| 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 |
| 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 |
| SA00080LA | | Installation of Teledyne Continental TSIO-520-NB engine and Hartzell three bladed propellers. | | Reissued | | 11/10/2009 |
| SA00161BO (1 OF 3) | | Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. | | Amended | | 2/8/2005 |
| 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 |
| SA00199AT | | Installation of carbon steel brake discs that have melonite surface treatment P/N AA-25A. | | Reissued | | 11/14/1994 |
| 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 (1OF 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 |
| SA00272WI | | Replacement of hydraulic system pressure switch. | | Reissued | | 11/8/2007 |
| 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 |
| SA00402SE | | Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) | | Amended | | 1/23/2007 |
| SA00409AT | | Installation of Cessna 02A entry door (P/N 1517080-1) and wind deflector. | | Issued | | 1/21/1994 |
| SA00410AT | | Design fabrication and installation of upper and lower windshield retaining gussets. | | Issued | | 1/21/1994 |
| SA00419NY | | Installation of cockpit utility light. | | Reissued | | 12/31/2002 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| SA00556AT | | Installation of Appalachian Accessories carbon steel brake discs P/N AA-27A. | | Reissued | | 1/24/1995 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| SA00680SE (4 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
| SA00729SE | | Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760 Revision - dated 7/20/99 or later FAA approved revision. | | Amended | | 11/30/2005 |
| SA00780SE (PAGE 2) | | 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 |
| SA00812CH | | Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. | | Reissued | | 6/30/2006 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00897WI | | Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. | | Issued | | 8/11/2000 |
| SA00944CH | | Replace Janitrol/JanAero Combustion Heater Model 81D94-X (XX) with C&D Associates Combustion Heater Model CD45K either P/N RA-81D94-3 or P/N CD81D94-3. (95-B55 S/N TC-1658 and up E55 S/N TE-959 TE-968 and up 58 S/N TH-437 and up) | | Amended | | 6/20/2000 |
| SA00972LA | | Installation of Teledyne Continental Motor Pressurized Magnetos Kit No. EQ6565. T337G s/n P3370001-P3370292 except P3370109 & P3370196 P337H S/N 3370293-3370356 & P3370196 | | Reissued | | 11/10/2009 |
| SA01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 0:00 |
| SA01090AT | | Manufacture of flap gap seals. | | Issued | | 7/24/1996 |
| SA01091AT | | Manufacture of mechanical cowl flap control system. | | Amended | | 2/20/2001 |
| SA01093AT | | Manufacture of short takeoff and landing (STOL) kit and tail boom to vertical fin fairings. | | Amended | | 5/13/1997 |
| SA01094AT | | Manufacture of modified Lightning Wingtips. | | Issued | | 7/24/1996 |
| SA01105WI-D (1 OF 2) | | Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). | | Amended | | 5/31/2007 |
| SA01114CH | | Installation of P2 Incorporated 6600 Audio Advisory system | | Reissued | | 11/4/2013 |
| SA01118WI | | Installation of the Concorde FLA or VRSLA RG series batteries in the Cessna Single Engine Airplanes listed on the attached FAA Approved Model List (AML) No. SA01118WI dated October 17 2001 | | Amended | | 11/30/2013 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| SA01158WI (1 OF 2) | | Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. | | Amended | | 3/29/2005 |
| SA01179AT | | Installation of an external cargo Pod. | | Amended | | 4/2/2001 |
| SA01205WI-D (1 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 |
| SA01215SE | | Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer and on both vertical stabilizers. | | Issued | | 5/13/2003 |
| SA01229SE Page 1 | | Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. | | Amended | | 6/27/2007 |
