# Aeronca 7GCBC - Type: Aircraft model (FAA registry) - Registry code: 2110133 - Manufacturer (registry): AERONCA - Model: 7GCBC - Aircraft type: Fixed wing single engine - Category: Airplane - Engines: 1 · Reciprocating - Seats: 2 - Weight class: Up to 12,499 lb - Certification: Type certificated - Data sheet: [TCDS A-759](https://openairdocs.org/tcds/A-759) (OpenAirDocs) - Holder: American Champion Aircraft Corp. - Registered aircraft: 1 - Page: https://openairdocs.org/model/aeronca-7gcbc Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2022-03-15](https://openairdocs.org/ad/2022-03-15): Fuel Quantity Indicator · Garmin G3X Touch Electronic Flight Instrument System (STC SA01899WI or SA02658SE). Effective Mar 21, 2022 - [AD 2009-22-02](https://openairdocs.org/ad/2009-22-02): Rear seat back hinge area and excessive elongation of the rear seat hinge bolt hole · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Dec 3, 2009 - [AD 2006-12-07](https://openairdocs.org/ad/2006-12-07): ECi cylinder assemblies · Aerostar AEIO-320-D1B, AEIO-320-D2B, AEIO-320-E1A and 386 more. Effective Jul 11, 2006 - [AD 2006-03-08](https://openairdocs.org/ad/2006-03-08): Vacuum pumps · Aero Advantage 14-19, 14-19-2, 14-19-3 and 299 more. Effective Mar 10, 2006 - [AD 2005-24-10](https://openairdocs.org/ad/2005-24-10): Pilot's Operating Handbook (POH) limitation · American Champion 7AC, 7ACA, 7BCM (Army L-16A) and 21 more. Effective Jan 17, 2006 - [AD 2000-25-02 R1](https://openairdocs.org/ad/2000-25-02-R1): Wood Spars · American Champion 11AC, 11BC, 11CC and 27 more. Effective Jul 13, 2001 - [AD 96-18-02](https://openairdocs.org/ad/96-18-02): Wing Strut Attach Fittings · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Sep 20, 1996 - [AD 89-18-06](https://openairdocs.org/ad/89-18-06): Front Folding Seats · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Sep 21, 1989 - [AD 80-25-07 R1](https://openairdocs.org/ad/80-25-07-R1): Oil Coolers · American Champion 7ECA, 7GCAA, 7GCBC and 39 more. Effective Sep 24, 1981 - [AD 81-16-04](https://openairdocs.org/ad/81-16-04): Competition Harness Installation · American Champion 7ECA, 7GCAA, 7GCBC and 2 more. Effective Jul 28, 1981 - [AD 80-21-06](https://openairdocs.org/ad/80-21-06): Muffler Core and Body Assembly · American Champion 7ECA, 7GC, 7GCA and 8 more. Effective Oct 16, 1980 - [AD 79-07-02](https://openairdocs.org/ad/79-07-02): Batteries · Aircraft Parts & Development A, A-2, A-3 and 149 more. Effective Apr 3, 1979 - [AD 77-22-05](https://openairdocs.org/ad/77-22-05): Operating Limitations · American Champion 7ECA, 7GC, 7GCA and 5 more. Effective Nov 7, 1977 - [AD 76-22-01](https://openairdocs.org/ad/76-22-01): Adjustable Front Seat · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Nov 2, 1976 - [AD 75-17-16](https://openairdocs.org/ad/75-17-16): Engine Power Loss · American Champion 7ECA, 7GCAA, 7GCBC and 3 more. Effective Aug 12, 1975 - [AD 72-20-06](https://openairdocs.org/ad/72-20-06): Aerobatic