Cessna 150 H-J-K

Number of Active Aircraft: 2297 Active- Map

Audries Certified

Description:

In 1967 the H model was introduced and was very similar to the previous models, the only changes were improved legroom and a flap switch outfitted for yoke operation. 2,007 of the H model were produced. The J model introduced a new starter system, slightly less reliable than the pull-style and more expensive to fix, it did have a more automotive function to it.

1714 were produced. The 150 K included the first introduction of the Aerobatic 150 not surprisingly it was named the Aerobat. Both versions included the new conical cambered wing. 832 of the "K" model were produced. The Aerobat differed from the standard model by increased structural strength. It was rated to +6/-3 G's. And included provisions for the pilots to carry parachutes required by FAR's for aerobatic flight. These included removable seat cushions to make room for the parachutes. Other modifications included skylights, as well jettison capable doors for quick escape.

970

Fuel Cost ($):
General Stats:
Seat Capacity: 2
Empty Weight: 975 lbs
Max Weight 1600 lbs
Useful Load: 625 lbs
Engine Name Continental O-200-A
Engine Number 1
Horsepower 100 HP
Never Exceed Speed: 143 kts
Stall speed: 95 kts
Service Ceiling: 12650 ft
Max Fuel 26 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 102 kts
GPH (75% BHP): 5.5
MPG (75% BHP) 18.5
Range (75% BHP): 394 nm
Fuel Cost Per Seat Mile 0.16 $
Fuel Cost Per Hour 33 $
MPG per 1000 lbs of Payload 11.59
F-T (Speed^2/FuelBurn) 18.9 HP
F-T Payload 11.8 kts
MPH To HP: 10.2 kts
T/O Roll - T/O over 50 FT OBST 735 ft / 1385 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
SA00034WI Installation of flap and aileron gap seals. Issued 2/11/1993
SA00037WI Installation of B & C Specialty Products BC100-1 battery. Issued 2/16/1993
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
SA00088WI Installation of replacement stabilizer and elevator tips. Amended 8/25/1993
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
SA00168BO Installation of Aero Ski Model M1800 main skis and T3000 tail ski. Modification limited to installation on 150L serial number 15073301 ONLY. Issued 4/15/2003
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
SA00191AT Installation of carbon steel brake discs that have melonite surface treatment. 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
SA00196AT Installation of Appalachian Accessories carbon steel brake discs that have melonite surface treatment P/N AA-17. Reissued 11/14/1994
SA00211AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/17/1994
SA00212AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/17/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
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
SA00284AT Installation of battery access door and elevator trim pulley access door. (Landplanes and Seaplanes 150 hp only) Issued 7/28/1993
SA00285AT Installation of ground power receptacle. (Landplanes and seaplanes 150 hp only) Issued 7/28/1993
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
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
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
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
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
SA00812CH Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. Reissued 6/30/2006
SA00843NY Aircraft fuel quantity transmitter replacement-from Stewart Warner Model 390 to Stewart Warner Model 385. Issued 5/28/1998
SA00855CH Installation of S-TEC Corp. System 50 Automatic Flight Control System in a Cessna 150J with a 180 horsepower engine installed. Issued 4/1/1998
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
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
SA01065SE Installation of vortex generators on the wings and vertical tail surfaces of the above model aircraft per Drawing Package MA2081 Revision IR dated January 15 2002 and Installation Manual MA2082 Revision IR dated February 13 2002 or later FAA approved revision of either of these documents.NOTE: If more than five vortex generators are damaged or missing the aircraft is not airworthy. Issued 3/18/2002
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
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
SA01125SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2171 Revision IR dated July 17 2002 and Installation Manual MA2172 Revision IR dated September 6 2002 or later FAA approved revision of either of these documents. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( NOTE: If more than five vortex generators are damaged or missing the aircraft is not airworthy. Issued 9/25/2002
SA01158WI (1 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005
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
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
