pratt & Whitney Canada, PT6A-135, dual fuel feed line configurationSTC SE615GLIncorporation of a fuel flow transducer.STC SE09286SCInstallation of an alternate gas generator case.STC SE09257SCConvert P&W Engine Models PT6A-15AG, -27, and -28, into PT6A-34 configuration.STC SE659NEInstallation of oil tank filler neck check valve, P/N TSA-76A.