Flight Placard · American Champion 7ECA, 7GCAA, 7GCBC and 2 more. Effective Oct 5, 1972 - [AD 72-18-03](https://openairdocs.org/ad/72-18-03): Corrosion of Rudder and Elevator Cables · American Champion 7GCAA, 7GCBC, 7KCAB and 1 more. Effective Sep 1, 1972 - [AD 71-20-04](https://openairdocs.org/ad/71-20-04): Lower Fuselage Longeron · American Champion 7ECA, 7GCAA, 7GCBC and 1 more. Effective Sep 30, 1971 - [AD 67-03-02](https://openairdocs.org/ad/67-03-02): Fuel Shutoff Valve Bracket · American Champion 7ECA, 7GCAA, 7GCB and 1 more. Effective Jan 18, 1967 - [AD 48-39-01](https://openairdocs.org/ad/48-39-01): Control Stick Rework · American Champion 7AC, 7ACA, 7BCM (Army L-16A) and 19 more - [AD 48-08-02](https://openairdocs.org/ad/48-08-02): Cleveland Wheels · American Champion 11AC, 11BC, 11CC and 33 more Historical (superseded or no longer in force): - [AD 96-03-11](https://openairdocs.org/ad/96-03-11) (historical): Wing Front Strut Fittings · American Champion 7ECA, 7GCBC, 8GCBC and 1 more. Effective Feb 26, 1996 ## Information bulletins (advisory) (8) - [SAIB SW-18-31](https://openairdocs.org/saib/SW-18-31): NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM. Issued Nov 21, 2018 - [SAIB CE-18-20](https://openairdocs.org/saib/CE-18-20): Electrical Power. Issued Jul 12, 2018 - [SAIB CE-13-40](https://openairdocs.org/saib/CE-13-40): Flight Compartment. Issued Jul 12, 2013 - [SAIB CE-11-43](https://openairdocs.org/saib/CE-11-43): Flight Controls. Issued Jul 6, 2011 - [SAIB CE-10-39](https://openairdocs.org/saib/CE-10-39): Equipment - Furnishings. Issued Jul 23, 2010 - [SAIB CE-09-20](https://openairdocs.org/saib/CE-09-20): Equipment - Furnishings. Issued Mar 20, 2009 - [SAIB CE-07-45](https://openairdocs.org/saib/CE-07-45): Flight Controls. Issued Aug 24, 2007 - [SAIB CE-04-83](https://openairdocs.org/saib/CE-04-83): . Issued Sep 9, 2004 ## Registered aircraft (1) - [N81425](https://openairdocs.org/aircraft/N81425): [Pegasus Copters LLC](https://openairdocs.org/faa-owner/PEGASUS%20COPTERS%20LLC), [Makawao, HI](https://openairdocs.org/faa-place/HI/Makawao), built 1945, S/N 7AC-42 ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (46) As reported by operators and repair stations, by the model named in the report. - [SDR CA141020007](https://openairdocs.org/sdr/CA141020007), Oct 20, 2014: SPAR. CRACKED. (CAN) DURING INSPECTION FOR FERRY FLIGHT DEFECT IN BUTT END OF SPAR AT ATTACH FITTING NOTICED A/C GROUND FOR REPAIRS AND FURTHER EVALUATION. - [SDR CA140925006](https://openairdocs.org/sdr/CA140925006), Sep 22, 2014: BATTERY PACK. INOPERATIVE. (CAN) DURING THE ANNUAL INSPECTION OF THE ELT, IT WAS DISCOVERED THAT THE BATTERIES WERE TIME-EXPIRED AND VERY LOW VOLTAGE (LESS THAN 1 VOLT FOR 3 OUT OF 4 BATT - [SDR 2014FA0000451](https://openairdocs.org/sdr/2014FA0000451), Jul 25, 2014: MAGNETO. FAILED. AFTER GROUND RUN, DISCOVERED THAT THE LT MAGNETO HAD FAILED IN FLIGHT. - [SDR OXZS2014022000092](https://openairdocs.org/sdr/OXZS2014022000092), Feb 