SA01243SE  Install a 14.6 gallon auxiliary fuel tank in the baggage compartment Issued 7/18/2003
SA01280CH Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) Issued 8/29/2000
SA01291SE Installation of a McCauley 1A101/HCM 6948 propeller in accordance with N. A. Waterhouse & Associates Aeronautical Consulting Engineers Document NW014-NAW-003 Revision IR dated October 13 2003 or later FAA approved revision Reissued 1/19/2010
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
SA01389SE Installation of 8-gallon extended range wing fuel tanks Issued 3/5/2004
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
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01538SE Incorporation of bushing on carburetor hot air box control arm in accordance with Dynamic Propeller Installation Instructions No. 7000 Revision A dated February 24 2005 or later FAA approved revision to this document. Issued 4/27/2005
SA01598AT Conversion from tricycle landing gear arrangement to conversion landing gear arrangement. Issued 4/13/1998
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
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
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01834CH (1 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009
SA01860NY (1 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 1)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01933LA-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (1 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006
SA01944CH (1 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
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
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
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
SA02137AT Installation of the Lord Corporation Nose Wheel Shimmy Damper P/N SE-1051 Amended 8/24/2006
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
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
SA02248LA Installation of Sensor Pod and wiring for a passenger operated monitoring system Reissued 1/30/2014
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
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
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
SA02415CH Installation of Flight Boss LTD S-RPE-CN Rudder Pedal Extensions. Issued 5/10/2007
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02446CH Installation of the Courtesy Light Kit. Issued 6/25/2007
SA02462CH Installation of Flight Boss LTD S-RPE-CO Rudder Pedal Extensions Issued 8/29/2007
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
SA02738CH (PAGE 4) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
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
SA03105AT Manufacture of engine cowling fasteners in accordance with MilSpec Products Inc. Master Drawing List No. C150MDL Revision A dated May 1 2005 or later FAA approved revision. Installation of engine cowling fasteners in accordance with MilSpec Products Inc. Installation Instructions Document No. MS-C150C Revision A dated February 22 2005 or later FAA approved revision. Issued 5/23/2005
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
SA06037SW-D Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems. Amended 8/6/2007
SA09147AC-D Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-628. Issued 4/3/1996
SA09224SC Installation of a modified Textron Lycoming O-235 engine (modified for use of only ethanol for fuel). Reissued 5/31/2007
SA09362SC Installation of a panel and radio lamp dimmer control system. Issued 7/24/1997
SA09463SC Installation of eyebrow lights on pilots side instruments. Issued 5/14/1998
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09491SC Installation of a low voltage warning system. Amended 5/3/2001
SA09643SC Modification to remove the Standard Airworthiness Certificate and placing them in Special Airworthiness Certificate-Primary Category to allow the pilot-owner to perform preventative maintenance beyond what is allow under Part 43 Appendix A. Issued 7/24/2000
SA1-124 Lube oil filter BP55-1. Issued 
SA1-479 Aero control AP and heading lock GD. Amended 
SA1-630 Dry vacuum pump and instrument vacuum system 113A5. Amended 1/1/1960
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
SA1000NW Installation of Lycoming O-235-L2C(modified) (SE792NW) engine McCauley 1A103/TCM 6958 propeller. Reissued 6/12/1986
SA1003GL Installation of a cooling shroud on engine driven dry air pumps. Amended 5/1/2007
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
SA1008NM Installation of a Sensenich S72CKS6-0-52 -54 or -56 propeller/spinner assembly on Lycoming 0-235-L2C or0-235-L2C(M) engine. Amended 3/21/1983
SA1008NW Installation of a Sensenich S72CKS6-0-52 -54 or -56 propeller/spinner assembly on Lycoming O-235-L2C or O-235-L2C(M)* engine in accordance with Kennis G. Blackman Installation Instructions No. KB 1030. (* O-235-L2C(M) - STC SE792NW) Amended 1/21/1983
