Piper PA34-200 Seneca

Number of Active Aircraft: 3 Active- Map

Description:



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Fuel Cost ($):
General Stats:
Seat Capacity: 6
Empty Weight: 2590 lbs
Max Weight 4000 lbs
Useful Load: 1410 lbs
Engine Name LYC IO-360-C1E6
Engine Number 2
Horsepower 200 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 20000 ft
Max Fuel 100 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 161 kts
GPH (75% BHP): 21
MPG (75% BHP) 7.7
Range (75% BHP): 671 nm
Fuel Cost Per Seat Mile 0.13 $
Fuel Cost Per Hour 126 $
MPG per 1000 lbs of Payload 10.81
F-T (Speed^2/FuelBurn) 12.3 HP
F-T Payload 17.3 kts
MPH To HP: 8.1 kts
T/O Roll - T/O over 50 FT OBST 750 ft / 1140 ft

SA00009SE Fiberglass wing tips and wing tip landing lights. Reissued 12/23/2011
SA00024NY Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Amended 10/3/2012
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
SA00072SE Cockpit sun visor installation. Amended 6/2/2005
SA00073AT Installation of main landing gear fairings. Issued 1/14/1993
SA00079NY Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00109SE Installation of vortex generators on the wing and vertical stabilizer and split flaps mounted on the lower trailing edge of the flaps Amended 8/12/1994
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
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
SA00243BO (4 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00261NY Installation of Aviation Services Inc. Model 1201 Cockpit Utility Light. Reissued 12/31/2002
SA00269BO (3 OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00290BO ( PAGE3) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010 0:00
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
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00474DE Installation of Oilamatic Preoiler system. Amended 5/17/2004
SA00654SE Replacement of certain BF Goodrich pneumatic deicer boots Reissued 5/4/2000
SA00666WI-D Installation of Bendix/King KFC 225 automatic flight control system. Approved for serial no. 3448038 thru 3448079 3449001 and later Issued 9/13/2000
SA00693CH Installation of an erosion protective nose cover Issued 7/21/1997
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
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
SA00793NY Installation of NLG downlock link assist. Reissued 12/6/2000
SA00821AT Installation of composite aft spinner bulkhead and/or composite spinner. Amended 10/13/2000
SA00823CH Installation of various de-icer wire harnesses. Reissued 10/10/2002
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00869AT-D Installation of replacement fuel cell assemblies (FFC replacement part number 573 is eligible for installation on Piper Seneca II models Pa-34-200T serial numbers 34-757001 and subsequent and Piper Seneca III models PA-34-200T serial numbers 34-8133001 and subsequent.). Reissued 4/16/2009
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
SA00996AT Installation of composite skinner. Amended 10/13/2000
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
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
SA01081AT Installation of Composite Spinner. Amended 10/13/2000
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
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
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
SA01337LA Installation of replacement wing tip fairing assemblies and stabilator tip fairing assemblies. Issued 6/7/2002
SA01384CH Installation of various de-icer harnesses. Issued 1/30/2001
SA01434AT Installation of a one-piece windshield Issued 7/23/1997
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
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
SA01627WI Installation of replacement gas spring door stays on the forward and/or rear cabin doors in accordance with Sioux Center Aviation Drawing List 65DL Revision C dated October 18 2010 or later FAA-approved revisions. Issued 4/4/2011
SA01643SE Installation of BAS Inc. shoulder harness with inertia reel Amended 12/2/2010
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01681SE Installation of vortex generators on the wings horizontal and vertical tail surfaces (all models) and an increase in maximum zero fuel weight (PA-34-200T and PZL M20 03 only). Amended 10/25/2006
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (4 OF 5) Installation of an antenna Amended 2/15/2007
SA01786SE Fabrication and installation of wing tips Issued 9/7/2007
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
SA01860NY (3 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
SA01923LA Installation of the P-1000 Digital Electronic Tachometer. Issued 1/23/2007
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 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
