| 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 |
| SA00058WI-D | | Installation of Bendix/King KAP100/KAP 150/KFC 150 automatic flight control systems with optional KAS297B altitude/vertical speed selector. | | Reissued | | 2/28/2000 |
| SA00061LA | | Installation of JPI digital tachometer. | | Amended | | 1/12/1996 |
| SA00068SE (PAGE 1) | | Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) | | Amended | | 10/20/2010 |
| SA00079SE | | Installation of low oil pressure warning in conjunction with ADC (Oberg) oil filter. | | Amended | | 11/10/1994 |
| SA00081NY | | Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | | Amended | | 5/15/2002 |
| SA00136WI | | Operation of airplane on unleaded or leaded automotive gasoline 91 minimum antiknock index (RON+MON)/2 | | Issued | | 8/12/1994 |
| SA00161BO (2 OF 3 | | Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. | | Amended | | 2/8/2005 0:00 |
| SA00187AT | | Installation of carbon steel brake discs P/N AA-20. | | Reissued | | 11/14/1994 |
| SA00206BO | | Installation of alternate air induction system. | | Reissued | | 9/26/2007 |
| 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 |
| SA00243BO (1 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 |
| 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 |
| 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 |
| SA00380LA | | Limited to installation on serial number AA5-0037 ONLY. | | Issued | | 6/12/1997 |
| SA00393SE | | Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. | | Issued | | 12/6/1996 |
| SA00402SE | | Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) | | Amended | | 1/23/2007 |
| SA00457WI | | Replacement of a new oil cooler. | | Issued | | 7/22/1996 |
| SA00478CH (PAGE 3) | | Installation of Cooper Superflite 102 Fabric. | | Amended | | 5/10/2012 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| 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 |
| 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 |
| SA00958CH | | Install split nose bowl. | | Issued | | 10/16/1998 |
| SA01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| 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 |
| SA01250WI | | Installation of Concorde Sealed Lead-acid (VRSLA) battery | | Reissued | | 7/30/2012 |
| 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 |
| SA01284AT | | Installation of Composite Spinner Bulkhead. | | Amended | | 10/13/2000 |
| SA01354CH | | Install BRC Aviation tailcone part number BRC 5103011-1 -2 BRC 5103012 -2. | | Issued | | 6/29/2001 |
| SA01406CH | | Install BRC Aviation main landing gear faring part numbers BRC 5701050-3 -4. | | Issued | | 1/10/2002 |
| SA01410CH | | Install BRC Aviation dorsal fin part number BRC 5302040-1. | | Issued | | 6/28/2001 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| 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 |
| SA01487SE-D (Page 2) | | Installation of a GDL 69 or GDL 69A XM Satellite Receiver | | Amended | | 5/4/2012 |
| SA01516AT | | Installation of Vision Micro Systems Inc. VM1000/EC100 digital/analog engine instrumentation and caution advisory system. | | Amended | | 10/24/2008 |
| 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 |
| SA01658NY | | Installation of MT-Propeller MTV-18-B/180-17 3-blade electrically controlled propeller. | | Issued | | 4/11/2003 |
| 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 |
| SA01800SE (PG 2) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01852AT | | Replace metal propeller spinner bulkhead with composite bulkhead. | | Amended | | 10/13/2000 |
| SA01860NY (2 OF 3) | | Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | | Amended | | 5/31/2006 |
| SA01861SE (PAGE 2) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| SA01933LA-D Page 2 | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation
);INSERT INTO stc_table VALUES ( System | | Amended | | 4/1/2013 |
| SA01933LA (2 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 0:00 |
| SA01944CH (1 OF 2) | | Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. | | Issued | | 3/5/2004 |
| SA01988SE (PAGE 4) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
| 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 1) | | Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. | | Amended | | 7/25/2008 |