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
SA1034SW Installation of Lycoming O-320-E2D engine and Sensenich 74DM or McCauley 1C172TM propeller. Reissued 7/15/2009
SA1035NE Installation of a 14.6 gallon aft fuselage fuel tank in baggage compartment. Amended 5/31/1994
SA1052SW Installation of Lycoming 0-320-E2D engine according to STC SA1034SW on floatplane version. Reissued 7/15/2009
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
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1143CE Installation of Aero Fabricators muffler assemblies P/N E477-001(L.H.) and P/N E477-002 (R.H.). Amended 2/1/1988
SA1143SW Redesigned muffler assemblies. Issued 5/15/1970
SA1148NW Installation of flap gap seals. Issued 12/19/1980
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA1201NW Installation of a Scott tail wheel McCauley propeller Issued 3/31/1981
SA1219EA Installation of a Sensenich Model 72CKS6-0-56 -54 or -52 metal propeller and a S72CK spinner assembly Reissued 6/14/2012
SA1221SO Fabrication and installation of wheel fairings. Reissued 7/17/1989
SA1235SO Replacement of the lower fuselage fuel drain cap (P/N AN929-6) with an adapter type coupling (belly drain P/N MT-101) and an exposed quick drain valve P/N CAV-160D). (A152 SERIES AIRPLANES STARTING WITH MODEL150F (S/N 15061533) AND SUBSEQUENT) Reissued 4/29/2003
SA1245GL Installation of a fuel system quick drain valve. Issued 10/20/1987
SA124EA Shur-Vent fuel tank filler cap. Issued 1/1/1960
SA1261WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1270GL Install SAF-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA1292SO 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
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
SA1346CE Chrome plate brake disc installation. Amended 9/6/1977
SA1371SW Wing leading cuff wing tips and upper surface flow fences. Amended 4/14/1983
SA1384CE Install Lycoming O-320-E2D engine and McCauley 1C172TM7458 propeller. Reissued 8/5/1981
SA1395SW Revise fuel and oil system for inverted flight. Issued 11/24/1971
SA1398SO Remove drain plug AN-806-6 from fuel line drain in belly of aircraft and replace with drain valve MT-101-1. (See limitations) Reissued 4/29/2003
SA1410GL Install Aero Fabricators Shoulder harness and seat belt assembly per Aero Fabricators. Amended 10/4/1990
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1422SO Installation of Model CC-1 checkpoint computer. Issued 3/24/1983
SA1431WE Installation of rudder trim system. Amended 4/2/1978
SA1433WE Installation of Brittain Model CSA-1 Stability Augmentation system. Reissued 10/20/1972
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1455WE Installation of Brittain Industries Model CSA-1 Flight Control System Amended 9/12/1979
SA1473WE Installation of Brittain Model B2C Flight Control System. Reissued 10/20/1972
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
SA1480GL Install portable hand control as manufactured under STC SA860SO and SA861SO. Issued 5/15/1990
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
SA1512WE (2 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007 0:00
SA1567SO Installation of Appalachian Accessories brake rotor P/N 75-27. Issued 1/18/1984
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1615CE Quick drain in fuel line at tee fitting forward of fuel selector valve. (A150 Series 150F AND SUBSEQUENT) Issued 11/19/1980
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
SA164WE Fuel filter PFF-100. Issued 1/1/1960
SA1663CE Installation of strut/wing and strut/fuselage fairings lightning hole covers and aerodynamic putty. Reissued 1/27/1993
SA1680NM Installation of a Lycoming O-320-A3A engine Afcon engine mount (P/N 1500-1) and exhaust system McCauley 1C172/TM7258 propeller modified nose cowl and associated system Issued 7/29/1982
SA172NW Installation of drooped type wing tips. Issued 4/14/1975
SA1735GL Installation of Master Nag warning system. Amended 3/21/1994
SA175GL Installation of conventional landing gear Amended 4/6/1989
SA1760SO Installation of Appalachian Access. stainless steel brake rotors P/N 75-15C. Reissued 2/6/1995
SA1761SO Installation of Appalachian Access stainless steel brake discs. Reissued 9/29/1995
SA17WE Conversion of aircraft for parachute jumping and aerial photography operations. Issued 1/25/1962
SA1809WE Installation of one twelve-gallon auxiliary fuel tank in each outboard wing panel. Amended 2/16/2007
SA1814NM Installation of Lompoc Aero Specialties inner plexiglass pane in swing out window frames presently employing a single window  Reissued 1/23/2004
SA1944WE Installation of Madras wing tips. Amended 8/16/1979
SA1977WE Installation of recontoured wing leading edge stall fences wing tips and positive aileron seals. Reissued 7/21/2005
SA1978SO Installation of Appalachian Accessories stainless steel brake discs P/N 75-40. Reissued 2/6/1995
