Mooney M20J 201 AT

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Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 0 lbs
Max Weight 0 lbs
Useful Load: 0 lbs
Engine Name Lycoming IO-360-A1B6D
Engine Number 1
Horsepower 200 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 0 ft
Max Fuel 0 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 170 kts
GPH (75% BHP): 14
MPG (75% BHP) 12.1
Range (75% BHP): -109 nm
Fuel Cost Per Seat Mile 0.12 $
Fuel Cost Per Hour 84 $
MPG per 1000 lbs of Payload 0
F-T (Speed^2/FuelBurn) 20.6 HP
F-T Payload 0 kts
MPH To HP: 8.5 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 0 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
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00063LA Installation of Acoustical/Thermal insulation. Reissued 1/5/2005
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00071SE Cockpit sun visor installation. Amended 7/7/2004
SA00072BO Installation of Avidyne Model 5RR-MFC-3XX-( ) multifunctional flight computer and Ryan International TCAD Model 9900B Traffic Alert and Collision Device. Amended 9/24/2001
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
SA00081SE Installation of Continental IO-550A engine and Hartzell PHC-C3YF-2UF/ FC7382 propeller. Reissued 5/20/1994
SA00105BO Installation of BF Goodrich WX-500 Stormscope Series II Weather Mapping Sensor to interface with Avidyne Model 5RR-MFC-1XX-() Multifunction Flight Computer. Issued 8/20/1999
SA00117DE Installation of Oilamatic Preoiler system per FAA approved Oilamatic Inc. Drawing List No. M20400 initial release dated 6/1/94 or later FAA approved revisions. Amended 3/14/2003
SA00133AT Installation of 0.250 inch side windows. Amended 3/20/1998
SA00133WI Installation of GARMIN global positioning system GPS 155. Issued 2/16/1994
SA00149BO Installation of Aircraft Components Volt and Vac Alert p/n 2044-1.  Amended 5/15/2003
SA00151WI-D Installation of Bendix/King KLX 135 and KLX 135A GPS/COMM (Global Positioning System Navigation Receiver with VHF Communications Transceiver) Reissued 2/28/2000
SA00161BO (2 OF 3 Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005 0:00
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
SA00187AT Installation of carbon steel brake discs P/N AA-20. Reissued 11/14/1994
SA00206AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
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
SA00241WI-D Installation of Bendix/King KLN 90B Global Positioning System (GPS) for enroute and approach IFR operation. Reissued 2/28/2000
SA00243BO (3 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
SA00243SE Gross weight increase as modified per STC SA5691NM. Amended 6/13/2001
SA00243WI-D Installation of Bendix/King KLN 35A GPS (Global Positioning System) Navigation Receiver. Reissued 2/28/2000
SA00244WI-D Installation of Bendix/King KLN 89 GPS (Global Positioning System) Navigation Receiver for VFR operations installation of KLN 89B GPS Navigation Receiver for IFR enroute and non-precision approach operations. Reissued 2/28/2000
SA00247WI-D Installation of Bendix/King KLX 135 and KLX 135A GPS/COMM (Global Positioning System Navigation Receiver with VHF Communications Transceiver). For serial numbers 680001 and above Reissued 2/28/2000
SA00260SE Installation of engine cowling. Issued 12/20/1995
SA00269BO (2 OF 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
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 ( PAGE3) 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 0:00
SA00300NY-D Update TNL2000T system to Trimble 2000 Approach. Reissued 11/18/1999
SA00306WI Installs TKS anti-icing system components and approves aircraft for flight into known icing conditions. Amended 4/6/2007
SA00366AT Installation of an oil filter funnel on oil dipstick tube. Issued 11/4/1993
SA00372WI Installation of GARMIN GNC300 VHF communication transceiver/ GPS receiver. Issued 10/16/1995
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00442WI-D Installation of Bendix/King KAP 140 Automatic Flight Control System. For model M20J serial numbers 24-3000 and after Reissued 2/28/2000
SA00472SE Gross weight increase as modified per STC SA00081SE. Issued 10/16/1997
SA00478CH (PAGE 1) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00502WI Installation of the GARMIN GNC 250XL VHF Communication Transceiver/GPS Receiver. );INSERT INTO stc_table VALUES (  Issued 4/24/1997
SA00511SE Installation of a type 7308 lamp. Issued 4/17/1998
