Hauptmenü:
Alle aufgelisteten STC sind der FAA Database for Supplement Type Certificates (STC) unter www.faa.gov entnommen und dienen ausschließlich der Information.
Da insgesamt über 250 STC zu finden sind, habe ich die STC nach Themenblöcken zusammengefasst.
"Speed Mods" sind Modifikationen mit dem Ziel, die Effizienz oder Geschwindigkeit weiter zu steigern. LASAR ist einer der noch aktiven Hersteller, wogegen ModWorks die Arbeit leider eingestellt hat.
Im Block "Powerplant" fasst Motor und Propeller samt Anbauteilen zusammen. Unter "Avionics" findet man alles, was mit Navigation und Kommunikation zu tun hat. Für die Motorüberwachung zuständige STC sind unter "Instrumente" zusammengefasst. Weitere Modifikationen unter "Other".
STC | Description | Status | Date |
Installation of Continental IO-550A engine and Hartzell PHC-C3YF-2UF/ FC7382 propeller. | Reissued | 20.05.1994 | |
Gross weight increase as modified per STC SA00081SE. | Issued | 16.10.1997 | |
Installation of low profile landing gear doors. | Amended | 04.09.1997 | |
Modification of brake system to a dual piston caliper brake system. | Issued | 13.07.1995 | |
Installation of a Mooney One-Piece Lower Fuselage Skin, P/N 310322-501, and related attachment | Amended | 09.10.1998 | |
Installation of vortex generators on the wings and tail surfaces of the above model aircraft | Amended | 19.11.2012 | |
Install Mooney aircraft model M20J windshield. | Amended | 13.12.2001 | |
Installation of a replacement composite instrument panel, glare shield, and center console. | Reissued | 24.09.1998 | |
Installation of composite nose cowl, nose landing gear doors, and induction air system. | Issued | 06.11.2000 | |
Installation of a camera housing | Amended | 01.11.2013 | |
Installation of Precise Flight speedbrake system. | Amended | 07.01.2003 | |
Installation of Spoilers, Inc hydraulically operated wing spoiler system | Reissued | 30.10.1987 | |
Installation of wing root fairings. | Reissued | 25.06.1996 | |
Installation of Precise Flight 100 or 2000 Series Speedbrake System. | Amended | 07.11.2003 | |
Installation of Precise Flight 24/28 Volt Series 100 Speedbrake System. | Amended | 24.12.1991 | |
Installation of gap seals and speed fairings involving 10 kits. | Issued | 09.07.1982 | |
Installation of dorsal fin. (M20A w/metal tail) | Reissued | 25.06.1996 | |
Installation of flap gap seals. | Issued | 21.09.1982 | |
Installation of wing tips similar to those for Mooney Model M20J, M20K, or earlier models. | Reissued | 25.06.1996 | |
Installation of wing tips similar to those for Mooney Model M20J, M20K, or earlier models. | Reissued | 25.06.1996 | |
Installation of Precise flight manual control speedbrake. | Amended | 07.11.2003 | |
Installation of composite wing tips. Position light installation approval is not part of this mod. Serial number airplanes eligible are: M20B/C/D/E - all; M20F - s/n 680171 and on; M20G - 680163 and on; M20J - s/n 24-0001 through 24-1037. | Reissued | 02.08.2002 | |
Installation of Mooney (OEM) wing tips. | Issued | 04.02.1993 |
STC | Description | Status | Date |
Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. | Amended | 10.03.2012 | |
Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | Amended | 15.05.2002 | |
Installation of Oilamatic Preoiler system per FAA approved Oilamatic, Inc. Drawing List No. M20400, initial release, dated 6/1/94 or later FAA approved revisions. | Amended | 14.03.2003 | |
Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | Amended | 14.08.1995 | |
Installation of Aviation Development Corporation's sump mounted chip detector | Issued | 31.10.1995 | |
Installation of an oil filter funnel on oil dipstick tube. | Issued | 04.11.1993 | |
Installation of a remote spin-on oil filter adapter. | Amended | 23.01.2007 | |
Installation of Vernier propeller control cable with ground adjustable friction lock. | Amended | 24.02.1999 | |
Installation of Vernier throttle control cable. | Issued | 09.01.1996 | |
