# Pilatus PC-7 - Type: Aircraft model (FAA registry) - Registry code: 7090401 - Manufacturer (registry): PILATUS - Model: PC-7 - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Turbo-prop - Seats: 2 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS A50EU](https://openairdocs.org/tcds/A50EU) (OpenAirDocs) - Holder: Pilatus Aircraft Ltd. - Registered aircraft: 19 - Page: https://openairdocs.org/model/pilatus-pc-7 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2020-26-19](https://openairdocs.org/ad/2020-26-19): Time Limits/Maintenance Checks · Pilatus PC-7. Effective Mar 29, 2021 - [AD 2021-04-06](https://openairdocs.org/ad/2021-04-06): Flight Compartment, Emergency Equipment · Pilatus PC-7. Effective Feb 12, 2021 - [AD 2019-05-15](https://openairdocs.org/ad/2019-05-15): Electric Power · Pilatus PC-7. Effective Apr 23, 2019 - [AD 2018-04-10](https://openairdocs.org/ad/2018-04-10): Landing Gear · Pilatus PC-7. Effective Apr 12, 2018 - [AD 2016-17-07](https://openairdocs.org/ad/2016-17-07): Fuselage · Pilatus PC-7. Effective Sep 30, 2016 - [AD 2015-07-04](https://openairdocs.org/ad/2015-07-04): Air Conditioning · Pilatus PC-7. Effective May 19, 2015 - [AD 2015-01-03](https://openairdocs.org/ad/2015-01-03): Standard Practices/Structures · Pilatus PC-7. Effective Mar 2, 2015 - [AD 2013-22-13](https://openairdocs.org/ad/2013-22-13): Electrical Power · Pilatus PC-7. Effective Nov 29, 2013 - [AD 2013-13-10](https://openairdocs.org/ad/2013-13-10): Engine Controls · Pilatus PC-7. Effective Aug 14, 2013 - [AD 2013-01-06](https://openairdocs.org/ad/2013-01-06): Fuselage · Pilatus PC-7. Effective Feb 7, 2013 - [AD 2010-22-09](https://openairdocs.org/ad/2010-22-09): Wings · Pilatus PC-7. Effective Dec 3, 2010 - [AD 2010-12-04](https://openairdocs.org/ad/2010-12-04): Fuselage · Pilatus PC-7. Effective Jul 13, 2010 - [AD 2009-26-05](https://openairdocs.org/ad/2009-26-05): Landing Gear. · Pilatus PC-7. Effective Feb 1, 2010 - [AD 2009-16-02](https://openairdocs.org/ad/2009-16-02): Fuselage. · Pilatus PC-7. Effective Sep 9, 2009 - [AD 2006-23-01](https://openairdocs.org/ad/2006-23-01): Main landing gear bay · Pilatus PC-7. Effective Dec 13, 2006 - [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005 - [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005 - [AD 2004-23-01](https://openairdocs.org/ad/2004-23-01): Fuel Booster pumps · Pilatus PC-7. Effective Dec 27, 2004 - [AD 2004-04-01](https://openairdocs.org/ad/2004-04-01): Engine-driven pump housing · Pilatus PC-12, PC-12/45 and PC-7. Effective Mar 29, 2004 - [AD 2003-20-05](https://openairdocs.org/ad/2003-20-05): Forward and Aft Dihedral Fittings · Pilatus PC-7. Effective Nov 14, 2003 - [AD 2002-22-03](https://openairdocs.org/ad/2002-22-03): Main Landing Gear Front Attachment Brackets · Pilatus PC-7. Effective Dec 20, 2002 - [AD 2001-26-13](https://openairdocs.org/ad/2001-26-13): Emergency Landing-gear Extension System · Pilatus PC-7. Effective Feb 12, 2002 - [AD 2001-05-02](https://openairdocs.org/ad/2001-05-02): Elevator and Rudder Attachment Brackets · Pilatus PC-7. Effective Apr 27, 2001 - [AD 2000-01-10](https://openairdocs.org/ad/2000-01-10): Elevator and Rudder Trim Tab Pivot Arms · Pilatus PC-7. Effective Mar 3, 2000 - [AD 98-16-16](https://openairdocs.org/ad/98-16-16): Main Lainding Gear And Nose Landing Gear Leg Seal Unit · Pilatus PC-7. Effective Sep 21, 1998 Historical (superseded or no longer in force): - [AD 2002-01-09](https://openairdocs.org/ad/2002-01-09) (historical): Gasket Material and Relief Valve Attachment Screws · Pilatus PC-12, PC-12/45 and PC-7. Effective Feb 28, 2002 - [AD 98-08-22](https://openairdocs.org/ad/98-08-22) (historical): Elevator and Rudder Attachment Brackets · Pilatus PC-7. Effective May 31, 1998 - [AD 98-08-07](https://openairdocs.org/ad/98-08-07) (historical): Elevator and Rudder Trim Tab Pivot Arms · Pilatus PC-7. Effective Apr 28, 1998 ## Registered aircraft (19) - [N101PC](https://openairdocs.org/aircraft/N101PC): [Somers Charles](https://openairdocs.org/faa-owner/SOMERS%20CHARLES), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1978, S/N 101 - [N1NG](https://openairdocs.org/aircraft/N1NG): [Lewis Aeronautical LLC](https://openairdocs.org/faa-owner/LEWIS%20AERONAUTICAL%20LLC), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio), built 1999, S/N 614 - [N517GM](https://openairdocs.org/aircraft/N517GM): [Spitfire Aviation LLC](https://openairdocs.org/faa-owner/SPITFIRE%20AVIATION%20LLC), [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale), built 1982, S/N 395 - [N519AH](https://openairdocs.org/aircraft/N519AH): [Comanche Maverick Air LLC](https://openairdocs.org/faa-owner/COMANCHE%20MAVERICK%20AIR%20LLC), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 1987, S/N 519 - [N548MB](https://openairdocs.org/aircraft/N548MB): [Somers Charles](https://openairdocs.org/faa-owner/SOMERS%20CHARLES), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1988, S/N 548 - [N60LT](https://openairdocs.org/aircraft/N60LT): [Eastern Stearman Inc Trustee](https://openairdocs.org/faa-owner/EASTERN%20STEARMAN%20INC%20TRUSTEE), [Leesburg, VA](https://openairdocs.org/faa-place/VA/Leesburg), S/N 615 - [N618S](https://openairdocs.org/aircraft/N618S): [Lewis Aeronautical LLC](https://openairdocs.org/faa-owner/LEWIS%20AERONAUTICAL%20LLC), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio), S/N 618 - [N66PN](https://openairdocs.org/aircraft/N66PN): [Somers Charles](https://openairdocs.org/faa-owner/SOMERS%20CHARLES), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), S/N 617 - [N6AT](https://openairdocs.org/aircraft/N6AT): [Mayer Jon R](https://openairdocs.org/faa-owner/MAYER%20JON%20R), [Reno, NV](https://openairdocs.org/faa-place/NV/Reno), S/N 447 - [N717LE](https://openairdocs.org/aircraft/N717LE): [Tentacle Corp](https://openairdocs.org/faa-owner/TENTACLE%20CORP), [Walnut Creek, CA](https://openairdocs.org/faa-place/CA/Walnut%20Creek), built 1988, S/N 549 - [N76XC](https://openairdocs.org/aircraft/N76XC): [Hangar C-403 LLC](https://openairdocs.org/faa-owner/HANGAR%20C-403%20LLC), [Walnut Creek, CA](https://openairdocs.org/faa-place/CA/Walnut%20Creek), built 1985, S/N 485 - [N795MK](https://openairdocs.org/aircraft/N795MK): [Southern Palms Leasing LLC](https://openairdocs.org/faa-owner/SOUTHERN%20PALMS%20LEASING%20LLC), [Sarasota, FL](https://openairdocs.org/faa-place/FL/Sarasota), built 1985, S/N 487 - [N807JH](https://openairdocs.org/aircraft/N807JH): [Clark Joseph](https://openairdocs.org/faa-owner/CLARK%20JOSEPH), [Seattle, WA](https://openairdocs.org/faa-place/WA/Seattle), built 1985, S/N 498 - [N816BP](https://openairdocs.org/aircraft/N816BP): [Als Aviation LLC](https://openairdocs.org/faa-owner/ALS%20AVIATION%20LLC), [Westlake Village, CA](https://openairdocs.org/faa-place/CA/Westlake%20Village), built 1985, S/N 480 - [N828PC](https://openairdocs.org/aircraft/N828PC): [Sbma Services LLC](https://openairdocs.org/faa-owner/SBMA%20SERVICES%20LLC), [Mcclellan, CA](https://openairdocs.org/faa-place/CA/Mcclellan), S/N 479 - [N870](https://openairdocs.org/aircraft/N870): [A & S Aviation LLC](https://openairdocs.org/faa-owner/A%20%26%20S%20AVIATION%20LLC), [Chesterfield, MO](https://openairdocs.org/faa-place/MO/Chesterfield), built 1993, S/N 607 - [N901AK](https://openairdocs.org/aircraft/N901AK): [A C Sunni LLC](https://openairdocs.org/faa-owner/A%20C%20SUNNI%20LLC), [Santa Monica, CA](https://openairdocs.org/faa-place/CA/Santa%20Monica), built 2000, S/N 616 - [N902AK](https://openairdocs.org/aircraft/N902AK): [Dillon Aero Inc](https://openairdocs.org/faa-owner/DILLON%20AERO%20INC), [Phoenix, AZ](https://openairdocs.org/faa-place/AZ/Phoenix), built 1988, S/N 560 - [N98VK](https://openairdocs.org/aircraft/N98VK): [Fb Aviation Services LLC](https://openairdocs.org/faa-owner/FB%20AVIATION%20SERVICES%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1989, S/N 