SA00569AT Installation of Aero-Trim 800 electric elevator trim system. (M20 up to and including M20J-24-854) Amended 12/14/1995
SA00600DE Installation of pilot and co-pilot instrument panels for M20C Serial No Issued 3/17/2006
SA00642WI Installation of GARMIN Transponder GTX 320. Issued 4/2/1998
SA00649AT Installation of an infinitely adjustable cowl flap control system. Issued 1/31/1995
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00688CH Installation of McCauley Propeller model D3A36C430/74SA-0. Reissued 9/21/2005
SA00735WI Installation of GARMIN dual GNS 430. Issued 2/8/1999
SA00736WI Installation of GARMIN GMA-340. Issued 2/9/1999
SA00744DE Installation of Automatic Dependent Surveillance  Amended 3/28/2013
SA00748SE Replace original power plant and propeller with a Continental TSIOL-550A engine and McCauley 3AF36C525/G-80VMFA-2 propellers. Issued 10/21/1999
SA00749AT Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent) Amended 12/10/1997
SA00771WI-D Installation of Bendix/King KFC 225 automatic flight control system. Reissued 2/28/2000
SA00780SE (PAGE 3) 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
SA00783NY Installation of an airfoil ahead of the fuel tank vent to sweep super cooled water droplets out of the air before they can impinge on the fuel tank vent and cause an ice obstruction. Issued 1/23/1998
SA00803AT Installation of low profile landing gear doors. Amended 9/4/1997
SA00805AT Installation of Lycoming IO-360-A3B6 or IO-360-A3B6D engine and 201 cowling. Issued 7/12/1995
SA00807AT Modification of brake system to a dual piston caliper brake system. Issued 7/13/1995
SA00824WI-D Installation of Bendix/King KMD 150 MDF Multi-Function Display. Reissued 2/28/2000
SA00832WI Installation of a McCauley propeller part number 2A34C241/82PGC-6. Issued 11/5/1999
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00879WI Installation of GARMIN Navtalk Pilot provisions kit. Issued 5/26/2000
SA00928WI Install Garmin GTX 327 GMA 340 GNS 430 GNS 530 for Mooney M20M with GNS 430 or GNS 530 VHF Communication Transceiver/VOR/ILS Receiver/GPS Receiver. Amended 12/18/2000
SA00933WI-D Installation of Bendix/King KMD 550 Multi-Function Display (MFD) system optional Bendix/King KGP 560 General Aviation Enhanced ground proximity warning system (GA-EGPWS) and optional WX 500 Stormscope. MDL 159-08262-0001 dtd 12/11/00 and 2. If KGP 560 is installed AFM Supplement 006-0881-0000 dtd 01/10/01 or later approved revision. Issued 1/10/2001
SA00934WI-D Installation of Bendix/King KLN 94 GPS (Global Positioning System) Navigation Receiver for IFR enroute and non-precision approach operations. Issued 1/15/2001
SA00941AT Repositioning of a battery from the engine compartment to the aft equipment bay. Issued 1/9/1996
SA00942AT Installation of Vernier propeller control cable with ground adjustable friction lock. Amended 2/24/1999
SA00943AT Installation of Vernier throttle control cable. Issued 1/9/1996
SA00944AT Installation of Vernier mixture control cable. Issued 1/10/1996
SA00946AT Installation of cowling upgrade Mod Works 201 style. Issued 1/10/1996
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
SA00954SE (2 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
SA00956WI Installation of a McCauley propeller part number 3A32C418-G/82NRC-9 using propeller and spinner installation drawing 3A32C418/G/82NRC-9. Reissued 7/8/2008
SA01026SE (PAGE 2) Improved fuel gascolator assembly. Amended 12/19/2012
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01105WI-D (2 OF 2) Installation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine). Amended 5/31/2007
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01205WI-D (2 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
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (1 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
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
SA01310AT Installation of a Mooney One-Piece Lower Fuselage Skin P/N 310322-501 and related attachment structure. Amended 10/9/1998
SA01405WI  Installation of the Garmin GFC 700 Automatic Flight Control System and TAWS Option. Reissued 11/17/2006
SA01435DE Installation of engines modified with a Firewall Forward Technologies LLC modified camshaft into aircraft listed on the AML per Firewall Forward Technologies LLC Installation Instructions FFT-INI-001-AFR Rev. - dated 02/06/03 or later FAA approved revision. This installation must be done concurrently with STC SE01436DE which installs the modified camshaft to the engine.  Reissued 5/25/2011
