| 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 |
| SA00025WI | | Installation of exhaust extension. | | Issued | | 2/8/1993 |
| SA00028WI | | Installation of flap and aileron gap seals. | | Issued | | 2/11/1993 |
| SA00054WI | | Installation of McCauley D3A32C411/82NDA-2 propeller. | | Reissued | | 9/22/2005 |
| SA00057LA | | Installation of a heat shield. | | Issued | | 3/15/1995 |
| SA00059LA | | Installation of observers windows per Aircraft Technical Service Inc. Master Drawing List Observers Window Instl. Cessna 182 Drawing No. 2769 Rev C dtd 2/7/95 or later FAA approved revision. | | Amended | | 8/17/2001 |
| 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 |
| SA00081NY | | Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | | Amended | | 5/15/2002 |
| SA00087DE | | Installation of Air Guard remote mounted oil filtration system. | | Issued | | 3/22/1994 |
| SA00087WI | | Installation of replacement stabilizer and elevator tips. | | Amended | | 8/25/1993 |
| SA00103BO | | Installation of Weemax cabin air vent. | | Issued | | 6/16/1999 |
| SA00116WI | | Installation of 18-gallon nylon auxiliary fuel tanks on planes equipped with standard range 64 gallon capacity bladder tank or 62 gallon fiberglass fuel tanks. (182Q thru S/N 18266590 R182 S/N R18200002 thru R18200583) | | Reissued | | 5/3/2004 |
| SA00137BO | | Installation of Cessna exhaust system P/N 0750238-21 cabin heat shround P/N 0750161-82 and carburetor head shroud assembly p/n 0752657-1. Installation of STC SA09530SC required in conjunction with this STC. Approved ONLY for Cessna 182E serial number 18254171. | | Amended | | 4/27/2005 |
| SA00147AT | | Installation of Type A sun visor. | | Amended | | 7/28/1993 |
| SA00152WI | | 1) Installation of Continental I0-520-D engine and Hartzell PHC-L3YF-1RF/F7691 propeller in accordance with Drawing List No. 1821 dated April 15 1994 or later FAA Approved revisions. OR
);INSERT INTO stc_table VALUES ( 2) Installation of Continental I0-550-D engine and Hartzell PHC-L3YF-1RF/F7691 or PHC-G3YF-1RF/F8468A()-6R propeller in accordance with Drawing List No. 1821 Revision 2 dated May 31 1996 or later FAA Approved revisions.
);INSERT INTO stc_table VALUES ( ** See continuation sheet for required flight manual supplement.** | | Amended | | 4/1/2011 |
| SA00161BO (1 OF 3) | | Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display. | | Amended | | 2/8/2005 |
| SA00162SE | | Installation of telemetry antennas. | | Reissued | | 5/28/1997 |
| 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 |
| SA00165SE | | Installation of 76 vortex generators and 2 small delta wings on the upper surface of the wings. | | Amended | | 5/18/2001 |
| SA00186AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| SA00188AT | | Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-26A. | | Reissued | | 11/14/1994 |
| SA00194AT | | Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-40. | | Reissued | | 11/14/1994 |
| SA00210AT | | Installation of carbon steel brake discs that have melonite surface treatment P/N AA-90. | | Reissued | | 11/14/1994 |
| SA00211AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/17/1994 |
| SA00212AT | | Installation of carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/17/1994 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| SA00236SE | | Installation of an extended baggage compartment | | Amended | | 9/10/2001 |
| SA00238SE | | Installation of Aviation Development Corporation s sump mounted chip detector | | Issued | | 10/31/1995 |
| SA00243BO (2 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 |
| SA00245BO | | ONE-ONLY STC: Installation of modified right hand cabin door floor mounted seat belts (4 places) and aft cabin bulkhead for 182N serial number 18260732. | | Issued | | 10/13/2006 |
| SA00258BO | | Installation of Avidyne Corporation Part Number 700-00159-( ) MultiLink Broadcast Receiver with either Micro-Ant P/N A420-ANTS-TD or Sensor Systems P/N S67-1575-650 antenna. | | Amended | | 1/30/2008 |
| 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 |
| SA00270WI | | Installation of fiberglass replacement wing tips. | | Amended | | 6/23/2000 |
| SA00272WI | | Replacement of hydraulic system pressure switch. | | Reissued | | 11/8/2007 |
| SA00276NY | | Reinforcement of wing assemblies and installation of Air Research Technology wing tip extension. | | Amended | | 1/15/1999 |
| 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 (PAGE 1 ) | | 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 |
| SA00294DE | | Installation of an external infrared imaging system. | | Amended | | 2/17/2009 |
