Cessna 185 E

Number of Active Aircraft: 272 Active- Map


Years Produced: 1965-72 This model 185 sported a more powerful engine making it much better fit to fly in and out of very small runways. It also was built for an additional 100 pounds of payload. However this performance did come at a price with a higher fuel burn.

Wikipedia Cessna 185 reference:

Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 1560 lbs
Max Weight 3300 lbs
Useful Load: 1740 lbs
Engine Name Continental IO-520-D
Engine Number 1
Horsepower 300 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 16900 ft
Max Fuel 65 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 145 kts
GPH (75% BHP): 17
MPG (75% BHP) 8.5
Range (75% BHP): 465 nm
Fuel Cost Per Seat Mile 0.12 $
Fuel Cost Per Hour 102 $
MPG per 1000 lbs of Payload 14.84
F-T (Speed^2/FuelBurn) 12.4 HP
F-T Payload 21.6 kts
MPH To HP: 4.8 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1290 ft

SA00005SE Installation of doubler on both left and right door posts. Issued 7/8/1993
SA00023SE Installation of modified control yoke and instrument panel. Amended 11/20/2002
SA00031WI Installation of flap and aileron gap seals. Issued 2/11/1993
SA00052NY Installation of wing tip extension. Issued 11/18/1993
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00064DE Installation of external cargo pod. Issued 11/24/1993
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
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
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
SA00206WI 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. (A185F thru S/N 18503683 and later airplanes originally equipped w/bladder fuel tanks) Reissued 5/3/2004
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
SA00214DE Installation of Turbo normalizer system. Reissued 10/16/1998
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00220NY Installation of Northstar Tech. Inc model M3 GPS Navigator. Issued 9/15/1994
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
SA00344WI Installation of Teledyne Continental Motors IO-550-D and McCauley D3A34C401/90DFA-6 propeller and associated changes. Reissued 9/22/2005
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
SA00412WI Installation of McCauley D3A34C401/90DFA -2 -4 -6 -8 -10 propeller with Teledyne Continental motors IO-550-D engines already installed and associated changes. Reissued 9/22/2005
SA00413WI Installation of McCauley Propeller D3A34C401/90DFA -2 -4 -6 -8 -10 on Models previously equipped with TCM IO-520-D engine. Reissued 9/22/2005
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
SA00478SE Replace existing horizontal stabilizer skins Issued 11/6/1997
SA00496SE Installation of Oregon Aircraft Design Engine Mount Heat Shields. Amended 12/20/2000
SA00501AT Installation of either a Hartzell 3-blade model PHC-C3YF-1RF/F8468A( )-6R or PHC-C3YF-1RF/F7691( ) propeller or McCauley 3-blade model D3A34C401/90DFA-10 or D3A34C401/90DFA-8 propeller and associated spinner assembly. Reissued 2/18/1999
SA00512SE Fabrication of a vortex generator system. Amended 5/14/1998
SA00640SE Installation of a McCauley D3A34C401 propeller hub with 90FDA-4 or -6 blades on the above model aircraft. Amended 11/23/1998
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
SA00697NY Installation of left-hand and right-hand EDO model 582-3430 floats. Issued 10/28/1997
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
SA00712CH Installation of Insight Avionics Strike Finder model SF 2000. Reissued 9/4/1997
SA00760SE Installation of glare shield. Reissued 5/20/2010
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
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
SA00843NY Aircraft fuel quantity transmitter replacement-from Stewart Warner Model 390 to Stewart Warner Model 385. Issued 5/28/1998
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
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
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
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
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
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
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
SA01272CH Installation of Wipaire Model 3450 amphibian/seaplane floats and Parts Kit No. W-PMA100. Issued 7/20/2000
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
