PA-16

Number of Active Aircraft: 356 Active- Map

Description:

Very similar aircraft, the Clipper is a stretched version of the PA15. Both are side by side seating instead of the tandem seating seen in earlier piper models. The PA15 was a two place machine while the PA16 was a four place. It feature the lycoming o-235.

264
Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 850 lbs
Max Weight 1650 lbs
Useful Load: 800 lbs
Engine Name Lycoming O-235
Engine Number 1
Horsepower 115 HP
Never Exceed Speed: 0 kts
Stall speed: 0 kts
Service Ceiling: 11000 ft
Max Fuel 36 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 97 kts
GPH (75% BHP): 6.6
MPG (75% BHP) 14.7
Range (75% BHP): 451 nm
Fuel Cost Per Seat Mile 0.1 $
Fuel Cost Per Hour 39.6 $
MPG per 1000 lbs of Payload 11.76
F-T (Speed^2/FuelBurn) 14.3 HP
F-T Payload 11.4 kts
MPH To HP: 8.4 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 925 ft

SA00009NY Installation of wing leading edge fairing. Issued 5/28/1993
SA00009WI Change belly skins from aluminum to stainless steel. Issued 11/17/1992
SA00010NY Installation of induction filter air scoop. Issued 5/28/1993
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 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00068SE (PAGE 2) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010 0:00
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
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
SA00156BO Installation of MT-Propeller MTV-12-B-C-R(M)/CRLD 188-119a propeller in accordance with MT-Propeller Report No. E-820-E dated January 14 2002 or later FAA-approved revisions or MTV-12-B/LD188-119a propeller in accordance with MT-Propeller Report No. E-958 dated February 10 2004 or later FAA-approved revisions.  Amended 5/12/2004
SA00159SE Installation of modified instrument panel. Issued 12/12/1994
SA00161BO (2 OF 3 Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005 0:00
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
SA00172BO Installation of Piper PA-18 right wing fuel tank. Limited to installation on PA-16 serial number 16-403 ONLY. Issued 7/11/2003
SA00173DE Installation of Oilamatic preoiler system. Amended 3/10/2008
SA00175DE Installation of Oilamatic Preoiler system. Amended 4/14/2003
SA00193AT Installation of carbon steel discs. Reissued 11/14/1994
SA00194BO Installation of P/N 2042 Landing Gear Warning System for amphibian aircraft. Reissued 1/23/2009
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
SA00207AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-67. Reissued 11/14/1994
SA00210AT Installation of carbon steel brake discs that have melonite surface treatment P/N AA-90. Reissued 11/14/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00216AT Installation of carbon steel brake discs. Reissued 11/17/1994
SA00229NY Installation of Sky Harbour Aircraft Refinishing Ltd Ice Damage Prevention Plates. (PA-23-250 6 place) Amended 1/24/1997
SA00238SE Installation of Aviation Development Corporation s sump mounted chip detector Issued 10/31/1995
SA00243BO (1 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
SA00243BO (3 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
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 (2 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
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
SA00283BO Installation of Lycoming O-320-A -A1B -A2A -A2B -A2C -C1A -C1B -C2A or  Issued 2/27/2009
SA00288DE Installation of a Dorsal fin fairing. Issued 4/18/1997
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
SA00333BO Installation of Falls Filtration Technologies ( Airmaze Reissued 8/26/2013
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
SA00363SE Installation of main landing gear doors. Issued 8/6/1996
SA00376SE Install vortex generators on the wings and vertical tail. Amended 2/19/1997
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
SA00448DE Installation of Oilamatic preoiler system. Amended 4/14/2003
SA00462AT Replacement of Appalachian stainless steel brake discs P/N 75-23 with Appalachian steel brake disk part number AA-47. Reissued 12/7/1994
SA00478CH (PAGE 1) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00478CH (PAGE 2) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00478CH (PAGE 3) Installation of Cooper Superflite 102 Fabric. Amended 5/10/2012
SA00484WI Installation of shoulder harness for two front seats. Reissued 3/25/2009
SA00506SE Installation of an AlliedSignal TPE331-1-151G turboprop engine and a Hartzell HC-B3TN-5E/T10282+4 propeller. (Restricted Category) Issued 4/2/1998