| SA01240SE (2 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 |
| SA01330LA (PAGE 1) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 |
| SA01344AT | | Installation of a baggage door on the aft right side of the fuselage. | | Issued | | 4/15/1997 |
| SA01473SE (2 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 1) | | 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 (2 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 4) | | 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 |
| SA01834CH (1 OF 2) | | Installation of the High Intensity Discharge Light Assembly Kit. | | Amended | | 3/20/2009 |
| SA01860NY (3 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 |
| SA01888AT | | Installation of a composite structure baggage door in RH side of the fuselage. | | Issued | | 4/27/1999 |
| SA01933LA-D Page 1 | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation
);INSERT INTO stc_table VALUES ( System | | Amended | | 4/1/2013 |
| SA01933LA (1 OF 5) | | Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System | | Amended | | 11/6/2006 |
| SA01985AT | | Installation of a fuel jettison system. | | Issued | | 11/5/1999 |
| SA01988SE (PAGE 3) | | 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 |
| SA02017AT | | Installation of a Wescam FLIR System NSI Microwave System and an Operator s Console. | | Issued | | 10/29/1999 |
| SA02019SE-D | | Installation of Garmin GTN 6XX/7XX Navigation System | | Amended | | 12/13/2013 |
| SA02023AT | | Installation of a fuel transfer system to transfer fuel from a wing tip extension fuel tank to the main wing fuel tank. | | Issued | | 11/7/1999 |
| SA02033AT (PAGE 2) | | 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 |
| SA02055AT | | Installation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions Revision D dated January 13 2000 or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII Revision C dated August 17 1999 or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs. | | Amended | | 7/3/2003 |
| SA02056AT | | Installation of wing tip extensions in accordance with Aviation Enterprises (AE) Installation Instructions Revision D dated January 13 2000 or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII Revision C dated August 17 or later FAA approved revisions. Increase in the Maximum Takeoff Gross Weight from 4700 lbs to 5120 lbs. | | Issued | | 1/14/2000 |
| SA02094SE | | Installation of a CO Guardian 452R Carbon Monoxide Detector per AeroMech Inc. Master Data List document AM0243-DL02-00 Revision A | | Issued | | 1/31/2011 |
| SA02095AK | | Installation of hourmeter airspeed switch. | | Issued | | 12/10/1997 |
| SA02110CH (PAGE 2) | | Installation of a Time Trac Data Recorder | | Reissued | | 1/11/2010 |
| SA02119SE Page 1 | | Installation of Garmin GDL 88 ADS-B UAT Transceiver System | | Issued | | 12/28/2012 |
| SA02153LA-D (Page 1) | | 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 |
| SA02203AK (PAGE 2) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| SA02217AK (3 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 0:00 |
| SA02265SE | | Installation of a camera housing | | Amended | | 11/1/2013 |
| SA02268CH (PAGE 2) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02268CH (PAGE 3) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02293AK (2 OF 3) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Reissued | | 1/11/2010 |
| SA02307AT | | Installation of wing tip extensions in accordance with Aviation Enterprises (AE) Installation Instructions Revision D dated January 13 2000 or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII Revision C dated August 17 or later FAA approved revisions. | | Amended | | 12/28/2004 |
| SA02308AT | | Installation of wing tip extension fuel tanks in accordance with Aviation Enterprises (AE) Installation Instructions Revision D dated January 13 2000 or later FAA approved revisions. Installation of wing aerodynamic fences in accordance with AE Drawing No. SKM-FTII Revision C dated August 17 1999 or later FAA approved revisions. | | Amended | | 12/28/2004 |