| SA02033AT (PAGE 5) | | 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 0:00 |
| SA02057AT | | Installation of a composite nose bowl. | | Amended | | 3/27/2001 |
| SA02119SE Page 2 | | Installation of Garmin GDL 88 ADS-B UAT Transceiver System | | Issued | | 12/28/2012 |
| SA02153LA-D (Page 2) | | Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System | | Amended | | 12/16/2013 |
| SA02154AK (PAGE 1 ) | | Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. | | Amended | | 1/12/2005 |
| SA02212AK (PG 4) | | 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 |
| SA02251LA | | Installation of fiberglass cowling and improved engine baffles. | | Reissued | | 8/6/2012 |
| SA02268CH (PAGE 5) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02268CH (PAGE 6) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02283SE Page 2 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02448AT | | Replace exhaust system with a tuned exhaust system. | | Issued | | 1/8/2002 |
| 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 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02738CH (PAGE 3) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
| 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 |
| SA03148NY (PAGE 2 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA08528SW-D | | Installation of a Century Flight System Model AK1051 consisting of a Century 2110/2150/2151 autopilot. | | Issued | | 7/3/1998 |
| SA09369AC-D | | Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems Model ST-822-20/30. | | Issued | | 6/19/1998 |
| SA09370AC-D | | Installation of S-TEC System 30 ALT altitude hold system Model ST-823. | | Issued | | 6/19/1998 |
| SA09386AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-840-20/30. | | Issued | | 9/17/1998 |
| SA09390AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-841. | | Issued | | 9/17/1998 |
| SA09990SC | | Installation of Sensenich Propeller 74DM7S10-1-57B and 74DM7S10-1.5-61B. | | Issued | | 5/16/2002 |
| SA10126SC (1 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 |
| SA1018NW | | Installation of a Lycoming O-320-E2A engine (with a controllable pitch propeller crankshaft P/N 75010) and a McCauley 1C172/BTM7356 propeller | | Issued | | 9/12/1980 |
| SA10344SC | | Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot. | | Issued | | 10/12/2004 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA1133SO | | Installation of an adjustable trim tab on left aileron. | | Amended | | 1/24/1991 |
| SA1169NW | | Installation of a Lycoming O-360-A4K engine and a Sensenich76EM8S10-0-63 propeller. | | Reissued | | 4/29/1991 |
| SA1186NW | | Installation of a Lycoming O-360-A4K engine a McCauley 1A170FFA/7563 or a Sensenich76EM8S10-0-60 thru -65 propeller and associated systems. | | Amended | | 4/29/1991 |
| SA1195NW | | Installation of Sensenich 76EM8S10-0-60 through -65 propellers on a Lycoming O-360-A4K engine | | Reissued | | 6/14/1991 |
| SA1299NW | | Installation of a McCauley propeller on Lycoming O-320-E2G engine. | | Reissued | | 4/29/1991 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1472SW | | Mitchell automatic flight system AK373 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 7/10/1984 |
| SA1486SW | | Mitchell automatic flight system AK374 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 7/10/1984 |
| SA1498NM | | Repair of the wing rear spar | | Issued | | 4/23/1982 |
| SA1512WE (2 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 0:00 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1600NM | | ONE-ONLY STC S/N AA5A-0342: Installation of Sensenich or McCauley propellers and engine cooling baffles | | Issued | | 4/2/1982 |
| 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 |
| SA1767NM | | Alteration of the oil cooler and air induction system. | | Reissued | | 4/29/1991 |
| SA191NE | | Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. | | Reissued | | 10/4/1984 |
| SA1965CE | | Operation on unleaded and/or leaded automotive gasoline. | | Amended | | 11/27/1985 |
| SA2125NM | | Installation of Lycoming 0-360-A4M engine and Sensenich76EM8S10-0-60 propeller. | | Reissued | | 4/29/1991 |
| SA2141NM | | Installation of Sensenich 76EM8S10-0-63 Propeller Model and a Gulfstream American Spinner Service Kit #143 | | Issued | | 8/23/1983 |