SA00519AT-D Installation of replacement fuel cell assemblies Reissued 4/16/2009
SA00520AT-D Installation of fuel ramp assemblies Reissued 5/5/2009
SA00618AT Installation of a stabilator modification kit. Issued 12/9/1994
SA00621LA Installation of an electronic digital engine tachometer horizon model P-1000. Amended 1/14/2002
SA00622LA Installation of an electronic digital engine tachometer horizon model P-1000. Reissued 1/14/2002
SA00631CH Installation of the Hartzell propeller model HC-C2YR-1BF/F7666A-4 or HC-C2YR-1BFP/F7497 propeller Amended 5/14/2013
SA00674WI-D Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II system installation. Amended 7/23/2012
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00680SE (4 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
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
SA00711CH Install replacement tail landing gear spring described by Drawing 5480 rev. E dated August 12 1996 or later FAA approved revisions. Reissued 12/9/2008
SA00721CH Installation of a Hartzell HC-C2YL-2CUF/FC7663-4 propellers and 836-29(P) spinners. Issued 7/29/1997
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
SA00734LA Installation of modified exhaust system. (PA-23-250 27-2505 and up) Issued 2/19/1999
SA00743SE Installation of vortex generators on the wing leading edge underside of the horizontal stabilizer and on the vertical fin in accordance with Micro AeroDynamics Drawing List MA2117 Revision IR dated July 14 1999 and Installation Instructions MA2118 Revision IR dated September 21 1999 or later FAA approved revisions to either of these documents. );INSERT INTO stc_table VALUES ( );INSERT INTO stc_table VALUES ( NOTE: If more than five vortex generators are damaged or missing the aircraft is not airworthy Amended 4/27/2004
SA00746WI Installation of diagonal shoulder harnesses for the rear seats. (PA-30 S/N 30-1 thru 30-901) Reissued 3/25/2009
SA00759NY Installation of Northeast Engineering landing gear actuator rod. Amended 10/3/2006
SA00762AT Installation of left hand and right hand fuel cell assemblies. (S/N 7654001 and up) Reissued 4/27/2009
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
SA00780SE (PAGE 4) 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
SA00800AT Installation of left hand and right hand fuel cell assemblies. (PA-23-250 S/N 7554001 AND UP) Reissued 4/27/2009
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
SA00881CH Install rudder servo tab. Reissued 8/21/1998
SA00927AT Installation of composite propeller spinner. Amended 5/20/2004
SA00930SE Installation of vortex generators on the wing and flap surfaces in accordance with Drawing Package MA2153 Revision IR dated January 26 2001 and Installation Manual MA2154 Revision IR dated May 29 2001 or later FAA approved revision of either of these documents. Issued 6/13/2001
SA00932SE Installation of the Stewart wing tip assembly in accordance with Stewart Wing Tip Assembly Master Drawing List SWT 3001 dated April 8 2001 or later FAA approved revision. Amended 1/25/2002
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
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
SA00954SE (2 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
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
SA01015SE Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. Amended 10/4/2012
SA01026SE (PAGE 1) Improved fuel gascolator assembly. Amended 12/19/2012
SA01027CH Installation of Walter Turboprop Model M601E-11 and AVIA-Hamilton Standard Aviation propeller model VJ8.510 or VJ8.510AG. Amended 2/8/2005
SA01057AT Installation of Composite skinner. Amended 10/13/2000
SA01058AT Installation of Composite spinner. Amended 10/13/2000
SA01063CH Installation of a Scott Model 3200 Tail Wheel with the AESI #T.S.05P Tail Spring. Reissued 2/16/2006
SA01065AT Installation of glare shield. Issued 6/21/1996
SA01077SE (PAGE 1) Installation of fluoropolymer film. Reissued 8/20/2003
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
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
SA01141WI-D Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head. Amended 5/24/2006
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
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
SA01233SE Manufacture of Alaskan Bushwheel Inc. (ABI) tail wheel and fork assembly per ABI Document ABI-3200B Revision A dated April 28 2005 or later FAA approved revision.  Amended 5/22/2012
SA01236CH Installation of Motorlet Walter M601E-11 turbine engine with an AVIA-Hamilton Standard VJ8.510 or VJ8.510AG model propeller. Amended 11/15/2002
