PA32 300 B C D E

Number of Active Aircraft: NA Active- Map

Audries CertifiedPiper PA 32-300 B - Detailed Data
Piper 32-300 B,C,D,E - Cruise and Fuel Burn Computer

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 1967 lbs
Max Weight 3400 lbs
Useful Load: 1433 lbs
Engine Name Lycoming O-540-K
Engine Number 1
Horsepower 300 HP
Never Exceed Speed: 184 kts
Stall speed: 55 kts
Service Ceiling: 21500 ft
Max Fuel 84 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 162 kts
GPH (75% BHP): 16
MPG (75% BHP) 10.1
Range (75% BHP): 749 nm
Fuel Cost Per Seat Mile 0.1 $
Fuel Cost Per Hour 96 $
MPG per 1000 lbs of Payload 14.51
F-T (Speed^2/FuelBurn) 16.4 HP
F-T Payload 23.5 kts
MPH To HP: 5.4 kts
T/O Roll - T/O over 50 FT OBST 1100 ft / 1500 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
SA00029AT Installation of Speed Splitter flap bracket fairings. Issued 11/20/1992
SA00059AT Installation of flap gap seals. Issued 12/21/1992
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00064AT 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
SA00072SE Cockpit sun visor installation. Amended 6/2/2005
SA00076WI Manufacture and installation of replacement wing tips. (PA-32RT-300T S/N 32R-7787001 and on PA-32-300 S/N 32-7940001 and on PA-32R-300 S/N 7680001 and on PA-32RT-300 S/N 32R-7885001 and on) Amended 10/29/1993
SA00079BO Installation of Meriden GS-22 glide slope antenna. Issued 1/21/1998
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
SA00190BO Installation of Avidyne Corporation Primary Flight Display. Issued 1/30/2004
SA00191BO Installation of Avidyne Corporation Multi-Function Display. Issued 1/30/2004
SA00193AT Installation of carbon steel discs. Reissued 11/14/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00236DE Installation of Oilamatic Preoiler system. Issued 6/5/1996
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
SA00282BO Installation of Avidyne Corporation Entegra Integrated Flight Display System Amended 4/4/2013
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
SA00332BO Installation of non-hazard ice protection system kits Issued 6/18/2013
SA00387NY Installation of replacement windshields. Issued 1/11/1996
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
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00639WI Installation of the GARMIN GPS 155SL GPS Receiver. Issued 3/16/1998
SA00640WI Installation of GARMIN GNC 300XL VHF Communication Transceiver/GPS Receiver. Issued 3/16/1998
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00705WI Installation of Garmin GNS 430 VHF Communication Transceiver/VOR/ILS Receiver/GPS Receiver. Amended 7/25/2002
SA00705WI-D Installation of the Garmin GNS 430 or 430A Reissued 10/17/2007
SA00710WI Installation of Garmin GMA 340 audio panel. Reissued 12/13/2001
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
SA00800WI Installation of GARMIN GPS 400 with (1) Garmin Dwg No. 005-C0084-00 Rev B dtd 6/17/99 Master Dwg List GPS 400 Installation in Piper PA32 and (2) FAA Approved Flight Manual Supplement (AFMS) for Piper PA32 Garmin GPS 400 Receiver Rev A dtd 7/6/99 or later FAA approved revisions of (1) or (2). Reissued 5/29/2001
SA00800WI-D Installation of the Garmin GPS 400. Reissued 10/17/2007
SA00801WI Installation of GARMIN GNC 420 or GNC 420A. Amended 7/24/2002
SA00801WI-D Installation of the Garmin GNC 420 or GNC 420A Issued 7/6/1999
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
SA00816CH Installation of McCauley Propeller Model B3D3C431/80VSA-2 and spinner assembly. Reissued 9/23/2005
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00864WI Installation of GNS 530 or GPS 500 for (1) Installation Data referenced on Sheet 2 and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) referenced on Sheet 2. Amended 11/22/2004
SA00864WI-D Installation of the Garmin GNS 530 530A or GPS 500 (GNC 500 Series TAWS Option).  Reissued 8/27/2007
SA00870WI Installation of GTX 327 transponder. Issued 4/3/2000
SA00923AT Installation of composite propeller spinner. Amended 10/13/2000
