| 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 |
| SA00081NY | | Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. | | Amended | | 5/15/2002 |
| SA00185BO | | Installation of McCauley 2A34C209/78CCA-2 propeller. | | Reissued | | 1/21/2004 |
| SA00197AT | | Installation of Appalachian carbon steel brake discs that have melonite surface treatment. | | Reissued | | 11/14/1994 |
| SA00215NY | | Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. | | Amended | | 8/14/1995 |
| SA00247BO | | ONE-ONLY: Addition of control stick mounted trim switches to Ray Allen electric elevator trim servo previously approved by STC SA00184BO serial number 3501. | | Issued | | 1/23/2007 |
| SA00259BO | | S/N 3501 ONLY: Installation of Cessna 150 seats. | | Issued | | 7/27/2007 |
| SA00260BO | | S/N 3501 ONLY: Installation of 15x6.00-6 tires. | | Issued | | 7/27/2007 |
| SA00402SE | | Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) | | Amended | | 1/23/2007 |
| SA00432SE (PG 4) | | Installation of EGT 701 series fuel flow instrument. | | Amended | | 4/12/2013 |
| SA00433NY | | Installation of Airwolf remote mounted engine oil filter model AFC-500 or AFC-600 on multi engine fixed wing light aircraft incorporating Franklin reciprocating engines of 450 horsepower or less. | | Amended | | 10/31/2012 |
| SA00655SE | | Installation of a redesigned fiberglass engine cowl nose bowl cowl and engine baffle modifications and a Cessna Spinner assembly (PIN 0752637 -K-200) | | Issued | | 12/23/1998 |
| SA00680SE (4 OF 6 | | Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer. | | Reissued | | 7/8/2005 |
| SA00861SE Page 4 | | Installation of J.P. Instruments (JPI) fuel flow indicating system | | Amended | | 4/12/2013 |
| SA00910AT | | Installation of control sticks. | | Reissued | | 12/21/2010 |
| 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 |
| SA01026SE (PAGE 1) | | Improved fuel gascolator assembly. | | Amended | | 12/19/2012 |
| SA01083SE | | Installation of electric elevator trim system in accordance with Ernest Hansen drawings photographs and instructions contained in the Federal Aviation Administration project file. Limited to installation on Globe Swift GC-1B aircraft Serial Number 115 only. | | Issued | | 4/30/2002 |
| SA01157LA | | Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. | | Reissued | | 1/20/2005 |
| SA01175NY | | Installation of an alternator system. | | Issued | | 3/8/2000 |
| SA01240SE (4 OF 5) | | Installation of secondary voltage indication system | | Reissued | | 4/3/2006 0:00 |
| SA01425SE | | Installation of auxiliary fuel tanks in a Globe Swift GC-1B. Limited to installation on serial number 115 ONLY. | | Issued | | 6/25/2004 |
| SA01435SE | | Installation of J.P. Instruments (JPI) Primary Engine Data Management System | | Amended | | 9/17/2013 |
| SA01590SE | | Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is therefore limited to the installation in Globe Swift airplane serial number 377 registration N90363 only. Installation of auxiliary fuel tanks. | | Issued | | 8/17/2005 |
| SA01659SE | | Installation of a Franklin 6A-350-C1 engine and McCauley 2A34C201/90DA-14 propeller composite engine cowling and associated components. Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation in Swift Museum model GC-1B aircraft Serial Number 2237 Registration Number N78237 only. | | Issued | | 3/31/2006 |
| SA01669CH | | Installation of Challenger Reusable Air Filter | | Amended | | 6/21/2012 |
| SA01800SE (PG 4) | | Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. | | Reissued | | 12/1/2011 |
| SA01860NY (2 OF 3) | | Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200. | | Amended | | 5/31/2006 |
| SA01861SE (PAGE 3) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| SA01861SE (PAGE 5) | | Fabrication and installation of Landing Light Controller | | Reissued | | 12/1/2011 |
| SA01988SE (PAGE 4) | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P. | | Issued | | 4/17/2009 0:00 |
| SA02033AT (PAGE 5) | | 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 |
| SA02052LA | | Installation of an electrical trim system for the horizontal stabilizer. | | Issued | | 6/15/2007 |
| SA02141LA | | Installation of a Sliding Canopy. | | Issued | | 5/16/2008 |
| SA02154LA | | Installation of wing leading edge stall strips | | Issued | | 7/8/2008 |
| 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 |