| SA00323BO | | Installation of Avidyne Corporation Autopilot | | Issued | | 10/1/2012 |
| SA00336NY | | Installation of second wind auxiliary vacuum system. | | Reissued | | 6/18/2002 |
| SA00353DE | | Installation of a large vertical left hand side window and an optional Del-Air passenger observation rear seat assembly. | | Issued | | 9/18/1998 |
| 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 |
| SA00406WI | | Installation of replacement flap trailing edge bulbs. (R172K XP) | | Amended | | 9/9/1999 |
| SA00419NY | | Installation of cockpit utility light. | | Reissued | | 12/31/2002 |
| SA00424SE | | Installation of Precise Flight Model 100(electric) Speedbrake System. | | Amended | | 11/7/2003 |
| SA00425DE | | Installation of model FB-02 Fixed Arm Pilot Arm Rest on R/H side of pilot seat and optional GPS Support Arm System. | | Amended | | 6/12/2001 |
| SA00426DE | | Installation of Model FB-01 Swing Arm Pilot Arm Rest System on R/H side of pilot seat. | | Amended | | 6/12/2001 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| SA00465NY | | Installation of Meterological Measurement System Model A1MMS-10 with optional installation of Telemetry Module Model AIRDAT-9600. | | Amended | | 10/28/1998 |
| SA00478SE | | Replace existing horizontal stabilizer skins | | Issued | | 11/6/1997 |
| SA00492DE | | Installation of a horizontal left-hand side aerial survey window per Del-Air Master Drawing List Document DEL-04-002 latest FAA approved revision. | | Issued | | 3/17/2003 |
| SA00496SE | | Installation of Oregon Aircraft Design Engine Mount Heat Shields. | | Amended | | 12/20/2000 |
| SA00508WI | | Energy absorbing seat. | | Issued | | 5/5/1997 |
| SA00512SE | | Fabrication of a vortex generator system. | | Amended | | 5/14/1998 |
| SA00541DE | | Installation of a Wescam Gimbled Camera System with Master Data List for Cessna 182 Wing Mounted Camera. | | Issued | | 3/30/2004 |
| SA00542DE | | Installation of a Wescam Skypod Microwave Antenna System with Master Data List for Cessna 182 Skypod Microwave Antenna. | | Issued | | 3/30/2004 |
| SA00562NY | | Installation of Teledyne Continental IO-470 engine modified to incorporate a carburetor system. | | Issued | | 2/10/1997 |
| SA00622DE | | Installation of John Deere AGRI Services Inc. JD3 Aerial Imaging System | | Reissued | | 11/15/2007 |
| SA00642SE | | Installation of a Ski Tube compartment extending aft of the baggage compartment. (182B S/N 53598 185 185A 185B 185C and 185E S/N 1149 182D S/N 53598 180G S/N 51774 182C S/N 53598 A185E S/N 1149 180 180A 180B 180C 180D 180E 180F and 180H S/ N 51774 182 and 182A S/N 53598) | | Amended | | 11/24/1998 |
| SA00648SE | | Fabrication of R.M.D. Aircraft Lighting Inc. wing-tip and landing light Kit No. 00190-C. | | Issued | | 11/30/1998 |
| SA00671NY | | Installation of AIRDAT Telemetry module. | | Amended | | 10/28/1998 |
| SA00678SE | | Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments | | Issued | | 3/5/1999 |
| SA00679SE | | Installation of interior fiberglass trim panels. | | Amended | | 5/2/2011 |
| SA00680SE (3 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
| SA00709CH | | Installation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2 no rev both dtd 8/30/96 or later FAA app rev. | | Issued | | 7/9/1997 |
| SA00709LA | | Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required. | | Reissued | | 5/14/2002 |
| SA00709SE | | Installation of replacement control surface skin panels. | | Issued | | 6/28/1999 |
| SA00727WI | | Installation of D3A3C401/90DFA -2 -4 -6 -8 & -10 propellers on Cessna Aircraft Models 182 128A though 182R and associated changes. | | Reissued | | 9/22/2005 |
| SA00740SE | | Installation of Dynamic Propellers support brackets. | | Amended | | 5/18/2001 |
| SA00744DE | | Installation of Automatic Dependent Surveillance | | Amended | | 3/28/2013 |
| SA00749AT | | Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) | | Amended | | 12/10/1997 |
| SA00753WI | | nstallation of the Concorde VRSLA (RG-24-15 RG-24-16 RG-35AXC and RG-35A) batteries | | Reissued | | 1/14/2013 |
| SA00760SE | | Installation of glare shield. | | Reissued | | 5/20/2010 |
| SA00780NY | | The installation removal and maintenance of Acorn Welding | | Amended | | 5/3/2013 |
| 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 |
| SA00796SE | | Installation of vortex generators on the wings and tail surfaces of the above model aircraft | | Amended | | 5/27/2004 |
| SA00797CH | | Installation of McCauley Propeller Model B3D36C431/80VSA-1 or B3D36C433/80VSA-1 and spinner assembly. | | Reissued | | 9/21/2005 |
