Cessna 180 J

Number of Active Aircraft: 271 Active- Map


Major changes were minimal after the G model, however the J model boosted 75 gallon fuel tanks.

Wikipedia Cessna 180 reference:

Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 1617 lbs
Max Weight 2800 lbs
Useful Load: 1183 lbs
Engine Name Continental O-470-R
Engine Number 1
Horsepower 230 HP
Never Exceed Speed: 167 kts
Stall speed: 0 kts
Service Ceiling: 19600 ft
Max Fuel 75 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 141 kts
GPH (75% BHP): 13.9
MPG (75% BHP) 10.1
Range (75% BHP): 670 nm
Fuel Cost Per Seat Mile 0.1 $
Fuel Cost Per Hour 83.4 $
MPG per 1000 lbs of Payload 12
F-T (Speed^2/FuelBurn) 14.3 HP
F-T Payload 16.9 kts
MPH To HP: 6.1 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1205 ft

SA00022SE Installation of modified instrument panel and U-style control yoke Issued 9/3/1993
SA00023SE Installation of modified control yoke and instrument panel. Amended 11/20/2002
SA00029WI Installation of flap and aileron gap seals. Issued 2/11/1993
SA00052NY Installation of wing tip extension. Issued 11/18/1993
SA00057LA Installation of a heat shield. Issued 3/15/1995
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00066SE Fabrication of interchangeable float spreader bars. Amended 10/10/2000
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
SA00103BO Installation of Weemax cabin air vent. Issued 6/16/1999
SA00137SE Installation of Aerocet Model 3500 or 3500L seaplane floats. Amended 5/29/2008
SA00144WI Installation of 18 gallon nylon auxiliary fuel tanks on airplanes equipped with standard range 64 gallon capacity bladder tank or 62 gallon fiberglass fuel tanks. (180K thru S/N 18053000) Reissued 5/3/2004
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
SA00164BO Installation of a Continental O-470-R engine with a McCauley 2A36C 2A34C 2A34C66 or 2A34C203 propeller. Issued 2/12/2003
SA00165SE Installation of 76 vortex generators and 2 small delta wings on the upper surface of the wings. Amended 5/18/2001
SA00188AT Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-26A. Reissued 11/14/1994
SA00192AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00194BO Installation of P/N 2042 Landing Gear Warning System for amphibian aircraft. Reissued 1/23/2009
SA00200AT Installation of carbon steel brake discs that have the melonite surface treatment P/N AA-36. Reissued 11/14/1994
SA00209AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-89. Reissued 11/14/1994
SA00210AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-90. Reissued 11/14/1994
SA00214AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-89. Reissued 11/17/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00227AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-94. Reissued 12/7/1994
SA00228AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-95. Reissued 12/7/1994
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
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
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
SA00360SE Installation of Edo 628-2960 floats. Issued 8/1/1996
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
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00462AT Replacement of Appalachian stainless steel brake discs P/N 75-23 with Appalachian steel brake disk part number AA-47. Reissued 12/7/1994
SA00465NY Installation of Meterological Measurement System Model A1MMS-10 with optional installation of Telemetry Module Model AIRDAT-9600. Amended 10/28/1998
SA00468WI Installation of P Ponk Aviation O-470-50 (TCM) engine approved per STC SE4988nm with McCauley D3A34C401/90DFA -2 -4 -6 -8 and -10 propellers. Reissued 11/20/2003
SA00478SE Replace existing horizontal stabilizer skins Issued 11/6/1997
SA00496SE Installation of Oregon Aircraft Design Engine Mount Heat Shields. Amended 12/20/2000
SA00512SE Fabrication of a vortex generator system. Amended 5/14/1998
SA00531WI Installation of D3A34C401/90DFA -2 -4 -6 -8 and -10 propellers. Reissued 9/22/2005
SA00562NY Installation of Teledyne Continental IO-470 engine modified to incorporate a carburetor system. Issued 2/10/1997
SA00581LA Limited to installation on Cessna model 180 serial number 30815 ONLY. Issued 2/27/1998
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
SA00740SE Installation of Dynamic Propellers support brackets. Amended 5/18/2001
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
SA00785AT Installation of a Teledyne Continental Model IO-550-D engine and various3 blade propellers. Reissued 6/3/1999
