| SA00024NY | | 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 | | 10/3/2012 |
| SA00061LA | | Installation of JPI digital tachometer. | | Amended | | 1/12/1996 |
| SA00063LA | | Installation of Acoustical/Thermal insulation. | | Reissued | | 1/5/2005 |
| SA00068SE (PAGE 2) | | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | | Amended | | 10/20/2010 0:00 |
| SA00071SE | | Cockpit sun visor installation. | | Amended | | 7/7/2004 |
| SA00072BO | | Installation of Avidyne Model 5RR-MFC-3XX-( ) multifunctional flight computer and Ryan International TCAD Model 9900B Traffic Alert and Collision Device. | | Amended | | 9/24/2001 |
| SA00079NY | | Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. | | Amended | | 10/31/2012 |
| SA00081NY | | Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | | Amended | | 5/15/2002 |
| SA00081SE | | Installation of Continental IO-550A engine and Hartzell PHC-C3YF-2UF/ FC7382 propeller. | | Reissued | | 5/20/1994 |
| SA00105BO | | Installation of BF Goodrich WX-500 Stormscope Series II Weather Mapping Sensor to interface with Avidyne Model 5RR-MFC-1XX-() Multifunction Flight Computer. | | Issued | | 8/20/1999 |
| SA00117DE | | 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 | | 3/14/2003 |
| SA00133AT | | Installation of 0.250 inch side windows. | | Amended | | 3/20/1998 |
| SA00133WI | | Installation of GARMIN global positioning system GPS 155. | | Issued | | 2/16/1994 |
| SA00149BO | | Installation of Aircraft Components Volt and Vac Alert p/n 2044-1. | | Amended | | 5/15/2003 |
| SA00151WI-D | | Installation of Bendix/King KLX 135 and KLX 135A GPS/COMM (Global Positioning System Navigation Receiver with VHF Communications Transceiver) | | Reissued | | 2/28/2000 |
| SA00161BO (2 OF 3 | | Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. | | Amended | | 2/8/2005 0:00 |
| SA00165BO | | 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 | | 2/20/2003 |
| SA00187AT | | Installation of carbon steel brake discs P/N AA-20. | | Reissued | | 11/14/1994 |
| SA00206AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| SA00238SE | | Installation of Aviation Development Corporation s sump mounted chip detector | | Issued | | 10/31/1995 |
| SA00241WI-D | | Installation of Bendix/King KLN 90B Global Positioning System (GPS) for enroute and approach IFR operation. | | Reissued | | 2/28/2000 |
| SA00243BO (3 OF 5) | | 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 | | 7/21/2011 |
| SA00243SE | | Gross weight increase as modified per STC SA5691NM. | | Amended | | 6/13/2001 |
| SA00243WI-D | | Installation of Bendix/King KLN 35A GPS (Global Positioning System) Navigation Receiver. | | Reissued | | 2/28/2000 |
| SA00244WI-D | | Installation of Bendix/King KLN 89 GPS (Global Positioning System) Navigation Receiver for VFR operations installation of KLN 89B GPS Navigation Receiver for IFR enroute and non-precision approach operations. | | Reissued | | 2/28/2000 |
| SA00247WI-D | | Installation of Bendix/King KLX 135 and KLX 135A GPS/COMM (Global Positioning System Navigation Receiver with VHF Communications Transceiver). For serial numbers 680001 and above | | Reissued | | 2/28/2000 |
| SA00260SE | | Installation of engine cowling. | | Issued | | 12/20/1995 |
| SA00269BO (2 OF 3) | | 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 | | 4/9/2010 |
| SA00281BO | | 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 | | 4/24/2012 |
| SA00290BO ( PAGE3) | | Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX | | Reissued | | 7/1/2010 0:00 |
| SA00300NY-D | | Update TNL2000T system to Trimble 2000 Approach. | | Reissued | | 11/18/1999 |
| SA00306WI | | Installs TKS anti-icing system components and approves aircraft for flight into known icing conditions. | | Amended | | 4/6/2007 |
| SA00366AT | | Installation of an oil filter funnel on oil dipstick tube. | | Issued | | 11/4/1993 |
| SA00372WI | | Installation of GARMIN GNC300 VHF communication transceiver/ GPS receiver. | | Issued | | 10/16/1995 |
| SA00402SE | | Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) | | Amended | | 1/23/2007 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| SA00442WI-D | | Installation of Bendix/King KAP 140 Automatic Flight Control System. For model M20J serial numbers 24-3000 and after | | Reissued | | 2/28/2000 |
| SA00472SE | | Gross weight increase as modified per STC SA00081SE. | | Issued | | 10/16/1997 |
| SA00478CH (PAGE 1) | | Installation of Cooper Superflite 102 Fabric. | | Amended | | 5/10/2012 |
| SA00502WI | | Installation of the GARMIN GNC 250XL VHF Communication Transceiver/GPS Receiver.
