Piper PA30C Turbo

Number of Active Aircraft: NA Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 2415 lbs
Max Weight 3725 lbs
Useful Load: 1310 lbs
Engine Name LYC IO-320-C1A
Engine Number 2
Horsepower 160 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 30000 ft
Max Fuel 120 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 194 kts
GPH (75% BHP): 26
MPG (75% BHP) 7.5
Range (75% BHP): 783 nm
Fuel Cost Per Seat Mile 0.13 $
Fuel Cost Per Hour 156 $
MPG per 1000 lbs of Payload 9.77
F-T (Speed^2/FuelBurn) 14.5 HP
F-T Payload 19 kts
MPH To HP: 12.1 kts
T/O Roll - T/O over 50 FT OBST 990 ft / 1590 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
SA00027SE Installation of CAPCO Auxiliary Nacelle Fuel Tanks Reissued 9/9/2003
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
SA00160SE 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
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
SA00187DE Installation of Oilamatic Preoiler system. Issued 10/5/1995
SA00193AT Installation of carbon steel discs. Reissued 11/14/1994
SA00229NY Installation of Sky Harbour Aircraft Refinishing Ltd Ice Damage Prevention Plates. (PA-23-250 6 place) Amended 1/24/1997
SA00233SE Installation of the Precise Flight Series 100 Speedbrake System Amended 3/10/2005
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
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
SA00356WI Installation of a 10.2 gallon auxiliary fuel tank in each wing nacelle and associated changes. Reissued 9/8/1995
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
SA00449AT Installation of flap gap seals. Issued 3/31/1994
SA00484WI Installation of shoulder harness for two front seats. Reissued 3/25/2009
SA00563AT Installation of Appalachian Accessories carbon steel brake discs P/N AA-22. Reissued 1/24/1995
SA00670AT Installation of an OCEM AP-2C or AP-3C autopilot system in accordance with Automatic Flight Systems OCEM AP-2C AP-3C Installation Manual for Aircraft Piper Models PA-30 and PA-39 Reissued 4/6/2004
SA00676CH Replace existing spinner with either Hartzell spinner P/N D-5749L or D-5749LP. Issued 5/20/1997
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
SA00726CH Replace lower cabin door sill. Issued 8/5/1997
SA00729SE Installation of twin temperature indicating system with fuel flow in accordance with J.P. Instruments (JPI) Installation manual Report No. 760 Revision - dated 7/20/99 or later FAA approved revision. Amended 11/30/2005
SA00733AT Installation of composite aft spinner bulkhead and/or composite spinner. Amended 3/31/2004
SA00735AT Installation of composite aft spinner bulkhead and/or composite spinner. Amended 10/13/2000
SA00746WI Installation of diagonal shoulder harnesses for the rear seats. (PA-30 S/N 30-1 thru 30-901) Reissued 3/25/2009
SA00763SE Installation of vortex generators on the wing leading edge and vertical fin surfaces. Issued 12/21/1999
SA00780SE (PAGE 1) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00786SE Installation of Aviation Innovations fuel pump motor modification in accordance with Aviation Innovations Drawing List DLPA30 Revision G dated August 1 2002 or later FAA approved revision. Amended 10/10/2002
SA00804SE Installation of an engine failure indicator system also referred to as a low Thrust Detector system.  Amended 7/16/2000
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00906AT Installation of replacement fuel cell assemblies for left-hand and right-hand auxiliary tank. Reissued 4/27/2009
SA00944CH Replace Janitrol/JanAero Combustion Heater Model 81D94-X (XX) with C&D Associates Combustion Heater Model CD45K either P/N RA-81D94-3 or P/N CD81D94-3. (95-B55 S/N TC-1658 and up E55 S/N TE-959 TE-968 and up 58 S/N TH-437 and up) Amended 6/20/2000
SA00971CH Remove South Wind 940 series combustion heater and install C&D Asociates TSO-C20 approved heater kit model CD35K or CD45K (310A (USAF U-3A) S/N 35000 trhu 35546 PA-23 S/N 23-1 and up 27-1 thru 27-3049 27-3051 thru 27-3053 PA-30 S/N 30-2 thru 30-401) Amended 3/29/2004
SA01085LA (PAGE 2) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