SA00796SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft Amended 5/27/2004
SA00800SE Installation of modified main landing gear assembly on aircraft Amended 3/21/2013
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
SA00843NY Aircraft fuel quantity transmitter replacement-from Stewart Warner Model 390 to Stewart Warner Model 385. Issued 5/28/1998
SA00852AT Installation of Hartzell PHC-C3YF-1RF/F7691 PHC-G3YF-1RF/F7691() PHC-C3YF-1RF/F8468A()-6R or PHC-G3YF-1RF/F8468A()-6R propellers to TCM O-470-A J K L R. S and U powered Cessna 180 series aircraft. Reissued 1/27/1999
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
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
SA00897WI Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Issued 8/11/2000
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
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
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
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
SA01087SE  Installation of titanium main landing gear assembly Amended 3/21/2013
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
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
SA01120SE Installation of Door Steward. Amended 3/4/2010
SA01158WI (1 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005
SA01163SE Installation of ARNAV Systems RCOM-100 Globalstar Satellite Telephone per ARNAV Systems Inc. RCOM-100 Installation Guide Part Number 570-8050B  Issued 1/21/2003
SA01170NY Installation of NPX138N-XXX FM Transceiver. Amended 1/17/2007
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
SA01217SE Installation of Zeiss Aerial Survey Camera System.  Issued 5/19/2003
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
SA01257SE Installation of Aerocet Model 3400 floats Amended 8/28/2003
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
SA01320CH Installation of Wipaire Model 3000 Amphibian/Seaplane floats. Amended 4/29/2009
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
SA01330LA (PAGE 1) Installation of alternate avionics support assembly. Reissued 10/6/2010
SA01345AT Installation of Teledyne Continental IO-520-D and either Hartzell PHC-C3YF-1RF/F8468A( )-6R Hartzell PHC-C3YF-1RF/F7691( ) or McCauley D3A34C401/90DFA-10 3 bladed propellers. Amended 3/12/2002
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
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
SA01442AT Installation of a Teledyne Continental Motors Model O-470-U engine. Reissued 6/3/1999
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
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
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
SA01573NY Installation of Seaplanes West Replacement Engine Mount. Amended 6/30/2003
SA01591AT Replacing Continental 0-470-A engine with Continental 0-470-L and installing McCauley propeller Model 2A34C203-B/G-90DCA-8. Reissued 10/5/2012
SA01598CH Replace existing propeller with Hartzell Propeller model PHC-G3YF-1RF/F8468A-2R or -6R. Amended 11/17/2009
SA01606CH Installation of alternate electro-hydraulic power pack system for operation of main wheel skis. Amended 4/16/2010
SA01636SE Manufacture and installation of an Alaskan Bushwheel tailwheel and fork assembly. Amended 4/11/2008
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
SA01664AT Installation of Bonaire heavy duty engine mount P/N BN180-802. Reissued 2/18/1999
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01679SE Installation of Sagem Avionics Inc. Integrated Cockpit Display System as a Primary Flight Display. Issued 6/16/2006
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
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
SA01756NY Installation of Cessna Main Landing Gear Legs P/N 0741001-3 through -8 and 054118-2 through -3. Reissued 10/23/2003
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01776AT Installation of a Teledyne Continental Motors Model O-470-U engine modified in accordance with IAW STC SE01153AT and McCauley C2a34C204/90DCB-8 2-blade propeller IAW Bonaire Aviation Doc #BOAC 1029A. Reissued 6/3/1999
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
SA01944CH (1 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
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
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02022AK Installation of Aero Twin Inc. Main Gear Gravel Deflector Kit No. GD5-100 Amended 8/13/1998
