Cessna 170 A-B

Number of Active Aircraft: 2421 Active- Map

Description:

The 170 was an extension of the 140 program in some ways even though they do have a different type certificate. It included room for 4 passengers and a much more powerful engine the Continental O-300. The first 170 had a metal fuselage and fabric covered wings. Supported by a "V" strut common on the 140's. The 170 A went to an all metal aircraft instead of fabric wings. It also removed the "V" strut, and changed the shape of the tail.

The 170 B model, built upon the military version of the 170 and included fowler flaps that were effective at improving the aircraft's low speed performance. It also included additional modification to the tail.

Wikipedia Cessna 170 reference:

758
Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1220 lbs
Max Weight 2200 lbs
Useful Load: 980 lbs
Engine Name Continental O-300
Engine Number 1
Horsepower 145 HP
Never Exceed Speed: 139 kts
Stall speed: 0 kts
Service Ceiling: 14000 ft
Max Fuel 37 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 114 kts
GPH (75% BHP): 9.6
MPG (75% BHP) 11.9
Range (75% BHP): 359 nm
Fuel Cost Per Seat Mile 0.13 $
Fuel Cost Per Hour 57.6 $
MPG per 1000 lbs of Payload 11.64
F-T (Speed^2/FuelBurn) 13.5 HP
F-T Payload 13.2 kts
MPH To HP: 7.9 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1820 ft

SA00030WI Installation of flap and aileron gap seals. Issued 2/11/1993
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
SA00103BO Installation of Weemax cabin air vent. Issued 6/16/1999
SA00130SO Installation of Lycoming O-360-A1D engine and McCauley 1A200/FA8242 fixed pitch propeller. This ONE-ONLY STC is applicable to this particular aircraft ONLY. Issued 1/3/2001
SA00158SE Installation of Hartzell HC-C3YR-1RF/F7282 PROPELLER Hartzell propeller govenor P/N F2-7A/3949W and Hartzell spinner P/N A2295-1P. Issued 11/22/1994
SA00161BO (1 OF 3) Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00173BO Installation of Cessna 180 landing gear springs 0741001-1 (left) /0741001-2 (right) or 0741001-3 (left) / 9741001-4 (right) or 0741001-5 (left) / 0741001-6 (right). Issued 7/16/2003
SA00188AT Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-26A. Reissued 11/14/1994
SA00189BO Installation of landing gear axles (P/N 1441003-1). Issued 12/30/2003
SA00202NY Installation of alternator system on Cessna170 170A & 170B with Continental engine C145-2 and O-300-A. Issued 7/15/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
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
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
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
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00433 Installation of Airwolf remote mounted engine oil filter Model AFC-500 or AFC-600 on multi engine fixed wing light aircraft incorporating Franklin reciprocating engines of 450 horsepower or less. (with Franklin engines) Amended 5/7/1997
SA00433NY Installation of Airwolf remote mounted engine oil filter model AFC-500 or AFC-600 on multi engine fixed wing light aircraft incorporating Franklin reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00436NY Installation of steel main landing gear wheel axle (Cessna P/N 1441003-1). Issued 5/14/1996
SA00461SE Install a Lycoming O-360 series engine and Hartzell McCauley or Sensenich propeller (See STC for specifications). Amended 10/24/2002
SA00478CH (PAGE 1) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00485SE Installation of Teledyne Continental IO-360A engine and McCauley D2A34C57/76C propeller. Issued 11/24/1997
SA00648SE Fabrication of R.M.D. Aircraft Lighting Inc. wing-tip and landing light Kit No. 00190-C. Issued 11/30/1998
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
SA00680SE (4 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
SA00728SE  Installation of various models of the Continental IO360 Engine Amended 3/21/2013
SA00760SE Installation of glare shield. Reissued 5/20/2010
SA00780SE (PAGE 1) 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
SA00792SE : Modify Cessna flap handle in accordance with Shorten Cessna 170B Flap Handle document #170-2-1 Installation Instructions Revision Original dated March 18 2000 or later FAA approved revision. Issued 3/28/2000