SA01296WI Installation of MT-Propeller Model MTV-9-D/210-58 hydraulic 3-blade variable speed propeller or Model MTV-15-D/210-58 hydraulic 2-blade variable speed propeller.  Reissued 3/20/2007
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
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
SA01473SE (2 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01560WI-D Installation of the Honeywell KFD 840 Primary Flight Display System. );INSERT INTO stc_table VALUES ( REQUIRED DATA: AML No. 159-08325-0002 Revision - dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. Amended 7/22/2010
SA01573NY Installation of Seaplanes West Replacement Engine Mount. Amended 6/30/2003
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
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
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
SA01827AT Manufacture of Composite Engine Cowlings. Issued 2/10/1999
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
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
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
SA02110CH (PAGE 1) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02113AK 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
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
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 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
SA02244AK Fabrication and installation of Airglas Inc. Model LH4000 hydraulically retractable wheel skis. Issued 6/8/2005
SA02246LA Installation of a flap handle extension. Amended 11/16/2010
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
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
SA02299SE Installation of the Alaskan Bushwheel Inc. (ABI) Cessna Tail Spring Issued 12/18/2013
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
SA02361AK Installation of a firewall mounted battery tray and heat shield Issued 12/18/2009
SA02386AK Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems Reissued 11/4/2013
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
SA02416AK Installation of replacement engine exhaust stack assembly P/N C185PMCF-SCAR or C185PMCF-LCAR Issued 8/19/2013
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
SA02528CH-D Installation of the Hartzell propeller model HC-C3YF-1RF/F8468A-2R or HC-C3YF-1RF/F8468AR or PHC-C3YF-1RF/F8468A-2R or PHC-C3YF-1RF/F8468AR and HARTZELL C-3575-(P) spinner. Issued 6/18/2007
SA02547AT (PG 1) Installation of a Voice Alert System. Amended 8/28/2007
SA02655AT (1 OF 2) Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. Amended 9/1/2004
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
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
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
SA09018AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-596. Amended 2/2/2001
SA09192AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-650. Amended 4/25/2001
SA09268AC-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
SA09270AC-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
SA09277AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-723. Issued 10/6/1997
SA09322AC-D Installation of S-TEC system 30 alt altitude hold system. Issued 1/3/1998
SA09352SC Add exhaust pipe extension. Amended 6/1/1998
SA09424AC-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
SA09501AC-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
SA09960SC Installation of Teledyne Continental Motors IO-550 engine per Texas Skyways Inc. Drawing No. TSI-00-1002 Rev C dtd 10/5/01 or later FAA approved revision. Issued 10/10/2001
SA1-519 Griswold lateralizer and heading lock. Amended 
SA1-576 External electrical power receptacle. Reissued 10/15/1974
SA1-629 Install 300 series dry vacuum pump conversion kits. Amended 5/9/2001
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
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
SA1007NE Installation of Northstar M2 navigator and Northstar Model 8100A airborne global position system sensor. Amended 6/1/1993
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
SA1027NE Installation of Northstar M2 navigator and Model 8100A airborne global positioning system sensor. Amended 12/9/1992
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
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA1081WE B-4 flight control system. Reissued 10/1/1973
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA108SW Edo 289-2700 and 439-2705 amphibious floats. Issued 1/1/1961