SA02096AK Installation of hourmeter airspeed switch. (PA-23-250 Navy UO-1) Issued 12/17/1997
SA02110CH (PAGE 3) 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
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 2 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
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
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
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
SA02785CH Installation of C&D Associates 24-volt combustion heater pump P/N CD52050  Issued 12/2/2009
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09194AC-D Installation of S-TEC Yaw Damper System Model ST-652. Issued 12/17/1996
SA09385AC-D Installation of S-TEC system 55 two axis automatic flight guidance system model ST-842 with optional autotrim system. Amended 12/8/2000
SA09520AC-D Installation of S-TEC Altitude Selector/Alerter Mode ST-1000. Issued 4/9/2002
SA09566AC Installation of a pilot-side Electronic Flight Instrument system. Issued 7/31/2002
SA1007NW Installation of a low thrust detector system. Reissued 3/6/1998
SA1015GL Installation of a Cooling Shroud on engine driven dry air pumps. Amended 5/1/2007
SA10236SC (3 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10530SC Installation of Cargo Net. Issued 1/10/2007
SA106RM Installation of freon air conditioning system. Reissued 5/17/2013
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1118SO Installation of Hartzell 3-bladed propellers Models - PHC-C3YF-2( )UF/FC-7663-2R and PHC-C3YF-2L( )UF/FJC-7663-2R or PHC-C3YF-( )UF/FC-7663B-2R and PHC-C3YF-2L( )UF/FJC-7663B-2R. Issued 12/21/1979
SA1147CE Installation of King Model KFC 2002 axis (3 optional) flight control system autopilot only or autopilot with flight director. Reissued 2/28/2000
SA1217SO Installation of an adjustable trim tab on the left aileron. Amended 11/4/1981
SA1225GL Install fairings over flap hinges. Amended 7/14/1997
SA1238GL Install wing root fairings. Amended 7/14/1997
SA1310SW Installation of stretcher in lieu of rear seats. Amended 11/18/1993
SA1321SW Mitchell automatic flight system AK298 cons. of altimatic IIIB-1 autopilot w/opt automatic command electric pitch trim radio coupler and glide slope coupler. Reissued 7/9/1984
SA1322SW Mitchell automatic flight system Model AK335 cons. of Piper auto- control III w/opt. radio coupler. Reissued 7/10/1984
SA1323SW Mitchell command electric pitch trim Model AK321. Reissued 7/9/1984
SA1336GL Install Egan Aviation Air Ambulance Stretcher Model EAS. Reissued 5/1/1997
SA1344SO Installation of Safe Flight SC-150 angle of attack indicator. Issued 6/25/1982
SA1363CE Chrome-plated brake disc instal- lation. Issued 8/18/1977
SA1393SO Installation of Speed Enhancement Kit. Reissued 6/20/2000
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
SA1512WE (2 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007 0:00
SA154NW Installation of full span flaps by removing aileron and changing deployment route of all flaps. Reissued 9/8/2005
SA154RM Install Hoskins Displays Model CFS-2000 or CFS-2000A -2001A or FT-200 fuel flow indicated systems. Reissued 1/30/1998
SA1553CE-D Installation of King KAS 297 altitude selector option in airplanes equipped with KFC 200 Flight Control System with Flight Director installed under STC SA1147CE. Reissued 2/28/2000
SA1575CE-D Install KAP-100 single axis KAP-150 two or three axis or KFC-150 two or three axis flight control system optional KAS-297B vertical speed and altitude selector and KFC-150 system with optional flight director displays. Reissued 2/28/2000
SA1601GL Installation of on-board engine analyzer system. Issued 5/13/1991
SA1626NM Page 2 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1640NM Installation of a modified air induction system to the Continental TS1O-360 engine turbocharger compressor (Rajay) system. Reissued 6/9/1995
SA1643NM Installation of a Fiberglass engine cowl nose bowl Reissued 5/30/1986
SA1644NM Installation of a Fiberglass upper tail cone Reissued 5/30/1986
SA1645NM Installation of a Fiberglass lower tail cone Reissued 5/30/1986
SA1673NM Installation of Demers super tips. Issued 7/13/1982
SA1675WE Installation of exhaust gas temperature monitoring systems EGT-2. Amended 8/28/1974
SA1694NM Installation of a Turboplus Inc. Model PA-34-2000A I.A.D. intercooler system on a Continental TSIO-360 series engine-turbocharger compressor (Rajay) system Davtron Model 301FD Delta temperature indicator and associated systems. Reissued 3/14/2006
SA1715GL Installation of Gear Lobe fairings. Amended 7/14/1997
SA1719SW Provide hole in fuselage for camera installation. Reissued 7/15/2010
SA1761NM Installation of a pressurized magneto system on the Continental turbocharged TSIO-360 and LTSIO-360 series engines. Reissued 3/14/2006