);INSERT INTO stc_table VALUES ( | | Issued | | 4/24/1997 |
| SA00511SE | | Installation of a type 7308 lamp. | | Issued | | 4/17/1998 |
| SA00569AT | | Installation of Aero-Trim 800 electric elevator trim system. (M20 up to and including M20J-24-854) | | Amended | | 12/14/1995 |
| SA00600DE | | Installation of pilot and co-pilot instrument panels for M20C Serial No | | Issued | | 3/17/2006 |
| SA00642WI | | Installation of GARMIN Transponder GTX 320. | | Issued | | 4/2/1998 |
| SA00649AT | | Installation of an infinitely adjustable cowl flap control system. | | Issued | | 1/31/1995 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| SA00688CH | | Installation of McCauley Propeller model D3A36C430/74SA-0. | | Reissued | | 9/21/2005 |
| SA00735WI | | Installation of GARMIN dual GNS 430. | | Issued | | 2/8/1999 |
| SA00736WI | | Installation of GARMIN GMA-340. | | Issued | | 2/9/1999 |
| SA00744DE | | Installation of Automatic Dependent Surveillance | | Amended | | 3/28/2013 |
| SA00748SE | | Replace original power plant and propeller with a Continental TSIOL-550A engine and McCauley 3AF36C525/G-80VMFA-2 propellers. | | Issued | | 10/21/1999 |
| SA00749AT | | Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) | | Amended | | 12/10/1997 |
| SA00771WI-D | | Installation of Bendix/King KFC 225 automatic flight control system. | | Reissued | | 2/28/2000 |
| SA00780SE (PAGE 3) | | 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 | | 5/11/2010 |
| SA00783NY | | 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 | | 1/23/1998 |
| SA00803AT | | Installation of low profile landing gear doors. | | Amended | | 9/4/1997 |
| SA00805AT | | Installation of Lycoming IO-360-A3B6 or IO-360-A3B6D engine and 201 cowling. | | Issued | | 7/12/1995 |
| SA00807AT | | Modification of brake system to a dual piston caliper brake system. | | Issued | | 7/13/1995 |
| SA00824WI-D | | Installation of Bendix/King KMD 150 MDF Multi-Function Display. | | Reissued | | 2/28/2000 |
| SA00832WI | | Installation of a McCauley propeller part number 2A34C241/82PGC-6. | | Issued | | 11/5/1999 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00879WI | | Installation of GARMIN Navtalk Pilot provisions kit. | | Issued | | 5/26/2000 |
| SA00928WI | | Install Garmin GTX 327 GMA 340 GNS 430 GNS 530 for Mooney M20M with GNS 430 or GNS 530 VHF Communication Transceiver/VOR/ILS Receiver/GPS Receiver. | | Amended | | 12/18/2000 |
| SA00933WI-D | | Installation of Bendix/King KMD 550 Multi-Function Display (MFD) system optional Bendix/King KGP 560 General Aviation Enhanced ground proximity warning system (GA-EGPWS) and optional WX 500 Stormscope. MDL 159-08262-0001 dtd 12/11/00 and 2. If KGP 560 is installed AFM Supplement 006-0881-0000 dtd 01/10/01 or later approved revision. | | Issued | | 1/10/2001 |
| SA00934WI-D | | Installation of Bendix/King KLN 94 GPS (Global Positioning System) Navigation Receiver for IFR enroute and non-precision approach operations. | | Issued | | 1/15/2001 |
| SA00941AT | | Repositioning of a battery from the engine compartment to the aft equipment bay. | | Issued | | 1/9/1996 |
| SA00942AT | | Installation of Vernier propeller control cable with ground adjustable friction lock. | | Amended | | 2/24/1999 |
| SA00943AT | | Installation of Vernier throttle control cable. | | Issued | | 1/9/1996 |
| SA00944AT | | Installation of Vernier mixture control cable. | | Issued | | 1/10/1996 |
| SA00946AT | | Installation of cowling upgrade Mod Works 201 style. | | Issued | | 1/10/1996 |
| SA00954SE (1 OF 2) | | 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 | | 8/11/2003 |
| SA00954SE (2 OF 2) | | 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 | | 8/11/2003 |
| SA00956WI | | Installation of a McCauley propeller part number 3A32C418-G/82NRC-9 using propeller and spinner installation drawing 3A32C418/G/82NRC-9. | | Reissued | | 7/8/2008 |
| SA01026SE (PAGE 2) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01077SE (PAGE 1) | | Installation of fluoropolymer film. | | Reissued | | 8/20/2003 |
| SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| SA01105WI-D (2 OF 2) | | 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 | | 5/31/2007 |
| SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| SA01205WI-D (2 OF 2) | | Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors.
