PA-24 400

Number of Active Aircraft: 88 Active- Map

Description:

Designed for the 400 horsepower IO-720. The model looks much the same as previous model but incorporats strengthened tail compents. Not many were built only 148. The perforamance and reliablity of the engine turned out to be disappointing considering the size of engine.

277
Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 2110 lbs
Max Weight 3600 lbs
Useful Load: 1490 lbs
Engine Name Lycoming IO-720
Engine Number 1
Horsepower 400 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 19500 ft
Max Fuel 100 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 185 kts
GPH (75% BHP): 17
MPG (75% BHP) 10.9
Range (75% BHP): 974 nm
Fuel Cost Per Seat Mile 0.14 $
Fuel Cost Per Hour 102 $
MPG per 1000 lbs of Payload 16.21
F-T (Speed^2/FuelBurn) 20.1 HP
F-T Payload 29.9 kts
MPH To HP: 4.6 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1500 ft

SA00022WI Installation of seals on lower surface between the wing ailerons and flaps. S/N 24-2844 AND UP Amended 5/24/1993
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
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
SA00079SE Installation of low oil pressure warning in conjunction with ADC (Oberg) oil filter. Amended 11/10/1994
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00159SE Installation of modified instrument panel. Issued 12/12/1994
SA00161BO (3 OF 3 Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005 0:00
SA00175DE Installation of Oilamatic Preoiler system. Amended 4/14/2003
SA00193AT Installation of carbon steel discs. Reissued 11/14/1994
SA00198AT Installation of carbon steel brake discs. Reissued 11/14/1994
SA00198LA Relocation and replacement of the fuel boost pumps. (PA-24-250 S/N 24-2999) Issued 5/20/1996
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
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
SA00290AT Installation of cowl flaps NACA air vent scoops for cabin ventilation and additional main landing gear doors. Issued 8/2/1993
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
SA00327WI Installation of seals on lower surface of airplane between wing ailerons and flaps. Issued 6/6/1995
SA00336NY Installation of second wind auxiliary vacuum system. Reissued 6/18/2002
SA00343AT Installation of engine cowl and full length gear doors and relocation of engine oil cooler and replacement exhaust system. For PA-24-250 S/N 24-103 and up for PA-24-260 S/N 24-3642 24-4000 to 24-4782 and 24-4784 to 24-4803. Reissued 5/2/2001
SA00391SE Installation of Rajay Model 315 F10 turbocharger on the above aircraft with a Lycoming O-360-A1A engine installed. Reissued 5/18/1999
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
SA00423LA Installation of Hartzell HC-C3YR-1RF/F7590 propeller. Issued 8/21/1997
SA00424AT Installation of flap gap seals. Issued 2/14/1994
SA00426AT Installation of a composite WHOLLEY COWL. Amended 1/24/1996
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00484WI Installation of shoulder harness for two front seats. Reissued 3/25/2009
SA00618AT Installation of a stabilator modification kit. Issued 12/9/1994
SA00631CH Installation of the Hartzell propeller model HC-C2YR-1BF/F7666A-4 or HC-C2YR-1BFP/F7497 propeller Amended 5/14/2013
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
SA00695SE Replacement of certain Rotomaster and Rayjay scavenge pumps Amended 2/14/2003
SA00746WI Installation of diagonal shoulder harnesses for the rear seats. (PA-30 S/N 30-1 thru 30-901) Reissued 3/25/2009
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
SA00773CH Installation of McCauley propeller model B3D32C412/82NDA-5 and McCauley governor model DC290D1/T34. Reissued 7/19/2006
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
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00927AT Installation of composite propeller spinner. Amended 5/20/2004
SA00947AT Installation of composite spinner. 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
SA01026SE (PAGE 1) Improved fuel gascolator assembly. Amended 12/19/2012