| SA00810AT | | Installation of a Teledyne Continental Motors IO-550-D engine and a Hartzell 3 blade model PHC-G3YF-1RF/F7691/() propeller. | | Issued | | 7/18/1995 |
| SA00812CH | | Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. | | Reissued | | 6/30/2006 |
| SA00812NY | | Installation of Technisonic Industries Limited TFM-138 A and B (does not include TFM-138 s/n 1540 and up TFM-138B s/n 1500 and up). | | Amended | | 9/12/2005 |
| SA00819CH | | Installation of McvCauley Propeller Model D3A36C435/80VEA-0 and spinner assembly. | | Reissued | | 9/23/2005 |
| SA00819SE | | Installation of Visual Instruments flap position indicating system. | | Issued | | 7/18/2000 |
| SA00819WI-D | | Installation of the Bendix/King KMD 150 MFD and optional L-3 WX 500 Stormscope. | | Amended | | 10/15/2004 |
| SA00834SE | | Installation of vortex generators on wings and tail surfaces. | | Issued | | 8/11/2000 |
| SA00843NY | | Aircraft fuel quantity transmitter replacement-from Stewart Warner Model 390 to Stewart Warner Model 385. | | Issued | | 5/28/1998 |
| SA00854AT | | Installation of Hartzell PHC-G3YF-1RF/F7691() or PHC-G3YF-1RF/ F8468A()-6R propellers to TCM O-470-L R S and U engines. | | Reissued | | 2/3/1999 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00861WI | | Installation of Lycoming IO-540-K1A5 engine and Hartzell HC-C3YR-1RF/8468-6R propeller. | | Amended | | 3/20/2003 |
| SA00864SE | | Installation of fiberglass nosebowl. | | Reissued | | 5/20/2010 |
| SA00871SE | | Cockpit sunvisor installation. | | Amended | | 5/11/2010 |
| SA00897CH | | Installation of Domed (Bubble) Window | | Amended | | 12/4/2013 |
| SA00900NY | | Installation of a Ryan Intl Corp TCAD model 9900B traffic and conflict alert device interfacing with an Eventide Avionics ARGUS 5000 series or ARGUS 7000 series moving map display. | | Issued | | 10/29/1998 |
| SA00905WI-D | | Installation of Bendix/King KMA 28 Audio Amplifier/Intercom/Marker beacon receiver. | | Issued | | 11/29/2000 |
| SA00910WI-D | | Installation of Bendix/King KLN 94 GPS (Global Positioning System) Navigation Receiver for IFR enroute and non-precision approach operations. | | Issued | | 11/1/2000 |
| SA00921NY | | Installation of a digital encryption device and global wolfsburg RT-9600 VHF/FM communications transceiver. | | Reissued | | 5/27/2003 |
| SA00927WI | | Installation of MT-Propeller Model MTV-9-D/195-18b hydraulic 3-blade constant speed propeller. | | Reissued | | 3/20/2007 |
| 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 |
| SA00963NY | | Installation of an Icarus Integral relay unit IRU-525. | | Issued | | 5/11/1999 |
| SA00980LA | | Installation of Accessory Power Receptable. | | Issued | | 7/11/2000 |
| SA01001SE | | Installation of 12 volt cabin power system for portable electronic devices in accordance with Olympic Aero Services Inc. Master Drawing List OAS-54-0001 Revision G dated September 26 2002 or later FAA approved revision. This system shall be maintained in accordance with Instructions for Continued Airworthiness Document OAS-54-23.1529 Revision B dated August 22 2001 or later FAA approved revision. | | Reissued | | 4/9/2012 |
| SA01015SE | | Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. | | Amended | | 10/4/2012 |
| SA01018CH | | Installation of Ryan International Traffic and Collision Alert Device (TCAD) 8800 Series P/N 71-3000 and 71-3001. | | Issued | | 3/16/1999 |
| SA01021WI-D | | Installation of Bendix/King KMH 880 Multi-Hazard Awareness System/KTA 870 Traffic Advisory System. | | Issued | | 11/8/2001 |
| SA01026SE (PAGE 2) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01032WI | | Installation of external aerodynamic Vortelator Kit on airplanes | | Amended | | 7/11/2008 |
| SA01033CH | | Installation of McCauley Propeller Model 2A34C203/90DCA-X.. | | Reissued | | 9/23/2005 |
| SA01068WI-D | | Installation of Bendix/King KMH 880 Multi-Hazard Awareness System. For model 182T approved for installation on serial number 18281103 and after. For model T182T serial number T18208139 and after. | | Issued | | 4/8/2002 |
| SA01070WI-D | | Installation of Bendix/King KDR 510 VHF Data Link System. | | Issued | | 4/9/2002 |
| SA01074WI | | Installation of McFarlane Aviation Flap Roller Assembly Service Kit MCSK100 on various Cessna single-engine aircraft. Cessna Service Bulletin SEB95-3 must be complied with before this STC is installed. | | Issued | | 4/22/2002 |
| SA01077SE (PAGE 1) | | Installation of fluoropolymer film. | | Reissued | | 8/20/2003 |
| SA01080SE | | Installation of Dynamic Propellers latch brackets on induction bellows and carburetor air box flange. | | Issued | | 4/26/2002 |