SA00953AT Installation of a composite HOWL COWL mod comp engine cowling w/COWL FLAPS full length nosegear close doors belly fairing aft of firewall to streamline forward sec of exposed belly structures strakes and large access doors on both sides of cowling. Issued 1/26/1996
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
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
SA01066WI Installation of B&C Specialty Products BC410-1 Standby Alternator System. Amended 11/6/2006
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
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
SA01125WI  Installation of Garmin GTX 330 Mode S Transponder with Traffic Information System Capability.  Amended 6/22/2005
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
SA01161SE Approval of this change in type design applies to the airplane models listed above only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications including changes in type design will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( If the holder agrees to permit another person to use this certificate to alter the product the holder shall give the other person written evidence of that permission. Issued 1/8/2003
SA01170NY Installation of NPX138N-XXX FM Transceiver. Amended 1/17/2007
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
SA01266SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft Amended 11/4/2009
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
SA01328WI Installation of TKS Ice Protection System components with placard stating Intentional Flight into known icing is prohibited. Data Required: (1) AS&T Master Drawing List No. 12700DL Revision 3 dated March 7 2005 or later FAA Approved revision and (2) FAA Approved Airplane Flight Manual Supplement (AFMS) Document 12700-FMS dated May 13 2005 or later FAA Approved revisions to (1) or (2).  Reissued 7/8/2008
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
SA01481SE Installation of the Garmin G1000 integrated avionics system in accordance with Garmin AT Master Data List 005-C0150-00 Revision B or later FAA approved revision. Issued 2/20/2008
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
SA01588NY-D Installation of a WSI Inflight Weater Briefing System (AV-200). Reissued 11/26/2003
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
SA01653WI Activation of Automatic Speech Recognition (ASR) on a GMA 350/350H Audio Panel Issued 12/1/2011
SA01660AT Installation of composite engine cowling with cowl flap. Issued 6/25/1998
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01675AT Installation of composite wingtips with recognition lights under a lens. Issued 7/9/1998
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
SA01800SE (PG 3) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01831AT-D Installation of FFC engineering order P28-2810-001. Issued 5/12/1999
SA01834CH (1 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009
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 4)  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
SA01988SE (PAGE 6) 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
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
SA02029CH Installation of a Projects Unlimited AVX-5 Interface Computer. Issued 9/8/2004
SA02033AT (PAGE 4) 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 0:00
SA02093AK Installation of hourmeter airspeed switch. Issued 10/17/1997
SA02097CH Installation of a McCauley Propeller Systems B3D32C414/82NDA-2 propeller with optional LORD engine mount isolators. Issued 3/22/2005
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
SA02153LA-D (Page 2) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
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
SA02168AK (PG 1) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001
SA02203AK (PAGE 2)  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
SA02256CH Installation of a Hartzell Propeller model HC-I3Y (scimitar) Issued 3/10/2006
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 (2 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02384CH Installation of Flight Boss LTD SPA-32/34 Series Organizers. Issued 3/2/2007