| SA2190NM Page 2 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2268SO | | Installation of an instrument panel overlay and glove box door. | | Issued | | 3/7/1988 |
| SA2275SO | | Installation of a glare shield assembly. | | Issued | | 3/7/1988 |
| 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 |
| SA2593NM | | Installation of Hoskins Model CFS-1000A -1001A FT-100 or FT-101 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA2601NM | | Installation of AVCO Lycoming IO360-A1B6 engine McCauley propeller Model 2D34C215/90DJA-14 Stewart Warner 486 oil cooler Bendix RSA-5Ad1 fuel pump and Wing Tip Landing Light Installation. | | Amended | | 12/3/1987 |
| SA2619NM | | Replace carburetor air induction system with a Beechcraft Airbox (P/M 169-910049-59) on Lycoming O-360-A4K engine with a Sensenich 76EM8S10-0-63 propeller installed per STC SA1195NW with Grumman Spinner Assembly SK142-K | | Issued | | 7/2/1984 |
| SA2620NM | | Modify engine baggles and relocate oil cooler to above and behind the left hand rear cylinder on Lycoming O-360-A4K engine with Sensenich76EM8S10-0-63 propeller. | | Reissued | | 4/29/1991 |
| SA2683NM | | Installation of Precise Flight Inc. stand-by vacuum system (SVS) | | Amended | | 3/10/2005 |
| 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 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA3031SW-D | | Mitchell automatic flight system AK514 consisting of Century I autopilot with omni tracking system. | | Reissued | | 6/21/1984 |
| SA3032SW-D | | Mitchell automatic flight system AK515 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 6/21/1984 |
| 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 |
| SA3301WE | | Installation of Model EGT-1 exhaust gas temperature monitoring system. | | Issued | | 11/23/1976 |
| SA3308NM | | Installation of Lycoming O-360-A4K engine | | Issued | | 2/4/1986 |
| SA3309WE | | Modification of primary control system by addition of rudder- aileron interconnect and installation of Pathfinder autopilot systems and/or pitch trim systems. | | Reissued | | 9/30/1998 |
| SA330NE | | 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 | | 6/18/2002 |
| SA3326NM | | Install Sensenich Propeller model76EM8S10-0 (60-inch to 63-inch pitch inclusive) and Gulfstream Aerospace spinner assembly Kit P/N SK143-2. | | Issued | | 2/7/1986 |
| SA3344NM | | Relocation of oil cooler. | | Issued | | 4/3/1986 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3564SW | | Modification of torque tube assembly. | | Amended | | 12/15/1989 |
| SA3760NM | | Installation of single piece frameless windshield. | | Reissued | | 6/25/2001 |
| SA3841NM | | Installation of a Lycoming O-360-F1A6 engine and a McCauley B2D34C propeller | | Issued | | 6/11/1987 |
| SA4005NM (PG 1) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4005NM (PG 5) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4165NM | | Installation of a Lycoming O-540-E4A5 engine and a Hartzell Model HC-C2YK-8477-8R propeller | | Issued | | 1/25/1988 |
| SA4172NM | | Installation of Aviation Development oil filter. | | Amended | | 5/22/2009 |
| SA4325NM | | Installation of modification to engine cowl nose bowl which splits the nose bowl horizontally allowing it to be removed without prop removal | | Issued | | 5/20/1988 |
| SA4708NM | | Installation of bolts to strengthen the nose gear torque tube assembly. | | Issued | | 2/28/1989 |
| SA4721NM | | Installation of SynCon alarm system. | | Amended | | 5/8/1990 |
| SA4740NM | | Installation of a landing light in the left wing tip or in both wing tips. | | Reissued | | 4/9/2012 |
| SA4849SW | | Install fuel flow transducer in fuel line and install fuel flowmeter/totalizer in aircraft | | Amended | | 10/26/1984 |
| SA4966NM | | Installation of a Lycoming IO-540-D4A5 engine and a Hartzell HC-C2YK-8477-7 propeller. | | Issued | | 9/4/1990 |
| SA4968NM | | Installation of a Lycoming O-320-E2D engine equipped with a Sensenich 4DM6-0-58 propeller reduced to 73-inch diameter using a Lycoming propeller spacer P/N E18776 modified with 5/8 bushings threaded to accept 3/8 bolts. | | Issued | | 8/14/1990 |
| SA5156NM | | Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | | Amended | | 5/22/2012 |