| SA01085LA (PAGE 1) | | Installation of the VNS 1000 Voice Navigation System. | | Reissued | | 4/26/2010 0:00 |
| SA01096WI | | Installation of Gomolzig C182R-606550 engine exhaust system silencer. | | Reissued | | 3/20/2007 |
| SA01102SE | | Installation of fiberglass extended baggage compartment. | | Reissued | | 5/20/2010 |
| 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 |
| SA01107SE | | RMD Aircraft Lighting high intensity discharge wingtip light manufactured | | Amended | | 4/2/2003 |
| 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 |
| SA01119CH | | Replace Cessna Sun visor assemblies with Aircraft Recycled Flying controls tinted Sun Visor Assemblies | | Reissued | | 3/20/2006 |
| SA01120SE | | Installation of Door Steward. | | Amended | | 3/4/2010 |
| SA01140WI | | Installation of a Garmin GNS 430/530 VHF NAV/COMM/GPS System and associated GI 106A Course Deviation Indicators (CDI) GTX 327 ATCRBS Transponder and GMA 340 Audio Panel. Data Required: (1) Garmin Master Drawing List (MDL) 005-C0001-00 Revision E dated February 18 2003 and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) for Cessna Models 182S 182T and T182T with Garmin GNS 430 and GNS 530 VHF NAV/COMM/GPS and GI 106A Course Deviation Indicators Garmin Document Revision B dated February 26 2003 or later FAA Approved Revisions to (1) or (2). | | Issued | | 2/27/2003 |
| SA01156CH | | Installation of Wipaire model 3000 amphibian/seaplane floats | | Amended | | 6/5/2013 |
| 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 |
| SA01170NY | | Installation of NPX138N-XXX FM Transceiver. | | Amended | | 1/17/2007 |
| SA01202LA | | Installation of Becker Avionics SAR DF-517 Search and Rescue Direction Finding System | | Reissued | | 2/13/2012 |
| SA01204LA | | Installation of replacement wing tip fairing assembly. | | Issued | | 10/3/2001 |
| 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 |
| SA01215WI | | Installation of Civil Air Patrol UPSTAT Avionics package in the Cessna 182T including GX-60 GPS/Com SL30 VHF Nav/Com Artex 406 Mhz ELT KR-21 Marker Beacon Receiver Apollo Annunciator Control Unit Mid-Continent Instruments MD-200 Nav Indicator and NAT AMS-44T two channel audio panel. Installation of the avionics package must be accomplished in accordance with Yingling Aviation Master drawing List MDL2701-34350 Revision A dated September 18 2003 or later FAA approved revision. | | Issued | | 11/25/2003 |
| SA01216WI | | Installation of Civil Air Patrol (CAP) Special Missions Equipment in the Cessna Models 182T/T182T including the KGS power converter Technisonics TDFM Transceiver Rhotheta/Becker ADF P/N 0531-324-924 and 12 and 28 VDC power outlets. The CAP Special Mission Equipment may be interfaced to the UPSAT Avionics package or the NAV III (Garmin G-1000 w/Dual GMA-1347 Audio Panels) Avionics package. An optional ARTEX 110-406 Emergency Locator Transmitter and/or audio provisions for ARNAV RCOM 100 SATCOM may be installed when the CAP equipment is installed with the NAV III package.
);INSERT INTO stc_table VALUES (
);INSERT INTO stc_table VALUES ( Installation of the CAP equipment in accordance with the installation data and FAA Approved Airplane Flight Manual Supplements (AFMS) listed on the Continuation Sheet (See page 3 of 3). | | Amended | | 7/22/2011 |
| SA01217WI | | Installation of a Left Hand Aft removable window. | | Reissued | | 12/15/2003 |
| SA01218AT | | Installation of a Teledyne Continental Motors Model IO-550-D engine and either a Hartzell Model PHC-C3YF-1RF/F8468A( )-6R or PHC-C3YF-1RF/F7691( ) or PHC-G3YF-1RF/F8468A( )-6R or PHC-G3YF-1RF/F7691( )or McCauley Mod D3A34C401/90DFA-10 3-blade propeller. | | Reissued | | 2/4/1999 |
| SA01224AT | | Installation of wheel hub cabs with valve stem access door. | | Amended | | 4/17/1998 |
| 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 |
| SA01293LA | | Installation of a modified exhaust collector assembly per Knisley Welding master drawing list (MDL) No. 6 Rev A dtd 12/31/01. | | Issued | | 1/16/2002 |
| SA01302AT | | Installation of Teledyne Continental Motors Model IO-520-D engine and either a McCauley Model D3A34C401/90DFA-10 or Hartzell Model PHC-C3YF-1RF/F8468A( )-6R or PHC-C3YF-1RF/F7691( ) or PHC-G3YF-1RF/F8468A( )-6Ror PHC-G3YF-1RF/F7691( ) 3-blade propeller. | | Reissued | | 2/3/1999 |
| SA01323WI | | Installation of flap gap seal per Aircraft Development Co. Drawing List 114-1 stamped FAA approved with a date of April 27 2005 or later. Conformity data for Drawing List 114-1 is derived from Drawing List 114-1 Revision C and STC | | Issued | | 4/27/2005 |