SA00804CH Installation of Wipaire Model 2100 amphibian floats. Reissued and Amended 1/3/2000
SA00812CH Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. Reissued 6/30/2006
SA00832SE Installation of vortex generators on wings and tail surfaces. Issued 8/4/2000
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
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
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
SA01107SE RMD Aircraft Lighting high intensity discharge wingtip light manufactured Amended 4/2/2003
SA01111CH Installation of Textron Lycoming 180 hp models: O-360-A1A -A1C -A1F -A1G -A1H -A1P -C1A -C1C -C1E -C1F -C1G with Hartzell propeller HC-C2YR-1BF/F8477-4 Hartzell damper assembly and Hartzell spinners. Reissued 10/11/2000
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
SA01139CH Installation of W.D. Davis V.I.C.C.L. Cessna Cowl Latch. Reissued 1/19/2010
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
SA01214SE Fabrication of Steve s Aircraft Fuel Vent System. Issued 5/12/2003
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01233SE Manufacture of Alaskan Bushwheel Inc. (ABI) tail wheel and fork assembly per ABI Document ABI-3200B Revision A dated April 28 2005 or later FAA approved revision.  Amended 5/22/2012
SA01240SE (2 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
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
SA01388SE Installation of 7-gallon or 15-gallon extended range wing fuel tanks manufactured and installed Amended 10/18/2007
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
SA01499SE Remove a Hartzell model HC-C2YR-1B/7666-2 propeller on the above model aircraft and install a McCauly model B3D36C424/74SA-0 propeller Issued 1/18/2005
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01695SE (1 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
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
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01814CH Replace Cessna S-43 fabric attachment clips with AD42ABSLF rivets in accordance with the Instructions and Procedures as listed on AML No. SA01814CH or later FAA Approved revisions. Amended 1/11/2012
SA01833SE Installation of Cessna 175 wings on a Cessna 170B fuselage Issued 5/5/2008
SA01837SE Installation of Teledyne Continental O-300-B engine with approved propeller and accessories per A-799 Type Certificate Data Sheet . Reissued 5/7/2008
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
SA01911SE Installation of vortex generators on the wings and horizontal tail surfaces of the above model aircraft . Issued 9/25/2008
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 (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
SA01949CH Installation of C & D Associates combustion heater kit 12. Issued 3/23/2004
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
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
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
SA02034NY Installation of an additional 12.5-gallon fuel tank in the left wing. Limited to installation on Cessna 170 serial number 18457 ONLY. Issued 12/14/2004
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
SA02103AK Installation and fabrication of R & J Aircraft extended bagage compartment. Issued 3/4/1998
SA02106AK Installation of Lycoming O-360 series engine and Sensenich M76EMM propeller. Reissued 11/11/2003
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
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
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02155AK Installation of Hartzell model HC-C2YR-1BF/F8477-4 propeller and Hartzell model C-1576 damper assembly. Reissued 1/15/2004
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
SA02245CH Installation of a MT-Propeller model MTV-15-() propeller and P-237-12 or P-277-B spinner assembly  Amended 5/1/2008
SA02246LA Installation of a flap handle extension. Amended 11/16/2010
SA02268CH (PAGE 1) 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
SA02282AK Installation of Lycoming IO-360 (200 or 180 hp) engine and associated powerplant components including propeller modified exhaust baffling cowling modifications. Amended 4/19/2010
