Cessna 172 C

Number of Active Aircraft: 427 Active- Map

Description:

889 were manufactured. Key changes included an optional child seat, floats and a key operated starter unit. Wikipedia Cessna 172 reference: Cessna 172 Guide:275
Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1325 lbs
Max Weight 2200 lbs
Useful Load: 875 lbs
Engine Name Continental O-300
Engine Number 1
Horsepower 145 HP
Never Exceed Speed: 139 kts
Stall speed: 45 kts
Service Ceiling: 15100 ft
Max Fuel 42 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 113 kts
GPH (75% BHP): 7
MPG (75% BHP) 16.1
Range (75% BHP): 589 nm
Fuel Cost Per Seat Mile 0.09 $
Fuel Cost Per Hour 42 $
MPG per 1000 lbs of Payload 14.13
F-T (Speed^2/FuelBurn) 18.2 HP
F-T Payload 15.9 kts
MPH To HP: 7.8 kts
T/O Roll - T/O over 50 FT OBST 825 ft / 1370 ft

SA00024NY Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Amended 10/3/2012
SA00033WI Installation of flap and aileron gap seaps. Issued 2/11/1993
SA00039LB Installation of an Ashtech AV-12 Global Positioning System and a Aero GPS Antenna. Reissued 11/5/1999
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
SA00087NY Installation of Cu-Sonde Meteorological Measurement/system models CS-1A or CS-1B and installation of Cu-Sonde Model CS-1B-RF with AIRDAT-9600. Reissued and Amended 8/22/1995
SA00103BO Installation of Weemax cabin air vent. Issued 6/16/1999
SA00147AT Installation of Type A sun visor. Amended 7/28/1993
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
SA00186AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00188AT Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-26A. Reissued 11/14/1994
SA00194AT Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-40. Reissued 11/14/1994
SA00194BO Installation of P/N 2042 Landing Gear Warning System for amphibian aircraft. Reissued 1/23/2009
SA00211AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/17/1994
SA00212AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/17/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
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
SA00261SE Installation of Lycoming O-320-E2D engines modified by STC SE00252SE O-320-D2G or O-320-D2J engine and McCauley 1C160/CTM 7557 or 1C160/DTM 7557 or 1A175/ETM (seaplane only) propeller. (Landplanes and Seaplanes) Amended 12/3/1998
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
SA00335LA Conversion of tricycle landing gear to tail wheel type (conventional) landing gear. (S/N 28058) Issued 1/8/1997
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
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
SA00455SE Modification of carburetor heat box. Issued 7/3/1997
SA00459WI Energy absorbing seat. Amended 1/28/1997
SA00461SE Install a Lycoming O-360 series engine and Hartzell McCauley or Sensenich propeller (See STC for specifications). Amended 10/24/2002
SA00465NY Installation of Meterological Measurement System Model A1MMS-10 with optional installation of Telemetry Module Model AIRDAT-9600. Amended 10/28/1998
SA00506WI Installation of a pallet assembly that houses a special mission camera and computer in the baggage area Issued 3/11/1997
SA00520WI Installation of engine mount gussets. Issued 5/13/1997
SA00545NY Installation of an Argus 5000/CE Moving Map Display. Issued 1/14/1997
SA00548AT Installation of camera hole. Issued 7/28/1994
SA00622DE Installation of John Deere AGRI Services Inc. JD3 Aerial Imaging System  Reissued 11/15/2007
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
SA00674CH Installation of Wipaire 2100 amphibian/seaplane floats. Amended 8/24/2005
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
SA00728SE  Installation of various models of the Continental IO360 Engine Amended 3/21/2013
SA00744DE Installation of Automatic Dependent Surveillance  Amended 3/28/2013
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
SA00795CH Installation of Baumann Model BF-2550 floats. Reissued 4/27/2005
SA00796SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft Amended 5/27/2004
SA00811WI Heat Air Induction System on above model. Issued 8/23/1999
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