559 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 19990730026509I](https://openairdocs.org/incident/19990730026509I), Jul 30, 1999: Pilats PC7 (N98VK), Oshkosh, WI, Minor damage. (-23) On July 30, 1999 at approx 1200 CST a pilatos PC-7 N98VK piloted by virgil l. kreder while landing runway 27 at Oshkosh airport, Oshkosh, WI, blew the… ## Service difficulty reports (9) As reported by operators and repair stations, by the model named in the report. - [SDR 2023FA0000272](https://openairdocs.org/sdr/2023FA0000272), May 1, 2023: SHIMMY DAMPENER. EXCESS PLAY. PILOT REPORTED NOSE WHEEL SHIMMY UPON LANDING. FOUND SLIGHT AMOUNT OF PLAY IN R/H SHIMMY DAMPER. BOTH SHIMMY DAMPERS WERE REPLACED. PILOT REPORTED NO ABNORMAL S - [SDR CA150927001](https://openairdocs.org/sdr/CA150927001), May 4, 2015: ENGINE. MALFUNCTIONED. (CAN) THIS EVENT WAS RE-CLASSIFIED FROM CAT 3 TO CAT 2. PILOT REPORTED THE FOLLOWING: "THE PILOT NOTICED THAT THE PCL WAS NOT MOVING FREELY ON THE PRE-FLIGHT. I - [SDR CA150519015](https://openairdocs.org/sdr/CA150519015), Apr 7, 2015: LINE. LEAKING. (CAN) AFTER LANDING WITH THE POWER LEVER AT IDLE, THE NG DROPPED TO 44 PERCENT WITH AMBER CAUTION AND NP DROPPED TO APPROXIMATELY 700. TROUBLESHOOTING FOUND A L - [SDR CA140602011](https://openairdocs.org/sdr/CA140602011), Apr 23, 2014: CHIP DETECTOR. BROKEN. (CAN) HAD TO ABORT A FLIGHT DUE TO UNEXPECTED SMOKE FROM THE RT EXHAUST. THE ACFT LANDED UNEVENTFUL. THE SUBSEQUENT INSPECTION IDENTIFIED A BROKEN REDUCTION GEA - [SDR CA110214007](https://openairdocs.org/sdr/CA110214007), Feb 7, 2011: ENGINE. FAILED. IFSD (SINGLE ENGINE) WHILE AT T/O FOR A NIGHT FLIGHT, AS THE POWER WAS INCREASED TO MAXIMUM, A LOUD NOISE WAS HEARD AND FIRE/SPARKS WERE SEEN COMING OUT OF THE - [SDR CA070514041](https://openairdocs.org/sdr/CA070514041), Mar 27, 2007: DRIVE SHAFT. SHEARED. (CAN) THE ENGINE WAS FOUND NOT TO RESPOND TO THROTTLE INPUT AND SUBSEQUENTLY ACCELERATED UNCOMMANDED. THE ENGINE WAS SHUTDOWN ON APPROACH. SUBSEQUENT INSPECTION - [SDR CA060531011](https://openairdocs.org/sdr/CA060531011), May 11, 2006: ENGINE. POWER LOSS. (CAN) THE ENGINE WAS REPORTED TO HAVE LOST POWER FOLLOWING TAKE-OFF, RESULTING IN A FORCED LANDING. - [SDR CA051006014](https://openairdocs.org/sdr/CA051006014), Sep 22, 2005: BLEED VALVE. OUT OF LIMITS. (CAN) ON TAKE-OFF ROLL, THE ENGINE SURGED, ACCOMPANIED BY FLAMES EMITTED FROM THE EXHAUST. SUBSEQUENT INVESTIGATION DETERMINED THE COMPRESSOR BLEED VALVE CLOSIN - [SDR CA050527024](https://openairdocs.org/sdr/CA050527024), May 14, 2005: ENGINE. MALFUNCTIONED. DURING DESCENT, THE ENGINE EXPERIENCED AN UNCOMMANDED DECREASE IN TORQUE, ACCOMPANIED BY AN INCREASE IN TURBINE TEMPERATURE. THE ENGINE DID NOT RESPOND TO THROT ## STCs that may be installed (OpenAirDocs) (54, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc - [STC SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc - [STC SA04046CH PAGE 2](https://openairdocs.org/stc/SA04046CH%20PAGE%202): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA02587AK](https://openairdocs.org/stc/SA02587AK): Installation of Electronic Flight Information System (EFIS) and avionics. Genesys Aerosystems Inc - [STC SA04264CH](https://openairdocs.org/stc/SA04264CH): Installation of Parker Hannifin Corporation, Aircraft Wheel & Brake Division 199-282 Conversion Kit for main wheels and brakes. Kaman Corporation Aircraft Wheel and Brake LLC - [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA02135SE](https://openairdocs.org/stc/SA02135SE): Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data). Electronics International Inc - [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation - [STC SA02153LA-D PAGE 1](https://openairdocs.org/stc/SA02153LA-D%20PAGE%201): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA8323SW](https://openairdocs.org/stc/SA8323SW): Install Pratt & Whitney Canada PT6A-25C engine and Hartzell HC-B3TN-2/T10178(N)-8R propeller. Sierra