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01439SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft Amended 11/19/2012
SA01465AT Install Mooney aircraft model M20J windshield. Amended 12/13/2001
SA01473SE (3 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
SA01477SE Installation of the Garmin G1000 integrated avionics system in accordance with Garmin AT Master Data List 005-C0229-00 Revision B or later FAA approved revision. Issued 11/16/2004
SA01516AT Installation of Vision Micro Systems Inc. VM1000/EC100 digital/analog engine instrumentation and caution advisory system. Amended 10/24/2008
SA01527AT Install Mooney M20J M20I rear side windows in Mooney M20F and M20G models. Issued 12/12/1997
SA01553AT Modify the side windows by replacing the existing 3/16 inch thick glass with 1/4 inch thick glass. Issued 2/18/1998
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
SA01642AT Installation of a Lycoming model IO-360-A1A or IO-360-A1B6D or IO-360-A3B6 or IO-360-A3B6D engine modified. Reissued 2/29/2000
SA01644AT Installation of a Landing Gear Warning System to incorporate a stall warning interface in accordance with Master Drawing List MDL-2037 Revision 7 dated July 14 2003 or later FAA Approved Revision.  Amended 9/12/2003
SA01648AT Installation of a replacement composite instrument panel glare shield and center console. Reissued 9/24/1998
SA01660LA  Installation of Air-Tec Alternator kit. Descriptive data pertaining to this design change are considered inadequate for duplication in other aircraft. This approval is limited to the installation on Mooney M20B S/N 1900 only.  Issued 3/30/2005
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 (3 OF 5) Installation of an antenna Amended 2/15/2007
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01734SE (PG 3) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
SA01800SE (PG 2) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01830SE  Installation of a Semi-Portable Oxygen System Reissued 2/12/2009
SA01860NY (2 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 3)  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 (3 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01982NY-D Installation of Garmin International GNS-530 COM/NAV/GS/GPS and GMA-340 audio system with Marker Beacon. Issued 12/11/2008
SA01983NY-D Installation of Garmin International GTX-330 Mode-S Transponder. Reissued 12/11/2008
SA01988SE (PAGE 5) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02004CH Installation of a Hartzell PHC-J3YF-1RF/F7963DF(B)-2 propeller and A-2295-10(P) spinner. Reissued 8/24/2004
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
SA02018SE-D (PAGE 2) Provisions installation of Garmin GPS/XM Antennas in accordance with FAA Approved Model List (AML) SA02018SE-D dated January 4 2011 or later FAA approved revision and FAA Approved GPS/XM Antenna STC Master Drawing List Document No.: 005-00638-01 Revision 1 Issued 1/4/2011 0:00
SA02019SE-D Page 2 Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/19/2012
SA02033AT (PAGE 3) 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
SA02041AT Installation of a new technology landing light. Issued 12/16/1999
SA02110CH (PAGE 2) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 2 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02168AK (PG 2) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001 1:00
SA02193CH Power increase to 310 BHP by Installation of Powerlite STC SE02930AT or CMI IO-550N Engine rated at 310 BHP/2700 RPMs and Hartzell Propeller Model PHC-J3YF-1RF/F7693DF(B)-2 propeller Amended 5/3/2013
SA02203AK (PAGE 1) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02204AT Installation of Continental IO-360-ES engine and other associated airplane mods. Amended 12/5/2000
SA02212AK (PG 3) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. Amended 5/4/2011
SA02217AK (1 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
SA02222NY-D Installation of Insight Instruments Corp TAS-1000 Air Data Computer Issued 4/16/2007
SA02232AT Installation of composite nose cowl nose landing gear doors and induction air system. Issued 11/6/2000
SA02265SE Installation of a camera housing Amended 11/1/2013
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
SA02349LA Installation of Lake Aero Styling and Repair Nose Gear Truss in accordance with Lake Aero Styling and Repair Master Document List LA155 Revision B dated February 23 2011 or later FAA approved revision.  Issued 6/6/2011
