| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| SA00478CH (PAGE 3) | | Installation of Cooper Superflite 102 Fabric. | | Amended | | 5/10/2012 |
| 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 |
| SA00985CH | | Replace Lycoming O-235-C2C with O-235-K2C engine or Lycoming O-235-C2C engine modified by Precision Engine STC SE00988CH. | | Issued | | 2/8/1999 |
| 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 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| SA01470AT | | Installation of composite spinner. | | Amended | | 10/13/2000 |
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| 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 |
| SA02795AT | | Installation of a PXE7300SR In-Flight Entertainment System | | Issued | | 2/12/2004 |
| SA02987CH | | Installation of the Electroair Electronic Ignition System | | Amended | | 7/23/2013 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA09382SC | | Installation of extended range fuel tanks. | | Issued | | 10/1/1997 |
| SA1009NW | | Installation of a dorsal fin (P/N 5302040-1) and associated assemblies | | Issued | | 8/21/1980 |
| SA1010CE | | Installation of wing leading edge cuffs. | | Amended | | 8/21/1984 |
| 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 |
| SA1012NW | | Installation of auxiliary fuel tank models 2 TAFTA and 4 TAFTA and incresed gross weight | | Reissued | | 7/17/1984 |
| SA1016NW | | Installation of a Lycoming O-360-A4M engine Sensenich 76EM8-0-62 propeller and AA-5 elevator system | | Issued | | 8/28/1980 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA10NW | | Installation of VA-3 fiberglass wheel fairings. | | Reissued | | 12/30/1992 |
| SA11137SC | | Installation of Plane-Power ALT-FLX alternator | | Reissued | | 5/10/2013 |
| SA11NW | | Installation of VA-2 wheel fairings. | | Reissued | | 12/30/1992 |
| SA1208NW | | Installation of a Lycoming engine with Sensenich propeller | | Issued | | 4/3/1981 |
| SA1209NW | | Relocation of battery from forward face of firewall to aft baggage compartment bulkhead. | | Amended | | 4/29/1991 |
| SA1313CE | | Chrome-plated brake disc installation. | | Amended | | 6/20/1977 |
| SA1410SW | | Mitchell automatic flight system AK301 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 7/10/1984 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| 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 |
| SA191NE | | Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. | | Reissued | | 10/4/1984 |
| SA2096NM | | Installatino of a Lycoming O320-D2H | | Issued | | 5/26/1983 |
| SA2104WE | | Installation of Brittain Models B2C and BSS flight control systems. | | Reissued | | 10/20/1972 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2129NM | | Installation of a Lycoming O-320-E2G engine AA-5A engine mount cowling air induction and a McCauley 1C172/ SBTM/7359 propeller. | | Reissued | | 4/8/1991 |
| SA2138NM | | Installation of a belly mounted Norton Radome a radar unit mounting hole in the belly pressure vessel a drop chute access hole in the pressure vessel near the rear door rerouted primary control cables with associated support brackets and an electronic rack in the aircraft cabin. | | Issued | | 7/22/1988 |
| SA2169NM | | Installation of a Sensenich 72 CK series propeller Gulfstream American spinner (P/N 506006-50) engine oil cooler on a Lycoming O-235-C2C engine. | | Reissued | | 4/29/1991 |
| SA2190NM Page 2 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2267SO | | Installation of an instrument panel overlay and glove box door. | | Issued | | 3/7/1988 |
| SA2274SO | | Installation of a glare shield assembly. | | Issued | | 3/7/1988 |
| SA2477SW | | Installation of Lycoming O-320 or O-290 engine. | | Reissued | | 3/20/1989 |
| 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 |
| 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 |
| 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 |
| SA3234WE | | Installation of Piper oil cooler and associated installation components. | | Issued | | 7/8/1976 |
| 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 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA3565SW | | Modification of torque tube assembly. | | Amended | | 12/15/1989 |
| SA3695WE | | Installation of Lycoming O-235-C2C engine and McCauley1A105/SCM7154 propeller. No installation data required. Placards required with this installation: At the fuel filler caps - 80/87 MIN OCTANE AVGAS (AA-1C UTILITY CATEGORY) | | Issued | | 7/7/1978 |
| 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 |
| SA4106SW | | Increase gross weight to 1560 lbs. for AA-1 1560 lbs. for AA-1A and1600 lbs. for AA-1B. | | Reissued | | 3/20/1989 |
| SA4172NM | | Installation of Aviation Development oil filter. | | Amended | | 5/22/2009 |
| SA4387NM | | Installation of Lycoming 0-320-A C or E series engine and a Sensenich 74DM6-0-58/64 or 74DM7-0-58/64 propeller. | | Amended | | 6/13/1991 |
| SA4708NM | | Installation of bolts to strengthen the nose gear torque tube assembly. | | Issued | | 2/28/1989 |
| SA4722NM | | Installation of a hat shelf in the aft baggage compartment. | | Issued | | 4/17/1989 |
| 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 |
| SA4917NM | | Modification of upper engine cowl. | | Issued | | 4/16/1990 |
| SA4994NM | | Installation of split nose bowl. | | Issued | | 12/5/1990 |
| 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 |
| SA5197NM | | Installation of split cowl nose bowl. | | Issued | | 11/4/1991 |
| 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 |
| SA5987SW | | Installation of main landing gear fairing clean-up kit. | | Issued | | 7/30/1985 |
| 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 |
| 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 |
| SA761NE | | Modifications to lower engine cowling with landing gear boot adapter and change to upper engine cowling with a split nose bowl configuration. | | Issued | | 6/18/1990 |
| SA762NE | | ONE ONLY- Installation of pilot and copilot control column stick type grip. S/N AA1C0071 | | Amended | | 7/18/1990 |
| SA7952SW | | Installation of conventional landing gear. | | Reissued | | 1/14/1993 |
| 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 |
| SA809NW | | Installation of fixed (flush) cowl flap nose gear strut fairing and retainer. | | Issued | | 7/20/1979 |
| SA810NW | | Installation of main landing gear fairings from the AA-5 series aircraft incorporating sheet metal covers over rubber in place of stock rubber parts. | | Amended | | 1/23/1981 |
| SA8431SW | | Installation of R15VON alternator control unit. | | Amended | | 1/6/1994 |
| SA868GL | | Superseded by STC SA01944CH. Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index. | | Surrendered | | 3/5/2004 |
| SA991NW | | Installation of model AA-5A engine mount cowling and carburetor air box | | Issued | | 7/17/1980 |
| ST00811CH | | Installation of Mitchell Aircraft Products gauge cluster. | | Issued | | 1/30/1998 |
| ST02547AT (2 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |
| ST10405SC | | Installation of a composite propeller spinner Part Number TCB506006-502 in accordance with Drawing Number 2501 Spinner Composite- AA-1 AA-1A AA-1B & AA-1C | | Issued | | 4/27/2005 |