SA01237AT Installation of fuel cell drain kit. Reissued 3/6/2000
SA01240SE (1 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01240SE (2 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01240SE (3 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006
SA01240SE (4 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01250AT Installation of left hand and right hand tip fuel cell assemblies. (PA-23-250 S/N 7654001 AND UP) Reissued 4/29/2009
SA01251SE The manufacture of a Sunvisor System. Amended 2/28/2012
SA01257AT Installation of composite spinner assemblies. Amended 10/13/2000
SA01258SE Installation of the Automatic Flagman Dispenser Models in accordance with Automatic Flagman Master Drawing Lists specified in attached AML or later FAA approved revision.This STC supercedes several existing STC Issued 9/5/2003
SA01263AT Installation of Composite Spinner. Amended 10/13/2000
SA01279NY Installation of a wing reinforcement kit. Issued 1/19/2001
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
SA01282NY Installation of Airwolf remote mounted engine oil filter kit AFC-K015 on aircraft powered by Pratt & Whitney radial reciprocating engine Series R-985 R-1340 and R-1830. Amended 10/31/2012
SA01295LA Installation of modified Pratt & Whitney R-1340 engine. This mod must be done concurrently with STC SE01200LA which modifies R-1340 engine. Amended 7/23/2003
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
SA01303AT Installation of OCEM AP-3C autopilot. Amended 11/16/2005
SA01306WI-D Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation. Amended 2/28/2007
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
SA01353CH Installation of Walter Turboprop Engine Model M601E-11 and the AVIA-Hamilton Standard Aviation Ltd. Propeller model VJ8.510(AG). Issued 1/23/2001
SA01377AT Installation of Textron Lycoming IO-360-A1B6. Bartow FL 33830  Issued 12/1/2005
SA01406NY Installation of Airwolf remote mounted engine oil filter kit AFC-K017 on single and multi-engine fixed light aircraft and );INSERT INTO stc_table VALUES ( rotary wing Amended 10/31/2012
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 (3 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
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
SA01526CH Replace Janitrol Models B1500 B2030 or South Wind 940 (12-volt) series combustion heaters with C & D Associates TSO-C20 approved heater kit Model CD35K part number CD12011K7. Issued 8/23/2001
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
SA01566CH Installation of C&D Associated combustion heater kit P/N CD11005K1 and CD11006K2. Amended 11/1/2004
SA01639NY Replacement of 12 refrigerant in air conditioning system with Enviro Refrigerant Hotshot R414B. Amended 6/1/2004
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01686SE Fabrication and installation of engine control levers. Reissued 5/7/2009
SA01688WI Installation of Pratt & Whitney R-985-AN14B or R-985-AN1 engine modified for fuel injection  Issued 8/28/2012
SA01689SE ONE-ONLY STC: Installation of an 18 gallon right wing fuel tank with electric fuel gauges relocation of fuel selector valve and switch and removal of 12 gallon fuselage tank Serial Number 16-623 Issued 7/18/2006
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (3 OF 5) Installation of an antenna Amended 2/15/2007
SA01695SE (4 OF 5) Installation of an antenna Amended 2/15/2007
SA01704LA Installation of the Grove Disk Brake System Issued 12/21/2004
SA01734SE (PG 3) Application of Stewart Systems synthetic fabric covering system to aircraft fuselage wings tail surfaces control surfaces and related parts. Amended 3/23/2011
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01796AT Installation of a Class E cargo compartment on Gulfstream G-159. Issued 1/7/1999
SA01800SE (PG 2) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01800SE (PG 3) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01800SE (PG 4) 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
SA01843SE Installation of Lycoming engine and modified fuel system Amended 3/10/2009
SA01853AT Replace Aluminum alloy propeller spinner with composite spinner. Amended 10/13/2000
SA01860NY (1 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01860NY (2 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01860NY (3 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 2)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01861SE (PAGE 3)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01861SE (PAGE 5)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01863SE Installation of Niagara Oil Cooler in the above model aircraft Amended 1/27/2009