SA1797NM Installation of a Continental TSIO-360-KB and LTSIO-360-KB or TSIO-360-EB(c) and LTSIO-360-EB(c) (Converted)* engines and associated systems Reissued 5/21/2012
SA2009SO Installation of a one-piece windshield. Reissued 11/23/1987
SA20GL Installation of Woodward Type II electronic propeller synchronizer or synchrophaser system. (G-44A MODIFIED COLEMILL - STC 2-13) (500-A modified - Colemill STC SA340SO) Reissued 4/30/2007
SA2115NM Installation of Precise Flight speedbrake Amended 11/7/2003
SA2190NM Page 2 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2205SW Installation of 15 gallon auxiliary fuel cells in each engine nacelle. Reissued 3/5/2004
SA2285SW Camera and viewfinder installation. Reissued 2/27/2007
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
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
SA2588NM Installation of aileron and flap gap seals closing ribs on on ailerons and flaps vortex generators behind engine Nacelle and cabin heater exhaust main landing gear wheel well fairings and other miscellaneous seals and fairings. Issued 8/22/1985
SA2693NM (PAGE 2) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009 0:00
SA289CH Installation of Inline Pneumatic Air Filter P/N CV1J4 Reissued 1/15/2013
SA292NW Installation of cooling louvers on top of both (L.H. and R.H.) nacelle accessory sections. Reissued 9/8/2005
SA2932WE Installation of oxygen system. Reissued 1/26/1984
SA2937WE Installation of turbosupercharged Lycoming IO/LIO-360-C1E6 engine. Reissued 7/3/2006
SA2947SW Addition of Hydro Seal Fluid Additive to landing gear shock struts. Reissued 8/8/1980
SA3002WE Installation of wing tip fuel tanks of 17 gal capacity (each). Reissued 9/8/2005
SA3023SW-D Mitchell automatic flight system AK487 cons. of Piper altimatic IIIC IIIC autopilot w/opt. command/ automatic electronic pitch trim system radio and glide coupler. Reissued 8/1/1984
SA3024SW-D Mitchell automatic flight system AK505 consisting of Piper Autocontrol IIIB autopilot with optional radio coupler Reissued 6/20/1984
SA3089SW-D Mitchell automatic flight system AK561 cons. of Century III Auto- pilot. Reissued 6/20/1984
SA3099SO Installation of Causey Aviation hinge assembly P/N 62371-108. Issued 12/16/1991
SA3221SO Removal of existing aluminum battery and starter cables and replacement of these cables with copper cables. Issued 4/29/1992
SA3269NM Installation of ARNAV systems FC-10/FT-10 digital fuel flow indicating system. Issued 7/3/1986
SA3371SW-D Installation of Mitchell automatic flight system AK881 consisting of Century 41 autopilot or AK881FD consisting of Century 41 flight director. Reissued 8/24/1983
SA3384SW-D Installation of Mitchell flight system AK882 consisting of Century 21 autopilot. Reissued 8/24/1983
SA3390SW-D Installation of Mitchell automatic flight system Model AK895 consisting of a Century 31 autopilot. Reissued 8/15/1983
SA3422SW-D Mitchell automatic flight system model AK923 consisting of command electric trim. Reissued 8/23/1983
SA3475SW-D Installation of Century automatic flight system Model AK982 consisting of a Century 2010/2030/2031 autopilot. Amended 10/4/1995
SA3505NM Installation of a Turboplus Inc. instrument sub-panel system. Reissued 10/15/2007
SA3554WE Installation of vertical tail floodlights on horizontal stabilizer. Reissued 2/28/1980
SA3669WE Installation of a Silver Instruments Fueltron IIIG digital fuel flow indicating system. Reissued 4/29/1991
SA3862NM Page 2 Installation of Electronics International Primary TIT/EGT/CHT instruments remote switches and associated accessories. Amended 4/25/1988
SA4005NM (PG 4) Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) Amended 12/18/2007
SA4018NM Installation of an inspection plate on the engine lower cowling. Issued 9/25/1987
SA4172NM Installation of Aviation Development oil filter. Amended 5/22/2009
SA4180NM Installation of an ACD Corporation Model 100 000 intercooler/induction system on a Continental TSIO-360 series engine-turbocharger compressor (Rayjay) system. Reissued 10/15/2007
SA4207WE Installation of DTL-1000 -1001 and/or -1002/3 autopilot adapters for the Edo-Aire Mitchell Century III autopilot. Issued 8/8/1980
SA4234WE Installation of inflatable door seal. Amended 5/16/1983
SA4302NM (PAGE 2) Installation of Electronics Int l digital automatic engine analyzer. Amended 10/13/1989
SA4469SW Installation of S-TEC system 60 two-axis flight guidance system Model ST-032 with optional autotrim system (14 volt system). Issued 9/22/1981
SA4586SW Installation of S-TEC system 60 single axis automatic flight guidance system Model ST-031. Issued 1/19/1982
SA4698SW Install System 60 pitch stabilization system model ST-035 with optional autotrim system(14 volt system). Issued 6/15/1982