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02286AT Data pertaining to this modification are considered to be inadequate for duplication in other aircraft. This approval is limited to the installation made in Cessna 170 B Serial No. 26539 only. Reissued 12/8/2004
SA02293AK (2 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02321AK Installation of EDO 89-2000 floats modified Issued 8/29/2008
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
SA02365AK Manufacture and installation of a carbon composite engine cowling Reissued 3/4/2010
SA02374AK Installation of Lycoming Engine Model IO-360-A1A MTV-15-B/210-58 propeller Custom Aircraft engine exhaust collector system and other engine fuel system and cowling modifications. Issued 5/24/2010
SA02400AK Installation of Aerocet 2200 floats  Issued 9/17/2012
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02446CH Installation of the Courtesy Light Kit. Issued 6/25/2007
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
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
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
SA02854CH Installation of Baumann Floats LLC models BF2550A amphibious floats Issued 6/23/2010
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09273SC Installation of Terra by Trimble TMA 350D audio control panel with integrated marker beacon receiver and intercom system Terra by Trimble TX 760D VHF communications transceiver and Terra by Trimble TRT 250D transponder. Reissued 12/21/2001
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09491SC Installation of a low voltage warning system. Amended 5/3/2001
SA1-107 69A103 gyro stabilizer. Issued 
SA1-13 Recovering of wings with metal except ailerons and flaps. 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
SA1-240 Lycoming O-435-C engine and Hartzell HC-12X20-8D/8433-6 or HC-12X20-5C/8433-6 propellers. Issued 
SA1-245 Lycoming O-340-A1A engine and Hartzell HC-82XL-1D/8433-12 propeller on aircraft with Edo89-2000 floats. Issued 
SA1-252 Safety gear Model A. Issued 
SA1-316 Dart I-M turn control unit. Issued 
SA1-416 Lube oil filter. Amended 9/11/1967
SA1-426 Auxiliary seat in baggage compartment. Reissued 10/25/2001
SA1-516 Griswold lateralizer and heading lock. Amended 
SA1-545 External electrical power receptacle. Reissued 10/15/1974
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
SA1-647 Installation of leading edge landing lights (2) as a unit outboard of structure. Reissued 9/5/2007
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
SA10077SC Installation of push-button starter system. Amended 4/26/2005
SA1008WE Installation of Poly-Fiber covering material. Reissued 5/27/2003
SA1011GL Surrendered and incorporated into STC SA00478CH. Surrendered 6/14/2002
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
SA1023NE Installationof replacement windshields Issued 11/10/1992
SA1042NW Installation of a Continental engine and a McCauley propeller Issued 1/23/1981
SA1048NW Installation of a Franklin 6A-335-B 6A350-C1R or -C2 engine McCauley 2A31C21/84S-4 to -8 2A31C21/84S-4 -6 or-8 2A34C22/84SF-4 -6 -8 -10 2A34C201/90DA (88 inch to 76-inch range) or Hartzell HC-C2YF-1BF/F8459-4 to -8 and associated systems. Amended 1/6/2000
SA1073CE Installation of wing leading edge cuffs Cessna drooped wing tips stall fences and aileron gap seals. Reissued 4/24/1979
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA10921SC Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators Issued 11/10/2008
SA111NW Installation of McCauley 1A175-DM propeller with Cessna 0550162 spinner on Continental C-145 series and O-300 series engines. Amended 2/23/1979
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
SA1209GL Install SAF-T-STOP auxiliary seat stop devices. Reissued 6/15/2012
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
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
SA1350WE Replace existing fabric on wings fuselage empennage and/or control surfaces with fiberglass cloth. Reissued 3/6/1969
SA1351WE (PG 1) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983
SA135CE Installation of Lycoming O-320-A1A A1B A3A A3B or Lycoming O-320-B1A B1B B3A B3B engine Hartzell HC-82X or HC-A2X series propellers with 7636D-4 blades and Woodward Model 210080 Governor. );INSERT INTO stc_table VALUES ( Data required: Doyn drawing 2000 dated February 21 1063 and Doyn installation instructions dated February 21 1963. );INSERT INTO stc_table VALUES (  Reissued 7/14/2011