SA01105WI-D (2 OF 2) Installation of Bendix/King KMD 550/850 Multi-Functional Display System with optional traffic terrain and weather sensors. This STC applies to both single-engine and small multi-engine aircraft (see 1 of 2 for small twin-engine). Amended 5/31/2007
SA01114CH Installation of P2 Incorporated 6600 Audio Advisory system Reissued 11/4/2013
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
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
SA01252SE Installation of engine mount heat shield modification in accordance with Oregon Aircraft Design Drawing List DLPA30 dated September 24 1999 (PA-30 PA-39) or DLPA30T dated August 28 1999 (Turbocharged PA-30 PA-39) or later FAA approved revisions to either document.  Reissued 1/20/2004
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
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
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
SA01516AT Installation of Vision Micro Systems Inc. VM1000/EC100 digital/analog engine instrumentation and caution advisory system. Amended 10/24/2008
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
SA01571CH Installation of modified nose cone. Issued 11/16/2001
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
SA01828SE Installation of J.P. Instruments (JPI) EDM-960 Primary Engine Data Management System Reissued 5/12/2011
SA01834CH (1 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009
SA01860NY (3 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
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
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
SA02096AK Installation of hourmeter airspeed switch. (PA-23-250 Navy UO-1) Issued 12/17/1997
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
SA02146AT Replace alternators solid state voltage regulations and wiring harness with Electrosystems equipment. Reissued 3/9/2009
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 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
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
SA02293AK (2 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02297AK Installation of a fixed mounted Max-Vis Enhanced Vision System (EVS) Model 1000 to include a nose mounted conformal fairing and associated sub structural mount a forward nose compartment mounted power supply an aft avionics rack installed 12 to 24 VDC power converter and a dash mounted dedicated display monitor. Issued 9/9/2007
SA02492CH Installation of a Three Point Torso Restraint System. Issued 10/29/2007
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
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
SA03708AT Replacement of the Main Landing Gear Housing Issued 6/2/2009
SA04019AT Installation of The Aeronautical Design Service (ADS) part number 1008020828 Stabilator Horn Reissued 9/12/2013
SA09359AC-D Installation of S-TEC System 20/30 single and two-axis automatic flight guidance systems Model ST-816-20/30. Amended 7/15/2008
SA09363AC-D Installation of S-TEC system 30 alt altitude hold system. Issued 5/8/1998
SA1007NW Installation of a low thrust detector system. Reissued 3/6/1998
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
SA1022NE Installation of 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
SA1027SW Mitchell manual electric pitch trim AK267. Reissued 7/9/1984
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
SA1111SW Outer wing integral auxiliary fuel tanks and increase gross weight of180 pounds. Amended 3/14/1983
SA1112SW Dorsal fin. Amended 3/14/1983
SA1113SW Extended nose with baggage compartment. Amended 3/14/1983
SA1114SW Nacelle baggage compartments. Amended 3/14/1983
SA1115SW Dual brakes. Reissued 11/22/1998
SA1151SW Lycoming IO-360-C1C engines(200 hp) with Hartzell HC-C2YK-2/ C7666A-4 propeller. Amended 3/14/1983
SA1152SW One-piece windshield. Reissued 3/14/1983
SA1153SW Square wing tips with dual navigation lights. Amended 9/7/1999
SA1154SW Rudder and aileron interconnect system. Reissued 3/14/1983
SA1202WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1239SW Turbosupercharged Lycoming IO-360-C1C engines. Reissued 3/14/1983