SA00819SE Installation of Visual Instruments flap position indicating system. Issued 7/18/2000
SA00831SE Installation of vortex generators on wings and tail surfaces. Issued 8/4/2000
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
SA00865NY Installation of nose gear strut fairing. Amended 9/20/1999
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
SA00900CH Installation of Wipaire Model 2350 Amphibian/Seaplane Floats and McCauley Model 1A200/WFA propeller. Amended 9/28/2011
SA00910WI-D Installation of Bendix/King KLN 94 GPS (Global Positioning System) Navigation Receiver for IFR enroute and non-precision approach operations. Issued 11/1/2000
SA00919SE : Installation of vacuum stall warning system as either the primary or as a secondary stall warning system in accordance with drawings and instructions listed in AML SA00919SE. );INSERT INTO stc_table VALUES (  Issued 5/24/2001
SA00926WI Installation of MT-Propeller MTV-18-B/183-17 electric 3-blade constant speed propeller. Reissued 3/20/2007
SA00954SE (1 OF 2) Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. Amended 8/11/2003
SA01001SE Installation of 12 volt cabin power system for portable electronic devices in accordance with Olympic Aero Services Inc. Master Drawing List OAS-54-0001 Revision G dated September 26 2002 or later FAA approved revision. This system shall be maintained in accordance with Instructions for Continued Airworthiness Document OAS-54-23.1529 Revision B dated August 22 2001 or later FAA approved revision. Reissued 4/9/2012
SA01015SE Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. Amended 10/4/2012
SA01026CH Change maximum gross weight limit to 2250 lbs. (172N s/n 17267616) Issued 4/13/1999
SA01026SE (PAGE 2) Improved fuel gascolator assembly. Amended 12/19/2012
SA01032WI Installation of external aerodynamic Vortelator Kit on airplanes Amended 7/11/2008
SA01070WI-D Installation of Bendix/King KDR 510 VHF Data Link System. Issued 4/9/2002
SA01074WI Installation of McFarlane Aviation Flap Roller Assembly Service Kit MCSK100 on various Cessna single-engine aircraft. Cessna Service Bulletin SEB95-3 must be complied with before this STC is installed. Issued 4/22/2002
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
SA01080LA Installation of Accessory Power Receptable in accordance with FAA Approved Master Drawing List Document No. 172-APR-100 Rev IR dtd 8/15/00 or later FAA approved revision. Reissued 3/2/2001
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
SA01088SE Installation of Dynamic Propellers induction air inlet on carburetor air box. Issued 5/14/2002
SA01095WI Installation of Gomolzig C172R-606550 engine exhaust system silencer. Reissued 3/20/2007
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
SA01183AT Installation of a Cockpit glare shield. Issued 10/29/1996
SA01202LA Installation of Becker Avionics SAR DF-517 Search and Rescue Direction Finding System Reissued 2/13/2012
SA01204LA Installation of replacement wing tip fairing assembly. Issued 10/3/2001
SA01205WI-D (1 OF 2) Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. );INSERT INTO stc_table VALUES (  Amended 11/20/2007
SA01220WI Installation of hydraulically controlled variable pitch 3 blade MTV-12-B/183-17 propeller. Issued 4/5/2004
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
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
SA01265AT Installation of Composite Spinner Assemblies. Amended 10/13/2000
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
SA01289AT Manufacture of composite engine cowlings. Reissued 5/21/2007
SA01298SE Installation of interior trim parts. Reissued 5/20/2010
SA01303WI Installation of a Thielert TAE-125-01 aircraft diesel engine associated systems and gross weight changes. Amended 11/23/2009
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
SA01328LA Modification of right hand side door to provide an openable window. Reissued 3/30/2005
SA01330LA (PAGE 1) Installation of alternate avionics support assembly. Reissued 10/6/2010
SA01386NY Installation of Fibre Glass Reinforced Plastic Nacelle Fairing Trade Name Exhaust Fairing . Reissued 10/9/2002