| SA01324WI | | Installation of aileron gap seal per Aircraft Development Co. Drawing List 115-1 stamped FAA approved | | Issued | | 4/27/2005 |
| SA01328LA | | Modification of right hand side door to provide an openable window. | | Reissued | | 3/30/2005 |
| SA01330LA (PAGE 1) | | Installation of alternate avionics support assembly. | | Reissued | | 10/6/2010 |
| SA01338WI | | Installation of TKS Ice Protection System components. | | Reissued | | 7/8/2008 |
| SA01353NY | | Installation of Aerocet 3500/3500L float conversion in accordance with Transport Canada approved Amtech Aeronautical Limited (AAL) Modification Data Summary MDS 305901 latest revision. | | Amended | | 7/25/2002 |
| SA01356WI | | Installation of the Garmin GFC 700 Automatic Flight Control System. | | Issued | | 9/30/2005 |
| SA01364SE | | Fabrication of Selkirk Aviation Inc. Fiberglass Extended Baggage Compartment. | | Reissued | | 5/20/2010 |
| SA01380CH | | Installation of wing fuel tank quick valve drains. | | Issued | | 1/25/2001 |
| SA01386NY | | Installation of Fibre Glass Reinforced Plastic Nacelle Fairing Trade Name Exhaust Fairing . | | Reissued | | 10/9/2002 |
| SA01407NY | | Installation of Airborne Position/Data Communicator. | | Issued | | 11/1/2001 |
| SA01422SE | | Installation of S-TEC System 30 Two Axis Autopilot per STC SA09289AC-D installed on an aircraft modified with a Mid-Continent STOL kit per STC SA1371SW. Limited to installation on serial number 52700 ONLY. | | Issued | | 6/9/2004 |
| 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 |
| SA01436SE (1 OF 2) | | Cockpit sunvisor retrofit kit. | | Issued | | 8/2/2004 |
| SA01438WI | | Installation of MT-Propeller Model MTV-9-D/203-52 hydraulic 3-blade constant speed propeller. | | Amended | | 7/20/2007 |
| SA01443AT | | Installation of Teledyne Continental Motors Model O-470-U engine modified. | | Reissued | | 2/3/1999 |
| SA01454SE | | Incorporation of a nylon sleeve on the carburetor heat cable housing to prevent abrasion of the cable | | Issued | | 9/20/2004 |
| SA01456NY | | Installation of Technisonic Industries Ltd OSAT-100 Airborne Position/Data Communicator. | | Issued | | 1/31/2002 |
| 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 |
| SA01518AT | | Installation of a McCauley C234C204/90DCB-8 propeller to a Teledyne Continental Motors Model O-470-U modified. | | Amended | | 4/19/2010 |
| SA01538SE | | Incorporation of bushing on carburetor hot air box control arm in accordance with Dynamic Propeller Installation Instructions No. 7000 Revision A dated February 24 2005 or later FAA approved revision to this document. | | Issued | | 4/27/2005 |
| SA01552WI | | Installation of Supplemental Audio System including #2 GMA 1347 Audio Panel | | Amended | | 11/12/2009 |
| 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 |
| SA01569WI | | Installation of two tinted flush cockpit skylights | | Issued | | 11/12/2009 |
| SA01570WI | | Installation of a pair of fixed extended flap with tab cowl cooling flaps in lieu of the movable cowl flaps | | Issued | | 12/14/2009 |
| SA01573NY | | Installation of Seaplanes West Replacement Engine Mount. | | Amended | | 6/30/2003 |
| SA01581AT | | Installation of McCauley C234C204/90DcB-8 propeller to Teledyne Continental Motors Model O-470-U. | | Amended | | 4/19/2010 |
| SA01589AT | | Installation of Composite Spinner. | | Amended | | 10/13/2000 |
| SA01598CH | | Replace existing propeller with Hartzell Propeller model PHC-G3YF-1RF/F8468A-2R or -6R. | | Amended | | 11/17/2009 |
| SA01601CH | | Installation of McCauley propeller model D3A36C435/80VEA-0. | | Reissued | | 9/23/2005 |
| SA01644SE | | Fabrication and Installation of composite engine cowling. | | Reissued | | 5/20/2010 |
| SA01646SE | | Installation of vortex generators on wings horizontal and vertical tail surfaces. | | Issued | | 2/28/2006 |
| SA01666AT | | Installation of Bonaire heavy duty mount P/N BN182-802 or P/N BN180-802. | | Reissued | | 2/18/1999 |
| 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 (1 OF 5) | | Installation of an antenna | | Amended | | 2/15/2007 |
| SA01695SE (2 OF 5) | | Installation of an antenna | | Amended | | 2/15/2007 |
| SA01700LA | | Installation of AMSAFE Aviation Inflatable Restraint (AAIR) system. | | Issued | | 12/3/2004 |
| SA01708WI | | Installation of third lap belt restraint in the center of the main cabin rear bench seat | | Issued | | 12/13/2012 |
| SA01709WI | | To increase the takeoff weight 150 lbs to 2950 lbs while the landing weight remains the same at 2800 lbs | | Amended | | 4/9/2013 |
| SA01710SE | | ONE-ONLY STC: Installation of a structural modification for model 182M serial number 18259626. | | Issued | | 10/3/2006 |