SA1254SW Installation of electrothermal propeller de-icing system. Aircraft must be placarded: WARNING. THIS AIRPLANE NOT APPROVED FOR FLIGHT INTO KNOWN ICING CONDITIONS. Reissued 11/22/1998
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
SA1320CE Chrome-plated brake disc installation. Amended 6/20/1977
SA1337SW Pneumatic de-icing system. Reissued 11/22/1998
SA1341SW Nose taxi light. Reissued 3/14/1983
SA1342SW Mitchell automatic flight system AK296 cons. of Piper altimatic IIIB-1 autopilot w/opt. Automatic pitch trim radio and glide slope couplers. Reissued 7/9/1984
SA1343SW Mitchell automatic flight system AK325 cons. of Piper autoflite II w/opt. tracking system. Reissued 7/9/1984
SA1344SW Mitchell command electric trim AK267. Issued 7/20/1971
SA135EA Installation of engine exhaust combustion monitor. Reissued 2/14/1972
SA1386SW Mitchell automatic flight system model AK339 cons. of Piper auto-control III autopilot with optional radio coupler. Reissued 7/10/1984
SA1401CE Install King Model KNS 80 digital area navigation system. Reissued 2/28/2000
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1431NM Installation of a Shadin 910502 or 910514 Digiflo digital fuel flow indicator system and optional removal of the fuel pressure indicating system on Piper PA-30 and PA-39 airplanes equipped with Lycoming Model IO-320-B1A and LIO-320-B1A or IO-320-C1A and LIO-320-ClA engines. Reissued 3/1/1988
SA1446NM-S Installation of 15x6.00-6 tire on original equipment nose wheel Issued 1/20/1982
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA148SW Replacement of right front seat with stretcher. Reissued 8/21/1987
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1512WE (2 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007 0:00
SA1530GL Install PA-30 or PA-39 lower cowl oil drain access panel with relief for quick drain. Amended 3/1/1991
SA1533GL Installation of on-board engine analyzer system. Issued 11/30/1990
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
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1638SW Mitchell automatic flight system AK355 consisting of Century I with omni tracker. Reissued 7/16/1984
SA1662GL Installation of rudder fin cap fairing with or without a strobe. Reissued 5/7/1997
SA1675NM Installation of a third seat belt in the center of the rear bench seat Issued 7/15/1982
SA1675WE Installation of exhaust gas temperature monitoring systems EGT-2. Amended 8/28/1974
SA1689SO Installation of shoulder harness. Issued 10/19/1984
SA1696NM Installation of Shadin 910502 Digiflo fuel flow indicator system and removal of fuel pressure indicating system. Reissued 3/17/1988
SA1712GL Installation of Gear Lobe fairings. Reissued 5/7/1997
SA1753NM Removal of the factory equipped vertical fin mounted rotating beach and installation of a vertical fin mounted Whelen strobe light assembly Issued 10/13/1982
SA1754NM Installation of a Shadin 910502 or 910514 Digiflo digital fuel flow indicator system and removal of the pressure indicating system on PA-30 and PA-39 airplanes equipped with Lycoming IO-320-B1A and LIO-320-B1A engines. Amended 2/7/1983
SA1756NM Installation of positive flap retraction system. Reissued 9/8/2005
SA1806SO Installation of nose landing gear tire. Issued 7/10/1985
SA184EA Installation of 13-quart alcohol propeller anti-icing kit utilizing either a Weldon pump (P/N 100B-6) or a Bendix pump (P/N 478360). Amended 10/15/1971
SA1870NM Installation of Aileron Gap Fairings Issued 4/18/1983
SA188SO Flight control wheel. Issued 1/1/1960
SA18CH Installation of windshield cowler fairing. Reissued 5/7/1997
SA1935WE Installation of Brittain Industries Inc. Model B5 B2C or NAV-2B Flight Control System Reissued 2/6/2013
SA209GL 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
SA214CH Installation of Hartzell HC-E2YL-2BSF/F7663D-4 or HC-E2YL-2BLSF/ FJ7663D-4 model propellers. Reissued 5/7/1997
SA215CH Installation of an induction system. Reissued 5/7/1997
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA225EA Installation of Monitair angle of attack and stall warning system. Reissued 2/14/1972
SA2273NM Installation of fiberglass window mouldings. (PA-30 SN 30-1 thru 30-901) Issued 4/16/1984