SA01388SE Installation of 7-gallon or 15-gallon extended range wing fuel tanks manufactured and installed Amended 10/18/2007
SA01428LA Installation of CO Guardian Carbon Monoxide Detector Instrument. Issued 2/10/2003
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
SA01454SE Incorporation of a nylon sleeve on the carburetor heat cable housing to prevent abrasion of the cable Issued 9/20/2004
SA01456NY Installation of Technisonic Industries Ltd OSAT-100 Airborne Position/Data Communicator. Issued 1/31/2002
SA01473SE (2 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01531LA Installation of CO Guardian Remote Carbon Monoxide Detector Instrument. Issued 8/28/2003
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
SA01551AT Installation of a Lycoming O-360-A1-A engine and a Hartzell HC-C3YF-1RF/F7282 propeller. Reissued 7/14/1998
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
SA01626WI One Aircraft Only installation of a Teledyne Continental Motors IO-360-D engine with two-bladed McCauley constant speed propeller powerplant installation and fuel system modifications. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( Data Required: );INSERT INTO stc_table VALUES ( 1. A copy of this certificate and );INSERT INTO stc_table VALUES ( 2. Installation Drawing No. 210-172-001 Rev. D dated April 25 2011 and );INSERT INTO stc_table VALUES ( 3. Supplemental Airplane Flight Manual No. SAFM-17248124 dated April 25 2011 and );INSERT INTO stc_table VALUES ( 4. Instructions for Continued Airworthiness No. 210-172-002 Rev (-) dated April 25 2011 or );INSERT INTO stc_table VALUES ( later FAA approved revisions thereof. Issued 4/25/2011
SA01646SE Installation of vortex generators on wings horizontal and vertical tail surfaces. Issued 2/28/2006
SA01660SE Installation of interior fiberglass panels. Reissued 5/20/2010
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01679CH Install BRS-172 parachute recovery system. Amended 8/29/2012
SA01686AT Installation of a Lycoming Model O-360-A1A engine and a Hartzell model HC-C3YR-1RF/F7282. Issued 1/1/1961
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
SA01700LA Installation of AMSAFE Aviation Inflatable Restraint (AAIR) system. Issued 12/3/2004
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01768SE Install oil cooler system. Issued 6/8/2007
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01801AT For the Cessna 172 airplane models incorporating Lycoming O-320 engines: Modification of the standard exhaust system as documented in Laminar Flow Systems Installation Instructions Document Laminar Flow System Extractor Exhaust System Revision A dated November 20 1998 and Technical Drawing List Book No. PFS-B-800 dated November 16 1998 or per Power Flow Systems Inc. Installation Instructions Document PFS-0058-00 Rev. A dated October 5 2001 and Master Drawing List Report No. PFS-0032-00 Rev. IR dated August 10 2000 or later FAA approved revisions. );INSERT INTO stc_table VALUES ( For the Cessna 172 airplane models incorporating Lycoming O-320 O-360 0r IO-360 engines: );INSERT INTO stc_table VALUES ( Modify the standard exhaust system as document in Power Flow Systems Inc. Installation Instructions Document PFS-13250-00 Rev B dated December 9 2002 and Master Drawing list PFS-13240-00 Rev IR dated October 3 2002. Reissued 10/16/2003
SA01815CH Installation of Baumann Model BF2550A floats. For models 172I through 172P a gross weight of 2350 lbs. at a center of gravity range of plus 39.5 inches to plus 45.5 inches is approved. For models R172K and R172K with STCs SA1436CE and SA1437CE the maximum gross weight is limited to 2550 lbs. at a center og gravity range of plus 39.5 inches to plus 45.5 inches. Reissued 1/10/2005
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
SA01923LA Installation of the P-1000 Digital Electronic Tachometer. Issued 1/23/2007
SA01933LA (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01944CH (1 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004
SA01951NY-D Installation of Wulfsberg P-2000 and/or C-2000-RT-2000 transceiver system. Reissued 3/18/2005
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02006CH Installation of air conditioning system. Amended 12/20/2011