SA01082AT Installation of new fiberglass cowling full length gear doors relocation of engine oil cooler and replacement of the exhaust system. (PA-24-180) Amended 1/26/1998
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
SA01120SE Installation of Door Steward. Amended 3/4/2010
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
SA01201AT Installation of left hand side and right hand side auxiliary tank fuel cell assemblies. Reissued 5/1/2009
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
SA01257AT Installation of composite spinner assemblies. Amended 10/13/2000
SA01280CH Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) Issued 8/29/2000
SA01299SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Micro AeroDynamics Inc. Drawing Package Document MA2191 Revision IR dated September 17 2003 and Installation Manual MA2192 Revision IR dated October 27 2003 or later FAA approved revision to either of these documents.  Issued 11/14/2003
SA01330LA (PAGE 2) Installation of alternate avionics support assembly. Reissued 10/6/2010 0:00
SA01349NY Installation of oil temperature coupler kit P/N ALH-I-005 with Airparts Installation Drawing List as listed on AML No. Sa01349NY. Issued 5/15/2001
SA01352LA Replacement of Piper Battery box part numbers 20659-00 21524-00 21524-02 25338-00 or 26240-00 and venting battery with Riley Aircraft Battery Box part number 1001TR and Gill manifold battery Model G-35M. Issued 7/18/2002
SA01421AT Installation of an OCEM AP-3C autopilot. (PA-24-180) Reissued 4/6/2004
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
SA01462WI Installation of 3-blade MT-Propeller model MTV-9-B/198-58a propeller and P-296-5 spinner Issued 12/21/2007
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
SA01487SE-D (Page 2) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01538AT Installation of Hartzell HC-C3YR-1RF/F7590 or HC-C2YK-1A or HC-C2YK-1B propellers. Issued 12/31/1997
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
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 (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
SA01834CH (1 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009
SA01853AT Replace Aluminum alloy propeller spinner with composite spinner. Amended 10/13/2000
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 (4 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
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
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
SA02033AT (PAGE 6) 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
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 2) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005 0:00
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
SA02260SE Move the main wheel brake calipers from the outboard side of the wheel forks to the inboard side of the wheel forks and modify the wing rib at station 33 Issued 1/7/2014
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
SA02492CH Installation of a Three Point Torso Restraint System. Issued 10/29/2007
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
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
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
SA03708AT Replacement of the Main Landing Gear Housing Issued 6/2/2009
SA04016AT Installation of The Aeronautical Design Service (ADS) part number 1008020828 Stabilator Horn Reissued 9/12/2013
SA09012AC-D Installation of S-TEC System 55 two axis automatic flight guidance system model ST-595 with optional automatic electric trim system. Eligible on Piper models PA-24 (PA-24-180) PA-24-260 when modified per STC SA4-1351 or STC SA4-1235 as applicable (wing tip tanks). Amended 5/30/2001
SA09260AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-715-20/30. (PA-24-180) Issued 7/29/1997
SA09266AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-716. Issued 8/12/1997
SA09413AC-D Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-777-40X/50X. Issued 9/12/2000
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA1-340 Oil-free vacuum pump PA-201. Issued 