);INSERT INTO stc_table VALUES ( | | Amended | | 11/20/2007 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01240SE (1 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 0:00 |
| SA01280CH | | Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) | | Issued | | 8/29/2000 |
| SA01310AT | | Installation of a Mooney One-Piece Lower Fuselage Skin P/N 310322-501 and related attachment structure. | | Amended | | 10/9/1998 |
| SA01405WI | | Installation of the Garmin GFC 700 Automatic Flight Control System and TAWS Option. | | Reissued | | 11/17/2006 |
| SA01435DE | | Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine. | | Reissued | | 5/25/2011 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| SA01439SE | | Installation of vortex generators on the wings and tail surfaces of the above model aircraft | | Amended | | 11/19/2012 |
| SA01465AT | | Install Mooney aircraft model M20J windshield. | | Amended | | 12/13/2001 |
| SA01473SE (3 OF 5) | | Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde | | Amended | | 5/21/2008 |
| SA01477SE | | Installation of the Garmin G1000 integrated avionics system in accordance with Garmin AT Master Data List 005-C0229-00 Revision B or later FAA approved revision. | | Issued | | 11/16/2004 |
| SA01516AT | | Installation of Vision Micro Systems Inc. VM1000/EC100 digital/analog engine instrumentation and caution advisory system. | | Amended | | 10/24/2008 |
| SA01527AT | | Install Mooney M20J M20I rear side windows in Mooney M20F and M20G models. | | Issued | | 12/12/1997 |
| SA01553AT | | Modify the side windows by replacing the existing 3/16 inch thick glass with 1/4 inch thick glass. | | Issued | | 2/18/1998 |
| SA01560WI-D | | Installation of the Honeywell KFD 840 Primary Flight Display System.
);INSERT INTO stc_table VALUES ( REQUIRED DATA: AML 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 | | 7/22/2010 |
| SA01642AT | | Installation of a Lycoming model IO-360-A1A or IO-360-A1B6D or IO-360-A3B6 or IO-360-A3B6D engine modified. | | Reissued | | 2/29/2000 |
| SA01644AT | | 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 | | 9/12/2003 |
| SA01648AT | | Installation of a replacement composite instrument panel glare shield and center console. | | Reissued | | 9/24/1998 |
| SA01660LA | | Installation of Air-Tec Alternator kit. Descriptive data pertaining to this design change are considered inadequate for duplication in other aircraft. This approval is limited to the installation on Mooney M20B S/N 1900 only. | | Issued | | 3/30/2005 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01692SE (Page 1 OF 2) | | Installation of a Garmin GMX 200 Multi-Function Display | | Reissued | | 10/3/2012 |
| SA01695SE (3 OF 5) | | Installation of an antenna | | Amended | | 2/15/2007 |
| SA01714WI (Page 1) | | Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality | | Issued | | 5/1/2013 |
| SA01734SE (PG 3) | | Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. | | Amended | | 3/23/2011 |
| SA01800SE (PG 2) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01830SE | | Installation of a Semi-Portable Oxygen System | | Reissued | | 2/12/2009 |
| SA01860NY (2 OF 3) | | Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | | Amended | | 5/31/2006 |
| SA01861SE (PAGE 3) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| SA01923LA | | Installation of the P-1000 Digital Electronic Tachometer. | | Issued | | 1/23/2007 |
| SA01933LA (3 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 0:00 |
| SA01982NY-D | | Installation of Garmin International GNS-530 COM/NAV/GS/GPS and GMA-340 audio system with Marker Beacon. | | Issued | | 12/11/2008 |
| SA01983NY-D | | Installation of Garmin International GTX-330 Mode-S Transponder. | | Reissued | | 12/11/2008 |
| SA01988SE (PAGE 5) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
| SA02004CH | | Installation of a Hartzell PHC-J3YF-1RF/F7963DF(B)-2 propeller and A-2295-10(P) spinner. | | Reissued | | 8/24/2004 |
| SA02013CH | | Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). | | Amended | | 5/2/2011 |
| SA02015SE-D | | Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. | | Amended | | 2/5/2014 |