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
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
SA02579AT Installation of a fuel transfer pump incorporating sold state hardware in place of older breaker point hardware. Issued 11/1/2002
SA02655AT (2 OF 2) Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. Amended 9/1/2004 0:00
SA02695CH Installation of MT-Propeller MTV-9-B/198-52 constant speed propeller in accordance with Professional Pilots Inc. Installation Instructions #SUTN3201MT dated December 22 2006 or later FAA approved revision.  Issued 3/25/2009
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
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
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09160AC-D Installation of S-TEC System 55 two axis automatic flight guidance system Model ST-640 with optional autotrim system. Amended 6/28/2001
SA09290AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-733-20/30. Issued 10/29/1997
SA09294AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-739-20/30. Issued 11/5/1997
SA09306AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-737-20/30. Issued 11/12/1997
SA09310AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-738. Issued 11/17/1997
SA09331AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-734. Issued 1/22/1998
SA09333AC-D Installation of S-TEC system 30 alt altitude hold system. Issued 1/29/1998
SA09454AC-D Installationo f S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-791-40X/50X Issued 6/5/2000
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
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
SA1013GL Modify the Piper standard nose and main landing gear wheel fairings. (PA-32-300 S/N UP THRU 32-7940020) Reissued 5/7/1997
SA10236SC (3 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10286SC Installation of a Chelton Aviation Corp (CAC) AP-3C autopilot.  Issued 9/27/2004
SA10530SC Installation of Cargo Net. Issued 1/10/2007
SA10594SC Modification of the Monroe Automotive Equipment Co. (MAECO) Shimmy Dampener. Issued 12/7/2006
SA1073GL Installation of cooling shroud on engine driven dry air pumps. Amended 5/1/2007
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1105CH Installation of a Hartzell HC-C3YR-1RF/F7693F propeller and 835-52(P) or C3535-1(P) spinner Issued 9/16/1999
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
SA1154EA Installation of radome pod on right wing. Reissued 2/6/1984
SA1156EA Installation of radome pod on right wing. Reissued 2/6/1984
SA1159EA Installation of DeVore Tel-Tail lights on lower surface of horizontal stabilator. Reissued 10/13/1983
SA1172SW Mitchell flight system AK304 cons. of Piper autoflite II with optional auto aileron stabilizer and tracking system. Reissued 7/9/1984
SA1195GL Install fairings over flap hinges. Amended 3/29/2010
SA1201CE Installation of King KFC 200 2 axis flight control system with a King KCS-55 (or -55A) compass and a King KI-255 (or -256) flight command indicator or a KG-258 attitude horizon gyro with a KC-292 mode controller. (PA-32R-300 S/N 32R-7680001 AND UP) Reissued 2/28/2000
SA1217GL Install wing root fairings. Amended 3/29/2010
SA1226NW Installation of a Hoskins C.F.S 1000 computerized fuel system Issued 5/7/1981
SA1310SW Installation of stretcher in lieu of rear seats. Amended 11/18/1993
SA1362CE Chrome-plated brake disc instal- lation. Issued 8/18/1977
SA1378SW Mitchell automatic flight system AK320 cons. of Century I and opt. tracker. Reissued 7/9/1984
SA1401NW Installation of fiberglass wing tips with recognition lights. Amended 8/14/2008
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1430CE Install King KFC-200 automatic flight control system. Reissued 2/28/2000
SA1439GL Installation of Pamco Emergency Backup Pneumatic System. Amended 4/11/1990
SA1486SO Installation of speed enhancement kit. Reissued 6/22/2000
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1521GL Installation of Flap Aileron Flap/Fuselage and Stabilator Gap Seals. Amended 3/29/2010
SA1522CE-D Installation of King KFC 200 Flight Control System (2 axis) with or without Flight Director. Reissued 2/28/2000