SA1-383 Lube oil filter PB 55-1. Issued 
SA1-544 External electrical power receptacle. Reissued 10/15/1974
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
SA1021NE Installation of a single pane increased thickness side windows. Amended 4/2/1997
SA10236SC (3 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA1026SW Mitchell automatic flight system Model AK186 consisting of Piper altimatic IIIB IIIB1 automatic auto-flite automatic/command electric pitch trim radio and glide slope couplers. Reissued 7/9/1984
SA1027SW Mitchell manual electric pitch trim AK267. Reissued 7/9/1984
SA1033EA Replace steel oil cooler lines with Aeroquip type 303-8 hose using AN-823-8D elbows AN-816-8D nipples and AN-321-8 hose fittings. Issued 1/29/1976
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
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA108NE Replacement of brake disc Piper P/N 751672. Reissued 6/18/2002
SA1109WE Hanlon and Wilson exhaust system. Issued 1/1/1960
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1115SW Dual brakes. Reissued 11/22/1998
SA112CE APU receptacle. Issued 1/1/1960
SA113CE APU receptacle. Issued 1/1/1960
SA1152SW One-piece windshield. Reissued 3/14/1983
SA1153SW Square wing tips with dual navigation lights. Amended 9/7/1999
SA1167NW Installation of an updated instrument panel Issued 2/10/1981
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA1178EA Installation of Silver Instruments fueltron IG or IP or Fuelgard digital fuel flow indicating system Reissued 4/29/1991
SA1182NW Installation of a Hartzell propeller on a Lycoming engine Issued 2/18/1981
SA1202WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1216NW Installation of B.F. Goodrich de-icing boots Issued 4/14/1981
SA1268NW Installation of a Hoskins FT-101 computerized fuel system Issued 7/20/1981
SA127EA Installation of Monitair angle of attack system Model AA-2. Reissued 2/14/1972
SA1315CE Chrome-plated brake disc installations. Issued 6/1/1977
SA1315WE Installation of Mixture Monitor (exhaust gas temperature probe gage and selector) in accordance with Delta Products Part Lists A-192 and A-193 or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9 1981 or later FAA approved revision and/or Drawing List MM-127 dated November 15 1981 or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29 1968 copy attached or later FAA approved revision. Reissued 4/15/2011
SA1331SW Mitchell automatic flight system AK326 consisting of Piper autoflite II and optional tracking system. Reissued 7/9/1984
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA1394GL Installation of Pamco Emergency Backup Pneumatic System. (PA-24-400 S/N 26-2 AND UP) Amended 10/17/1989
SA1412NM Installation of a Beech Craft Vernier throttle PN 35-944046 and associated changes Issued 12/30/1981
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1485WE Installation of Brittain Industries Inc. Model B-11 B2C or BSS Flight Control System Reissued 1/29/2013
SA148SW Replacement of right front seat with stretcher. Reissued 8/21/1987
SA1497NM Installation of Shadin Digiflo fuel flow indicator system and removal of fuel pressure indicator system Issued 4/2/1982
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1521SW Mitchell automatic flight system AK393 consisting of Century I autopilot with optional omni tracker. Reissued 7/13/1984
SA1531GL Installation of on-board engine analyzer system. Reissued 10/25/1990
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1588WE Installation of supplemental exterior flashing lights. Issued 1/30/1968
SA1605WE Installation of Brittain Industries B-4A Flight Control System Reissued 7/2/2013
SA160SW Automatic pilot AK115 AK115E or AK115E-3 and lateral guidance radio coupler AK123. Issued 1/1/1960
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1628NM Installation of nose gear doors and mounting of wheel brakes on inboard side of wheel fork Issued 4/30/1982
SA1661GL Installation of rudder fin cap fairing with a strobe. Reissued 5/7/1997