Installation of Vernier mixture control cable. | Issued | 10.01.1996 | |
Installation of Challenger Spin-On Oil Filters. | Issued | 29.08.2000 | |
Installation of a Lycoming model IO-360-A1A, or IO-360-A1B6D, or IO-360-A3B6 or IO-360-A3B6D engine modified. | Reissued | 29.02.2000 | |
Installation of Challenger Reusable Air Filter | Amended | 21.06.2012 | |
Modification to install an air-oil separator to prevent oil from being aspirated from the engine | Amended | 25.07.2008 | |
Installation of Continental IO-360-ES engine and other associated airplane mods. | Amended | 05.12.2000 | |
Installation of the Hartzell propeller model HC-C2YR-1BFP/F7497 and Hartzell 835-54(P) or A-2295-5(P) spinner. | Amended | 04.08.2010 | |
Installation of a BAE-14/28 Air Driven Alternator on a Mooney M20 Aircraft | Issued | 29.11.2001 | |
Installation of propeller MTV-12-B/180-59b. | Issued | 05.10.2007 | |
Installation of M-20 Oil Separator, model 600-WP. | Issued | 30.05.2002 | |
Installation of the Electroair Electronic Ignition System | Amended | 23.07.2013 | |
Installation of MT-Propller MTV-12-B/180-17. | Issued | 23.07.2002 | |
Installation of Lycoming IO-390-A3A6 engine and Hartzell Model HC-C2YR-1BFP/F7497 or HC-C3YR-1RF/F7282 propeller | Reissued | 07.01.2013 | |
Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision. | Amended | 23.10.2003 | |
Installation of a cooling shroud. | Amended | 01.05.2007 | |
Installation of Plane-Power ALT-FLX alternator | Reissued | 10.05.2013 | |
Installation of Edo-Aire propeller governor Model 34-828-014-11. | Reissued | 17.09.1990 | |
Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | Reissued | 12.06.1984 | |
Installation of McCauley propeller model B3D36C424/74SA. | Reissued | 19.07.2006 | |
Installation of the Precise Flight stand-by vacuum system (SVS). | Amended | 07.01.2003 | |
Installation of either Lycoming IO-360-A1B6 or IO-360-A3B6 or IO-360-A3B6D model engines with various Hartzell and McCauley propellers. | Amended | 19.01.1996 | |
Installation of a Lycoming IO-360-A3B6 or A3B6D engine. | Amended | 07.09.2005 | |
Installation of Woodward propeller governors on single and twin engine aircraft. | Amended | 14.05.1992 | |
Installation of Roto-Master (Rajay) turbocharged Lycoming IO-360-A3B6D and/or IO-360-A1D6D engines. | Reissued | 31.08.1995 | |
Installation of Aviation Development oil filter. | Amended | 22.05.2009 | |
Installation of a Hartzell HC-C3YR-1RF/F7282 constant speed propeller. | Reissued | 21.12.1992 | |
Installation of the Hartzell propeller model HC-C3YR-1RF/F7282 | Amended | 31.03.2010 | |
Installation of a Lycoming IO-360-A1B6D or IO-360-A3B6D engine modified. | Reissued | 09.11.1990 | |
Installation of electrically driven vacuum pump as a standby auxiliary pump to the existing instrument air system. | Reissued | 06.04.2007 | |
Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines. | Reissued | 10.02.2009 | |
Installation of Auto-Vac 2 auxiliary vacuum system. | Issued | 04.04.1988 | |
Install Champion SlickSTART magneto booster system. | Reissued | 10.02.2009 | |
Installation of McCauley C3D36C415/82NGA-8 propeller | Amended | 03.05.1991 | |
Installation of air filters | Reissued | 20.06.2000 | |
Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. | Issued | 21.07.1994 | |
Installation of various SMR Technologies electrical propeller deicer models. | Amended | 25.07.2006 |
STC | Description | Status | Date |
Installation of Avidyne Model 5RR-MFC-3XX-( ) multifunctional flight computer and Ryan International TCAD Model 9900B Traffic Alert and Collision Device. | Amended | 24.09.2001 | |
Installation of BF Goodrich WX-500 Stormscope Series II Weather Mapping Sensor to interface with Avidyne Model 5RR-MFC-1XX-() Multifunction Flight Computer. | Issued | 20.08.1999 | |
Installation of GARMIN global positioning system GPS 155. | Issued | 16.02.1994 | |
Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. | Amended | 08.02.2005 | |