| 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 |
| SA01765SE | | Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. | | Amended | | 10/11/2012 |
| SA01800SE (PG 1) | | 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 (1 OF 3) | | Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | | Amended | | 5/31/2006 |
| SA01861SE (PAGE 1) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| 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 |
| 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 |
| SA01951NY-D | | Installation of Wulfsberg P-2000 and/or C-2000-RT-2000 transceiver system. | | Reissued | | 3/18/2005 |
| SA01981AT | | Installation of an Inframetrics Model IRTV-445G MK II Airborne Thermal Imaging system. | | Issued | | 9/2/1999 |
| SA01988SE (PAGE 3) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
| SA01999CH | | Install BRS-182 parachute recovery system. | | Amended | | 8/29/2012 |
| SA02006CH | | Installation of air conditioning system. | | Amended | | 12/20/2011 |
| SA02008AK | | Fabrication and installation of left-hand or right-hand removable folding jump seat or both. | | Issued | | 12/21/1993 |
| 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 |
| SA02019NY | | Installation of EDO 2870/2960 model floats. STC SA01353NY required with this modification. Approved for models 182E-H 182J-N 182P-Q. | | Amended | | 8/4/2005 |
| SA02019SE-D | | Installation of Garmin GTN 6XX/7XX Navigation System | | Amended | | 12/13/2013 |
| SA02026SE | | Fabrication and installation of Dynamic Propeller Cowl Flap Support Kit. | | Issued | | 9/18/2009 |
| SA02031NY | | Installation of the Aerocet 3400 Amphibious Float conversion. | | Issued | | 12/2/2004 |
| 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 |
| SA02049SE | | Fabrication of Stene Aviation Inc. Wing Tip Part Numbers SA-0523565-29 and SA-0523565-30 | | Issued | | 2/2/2010 |
| SA02069AK | | Fabrication and Installation of the Airglas PA32-206LA Nose Fork equipped with Goodyear 8.50 x 6 tires. | | Amended | | 6/5/2006 |
| SA02072AK | | Installation of hourmeter airspeed switch. | | Amended | | 11/14/1997 |
| SA02092SE | | Installation of Continental/P. Ponk O-470-50 engine and a McCauley D2A34C58/90AT-8 or 2A34C66/90AT-8 or D3A32C90/82NC-2 or D3A34C401/90DFA-8 or D2A37C230/90REB-8 propeller in accordance with P. Ponk Report Number PPA-10182 Revision IR dated August 30 2010 or later FAA-approved revision. | | Amended | | 12/8/2010 |
| SA02106AT | | Installation of a Spectrolab SX-5 searchlight. | | Issued | | 3/30/2000 |
| SA02110CH (PAGE 1) | | 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 |
| SA02149AK | | Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. | | Reissued | | 5/17/2013 |
| 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 |
| SA02161AK | | Fabrication and installation of Stabilizer Jack-Screw Actuator in accordance with North Pacific Welding Drawing Number C-0712500 dated March 31 2000 and Cessna 100 Series 1962 and prior Service Manual dated February 1 1962 or McFarlane Aviation Inc. Drawing 1111-1 revision original dated June 1 2010 or later FAA approved revisions. | | Amended | | 5/13/2011 |
| SA02163AT | | Removal of right passenger entry door for aerial photography purposes with a hand-held camera. Limited to S/N 182-60855 ONLY. | | Issued | | 7/24/2000 |
| SA02173AT | | Manufacture of composite engine cowlings. | | Reissued | | 1/1/2007 |
| SA02179AK | | Fabrication and installation of an Alaskan SkyPod P/N SP1-100 cargo belly pod. | | Reissued | | 8/12/2010 |
| SA02180AK | | Fabrication and installation of Extended Baggage Compartment (P/N 180EB) in accordance with Aerovative Composites Inc. Master Drawing List Rev. A dated July 21 2011 or later FAA approved revision. For Instructions for Continued Airworthiness refer to Aerovative Composites Inc. Installation Maintenance and Instructions for Continued Airworthiness (ICA) for EB-180 EB-180-105 Revision A dated
);INSERT INTO stc_table VALUES ( July 21 2011 or later FAA approved revision. | | Amended | | 9/14/2011 |
| SA02186AT | | Installation of E-Z Charge 2000 plug (for battery charger). | | Issued | | 8/28/2000 |
| SA02203AK (PAGE 1) | | Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). | | Amended | | 12/21/2011 |
| SA02211CH | | Installation of a Three Point Torso Restraint System | | Issued | | 11/15/2005 |
| SA02212AK (PG 1) | | Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems | | Amended | | 5/4/2011 |
| SA02217AK (2 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 |