| SA02212AK (PG 4) | | Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems. | | Amended | | 5/4/2011 |
| SA02268CH (PAGE 5) | | Installation of Airwolf Filter Corp. Air Oil Separator | | Amended | | 8/28/2011 |
| SA02283SE Page 1 | | Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P | | Reissued | | 8/27/2013 |
| SA02520AT | | Installation of M-20 Oil Separator model 600-WP. | | Issued | | 5/30/2002 |
| SA02738CH (PAGE 2) | | Installation of L-3 Communications Avionics Systems | | Amended | | 5/7/2010 |
| SA02930NY | | Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. | | Reissued | | 6/12/2012 |
| SA09470SC | | Installation of Starter Indicator light system. | | Issued | | 6/18/2001 |
| SA1-326 | | Installation of Teledyne Continental Mode IO-300-A engine with McCauley Model 1A170-DM7359 propeller and Cessna spinner AK7053-3. | | Amended | | 3/20/2003 |
| SA1-335 | | Sensenich 62-inch pitch propeller M74DR-1 on aircraft equipped with Continental C-145-2 engine. | | Issued | | |
| SA10077SC | | Installation of push-button starter system. | | Amended | | 4/26/2005 |
| SA1041NW | | Installation of an additional Harrison oil cooler and associated systems | | Issued | | 10/23/1980 |
| SA10822SC | | Installation of EFD1000 Primary Flight Display | | Amended | | 9/29/2009 |
| SA10921SC | | Installation of an alternator and regulator as a replacement to existing OEM generators and mechanical voltage regulators | | Issued | | 11/10/2008 |
| SA1177WE | | WECO carburetor temperature monitor. | | Issued | | 1/1/1960 |
| SA124CE | | Rear seat and/or instrument panel. | | Issued | | 1/1/1961 |
| SA1315WE | | Installation of Mixture Monitor (exhaust gas temperature probe gage and selector) in accordance with Delta Products Part Lists A-192 and A-193 or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9 1981 or later FAA approved revision and/or Drawing List MM-127 dated November 15 1981 or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29 1968 copy attached or later FAA approved revision. | | Reissued | | 4/15/2011 |
| SA145NW | | Installation of a single (center located) control column | | Issued | | 12/20/1974 |
| SA146NW | | Installation of a retractable tail wheel and door assembly | | Issued | | 11/19/1979 |
| SA147NW | | Installation of a Franklin 6AS-350-A engine McCauley 2A34C201/90DA-12 propeller Bendix-Stromberg PS-5C Carburetor modified forward fuselage single (center located) control column with electric propeller pitch control electric throttle control and electric elevator trim inverted fuel and oil system retractable tail wheel assembly aileron centering spring modified engine baffles engine cowl flap modified elevator trim tab landing gear wheel-well doors and a modified center section wing fairing | | Amended | | 2/3/1975 |
| SA1490CH | | Installation of a Sensenich 74DR-1 model propeller. Limited to Tel Continental O-300A C-145-2 or C-145-2H or O-300B with propeller control valve secured in closed position. Model O-300C or O-300D engines with model 530860 crankshaft installed. Maximum takeoff power limited to 125 horsepower. | | Issued | | 8/14/2001 |
| SA149CE | | Relocation of battery and removal of tail ballast. | | Issued | | 1/1/1961 |
| SA1512WE (1 OF 2) | | Installation of exhaust gas temperature monitoring systems Model EGT-1. | | Amended | | 2/22/2007 |
| SA157NE | | Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. | | Amended | | 10/18/1996 |
| SA1626NM Page 2 | | Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) | | Amended | | 3/9/1993 |
| SA167NW | | Installation of access door aft of luggage compartment. | | Issued | | 3/25/1975 |
| SA169NW | | Installation of Merlyn Products motor part number 06-6001 | | Amended | | 9/22/2000 |
| SA174NW | | Installation of Continental IO-360 engine and McCauley D2A34C67/76-C2 propeller and associated changes | | Issued | | 5/7/1975 |
| SA1843NM | | Installation of Beltmaster shoulder harness. | | Amended | | 5/2/1983 |
| SA2-1007 | | Installation of Lycoming Model O-290-D2A or O-320-A3A engines | | Reissued | | 5/5/2009 |
| SA2-226 | | Windshield manufactured in accordance with Luminous Plastics. | | Reissued | | 4/9/1979 |
| SA2001WE | | Installation of Brittain Model B2C Flight Control System | | Amended | | 11/4/1969 |
| SA203NW | | Installation of Franklin 6A-350-C1 engine and McCauley2A34C22/SF84-10 propeller. | | Issued | | 9/16/1975 |