SA1523WE Installation of Brittain Model B-4A Flight Control System Reissued 7/2/2013
SA1557WE Installation of turbocharged Lycoming O-540-E4B5 engine  Reissued 6/26/2006
SA1567CE-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
SA1568SW Wing leading edge cuff flow fences optional wing tips and dorsal fin. Reissued 9/5/1979
SA1572CE-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
SA1572GL Installation of rudder fin cap fairing with or without a strobe. Amended 7/15/1997
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1596GL Installation of on-board analyzer system. Issued 5/8/1991
SA1607SO Fabrication and installation of nose wheel fairings. Reissued 7/17/1989
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1714GL Installation of Gear Lobe Fairings. Amended 7/21/1997
SA1735GL Installation of Master Nag warning system. Amended 3/21/1994
SA1742SO Installation of Lycoming IO-540-KIG5D engine. Issued 2/6/1985
SA1791GL Installation of Hartzell HC-C3YR-1( )F/F7663R. Issued 9/4/1992
SA17PC ONE ONLY STC SN 32-7440102: Removal of aft baggage door and installation of overboard dispensing unit.  Issued 11/15/1974
SA1801SO Installation of Laminar landing gear fairing additions. Reissued 6/20/2000
SA1854SO Installation of a one-piece windshield. Reissued 11/16/1996
SA1892SO Installation of adjustable trim tab on left aileron. Issued 2/5/1986
SA2072NM Installation of Goodrich de-icing boots on the Hartzell HC-C3YR-1RF/F76663R propeller Issued 4/8/1983
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2114SO Installation of a hand control for the rudder. Issued 5/14/1987
SA2167NM Installation of the Precise Flight stand-by vacuum system (SVS). Amended 11/7/2003
SA2190NM Page 2 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA21NE Installation of Whelen A600-PR and A600-PG anti-collision strobe with forward and tail position light assemblies as replacements for wing tip lights. Issued 3/1/1978
SA2217WE Installation of recontoured wing leading edge raked wing tips fuselage flap wing stall fences drooped ailerons in flaps down mode and dorsal fin (optional). (PA-32S-300 landplane only) Reissued 9/8/2005
SA2241SO Fabrication and installation of main wheel fairings. Reissued 7/17/1989
SA2253WE Installation of Edo Model FD-3500-21 amphibious floats. Amended 2/15/2001
SA2337SO Replacement of Cleveland brake discs P/N 164-22A and/or 164-23 or 164-123 with Appalachian Accessories stainless steel brake discs P/N 75-23. Issued 5/17/1988
SA2350NM Page 2 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2356NM Installation of R.M.D. Aircraft Lighting Inc. Landing/Recognition Lights Kit. Amended 3/29/2010
SA2498WE Installation of Goodrich de-icing boots on the Hartzell HC-C2YK propeller Amended 1/10/1979
SA249NE Modification of the engine cooling and induction system. Issued 3/28/1984
SA2556NM Installation of rear facing center seats (club seats).  Issued 2/20/1985
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 4) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA260GL Install a BF Goodrich RNAV 511 area navigation system with 51ASA(Alpha) or 51DSA (Delta) steering adapter or without either adapter. Reissued 1/31/1992
SA2687NM (PAGE 2) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000 0:00
SA2693NM (PAGE 2) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009 0:00
SA281AL Installation of large nose gear fork and 8.00-6 nose gear tire. Reissued 4/5/2012
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2933WE Installation of oxygen system. Reissued 1/26/1984
SA2935NM Installation of Turboplus Intercooler System. Reissued 10/15/2007
SA2941NM Installation of Precise Flt Speedbrake system. Amended 11/7/2003
SA2946SW Addition of Hydro Seal Fluid Additive to landing gear shock struts. Reissued 8/8/1980
SA3011SW-D Mitchell automatic flight system AK488 cons. of Piper altimatic IIIC w/opt. command/automatic electronic pitch trim radio coupler and glide slope coupler. Reissued 8/1/1984
SA3026SW-D Mitchell automatic flight system AK463 consisting of Century IIB autopilot with optional radio coupler. Amended 8/1/1984