SA2-1533 Installation of windshield wiper. Reissued 1/31/1997
SA2035WE Installation of Aerial photo- graphic camera kit serial No. 101. Reissued 8/10/1992
SA2048CE Operation of airplane on unleaded automotive gasoline Amended 2/21/2012
SA2053WE An adjustable lateral trim capability through spring bungee control of aileron per Strato Engineering Company. Reissued 5/23/1973
SA2105NM Modification of the landing gear system form a tricycle to a convetional (tail dragger). Reissued 10/3/2003
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2119WE Installation of recontoured wing leading edge stall fences wing tips and positive aileron seals. Reissued 7/21/2005
SA2137SO Fabrication and installation of nose wheel fairings. Reissued 7/17/1989
SA2162NM Installation of the Precise Flight stand-by vacuum system (SVS) Amended 11/7/2003
SA217RM Installation of Lycoming O-360-A1A engine (150 hp.) Sensenich76EM8S10-0-56 propeller revised engine mount and fuel system dorsal fin wing leading edge cuffs wing fences aileron gap closures and other changes. Reissued 4/19/1991
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2191WE Installation of recontoured wing leading edge stall fences and drooped ailerons in flaps down mode. Reissued 7/21/2005
SA2192WE Installation of recontoured wing leading edge stall fences and drooped ailerons in flaps down mode. Reissued 7/21/2005
SA220SO Tow bar release mechanism and safety tow link. Reissued 10/3/2011
SA2219WE Installation of Filtrator Company Engine Crankcase Breather and Vacuum Pump Air-Oil Separator in accordance with the applicable FAA sealed drawing listed on the attached Master Eligibility List Number SA2219WE.Installation of Filtrator Company engine crankcase breather and vacuum pump air-oil separator. Reissued 7/14/2011
SA221GL Installation of wheel replacement type skis FluiDyne all metal (TSO approved) Model A2000A main skis FluiDyne Model AT2000A tail ski. Reissued 4/13/1982
SA223GL The installation of the stall strips. Amended 4/24/1979
SA2276CE Installation of a loudspeaker system. (150H S/N 15068108) Issued 9/10/1987
SA2278NM Installation of Lycoming0-235-L2C(M) engine and McCauley1A135/KCM7054 propeller. Reissued 3/29/1991
SA2290NM Installation of Elano P/N ELO99001-060 B (or later FAA app. revision) muffler in lieu of original Cessna muffler. Issued 6/22/1984
SA2335SO Installation of Appalachian Accessories P/N 73-5 brake discs. Reissued 9/29/1995
SA2342CE Installation of Sensenich69CK-S12-0-52 propeller. Issued 12/17/1987
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2355SO Replacement of Cleveland brake discs P/N 164-17 or 164-117 with Appalachian Accessories stainless steel brake discs P/N 64-17. Reissued 9/29/1995
SA2356SO Replacement of Cleveland brake discs P/N 164-40 or 164-140 with Appalachian Accessories stainless steel brake discs P/N 75-40. (182 SERIES THRU 182Q) Reissued 2/6/1995
SA2360NM Installation of a Motorola alternator and regulator. Issued 3/20/1984
SA2381NM Installation of Knots 2U Ltd Wheel and Body Fairings Amended 8/19/2008
SA2381SO Installation of Appalachian Accessories P/N 75-92 Brake Rotors. (182 SERIES THRU 182A) Reissued 9/29/1995
SA2382NM Installation of Aileron and Flap Gap Seals. Amended 7/15/2003
SA2382SO Installation of Appalachian Accessories stainless steel brake discs. (182 SERIES THRU 182Q) Reissued 9/29/1995
SA2383SO Installation of Appalachian Accessories P/N 75-94 Brake Rotors. Reissued 9/29/1995
SA2396WE Installation of Aural IAS Signalling device Issued 7/29/1971
SA2433CE Installation of aileron and/or flap gap seals. Issued 11/4/1988
SA2515CE Installation of replacement wing tips. Issued 7/31/1989
SA2535SO Installation of a Water in Fuel Detection System. Reissued 7/6/1989
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
SA2577NM Installation of Lycoming 0-360-F1A6 (modified per STC SE2574NM) and Hartzell HC-C2YK-1BK/FY666A-2 Issued 6/7/1985
SA2582CE Installation of auxiliary seat per Aviation Fabricators. Issued 2/8/1990
SA2583CE Installation of auxiliary seat. Issued 2/8/1990
SA2586NM (PAGE 2) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2604NM Installation of Lycoming O-235-L2C-M engine. Issued 6/13/1984
SA2613CE Operation of airplane on leaded and unleaded automotive gasoline 91 minimum antiknock index(RON + MON)/2. Amended 6/23/1992
SA2662CE Installation of wing leading edge cuffs drooped tips stall fences and aileron gap seals. Issued 10/24/1990
SA2665NM Removal of existing inverted oil system and installation of Christen Industries Model 801 Series Inverted Oil System  Issued 10/4/1984
SA2680CE Installation of steering rod boots. Issued 12/19/1990
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2687WE Installation of protective device on fuel tank vent line. Reissued 7/19/2011