| SA02446CH | | Installation of the Courtesy Light Kit. | | Issued | | 6/25/2007 |
| SA02460AT | | Replace propellers with MT-Propeller Company model MTV-12 propellers per Coastal Planes installation manual. No intermixing of propellers is allowed. | | Amended | | 5/16/2006 |
| SA02510AT | | Installation of a rear firewall engine accessory access door. | | Issued | | 5/14/2002 |
| SA02520AT | | Installation of M-20 Oil Separator model 600-WP. | | Issued | | 5/30/2002 |
| SA02527AT | | Installation of a landing gear in-transit warning light in 337 models that are equipped with an electric motor to retract landing gear instead of engine driven hydraulic pump. | | Issued | | 5/31/2002 |
| SA02547AT (PG 2) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 0:00 |
| SA02686AT | | Installation of air intake louvers on the rear engine lower cowl in accordance with Aviation Enterprises Installation Instructions dated June 15 2003 or later FAA approved revision. | | Issued | | 7/21/2003 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02738CH (PAGE 5) | | 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 |
| SA03100AT | | Installation of Wing Auxiliary Fuel Tanks. | | Issued | | 6/15/2005 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA03618AT | | Installation of Teledyne Continental Motors Model IO-550-N engines Hartzell Model PHC-G3YF-2UF/F7663D-2R propeller front Hartzell Model PHC-I3YF-2AL/FLC7663DF-2 propeller rear front and back AirScan engine installations and 5120 pounds Maximum Gross Weight | | Amended | | 2/13/2009 |
| SA09120AC-D | | Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-603 with optional autotrim system. | | Amended | | 4/19/2001 |
| SA09419AC-D | | Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems Model ST-869-20/30. | | Issued | | 10/25/1999 |
| SA1021SW | | Flap on switch on control wheel. | | Reissued | | 9/20/1977 |
| SA10236SC (2 OF 4) | | Installation of a GDC 31 Roll Steering Converter | | Amended | | 3/22/2011 |
| SA1056SW | | Revise wing contours leading edge and redesign landing light deflector plates. | | Reissued | | 4/27/1984 |
| SA1205CE | | Installation of King KFC-200 2-axis(3 optional) flight control system with a King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller. | | Reissued | | 2/28/2000 |
| SA1258CE | | Installation of FIQUENCH fire extinguishing system in cabin and/or fire extinghishant system in engine compartments. | | Reissued | | 12/15/1977 |
| SA1261WE | | Installation of control position indicator (CPI) system. | | Reissued | | 2/18/1972 |
| SA1273GL | | Install SAF-T-STOP auxiliary seat stop device. | | Reissued | | 6/15/2012 |
| SA1356CE | | Chrome-plated brake disc installation. | | Issued | | 1/16/1978 |
| SA1359SW | | Mitchell automatic flight system FD/AP282-345 consisting of flight director/autopilot with optional automatic pitch trim. | | Reissued | | 7/10/1984 |
| SA1418SO | | Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) | | Reissued | | 6/12/1984 |
| SA1455NM | | Installation of a flame proof auxiliary heater-dryer Model12-1600. | | Amended | | 12/11/1985 |
| SA1473CE | | Installation of Tull microwave landing system with modified King KX175B and KN 73 receivers. | | Issued | | 2/12/1979 |
| SA1478SW | | Mitchell automatic flight system AK345 consisting of Century III autopilot with optional automatic pitch trim radio coupler and glide slope coupler. | | Reissued | | 7/10/1984 |
| SA1494SW | | Installation of Mitchell flight director remote annunciator Model AK375. | | Amended | | 7/10/1984 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA1520SW | | Mitchell automatic flight system AK400 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 7/13/1984 |
| SA1546GL | | Installation of on-board engine analyzer system. | | Issued | | 1/4/1991 |