| SA02231AK | | Installation of Cleveland Main Wheels and Brakes. | | Reissued | | 3/17/2008 |
| SA02246LA | | Installation of a flap handle extension. | | Amended | | 11/16/2010 |
| SA02248LA | | Installation of Sensor Pod and wiring for a passenger operated monitoring system | | Reissued | | 1/30/2014 |
| SA02249SE | | Installation of a silicone rubber wingtip device intended as a provision for mounting battery powered devices such as strobes or air temperature sensor | | Amended | | 9/18/2013 |
| SA02262SE | | Installation of split seam wing strut cuff as replacement parts for the strut fairings | | Issued | | 3/8/2013 |
| SA02264NY | | Installation of the Whipline Model 3000 floats. | | Issued | | 6/2/2006 |
| SA02265SE | | Installation of a camera housing | | Amended | | 11/1/2013 |
| SA02266AK | | Replacement of Rudder and Elevator Hinge Bearings with P. Ponk Aviation Bearing p/n PPA-1401. | | Reissued | | 6/19/2006 |
| 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 |
| SA02276AK | | Installation of AMSAFE Aviation Inflatable Restraints | | Amended | | 3/12/2013 |
| SA02277AK | | Installation of FMK Light Emitting Diode (LED) Instrument Panel Lights. | | Issued | | 9/30/2006 |
| SA02278AK | | Installation of Hartzell Propeller Models PHC-C3YF-1RF/F8068-4 to F8068+2 and PHC-G3YF-1RF/F8068-4 to F8068+2. | | Amended | | 2/9/2009 |
| 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 |
| SA02294CH | | Installation of an MT-Propeller MTV-(9 or 15)-D/205-58 or MTV-(9 or 15)-D/210-58 and spinner assembly | | Reissued | | 12/17/2008 |
| SA02311NY | | Installation of 260HP Lycoming IO-540-D4B5 engine | | Issued | | 11/7/2006 |
| SA02312AK-D | | Fabrication and Installation of Aero Twin Inc. Main Gear Gravel Deflector Kit No. GD5-102 | | Issued | | 6/18/2008 |
| SA02323AK | | Installation of Horizontal Stabilizer Screw-on Leading Edge. | | Issued | | 10/20/2008 |
| SA02332AK | | Installation of a fixed mounted Forward.Vision Enhanced Vision System (EVS) Models 100/600 to include an under-wing conformal fairing with sensor and a glareshield mounted dedicated display monitor | | Issued | | 6/24/2009 |
| SA02359AK-D | | Fabrication and installation of F. Atlee dodge Aircraft Services Cessna Tie-Down clamp | | Issued | | 11/6/2009 |
| SA02361AK | | Installation of a firewall mounted battery tray and heat shield | | Issued | | 12/18/2009 |
| SA02411CH | | Installation of the Aero Vent Cabin Ventilation System. | | Issued | | 7/25/2008 |
| SA02415CH | | Installation of Flight Boss LTD S-RPE-CN Rudder Pedal Extensions. | | Issued | | 5/10/2007 |
| SA02434NY | | Installation of a Digital Engine Monitoring system. | | Amended | | 2/7/2012 |
| SA02446CH | | Installation of the Courtesy Light Kit. | | Issued | | 6/25/2007 |
| SA02462CH | | Installation of Flight Boss LTD S-RPE-CO Rudder Pedal Extensions | | Issued | | 8/29/2007 |
| SA02497CH | | Installation of the Knots 2U Flight Lite System | | Issued | | 8/10/2006 |
| SA02511CH | | Installation of Saf-Air Products fuel quick drain backing plate C187 and fuel drain valve B187 | | Issued | | 1/7/2008 |
| SA02520AT | | Installation of M-20 Oil Separator model 600-WP. | | Issued | | 5/30/2002 |
| SA02547AT (PG 1) | | Installation of a Voice Alert System. | | Amended | | 8/28/2007 |
| SA02605CH | | Installation of Backup Alternator Kit | | Amended | | 9/10/2009 |
| SA02632AT-D | | Installation of fuel cell modifications | | Reissued | | 4/16/2009 |
| SA02655AT (1 OF 2) | | Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. | | Amended | | 9/1/2004 |
| SA02717AT | | Conversion of Cessna Model TR182 to Model R182 by removal of Cessna installed turbocharger and related systems and replacement of engine model Lycoming O-540-L3C5D with O-540-J3C5D. Conversion in accordance with AvPower Master Parts List AP1010-4 dated June 4 2003 or later FAA approved revision. This is a one time STC valid for Cessna Aircraft Model TR182 Serial Number R18201980 only. | | Issued | | 9/29/2003 |
| SA02717NY | | Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module | | Amended | | 1/9/2012 |
| SA02725CH | | Installation of North American Surveillance Systems Strut Mount and Optional Cloud Cap Technologies TASE / TASE Dou Gimbals | | Issued | | 5/29/2009 |
| SA02735CH | | Installation of Hartzell Propeller Model (P)HC-()3YF-1RF/8068(B K)() and /or (P)HC-()3YF-1RF/7693DF(B K)() 3 bladed metal propeller | | Issued | | 8/14/2009 |
| SA02738CH (PAGE 4) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
| SA02795AT | | Installation of a PXE7300SR In-Flight Entertainment System | | Issued | | 2/12/2004 |