SA02026SE Fabrication and installation of Dynamic Propeller Cowl Flap Support Kit. Issued 9/18/2009
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
SA02072AK Installation of hourmeter airspeed switch. Amended 11/14/1997
SA02105AK Fabrication and installation of MFD 5200 CDU and GeoLink computer/transceiver. Issued 3/18/1998
SA02110CH (PAGE 1) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02112AK  Fabrication and installation of Stabilizer Jack-Screw Actuator in accordance with North Pacific Welding Drawing Number C-0712500 dated March 31 2000 and Cessna Skywagon 180 and 185 Series Service Manual or McFarlane Aviation Inc. Drawing 1111-1 revision original dated June 1 2010 or later FAA approved revisions.  Amended 5/13/2011
SA02116AK Installation of DGA Aviation Extended Baggage Compartment. Amended 10/13/1998
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
SA02153AK Installation of Burl s Aircraft Rebuild Magnum I tail wheel penetration tail ski per Burl s Aircraft Rebuild LLC Master Data List No. MDL-3234-1 latest FAA approved revision. Issued 12/22/1999
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
SA02165AK Installation of ARNAV Systems Inc. MFD 5200 CDU p/n 453-2550 MFD 5115 RPU P/N 453-2530-08 DR-100 Receiver P/N 453-0160 and EMM 35 Engine Trend Monitor P/N 453-5030. Issued 11/6/2000
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
SA02203AK (PAGE 2)  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
SA02244AK Fabrication and installation of Airglas Inc. Model LH4000 hydraulically retractable wheel skis. Issued 6/8/2005
SA02245AK Data pertaining to this modification are inadequate for duplication in other airplanes. This approval is limited to Cessna Model 180C airplane Registration Number N9311T Serial Number 50811 only. Installation of Cessna 182G wings with Robertson Aircraft Corporation STOL Kit long range fuel tanks and replacement of original fuel gage system. Issued 5/20/2005
SA02246LA Installation of a flap handle extension. Amended 11/16/2010
SA02250AK Data pertaining to this modification are considered inadequate for duplication on other airplanes. This approval is limited to Cessna Model 180 aircraft serial number 32851. Installation of Satellite ATM system. Issued 7/6/2005
SA02262SE Installation of split seam wing strut cuff as replacement parts for the strut fairings Issued 3/8/2013
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 (2 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
SA02299SE Installation of the Alaskan Bushwheel Inc. (ABI) Cessna Tail Spring Issued 12/18/2013
SA02319AK-D Fabrication and installation of F. Atlee Dodge p/n 180VBE Windshield V-Brace Issued 8/19/2008
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
SA02333AK-D Fabrication and installation of F. Atlee Dodge p/n 8008 Firewall Battery Box Issued 1/22/2009
SA02359AK-D Fabrication and installation of F. Atlee dodge Aircraft Services Cessna Tie-Down clamp  Issued 11/6/2009
SA02360AK Fabrication and installation of Airglas Inc. Model GLH3000 hydraulically retractable wheel skis Amended 11/25/2013
SA02361AK Installation of a firewall mounted battery tray and heat shield Issued 12/18/2009
SA02385AK Installation of replacement engine exhaust stack assemblies (P/N Amended 6/29/2012
SA02387AT Installation of engine cowling and firewall fasteners. Issued 8/29/2001
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
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
SA02632AT-D Installation of fuel cell modifications Reissued 4/16/2009
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 5) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
SA02839AT Modification of the main landing gear bulkhead to improve static strength and fatigue characteristics.  Issued 4/13/2004
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
SA03030CH Installation of the Custom Fiberglass Molding Inc. (CFMI) model 3000 Aircraft Main Landing Gear Skis with optional CFMI Model 1500 Tail Wheel Ski in accordance with Custom Fiberglass Molding Inc. installation design data contained within AML No. SA03030CH issued November 3 2011 or later FAA Approved revision. Issued 11/3/2011
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
SA09001SC Installation of Hartzell Propeller Model PHC-G3YF-1RF/F7691 and Spinner Assembly D5732 or C4582. Amended 11/4/1996
SA09017AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-596. Amended 2/2/2001