| SA1558SW | | Installation of vortex generators wing leading edge cuffs wing tips fairings de-icing boots and stall strips. | | Amended | | 1/28/1982 |
| SA1568SO | | Installation of Sorensen external fuselage insecticide spray tank and associated spray equipment. | | Issued | | 1/18/1984 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1626NM Page 1 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA1627WE | | Installation of drooped ailerons in flaps down mode recontoured wing leading edge stall fences aileron centering springs conical cambered wing tips and flap actuated elevator trim spring. | | Reissued | | 9/8/2005 |
| SA1675WE | | Installation of exhaust gas temperature monitoring systems EGT-2. | | Amended | | 8/28/1974 |
| SA1762NM | | Installation of a pressurized magneto system on the Continental turbocharged TSIO-360-C F and FB engines. | | Reissued | | 3/14/2006 |
| SA1801CE | | Installation of fire extinguishing system in cabin and/or fire extinguishant system in engine compartments. | | Amended | | 5/30/1995 |
| SA1823NM | | Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4 1983 together with their FAA sealed Installation Instructions dated September 20 1982 or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6 1982 LAS 1013 dated October 5 1982 and LAS 1014 dated October 6 1982 or later FAA approved sealed revisions. | | Reissued | | 1/23/2004 |
| SA1877NM | | Installation of Hoskins Model CFS-2000A -2001A FT-200 fuel flow indicating system. | | Reissued | | 1/30/1998 |
| SA190SO | | Cabin door removed and wind deflector installed. | | Issued | | 1/1/1961 |
| SA1922SW | | Installation of Mitchell automatic flight system AK404 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 8/1/1984 |
| SA2067NM | | Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System | | Amended | | 7/11/2012 |
| SA20GL | | Installation of Woodward Type II electronic propeller synchronizer or synchrophaser system. (G-44A MODIFIED COLEMILL - STC 2-13) (500-A modified - Colemill STC SA340SO) | | Reissued | | 4/30/2007 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2190NM Page 1 | | Installation of electronics International Digital Volt/Amp Gauges and Accessories. | | Issued | | 2/16/1984 |
| SA2200WE | | Installation of Brittain Industries Model B2C and BSS Flight Control Systems | | Reissued | | 7/2/2013 |
| SA2242SO | | Installation of external fuselage insecticide spray tank and associated dispersal equipment. | | Reissued | | 2/18/1996 |
| SA2335WE | | Installation of one-piece windshield and relocation of compass. | | Reissued | | 8/16/2011 |
| SA2350NM Page 1 | | Installation of Electronics International Inc digital carburetor/outside air temperature gauges | | Amended | | 6/6/1990 |
| SA2364CE | | Replacement of right front seat with stretcher. | | Issued | | 3/18/1988 |
| SA2492SO | | Installation of Appalachian Accessories stainless steel brake discs P/N 75-25A. | | Reissued | | 9/29/1995 |
| SA250CE | | Installation of Woodward electronic propeller synchraphaser system. | | Reissued | | 4/30/2007 |
| 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 2) | | 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 |
| SA2821CE | | Installation of wing tips. | | Issued | | 4/17/1992 |
| SA2832SO | | Installation of a combination radio/throttle/gust lock. | | Amended | | 12/3/2001 |
| SA2844CE (1 OF 2) | | Installation of a plastic cap enclosure over the anti-collision strobe light system. | | Issued | | 7/29/1992 |
| SA2858SO | | Installation of a FLIR airborne surveilance system. | | Reissued | | 5/5/2010 |
| SA3056WE | | Installation of fuel flow instruments. | | Issued | | 8/15/1975 |
| SA3148SW-D | | Mitchell automatic flight system AK537 consisting of Century III autopilot with optional radio coupler and glide slope coupler. | | Reissued | | 6/6/1984 |
| SA3149SW-D | | Mitchell automatic flight system AK536 consisting of Century IV autopilot or Model AK536FD consisting of a Century IV flight director autopilot with optional remote annunciator. | | Reissued | | 6/6/1984 |