SA3052SW-D Mitchell automatic flight system AK529 consisting of Piper Altimatic IIIC autopilot with command/automatic electric pitch trim optional radio coupler. Reissued 6/22/1984
SA3053SW-D Installation of Mitchell automatic flight system AK530 cons. of Piper autocontrol IIIB autopilot with opt. radio coupler. Reissued 6/22/1984
SA3054SW-D Mitchell automatic flight system AK531 cons. of Piper autoflite II w/opt. omni tracker. Reissued 6/22/1984
SA3055SW-D Mitchell command/electric trim system Model AK532. Reissued 6/22/1984
SA308EA (2 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 0:00
SA3098SO This modification will allow installation of Causey Aviation hinge assembly P/N 62371-108. Amended 7/2/1992
SA3102SW-D Mitchell automatic flight system AK591 consisting of Century IIB autopilot w/opt radio coupler. Reissued 5/24/1984
SA3103SW-D Mitchell automatic flight system model AK592 consisting of Century III autopilot with optional radio coupler and glide slope coupler. Reissued 5/24/1984
SA3107SW-D Installation of Mitchell automatic flight system model AK581 consisting of a Century III autopilot with optional radio coupler and glide slope coupler. Reissued 5/24/1984
SA311NW Installation of full span flaps by removing aileron and changing the deployment route of all flaps. Reissued 9/8/2005
SA3152SW-D Installation of Mitchell automatic flight system model AK621 consisting of Century IV autopilot or AK621FD consisting of Century IV flight director autopilot with optional remove annunciator. Reissued 6/6/1984
SA3159SO Replacement of Piper stabilator trim barrel P/N 63530-000 with Causey Aviation stabilator trim barrel P/N CA-63530-100. Issued 2/12/1992
SA3167SW-D Installation of Mitchell automatic flight system model AK304 consisting of Piper autoflite II autopilot with optional omni tracker system. Reissued 6/7/1984
SA3173SW-D Mitchell automatic flight system AK174 cons. of Piper autocontrol IIIB autopilot w/opt radio coupler. Reissued 6/18/1984
SA317NE Installation of Auto-Vac-2 manifold vacuum system. Amended 2/2/1990
SA3181NM Installation of Hartzell HC-E3YR-1()F/F7673DR-0 three-blade propeller on a Lycoming TIO-540-SIAD engine. Reissued 6/2/1999
SA3218SO Replacement of Piper stabilator trim shaft P/N 65246-000 with Causey Aviation stabilator trim shaft P/N CA65246-100. Issued 4/29/1992
SA3253SW-D Mitchell automatic flight system AK677 consisting of Piper altimatic IIIC autopilot with optional radio and glide slope couplers. Reissued 3/29/1984
SA3254SO Installation of main landing gear fairings. Issued 6/8/1992
SA3254SW-D Mitchell command electric trim system AK 678. Reissued 3/29/1984
SA3255SW-D Mitchell automatic flight system AK 679 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 3/29/1984
SA3273SO This modification will allow installation of Causey Aviation cowl plate assembly P/N CA69791-000. Issued 7/2/1992
SA3287NM Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system. Amended 11/14/1986
SA3305SW-D Mitchell automatic flight system AK775 consisting of Piper altimatic IIIC autopilot with optional radio and glide slope couplers. Reissued 9/21/1983
SA3306SW-D Mitchell automatic flight system AK776 consisting of Century III autopilot with optional and glide slope couplers. Reissued 9/21/1983
SA3309SW-D Installation of Mitchell automatic flight system consisting of Century IV autopilot or AK771 consisting of flight director autopilot with optional remote annunciator. Reissued 9/21/1983
SA3334NM The Model 706 VHF Communication Radio P/N 430-0054-0 ( )-0( ) is installed on the Piper Model PA-32R-300 airplane in accordance with II Morrow Inc. Installation Report No. 49 dated November 26 1985. Reissued 12/5/2003
SA3361SW Mitchell automatic flight system AK865 consisting of Century 41 autopilot or AK865FD consisting of flight director autopilot. Reissued 8/24/1983
SA3362SW-D Mitchell automatic flight system AK864 consisting of Century 21 autopilot. Reissued 8/24/1983
SA3370SW-D Mitchell automatic flight system AK320 consisting of Century I and optional tracker. Issued 3/27/1980