SA02353AK-D Fabrication and installation of F. Atlee Dodge Aircraft Services LLC P/N 6103-01 (left) and/or 6103-02 (right) rear jump seat  Issued 7/23/2009
SA02414CH-D Installation of the Hartzell propeller model HC-C2YR-1BFP/F7497 and Hartzell 835-54(P) or A-2295-5(P) spinner. Amended 8/4/2010
SA02431AT Installation of a BAE-14/28 Air Driven Alternator on a Mooney M20 Aircraft Issued 11/29/2001
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02461NY Installation of propeller MTV-12-B/180-59b. Issued 10/5/2007
SA02482CH Installation of Hartzell Propeller Model PHC-J3YF-1N/N7605()-2 composite propeller Amended 6/7/2013
SA02483CH Modify aircraft to utilize full 310 BHP @ 2700 rpm rated power of existing installed Teledyne Continental Motors (TCM) TSIO-550-G engine. Amended 6/7/2013
SA02491AT Installation of air traffic detector ATD-200. Issued 4/25/2002
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02547AT (PG 2) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02549AT Modification of engine exhaust system for improved engine performance. Amended 1/9/2003
SA02624AT This STC converts the Mooney M20L to essentially an M20R. The STC requires minor changes to the aircraft structure and includes installation of a Continental IO-550-N16B engine (The engine is operated at the performance limits of 280 hp at 2500 rpm just like the Continental IO-550-G used on the Mooney M20R.) The STC is to be accomplished in accordance with Mod Works Master Document List MW8800-000 Revision B dated April 30 2003 or later FAA approved revision. Reissued 11/25/2003
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 1) 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
SA02988AT Change in rating of the existing Teledyne Continental Motors IO-550-G Model engine to the same as that for the IO-550-G engine installed in the Mooney M20R 280 hp at 2500 rpm and the installation of a Hartzell Model PHC-J3YF-1RF/F7693DF(B)-2 propeller. Aircraft modification shall be performed in accordance with PowerLite Report AP1016-5 Installation Instructions Revision A dated November 25 2004 or later FAA Approved revision.  Reissued 5/17/2005
SA03024CH Installation of Hartzell Propeller models PHC-J3YF-1RF/7498()3 bladed metal propeller. Modification of aircraft in accordance with Minnis Aviation Installation Instructions No. M2011-3 Revision IR dated 10/25/11 or later. FAA Approved revision. This STC may be used with previously modified aircraft that incorporate STC Nos SA02842CH SA02843CH or SA02988AT. Issued 12/7/2011
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03165CH Installation of MT Propeller model MTV-14-D/(188-193)-30( ) in Mooney aircraft models M20R M20S and M20TN Amended 5/7/2013
SA03393AT Installation of Monroy Aerospace Corporation Traffic-Watch ATD-300. Issued 8/26/2004
SA09011AC-D Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-592 with optional autotrim system. Amended 1/3/2002
SA09122AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System with optional autotrim system. Amended 11/6/2001
SA09158AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-632 with Optional Autotrim System. Amended 8/15/2001
SA09212AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-676-20/30. Amended 6/13/1997
SA09219AC-D Installation of S-TEC System20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-678-20/30. Issued 5/19/1997
SA09220AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-677. Issued 5/21/1997
SA09221AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-679. Issued 5/23/1997
SA09223AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-680-20/30. Issued 5/20/1997
SA09271AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-681. Issued 8/20/1997
SA09308AC-D Installation of S-TEC system 20/30 single and two axis automatic flight guidance systems. Amended 6/20/2000
SA09309AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-746. Amended 8/3/2000
SA09382AC-D Installation of S-TEC system 55 two axis automatic flight guidance system Model ST-839 with optional autotrim system. Amended 7/19/2001
SA09392AC-D Installation of S-TEC Manual Electric Trim System Model ST-846. Amended 2/16/1999
SA09393AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-843-20/30. Amended 2/16/1999
SA09395AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-844. Issued 9/23/1998