SA1371SW Wing leading cuff wing tips and upper surface flow fences. Amended 4/14/1983
SA13GL Installation of Cleveland wheel No. 40-97A and brake No. 30-63A. (140A S/N 13400 AND UP) Amended 4/1/1981
SA1417SW Mitchell automatic flight system AK358 consisting of Century I auto- pilot with optional omni tracker. Reissued 7/10/1984
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1455WE Installation of Brittain Industries Model CSA-1 Flight Control System Amended 9/12/1979
SA1467NM Installation of a new instrument panel and associated wiring Amended 8/26/1982
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
SA1490CE 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
SA1517GL Install Aero Fabricators shoulder harness and seat belt assembly. Issued 8/31/1990
SA1526GL Install Woychik retractable lifting handles Model H. Issued 10/17/1990
SA152NW Installation of deck and glare shield (with or without instrument lights). Amended 5/21/1981
SA1570NM Installation of Jensen aircraft fuel valve plug No. 011-4. Reissued 1/29/1999
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
SA158CE Cessna wing tips and attached lights 1223000-1 left 1223000-2 right tips and 1423006-12 left 0423006-13 right lights or an eqivalent. Issued 1/1/1960
SA15CE Dry vacuum pump and vacuum system113A6. Issued 1/1/1960
SA1614WE Installation of one 12-gallon auxiliary fuel tank in each outboard wing panel. Amended 12/6/2006
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1643GL Installation of V-type or Y-type shoulder harness. (182 SERIES EXCEPT R182 & TR182) Amended 8/31/1995
SA1664CE Installation strut/wing and strut/fuselage fairings lightning hole covers and aerodynamic putty. Reissued 1/27/1993
SA170CH Install a control yoke and instrument panel. Amended 7/1/2009
SA172NW Installation of drooped type wing tips. Issued 4/14/1975
SA175EA Installation of wing struts modified to include Wings With Springs Model200 hydraulic-pneumatic shock absorbers and associated airframe modifications. Amended 8/17/1977
SA1909NM 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 2/22/1983
SA1916NM Installation of Schneider Model SWS-4000C-15 main wheel skis. Issued 2/11/1983
SA196NW Installation of blown bubble one- piece clear plexiglass windshield. Issued 7/10/1975
SA1971WE Installation of Model ARB-3 Automatic Downed Aircraft Marker( ADAM ). Amended 11/21/1969
SA2-1178 Replacement of right front seat with stretcher. Amended 11/14/2001
SA2-1533 Installation of windshield wiper. Reissued 1/31/1997
SA2-224 Windshield manufactured in accordance with Luminous Plastics Inc. Drawing LP-306. Reissued 4/9/1979
SA2-289 Installation of electronic equipment rack. Reissued 12/1/1999
SA2-952 Installation of fiberglass covering. Reissued 9/10/1996
SA2019CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON+MON)/2. Amended 6/23/1992
SA2067NM Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System Amended 7/11/2012
SA2083SO Installation of a Sensenich Model76 EM8 propeller and Gulfstream spinner assembly. Issued 4/8/1987
SA2092NM Installation of a Continental O-300-D engine and McCauley 1A175/SFC 8043 propeller and spinner assembly Issued 5/6/1983
SA2100WE Installation of contoured wing leading edge and aileron gap cover. (170B LANDPLANE ONLY NORMAL & UTILITY CATEGORY) Reissued 5/6/2005
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA210GL Installation of Great Lakes Aero Products windshield P/Ns W-2055 W/T-2055 or W/G-2055. Amended 8/25/2008
SA2162NM Installation of the Precise Flight stand-by vacuum system (SVS) Amended 11/7/2003
SA2178NM Installation of a Lycoming 10-360-B1E engine Hartzell HC-C2YK-1BF/F7666A-4Q and Avcon Inc. Spinner Assembly No. 67790 Reissued 3/27/2012
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA21NW Installation of a 70 pound baggage compartment in either or both EDO 89-2000 89A-2000 or 689-2130 floats Amended 9/25/2009
SA220SO Tow bar release mechanism and safety tow link. Reissued 10/3/2011
SA224AL Installation of L-2500A or L-3000 skis. Issued 1/1/1960
SA2256WE Installation of leading edge cuff on each wing. Reissued 1/21/2010