Installation of Avidyne Corporation Datalink Coupler, part number 700-00015-000 per Avidyne Corporation Master Document List, Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. | Issued | 20.02.2003 | |
Installation of Bendix/King KLN 90B Global Positioning System (GPS) for enroute and approach IFR | Reissued | 28.02.2000 | |
Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200). | Amended | 21.07.2011 | |
Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000. | Reissued | 09.04.2010 | |
Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000 | Amended | 24.04.2012 | |
Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX | Reissued | 01.07.2010 | |
Update TNL2000T system to Trimble 2000 Approach. | Reissued | 18.11.1999 | |
Installation of GARMIN GNC300 VHF communication transceiver/ GPS receiver. | Issued | 16.10.1995 | |
Installation of Bendix/King KAP 140 Automatic Flight Control System. For model M20J, serial numbers 24-3000 and after | Reissued | 28.02.2000 | |
Installation of the GARMIN GNC 250XL VHF Communication Transceiver/GPS Receiver. | Issued | 24.04.1997 | |
Installation of GARMIN Transponder, GTX 320. | Issued | 02.04.1998 | |
Installation of GARMIN dual GNS 430. | Issued | 08.02.1999 | |
Installation of GARMIN GMA-340. | Issued | 09.02.1999 | |
Installation of Automatic Dependent Surveillance – Broadcast (ADS-B) Out Equipment using a Trig | Amended | 28.03.2013 | |
Installation of Automatic Dependent Surveillance – Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor | Reissued | 25.03.2014 | |
Installation of GARMIN Navtalk Pilot provisions kit. | Issued | 26.05.2000 | |
Installation of the VNS 1000 Voice Navigation System. | Reissued | 26.04.2010 | |
Installation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic, terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine). | Amended | 31.05.2007 | |
Installation of P2 Incorporated 6600 Audio Advisory system | Reissued | 04.11.2013 | |
Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. | Amended | 20.11.2007 | |
Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | Amended | 27.06.2007 | |
Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponder | Amended | 21.05.2008 | |
Installation of a GDL 69 or GDL 69A XM Satellite Receiver | Amended | 04.05.2012 | |
Installation of the Honeywell KFD 840 Primary Flight Display System. REQUIRED DATA: AML No. No. 159-08325-0002, Revision -, dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. | Amended | 22.07.2010 | |
Installation of a Landing Gear Warning System to incorporate a stall warning interface in accordance with Master Drawing List MDL-2037, Revision 7, dated July 14, 2003, or later FAA Approved Revision. | Amended | 12.09.2003 | |
Installation of a Garmin GMX 200 Multi-Function Display | Reissued | 03.10.2012 | |
Installation of an antenna | Amended | 15.02.2007 | |
Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality | Amended | 27.08.2013 | |
Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | Amended | 06.11.2006 | |
Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | Amended | 01.04.2013 | |
Installation of Garmin International GNS-530 COM/NAV/GS/GPS and GMA-340 audio system with Marker | Issued | 11.12.2008 | |
Installation of Garmin International GTX-330 Mode-S Transponder. | Reissued | 11.12.2008 | |
Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) | Issued | 17.04.2009 | |
Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). | Amended | 02.05.2011 | |
Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. | Amended | 05.02.2014 | |
Provisions installation of Garmin GPS/XM Antennas in accordance with FAA Approved Model List (AML) | Issued | 04.01.2011 | |
Installation of Garmin GTN 6XX/7XX Navigation System | Amended | 19.12.2012 | |
Installation of a Time Trac Data Recorder | Reissued | 11.01.2010 | |
Installation of Garmin GDL 88 ADS-B UAT Transceiver System | Issued | 28.12.2012 | |
Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System | Amended | 16.12.2013 | |
Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500. | Amended | 12.01.2005 | |
Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | Amended | 21.12.2011 | |
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 | Amended | 01.12.2004 | |
Installation of Insight Instruments Corp TAS-1000 Air Data Computer | Issued | 16.04.2007 | |
Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | Reissued | 11.01.2010 | |
Installation of air traffic detector ATD-200. | Issued | 25.04.2002 | |
Installation of a Voice Alert System. | Amended | 28.08.2007 | |
Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | Amended | 09.01.2012 | |
Installation of L-3 Communications Avionics Systems | Amended | 07.05.2010 | |
Installation of a PXE7300SR, In-Flight Entertainment System | Issued | 12.02.2004 | |
The installation of the Latitude Technologies Corporation S100 Tracking System | Issued | 26.09.2012 | |
Installation of Monroy Aerospace Corporation Traffic-Watch ATD-300. | Issued | 26.08.2004 | |
Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System, Model ST-632 with Optional Autotrim System. | Amended | 15.08.2001 | |
Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-676-20/30. | Amended | 13.06.1997 | |
Installation of S-TEC System20/30 Single and Two Axis Automatic Flight Guidance Systems, Model ST-678-20/30. | Issued | 19.05.1997 | |
Installation of S-TEC System 30 ALT Altitude Hold System, Model ST-677. | Issued | 21.05.1997 | |
Installation of S-TEC System 30 ALT Altitude Hold System, Model ST-679. | Issued | 23.05.1997 | |
Installation of a GDC 31 Roll Steering Converter | Amended | 22.03.2011 | |
Installation of Pamco emergency backup pneumatic system. | Amended | 27.04.1998 | |
Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot in accordance with the Master Drawing List No ST7893SC-A-12, Rev. B, dated January 7, 2005, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement No. ST7893SC-A-14, Rev. I.R., dated January 19, 2005, or later FAA approved revision is required. | Amended | 07.07.2005 | |
Installation of EFD1000 Primary Flight Display | Amended | 29.09.2009 | |
Installation of King KFC 200 2 axis (3 optional) flight control system with KCS 55/55A compass and King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller or third axis (yaw damper) only, or manual electric trim only (M20J S/N 24-001 THRU S/N 24-1093 EXCLUDING S/N 24-0073 AND S/N 24-0939 S/N 24-001 THRU S/N 24-1093 EXCLUDING S/N 24-0773 AND S/N 24-0939, M20F S/N 22-1305 AND ON) | Reissued | 28.02.2000 | |
Installation of KFC 200 two axis(three optional) flight control system. (M20J 24-0773; -0939; 24-1094 THRU 24-1418 EXCEPT 24-1368; M20K S/N 25-0001 thru 25-0790 except 25/0740) | Reissued | 28.02.2000 | |
Installation of King KNS 81 digital area navigation system. | Issued | 23.01.1980 | |
Installation of King KNS 81 digital area navigation system when interfaced with approved DME or TACAN. | Reissued | 28.02.2000 | |
Installation of KAS 297 altitude select option. | Reissued | 28.02.2000 | |
Installation of KAP 100 single axis, KAP 150 two axis, or KFC 150 two axis Flight Control System and optional KAS 297B vertical speed and altitude selector. | Reissued | 28.02.2000 | |
Installation safe flight SC-150 stall warning and angle of attack indicating system. | Issued | 13.03.1981 | |
Installation of King KFC 200 flight control system (2 axis), with or without flight director. | Reissued | 28.02.2000 | |
Installation of Brittain NAV-2B flight control system | Reissued | 21.06.2013 | |
Installation of multi-sensor long range navigation system. Limited to installation on serial number 24-0336 ONLY. | Reissued | 17.02.2004 | |
Brittain LSA-6 lateral stability augmentation system (positive control). | Reissued | 15.07.2013 | |
Installation of electronics International Digital Volt/Amp Gauges and Accessories. | Issued | 16.02.1984 | |
Installation of Brittain Industries Inc. NAV-FLITE II and B-5 Flight Control Systems | Reissued | 21.06.2013 | |