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09564AC Installation of MT-Propller MTV-12-B/180-17. Issued 7/23/2002
SA09565AC Installation of MTV-12-D/188-53 propeller. Issued 7/23/2002
SA09695AC Installation of Lycoming IO-390-A3A6 engine and Hartzell Model HC-C2YR-1BFP/F7497 or HC-C3YR-1RF/F7282 propeller Reissued 1/7/2013
SA1-585 External electrical power receptacle. Amended 1/1/1960
SA1-615 Installation of Fram lube oil filter Model PB55-1. Amended 9/11/1967
SA1008WE Installation of Poly-Fiber covering material. Reissued 5/27/2003
SA10126SC (2 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 (1 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1026GL Installation of Pamco emergency backup pneumatic system. Amended 4/27/1988
SA10372SC Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot in accordance with the Master Drawing List No ST7893SC-A-12 Rev. B dated January 7 2005 or later FAA approved revision. FAA approved Airplane Flight Manual Supplement No. ST7893SC-A-14 Rev. I.R. dated January 19 2005 or later FAA approved revision is required. Amended 7/7/2005
SA1053SW Installation of Mitchell automatic flight system model AK287 consisting of Century III autopilot with optional automatic pitch trim and radio coupler. Reissued 9/7/1984
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA1074GL Installation of a cooling shroud. Amended 5/1/2007
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1090GL Installation of an auxiliary blower motor driven in cabin/ windshield heating system. Issued 11/17/1986
SA10SW External power plug. Issued 1/1/1961
SA1111SO Installation of an adjustable trim tab on the left aileron. Amended 11/8/1996
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1156WE Installation of Roto-Master (Rajay) turbocharged Lycoming IO-360-A1A or O-360-A1D engine. Reissued 11/14/2002
SA1172WE Lateral stability augmentation system LSA-4. Reissued 10/1/1973
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA1198WE NAV-2 flight control system or B-6 flight control system. Reissued 10/1/1973
SA1212CE Installation of King KFC 200 2 axis (3 optional) flight control system with KCS 55/55A compass and King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller or third axis (yaw damper) only or manual electric trim only (M20J S/N 24-001 THRU S/N 24-1093 EXCLUDING S/N 24-0073 AND S/N 24-0939 S/N 24-001 THRU S/N 24-1093 EXCLUDING S/N 24-0773 AND S/N 24-0939 M20F S/N 22-1305 AND ON) Reissued 2/28/2000
SA1258SW Porta-cool Model PC70 portable air conditioner. Issued 2/1/1971
SA1300CE Installation of Edo-Aire propeller governor Model 34-828-014-11. Reissued 9/17/1990
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
SA1351WE (PG 1) Replace existing fabric on wings fuselage empennage and/or control surfaces with Ceconite101 material. (262A Series -12) Amended 8/19/1983
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA1387GL Installation of Lycoming O-360-A1F6D and McCauley propeller B2D34C214. Issued 6/7/1989
SA138WE Installation of Grimes Model D-7080 rotating beacon on vertical fin. Reissued 2/25/2000
SA1411WE Installation of Roto-Master (Rajay) turbocharged Lycoming IO-360-A1A engine. Reissued 11/14/2002
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1462WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1464CE Installation of KFC 200 two axis(three optional) flight control system. (M20J 24-0773 -0939 24-1094 THRU 24-1418 EXCEPT 24-1368 M20K S/N 25-0001 thru 25-0790 except 25/0740) Reissued 2/28/2000
SA1489WE Installation of Brittain Industries Inc. Model B2C or BSS Flight Control System Reissued 1/31/2013
SA1502GL Installation of on-board engine analyzer system. Issued 7/18/1990
SA1505GL Installation of Hartzell propeller model PHC-J3YF-1RF/F7663-2R and associated spinner assembly. Amended 5/25/1994
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1525CE-D Installation of King KNS 81 digital area navigation system when interfaced with approved DME or TACAN. Reissued 2/28/2000
SA1525CED Installation of King KNS 81 digital area navigation system. Issued 1/23/1980
SA152NW Installation of deck and glare shield (with or without instrument lights). Amended 5/21/1981
SA1550WE Installation of Brittain LSA-4 flight control system. Issued 1/1/1960
SA1557CE-D Installation of KAS 297 altitude select option. Reissued 2/28/2000
SA1557CED Installation of KAS 297 altitude select option. Amended 8/1/1983