| SA5156NM (PG 3) | | Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | | Amended | | 7/29/2010 0:00 |
| SA5159NM (1 OF 2) | | Installation of chip detector system. | | Amended | | 11/6/1992 |
| SA5372SW-D | | Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-278. | | Reissued | | 10/10/1986 |
| SA5376SW-D | | Installation of S-TEC System 60 pitch stabilization system Model ST-279. | | Issued | | 2/15/1985 |
| SA5386SW-D | | Installation of 40/50 single and two axis automatic flight guidance systems. | | Reissued | | 5/12/1989 |
| SA5387SW-D | | Installation of S-TEC System 60 single axis automatic flight guidance system model ST-277. | | Issued | | 3/25/1985 |
| SA540NE | | Installation of an aft baggage compartment auxiliary 18 gallon fuel tank and transfer system to the right wing tank. | | Issued | | 10/14/1987 |
| SA5452NM | | Installation of a Lycoming IO-360-C1C6 engine and Hartzell HC-C2YK-1BF/F7666A-2 propeller. | | Reissued | | 5/24/2004 |
| SA563CH | | 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 | | 2/10/2009 |
| SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5775NM | | Replacement of rudder tip with Aviation Red Lexan tip with flashing anticollision light located inside. | | Issued | | 10/2/1992 |
| SA5924NM | | Installation of RPM instrument. | | Amended | | 11/24/1997 |
| SA5925NM | | Installation of oil pressure/temperature instrument. | | Amended | | 12/8/1997 |
| SA5926NM | | Installation of manifold pressure instrument. | | Amended | | 8/15/1993 |
| SA5934NM | | Installation of cockpit sunvisor. | | Reissued | | 3/24/2003 |
| SA593CH (1 OF 5) | | Install Champion SlickSTART magneto booster system. | | Reissued | | 2/10/2009 |
| SA6016NM | | Installation of an electronic digital engine tachometer Horizon Model P-1000 P/N P100050-( ). | | Amended | | 1/14/2002 |
| SA6089SW-D | | Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-381. | | Issued | | 10/10/1986 |
| SA615EA (PAGE 1) | | Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. | | Reissued | | 7/6/2010 |
| SA66NW | | Installation of Van s Aircraft model BA-4 fiberglass wheel fairings. | | Amended | | 9/23/1994 |
| SA683NE | | Installation of Lycoming Model O-320-E2G engine that has been converted to high compression IAW STC SE682NE amended 10/27/89. | | Amended | | 11/1/1989 |
| SA693CE | | Replace existing engine induction air filter with AC Spark Plug filter. | | Reissued | | 6/20/2000 |
| SA69NW | | Installation of Matney s engine charge air-air filter assembly. (AA-1B AA-1 AA-1A 1969 AND ON) (AA-5 1972 1973 AND 1974 ONLY) | | Amended | | 10/8/1974 |
| SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
| SA7205SW-D | | Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-456. | | Reissued | | 9/27/1990 |
| SA7211SW-D | | Installation of S-TEC System 60 single axis automatic flight guidance system model ST-277. | | Reissued | | 10/15/1990 |
| SA7212SW-D | | Installation of S-TEC system 60 pitch stabilization system. | | Reissued | | 10/19/1990 |
| SA7213SW-D | | Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-458-40/50. | | Reissued | | 9/28/1990 |
| SA7974SW | | Installation of wheel pant fairings. | | Amended | | 1/10/2006 |
| SA800EA (PAGE 1) | | Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429 A430 A434 A450 A408 (white) A408R/W or A47OR/W (red/white) A500 A625 or A650 and associated power supplies or Model SA strobe light system. | | Amended | | 7/6/2010 |
| SA8031SW | | Installation of Zeftronics alternator controller unit P/N R15100 or R15V00. | | Amended | | 1/6/1994 |
| SA8505SW-D | | Installation of a Century Automatic Flight System Model AK1022 consisting of a Century 2010/2050/2051 autopilot. | | Issued | | 9/20/1995 |
| SA863SO | | Installation of portable hand control | | Reissued | | 7/7/2013 |
| SA867GL | | Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. | | Surrendered | | 3/5/2004 |
| SE683NE | | Installation of Lycoming Model O-320-E2G engine that has been converted to high compression. | | Reissued | | 8/7/1998 |
| ST00811CH | | Installation of Mitchell Aircraft Products gauge cluster. | | Issued | | 1/30/1998 |
| ST01085LA (PAGE 2) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| ST02547AT (2 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |
