PA-28 160 and c

Number of Active Aircraft: 306 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1210 lbs
Max Weight 2200 lbs
Useful Load: 990 lbs
Engine Name Lycoming O-320-B2B
Engine Number 1
Horsepower 160 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 15000 ft
Max Fuel 36 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 115 kts
GPH (75% BHP): 8
MPG (75% BHP) 14.4
Range (75% BHP): 431 nm
Fuel Cost Per Seat Mile 0.1 $
Fuel Cost Per Hour 48 $
MPG per 1000 lbs of Payload 14.23
F-T (Speed^2/FuelBurn) 16.5 HP
F-T Payload 16.3 kts
MPH To HP: 7.2 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1700 ft

SA00009SE Fiberglass wing tips and wing tip landing lights. Reissued 12/23/2011
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
SA00028AT Installation of speed splitter flap bracket fairings. Issued 11/20/1992
SA00043AT Removal of existing aluminum battery and starter cables and replacement of cables with copper cables. Issued 12/21/1992
SA00047NY Installation of replacement windows. Amended 7/21/1997
SA00060AT Installation of flap gap seals. Issued 12/21/1992
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00063AT Installation of aileron gap seals. Issued 12/21/1992
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00070BO Installation of P/N 9725 carburetor heat shroud. Issued 6/26/1997
SA00072SE Cockpit sun visor installation. Amended 6/2/2005
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
SA00161BO (3 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
SA00176AT Installation of composite spinner assemblies. Issued 4/5/1993
SA00178AT Installation of composite spinner and/or spinner bulkheads. Amended 10/13/2000
SA00191AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00193AT Installation of carbon steel discs. Reissued 11/14/1994
SA00198AT Installation of carbon steel brake discs. 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
SA00243BO (4 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
SA00261NY Installation of Aviation Services Inc. Model 1201 Cockpit Utility Light. Reissued 12/31/2002
SA00269BO (3 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
SA00379NY Increase in maximum gross weight to 2440 pounds. Reissued 8/8/2006
SA00393SE Installation of the G/S 2500 and G/S2500R Aircraft Security Alarm System. Issued 12/6/1996
SA00395NY Installation of .250 in. thick replacement windshields. Issued 2/1/1996
SA00397NY Increase in maximum gross weight to 2440 pounds. Issued 2/14/1996
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
SA00444WI-D Installation of Bendix/King KAP 140 Automatic Flight Control System with optional KCS 55A Compass System. For model PA-28-181 serial numbers 2890206 thru 2890231 and 2843001 and after Reissued 2/28/2000
SA00477DE Installation of engine cowling baffle exhaust and oil cooler. Limited to installation on PA-28-140 serial number 28-7325528 ONLY. Issued 7/12/2002
SA00507AT Modification of battery box. Issued 6/8/1994
SA00633LA Installation of an electric constant speed propeller MTV-18B/180-7 and control unit P-120-U. Issued 5/15/1998
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (5 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00720CH Installation of McCauley Propeller Model B3D36C431/80VSA-1. Reissued 9/21/2005
SA00744DE Installation of Automatic Dependent Surveillance  Amended 3/28/2013
SA00760SE Installation of glare shield. Reissued 5/20/2010
SA00762SE Installation of Precise Flight Inc. Speedbrake 2000 System Amended 11/7/2003
SA00769CH Installation of Champion Limited Authority Spark Advance Regulator (LASARTM) ignition system with Cylinder Head Temperature (CHT) monitoring capability on airframes with FAA approved installations of Textron Lycoming model IO-540 AEIO-540 and HIO-540 engines. Reissued 2/10/2009
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
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
SA00849SE Installation of vortex generators on wings and tail surfaces. Issued 10/27/2000
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00915CH Installation of McCauley Propeller Model D3A36C436/74SA-0 and spinner assembly. Reissued 9/23/2005
SA00927AT Installation of composite propeller spinner. Amended 5/20/2004
SA00945AT Installation of composite forward bulkhead. Amended 10/13/2000
SA00954AT Installation of composite bulkhead. Amended 3/31/2004
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
SA00954WI Installation of Concorde RG Series Battiers in Piper Single Engine Airplanes. Issued 4/2/2001
SA00955AT Installation of composite bulkhead. Amended 10/13/2000
SA01024CH Installation of a Hartzell PHC-C3YF-1RF/F7663-4T propeller and C-3570(P) spinner in accordance with Hartzell installation instructions HP2834 dated February 3 1999 or later FAA approved revision. Issued 4/6/1998
SA01026SE (PAGE 1) Improved fuel gascolator assembly. Amended 12/19/2012
SA01038AT Installation of composite construction wingtips with Hoernr chordwise section with a clear plexiglass nose enclosure for aircraft lighting. (PA-28 -28R -32 -32R -34 series MODELS WITH CONSTANT-CHORD WINGS) Issued 5/13/1996
SA01042AT Installation of Composite Spinner. Amended 10/13/2000
SA01071LA Installation replacement tail cone fairing assembly. Issued 10/6/2000
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
SA01100AT Installation of Composite Spinner. Amended 3/31/2004
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
SA01107SE RMD Aircraft Lighting high intensity discharge wingtip light manufactured Amended 4/2/2003
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
SA01120SE Installation of Door Steward. Amended 3/4/2010
SA01121AT-D Installation of FFC engineering order P28-2810-001. Issued 5/12/1999
SA01143WI Installation of Main Landing Gear Fairings for fixed gear Piper Cherokee aircraft. Reissued 3/12/2003
SA01147WI Installation of Concorde FLA or VRSLA series batteries in Piper Light Airplanes. Reissued 7/30/2012
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01170NY Installation of NPX138N-XXX FM Transceiver. Amended 1/17/2007
SA01174LA Installation of supplemental baggage compartment below existing rear baggage compartment. Issued 2/28/2002
SA01190LA Installation of Hartzell HC-C3YR-1RF/F7693F propeller and Hartzell C-3535-1(P) spinner. Issued 8/15/2001
SA01191LA Installation of Hartzell HC-F3YR-1ARF/F7693F propeller and Hartzell C-3570(P) spinner. Responsible ACO is Los Angeles NM-L. Issued 8/15/2001
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
SA01224AT Installation of wheel hub cabs with valve stem access door. Amended 4/17/1998
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01240SE (4 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
SA01319AT Installation of new composite engine cowling with cowl flap and large inspection access doors on both sides of cowling. Amended 5/20/1997
SA01330LA (PAGE 2) Installation of alternate avionics support assembly. Reissued 10/6/2010 0:00
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
SA01473SE (4 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
SA01482AT Manufacture of sun visor. Issued 10/20/1997
SA01487SE-D (Page 2) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01560WI-D Installation of the Honeywell KFD 840 Primary Flight Display System. );INSERT INTO stc_table VALUES ( REQUIRED DATA: AML No. 159-08325-0002 Revision - dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. Amended 7/22/2010
SA01582SE Installation of battery box. Amended 5/12/2006
SA01627WI Installation of replacement gas spring door stays on the forward and/or rear cabin doors in accordance with Sioux Center Aviation Drawing List 65DL Revision C dated October 18 2010 or later FAA-approved revisions. Issued 4/4/2011
SA01643SE Installation of BAS Inc. shoulder harness with inertia reel Amended 12/2/2010
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01690AT Installation of Archangel Avionics Cockpit Display System. Issued 8/21/1998
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (4 OF 5) Installation of an antenna Amended 2/15/2007
SA01786SE Fabrication and installation of wing tips Issued 9/7/2007
SA01787SE Fabrication and installation of wing tips Issued 9/7/2007
SA01800SE (PG 3) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01807SE Installation of vortex generators on the wings and horizontal and vertical tail surfaces of the above model aircraft Issued 12/4/2007
SA01834CH (2 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009 0:00
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
SA01933LA-D Page 2 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (4 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01944CH (2 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 0:00
SA01982AT Installation of new composite wingtip with recognition light. Amended 9/23/1999
SA01988SE (PAGE 5) 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
SA02015CH Installation of Three-Point Torso Restraint System. Issued 7/30/2004
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
SA02022CH Installation of Pneumatic Luggage Door Strut Kit. Issued 8/16/2004
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
SA02093AK Installation of hourmeter airspeed switch. Issued 10/17/1997
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
SA02149AK Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. Reissued 5/17/2013
SA02154AK (PAGE 2) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005 0:00
SA02168AT Modification of engine exhaust system for improved engine performance by installation of a Laminar Flow System Extractor Exhaust System. Amended 2/28/2003
SA02203AK (PAGE 1) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
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 (4 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
SA02246LA Installation of a flap handle extension. Amended 11/16/2010
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
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02268CH (PAGE 4) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02268CH (PAGE 5) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02276AK Installation of AMSAFE Aviation Inflatable Restraints Amended 3/12/2013
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
SA02410AT Replace existing Auxiliary Electric Standby Fuel Pump with PMA Products Inc. P/N CA35328-800E Fuel Pump (1A10-S/N 27-1 through 27-2504(14v) 1A15-s/n 24-3642 24-4000 through 24-4782 24-4784 through 24-4803 2A13-s/n 28-7690001 through 28-7990626 28-8090001 and up(14v) Issued 10/10/2001
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02454AT Installation of a shoulder harness restraint system. Issued 5/7/2002
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02532AT Installation of subject Michelin tires on appropriate aircraft. For Michelin 5 6 8 and 10-inch rim diameter tires on General Aviation Aircraft. Issued 6/5/2002
SA02547AT (PG 2) Installation of a Voice Alert System. Amended 8/28/2007 0:00
SA02555CH Installation of Hartzell HC-C2YR-1BFP/F7497 constant speed propeller. Issued 4/17/2008
SA02572AT Installation of a PXE7300 In-Flight Entertainment System. Amended 2/13/2003
SA02579AT Installation of a fuel transfer pump incorporating sold state hardware in place of older breaker point hardware. Issued 11/1/2002
SA0258AT Install MT-Propeller Model MTV-12-D/188-30d Propeller and Spinner Assembly on Piper Models PA-28R-201T and PA-28RT-201T aircraft per MT-Propeller Operation and Installation Manual E-124 Issue 26 dated November 29 2001 or later FAA approved revision. Airplane Flight Manual Supplement (AFMS) E-677-E dated December 19 2000 or later FAA approved revision is a required part of this STC. Issued 1/8/2003
SA02707AT Installation of a PAV80 In-Flight Entertainment Audio-Video System on a Piper PA-28-181 Archer III aircraft  Issued 9/3/2003
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 2) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02770AT Installation of Aeronautical Electronics Corporation Electronic Checklist Models AEC-ECTO AEC-ECTS or AEC-APWS. Issued 12/18/2003
SA02777CH Installation of a Hartzell PHC-C3YF-1RF/F7663-2R Model Propeller Issued 11/6/2009
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
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03207AT Installation of Gomolzig Quietflight Low Noise Silencer P/N PA28-606500. Issued 1/20/2006
SA03208AT Installation of Gomolzig Quietflight low noise silencer.  Issued 1/20/2006
SA03209AT Installation of Gomolzig Quietflight low noise silencer P/N PA-28-606503. Issued 1/20/2006
SA03210AT Installation of Gomolzig Quietflight low noise silencer P/N PA-28-606504  Issued 1/20/2006
SA03303AT Installation of Thielert Aircraft Engines (TAE) Aircraft Diesel Engine model TAE 125-01 and MT-Propeller model MTV-6-A-187/129 propeller and other minor modifications. Issued 7/24/2006
SA03470AT Installation of a replacement cowling for Piper Turbo Arrow models. Issued 8/13/2007
SA09129AC-D Installation of S-TEC System 55 Two Axis automatic flight guidance system Model ST-610 with optional autotrim system. Amended 11/20/2000
SA09155AC-D Installation of S-TEC System 60 Pitch Stabilization System Model ST-630 with Optional Autotrim System. Issued 5/20/1996
SA09159AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-635 with Optional Autotrim System. Eligibility limited to Piper model PA-28-235 serial number 28-7310001 and up. Amended 5/25/2001
SA09166AC-D Installation of S-TEC System 55 Two Axis autoomatic flight guidance system Model ST-642 with Optional Autotrim System. Eligibility limited to Piper PA-28-235 s/n 28-10003 through 28-11393 and s/n 28-7110001 through s/n 28-7210023. Amended 8/1/2002
SA09222AC-D Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems Model ST-683-2/30. Issued 5/19/1997
SA09233AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-684. Issued 6/3/1997
SA09251AC-D Installation of S-Tec System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-703-20/30. Issued 6/26/1997
SA09252AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-704. Issued 6/30/1997
SA09254AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-711-20/30. Issued 7/7/1997
SA09257AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-712. Issued 7/11/1997
SA09287AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance System Model ST-729-20/30. Issued 10/13/1997
SA09292AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-730. Issued 10/24/1997
SA09328AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-764-20/30. Issued 1/19/1998
SA09346AC-D Installation of S-TEC system 30 alt altitude hold system. Issued 3/3/1998
SA09414AC-D Installation of S-TEC System 40X/50X single and two axis automatic flight guidance systems model ST-867-40X/50X. Issued 2/17/2000
SA09415AC-D Installation of S-TEC system 50XP two axis automatic flight guidance system Model ST-779. Issued 10/13/1999
SA09444AC-D Installation of S-TEC GPSS ARINC 429 converter/interface Model ST-901. Eligibility limited to model PA-28-140 serial number 28-21392. Amended 12/10/2001
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA09491SC Installation of a low voltage warning system. Amended 5/3/2001
SA09524SC Conversion of existing Piper air conditioning system from R12 to R134a refrigerant. Amended 3/26/2002
SA09623AC Installation of Century Flight Systems Model AK1069 Triden autopilot. Eligible on Piper PA-28-180 serial number 28-4378 and after. Issued 3/21/2003
SA09666AC Installation of a Global Positioning Steering System (GPSS) consisting of a GPSS Adapter Controller 1C975-0 and a GPSS Annunciator/Switch 1C977-0 or 1C977-1  Issued 3/21/2006
SA1-468 Six or 13 quart propeller anti- icing kit WAP-101A revision 2. Amended 
SA1-649 Lube oil filter PB55-1. Issued 1/1/1960
SA100EA AF-510 AF-512A or AF-512B autopilots. Issued 1/1/1961
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
SA1012GL Modify the Piper standard nose and main landing gear wheel fairings. (PA-28-151 ALL S/N S PA-28-161 S/N S UP THRU 28-7916228 PA-28-181 S/N S UP THRU 28-7990242) Amended 8/5/1998
SA10207SC Limited to installation on PA-28-140 serial number 28-20983 ONLY. Issued 1/30/2004
SA10236SC (3 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10281SC Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot.  Reissued 9/28/2006
SA1043NW Installation of a ski compartment Issued 10/27/1980
SA1046SO Installation of an adjustable trim tab on left aileron. Amended 4/26/1996
SA1053GL Install hand controller to actuate rudder pedals. Amended 8/3/1988
SA10594SC Modification of the Monroe Automotive Equipment Co. (MAECO) Shimmy Dampener. Issued 12/7/2006
SA10682SC Installation of alternator and voltage regulator Reissued 11/16/2007
SA1072CE Installation of wing leading edge cuffs and droop tips dorsal fin and vertical stabilizer vortex generator. Amended 11/6/1984
SA1072GL Installation of cooling shroud on engine driven dry air pumps. Amended 5/1/2007
SA1075SO Wing-Ding door stop to be installed using existing screws(Piper P/N 415 309 MS27039-0809) on leading edge of right wing at inboard side of fuel cell(W.S. 57.00). Issued 5/18/1979
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1093GL Installation of Airborne Auxiliary Dry Air Pump Kit No. 374-2 or 374-3. Reissued 1/27/1987
SA110SO Electric pitch trim system. Issued 1/1/1996
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1123EA Installation of Devore vertical tail floodlights on upper surface of horizontal stabilator. Reissued 2/28/1980
SA1131EA Installation of a radome pod on right wing. Reissued 2/6/1984
SA1156EA Installation of radome pod on right wing. Reissued 2/6/1984
SA1157SW Mitchell flight system AK295 con- sisting of Piper AutoFlite II auto- matic aileron stabilizer and optional tracking system. Reissued 7/9/1984
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA1183CE Installation of King Model KFC 2002 axis flight control system with a King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon indicator with a KC-292 mode controller. (PA-28R-200 S/N 28R-7235001 AND UP PA-28R-201 S/N 28R-7737002 and up Reissued 2/28/2000
SA1189SW Air circulator. Issued 9/15/1970
SA1191WE Removal of baggage door for aerial photography operations. Issued 1/1/1960
SA1192EA Installation of Safe Flight (SFIC) SC-150 speed control system. Issued 4/15/1980
SA1194GL Install fairings over flap hinges. Amended 7/15/1997
SA1202WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1214GL Installation of Pamco emergency backup pneumatic system. (PA-28-181 S/N 28-7690001 THRU 28-7990626) Amended 4/27/1988
SA1216GL Install wing root fairings. Amended 7/15/1997
SA1216SO Installation of an adjustable trim lab on the left aileron.  Amended 11/4/1981
SA1227CE Installation of dorsal fin. Amended 7/10/1991
SA1228CE Installation of wing tip extension. Amended 6/1/1974
SA1237SW Mitchell automatic flight system Model AK314 consisting of altimatic IIIB-1 with optional automatic pitch trim and radio coupler and glide slope coupler. Amended 8/3/1988
SA1258EA Installation of Cosco model78-( ) child restraint system. (172M S/N 17263459 - 17267584) Amended 4/11/1983
SA1272SW Mitchell automatic flight system AK307 consisting of Century I and omni tracker. Reissued 7/9/1984
SA129CH Installation of propeller model B3D36C424/74SA. Reissued 7/19/2006
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
SA1317CE Chrome-plated brake disc installation. Amended 3/1/1978
SA1331CE Installation of 160 hp Lycoming engine and repitched Sensenich propeller. Amended 1/25/1996
SA1354WE PAS-1 stability augmentation system. Reissued 10/20/1972
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA1373CE Install third window. (PA-28-180 S/N 28-1 THRU 28-4377 PA-28-235 S/N 28-10003 THRU 28-11039) Amended 11/17/1977
SA1383CE Installation of Edo-Aire propeller governor Model 34-828-014-12. Reissued 9/17/1990
SA1401NW Installation of fiberglass wing tips with recognition lights. Amended 8/14/2008
SA1406SW Mitchell automatic flight system Model AK269 consisting of Piper Autocontrol III autopilot with optional radio coupler. Reissued 7/10/1984
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1437NM Installation of a rear cabin shelf and closeout panel. Reissued 12/3/1996
SA1463SO Installation of Speed Enhancement Kit. Issued 6/2/1983
SA1469WE Installation of Brittain Model B2C Flight Control System Reissued 7/2/2013
SA1470WE Installation of Brittain Model PAS-1 stability augmentation system. Reissued 10/20/1972
SA1484WE Installation of Brittain Industries Inc. Model B2C Flight Control System Reissued 1/29/2013
SA1485NM Installation of a Lycoming IO-360-A1B6 and a Hartzell HC-M2YR-1B/7666A-2 propeller and associated baffling changes Issued 3/15/1982
SA1487SO Installation of speed enhancement kit. Reissued 6/21/2000
SA148RM Install Hoskins Model CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. Reissued 1/30/1998
SA148SW Replacement of right front seat with stretcher. Reissued 8/21/1987
SA1498CE Installation of King KFC 200 automatic flight control system two axis with or without flight director Reissued 2/28/2000
SA1499GL Installation of on-board engine analyzer system. Issued 7/12/1990
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1563CE-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
SA1565CE-D Installation of KAP 100 single axis KAP 150 two axis or KFC 150 two axis flight control system. Reissued 2/28/2000
SA1571GL Installation of rudder fin cap fairing with or without a strobe. Amended 7/21/1997
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1580SO Installation of speed enhancement kit. Reissued 6/20/2000
SA1588WE Installation of supplemental exterior flashing lights. Issued 1/30/1968
SA1607SO Fabrication and installation of nose wheel fairings. Reissued 7/17/1989
SA1616NM Installation of a Hartzell propeller on a Continental engine Issued 4/14/1982
SA1623GL Installation of McCauley governor model C290D3(x)/T39. Reissued 7/19/2006
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA164SW Automatic pilot AK092E. Issued 1/1/1960
SA1692GL Installation of Pamco emergency backup pneumatic system. (PA-28-236 s/n 28-7911001 thru 28-8111018) Issued 1/22/1992
SA1696SO Installation of one-piece windshield. Amended 6/1/1994
SA1713GL Installation of gear lobe fairings. Amended 7/15/1997
SA1716SW Mitchell automatic flight system AK430 consisting of AutoFlite II with optional omni tracker. Reissued 7/16/1984
SA1717SW Mitchell automatic flight system AK431 consisting of auto-control III or IIIB with optional radio coupler. Reissued 7/16/1984