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
SA02033AT (PAGE 2) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008
SA02049SE Fabrication of Stene Aviation Inc. Wing Tip Part Numbers SA-0523565-29 and SA-0523565-30 Issued 2/2/2010
SA02069AK Fabrication and Installation of the Airglas PA32-206LA Nose Fork equipped with Goodyear 8.50 x 6 tires. Amended 6/5/2006
SA02072AK Installation of hourmeter airspeed switch. Amended 11/14/1997
SA02104AK Installation and fabrication of R & J Aircraft extended baggage compartment. Issued 3/4/1998
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
SA02138AT Installation of Lord Corporation nose wheel shimmy damper part number SE-1051-2/3. Amended 8/11/2006
SA02149AK Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. Reissued 5/17/2013
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02155AK Installation of Hartzell model HC-C2YR-1BF/F8477-4 propeller and Hartzell model C-1576 damper assembly. Reissued 1/15/2004
SA02186AK Installation of Hartzell HC-C2YR-1BF/F8477-4 or HC-C2YK-1BF/F8477-4 propeller and Hartzell model C1576 damper assembly. Reissued 6/16/2004
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
SA02228AT For model 172 airplanes with Lycoming O-360 engines per STC SA332GL or STC SA4428SW modification of standard exhaust system. For model 172 with Lycoming O-360 engines per STC SA647CE or STC SA1324CE modification of standard exhaust system. Amended 1/16/2001
SA02231AK Installation of Cleveland Main Wheels and Brakes. Reissued 3/17/2008
SA02236AT Installation of a Paravion (formerly FSI) Eagle Vision Camera System on the Model 172M (S/N 17262323) and a Spectrolab SX5 Search Light on the Model 172S (S/N 172S8566) both fuselage mounted in accordance with Aero Avionics Master Drawing List No. AA-C172-001 dated September 21 2000 or later FAA approved revision. Amended 4/17/2003
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
SA02248LA Installation of Sensor Pod and wiring for a passenger operated monitoring system Reissued 1/30/2014
SA02249SE Installation of a silicone rubber wingtip device intended as a provision for mounting battery powered devices such as strobes or air temperature sensor Amended 9/18/2013
SA02262SE Installation of split seam wing strut cuff as replacement parts for the strut fairings Issued 3/8/2013
SA02265SE Installation of a camera housing Amended 11/1/2013
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
SA02293AK (1 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02302SE Remove standard Scott 3200 tail wheel and fork and replace with a Gar-Aero-32 tail wheel fork 24 spacer and a 4.00 x 4 6 ply tire Issued 2/4/2014
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
SA02359AK-D Fabrication and installation of F. Atlee dodge Aircraft Services Cessna Tie-Down clamp  Issued 11/6/2009
SA02376AK Replacement of tricycle landing gear with conventional (tail-wheel) landing gear Issued 12/12/2010
SA02400AK Installation of Aerocet 2200 floats  Issued 9/17/2012
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
SA02419AT Manufacture of Composite Engine Cowlings Issued 11/9/2001
SA02427AT Installation of an Avia V503AP propeller in accordance with Turbine Design Inc. Installation Instructions Report No. 2000-008 original revision March 1 2000 or later FAA approved revision. Reissued 11/14/2003
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02437LA Installation of straight tail vertical stabilizer and rudder assembly Issued 12/14/2012
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
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
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
SA02725CH Installation of North American Surveillance Systems Strut Mount and Optional Cloud Cap Technologies TASE / TASE Dou Gimbals  Issued 5/29/2009
SA02738CH (PAGE 4) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
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
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03984AT Installation of a FreeFlight Systems Universal Access Transceiver - Automatic Dependent Surveillance  Issued 12/13/2012