| SA02827AT | | Installation of a cargo restraint net and protective flooring in accordance with Zerotime Aviation LLC Report No. 33126 dated April 18 2004 or later FAA approved revision. | | Issued | | 4/23/2004 |
| 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 |
| SA02933CH | | Installation of the Cessna 182D cowling (upper cowling P/N 0752031-27 lower cowling P/N 0752031-28) with cowl flaps and cowl flap mechanism in accordance with Tom P. O | | Issued | | 2/25/2011 |
| SA03078CH | | Installation of Hartzell HC-(C I F)3YR-1(A)RF/F8068(K) or HC-(C I F)3YR-1(A)RF/F7693F(K)+2 propeller | | Issued | | 5/4/2012 |
| SA03139AT | | Conversion of Cessna Models 182 182A 182B 182C and 182D from a Tricycle Landing Gear (nose wheel) to a Conventional Landing Gear (tail wheel) configuration. | | Issued | | 8/18/2005 |
| SA03148NY ( PAGE 1 OF 2) | | The installation of the Latitude Technologies Corporation S100 Tracking System | | Issued | | 9/26/2012 |
| SA03286CH | | Install an electronic engine ignition system | | Issued | | 1/13/2014 |
| SA03302AT | | Installation of Societ | | Reissued | | 1/7/2014 |
| SA03608AT | | Increased Maximum Gross Takeoff Weight (MGTOW). | | Issued | | 8/25/2008 |
| SA03984AT | | Installation of a FreeFlight Systems Universal Access Transceiver - Automatic Dependent Surveillance | | Issued | | 12/13/2012 |
| SA09000SC | | Installation of a Hartzell propeller Model PHC-G3YF-IRF/F7691 and Spinner Assembly D5732 or C4582. (182 S/N 18265176 AND SUBSEQUENT EQUIPPED WITH O-470-U ENGINE) | | Amended | | 10/13/2000 |
| SA09001SC | | Installation of Hartzell Propeller Model PHC-G3YF-1RF/F7691 and Spinner Assembly D5732 or C4582. | | Amended | | 11/4/1996 |
| SA09002AC-D | | Installation of S-TEC System 55 two axis automatic flight guidance system Model ST-586 with optional autotrim system. | | Amended | | 2/2/2001 |
| SA09007AC-D | | Installation of S-TEC System 55 two axis automatic flight guidance system Model ST-587 with optional autotrim system. | | Amended | | 2/15/2001 |
| SA09009AC-D | | Installation of S-TEC System 55 two axis autmatic flight guidance system Model ST-588 with optional autotrim system. | | Amended | | 6/11/2001 |
| SA09026SC | | Installation of modified Teledyne Continental IO-520-F engine designated O-520-F-TS and Hartzell propeller model OHC-G3YF-1RF/F7691 and spinner assembly D5732 or C4582 or McCauley Propeller Model D3A34C401/90DFA-1D and Spinner Assembly D6594. | | Amended | | 6/26/2002 |
| SA09056SC | | Installation of Teledyne Continental IO-520-F engine modified under STC SE09054SC. | | Amended | | 11/4/1996 |
| SA09133SC | | Installation of modified Teledyne Cont IO-550-F engine and Hartzell propeller model PHC-G3YF-1RF/ F7691 with spinner assembly D5732 or D4582 or McCauley propeller model D3A34C401/90DFA/10 and spinner assembly D6594. | | Amended | | 11/4/1999 |
| SA09149SC | | Modification of nose gear fork P/N SK150-11 to the SK182-34 configuration. | | Amended | | 2/22/1996 |
| SA09193AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-651 with Optional Autotrim System. | | Amended | | 3/5/2001 |
| SA09240SC | | Installation of dual Terra TX-760D communications transcievers single Terra TN-200D with glide slope single TN-200D without glide slope single tri-nav indicator single tri-nav C indicator. | | Reissued | | 12/21/2001 |
| SA09241SC | | Installation of single TRA-3500 radar altimeter using TRI 40 indicator and the installation of TM-23 marker beacon receiver using MLC28-5 voltage converter. | | Reissued | | 12/21/2001 |
| SA09242SC | | Installation of TDF-100D Automatic Direction Finder (ADF) System. | | Reissued | | 4/5/2002 |
| SA09261AC-D | | Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-586 with Optional Autotrim System. | | Amended | | 2/2/2001 |
| SA09262AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance System Model ST-718-20/30. | | Issued | | 8/4/1997 |
| SA09263AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance System Model ST-718-20/30. | | Issued | | 8/4/1997 |
| SA09272AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model ST-719. | | Issued | | 10/7/1997 |
| SA09273AC-D | | Installation of S-TEC System 30 ALT Altitude Hold System Model St-719. | | Issued | | 10/7/1997 |
| SA09289AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-731-20/30. | | Issued | | 10/29/1997 |
| SA09316AC-D | | Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-759-20/30. | | Issued | | 12/18/1997 |
| SA09319AC-D | | Installation of S-Tec system 20/30 single and two axis automatic flight guidance systems. | | Amended | | 6/18/2002 |
| SA09323AC-D | | Installation of S-TEC System 30 Alt Altitude Hold System. | | Issued | | 1/13/1998 |