SA1665NM Installation of a Shadin Digiflo P/N 910501 or Miniflo P/N 912001 series fuel flow indicator system. Reissued 4/12/1988
SA1667NM Installation of a Shadin Digiflo digital fuel flow indicator system Issued 6/28/1982
SA1689SO Installation of shoulder harness. Issued 10/19/1984
SA1706SW Portable solid oxygen system. Issued 7/27/1973
SA1711GL Installation of Gear Lobe fairings. Reissued 5/7/1997
SA1735GL Installation of Master Nag warning system. Amended 3/21/1994
SA1755NM Installation of positive flap retraction system. Reissued 9/8/2005
SA17CH Installation of windshield cowler fairing. Reissued 5/7/1997
SA1806SO Installation of nose landing gear tire. Issued 7/10/1985
SA1845WE  );INSERT INTO stc_table VALUES ( Installation of Vibration Isolation Products (VIP) engine mount P/N VIP-50804-20 on various aircraft as shown on FAA Approved Model List (AML) No. SA1845WE. Amended 10/17/2002
SA188SO Flight control wheel. Issued 1/1/1960
SA18SO Cockpit operated fuel drain valve. Issued 1/1/1960
SA1918WE Installation of Fiberglass wing tips. Issued 4/24/1969
SA191NE Replace original brake discs with discs modified in accordance with Roland Longarzo procedure. Reissued 10/4/1984
SA203SO Fyr-Fyter 23-4 2-1/2 pound dry chemical fire extinguisher. Issued 1/1/1960
SA2062WE Installation of Lycoming IO-540-R1A5 engine and Rajay turbosuperchargers. Reissued 6/1/1970
SA2071SO Installation of an adjustable trim tab on the left aileron. Issued 3/4/1987
SA208GL Installation of one piece windshield. Reissued 1/31/2007
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA2167NM Installation of the Precise Flight stand-by vacuum system (SVS). Amended 11/7/2003
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2269SO 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
SA2272NM Installation of fiberglass window mouldings. (PA-24-260 24-1 thru 24-4299) Issued 4/16/1984
SA230CE Airspeed indicator landing gear warning system. Issued 1/1/1960
SA2336SO Replacement of Cleveland brake discs P/N 164-19 or 164-119 with Appalachian Accessories stainless steel brake discs P/N 73-19. Reissued 9/29/1995
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 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2359WE Installation of Turbocharged Lycoming 10-720-A1A engine  Reissued 6/26/2006
SA2485CE Installation of side windows with an increase of thickness from 1/8 inch to 1/4 inch. Issued 4/14/1989
SA2495WE Installation of recontoured wing leading edge staff fences drooped ailerons in flaps down mode flap actuated stabilator trim system new wing tips SC-100 stall warning system. Reissued 9/8/2005
SA2541NM Installation of fiberglass wing tips. Issued 12/19/1984
SA2549CE Installation of a Webco door latch kit. Issued 10/27/1989
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA2584CE Installation of LH and RH main fuel cell bladders P/N s DF054-324 and DF054-325 as replacements for original bladders. Reissued 7/31/2002
SA2586NM (PAGE 4) 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
SA2648CE Installation of flap actuated gear warning system. Amended 12/15/1997
SA2652CE Installation of main fuel cell bladders as replacements for original bladders. Reissued 7/31/2002
SA2653WE Installation of Beryl D Reissued 7/14/2011
SA2654WE Installation of Pathfinder Model P2A( ) autopilot. Amended 7/3/1979
SA2674NM Installation of a Lamar Model B-00264-2 over-voltage relay and the replacement of the existing voltage regulator with Lamar regulator Model B-00288-1 Issued 11/27/1984
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 2) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009 0:00
SA2694CE Installation of manually controlled engine induction alternate air heat system. Issued 2/22/1991
SA270GL Installation of forward windows P/N s W- W/T- WG-2058-187 or-250 and W- W/G-20599-187 or -250. Reissued 11/26/2008
SA2713CE Installation of PRONAV global positioning system GPS-100 navigator. Reissued 10/7/1991
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA288CH Installation of Hartzell HC-C3YR-1RF/ F7590 propeller and 835-52P spinner. Amended 12/9/2002