SA268GL Installation of wheel and ski adapters on Models 150F G H J K L M 152 aircraft modified per STCSA175GL. Installation of adapter extension-landing gear landing-gear extended-assembly of Models 150 150A - H J - M A150K - A150M 152 A152 aircraft modified per STC SA175GL. Reissued 4/13/1982
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA270SO Water and ice detector in fuel gascolator and carburetor. Issued 1/1/1961
SA2742SO Fabrication and installation of wheel fairings. Issued 4/17/1990
SA2776NM Installation of exhaust gas analyzer system. Issued 3/4/1987
SA2780CE Installation of wing leading edge cuffs drooped wing tips stall fences and aileron gap seals. (F152 S/N F15201429 THRU F15201528) Issued 12/4/1991
SA2790WE Installation of angle of attack indicator. Issued 12/10/1973
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
SA2846SW Conversion from trigear to conventional gear configuration  Reissued 2/4/2004
SA2850SW Installation of leading edge cuffs stall fences aileron seals wing tips. Reissued 6/6/1980
SA2851CE Installation of wheel fairings. Amended 11/4/1992
SA287GL Installation of Lycoming O-320-D2B engine and McCauley Model 1C172/TM propeller using the existing installation hardward on an aircraft previously modified in accordance with STC SA572CE. Issued 12/15/1978
SA2912WE Installation of palletized dual LTN-51 INS or dual LTN-72 INS or combination of either. Amended 9/26/1974
SA2960NM Install stay put (seat position locking device). Amended 3/14/1986
SA3037SW-D Installation of Mitchell automatic flight system AK457 consisting of Century I autopilot with optional omni tracker system. Reissued 8/16/1984
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
SA3112WE Installation of flap slot closures. Amended 7/19/1977
SA3147SO Installation of aileron and flap gap seals. Reissued 1/23/2012
SA316SO Carburetor ice detector. Amended 10/5/1966
SA318GL Installation of Bolen wheel extenders on Cessna models modified per STC SA175GL and/or SA268GL. Reissued 4/13/1982
SA324GL Installation of fuel tank caps. Issued 7/16/1979
SA326EA Wet-to-dry vacuum pump conversion kit 300-3. Reissued 4/22/2003
SA3284SO Installation of engine cowling and firewall fasteners. (150 S/N 15060088 THRU15079405) (A150K S/N A1500001 THRU A1500684)) Amended 8/29/2001
SA3345WE Recognition light installation on horizontal stabilizer. Reissued 2/28/1980
SA3438SW-D Installation of Century automatic flight systems Model AK943. Issued 3/18/1986
SA3439SW-D Installation of Century automatic flight system Model AK944. Issued 3/18/1986
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA356CH Installation of seaplane safety covers. Issued 5/22/1995
SA3659SW Installation of Jetton Alert II alarm system. Reissued 3/30/2007
SA3687WE Installation of an air/oil separator. Reissued 9/28/2001
SA3688NM Cockpit sun visor installation. Reissued 3/24/2003
SA3733WE Installation of a special door(right hand side only) to facilitate aerial photography. (150L UTILITY CATEGORY) Issued 9/6/1978
SA3788NM Installation of Sensenich 74DM6S5 Propeller Elano Exhaust System P/N EL 099001-063 and -060 and Cessna Muffler P/N 0454011-1 in accordance with FAA Approved ACT Report No. 104 dated February 10 1992 or later FAA approved revisions. STC SA4795SW for the installation of Lycoming 0-320-E2D engine is required as part of this installation. Reissued 2/4/2004
SA3851NM Installation of a BAS tail pull handle in the aft fuselage. Amended 12/2/2010
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4-1342 Installation of Winslow Aerofilter Corporation Model 30409A full flow lube oil filter with element 1A0235. Issued 7/8/1964
SA4-1373 Brake blocks AB-6531 and AB-6532. Issued 1/1/1960
SA4-394 Installation of George M. Adams DGA-2000 wheels and Bodell Mfg Model BMI-252 brakes. Reissued 6/25/2003
SA4-925 Magnetic flight director 2000. Issued 1/1/1960
SA4-965 Autopilot. Reissued 10/1/1973
SA4005NM (PG 2) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA403CE Install FluiDyne A2000A main skis and NA800 nose ski. (150 AT 1500 LBS GR WT) (150J AT 1600 LBS GR WT) (150H AT 1600 LBS GR WT) (150G AT 1600 LBS GR WT) (150F AT 1600 LBS GR WT) (150E AT 1600 LBS GR WT) (150D AT 1600 LBS GR WT) (150C AT 1500 LBS G R WT) (150A AT 1500 LBS GR WT) (150K AT 1600 LBS GR WT) (150B AT 1500 LBS GR WT) Reissued 2/16/1993
SA4057WE Installation of a muffler and exhaust heat exchanger. Amended 9/11/2007
SA4065SW Metal chip detector in engine oil. Issued 12/4/1979
SA4166NM Installation of Fairchild voltage regulator No. UA78 GUIC to replace the original voltage regulator in Cessna turn coordinator P/N 0661003-0506. Issued 1/25/1988
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4278WE Installation of quick drain valve at low point of aircraft fuel system. Issued 12/19/1980
SA4302NM (PAGE 1) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
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)