SA2280CE Installation of aileron and/or flap gap seals. Amended 10/1/1993
SA2296SO Replacement of Cleveland brake discs P/N 164-26A or 164-126A with Appalachian Accessories stainless steel brake discs P/N 75-27. Issued 4/18/1988
SA2333NM Installation of hydraulic ski-brake assembly. Issued 2/14/1986
SA2345NM Installation of SWS-11000 Tundra tires wheels and hubs. Issued 8/29/1986
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA235SO Recovering of wings with .020 alclad 2024-T3 aluminum. Issued 1/1/1960
SA2362NM Installation of a Lycoming 0-360-A1F6D engine McCauley BeD34C207/78TCA-0 propeller flap gap seals and aileron gap seals and associated systems.  Issued 2/15/1984
SA236WE Cessna 210 wing tips 12230000-1 and -2. Issued 1/1/1961
SA2382NM Installation of Aileron and Flap Gap Seals. Amended 7/15/2003
SA238SW Installation of cargo door. Reissued 3/9/1987
SA23GL Installation of wheel replacement skis Model M2000 M3000. Amended 3/1/1990
SA2443WE Installation of the McCauley 1A175-DM-8040 propeller on Cessna 170B aircraft with Continental O-300 engines Issued 12/10/1971
SA2454WE Installation of Madras wing tips. (170B NORMAL CATEGORY) Amended 2/21/1973
SA2472WE Installation of high intnesity anti-collision light system Issued 2/9/1972
SA2516CE Installation of replacement wing tips. Issued 7/31/1989
SA2538NM Installation of 60 amp alternator and associated installations. Issued 11/20/1984
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA256NW Installation of aileron gap seals.  Amended 4/12/1993
SA2586NM (PAGE 2) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA268CE Installation of tow hitch assembly. Issued 1/1/1960
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA280NW Installation of an instrumentation boom Issued 4/2/1976
SA2832SO Installation of a combination radio/throttle/gust lock. Amended 12/3/2001
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2851CE Installation of wheel fairings. Amended 11/4/1992
SA2851SW Leading edge cuffs stall fences aileron seals wing tips. Reissued 6/6/1980
SA2912NM Installation of a Continental IO-360-C engine McCauley 1B235/DFC7846 propeller Maule fuel reservoir tank and fuel shut-off valve Continental C-145 heat exhchanger Cessna R172K engine mount Cessna 337 exhaust system electric fuel pump and relocated the fuel tank vents and battery Issued 3/20/1985
SA2918NM Attach a casting to landing gear fuselage attach angles above main landing gear legs. Amended 9/14/1987
SA293NW Installation of Franklin 6A-350-C1 or 6A-350-C2 engines Hartzell HC-C2YF-1BF/F8459A -4 to -8 HC-C2YF-1BF/F8459A-4Q to -8Q or McCauley 2A31C21/84S-4 to -8 propellers in accordance with Seaplane Flying Inc. Assembly and Installation Instructions SF 20690 SF20821 or SF 20820 on Cessna Models 170A 170B 172 172A 172B through P 175 175A 175B and 175C as defined in AML. );INSERT INTO stc_table VALUES ( 2.) Installation of Franklin 6A-350-C1R engines Hartzell HC-C2YF-1BF/F8459A-4 to -8 HC-C2YF-1BF/F8459-4Q to -8 McCauley 2A31C21/84S-4 to -8 or 2A34C201/90DA-10 to -14 propellers in accordance with Seaplane Flying Inc. Assembly and Installation Instructions SF 20690 on Cessna Models 170A 170B (Serial Numbers 20267 to 26504) as defined in AML. Amended 4/21/2011
SA2960NM Install stay put (seat position locking device). Amended 3/14/1986
SA3-13 Install 170 hp Lycoming O-340-A1A engine and Hartzell HC-82XL-1DB/8433-12 propeller according to Doyn data listed on Engineering Releases 100 (3/22/58) 1010 (3/16/57) 1011 (8/28/57) 1012 (7/15/57) 1014 (3/30/57) 1050 (7/13/57) 1051 (& DCN 1 12/10/57) 1052 (7/19/57) 1053 (7/19/57) 1099 (3/22/58) and Instructions (2 sheets undated) Data required for parts manufacture: As listed on Engineering Releases 1001 (1/18/57) 1002 (12/21/57) 1003 (5/1/57) 1004 (7/13/57) 1005 (7/12/57) 1006 (3/30/57) 1007 (4/12/57) 1008 (2/27/57) 1009 (10/23/57) 1015 (2/25/56). Reissued 7/14/2011
SA3-159 C-3000 main and AWT 2500A or CT-3000 tail wheel ski. Issued 1/1/1960
SA3-329 C-3000 main ski and AWT 2500A tail wheel ski. Issued 1/1/1960
SA3-333 Installation of Doyn fiberglass wheel fairings. Reissued 8/16/2011
SA3-339 C-3000 wheel ski on airplanes having a cross-wind wheel utilizing a 6.00-6 tire. Issued 1/1/1960
