- Registered owner
- Stanwyck T Scott
- Location
- Nasotah, WI
- Owner type
- Individual
- Serial number
- EVO-007
- Year built
- 2013
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Experimental, amateur built
- Airworthiness date
- June 23, 2013
- Certificate issued
- September 25, 2012
- Expires
- September 30, 2028
- Mode S code
- A98011
- Kit
- Lancair International Inc LANCAIR EVOLUTION
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 3
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1986 | 1 |
|---|---|
| 1997 | 1 |
| 2012 | 1 |
Engine · Pratt & Whitney Canada PT6A-42
AD 2012-09-10First stage sun gearsAD 97-04-12Compressor Bleed-off ValveAD 86-10-05First Stage Compressor HubInformation bulletins that may apply · 2
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N711DBMatched 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 T Scott Stanwyck LANCAIR EVOLUTION aircraft
FAA incident reports
No FAA accident or incident reports matched to N711DBMatched 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 T Scott Stanwyck LANCAIR EVOLUTION aircraft
Reports on N711DB not matched to an aircraft · 1
They name N711DB, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports
No reports matched to N711DBGeneral 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 T Scott Stanwyck LANCAIR EVOLUTION aircraft
STCs that may be installed · 10
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-42
STC SE12225ACThis STC will incorporate P&W 1700 rpm propeller reduction gearbox on P&WC engines to allow 1700 rpm propeller installationSTC SE00001ENEngines will be maintained IAW 'Maintenance or Reliable Engines(MORE) Program,' Rev 2, 8/16/95.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 SE2960SOInstallation of an oil filler cap safety adapter.STC SE615GLIncorporation of a fuel flow transducer.STC SE01805NYInstallation of Fuel Nozzle Adapters using studs and nuts.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.STC SE4570SWRevise accessory drive spline, P/N 3008181.