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 (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01933LA (3 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01933LA (4 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01944CH (2 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004 0:00
SA01988SE (PAGE 1) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009
SA01988SE (PAGE 4) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 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 1) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line. Amended 7/25/2008
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
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
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
SA02128LA Installation of aileron and flap hinge repair bushings Amended 6/10/2009
SA02135SE Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50T in accordance with the Installation Instructions Document No. II 1211061 Revision D dated June 15 2011 or later Federal Aviation Administration (FAA)-approved revision.  Issued 7/7/2011
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02153NY Installation of Lake Central Air Services Horizontal Stabilizer Attachment Fitting. Reissued 9/16/2005
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
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 2) Installation of hourmeter airspeed switch. For unpressurized aircraft only. Pressurized aircraft must have pressurization system deactivated. Issued 3/23/2001 1:00
SA02203AK (PAGE 1) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02203SE Installation of a Hartzell Propellers Inc. model HC-C2YK-1BLF/FL7666A-4Q constant speed propeller in accordance with Installation Instructions Document No. 012-010 dated September 20 2011. Issued 11/1/2011
SA02212AK (PG 1) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems  Amended 5/4/2011
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 (1 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
SA02217AK (3 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
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
SA02241AK Installation of a Maule Fuel Selector Valve and Associated Fuel System Upgrade in accordance with the Descriptive Data listed in Trimmer Aviation LLC Master Data List MDL-001 dated March 22 2005 or later FAA approved revision. Issued 5/6/2005
SA02243CH Install enlarged rear baggage area to accommodate skis. Issued 3/2/2007
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
SA02263AK Fabrication and Installation of a Left Hand Seaplane Door. Issued 3/17/2006
SA02264AK Fabrication and Installation of a Right Hand Seaplane Door. Issued 3/24/2006
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02268CH (PAGE 1) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
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
SA02283SE Page 2 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
SA02298CH Installation of a Three Point Torso Restraint System Issued 6/15/2006
SA02306AK Installation of a Lycoming O-360-A1A A1D A2A A2D A2E A2F A3A A3D A4A A4M A4N or A4P engine on Piper PA-22 PA-20 and PA-16 airplanes. Issued 3/11/2008
SA02334NY Provide improved access to the engines during the maintenance process. Issued 1/29/2007
SA02345AK Installation of Piper PA-18 three-inch extended gear & Maule Oleo Strut Issued 6/30/2009
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
SA02440AT Removal of chemical hopper tank and installation of 2-place passenger bench seat and associated restraint system. Must be operated under Restricted Category operating limitations of FAR 91.313. A placard which states Never Exceed Speed (Vne) = 132 mph must be installed in full view of pilot. Issued 4/10/2002
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
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
SA02751CH Installation of McCauley Propeller model 1A200FA824X Amended 6/25/2012
SA02786CH Installation of a Single Point Ground Fueling System  Issued 12/22/2009
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
SA02846CH Installation of MT Propeller model MTV-15-B/210-58 on Piper Aircraft models PA-20 and PA-22  Issued 6/22/2010
SA02874CH-D Installation of Hartzell HC-E2YR-2BTF/FC7693F(B)+1 propellers  Issued 12/14/2010
SA02929CH Installation of Lycoming O-360 engine in accordance with Installation Instructions Report SA300 dated 7/5/2009. Issued 3/25/2011
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
