Cessna 182 E F G H

Number of Active Aircraft: 1639 Active- Map


Years Produced: 1961-64 The most notable changes with these models the gross weight increase to 2800 pounds.

Wikipedia Cessna 182 reference:

Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1560 lbs
Max Weight 2800 lbs
Useful Load: 1240 lbs
Engine Name Continental O-470-L
Engine Number 1
Horsepower 230 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 20100 ft
Max Fuel 55 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 139 kts
GPH (75% BHP): 13
MPG (75% BHP) 10.7
Range (75% BHP): 497 nm
Fuel Cost Per Seat Mile 0.14 $
Fuel Cost Per Hour 78 $
MPG per 1000 lbs of Payload 13.26
F-T (Speed^2/FuelBurn) 14.9 HP
F-T Payload 18.5 kts
MPH To HP: 6 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1020 ft

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
Fusulage Construction
Airframe Material
Number of Doors
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
Aileron Type
Aileron Trim
Aileron Control System
Flap Type
Wing Flap Actuation
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Instrument Panel
Flight Control
Number of Seats
Window Defrost
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)


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