Installation of the Bendix/King KLN 88 Loran C system. | Reissued | 28.02.2000 | |
Installation of Inline Pneumatic Air Filter, P/N CV1J4 | Reissued | 15.01.2013 | |
Mitchell automatic flight system AK523 consisting of Century III autopilot with optional radio and glide slope couplers. | Reissued | 22.06.1984 | |
Mitchell automatic flight system AK476 consisting of Century IIB autopilot with optional radio coupler. | Reissued | 16.08.1984 | |
Mitchell automatic flight system AK475 consisting of Century I autopilot with optional omni tracker. | Reissued | 16.08.1984 | |
Mitchell command electric trim AK541. | Reissued | 22.06.1984 | |
Installation of Pathfinder autopilot systems and/or pitch trim systems. | Reissued | 30.09.1998 | |
Installation of Mitchell automatic flight system AK801 consisting of Century 41 autopilot or model AK801FD consisting of Century 41 flight director autopilot. | Reissued | 21.09.1983 | |
Installation of Mitchell automatic flight system AK802 consisting of Century 21 autopilot. | Reissued | 21.09.1983 | |
Installation of Mitchell automatic flight system, Model AK 884 consisting of a Century 31 autopilot. | Reissued | 15.08.1983 | |
Installation of Century automatic flight systems, Model AK961 consisting of a Century 2110/2130/2131 autopilot. | Issued | 19.02.1987 | |
Installation of Century automatic flight system, Model AK967 consisting of a Century 2010/2030/2031 autopilot. | Amended | 15.03.2000 | |
Installation of Century Command Electric Trim System Model AK984. | Issued | 22.08.1988 | |
Installation of Century Command Electric Trim System Model AK985. | Issued | 16.09.1988 | |
S-TEC system 60 (two axis) flight guidance system, Model ST-015, with optional flight director steering horizon and vertical speed indicator/selector(14 volt system). | Issued | 11.08.1980 | |
S-TEC manual electric trim system, Model ST-022. | Issued | 14.08.1980 | |
S-TEC system 60 pitch stabilization system Model ST-049 (14 volt system). | Reissued | 12.07.1982 | |
Installation of Brittain PC/AH II pitch stabilization system and altitude hold system. | Reissued | 12.07.2013 | |
Loran C Model TI 9100. | Issued | 18.05.1982 | |
S-TEC yaw damper system model ST-112 (14 volt system). | Issued | 07.07.1982 | |
Installation of SynCon alarm system. | Amended | 08.05.1990 | |
S-TEC system 60 pitch stabiization system ST-049 with optional automatic electric trim. | Amended | 28.08.1984 | |
Installation of S-TEC system 40/50 single and two axis automatic flight guidance systems, model ST-192-40/50. | Amended | 28.08.1984 | |
Installation of S-TEC yaw damper system, Model ST-112. | Amended | 23.10.1986 | |
Installation of S-TEC system 60 two axis automatic flight guidance system model ST-015 with optional automatic electric trim system. | Reissued | 14.10.1986 | |
Installation of S-TEC System 60 single axis automatic flight guidance system, model ST-318. | Issued | 03.06.1985 | |
Installation of S-TEC yaw damper system, model ST-320. | Amended | 21.10.1986 | |
Installation of S-TEC manual electric trim system, model ST-322. | Issued | 07.06.1985 | |
Installation of burglar alarm system. | Reissued | 21.07.1993 | |
Installation of S-TEC system 60 two axis automatic flight guidance system, model ST-333. | Issued | 09.04.1986 | |
Installation of S-TEC system 60 pitch stabilization system, Model ST-335. | Issued | 23.06.1986 | |
Installation of S-TEC system 40/50 single and two axis automatic flight guidance systems model ST-334-40/50. | Issued | 01.08.1986 | |
Installation of S-TEC System 65 two axis automatic flight guidance system. | Issued | 23.09.1986 | |
Installation of S-TEC System 65 two axis automatic flight guidance system, Model ST-383. | Issued | 26.11.1986 | |
Installation of S-TEC System 500 two axis automatic flight guidance system, Model ST-537, with optional automatic electric trim system. | Amended | 15.08.2001 | |
Installation of the VNS 1000 Voice Navigation System. | Reissued | 26.04.2010 | |
Installation of a voice alert system. | Amended | 13.05.2003 |