| SA2098SO | | Installation of a pneumatic squat switch on the landing gear retraction system in accordance with installation procedures dated April 24 1987 or later FAA approved revisions. | | Reissued | | 6/15/2009 |
| SA2105WE | | Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) | | Issued | | 2/9/1970 |
| SA2137CE | | Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON + MON) /2. | | Amended | | 3/7/1986 |
| SA217NW | | Installation of a Franklin 6A-350-C1 engine and a McCauley 2A34C22/SF84-10 propeller | | Issued | | 9/5/1975 |
| SA2231SO | | Replacement of Cleveland brake discs P/N 164-43 or 164-143 with Appalachian Accessories stainless steel brake discs P/N 75-43. | | Issued | | 1/21/1988 |
| SA2321WE | | Installation of smooth skins with internal chordwise stringers for outboard wing panel in lieu of beaded skins. | | Issued | | 3/15/1971 |
| SA2358WE | | Installation of fiberglas wing tips. | | Issued | | 5/26/1971 |
| SA2535NM | | Installation of Lycoming 0-320-A3A engine and Hartzell HC-C2YL-4BF/FC-7663-4 propeller fiber glass cowling associated engine changes modified airspeed system and other miscellaneous changes. | | Amended | | 7/16/1985 |
| SA2557NM (1 OF 2) | | Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. | | Amended | | 2/22/2007 |
| SA255SO | | Auxiliary fuel tanks. | | Reissued | | 12/14/2009 |
| SA2586NM (PAGE 3) | | Installation of J.P. Instruments temperature monitoring systems. | | Amended | | 7/20/2008 0:00 |
| SA2640NM | | Installation of Jack Nagel Sliding Bubble Canopy | | Issued | | 9/24/1984 |
| SA2642NM | | Installation of jack nagel sliding bubble canopy | | Issued | | 9/4/1984 |
| SA2644NM | | Installation of Jack Nagel sliding bubble canopy. | | Issued | | 9/4/1984 |
| SA2683NM | | Installation of Precise Flight Inc. stand-by vacuum system (SVS) | | Amended | | 3/10/2005 |
| SA275NW | | Installation of a Lycoming IO-360-A C or D engine and a Hartzell HC-C2YK-1BF/F7666A-2 propeller | | Reissued | | 7/15/1986 |
| SA2859WE | | Installation of Lycoming 0-320-A3B engine & Hartzell HC-C2YL-1BF/F7663A-4 propeller.
);INSERT INTO stc_table VALUES ( | | Issued | | 4/1/1974 |
| SA2996SW | | Install Brittain Model BSS Stability Augmentation System | | Reissued | | 3/26/2013 |
| SA2GL | | Installation of wheel and brake assemblies and axle spacer. | | Amended | | 4/1/1981 |
| SA3-267 | | Narco Omnigator with (VIR-1) transmitter-receiver unit and (V12 MP-2) power unit. | | Issued | | 1/1/1960 |
| SA3001SO | | Installation of Appalachian Accessories stainless steel brake discs P/N 75-43. | | Reissued | | 9/29/1995 |
| SA3088SW-D | | Mitchell automatic flight system AK564 consisting of Century I autopilot with optional omni tracker. | | Reissued | | 6/20/1984 |
| SA308EA (1 OF 2) | | Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) | | Amended | | 11/20/1978 |
| SA313WE | | Dowty Equpment Co. hand pump. | | Issued | | 1/1/1960 |
| SA345SO | | Replace hand operated wobble pump with electric fuel pump Piper P/N 48-666 replace factory cockpit hatch & side glasses with fiberglass canopy. Add clear vision window 4-inch X 6-inch in left side of canopy. | | Reissued | | 10/15/2001 |
| SA3531NM | | Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) | | Reissued | | 9/8/2010 |
| SA382NW | | Installation of a gross weight increase to 1835 pounds and associated changes | | Reissued | | 12/20/2002 |
| SA389NW | | Installation of Continental IO-360-D engine and McCauley D2A34C67/76C-2 propeller and a gross weight increase. | | Issued | | 12/28/1976 |
| SA4-1200 | | Delco-Remy generator 1101879 and regulator 1118384. | | Issued | | 1/1/1960 |
| SA4-145 | | Removal of C-125 Continental Engine and installation of C145 Continental Engine and Koppers Model F200 and F200-H propellers with 0073-E blades in all model GC-1B Swifts. Maximum engine power restricted to 125 hp at 2550 rpm and 25.8 in. Hg. MAP. Installation must be made per Preston Johnson Drawing No. PDJ-3. | | Reissued | | 6/25/2003 |
| SA4-156 | | Slightly modified Bonanza wing tips. | | Reissued | | 1/24/1965 |
| SA4-157 | | Removal of present trim control handle and relocating it on the left side of the fuselage about nine inches below window and about nine inches to the rear of the instrument panel. | | Reissued | | 6/25/2003 |
| SA4-302 | | Installation of BN-1 propeller spinner. | | Reissued | | 10/30/1985 |
| SA4-395 | | Fiberglas wing tips. | | Issued | | 1/1/1960 |
| SA4-403 | | GC 1-1 heavy duty bubble windshield. | | Reissued | | 10/24/2007 |