SA1561CE-D Installation of KAP 100 single axis KAP 150 two axis or KFC 150 two axis Flight Control System and optional KAS 297B vertical speed and altitude selector. Reissued 2/28/2000
SA1561CED Installation of KAP 100 single axis KAP 150 two-axis or FKC 150 two-axis flight control system. Amended 7/29/1983
SA1570WE Installation of Brittain NAV-2 flight control system. Reissued 10/20/1972
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1584WE Installation of Brittain Model B-6 flight control system. Reissued 10/20/1972
SA1588WE Installation of supplemental exterior flashing lights. Issued 1/30/1968
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1641CE Installation safe flight SC-150 stall warning and angle of attack indicating system. Issued 3/13/1981
SA1735GL Installation of Master Nag warning system. Amended 3/21/1994
SA1745SO Installation of Appalachian Access. stainless steel brake rotors P/N 75-20. Reissued 2/6/1995
SA1762NM Installation of a pressurized magneto system on the Continental turbocharged TSIO-360-C F and FB engines. Reissued 3/14/2006
SA1771CE-D Installation of King KFC 200 flight control system (2 axis) with or without flight director. (M20J s/n 24-1368 24-1419 and up.) (M20K s/n 25-0740 25-0791 and up) Reissued 2/28/2000
SA1771CED Installation of King KFC 200 flight control system (2 axis) with or without flight director. (M20J s/n 24-1368 24-1419 and up) (M20K s/n 25-0740 25-0791 and up) Amended 3/18/1983
SA1780WE Installation of Brittain Industries LSA-5 flight control system. Reissued 10/20/1972
SA1785WE Installation of Brittain Industries B2C flight control system. Reissued 10/20/1972
SA1786WE Installation of Brittain Industries B-6 flight control system. Reissued 10/20/1972
SA1787WE Installation of Brittain NAV-2B flight control system Reissued 6/21/2013
SA1798GL Installation of multi-sensor long range navigation system. Limited to installation on serial number 24-0336 ONLY. Reissued 2/17/2004
SA179SW Nose wheel well doors 8367-1 and8367-2. Issued 1/1/1960
SA1838SO Installation of auxiliary fuel tanks. Issued 9/30/1985
SA1913SO Auxiliary fuel cells are installed. Amended 3/16/2007
SA191NE Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. Reissued 10/4/1984
SA1938SW Brittain LSA-6 lateral stability augmentation system (positive control). Reissued 7/15/2013
SA195CH Installation of McCauley propeller model B3D36C424/74SA. Reissued 7/19/2006
SA2-952 Installation of fiberglass covering. Reissued 9/10/1996
SA2052NM Installation of Beryl D Shannon Aviation Specialties Engine Crankcase Breather Air-Oil Seperator Issued 3/4/1983
SA2074CE-D Install KAP-100 single axis KAP-150 two axis or KFC-150 two axis Flight Control System and optional KAS-297B vertical speed and altitude selector. Reissued 2/28/2000
SA2078NM Installation of a late model instrument panel Issued 7/18/1983
SA2154NM Installation of Turboplus intercooler system M20K-12000. Reissued 10/15/2007
SA2168NM Installation of the Precise Flight stand-by vacuum system (SVS). Amended 11/7/2003
SA2174NM Installation of Precise Flight speedbrake system. Amended 11/7/2003
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2207SW Installation of Brittain Industries Inc. NAV-FLITE II and B-5 Flight Control Systems Reissued 6/21/2013
SA2210NM Installation of Hoskins Model CFS-1000A -1001A FT-100 or FT-101 fuel flow indicating system. (M20C S/N 2807 and up) Reissued 1/30/1996
SA224SW Automatic pilot AK117. Issued 1/1/1960
SA225NE Replace original wheel brake discs with discs modified in accordance with Aviation Services. Issued 1/10/1984
SA2271SO Replacement of Cleveland brake discs P/N 164-9 or 164-109 with Appalachian Accessories stainless steel brake discs P/N 73-9. Reissued 9/29/1995
SA2277CE Installation of fuel bladder cells in wet wing fuel cavities. Amended 12/22/2003
SA2318CE-D Installation of Bendix/King EHI 40 electronic horizontal situation indicator system. Reissued 2/28/2000
SA2319CE-D Installation of the Bendix/King KAP 100 Single Axis KAP 150 Two Axis or KFC 150 Two Axis Automatic Flight Control System and optional KAS 297B Vertical Speed and Altitude Selector. Reissued 2/28/2000
SA2320CE-D Installation of the Bendix/King KLN 88 Loran C system. Reissued 2/28/2000
SA2330SO Installation of an adjustable trim tab on the rudder. Issued 5/17/1988
SA2332CE-D Installation of the Bendix/King KLN 90 global positioning system(GPS). Reissued 2/28/2000
SA2350CE Installation of fuel bladder cells in integral fuel tank and wing cavities. Amended 12/22/2003
