# N711DB: 2013 T Scott Stanwyck LANCAIR EVOLUTION - Status: Valid registration - Airframe: [T Scott Stanwyck LANCAIR EVOLUTION](https://openairdocs.org/model/t-scott-stanwyck-lancair-evolution) (registry code 0563189, 4 seats) - Engine: [Pratt & Whitney Canada PT6A-42](https://openairdocs.org/engine/pratt-whitney-canada-pt6a-42) (registry code 52062) - Data sheets: [TCDS E4EA](https://openairdocs.org/tcds/E4EA) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: EVO-007 - Year built: 2013 - Type: Fixed wing single engine - Engine type: Turbo-prop - Kit: Lancair International Inc LANCAIR EVOLUTION - Airworthiness: Experimental, amateur built - Airworthiness date: June 23, 2013 - Certificate issued: September 25, 2012 - Expires: September 30, 2028 - Mode S code: A98011 - Registered owner: [Stanwyck T Scott](https://openairdocs.org/faa-owner/STANWYCK%20T%20SCOTT) - Location: [Nasotah, WI](https://openairdocs.org/faa-place/WI/Nasotah) - Owner type: Individual - Owner's area on the map: 43.1126° N, 88.4119° W: Placed by OpenAirDocs at the center of ZIP code 53058, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=711DB - Page: https://openairdocs.org/aircraft/N711DB From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. ## ADs that may apply (OpenAirDocs): 3 in force ### Matched by airframe (T Scott Stanwyck LANCAIR EVOLUTION) None in force. ### Matched by engine (Pratt & Whitney Canada PT6A-42) - [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012 - [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997 - [AD 86-10-05](https://openairdocs.org/ad/86-10-05): First Stage Compressor Hub · Pratt & Whitney Canada PT6A-42. Effective Jun 5, 1986 ## Information bulletins (advisory) (2 in force) - [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015 - [SAIB NE-06-34](https://openairdocs.org/saib/NE-06-34): . Issued Mar 21, 2006 ## NTSB investigations None matched to N711DB. ## FAA accident and incident reports None matched to N711DB. ## 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. - [Incident 19930628023409I](https://openairdocs.org/incident/19930628023409I), Jun 28, 1993: Maule M5180C (N711DB), Plainview, TX, Minor damage. Pilot groundlooped on landing rollout. Aircraft was hit by a sudden and violent crosswind. Right gear collapsed. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## STCs that may be installed (OpenAirDocs) (10) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the engine (Pratt & Whitney Canada PT6A-42) - [STC SE12225AC](https://openairdocs.org/stc/SE12225AC): This STC will incorporate P&W 1700 rpm propeller reduction gearbox on P&WC engines to allow 1700 rpm propeller installation. High Cotton Aircraft Conversions, LLC - [STC SE00001EN](https://openairdocs.org/stc/SE00001EN): Engines will be maintained IAW 'Maintenance or Reliable Engines(MORE) Program,' Rev 2, 8/16/95. MORE Company Inc - [STC SE00014EN](https://openairdocs.org/stc/SE00014EN): Installation 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. Pratt & Whitney Engine Services Inc - [STC SE00020EN](https://openairdocs.org/stc/SE00020EN): Installation of the Pratt & Whitney Engine Services, Inc. TrendCheck/ TrendCheck Plus Engine Monitor Kit P/N TREND-K-010-1. Pratt & Whitney Engine Services Inc - [STC SE2960SO](https://openairdocs.org/stc/SE2960SO): Installation of an oil filler cap safety adapter. Jet Avion Corporation - [STC SE615GL](https://openairdocs.org/stc/SE615GL): Incorporation of a fuel flow transducer. Shadin Avionics - [STC SE01805NY](https://openairdocs.org/stc/SE01805NY): Installation of Fuel Nozzle Adapters using studs and nuts. Atlantic Turbines International Inc - [STC SE09257SC](https://openairdocs.org/stc/SE09257SC): Convert P&W Engine Models PT6A-15AG, -27, and -28, into PT6A-34 configuration. Covington Aircraft Engines, Inc - [STC SE659NE](https://openairdocs.org/stc/SE659NE): Installation of oil tank filler neck check valve, P/N TSA-76A. Aviation Components Support - [STC SE4570SW](https://openairdocs.org/stc/SE4570SW): Revise accessory drive spline, P/N 3008181. Aviall of Texas, Inc ## Related - Other T Scott Stanwyck LANCAIR EVOLUTION aircraft: https://openairdocs.org/model/t-scott-stanwyck-lancair-evolution/aircraft.md - The Pratt & Whitney Canada PT6A-42 engine: https://openairdocs.org/engine/pratt-whitney-canada-pt6a-42.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.