SA2312WE Installation of leading edge cuffs stall fences stall strips drooped ailerons flap actuated stabilator trim system raked wing tips(optional) and dorsal fin. Reissued 9/8/2005
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
SA233EA Reservoir-type pneumatic wing and tail deicing system. Amended 10/7/1970
SA2350NM Page 2 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2484CE Installation of side windows with an increase of thickness from 1/8 inch to 1/4 inch. Issued 4/14/1989
SA2550CE Installation of a Webco door latch kit per Webco Aircraft Drawing List2430-101. 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
SA2586NM (PAGE 4) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2647CE Installation of flap actuated gear warning system. Reissued 5/7/1997
SA2652CE Installation of main fuel cell bladders as replacements for original bladders. Reissued 7/31/2002
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
SA271GL Installation of Great Lakes forward windows P/N s W- W/T- W/G-2058-187 or -250 and W- W/G-20599-187 or -250. Reissued 11/26/2008
SA282CE GUART System (Gear-up automatic response device). Issued 1/1/1960
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2849WE Installation of oxygen system. Reissued 1/26/1984
SA2949SW Addition of Hydro Seal Fluid Additive to landing gear shock struts. Reissued 8/8/1980
SA3028SW-D Mitchell auto. Flight system AK481 consisting of Piper altimatic IIIC autopilot with command automatic electronic pitch trim system optional radio and glide slope couplers. Reissued 8/16/1984
SA3036SW-D Mitchell automatic flight system AK506 consisting of Piper Autocontrol IIIB autopilot with optional radio coupler. Reissued 6/21/1984
SA3045SW-D Mitchell automatic flight system consisting of Century IIB autopilot with optional radio coupler. Reissued 6/22/1984
SA308CH Replace baggage door holdup bracket with air strut bracket. Reissued 5/7/1997
SA3105SO Installation of speed spats main landing gear fairings. Issued 12/18/1991
SA3128SW-D Mitchell automatic flight system AK598 consisting of Century III autopilot with optional command automatic trim radio and glide slope couplers. Reissued 6/5/1984
SA313SW Pitch trim system AK124. Issued 1/1/1960
SA3205NM Installation of fiberglass wing tips. Issued 12/6/1985
SA3282SO Installation of flap bracket fairings. Issued 7/13/1992
SA3302SO Installation of fiberglass nose bowl. Amended 3/4/1993
SA331SO External power supply plug. Issued 1/1/1960
SA3336WE Installation of single piece windshield. Reissued 4/8/1999
SA334SW Installation of InterAv Alternator. Reissued 7/20/1981
SA3395SW-D Installation of Mitchell automatic system AK893 consisting of Century IIB autopilot. Reissued 8/24/1983
SA343SW Automatic pilot AK127 AK127E or AK127E-3 and lateral guidance radio coupler AK123. Issued 1/1/1960
SA3468SW-D Installation of Century automatic flight system Modedl AK974 consisting of a Century 2010/2030/2031/2050/2051 autopilot. Amended 10/21/1992
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA3563NM Installation of ARNAV Systems FC-10/FT-10 digital fuel flow indicating systems. Issued 9/14/1987
SA3707WE Installation of single piece windshield. Reissued 6/25/2001
SA370CH Installation of wing fillet. Reissued 5/7/1997
SA3729WE Installation of Hoskins Model CFS-2000 -2001 or FT-200 fuel flow indicating system. Reissued 1/30/1998
SA3862NM Page 1 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA394CH Installation of cowl nose bowl. Reissued 5/7/1997
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
SA4066WE Installation of Silver Instruments Fueltron IIIG or IIIP digital fuel flow and totalizer system. Reissued 4/29/1991
SA4189WE Installation of DTL-1000 -1001 and/or -1002/3 autopilot adapters for the Edo-Aire Mitchell Centrury III autopilot. Issued 7/29/1980
SA4238WE Installation of inflatable door seal. Issued 9/25/1980
SA426CH Installation of electronic tachometer fuel flow manifold pressure and fuel totalizer instruments. (PA-30 SN 30-147) Issued 10/18/1995
SA428NE Installation of William C. Roberts brake discs P/N 202-22SS in lieu of Piper brake discs P/N 754-554. Amended 12/15/2003