Industries Ltd - [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. Avidyne Corporation - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00352BO PAGE 2](https://openairdocs.org/stc/SA00352BO%20PAGE%202): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA02119SE PAGE 2](https://openairdocs.org/stc/SA02119SE%20PAGE%202): Installation of Garmin GDL 88 ADS-B UAT Transceiver System. Garmin International Inc - [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics - [STC SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc - [STC SA02442AK PAGE 2](https://openairdocs.org/stc/SA02442AK%20PAGE%202): Approval of the L-3 Communications NGT 2000/2500 ADS-B system. ADS-B Technologies, LLC - [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc - [STC SA02717NY PAGE 1](https://openairdocs.org/stc/SA02717NY%20PAGE%201): Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module. VoiceFlight Systems LLC - [STC SA02015SE-D](https://openairdocs.org/stc/SA02015SE-D): Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc - [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation - [STC SA00674WI-D](https://openairdocs.org/stc/SA00674WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II system installation. Rockwell Collins Inc - [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc - [STC SA00681WI-D](https://openairdocs.org/stc/SA00681WI-D): Modification of Collins VHF-20/VHF-20A/VHF-20B VHF COMM Receiver Transmitter with CTL-20 Control Pro Line I System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation. Rockwell Collins Inc - [STC SA02018SE-D](https://openairdocs.org/stc/SA02018SE-D): Provisions installation of Garmin GPS/XM Antennas in accordance with FAA Approved Model List (AML) SA02018SE-D, dated January 4, 2011, or later FAA approved revision, and FAA Approved GPS/XM Antenna STC Master Drawing List, Document No.: 005-00638-01, Revision 1 , approved on January 4, 2011, or later FAA approved revision. Garmin International Inc - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc - [STC SA02293AK](https://openairdocs.org/stc/SA02293AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Chelton Flight Systems Inc - [STC SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc - [STC SA01306WI-D](https://openairdocs.org/stc/SA01306WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation. Rockwell Collins Inc - [STC SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc - [STC ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models. SMR Technologies - [STC SA01141WI-D](https://openairdocs.org/stc/SA01141WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head. Rockwell Collins Inc - [STC SA01668SE](https://openairdocs.org/stc/SA01668SE): Schroth Pilot and Copilot seat harness installation. Western Aircraft - [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision. Garmin AT Inc - [STC SA02154AK](https://openairdocs.org/stc/SA02154AK): Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500. Garmin AT Inc - [STC SA02217AK](https://openairdocs.org/stc/SA02217AK): Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision. Garmin AT Inc - [STC SA8545SW-D](https://openairdocs.org/stc/SA8545SW-D): Installation of a Century Automatic flight system kit no. AK1067, consisting of a Century 41 autopilot/flight director. (when modified by STC SA8323SW, increased shaft horsepower). Century Flight Systems Inc - [STC SA8546SW-D](https://openairdocs.org/stc/SA8546SW-D): Installatio of a Century yaw damper system, kit no. YK1068 consisting of a Century yaw damper per bulletin no. 2133 dtd 3/28/01, and master drawing list no. 87A1292 dtd 3/28/01 (28-volt system) and/or later FAA/DAS approved revision. Century Flight Systems Inc - [STC SA688NE](https://openairdocs.org/stc/SA688NE): Installation of Safeway Model 6900 deicer boot. Safeway Products, Inc All 54: https://openairdocs.org/model/pilatus-pc-7/stcs.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.