| SA4-761 | | GC-1-3 heavy duty bubble windshield. | | Reissued | | 6/4/1973 |
| SA4005NM (PG 5) | | Installation of Precise Pulselite control unit in landing/taxi system. (HP Jetstream Model 3101 AND SUPER 31) | | Amended | | 12/18/2007 |
| SA4011WE | | Installation of extended length gear door fairings. | | Reissued | | 8/30/1983 |
| SA4061WE | | Installation of dual control sticks. | | Amended | | 3/28/1984 |
| SA4302NM (PAGE 3) | | Installation of Electronics Int l digital automatic engine analyzer. | | Amended | | 10/13/1989 0:00 |
| SA4392NM | | Installation of a redesigned fiberglass engine cowl nose bowl cap section NACA oil cooler inlet duct new aluminum lower cowl center section and Hartzell spinner assembly. | | Reissued | | 7/17/1995 |
| SA452NW | | Installation of auxiliary fuel tanks | | Reissued | | 5/10/1988 |
| SA4727NM | | Installation of a new gull-wing canopy and canopy locking system. | | Issued | | 4/25/1989 |
| SA4855NM | | Installation of dual-stick flight control system. | | Reissued | | 10/22/2009 |
| SA489EA | | Installation of ARP Inc. carburetor ice detection system Models 107AP (-12 -R-12 -24 and -R-24 series) in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Precision A ir-Motive (Facet or Marvel-Schebler) MA-2 MA-3 MA-3SPA MA-4 MA-4-5 MA-4SPA MA-5 MA-6 MA-6AA and HA-6 series carburetors. | | Amended | | 12/5/2002 |
| SA53NW | | Installation of Continental IO-360-C engine with McCauley propeller. | | Amended | | 5/7/2010 |
| SA563NW | | Install of a swift alturair rudder cap. | | Issued | | 1/31/1978 |
| SA564GL | | Installation of Continental IO-360 engine per STC SA53NW and further modified with new engine baffling Alturair cowling relocated battery box and Cessna propeller spinner. Also included is the installation of an Aero Instruments P/N PH500 heated pitot tube and flush mounted static port. | | Issued | | 10/6/1981 |
| SA5656NM | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5656NM (PAGE 1) | | Installation of burglar alarm system. | | Reissued | | 7/21/1993 |
| SA5840NM | | Limited to installation on serial number 32 ONLY. | | Issued | | 9/18/1992 |
| 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 (4 OF 5) | | Install Champion SlickSTART magneto booster system. | | Reissued | | 2/10/2009 0:00 |
| SA60WE | | Continental O-300-A engine. | | Issued | | 2/22/2010 |
| SA677NW | | Installation of a Continental engine and McCauley propeller | | Issued | | 11/29/1978 |
| SA684NW | | Installation of a McCauley propeller on a Franklin engine | | Reissued | | 7/20/1988 |
| SA68SO | | Down-draft cowling and baffles. | | Amended | | 11/22/1978 |
| SA699NW | | Installation of a Lycoming O-320-E3D engine Sensenich 74DN6-O-60 propeller throttle quadrant controls (Piper P/N 65850-00) and quadrant pedistal and associated systems | | Amended | | 2/13/1979 |
| SA69NW | | Installation of Matney s engine charge air-air filter assembly. (AA-1B AA-1 AA-1A 1969 AND ON) (AA-5 1972 1973 AND 1974 ONLY) | | Amended | | 10/8/1974 |
| SA712NW | | Installation of Continental TSIO-360-A engine and McCauley 02A34C67/76C-2 propeller | | Reissued | | 3/6/1985 |
| SA71GL | | Installation of air filters | | Reissued | | 6/20/2000 |
| SA7643SW | | Data pertaining to this modification are considered inadequate for duplication in other aircraft. This approval is limited to the installation made in a Globe Model GC-1B Swift Serial Number 2083 and Registration No. N78083. Remove existing Stall Strips and install new Stall Strips. | | Reissued | | 2/17/2005 |
| SA765NW | | Installation of a left hand rotation Lycoming engine Hartzell propeller engine mount and Hartzell spinner | | Issued | | 6/26/1979 |
| SA7891SW | | Installation of a replacment landing gear retraction link. | | Issued | | 9/21/1990 |
| SA803SO | | Installation of Lycoming O-360- A1A engine equipped with a McCauley Model 2D34C53-A/74E-0. | | Reissued | | 12/20/1999 |
| SA822NW | | Installation of Beech control wheels relocation of manual elevator trim control installation of electric trim control system | | Issued | | 8/16/1979 |
| SA8532SW-D | | Installation of a Century Flight Systems Inc. Automatic Flight System Model AK1058 consisting Century I Autopilot with Radio Tracker. | | Issued | | 8/13/1999 |
| SA93NW | | Installation of a modified engine cowl wing trailing edge/body fillet and a 16-gallon auxiliary fuel tank | | Issued | | 3/1/1974 |