SA4295SW Propeller synchrophaser system. Issued 3/6/1981
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
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
SA477EA SAGA (semi-automatic gear actuating) system. Issued 1/1/1960
SA4852NM Installation of electrical heater including engine driven alternators and controls. Issued 4/4/1990
SA5112SW-D Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-127 with optional autotrim system. Amended 1/23/1997
SA5138SW-D Install S-TEC System 60 pitch stabilization system Model ST-128 with optional autotrim system. Amended 3/19/1997
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
SA5159NM (1 OF 2) Installation of chip detector system. Amended 11/6/1992
SA516GL Installation of aileron flap flap to fuselage rudder gap seals wing root fairings dorsal fin and engine nacelle fairing. Reissued 1/21/1999
SA520SO Installation of Bendix FCS-810(Piper Altimatic V/F/D) automatic flight control including manual electric trim and optional flight director indicator. Amended 8/13/1976
SA5227SW-D Install S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-205-40/50. Amended 3/28/1997
SA524SW Pitch trim system AK164. Issued 1/1/1960
SA525SW Piper autocontrol III Mitchell AK161 autopilot. Issued 1/1/1960
SA531SW Fifth seat. Issued 1/1/1960
SA533NW Installation of aileron trim. Issued 10/19/1977
SA534EA Replacement of existing stall warning detector Safe Flight P/N C-52207 with pre-stall warning and speed control transducer Safe Flight P/N 792 and speed control indicator P/N 571. Issued 1/2/1990
SA551CH Modify the fuselage nose cover. Issued 9/12/1996
SA557GL Installation of Hartzell Propeller Models HC-E2YL-2BSF/F7663-6Q and HC-E2YL-2BLSF/FJ7663-6Q and Hartzell D-5749(P) or D-5749(P) spinners. Amended 6/22/1999
SA559WE B-4 flight control system including autopilot PC-1 pitch assist AH-1 altitude hold and NAV-1 navigation coupler. Reissued 10/1/1973
SA563CH Authorizes installation of engines equipped w/Unison Limited Authority Spark Advance Regulator (LASAR) ignition system w/Cylinder Head Temp. (CHT) monitoring capability on airframes. engines. Reissued 2/10/2009
SA5656NM Installation of burglar alarm system. Reissued 7/21/1993
SA5656NM (PAGE 1) Installation of burglar alarm system. Reissued 7/21/1993
SA576SW Installation of Mitchell automatic flight system model AK186 consisting of Piper altimatic IIIB autopilot radio coupler and automatic aileron stabilizer model AK179. Reissued 6/25/1984
SA581SW Installation of Mitchell automatic aileron stabilizer model AK179. Reissued 6/25/1984
SA5841NM Installation of an engine electronic digital tachometer. Reissued 1/14/2002
SA589WE Full flow oil filter F-94056 and F-94056-12 with element E-3560 MEL 800. Reissued 10/5/1976
SA591CE Install Alco XW20101-PA-30-L windshield wiper system. Issued 1/1/1960
SA5924NM Installation of RPM instrument. Amended 11/24/1997
SA5925NM Installation of oil pressure/temperature instrument. Amended 12/8/1997
SA5926NM Installation of manifold pressure instrument. Amended 8/15/1993
SA593CH (3 OF 5) Install Champion SlickSTART magneto booster system. Reissued 2/10/2009 0:00
SA5983NM Cockpit sun visor installation. Reissued 3/24/2003
SA6058SW-D Installation of S-TEC manual electric trim system Model ST-355. Issued 3/19/1986
SA615EA (PAGE 2) Installation of Whelen Anti-Collision Strobe Light Systems Part Number 01-0770006-( ) 01-0770028-( ) 01-0770029-( ) 01-0770062-( ) 01-0770900-( ) and 01-0771055-( ) as replacement for originally installed anti-collision lights. Reissued 7/6/2010
SA630WE Installation of oil filter assemblies. (NAVION A AND B with optional engine) Reissued 8/29/1974
SA634NE Installation of Cleveland Wheel & Brakes (Parker Hannifin). Issued 2/21/1989
SA662SW Installation of Mitchell automatic flight system model AK220 consisting of Century III autopilot with option automatic pitch trim automatic aileron stabilizer and radio coupler. Issued 6/25/1984
SA662WE Hi-Lo sensitivity adaptor BI-400 and autopilot with NAV-1 navigation coupler and heading lock. Reissued 10/1/1973