SA09018SC Installation of mod Teledyne Continental IO-520-F engine designated O-520-F-TS and Hartzell propeller Model PHC-G3YF-1RF/F7691 and spinner assembly D5732 or C4582 or McCauley Propeller Model D3A34C401/90DFA-1D and spinner ass D6594. Amended 6/26/2002
SA09025SC Installation of Hartzell propeller Model PHC-G3YF-1RF/F7691 and spinner assembly D5732 or C4582. Reissued 5/5/1997
SA09030SC Installation of Hartzell Propeller Model PHC-G3YF-1RF/F7691 and spinner assembly D5732 or C4582. Issued 12/20/1994
SA09055SC Installation of Teledyne Continental Model IO-520-F engine modified under STC SE09054SC. Amended 11/4/1996
SA09132SC Installation of modified Teledyne Continental IO-550-F engine and Hartzell propeller model PHC-G3YF-1RF/F7691 with spinner assembly D5732 or C4582 or McCauley propeller model D3A34C401/90DFA-10 and spinner assembly D6594. Amended 11/4/1999
SA09168AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-650. Amended 3/22/1999
SA09267AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-720-20/30. Amended 3/19/1999
SA09269AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-722-20/30. Amended 4/23/1999
SA09276AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-723. Issued 10/6/1997
SA09321AC-D Installation of S-TEC System 30 alt altitude hold system. Issued 1/3/1998
SA09352SC Add exhaust pipe extension. Amended 6/1/1998
SA09400SC Installation of a McCauley Propeller system. Amended 11/4/1999
SA09423AC-D Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-781-40X/50X Issued 6/5/2000
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09491SC Installation of a low voltage warning system. Amended 5/3/2001
SA09500AC-D Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-792-40X/50X. Issued 6/27/2000
SA09530SC Installation of a modified Teledyne Continental O-470-U engine modified by STC SE8949SW to be designated O-470-U/TS and to be further modified by STC SE09531SC to change the carburation to accommodate the use of E-85 Ethanol fuel. Amended 6/7/2000
SA09546SC Installation of the Teledyne Continental O-470-R engine the McCauley 2A36C/90M-8 propeller and Cessna Engine Mount Part Number 0751001-13. Issued 5/5/1999
SA09964SC Installation of engine mount heat shields. Issued 11/7/2001
SA1-106 Gyro-stabilizer 69A107. Issued 
SA1-124 Lube oil filter BP55-1. Issued 
SA1-16 Federal F-300 autopilot. Issued 
SA1-188 Removal of right door right front seat right control column and right rear window (optional) and installation of Sky-Diver Jump Step and static line attachment. (180A LANDPLANES) Reissued 10/18/1995
SA1-212 Hole cut in lower skin and reinforced. Issued 
SA1-221 Gyro-stabilizer 69A124. Issued 
SA1-252 Safety gear Model A. Issued 
SA1-363 Installation of Edo Model 439-2705 amphibious floats. Reissued and Amended 7/31/1998
SA1-37 Installation of Tactair T-3 automatic pilot and optional installation of Tactair AH-1 altitude hold device (for use with Tactair T-3 autopilot). Reissued 8/7/1972
SA1-426 Auxiliary seat in baggage compartment. Reissued 10/25/2001
SA1-464 Installation of Edo models 439-2705 amphibious floats. (180 180A 180B 180C 180D SEAPLANE) Reissued and Amended 7/31/1998
SA1-519 Griswold lateralizer and heading lock. Amended 
SA1-576 External electrical power receptacle. Reissued 10/15/1974
SA1-611 Install 300 series dry vacuum pump conversion kits. Reissued 4/22/2003
SA1-612 Installation of Tactair T-101 autopilot and optional installation of Tactair T-201 autopilot accessory kit (for use with Tactair T-101 autopilot). Reissued 8/7/1972
SA1-622 Installation of Edo Model 249A2870 seaplane floats Reissued 7/31/1998
SA1-7 Gyro-stabilizer 69A116 on aircraft with serial numbers 32151 and up. Issued 1/1/1996
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
SA1004CE Install STOL kit. Amended 8/28/1985
SA1005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Issued 7/23/2002
SA10070SC Installation of Hartzell 3-bladed propeller. Issued 11/6/2002
SA10082SC Installation of Texas Skyways engine mount. Issued 10/9/2002
SA10126SC (1 OF 2) Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.  Amended 10/23/2003
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA102AL Shackle release at wing lift strut fittings right and left wings(seaplane only). Issued 1/1/1961
SA102SW Automatic pilot AK109 and lateral guidance radio coupler AK123. Issued 1/1/1960
SA10351SC Installation of decorative fiberglass fairing in accordance with Texas Skyways Inc. Master Drawing No. TSFG-100-1 dated November 18 2004 or later FAA approved revisions. Issued 2/4/2005