SA02985CH Installation of a Cool Start System in accordance with Installation Instructions Revision A dated April 14 2011 or later FAA Approved revision. Issued 5/10/2011
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03029CH Installation of Honeywell Engine Model TPE-331-1-151A with a Hartzell HC-B3TN-5M/T10282N+4 model propeller in accordance Project Report Number JTC2010ST001 Revision NC date March 3 2011 and submitted previously FAA Approved data accomplished under Federal Aviation Administration (FAA) Field Approval process. Issued 11/2/2011
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA03217AT Installation of improved Horizontal Stabilizer Attachment Fitting XLS Kit  Issued 1/26/2006
SA03251AT For Lake Model 250 including this model incorporating STC SA469NE replace existing propeller with MT-Propeller model no. MTV-9-B-C-R(M)/CRLD193-109 (reversing type) per MT-Propeller Installation Doc. No. E-1261 dated 11/10/2005 or later FAA approved revision or install Propeller model no. MTV-9-B/LD193-109 (non-reversing type) per Doc. No. E-1262 dated 11/10/2005 or later FAA approved revision. Issued 8/15/2006
SA03274NY Installation operation and maintenance of the Lycoming Issued 5/2/2013
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
SA08997AC-D Installation of S-TEC System 60 pitch stabilization system Model ST-581. Issued 4/10/1995
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
SA09119AC-D Installation of S-TEC System 65 Two Axis automatic flight guidance system Model ST-601. Issued 9/20/1995
SA09123AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-607 with Optional Autotrim System. Limited to Piper models PA-23-250 and PA-E23-250 s/n 27-2000 through s/n 27-7554172. Eligible on same models when equipped with approved turbocharged engines (250 hp) and/or wing tip tanks per STC SA1480WE. Amended 8/29/2007
SA09198AC-D Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System Model ST-662. Installation of S-TEC System 55X Two Axis Automatic Flight Guidance System Model ST-662-1. Eligibility limited to Piper models PA-23-250 and PA-E23-250 s/n 27-2000 through 27-7554172. Amended 4/18/2007
SA09199AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-664. Issued 3/5/1997
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
SA09394AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-847-20/30. Issued 9/24/1998
SA09396AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-848. Issued 9/29/1998
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
SA09503AC-D Installation of S-TEC System 20/30 single and two-axis automatic flight guidance system Model ST-882-20/30. Issued 10/5/2000
SA1-103 Radio-shelf. Issued 
SA1-117 Propeller anti-icing kit. Issued 
SA1-120 F-300 automatic pilot. Issued 
SA1-137 Installation of Tactair T-3 automatic pilot and optional installation of Tactair AH-1 altitude hold device (for use with Tactair T-3 autopilot). Reissued 8/7/1972
SA1-169 Reinforcement of floor structure between fuselage station 91-1/2 and 123-3/4 and provision for tie-down facilities. Issued 
SA1-177 Lightweight reservoir type pneumatic deicing system. Reissued 3/1/1996
SA1-198 Spray rails addition. Issued 
SA1-28 Radio rack limited to 30 pounds of radio equipment. Issued 
SA1-282 Replacement of fabric covering with metal skins. Reissued 11/15/2007
SA1-327 Replacement of fabric covering with metal skins. Reissued 8/15/2007
SA1-340 Oil-free vacuum pump PA-201. Issued 
SA1-383 Lube oil filter PB 55-1. Issued 
SA1-399 Forward and aft attachment for HF antenna. Issued 
SA1-400 Bendix radar scanner attaching brackets and electrical cable firewall plugs. Issued 
SA1-401 Glide slope antenna mounting bracket. Issued 
SA1-402 Installation of 37K-2 Marker Beacon Antenna. Amended 7/24/1968
SA1-403 Fabrication of mounting blocks and installations of Lear sense antenna. Issued 
SA1-404 Fabrication and installation of adaptor for mounting Chance Vought seat 22-93597-B-2. Issued 
SA1-405 DL-1 loop assembly. Issued 
SA1-406 Collins 37R-2 antenna. Issued 1/1/1996
SA1-407 AC Spark Plug Division FM telephone antenna. Issued 
SA1-408 Radio equipment shelves. Issued 
SA1-412 Bulkhead at station 193.0. Issued 
SA1-413 Double-hinged door. Issued 
SA1-414 Bulkhead and door at station 232.5. Issued 
SA1-415 Bulkhead and door at station 485.5. Issued 
SA1-417 Baggage compartment smoke detector system. Issued 
SA1-420 AC Spark Plug Division FM telephone antenna. Issued 
SA1-421 Bendix LPA-70C loop antenna. Issued 
SA1-432 High frequency antenna. Amended 7/25/1967
SA1-447 Bulkhead and door at station 251.5. Amended 
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)