SA673EA Installation of radome kit 3058X. Amended 5/26/1976
SA676EA Installation of Norton Company radome kit 3058-B. Amended 3/24/1971
SA693CE Replace existing engine induction air filter with AC Spark Plug filter. Reissued 6/20/2000
SA7063NM Installation of acrylic window liners in accordance with FAA approved Drawing Lists. Drawing lists are listed on FAA approved Model List Number SA7063NM or later FAA approved revision. Reissued 10/17/2008
SA7151SW-D Installation of S-TEC System 65 two axis automatic flight guidiance system Model ST-414. Amended 3/31/1997
SA71GL Installation of air filters Reissued 6/20/2000
SA727WE Installation of Brittain Industries Model TT-5 wing tip fuel tanks. Reissued 9/17/1987
SA72RM Installation of camera wells. Amended 12/9/1976
SA738CE Install King Radio KNC 610 area navigation computer. Reissued 2/28/2000
SA756SW Installation of Mitchell automatic flight system model AK236 consisting of Century II autopilot with optional radio coupler. Reissued 6/25/1984
SA766WE Plastic wing tips replaced with Speedplates SP51463. Issued 6/6/1965
SA767WE Modification to include three pair of seat belts on rear seat to accommodate three passengers. Issued 1/1/1960
SA776CE Installation of King Radio KN-74 area navigation computer. Reissued 2/28/2000
SA787WE Installation of turbosupercharged Lycoming IO-320-B1A IO-320-C1A LIO-320-B1A or LIO-320-C1A engines in accordance with FAA sealed Rajay Drawing List No. RJ0600.  Reissued 6/26/2006
SA789CE Install Woodward propeller unfeathering accumulator kit number 213630. Reissued 3/20/1992
SA800EA (PAGE 2) Installation of Aviation White Anti-Collision Strobe Lights. Whelen Models A429 A430 A434 A450 A408 (white) A408R/W or A47OR/W (red/white) A500 A625 or A650 and associated power supplies or Model SA strobe light system. Amended 7/6/2010
SA808NW Installation of an Edo-Aire Mitchell Century IIB autopilot (approved for installation on a Piper PA-30 by STC SA3045SW) on a Robertson modified PA-30 (STC 2312WE) Issued 7/26/1979
SA808SW Installation of Mitchell Model AK246 omni-tracker. Applicable only to aircraft modified by STC SA615SW. Reissued 6/29/1984
SA816EA Installation of 13 quart alcohol propeller anti-icing kit WAP-500B. Amended 10/15/1971
SA838SW Installation of Mitchell glide slope coupler Model 1C493. Reissued 6/29/1984
SA8430SW Installation of an EQ1500 paralleling relay. Issued 8/26/1992
SA8431SW Installation of R15VON alternator control unit. Amended 1/6/1994
SA848EA Installation of pneumatic pump operated wing and tail de-icing boot system. Issued 10/22/1970
SA8513SW-D Installation of a Century Automatic Flight System Model AK1017 consisting of a Century 2110/2130/2131/2150/2151 autopilot. Issued 2/19/1996
SA871WE Installation of fiberglass wing tips. Amended 9/23/1996
SA875GL Install speed sweep windshield. Reissued 5/7/1997
SA8891SW-D Install S-TEC System 55 2 axis automatic flight guidance system Model ST-562 with optional autotrim system. Amended 4/18/2001
SA890EA Installation of Grimes three light strobe kit P/N 34-0101-2 as supplemental lighting. Reissued 6/4/2007
SA891SO Remove existing windshield and install single piece windshield. Reissued 8/16/2011
SA8922SW Installation of replacement Ultimate Engine Oil Filter for Textron Lycoming and Teledyne Continental engines. (411 S/N 000 THRU 0126 S/N 0127 AND UP) (T188C S/N 03474 AND UP) (206 S/N 05030 AND UP) (207 S/N 05227 AND UP) (T207 S/N 05227 AND UP) (P21 0 SERIES S/N 278 AND UP) (180 S/N 53087 AND UP) (210 S/N 63373 - 63375 AND UP) (B19 SPORT) Issued 7/21/1994
SA917EA Installation of Grimes aviation white anti-collision strobe light system two light or three light series 555 for wing tips and tail P/N 30-0555-( ). Reissued 6/4/2007
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST01494LA (PG 2) Installation of the FiberLite Aircraft Lighting System in accordance with Master Document List listed on Aircraft Model List (AML) Number ST01494LA or later FAA approved revisions. No flight manual is required. Reissued 8/30/2011
ST02547AT (2 OF 2) Installation of a voice alert system. Amended 5/13/2003
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)