| 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 | | |