SA4721NM Installation of SynCon alarm system. Amended 5/8/1990
SA473GL Installation of Airborne wing and empennage pneumatic deice kit 711A or 711B. Reissued 1/12/1981
SA4745NM Installation of Lifeport Patient Loading and Support System. Amended 11/23/1993
SA4927NM Install Teledyne Continental engines models LTSIO/TSIO-360-E -EB and-KB modified by STC SE4731NM. Issued 4/23/1990
SA493SO Installation of Bendix FCS-810(Piper altimatic V/FD) automatic flight control system including manual electric trim and optional flight director indicator. Issued 2/17/1972
SA50GL Installation of Norton Radome Kit No. 4011KX Amended 4/15/1981
SA510NW Installation of Cessna fuel tank cap assembly. Reissued 9/8/2005
SA5143SW-D Installation of S-TEC System 60 pitch stabilization system Model ST-035 with optional automatic electric trim system. Amended 9/14/1994
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
SA5165SW-D Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-032 with optional automatic electric trim system. Amended 9/12/1994
SA5166SW-D S-TEC yaw damper system ST-141. Amended 7/27/1987
SA5300SW-D S-TEC System 40/50 single and two axis automatic flight guidance system ST-222-40/50. Issued 4/5/1984
SA534NW Installation of wing tip fuel tanks of 17 gal. Capacity(each). Reissued 9/8/2005
SA5581SW Installation of ALCOR true-flow/ totalizer system. Requires STC SE5583SW which can be installed on aircraft equipped with Teledyne Continental engines IO-360 L/TSIO-360 TSIO-360 TIO-360 TSIO-470 GTSIO-520 L/TSIO-520 TSIO-520 IO-520 and IO-470. The approved model numbers listed may not be inclusive. Amended 9/30/2002
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
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
SA594CH Install club seating. (PA-34-200T SN 34-7570096) Issued 12/19/1996
SA641GL Installation of a Shadin Co. fuel flow indicating system. Reissued 6/8/2006
SA649GL Installation of TRW Hartzell Prop. Models PHC-C3YF-2KUF/FC7453(K) and PHC-C3YF-2LKUF/FJC7453(K) used with Continental engine models TSIO-360-KB and LTSIO-360-KB respectively. Amended 12/17/1982
SA693CE Replace existing engine induction air filter with AC Spark Plug filter. Reissued 6/20/2000
SA696NW Installation of a Ryan Stormscope model WX-7A weather mapping system Issued 1/3/1979
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
SA7157SW-D Installation of S-TEC System 65 two axis automatic flight guidance system Model ST-421. Amended 3/10/1994
SA729GL Installation of Aileron and Flap Gap Seals. Amended 7/14/1997
SA783NE Installation of Safeway Model 6981 de-icer boot. Issued 9/25/1990
SA785NE Installation of Safeway model 6983 de-icer boot. Issued 9/25/1990
SA786NE Installation of Safeway Model 6985 de-icer boot. Issued 9/25/1990
SA787NE Installation of Safeway model 6986 de-icer boot. Issued 9/25/1990
SA788NE Installation of model 6988 de-icer boot. Issued 9/25/1990
SA789NE Installation of Safeway Model 6989 de-icer boot. Issued 9/25/1990
SA8897SW-D Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System Model ST-567. Amended 5/16/2001
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
SA900EA Installation of electrothermal propeller de-icer system. Reissued 3/1/1996
SA901EA Installation of wing ice light kit. Reissued 3/1/1996
SA903EA Installation of B.F. Goodrich pneumatic de-icing system. (PA-34-200 SN 34-E4 34-7250001 and up) Reissued 3/1/1996
SA929GL Install molded plastic fairings P/N s LI LO LC RI RO RC enclosing all wing flap hinges. Reissued 5/7/1997
SA949NE Installation of replacement windows. Amended 2/2/1996
SA968SO Installation of Bendix FCS-870 automatic flight control system including manual electric pitch trim and optional flight director system. Issued 1/10/1978
SA969SO Installation of NP-2041A area navigation computer programmer. Issued 1/9/1978
SA979EA Installation of L/R wing tip trans- parent fairings and sensor mounting bracketry. Issued 4/5/1974
ST00961LA Installation of MASS Systems fire extinguisher cartridges as replacements for Walter Kidde Aerospace fire extinguisher cartridges in fire extinguisher bottles installed in the airplane models noted on the FAA Approved Model List dated June 29 2000 or later FAA approved revisions. These fire extinguisher cartridges are in accordance with the MASS Systems Master Drawing List No. 30980-1 Slug Thrower Cartridges Master Drawing List Reissued 7/13/2011
ST01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010
ST01327LA Installation of Glareshield per FAA Approved Ashby Glareshield Master Drawing List. Reissued 1/28/2009
ST01468CH Installation of various SMR Technologies electrical propeller deicer models. Amended 7/25/2006
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)