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA111CE Retractable lifting handles Model H P/N 50-10. Issued 1/1/1960
SA1148SW Installation of aileron drooping Reissued 4/27/1984
SA1151NW Installation of North American Industries Inc. Model 135 pistol grip Amended 3/29/2002
SA115NW Modification of R.H. Door and the addition of a jump seat. Amended 4/30/1981
SA1221GL Installation of fuel quick drain at lower end of accumulator tank at fuselage station 8.12. Amended 5/23/1988
SA1227GL Install SAF-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA123CE Installation of Model B high intensity wing tip lights Model C tail lights with or without models 1 or 2 high intensity fuselage lights. Reissued 9/30/2011
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
SA1280NW Installation of a one-piece LP Aero Plastics Inc windshield (without the center stiffener) Issued 7/27/1981
SA1289GL Replace Cessna fuel cell drain valve assembly P/N 84C with Safe Air Repair P/N SAR-2. Reissued 4/22/2005
SA1298SO Installation of adjustable nine-inch trim tab on left aileron. Issued 11/13/1981
SA12WE Installation of fiberglass wing tips. Reissued 5/4/2010
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
SA1351CE 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
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1441WE Installation of drooped ailerons in flaps down mode recontoured wing leading edge (except A185F) stall fence flap actuated elevator trim system and installation of SC-100 stall warning system. (A185F LANDPLANE FLOATPLANE AMPHIBIAN SKIPLANE) Reissued 7/21/2005
SA1443NM Installation of a Hartzell HC-C3YF-1RF/F9587C-15R or HC-C3YF-1RF/ F9587C-17S propeller Hartzell C-3535-1() spinner governor and associated system on a Continental IO-520-D engine. (A185F LANDPLANE AND FLOATPLANE) Amended 5/15/1996
SA1449SO 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
SA1473GL Install shoulder harness and seat belt assembly. Amended 1/6/1994
SA1473WE Installation of Brittain Model B2C Flight Control System. Reissued 10/20/1972
SA1474SW Installation of MASA 1223000-7 and -8 wing tip. Reissued 9/5/1979
SA147CE Moni-Meters on aircraft equipped with King KY-90 KY-95 Narco Mark 4 or Mark 12 transceivers. Issued 1/1/1960
SA147SW Edo 429-2705 or 289-2700 amphibious floats. Issued 1/1/1960
SA1483NM Installation of Lycoming IO-540K L. P. and S series engine modified engine mount Harrison oil cooler Hartzell model AP18AV06-03 oil cooler Hartzell HC-C2YK-1BF/F8475R-2 propeller and associated systems Issued 3/29/1982
SA1495CE Installation of flap and aileron gap seals. Amended 2/24/2005
SA150NW Installation of flap gap seals. Amended 3/22/1994
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1522GL Installation of Teledyne Continental Motors IO-550-D engine McCauley D3A34C401/90DFA-10 propeller and associated changes. Amended 7/27/1995
SA152NW Installation of deck and glare shield (with or without instrument lights). Amended 5/21/1981
SA155NW Addition of baggage hatch to EDO 249-2870 628-2960 and628A2960 floats. Amended 9/4/1996
SA1568WE Installation of emergency fuel system. Issued 1/1/1960
SA1569GL Installation of Wipaire Model 4000 amphibian or seaplane floats. Amended 9/15/1995
SA1573CE-D Installation of KAP 100 single axis flight control system. (A185F S/N 18503154 AND ABOVE) Reissued 2/28/2000
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1588WE Installation of supplemental exterior flashing lights. Issued 1/30/1968
SA1601NM Installation of 8.50x6 6 ply aircraft tires Issued 4/19/1982
SA1603SO Installation of Snider speed kit. Amended 8/26/1996
SA1618GL Installation of on-board engine analyzer system. Issued 6/14/1991
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1635SO Installation of replacement fuel cell assemblies. (SEE LIMITATIONS) Reissued 3/10/1995
SA1643GL Installation of V-type or Y-type shoulder harness. (182 SERIES EXCEPT R182 & TR182) Amended 8/31/1995
SA164NW Installation of EDO-628-2960 sea- plane floats with Cessna cargo pack kit No. AK-185-23D cargo pack fairing rudder non-linear centering spring and ventral fin. Reissued 1/12/1983
SA1662CE Installation strut/wing and strut/fuselage fairings lightning hole covers and aerodynamic putty. Reissued 1/27/1993
SA1686WE Installation of Vibration Isolation Products (VIP) engine mount P/Ns VIP 50525-1 and VIP 50545-1 on various aircraft as shown on FAA Approved Model List (AML) No. SA1686WE. Amended 10/17/2002