SA2944SW Addition of Hydro Seal Fluid Additive to landing gear shock struts. Reissued 8/8/1980
SA2SO Fifth passenger seat. Issued 1/1/1960
SA3-309 L2-B autopilot with or without altitude control. Issued 1/1/1960
SA3-315 Arcon B automatic rudder control. Amended 4/26/1966
SA3-351 L-2B autopilot with optional altitude control and automatic approach coupler. Issued 1/1/1960
SA3042SO Installation of Speed Spats main landing gear fairings. Issued 10/18/1991
SA3045SW-D Mitchell automatic flight system consisting of Century IIB autopilot with optional radio coupler. Reissued 6/22/1984
SA3070WE Installation of single piece windshield. Reissued 4/8/1999
SA3074SW-D Mitchell automatic flight system AK547 consisting of Century I autopilot with optional omni tracker. Reissued 6/21/1984
SA3077SO Installation of speed spats main landing gear fairings and/or installation of Comanche speed slipper nose gear fairing. Amended 1/8/1992
SA307CH Replace existing baggage door hold up bracket with an air strut bracket. (PA-24-260 24-4247 24-4300 and up) Reissued 5/17/1997
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
SA3134SW-D Mitchell automatic flight system AK593 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 6/5/1984
SA3135SW-D Mitchell automatic flight system AK597 consisting of Century IIB autopilot with optional radio coupler. Reissued 6/5/1984
SA3136SW-D Mitchell automatic flight system AK609 consisting of Century I auto-pilot with optional omni tracker. Reissued 6/5/1984
SA313SW Pitch trim system AK124. Issued 1/1/1960
SA315SW Fabrication and installation of split rear seat back. Issued 1/1/1960
SA317NE Installation of Auto-Vac-2 manifold vacuum system. Amended 2/2/1990
SA31NW Installation of Madras wing tips. Issued 3/13/1973
SA3281SO Installtion of flap bracket fairings. Issued 7/13/1992
SA331SO External power supply plug. Issued 1/1/1960
SA334SW Installation of InterAv Alternator. Reissued 7/20/1981
SA3359NM Modification of the vacuum system including installation of an engine which has been modified by the addition of a second engine driven vacuum pump. Issued 4/15/1986
SA341CE SAGA (semi-automatic gear actuator) control system. Amended 9/6/1966
SA3451WE Installation of Hartzell HC-A3VK4/V7636D-0 or V7636N-0 constant speed propeller. Amended 5/27/1980
SA3466SW-D Installation of Century automatic flight system Model AK972 consisting of a Century 2010/2030/2031/2050/2051 autopilot. Amended 12/9/1992
SA3469SW-D Installation of Century automatic flight system Model AK975 consisting of a Century 2010/2030/2031 autopilot. Amended 5/3/1994
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3550NM Installation of Hartzell / HC-C2YK-1BF/F8477D-5R . propeller Issued 12/10/1986
SA3551NM Installation of Hartzell HC-C2YK-1BF/F8477D-5R propeller. Issued 12/10/1986
SA3559NM Installation of ARNAV systems FC-10 or FT-10 digital fuel flow indicating system. (PA-24-260 with fuel injected normally aspirated engine) Issued 12/19/1986
SA3565WE Installation of single piece windshield. Reissued 6/25/2001
SA360CH Installation of McCauley propeller Model B3D36C424/74SA-0. Reissued 7/19/2006
SA362WE Pneumatic pitch assist PC-1 and optional altitude hold AH-1. Reissued 10/1/1973
SA3684WE Installation of an air/oil separator. Reissued 9/28/2001
SA3707NM Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system. Issued 5/7/1987
SA371CH Installation of wing fillet. Reissued 5/7/1997
SA3773WE Installation of Hoskins Model CFS-1000 -1001 FT-100 or FT-101 fuel flow indicating system. *This installation limited to those aircraft with fuel injected engines. Reissued 1/30/1998
SA3776WE Installation of flexible stainless steel oil cooler hoses. Issued 11/1/1978
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA3872NM Installation of an AVCO Lycoming IO-540-R1A5 engine as modified per STC No. SE3873NM for the addition of induction air intercoolers. Reissued 4/27/1995
SA3955NM Installation of Weldon Model 8163A Auxiliary Fuel Pump in lieu of Dukes Model 4140-00-218 Fuel Pump Issued 10/11/1988