SA3374SW-D Mitchell automatic flight system AK872 consisting of command electric trim. Reissued 8/24/1983
SA3380SW-D Mitchell automatic flight system AK879 consisting of Century 31 autopilot. Reissued 8/24/1983
SA3405SW-D Edo Avionics automatic flight system AK896 consisting of Century 31 autopilot. Reissued 8/23/1983
SA3442SW-D Installation of Century automatic flight system Model AK947. Amended 2/28/1997
SA3472SW-D Installation of Century Automatic Flight System Model AK979. Amended 3/13/2013
SA3504NM Installation of a Turboplus Inc. instrument sub-panel system Reissued 10/15/2007
SA3513WE Installation of Roto-Master (Rajay) turbocharged Lycoming IO-540-K1G5D engine. Reissued 7/3/2006
SA364GL For T tail configuration - installation of Norton radome kit No. 4229X. For conventional tail configuration - installation of Norton radome kit No. 4229XC. Reissued 12/5/2000
SA3670WE Installation of Silver Instruments Fueltron IG or IP or Fuelgard digital fuel flow indicating system. Reissued 4/29/1991
SA371EA Zeiss aerial camera and intervalometer. Issued 1/1/1960
SA3736WE Installation of an engine oil cooler hose. Issued 9/22/1978
SA3774WE Installation of Hoskins Model CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. Reissued 1/30/1998
SA3839WE Installation of an air/oil separator. Reissued 9/28/2001
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA3NW Installation of Van s Aircraft Model VA-1 fiberglass wheel fairings. Issued 8/1/1972
SA4005NM (PG 4) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4008NM Installation of removable panels on the battery box slides. Reissued 9/30/2005
SA409GL Installation of a Lycoming IO-540-K1A5 engine Hartzell propeller and associated components. Issued 5/23/1980
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4288WE Installation of inflatable door seal. Amended 8/18/1983
SA429GL Installation of Edo-Aire Mitchell automatic flight system Model AK771 consisting of a Century IV autopilot. Issued 8/4/1980
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4327WE Installation of rudder brake and flap systems hand controls MFG. Amended 1/19/1984
SA433CH Installation of McCauley Propeller Model B3D36C427/82NGA-2. Amended 10/30/2006
SA4345WE Installation of cooling louvers in the top cowling. Issued 5/7/1981
SA472SO Installation of hand control for rudder pedal operation. rudder pedal operation. Amended 6/27/1974
SA4745NM Installation of Lifeport Patient Loading and Support System. Amended 11/23/1993
SA4778NM Installation of Blackwood Cherokee Mk. I hand control. Issued 10/12/1989
SA4840SW Installation of an Auxiliary Instrument Air System. Reissued 4/6/2007
SA4994SW Install TI 9100 Loran C Navigator. Issued 4/26/1983
SA4995SW TI 9100 Loran C navigator and King Radio KAP autopilot or KFC 200 integrated autopilot flight director system. Issued 4/27/1983
SA5121SW-D S-TEC System 60 two axis flight guidance system ST-098 with optional automatic electric trim system. Reissued 9/18/1990
SA5122SW-D Installation of S-TEC yaw damper system Model ST-134. Reissued 7/9/1984
SA5123SW-D S-TEC System 60 single axis autopilot ST-126 (14 volt). Issued 12/1/1982
SA5131SW-D S-TEC System 60 single axis automatic flight guidance system ST-097. Amended 9/19/1984
SA5137SW-D S-TEC System 60 pitch stabilization system ST-099 with optional autotrim system. Issued 2/24/1983
SA514GL Installation of Norton radome kit No. 4262X. Reissued 12/5/2000
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
SA5156NM (PG 2) Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 7/29/2010 0:00
SA5160SW-D S-TEC System 60 two axis automatic flight guidance system Model ST-162 with optional automatic electric trim system. Amended 6/24/1992
SA5161SW-D S-TEC yaw damper system ST-164. Issued 5/20/1983
SA5163SW-D Installation of S-TEC System60 single axis automatic flight guidance system ST-161. Amended 3/22/1993
SA5164SW-D S-TEC System 60 pitch stabilizer system ST-163 with optional automatic electric trim system. Amended 2/23/1993
SA5255SW-D S-TEC System 40/50 single and two axis automatic flight guidance system ST-203-40/50. Amended 2/10/1993
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)