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2367CE Installation of TKS anti-icing system components with placard stating Flight into known icing conditions prohibited.  Reissued 7/8/2008
SA241SO Mooney dorsal fin 4175-51. Issued 1/1/1960
SA2445CE Installation of Continental TSIO-360-MB engine McCauley Model 2A34C221-B/90DHC-16E propeller and new Mooney cowling. (M20K SN 25-0001 thru 25-0999) Reissued 9/7/1993
SA250GL Installation of either Lycoming IO-360-A1B6 or IO-360-A3B6 or IO-360-A3B6D model engines with various Hartzell and McCauley propellers. Amended 1/19/1996
SA2513NM Installation of relocated oil radiator. Issued 10/9/1985
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2586NM (PAGE 3) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2619WE Installation of Pathfinder Model P1-( ) autopilot system. Reissued 9/30/1998
SA2620WE Installation of Pathfinder Model P2-( ) autopilot system. Reissued 9/30/1998
SA2654WE Installation of Pathfinder Model P2A( ) autopilot. Amended 7/3/1979
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA2711NM Installation of Lycoming IO-360-A3B6 engine with McCauley propeller B2D34C214. Reissued 2/10/1994
SA2742NM Installation of a Lycoming IO-360-A3B6 or A3B6D engine. Amended 9/7/2005
SA2763NM Installation of freon type cabin air conditioning system. (M20K SN 25-1000 and on) Reissued 6/16/1987
SA2823SW Reinforcement of vertical tail spar. Issued 7/31/1978
SA2844CE (2 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992 0:00
SA289CH Installation of Inline Pneumatic Air Filter P/N CV1J4 Reissued 1/15/2013
SA2968WE Installation of manifold pressure gage/fuel flow meter (fuel pressure gage) in lieu of original gage/ meter. Reissued 6/25/1996
SA2986WE Installation of Pathfinder autopilot systems. (M20 SERIES see MDL No. 77-030-1 for approved models) Reissued 9/30/1998
SA2993WE Installation of Pathfinder autopilot systems and/or electric pitch trim systems. (M20C s/n 20-0011 and on-1974 s/n 20-1147 and on-1975) (M20E s/n 21-0025 and on-1974 s/n 21-1161 and on-1975) Reissued 9/30/1998
SA300CE Installation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO) Amended 5/14/1992
SA3047SW-D Mitchell automatic flight system AK523 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 6/22/1984
SA3047SWD Mitchell automatic flight system AK523 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 6/22/1984
SA3048SW-D Mitchell automatic flight system AK476 consisting of Century IIB autopilot with optional radio coupler. Reissued 8/16/1984
SA3048SWD Mitchell automatic flight system AK476 consisting of Century IIB autopilot with optional radio coupler. Reissued 8/16/1984
SA3049SW-D Mitchell automatic flight system AK475 consisting of Century I autopilot with optional omni tracker. Reissued 8/16/1984
SA3049SWD Mitchell automatic flight system AK475 consisting of Century I autopilot with optional omni tracker. Reissued 8/16/1984
SA3064SW-D Mitchell command electric trim AK541. Reissued 6/22/1984
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
SA3106SO Installation of a Teledyne Continental Motors model TSIO-360MB engine. (M20K SN 25-0001 thru 25-0889) Issued 12/31/1991
SA3145SO Provides an approved procedure for applying Aero-Trim Aeroseal P/N 500 externally to wing skin seams of fuel tanks to stop seepage from micro leaks up to .005 inches wide. Amended 2/20/1992
SA315CH Installation of McCauley propeller model B3D36C424/74SA-0. Amended 11/9/2006
SA3186WE Installation of Pathfinder autopilot systems and/or pitch trim systems. Reissued 9/30/1998
SA320GL Installation of Hartzell Model HC-C2YK-1( )F/F7666A-4Q propeller in lieu of Hartzell Model HC-C2YK-1/7666-2 propeller using original installation hardware and components on aircraft previously modified in accordance with STC No. SA250GL. No installation data are required. Issued 6/28/1979
SA3222WE Installation of Pathfinder autopilot systems and/or pitch trim systems. (M20C s/n 20-0011 and on) (M20E s/n 21-0025 and on) Reissued 9/30/1998
SA3252NM Installation of fiberglass belly fairing. Issued 5/27/1986
Fusulage Construction
Airframe Material
Number of Doors
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
Aileron Type
Aileron Trim
Aileron Control System
Flap Type
Wing Flap Actuation
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Instrument Panel
Flight Control
Number of Seats
Window Defrost
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)


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