SA09132AC-D Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-612 with optional autotrim. Amended 2/28/2001
SA09149SC Modification of nose gear fork P/N SK150-11 to the SK182-34 configuration. Amended 2/22/1996
SA09151AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-616 with Optional Autotrim System. Amended 10/12/2001
SA09152SC Installation of a wing mounted video camera VCR and associated equipment. Issued 1/31/1996
SA09156AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-633 with Optional Autotrim System. Amended 10/18/2001
SA09201AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-563 with Optional Autotrim System. Amended 2/1/2001
SA09202AC-D Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems Model ST-184-40/50. Issued 4/1/1997
SA09207AC-D Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems Model ST-671-20/30. Issued 5/12/1997
SA09208AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-671-20/30. Amended 9/23/1998
SA09213AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-673. Issued 5/16/1997
SA09214AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-673. Amended 9/25/1998
SA09224AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-685-20/30. Amended 9/10/1999
SA09228AC-D Installation of S-TEC System 30 ALT Altitude Hold System. Issued 6/4/1997
SA09237AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-674-20/30. Issued 6/16/1997
SA09278AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-675. Issued 10/10/1997
SA09350SC Approves Aircraft Publications Pilot Operating Handbook as an Airplane Flight Manual (AFM) for aircraft listed on FAA Approved Model List. Amended 11/28/1997
SA09352SC Add exhaust pipe extension. Amended 6/1/1998
SA09362SC Installation of a panel and radio lamp dimmer control system. Issued 7/24/1997
SA09370SC Installation of a 95-ampere alternator. Reissued 5/30/2012
SA09371SC Installation of a vapor cycle air conditioning system. Reissued 5/30/2012
SA09412AC-D Installation of S-TEC manual electric trim system Model ST-157 Issued 8/25/1999
SA09425AC-D Installation of S-TEC System 40X/50X Single and Two-Axis Automatic Flight Guidance Systems Model ST-868-40X/50X. Issued 3/17/2000
SA09426AC-D Installation of S-TEC System 40X/50X single and two axis automatic flight guidance systems Model ST-868-40X/50X. Issued 3/17/2000
SA09457SC Installation of a vapor-cycle air conditioning system. Reissued 5/17/2013
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09491SC Installation of a low voltage warning system. Amended 5/3/2001
SA09524AC-D Installation of S-TEC System 60 Pitch Stabilization System Model ST-060. Issued 3/25/2002
SA09526AC-D Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System Model ST-025. Issued 3/25/2002
SA1-116 Federal F-300 autopilot. Issued 
SA1-124 Lube oil filter BP55-1. Issued 
SA1-193 Conversion of aircraft for parachute jumping operations. Reissued 10/18/1995
SA1-219 Gyro-stabilizer 69A122. Issued 
SA1-252 Safety gear Model A. Issued 
SA1-426 Auxiliary seat in baggage compartment. Reissued 10/25/2001
SA1-438 Lycoming O-360-A1A engine and McCauley 2D36C14/78 KM-4 propeller with Woodward 210105 AA governor. Amended 
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
SA1-9 69A115 gyro-stabilizer. Issued 1/1/1961
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
SA1000EA Installation of Pee-Kay Model 2300 or B2300 (TSO-C27-2) seaplane floats. (172N SEAPLANE) Reissued 10/13/2000
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
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
SA1017NW Installation of a Nite Sign Inc Model II Aerial Advertising System Issued 9/5/1980
SA1018NE Installation of .187 in. thick windshield. Issued 10/16/1992
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
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
SA10406SC Installation of a McCauley Model 1A170E/JHA7660 propeller and new 6.00X6 6 ply main tires in accordance with Alamo Aerospace Master Drawing List 1000 dated December 6 2004 or later FAA approved revision. An increase in the takeoff and max-continuous power to 180 horsepower and an increase in the max gross weight to 2550 pounds in accordance with the Airplane Flight Manual Supplement dated May 6 2005 or later FAA approved revision.  Issued 5/6/2005