| SA02018SE-D (PAGE 2) | | 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 | | Issued | | 1/4/2011 0:00 |
| SA02019SE-D Page 2 | | Installation of Garmin GTN 6XX/7XX Navigation System | | Amended | | 12/19/2012 |
| SA02033AT (PAGE 3) | | Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) | | Amended | | 7/25/2008 |
| SA02041AT | | Installation of a new technology landing light. | | Issued | | 12/16/1999 |
| SA02110CH (PAGE 2) | | Installation of a Time Trac Data Recorder | | Reissued | | 1/11/2010 |
| SA02119SE Page 2 | | Installation of Garmin GDL 88 ADS-B UAT Transceiver System | | Issued | | 12/28/2012 |
| SA02154AK (PAGE 1 ) | | Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. | | Amended | | 1/12/2005 |
| SA02168AK (PG 2) | | Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. | | Issued | | 3/23/2001 1:00 |
| SA02193CH | | Power increase to 310 BHP by Installation of Powerlite STC SE02930AT or CMI IO-550N Engine rated at 310 BHP/2700 RPMs and Hartzell Propeller Model PHC-J3YF-1RF/F7693DF(B)-2 propeller | | Amended | | 5/3/2013 |
| SA02203AK (PAGE 1) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| SA02204AT | | Installation of Continental IO-360-ES engine and other associated airplane mods. | | Amended | | 12/5/2000 |
| SA02212AK (PG 3) | | Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. | | Amended | | 5/4/2011 |
| SA02217AK (1 OF 5) | | 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 | | 12/1/2004 |
| SA02222NY-D | | Installation of Insight Instruments Corp TAS-1000 Air Data Computer | | Issued | | 4/16/2007 |
| SA02232AT | | Installation of composite nose cowl nose landing gear doors and induction air system. | | Issued | | 11/6/2000 |
| SA02265SE | | Installation of a camera housing | | Amended | | 11/1/2013 |
| SA02283SE Page 1 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
| SA02293AK (1 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
| SA02349LA | | 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 | | 6/6/2011 |
| SA02353AK-D | | Fabrication and installation of F. Atlee Dodge Aircraft Services LLC P/N 6103-01 (left) and/or 6103-02 (right) rear jump seat | | Issued | | 7/23/2009 |
| SA02414CH-D | | Installation of the Hartzell propeller model HC-C2YR-1BFP/F7497 and Hartzell 835-54(P) or A-2295-5(P) spinner. | | Amended | | 8/4/2010 |
| SA02431AT | | Installation of a BAE-14/28 Air Driven Alternator on a Mooney M20 Aircraft | | Issued | | 11/29/2001 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02461NY | | Installation of propeller MTV-12-B/180-59b. | | Issued | | 10/5/2007 |
| SA02482CH | | Installation of Hartzell Propeller Model PHC-J3YF-1N/N7605()-2 composite propeller | | Amended | | 6/7/2013 |
| SA02483CH | | Modify aircraft to utilize full 310 BHP @ 2700 rpm rated power of existing installed Teledyne Continental Motors (TCM) TSIO-550-G engine. | | Amended | | 6/7/2013 |
| SA02491AT | | Installation of air traffic detector ATD-200. | | Issued | | 4/25/2002 |
| SA02520AT | | Installation of M-20 Oil Separator model 600-WP. | | Issued | | 5/30/2002 |
| SA02547AT (PG 2) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 0:00 |
| SA02549AT | | Modification of engine exhaust system for improved engine performance. | | Amended | | 1/9/2003 |
| SA02624AT | | This STC converts the Mooney M20L to essentially an M20R. The STC requires minor changes to the aircraft structure and includes installation of a Continental IO-550-N16B engine (The engine is operated at the performance limits of 280 hp at 2500 rpm just like the Continental IO-550-G used on the Mooney M20R.) The STC is to be accomplished in accordance with Mod Works Master Document List MW8800-000 Revision B dated April 30 2003 or later FAA approved revision. | | Reissued | | 11/25/2003 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02738CH (PAGE 1) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
| SA02795AT | | Installation of a PXE7300SR In-Flight Entertainment System | | Issued | | 2/12/2004 |
| SA02930NY | | 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 | | 6/12/2012 |
| SA02987CH | | Installation of the Electroair Electronic Ignition System | | Amended | | 7/23/2013 |