SA4-1032 Aerofilter 30409A full flow lube oil filter with element 1A0235. Issued 1/1/1960
SA4-1132 SP-3 autopilot less altitude and navigation-hold features. Issued 1/1/1960
SA4-1235 Installation of 15-gallon wing tip fuel tanks. Reissued 8/17/1987
SA4-1248 Fuel drain modified to incorporate a handle extending forward through front bulkhead. Issued 1/1/1960
SA4-1351 Wing tip fuel tanks installed. Reissued 9/17/1987
SA4-1501 AB-6562 and AB-6563 brake blocks. Issued 1/1/1960
SA4-572 Autopilot and optional navigation coupler add-on BI-300 BI-301 or BI-304. Reissued 10/1/1973
SA4-666 Installation of a Grimes D-7080-1-12 rotating beacon. Reissued 4/8/1991
SA4-852 Full flow oil filter 30409A with element 1A0235. Issued 1/1/1960
SA4-925 Magnetic flight director 2000. Issued 1/1/1960
SA4-955 Fiberglass vertical fin mount for either Grimes or Whelen WRM rotating beacons. Reissued 7/14/2005
SA4-956 Three seat belts to accommodate three persons or rear seat. Issued 1/1/1960
SA4-971 20-gallon auxiliary fuel tank in baggage compartment. Issued 1/1/1960
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
SA4014NM Installation of a McCauley Model B3D32C412/82NDA propeller. Reissued 4/27/1995
SA4150NM Installation of Precise Flight Series 100 Speedbrake System. Amended 11/7/2003
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4179WE Installation of inflatable door seal. Issued 6/30/1980
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4313NM Installation of a stainless steel exhaust crossover system with dual outlets and dual heat muffs Issued 4/28/1988
SA4317SW S-TEC system 60 two axis automatic flight guidance system Model ST-021 with optional autotrim flight director/steering horizon(14 volt system). Issued 3/26/1981
SA434NE Installation of William C. Roberts steel brake discs P/N 201-19-SS dated 6/29/85 in lieu of Piper carbon steel brake discs Piper 754-530. Reissued 8/7/2002
SA4361WE Installation of Silver Instruments Fueltron IG or Fueltron IP digital fuel flow indicating system. Reissued 2/2/1993
SA4384SW Installation of cabin vent system. (PA-24 SN 24-1 to 24-3687) Reissued 8/18/1992
SA4390SW Installation of single or dual toe brakes. Reissued 8/18/1992
SA4401SW S-TEC system 60 single axis flight guidance system Model ST-020(14 volt system). Issued 6/30/1981
SA4581SW Installation of S-TEC system Model ST-507 with optional autotrim system. Issued 1/11/1982
SA4582SW Installation of JASC 6550 12-volt50 amp alternator J12-100 SP voltage regulator and associated wiring. Reissued 2/17/1982
SA463GL Install instrument panel and instruments. (PA-24-250 24-2299 and above) (PA-24-260 24-3642 24-4000 thru 24-4802) (PA-24-400 26-2 and above) Issued 10/24/1980
SA466SW Pitch trim system AK147. Issued 1/1/1960
SA4721NM Installation of SynCon alarm system. Amended 5/8/1990
SA475SW Pitch trim system AK152. Issued 1/1/1960
SA478EA SAGA (semi-automatic gear actuator) system. Issued 1/1/1960
SA482WE Plastic wing tips replaced with Speedplates . Issued 6/6/1965
SA489EA Installation of ARP Inc. carburetor ice detection system Models 107AP (-12 -R-12 -24 and -R-24 series) in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Precision A ir-Motive (Facet or Marvel-Schebler) MA-2 MA-3 MA-3SPA MA-4 MA-4-5 MA-4SPA MA-5 MA-6 MA-6AA and HA-6 series carburetors. Amended 12/5/2002
SA48WE Belly-mounted rotating anti- collision light to supplement top fuselage-mounted standard rotating light. Issued 1/1/1960
SA4958NM Installation of a hand control for the rudder. Issued 8/2/1990
SA5-27 Remove Lycoming O-540-A1A5(250 hp) engine and install Lycoming O-540-B1B5 (235 hp) engine. Amended 3/3/1962
SA510CE Modify electrical system to combination 12/24 volt system for starting engine. Issued 1/1/1960
SA511WE Lycoming O-540-B1B5 engine Hartzell HC-A2XK-1/8433-7 propeller required. Issued 1/1/1960
SA5156NM Fabrication and installation of Pulsar-MOSFET Landing Light Flasher System Amended 5/22/2012
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)