SA3-423 Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels. Amended 4/16/2010
SA3-451 Speed kit. Reissued 1/27/1993
SA3-468 CF-3000 main wheel skis and AWT2500A or CT-3000 tail wheel ski. Issued 1/1/1960
SA3-53 Model 3000 main and Model 1000 tail skis. Issued 1/1/1960
SA3-672 Installation of Lycoming O-360-A1A A1D or B1B engine with McCauley 2D36C14-X/78KM-4 propeller or Lycoming O-360-A1A and A1D engines with Hartzell HC-C2YK-1A/7666A-2 propeller. Data required: Doyn Aircraft Inc. Drawings: 1000 1005 Rev. C 1006 Rev. C 1009 1010 Rev. A 1011 1012 Rev. A 1013 1014 1015 1016 1099 1100 Rev. B 1101 Rev. A 1102 1103 Rev. A 1104 1107 1150. Drawing Changes Notices: 1005-5A 1006-8A 1006-6 1009-2A 1199-1A 1199-2A and 1199-3A. );INSERT INTO stc_table VALUES (  Reissued 7/14/2011
SA3-695 Dacron fabric on wings. Issued 1/1/1960
SA3-75 Grimes rotating anti-collision light D-7080-1-12. Issued 1/1/1960
SA301NW Installation of a larger electrical generating system with additional circuit breakers per AVCON Industries Inc. Drawing 17005A and installation of a one piece windshield Issued 5/18/1976
SA307NW Installation of a 1968 Cessna Model 172 airframe (forward of Station 27) and engine cowling l Cessna Model 172 AVCON conversion power-pac consisting of a Lycoming O-360-A1A engine Cessna 172 engine mount (P/N 0551017-1) Hartzell HC-C2YK-1F/7666A-2 propeller carburetor air box and nose cowling and a Cessna Model 172 baggage door assembly Amended 5/5/1979
SA308EA (1 OF 2) Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) Amended 11/20/1978
SA3147SO Installation of aileron and flap gap seals. Reissued 1/23/2012
SA316SO Carburetor ice detector. Amended 10/5/1966
SA318WE Torso tank 61900 or 64200. Amended 10/18/1965
SA3203SO Replacement of Cleveland brake disks P/N 164-26A and/or 164-126A with Appalachian Accessories stainless steel brake disks P/N 75-27. Reissued 9/29/1995
SA325GL Installation of fuel tank caps. Issued 7/16/1979
SA3318WE Installation of flap gap closures. (170B LANDPLANE ONLY NORMAL & UTILITY CATEGORY) Issued 1/5/1977
SA331CE New base instrument panel incorporating artificial horizon. Issued 1/1/1960
SA3423 Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels. Amended 11/18/2009
SA342NW Installation of Hartzell HC-C2YF-1FB/F8459-6 propeller on a Franklin 6A-350-C2 engine and Edo 248-2440 floats Issued 9/17/1976
SA34CE Tow hitch assembly. Issued 1/1/1960
SA34NW Installation of CEE Bailey windshield Item No 36J Issued 3/21/1973
SA351WE Pneumatic pitch assist PC-1. Reissued 10/1/1973
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3546NM Installation of relocated battery box. Issued 12/4/1986
SA3547NM Installation of baggage door. Reissued 3/15/1993
SA3548NM Installation of one-piece windshield. Issued 12/4/1986
SA356CH Installation of seaplane safety covers. Issued 5/22/1995
SA35NW Installation of CEE Bailey windshield Item No 36J Issued 3/21/1973
SA360EA Installation of Franklin Engine Co Inc Model 6A-335-B engine with McCauley 2A31C21/84S-8 propeller and new engine mount and associated components Amended 6/19/1970
SA3689NM Cockpit sun visor installation. Reissued 3/24/2003
SA3715WE Installation of vertical tail floodlight. Reissued 2/28/1980
SA3735NM Installation of inflatable door seal. Issued 9/9/1987
SA3797WE Installation of Elano P/N099001-063 F or later FAA approved revision muffler in lieu of original Avcon muffler. (170B LANDPLANE ONLY NORMAL CATEGORY) Reissued 3/15/1993
SA3814NM Installation of BAS Inc. tail pull handle in the aft fuselage. Amended 12/2/2010
AirFrame
Fusulage Construction
Airframe Material
Number of Doors
Wing
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
--Aileron
Aileron Type
Aileron Trim
Aileron Control System
--Flap
Flap Type
Wing Flap Actuation
Empennage
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
Retractable
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Cabin
Instrument Panel
Flight Control
Number of Seats
Heating
Window Defrost
Cooling
Profiles
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Engine
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Geared
Cooled
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller
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
Limitations
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)