SA169CE Install Wipline Model 3700 3800 or 3900 twin floats. (185 185A 185B 185C 185D 185E A185E FLOATPLANE CONFIGURATION ONLY) Amended 4/8/1991
SA172NW Installation of drooped type wing tips. Issued 4/14/1975
SA172WE Conversion of aircraft for parachute jumping and aerial photography operations. Issued 1/1/1960
SA1749WE Installation of Canadian Aircraft Products Series 3000D floats. Reissued 10/19/1994
SA1750NM Installation of Airesearch Model TE-0659 P/N C295001-0101 Turbocharger. Amended 5/16/2008
SA1754CE Installation of modified 300 hp. turbo-supercharged Continental TSIO-520-G-CS82 engine and D3A32C90/82NC-2 McCauley propeller. (A185F LANDPLANE FLOATPLANE AMPHIBIAN) Reissued 12/3/1991
SA17EA Installation of Tactair T-101 auto- pilot and optional installation of Tactair T-201 autopilot accessory kit (for use with Tactair T-101 autopilot). Reissued 8/7/1972
SA17NE Installation of EDO Model 696-3500 amphibious seaplane floats with Model 696-1200 attachment gear. Reissued and Amended 7/31/1998
SA1816NM Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4 1983 together with their FAA sealed Installation Instructions dated September 20 1982 or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6 1982 LAS 1013 dated October 5 1982 and LAS 1014 dated October 6 1982 or later FAA approved sealed revisions. Reissued 1/23/2004
SA182CH Installation of removable Telonics telemetry antennas. Reissued 5/4/1994
SA1830CE Installation of photo bubble in place of baggage door. Issued 1/16/1983
SA1883NM Installation of front row seats seat tracks and associated installation components. Amended 1/27/1986
SA1907NM Installation of Schneider Model SWS-4000C-15 Model SWS-4000C-19 or Model SWS-4000C-23 main wheel skis. Issued 1/4/1983
SA1911NM Installation of Schneider wheel skis 6-inch to 10-inch aluminum wheel adapters and 29x11.0-10 8-ply minimum tires on main landing gear. Issued 2/17/1983
SA1960SO Installation of Appalachian Accessories stainless steel brake rotor discs P/N 73-47 for use with EDO Model 597-2790 dual-wheel amphibious floats. Amended 1/14/1987
SA1971WE Installation of Model ARB-3 Automatic Downed Aircraft Marker( ADAM ). Amended 11/21/1969
SA1990WE Installation of Tritan Amphibious float model TA 3500. Amended 2/15/2001
SA199EA Installation of Tactair T-3 auto- pilot and optional installation of Tactair AH-1 altitude hold device(for use with Tactair T-3 autopilot). Reissued 8/7/1972
SA2-1178 Replacement of right front seat with stretcher. Amended 11/14/2001
SA2014WE Installation of Tritan Amphibious Floats Model TA 3500 Issued 10/15/1969
SA202WE Cessna 210 wing tip assemblies1223000-1 -2 and wing tip mounted navigation lights. Issued 1/1/1960
SA2067NM Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System Amended 7/11/2012
SA2091SO Installation of Appalachian Acces stainless steel brake discs P/N 73-47. Issued 4/9/1987
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2106NM Installation of Precise Flight Speedbrake System. Amended 11/7/2003
SA2108WE Installation of Madras Air Service wing tips. Amended 5/16/2000
SA2118NM Installation of a Lycoming TIO-540- J2BD or 72B engine AiResearch Model THO8A60 turbocharger Hartzell HC-C3YR-1RF/F7854 (three blade) propeller Hartzell Model F4-13 governor and associated systems. (185 185A 185B 185C 185D 185E A185E A185F LAND PLANE FLOATPLANE AMPHIBIAN) Amended 12/9/1992
SA213AL Fabrication of attaching and rigging parts for the installation of Airglas Engineering Co Inc model LW3600-180 single position or Model LW3600-180A two position fixed penetration wheel skis. Reissued 4/26/2000
SA213WE Full flow lube oil filter30409A with element 1A0235. Issued 1/1/1960
SA215SW L-2 autopilot. Issued 1/1/1960
SA2162NM Installation of the Precise Flight stand-by vacuum system (SVS) Amended 11/7/2003
SA2171SO Replacement of Cleveland brake discs P/N 164-15A or 164-115A with Appalachian stainless steel brake discs P/N 75-15A. Issued 9/25/1987
SA2189WE Installation of recontoured wing leading edge stall fences wing tips and positive aileron seals. (185 185A 185B 185C 185E LANDPLANE FLOATPLANE AND AMPHIBIAN) (185D SKIPLANE) Reissued 7/21/2005
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
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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