| SA02988AT | | Change in rating of the existing Teledyne Continental Motors IO-550-G Model engine to the same as that for the IO-550-G engine installed in the Mooney M20R 280 hp at 2500 rpm and the installation of a Hartzell Model PHC-J3YF-1RF/F7693DF(B)-2 propeller. Aircraft modification shall be performed in accordance with PowerLite Report AP1016-5 Installation Instructions Revision A dated November 25 2004 or later FAA Approved revision. | | Reissued | | 5/17/2005 |
| SA03024CH | | Installation of Hartzell Propeller models PHC-J3YF-1RF/7498()3 bladed metal propeller. Modification of aircraft in accordance with Minnis Aviation Installation Instructions No. M2011-3 Revision IR dated 10/25/11 or later. FAA Approved revision. This STC may be used with previously modified aircraft that incorporate STC Nos SA02842CH SA02843CH or SA02988AT. | | Issued | | 12/7/2011 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA03165CH | | Installation of MT Propeller model MTV-14-D/(188-193)-30( ) in Mooney aircraft models M20R M20S and M20TN | | Amended | | 5/7/2013 |
| SA03393AT | | Installation of Monroy Aerospace Corporation Traffic-Watch ATD-300. | | Issued | | 8/26/2004 |
| SA09011AC-D | | Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-592 with optional autotrim system. | | Amended | | 1/3/2002 |
| SA09122AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System with optional autotrim system. | | Amended | | 11/6/2001 |
| SA09158AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-632 with Optional Autotrim System. | | Amended | | 8/15/2001 |
| SA09212AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-676-20/30. | | Amended | | 6/13/1997 |
| SA09219AC-D | | Installation of S-TEC System20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-678-20/30. | | Issued | | 5/19/1997 |
| SA09220AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-677. | | Issued | | 5/21/1997 |
| SA09221AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-679. | | Issued | | 5/23/1997 |
| SA09223AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-680-20/30. | | Issued | | 5/20/1997 |
| SA09271AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-681. | | Issued | | 8/20/1997 |
| SA09308AC-D | | Installation of S-TEC system 20/30 single and two axis automatic flight guidance systems. | | Amended | | 6/20/2000 |
| SA09309AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-746. | | Amended | | 8/3/2000 |
| SA09382AC-D | | Installation of S-TEC system 55 two axis automatic flight guidance system Model ST-839 with optional autotrim system. | | Amended | | 7/19/2001 |
| SA09392AC-D | | Installation of S-TEC Manual Electric Trim System Model ST-846. | | Amended | | 2/16/1999 |
| SA09393AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-843-20/30. | | Amended | | 2/16/1999 |
| SA09395AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-844. | | Issued | | 9/23/1998 |
| SA09470SC | | Installation of Starter Indicator light system. | | Issued | | 6/18/2001 |
| SA09564AC | | Installation of MT-Propller MTV-12-B/180-17. | | Issued | | 7/23/2002 |
| SA09565AC | | Installation of MTV-12-D/188-53 propeller. | | Issued | | 7/23/2002 |
| SA09695AC | | Installation of Lycoming IO-390-A3A6 engine and Hartzell Model HC-C2YR-1BFP/F7497 or HC-C3YR-1RF/F7282 propeller | | Reissued | | 1/7/2013 |
| SA1-585 | | External electrical power receptacle. | | Amended | | 1/1/1960 |
| SA1-615 | | Installation of Fram lube oil filter Model PB55-1. | | Amended | | 9/11/1967 |
| SA1008WE | | Installation of Poly-Fiber covering material. | | Reissued | | 5/27/2003 |
| SA10126SC (2 OF 2) | | Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision. | | Amended | | 10/23/2003 |
| SA10236SC (1 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA1026GL | | Installation of Pamco emergency backup pneumatic system. | | Amended | | 4/27/1988 |
| SA10372SC | | 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 | | 7/7/2005 |
| SA1053SW | | Installation of Mitchell automatic flight system model AK287 consisting of Century III autopilot with optional automatic pitch trim and radio coupler. | | Reissued | | 9/7/1984 |
| SA10682SC | | Installation of alternator and voltage regulator | | Reissued | | 11/16/2007 |