STC | Description | Status | Date |
Installation of JPI digital tachometer. | Amended | 01.12.1996 | |
Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | Amended | 20.10.2010 | |
Installation of Aircraft Components Volt and Vac Alert, p/n 2044-1. | Amended | 15.05.2003 | |
Installation of EGT 701 series fuel flow instrument. | Amended | 12.04.2013 | |
Installation of J.P. Instruments Slimline EGT-100 series primary instruments | Issued | 05.03.1999 | |
Installation of J.P. Instruments (JPI) fuel flow indicating system | Amended | 12.04.2013 | |
Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711, Report 106P, Revision B, dated August 2, 2001, or later FAA approved revision. | Amended | 11.08.2003 | |
Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | Reissued | 20.01.2005 | |
Installation of secondary voltage indication system | Reissued | 03.04.2006 | |
Installation of J.P. Instruments (JPI) Primary Engine Data Management System | Amended | 17.09.2013 | |
Installation of Vision Micro Systems Inc., VM1000/EC100 digital/analog engine instrumentation and caution advisory system. | Amended | 24.10.2008 | |
Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | Amended | 31.05.2006 | |
Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. | Issued | 23.03.2001 | |
Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) | Amended | 10.12.2013 | |
Installation of a Digital Engine Monitoring system. | Amended | 07.02.2012 | |
Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3, G2, and G1 as primary Cylinder Head Temperature (CHT), Exhaust Gas Temperature (EGT), and Turbine Inlet Temperature (TIT) Instruments. | Reissued | 12.06.2012 | |
Installation of Starter Indicator light system. | Issued | 18.06.2001 | |
Installation of Mixture Monitor (exhaust gas temperature probe, gage and selector) in accordance with Delta Products Part Lists A-192 and A-193, or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9, 1981, or later FAA approved revision and/or Drawing List MM-127 dated November 15, 1981, or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29, 1968, copy attached, or later FAA approved revision. | Reissued | 15.04.2011 | |
Installation of on-board engine analyzer system. | Issued | 18.07.1990 | |
Installation of exhaust gas temperature monitoring systems Model EGT-1. | Amended | 22.02.2007 | |
Installation of Electronics Int'l Digital EGT/CHT Instruments and accessories. (201 Series) | Amended | 09.03.1993 | |
Installation of Master Nag warning system. | Amended | 21.03.1994 | |
Installation of Electronics International Inc digital carburetor/outside air temperature gauges | Amended | 06.06.1990 | |
Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | Amended | 22.02.2007 | |
Installation of J.P. Instruments temperature monitoring systems. | Amended | 20.07.2008 | |
Installation of Truboplus/ Electronics Int'l gauges and switches. | Amended | 25.10.2000 | |
Installation of Electronics International digital volt/amp gauges and accessories. | Amended | 10.12.2009 | |
Installation of manifold pressure gage/fuel flow meter (fuel pressure gage) in lieu of original gage/ meter. | Reissued | 25.06.1996 | |
Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system. | Issued | 03.07.1986 | |
Installation of Hoskins Model CFS-1000, -1001, FT-100, or FT-101 fuel flow indicating system. | Reissued | 30.01.1998 | |
Installation of Electronics International Primary TIT/EGT/CHT instruments, remote switches and associated accessories. | Amended | 25.04.198 | |
Installation of Silver Instruments Fueltron IG or IP or Fuelgard digital fuel flow and totalizer system. | Reissued | 29.04.1991 | |
Installation of Electronics Int'l digital automatic engine analyzer. | Amended | 13.10.1989 | |
Installation of ALCOR fuel flow/totalizer system 24606. | Reissued | 30.09.2002 | |
Installation of an electronic digital engine tachometer, Model P-1000, P/N P100030- . | Amended | 14.01.2002 | |
Installation of RPM instrument. | Amended | 24.11.1997 | |