SA1735GL Installation of Master Nag warning system. Amended 3/21/1994
SA1741WE Installation of hand control for the rudder system. Reissued 5/5/1997
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
SA1764GL Installation of Vortex generators. Amended 6/25/2001
SA1766NM Installation of rudder hand control for paraplegic Issued 12/3/1982
SA1789WE Installation of Brittain lateral stability augmentation system and super venturi. Reissued 10/1/1973
SA178WE Full flow aerofilter 30409A with element 1A0235. Issued 1/1/1960
SA1792WE Installation of Morse protection system. Issued 1/1/1960
SA1800SO Installation of Laminar landing gear fairing additions. Reissued 6/21/2000
SA180EA Geared starter. Issued 1/1/1960
SA1842NM Installation of an Avco Lycoming O-360-A4M engine and a Sensenich 76EM8-0-60 propeller and associated installation components. Reissued 5/10/2005
SA1898SW Installation of wing leading edge cuff flow fences optional wing tips and dorsal fin. Reissued 9/5/1979
SA1914SO Installation of a STOL kit or STOL/Speed kit combination. Issued 4/23/1986
SA191NE Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. Reissued 10/4/1984
SA194GL Installation of Lycoming IO-360-C1C6 engine in lieu of Lycoming IO-360- C1C engine using original instal- lation hardware and components. Reissued 2/10/1997
SA1963CE Operation on unleaded and/or leaded automotive gasoline. Issued 3/23/1984
SA1964CE Operation on unleaded and/or leaded automotive gasoline. Issued 3/23/1984
SA1971WE Installation of Model ARB-3 Automatic Downed Aircraft Marker( ADAM ). Amended 11/21/1969
SA2-952 Installation of fiberglass covering. Reissued 9/10/1996
SA2052WE Installation of Hartzell HC82XL-6F/8433-12 propeller(after conversion of engine to Lycoming O-320-E1A model). Reissued 3/25/2004
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2143WE Installation of recontoured wing leading edge drooped ailerons in flaps down mode wing stall fences fuselage flap raked wing tips flap actuated elevator trim spring modified flap cove and dorsal fin. (PA-28-235 S/N28-10001 thru 28-7210023) Reissued 9/8/2005
SA2144NM Installation of a modified air induction system to the Continental TSIO-360 engine turbocharger compressor (Rayjay) system. Reissued 10/15/2007
SA2145NM Installation of Turboplus intercooler system. Reissued 10/15/2007
SA2147NM Installation of Continental TSIO-360-FB(C) (converted)* engine and associated system. (PA-28RT-201T Turbo Arrow III) (PA-28-201T Cherokee) Reissued 10/15/2007
SA2147WE Installation of Brittain Industries B-7 flight control system. Reissued 11/20/1972
SA2148NM Installation of Turboplus engine nacelle cowl flaps. Reissued 10/15/2007
SA2156CE Installation of flap and aileron gap seals. Amended 12/14/1988
SA2167NM Installation of the Precise Flight stand-by vacuum system (SVS). Amended 11/7/2003
SA2171NM Installation of Precise Flight speedbrake system. Amended 3/10/2005
SA2178SO Replacement of Cleveland brake discs P/N 164-25A or 164-125A with Appalachian Accessories stainless steel brake discs P/N 75-25A. Issued 9/25/1987
SA2179WE Installation of leading edge cuff drooped ailerons in flaps down mode wing stall fences raked wing tips fuselage flap stabilator trim spring and dorsal fin (optional). (PA-28-180 S/N 28-03 28-1 thru 28-7205318 S/N 28-E13) (PA-28 SERIES 7305001 AN D UP Reissued 9/8/2005
SA2190NM Page 2 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2194CE Installation of Hoerner style wing tips. Issued 9/26/1986
SA21NW Installation of a 70 pound baggage compartment in either or both EDO 89-2000 89A-2000 or 689-2130 floats Amended 9/25/2009
SA2202WE Installation of recontoured leading edge drooped ailerons in flaps down mode fuselage flap stabilator trim spring wing stall fences raked wing tips and dorsal fin (optional). (PA-28R-200 s/n 28R-35001 thru 28R-7135329 and s/n 28-R-235001 and up) Reissued 10/10/1986
SA2213WE Conversion of Lycoming O-360-A3A engine to Model O-360-A1A engine and installation of Hartzell HC-C2YK1-B/7666A-0 propeller. Reissued 3/25/2004
SA2223NM Installation of Hoskins Model CFS-1000A -1001A FT-100 or FT-101 fuel flow indicating system. Reissued 1/30/1998
SA222SW Hartzell HC-82XL-6N/7636D-4 propeller and cowl rework. Issued 1/1/1960
SA2230CE Installation of replacement stabilator tips. Issued 2/27/1987
SA2241SO Fabrication and installation of main wheel fairings. Reissued 7/17/1989
SA224CE Installation of Model A3000 main skis and NB-1200 nose skis. Reissued 2/16/1993
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)