| SA1074GL | | Installation of a cooling shroud. | | Amended | | 5/1/2007 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA1090GL | | Installation of an auxiliary blower motor driven in cabin/ windshield heating system. | | Issued | | 11/17/1986 |
| SA10SW | | External power plug. | | Issued | | 1/1/1961 |
| SA1111SO | | Installation of an adjustable trim tab on the left aileron. | | Amended | | 11/8/1996 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1156WE | | Installation of Roto-Master (Rajay) turbocharged Lycoming IO-360-A1A or O-360-A1D engine. | | Reissued | | 11/14/2002 |
| SA1172WE | | Lateral stability augmentation system LSA-4. | | Reissued | | 10/1/1973 |
| SA1177WE | | WECO carburetor temperature monitor. | | Issued | | 1/1/1960 |
| SA1198WE | | NAV-2 flight control system or B-6 flight control system. | | Reissued | | 10/1/1973 |
| SA1212CE | | 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 | | 2/28/2000 |
| SA1258SW | | Porta-cool Model PC70 portable air conditioner. | | Issued | | 2/1/1971 |
| SA1300CE | | Installation of Edo-Aire propeller governor Model 34-828-014-11. | | Reissued | | 9/17/1990 |
| SA1315WE | | 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 | | 4/15/2011 |
| SA1351WE (PG 1) | | Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) | | Amended | | 8/19/1983 |
| SA135EA | | Installation of engine exhaust combustion monitor. | | Reissued | | 2/14/1972 |
| SA1387GL | | Installation of Lycoming O-360-A1F6D and McCauley propeller B2D34C214. | | Issued | | 6/7/1989 |
| SA138WE | | Installation of Grimes Model D-7080 rotating beacon on vertical fin. | | Reissued | | 2/25/2000 |
| SA1411WE | | Installation of Roto-Master (Rajay) turbocharged Lycoming IO-360-A1A engine. | | Reissued | | 11/14/2002 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1462WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1464CE | | 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 | | 2/28/2000 |
| SA1489WE | | Installation of Brittain Industries Inc. Model B2C or BSS Flight Control System | | Reissued | | 1/31/2013 |
| SA1502GL | | Installation of on-board engine analyzer system. | | Issued | | 7/18/1990 |
| SA1505GL | | Installation of Hartzell propeller model PHC-J3YF-1RF/F7663-2R and associated spinner assembly. | | Amended | | 5/25/1994 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1525CE-D | | Installation of King KNS 81 digital area navigation system when interfaced with approved DME or TACAN. | | Reissued | | 2/28/2000 |
| SA1525CED | | Installation of King KNS 81 digital area navigation system. | | Issued | | 1/23/1980 |
| SA152NW | | Installation of deck and glare shield (with or without instrument lights). | | Amended | | 5/21/1981 |
| SA1550WE | | Installation of Brittain LSA-4 flight control system. | | Issued | | 1/1/1960 |
| SA1557CE-D | | Installation of KAS 297 altitude select option. | | Reissued | | 2/28/2000 |
| SA1557CED | | Installation of KAS 297 altitude select option. | | Amended | | 8/1/1983 |
| SA1561CE-D | | 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 | | 2/28/2000 |
| SA1561CED | | Installation of KAP 100 single axis KAP 150 two-axis or FKC 150 two-axis flight control system. | | Amended | | 7/29/1983 |
| SA1570WE | | Installation of Brittain NAV-2 flight control system. | | Reissued | | 10/20/1972 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1584WE | | Installation of Brittain Model B-6 flight control system. | | Reissued | | 10/20/1972 |
| SA1588WE | | Installation of supplemental exterior flashing lights. | | Issued | | 1/30/1968 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1641CE | | Installation safe flight SC-150 stall warning and angle of attack indicating system. | | Issued | | 3/13/1981 |
| SA1735GL | | Installation of Master Nag warning system. | | Amended | | 3/21/1994 |
| SA1745SO | | Installation of Appalachian Access. stainless steel brake rotors P/N 75-20. | | Reissued | | 2/6/1995 |
| SA1762NM | | Installation of a pressurized magneto system on the Continental turbocharged TSIO-360-C F and FB engines. | | Reissued | | 3/14/2006 |
| SA1771CE-D | | Installation of King KFC 200 flight control system (2 axis) with or without flight director. (M20J s/n 24-1368 24-1419 and up.) (M20K s/n 25-0740 25-0791 and up) | | Reissued | | 2/28/2000 |