Installation of oil pressure/temperature instrument. | Amended | 08.12.1997 | |
Installation of manifold pressure instrument. | Amended | 15.08.1993 | |
Installation of a Shadin Company Fuel Flow Indicating System | Reissued | 08.06.2006 | |
Installation of the following Aerospace Logic aircraft instruments: EGT-100 Exhaust Gas Temperature | Issued | 08.07.2003 |
STC | Description | Status | Date |
Installation of engine cowling. | Issued | 20.12.1995 | |
Installation of fluoropolymer film. | Reissued | 20.08.2003 | |
Installation of an adjustable trim tab on the left aileron. | Amended | 08.11.1996 | |
Installation of an adjustable trim tab on the rudder. | Issued | 17.05.1988 | |
Installation of TKS anti-icing system components, with placard stating 'Flight into known icing conditions prohibited.' | Reissued | 08.07.2008 | |
Installation of fiberglass belly fairing. | Issued | 27.05.1986 | |
Installation of cowling stiffener. | Reissued | 02.05.1993 | |
Installation of a one-piece fiberglass belly pan with skid runners. | Issued | 13.06.1990 | |
Installation of inflatable door seal. | Issued | 30.06.1980 | |
Installation of extended baggage compartment. | Amended | 19.08.1988 | |
Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) | Amended | 10.12.1997 | |
Installation of an airfoil ahead of the fuel tank vent to sweep super cooled water droplets out of the air before they can impinge on the fuel tank vent and cause an ice obstruction. | Issued | 23.01.1998 | |
Improved fuel gascolator assembly. | Amended | 19.12.2012 | |
Auxiliary fuel cells are installed. | Amended | 16.03.2007 | |
Installation of fuel bladder cells in wet wing fuel cavities. | Amended | 22.12.2003 | |
Installation of carbon steel brake discs, P/N AA-20. | Reissued | 14.11.1994 | |
Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE, dated February 1, 2001, or later FAA approved revision. | Amended | 11.05.2010 | |
Installation of Lake Aero Styling and Repair Nose Gear Truss in accordance with Lake Aero Styling and Repair Master Document List LA155, Revision B, dated February 23, 2011 or later FAA approved revision. | Issued | 06.06.2011 | |
Installation of Appalachian Access. stainless steel brake rotors, P/N 75-20. | Reissued | 06.02.1995 | |
Replace original wheel brake discs with discs modified in accordance with Aviation Services. | Issued | 10.01.1984 | |
Replace original brake discs w/William C. Roberts stainless steel discs, P/N 201-120-SS. (M20M s/n 27-0001 thru 27-0116) | Reissued | 18.06.2002 | |
Installation of modified nose gear bushings. | Reissued | 21.08.2013 | |
Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | Amended | 18.12.2007 | |
Installation of a Nose Landing Gear Steering Horn Assembly in accordance with FAA approved Lake Aero Styling and Repair Master Drawing List No. LA720000MDL, Revision B, dated October 15, 2003 or later FAA approved revisions. | Issued | 17.10.2003 | |
Installation of a type 7308 lamp. | Issued | 17.04.1998 | |
Fabrication and installation of new or replacement of existing instrument panel lights dimmer | Reissued | 01.12.2011 | |
Fabrication and installation of Landing Light Controller | Reissued | 01.12.2011 | |
Installation of a new technology landing light. | Issued | 16.12.1999 | |
Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. | Amended | 04.05.2011 | |
Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | Amended | 22.05.2012 | |
Installation of tail floodlight system. | Issued | 03.06.1985 | |
Fabrication and installation of F. Atlee Dodge Aircraft Services, LLC P/N 6103-01 (left) and/or 6103-02 (right) rear jump seat | Issued | 23.07.2009 | |
Cockpit sun visor installation. | Amended | 07.07.2004 | |
Installation of 0.250 inch side windows. | Amended | 20.03.1998 | |
Modify the side windows by replacing the existing 3/16 inch thick glass with 1/4 inch thick glass. | Issued | 18.02.1998 | |
Installation of .250-inch side windows. | Amended | 18.03.1993 |