SA104CE Installation of Hoskins Supplemental Model B High Intensity Wing Tip Lights Model C Tail Light with or without Models 1 or 2 High Intensity Fuselage Lights. Reissued 9/30/2011
SA105NW Mounting and wiring for occasional installation and use of Barnes Engineering Company airborne fire spotter system. Issued 4/30/1974
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA108CE Continental O-470 Series engines modified for Bendix RSA5 fuel injection system. Issued 1/1/1961
SA10WE Arens Vernier type throttle control. Issued 1/1/1961
SA1101GL Installation of a Shadin Co. fuel flow indicating system. Reissued 6/8/2006
SA1109NW Installation of a sleeping bag compartment aft of the baggage compartment Issued 4/17/1981
SA110SW Removal of perforated cones from exhaust muffler. Issued 1/1/1960
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1157WE Installation of Roto-Master (Rajay) turbocharged Continental O-470-A J K L or R engine. Reissued 5/19/2000
SA115NW Modification of R.H. Door and the addition of a jump seat. Amended 4/30/1981
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA1190NW Installation of Teflon bushings with stainless steel inserts in elevator and rudder hinges Issued 2/27/1981
SA1198NW Installation of a Continental engine Hartzell or McCauley propeller Scott tailwheel Issued 10/10/1989
SA1211GL Install SAF-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA1218NW Installation of a Cessna model 180K landing gear assembly cowl deck brace a Cessna model 185 tail wheel assembly 8.50 X 6 (and smaller diameter) tires and a modified Cessna model 172 rear seat and seat belt attach points Issued 4/17/1981
SA121CE Nose and main gear wheel fairing(Jetstreams) using standard unaltered Cessna landing gear and nose gear fork for model and year using 500 x 5 nose and 600 x 6 main gear tires. Amended 3/1/1977
SA1231NW Installation of a Continental engine McCauley propeller Issued 5/13/1981
SA1247NW Installation of a redesigned instrument panel with center stack radios and a U shaped control yoke Issued 5/29/1981
SA1261WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1266NW Installation of a camera door P/N CA1010 Reissued 4/10/1995
SA1296SO Installation of an adjustable nine- inch trim tab on left aileron. Issued 11/13/1981
SA12WE Installation of fiberglass wing tips. Reissued 5/4/2010
SA1304GL Replace Cessna fuel cell drain vavle assembly P/N 84C with Safe Air Repair P/N SAR-2. Reissued 4/22/2005
SA1315WE Installation of Mixture Monitor (exhaust gas temperature probe gage and selector) in accordance with Delta Products Part Lists A-192 and A-193 or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9 1981 or later FAA approved revision and/or Drawing List MM-127 dated November 15 1981 or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29 1968 copy attached or later FAA approved revision. Reissued 4/15/2011
SA1345GL Install Egan Aviation 182 Wings onto Cessna Model 180H S/N 180252183. Issued 12/13/1988
SA1349CE Chrome-plated brake disc installation. Issued 8/22/1977
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA1371SW Wing leading cuff wing tips and upper surface flow fences. Amended 4/14/1983
SA1373WE Model 3000 floats. Amended 5/23/1967
SA13GL Installation of Cleveland wheel No. 40-97A and brake No. 30-63A. (140A S/N 13400 AND UP) Amended 4/1/1981
SA1412SO Remove drain plug Cessna Part Number MS20913-10 or MS20913-ID from the fuel selector valve and replace with CAV-110D (MT-1080) or CAV-110H-4D (CM-1080) in accordance with instructions dated January 12 2004 or later FAA revisions. (See limitations) Amended 3/17/2004
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1431WE Installation of rudder trim system. Amended 4/2/1978
SA1435WE Installation of drooped ailerons in flaps down mode recontoured wing leading edge except 180J and K actuated elevator trip system and installation of SC-100 stall warning system. (180 A B C D E F G H J K LANDPLANE FLOATPLANE AND AMPHIBIAN) Reissued 7/21/2005
SA1448SO Installation of replacement fuel cell assemblies. (SEE LIMITATIONS) Reissued 3/10/1995
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1455WE Installation of Brittain Industries Model CSA-1 Flight Control System Amended 9/12/1979
SA1473WE Installation of Brittain Model B2C Flight Control System. Reissued 10/20/1972
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)


Subscribe To Our Newsletter

Join our mailing list to receive the latest news and updates from our team.

You have Successfully Subscribed!