| SA1771CED | | Installation of King KFC 200 flight control system (2 axis) with or without flight director. (M20J s/n 24-1368 24-1419 and up) (M20K s/n 25-0740 25-0791 and up) | | Amended | | 3/18/1983 |
| SA1780WE | | Installation of Brittain Industries LSA-5 flight control system. | | Reissued | | 10/20/1972 |
| SA1785WE | | Installation of Brittain Industries B2C flight control system. | | Reissued | | 10/20/1972 |
| SA1786WE | | Installation of Brittain Industries B-6 flight control system. | | Reissued | | 10/20/1972 |
| SA1787WE | | Installation of Brittain NAV-2B flight control system | | Reissued | | 6/21/2013 |
| SA1798GL | | Installation of multi-sensor long range navigation system. Limited to installation on serial number 24-0336 ONLY. | | Reissued | | 2/17/2004 |
| SA179SW | | Nose wheel well doors 8367-1 and8367-2. | | Issued | | 1/1/1960 |
| SA1838SO | | Installation of auxiliary fuel tanks. | | Issued | | 9/30/1985 |
| SA1913SO | | Auxiliary fuel cells are installed. | | Amended | | 3/16/2007 |
| SA191NE | | Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. | | Reissued | | 10/4/1984 |
| SA1938SW | | Brittain LSA-6 lateral stability augmentation system (positive control). | | Reissued | | 7/15/2013 |
| SA195CH | | Installation of McCauley propeller model B3D36C424/74SA. | | Reissued | | 7/19/2006 |
| SA2-952 | | Installation of fiberglass covering. | | Reissued | | 9/10/1996 |
| SA2052NM | | Installation of Beryl D Shannon Aviation Specialties Engine Crankcase Breather Air-Oil Seperator | | Issued | | 3/4/1983 |
| SA2074CE-D | | Install 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 | | 2/28/2000 |
| SA2078NM | | Installation of a late model instrument panel | | Issued | | 7/18/1983 |
| SA2154NM | | Installation of Turboplus intercooler system M20K-12000. | | Reissued | | 10/15/2007 |
| SA2168NM | | Installation of the Precise Flight stand-by vacuum system (SVS). | | Amended | | 11/7/2003 |
| SA2174NM | | Installation of Precise Flight speedbrake system. | | Amended | | 11/7/2003 |
| SA2190NM Page 1 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2207SW | | Installation of Brittain Industries Inc. NAV-FLITE II and B-5 Flight Control Systems | | Reissued | | 6/21/2013 |
| SA2210NM | | Installation of Hoskins Model CFS-1000A -1001A FT-100 or FT-101 fuel flow indicating system. (M20C S/N 2807 and up) | | Reissued | | 1/30/1996 |
| SA224SW | | Automatic pilot AK117. | | Issued | | 1/1/1960 |
| SA225NE | | Replace original wheel brake discs with discs modified in accordance with Aviation Services. | | Issued | | 1/10/1984 |
| SA2271SO | | Replacement of Cleveland brake discs P/N 164-9 or 164-109 with Appalachian Accessories stainless steel brake discs P/N 73-9. | | Reissued | | 9/29/1995 |
| SA2277CE | | Installation of fuel bladder cells in wet wing fuel cavities. | | Amended | | 12/22/2003 |
| SA2318CE-D | | Installation of Bendix/King EHI 40 electronic horizontal situation indicator system. | | Reissued | | 2/28/2000 |
| SA2319CE-D | | Installation of the Bendix/King KAP 100 Single Axis KAP 150 Two Axis or KFC 150 Two Axis Automatic Flight Control System and optional KAS 297B Vertical Speed and Altitude Selector. | | Reissued | | 2/28/2000 |
| SA2320CE-D | | Installation of the Bendix/King KLN 88 Loran C system. | | Reissued | | 2/28/2000 |
| SA2330SO | | Installation of an adjustable trim tab on the rudder. | | Issued | | 5/17/1988 |
| SA2332CE-D | | Installation of the Bendix/King KLN 90 global positioning system(GPS). | | Reissued | | 2/28/2000 |
| SA2350CE | | Installation of fuel bladder cells in integral fuel tank and wing cavities. | | Amended | | 12/22/2003 |
| SA2350NM Page 1 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA2367CE | | Installation of TKS anti-icing system components with placard stating Flight into known icing conditions prohibited. | | Reissued | | 7/8/2008 |
| SA241SO | | Mooney dorsal fin 4175-51. | | Issued | | 1/1/1960 |
| SA2445CE | | Installation of Continental TSIO-360-MB engine McCauley Model 2A34C221-B/90DHC-16E propeller and new Mooney cowling. (M20K SN 25-0001 thru 25-0999) | | Reissued | | 9/7/1993 |