| SA3240SO | | Removal of main landing gear wheel doors and actuators which are replaced with a fixed composite panel containing a cutout for gear passages. | | Amended | | 12/8/1993 |
| SA3250SW-D | | Mitchell automatic flight system AK404 consisting of Century IIB autopilot with optional radio coupler. | | Amended | | 8/12/1993 |
| SA3252SW-D | | Mitchell automatic flight system AK400 consisting of Century IIB autopilot with optional radio coupler. | | Reissued | | 3/28/1984 |
| SA3258NM | | Installation of ARNAV systems FC-10/FT-10 digital fuel flow indicating system. | | Issued | | 6/6/1986 |
| SA32RM | | Installation of electrically driven freon air-conditioning system. | | Reissued | | 5/17/2013 |
| SA3729NM | | Installation of electric heater and auxiliary alternator. | | Issued | | 6/25/1987 |
| SA3818WE | | Installation of Fueltron IIIG or IIIP digital fuel flow and totalizer system. | | Reissued | | 4/29/1991 |
| SA385GL | | Installation of Norton radome kit No. 4231X. | | Reissued | | 4/17/1981 |
| SA3862NM Page 1 | | Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. | | Amended | | 4/25/1988 |
| SA3863NM | | Installation of American intercooled engines as modified by STC SE3864NM. | | Amended | | 11/1/1998 |
| SA4005NM (PG 2) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4024NM | | Replace the standard Cessna oil drain plug with a Bogert Aviation quick drain. | | Amended | | 4/12/1989 |
| SA406CE | | Installation of Hoskins Supplemental Position Light System which includes Model (A) Wing Tip Lights Model 2 Fuselage Light used as a Tail Light or the Model L Tail Light. | | Reissued | | 9/30/2011 |
| SA4166NM | | Installation of Fairchild voltage regulator No. UA78 GUIC to replace the original voltage regulator in Cessna turn coordinator P/N 0661003-0506. | | Issued | | 1/25/1988 |
| SA4302NM (PAGE 2) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 |
| SA4504NM | | Installation of an Intercooler in the air induction system of both engines. (T337G S/N P3370001 - P3370292 EXCEPT P3370109 AND P3370196) (P337H S/N P3370293 - P3370356 AND P3370196) | | Reissued | | 11/10/2009 |
| SA4526NM | | Limited to installation on serial number P3370109 ONLY. Installation of intercoolers in air induction system of both engines. | | Issued | | 1/27/1989 |
| SA478NW | | Installation of Bendix RDR 160 weather radar system. | | Amended | | 9/25/1979 |
| SA482SO | | Installation of Bendix FCS-810 automatic flight control system including manual electric trim and flight director indicator. | | Amended | | 7/2/1976 |
| SA491SW | | Automatic pilot AK135 automatic pitch trim AK156 and lateral guidance radio coupler AK123. | | Issued | | 1/1/1960 |
| SA4961NM | | Installation of a NSA sunvisor system for the pilot and copilot. | | Reissued | | 3/24/2003 |
| SA5017NM | | Installation of an inflatable door seal. | | Reissued | | 11/10/2009 |
| SA5033NM | | Installation of Teledyne Continental Motor pressurized magnetos kit no. EQ6565. (T337G S/N P3370001-P3370292 except P3370109 and P3370196) (P337H S/N P3370293-P3370356 and P3370196) | | Reissued | | 11/10/2009 |
| SA5090NM | | Installation of a nineteen and a half(19.5 U.S.) gallons wing tip fuel tank on each wing tip. | | Reissued | | 2/25/2000 |
| SA5114NM | | Installation of spoiler system. | | Reissued | | 7/9/2013 |
| SA5156NM | | Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System | | Amended | | 5/22/2012 |
| SA5159NM (1 OF 2) | | Installation of chip detector system. | | Amended | | 11/6/1992 |
| SA5176NM | | Installation of an ADC Corporation Model 5001A engine pre-oiler system | | Issued | | 8/10/1991 |
| SA5495NM | | Installation of an engine driven air conditioning system. | | Reissued | | 11/10/2009 |
| SA5581SW | | Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. | | Amended | | 9/30/2002 |
| SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA589WE | | Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. | | Reissued | | 10/5/1976 |
| 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 |
| SA593CH (2 OF 5) | | Install Champion SlickSTART magneto booster system. | | Reissued | | 2/10/2009 0:00 |
| SA615EA (PAGE 2) | | 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 |
| SA638GL | | Installation of a Shadin Co. 910516 fuel flow indicating system. | | Reissued | | 6/8/2006 |
| SA660WE | | Installation of HRD-type fire extinguishing system. (AND STC SA111WE) | | Reissued | | 2/4/1987 |
| SA668SW | | Installation of Mitchell automatic flight system Model AK210 consisting of Century III autopilot automatic pitch trim automatic aileron stabilizer and radio coupler. | | Reissued | | 6/25/1984 |
| SA672CE | | Install auxiliary fuel tank in rear baggage area. | | Reissued | | 6/23/2006 |
| SA678CE | | Install fuselage top emergency exit door. | | Reissued | | 6/23/2006 |
| SA704NW | | Installation of a Hoskins CFS 2000 computerized fuel system | | Issued | | 1/15/1979 |
| SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
| SA7203SW-D | | Installation of S-TEC System 65 Two axis Automatic Flight Guidance System Model ST-313. | | Reissued | | 2/27/1990 |
| SA7208SW-D | | Installation of S-TEC system 65 two axis automatic flight guidance system Model ST-313. | | Issued | | 2/27/1990 |
| SA7209SW-D | | Installation of S-TEC System 60 Two Axis Automatic /Flight Guidance System with Optional Autotrim System Model ST-314. | | Issued | | 4/6/1990 |
| SA7774SW-D | | Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems model ST-317-40/50. | | Issued | | 6/15/1990 |
| SA7808SW-D | | Installation of S-TEC System 60 pitch stabilization system model ST-478 with optional automatic electric trim system. | | Issued | | 1/1/1960 |
| SA798EA | | Installation of Monitair exhaust gas combustion monitor kit. | | Reissued | | 2/14/1972 |
| SA8008SW | | Installation of Zeftronics alternator control units P/N s R25101 (27.7V systems) or R25102 (28.8V systems). | | Reissued | | 5/12/1998 |
| SA801SW | | Mitchell automatic flight system AK244 Century II autopilot with optional radio coupler. | | Reissued | | 6/29/1984 |
| SA808SW | | Installation of Mitchell Model AK246 omni-tracker. Applicable only to aircraft modified by STC SA615SW. | | Reissued | | 6/29/1984 |
| SA8367SW-D | | Installation of System 65 two axis automatic flight guidance system Model ST-506. | | Issued | | 3/25/1993 |
| SA8368SW-D | | Installation of System 65 two axis automatic flight guidance system Model ST-506. | | Issued | | 3/25/1993 |
| SA8371SW-D | | Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-510. | | Issued | | 8/17/1993 |
| SA8372SW-D | | Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-510. | | Issued | | 8/17/1993 |
| SA842SW | | Mitchell automatic flight system AK252 consisting of Century III autopilot with optional automatic pitch trim automatic aileron stabilizer and radio coupler. | | Reissued | | 6/29/1984 |
| SA8533SW-D | | Installation of a Century Automatic Flight System. | | Amended | | 8/8/2003 |
| SA8922SW | | Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) | | Issued | | 7/21/1994 |
| SA917EA | | Installation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail P/N 30-0555-( ). | | Reissued | | 6/4/2007 |
| SA937CE | | Installation of leading edge cuffs stall fences droop wing tips and vortex generators on rear engine lower cowling. | | Amended | | 10/4/1990 |
| ST01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 |
| ST01494LA (PG 1) | | Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. | | Reissued | | 8/30/2011 |
| ST01548LA | | Installation of external landing gear position verification mirrors and aft engine cowl observation mirrors. | | Reissued | | 8/16/2004 |
| ST02307CH | | Installation of Rudder Pedal Extensions. | | Amended | | 10/13/2006 |
| ST02547AT (1 OF 2) | | Installation of a voice alert system. | | Amended | | 5/13/2003 |