SA10555SC ONE-ONLY STC: Installation of Aluminum Rudder Pedals and Portable Union Aviation Hand Control on Serial Number 17281100. Issued 8/11/2006
SA105NW Mounting and wiring for occasional installation and use of Barnes Engineering Company airborne fire spotter system. Issued 4/30/1974
SA1078WE Installation of Franklin 6A-335-B engine with McCauley 2A31C/84S-6 propeller using EDO 89-2000 floats. (172B 172C 172D 172E 172F 172G LAND OR SEAPLANE) Reissued 7/19/2000
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
SA109SW Automatic pilot AK106. Issued 1/1/1961
SA10WE Arens Vernier type throttle control. Issued 1/1/1961
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1119NW Installation of a Lycoming O-320-E2D engine and associated systems. Amended 4/10/1981
SA1124GL Installation of a Shadin Co. fuel flow indicating system. Reissued 6/8/2006
SA1150NW Installation of a 1976 Cessna 172 wing an updated right wing leading edge late model 172 dorsal fin and later model 172 cowl Issued 12/24/1980
SA115NW Modification of R.H. Door and the addition of a jump seat. Amended 4/30/1981
SA1168SO Installation of Aqua Model 2200 floats. Amended 8/15/2001
SA116EA Installation of Fram Part flow Lube oil filter model PB 55-1. Amended 9/11/1963
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA117EA Flow lube oil filter PB 55-1. Amended 9/11/1967
SA1191NW Installation of Edo seaplane floats Issued 3/11/1981
SA1196GL Install SAF-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA1211EA Installation of EPA portable enviro-pod with Tensor-Hasselblad camera configuration. Reissued and Amended 2/1/1982
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
SA1221SO Fabrication and installation of wheel fairings. Reissued 7/17/1989
SA1221SW Mitchell automatic flight system AK312 consisting of Century I with optional omni tracker. Reissued 7/9/1984
SA1225CE Installation of Lycoming O-320-E2D/ STC SE1226CE or O-320-D2G engine and McCauley 1C160/CTM 7557 or 1C160/DTM 7557 propeller Reissued 1/25/1996
SA124EA Shur-Vent fuel tank filler cap. Issued 1/1/1960
SA1253NW Installation of a Cee Bailey (one-piece) plexiglass windshield Issued 6/8/1981
SA1258EA Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584) Amended 4/11/1983
SA1261WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1279NW Installation of a Harrison Model AP07A006-03 oil cooler and associated parts on a Continental O-300-A engine Issued 7/27/1981
SA1294SO 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
SA1308WE Installation of Brittain Model CSA-1 stability Augmentation System.  Issued 1/1/1960
SA1311CE Chrome plated brake disc installation. Amended 6/20/1977
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
SA1324CE Installation of Lycoming O-360-A1A engine and Hartzell HC-C2YK-1B/7666A-2 propeller. Issued 5/1/1977
SA1334WE Installation of Franklin 6A-350-C2 engine and McCauley 2A31C/84S-6 propeller using Columbia Marine Inc. Kit No. 105. Reissued 7/19/2000
SA1342GL Installation of Porsche Model PFM3200/NO3 engine and Hartzell Model BHC-JTYF-1C/B7421 propeller. Issued 12/2/1988
SA1356GL Installation of Lycoming 0-320-D2J -D2G or -D1A. Reissued 11/1/2005
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
SA1395SO Remove drain plug Cessna Part Number MS20913-10 or MS20913-1D from the fuel selector valve and replace with Part Number CAV-110D (MT-1072) or CAV-110H-4D (CM-1072) in accordance with installation instructions dated January 12 2004 or later FAA approved revision. See limitations. Amended 3/17/2004
SA1396SO Remove drain plug Cessna Part Number AN814-3DL from the fuel selector valve and replace with CAV-180 (MT-1072-77) or CAV-180H-4 (CM-172-77) in accordance with instructions dated January 12 2004 or later FAA revisions. (*Model: C-172N Serial Nos.: 17261445 17267585 through 17269309 (1977 Model) 17261578 17269310 through 17271034 (1978 Model) (Except 17270050) 17271035 through 17272884 (1979 Model) 17270050 17272885 through 17274009 (1980 Model)) Amended 3/17/2004
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)