| SA250GL | | Installation of either Lycoming IO-360-A1B6 or IO-360-A3B6 or IO-360-A3B6D model engines with various Hartzell and McCauley propellers. | | Amended | | 1/19/1996 |
| SA2513NM | | Installation of relocated oil radiator. | | Issued | | 10/9/1985 |
| SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
| SA2586NM (PAGE 3) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2619WE | | Installation of Pathfinder Model P1-( ) autopilot system. | | Reissued | | 9/30/1998 |
| SA2620WE | | Installation of Pathfinder Model P2-( ) autopilot system. | | Reissued | | 9/30/1998 |
| SA2654WE | | Installation of Pathfinder Model P2A( ) autopilot. | | Amended | | 7/3/1979 |
| SA2687NM (PAGE 1) | | Installation of Truboplus/ Electronics Int l gauges and switches. | | Amended | | 10/25/2000 |
| SA2693NM (PAGE 1) | | Installation of Electronics International digital volt/amp gauges and accessories. | | Amended | | 12/10/2009 |
| SA2711NM | | Installation of Lycoming IO-360-A3B6 engine with McCauley propeller B2D34C214. | | Reissued | | 2/10/1994 |
| SA2742NM | | Installation of a Lycoming IO-360-A3B6 or A3B6D engine. | | Amended | | 9/7/2005 |
| SA2763NM | | Installation of freon type cabin air conditioning system. (M20K SN 25-1000 and on) | | Reissued | | 6/16/1987 |
| SA2823SW | | Reinforcement of vertical tail spar. | | Issued | | 7/31/1978 |
| SA2844CE (2 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 0:00 |
| SA289CH | | Installation of Inline Pneumatic Air Filter P/N CV1J4 | | Reissued | | 1/15/2013 |
| SA2968WE | | Installation of manifold pressure gage/fuel flow meter (fuel pressure gage) in lieu of original gage/ meter. | | Reissued | | 6/25/1996 |
| SA2986WE | | Installation of Pathfinder autopilot systems. (M20 SERIES see MDL No. 77-030-1 for approved models) | | Reissued | | 9/30/1998 |
| SA2993WE | | Installation of Pathfinder autopilot systems and/or electric pitch trim systems. (M20C s/n 20-0011 and on-1974 s/n 20-1147 and on-1975) (M20E s/n 21-0025 and on-1974 s/n 21-1161 and on-1975) | | Reissued | | 9/30/1998 |
| SA300CE | | Installation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO) | | Amended | | 5/14/1992 |
| SA3047SW-D | | Mitchell automatic flight system AK523 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 6/22/1984 |
| SA3047SWD | | Mitchell automatic flight system AK523 consisting of Century III autopilot with optional radio and glide slope couplers. | | Reissued | | 6/22/1984 |
| SA3048SW-D | | Mitchell automatic flight system AK476 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 8/16/1984 |
| SA3048SWD | | Mitchell automatic flight system AK476 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 8/16/1984 |
| SA3049SW-D | | Mitchell automatic flight system AK475 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 8/16/1984 |
| SA3049SWD | | Mitchell automatic flight system AK475 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 8/16/1984 |
| SA3064SW-D | | Mitchell command electric trim AK541. | | Reissued | | 6/22/1984 |
| SA308EA (1 OF 2) | | Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) | | Amended | | 11/20/1978 |
| SA3106SO | | Installation of a Teledyne Continental Motors model TSIO-360MB engine. (M20K SN 25-0001 thru 25-0889) | | Issued | | 12/31/1991 |
| SA3145SO | | Provides an approved procedure for applying Aero-Trim Aeroseal P/N 500 externally to wing skin seams of fuel tanks to stop seepage from micro leaks up to .005 inches wide. | | Amended | | 2/20/1992 |
| SA315CH | | Installation of McCauley propeller model B3D36C424/74SA-0. | | Amended | | 11/9/2006 |
| SA3186WE | | Installation of Pathfinder autopilot systems and/or pitch trim systems. | | Reissued | | 9/30/1998 |
| SA320GL | | Installation of Hartzell Model HC-C2YK-1( )F/F7666A-4Q propeller in lieu of Hartzell Model HC-C2YK-1/7666-2 propeller using original installation hardware and components on aircraft previously modified in accordance with STC No. SA250GL. No installation data are required. | | Issued | | 6/28/1979 |
| SA3222WE | | Installation of Pathfinder autopilot systems and/or pitch trim systems. (M20C s/n 20-0011 and on) (M20E s/n 21-0025 and on) | | Reissued | | 9/30/1998 |
| SA3252NM | | Installation of fiberglass belly fairing. | | Issued | | 5/27/1986 |