4, 2014: HANDLE. CRACKED. HANDLE CRACKED AND SNAPPED OFF RENDERING THE FLAPS UNUSABLE. THIS OCCURRED AFTER 13 YEARS OF REGULAR USAGE. THE CAUSE WAS PROBABLY RELATED TO DESIGNS OF THE HAN - [SDR 2013FA0000441](https://openairdocs.org/sdr/2013FA0000441), Jul 16, 2013: SPAR. CRACKED. DURING INSPECTION OF WING IAW AD 2000-25-02R1, FOUND CRACK IN REAR SPAR ABOUT THREE INCHES LONG. ORIGINATES FROM FLAP SUPPORT BRACKET ATTACH POINT OUTWARD. - [SDR 2010FA0000936](https://openairdocs.org/sdr/2010FA0000936), Aug 3, 2010: IGNITION SWITCH. MISMANUFACTURED. THE SWITCH WAS INSTLLED IN ACFT ON 8/3/10. IT WAS BRAND NEW, RIGHT OUT OF THE BOX. THIS MODEL SWITCH HAS THE STARTER FUNCTION. WHEN THE SWITCH WAS TURNED TO THE - [SDR CA090915003](https://openairdocs.org/sdr/CA090915003), Jul 29, 2009: FOLLOWER. BROKEN. (CAN) HEAD OF CAM FOLLOWER BROKE OFF AND JAMMED UNDER HEAD OF AJOINING FOLLOWER, DAMAGING CRANKCASE. (TC# 20090915003) - [SDR 2009FA0000454](https://openairdocs.org/sdr/2009FA0000454), May 28, 2009: TAIL WHEEL. CRACKED. FOUND TAILWHEEL HAD LONGITUDINAL CRACK IN BRACKET ASSEMBLY. - [SDR 2008FA0000323](https://openairdocs.org/sdr/2008FA0000323), May 4, 2008: SLEEVE. CRIMPED. RIGHT RUDDER CABLE SEPARATED AT RUDDER BELLCRANK DURING RECOVERY OF INTENTIONAL LEFT SPIN. CABLE APPARENTLY PULLED OUT OF NICOPRESS SLEEVE. AIRPLANE WAS LANDED - [SDR CA061120006](https://openairdocs.org/sdr/CA061120006), Nov 20, 2006: RUDDER PEDAL. CRACKED. (CAN) DURING REPLACEMENT OF THE FUEL SHUTOFF VALVE THE LT FRONT RUDDER/BRAKE PEDAL WAS FOUND CRACKED BETWEEN THE BRAKE PEDAL UPRIGHT AND THE OB PEDAL HINGE. THE - [SDR CA061002005](https://openairdocs.org/sdr/CA061002005), Aug 31, 2006: CABLE. DAMAGED. (CAN) IAW AD 2005-24-10 AND MFG SERVICE LETTER NR 427, THE FLIGHT CONTROL CABLE INCLUDED IN THE WING RETROFIT KIT WAS INSPECTED FOR PROPER SWAGING. AILERON CABL - [SDR 2006FA0000500](https://openairdocs.org/sdr/2006FA0000500), Apr 28, 2006: SPAR. CRACKED. DURING WING RECOVER, FOUND LT WING FRONT SPAR WITH A CRACK ORIGINATING AT THE BUTT END, FOLLOWING THE WOOD GRAIN OB THROUGH UPPER ATTACH BRACKET HOLES AND EXTEN - [SDR 2005FA0001442](https://openairdocs.org/sdr/2005FA0001442), Sep 30, 2005: CONTROL CABLE. BROKEN. LT RUDDER CABLE BROKE NEAR REAR SEAT BACK HINGE PIVOT BOLT. NO EVIDENCE OF CABLE CHAFFING ON REAR SEAT FRAME, PULLEY AREA, CABLE GUIDE OR SIDE PANEL UPHOLSTERY. - [SDR 2005FA0001356](https://openairdocs.org/sdr/2005FA0001356), Sep 22, 2005: SPAR. CRACKED. CRACKED SPAR PLATE AT WING STRUT ATTACHMENT LT WING. APPEARS THAT SOME ONE HAS ATTEMPTED TO ADD GLUE TO PLATE FROM A HOLE CUT INTO FABRIC ON TOP WING. IN OTHER - [SDR CA041221003](https://openairdocs.org/sdr/CA041221003), Dec 10, 2004: MUFFLER. CRACKED. (CAN) AD CF90-03R2 REQUIRES PRESSURE TESTING OF MUFFLERS USED FOR CABIN HEAT. CRACK NOTED AT RT END PLATE ABOVE INLET PORT, AT OUTER EDGE OF PREVIOUS WELD REPAI - [SDR 2004FA0000773](https://openairdocs.org/sdr/2004FA0000773), Jun 27, 2004: LINE. CHAFED. IN COMPLIANCE WITH MFG SL NR 419. FOUND FUEL LINE CHAFED OVER .5000 WAY THROUGH TUBE WALL. CAUSED BY FLAP ACTUATOR. CHAFE WAS NOT VISIBLE. FOUND BY FEELING. REC - [SDR 2004FA0000574](https://openairdocs.org/sdr/2004FA0000574), Jun 11, 2004: SPAR. DAMAGED. TWO SPARS SPLIT AT WING ROOT WING ATTACH FITTINGS, ONE SPAR SPLIT AT WING LIFT STRUT ATTACH FITTING. SPLITS FOUND DURING ANNUAL INSPECTION. PROBABLE CAUSE: DRYI - [SDR CA040512005](https://openairdocs.org/sdr/CA040512005), May 7, 2004: SPAR. CHAFED. (CAN) ON METAL-SPAR WINGS RETROFITTED TO THIS AC THE AFT SPARS HAVE THREE FOOT STIFFENERS RIVETED TO THEM AT AFT STRUT ATTACH POINT. CLEARANCE BETWEEN FABRIC AN - [SDR 2004F00121](https://openairdocs.org/sdr/2004F00121), Mar 26, 2004: LEG ASSY. BROKEN. UPON LANDING, GEAR RT MLG, BROKE FLUSH AT FUSELAGE. AIRCRAFT HAD SADDLE BLOCKS INSTALLED BY STC437SWP. THE LANDING GEAR BREAK, SHOW SIGNS OF INTERGRANULAR CORRO - [SDR CA031203005](https://openairdocs.org/sdr/CA031203005), Nov 19, 2003: LINE. LOOSE. (CAN) PILOT REPORTED LOW OIL PRESSURE AND SMOKE. LANDED OFF AIRPORT TO MINIMIZE POSSIBLE DAMAGE TO ENGINE. NO LOSS OF POWER. INSPECTION REVEALED A LOOSE OIL PRE - [SDR CA030708007](https://openairdocs.org/sdr/CA030708007), Apr 15, 2003: WINDOW. DAMAGED. (CAN) THE ONLY EXPLANATION WE HAVE FOR THIS BURNED AREA COMES FROM THE FEW TIMES THIS AIRCRAFT HAS BEEN PARKED OUTSIDE, OR DURING FLIGHT. IT MIGHT SOUND CRAZY, - [SDR 2003FA0000226](https://openairdocs.org/sdr/2003FA0000226), Feb 19, 2003: PUSHROD. LOOSE. AILERON RODEND JAM NUTS FOUND LOOSE. HAVE FOUND SIMULAR CONDITION ON PREVIOUS AIRCRAFT NEW FROM FACTORY. - [SDR CA030218006](https://openairdocs.org/sdr/CA030218006), Feb 5, 2003: TUBE. CRACKED. (CAN) AIRCRAFT HAS OVER 2,700 HOURS OF TOWING GLIDERS OFF A GRASS STRIP. DEFECT WAS FOUND DURING RECOVERING OF FUSELAGE. VERTICAL CRACK ON BOTH SIDES OF LT REAR - [SDR CA030106017](https://openairdocs.org/sdr/CA030106017), Aug 27, 2002: COTTER PIN. BROKEN. (CAN) DURING A SCHEDULED INSPECTION THE FLAP HANDLE RELEASE ASSEMBLY WAS NOT ENGAGING THE FLAPS IN THE CORRECT DEGREES SETTING. UPON INVESTIGATING THE FLAP HAND - [SDR CA020313001](https://openairdocs.org/sdr/CA020313001), Mar 13, 2002: SPAR. CRACKED. (CAN) LT WING SPAR CRACKS WERE FOUND. THE FRONT SPAR WAS CRACKED FROM THE STRUT ATTACHMENT OUTBOARD. THE REAR SPAR HAD A SEVERE COMMPRESSION CRACK STARTING 3 FE - [SDR CA020408006](https://openairdocs.org/sdr/CA020408006), Mar 11, 2002: AXLE. SHEARED. (CAN) DURING THE TAKEOFF RUN ON ICE THE AIRCRAFT CROSSED OVER SOME SMALL SNOWMOBILE TRACKS. WHEN THE AIRCRAFT BECAME AIRBORNE THE RIGHT SKI SEPARATED. THE SKI, - [SDR 2002FA0000236](https://openairdocs.org/sdr/2002FA0000236), Oct 17, 2001: SPAR. CRACKED. FOUND A CRACK AT THE SPAR BUTT ON THE RIGHT FORWARD SPAR WHILE COMPLYING WITH AD. THE CRACK WAS CLOSE TO THE WING ATTACH FITTING WHICH LIMITED THE ABILITY TO FU - [SDR 2001FA0000415](https://openairdocs.org/sdr/2001FA0000415), Oct 4, 2001: SPAR. CRACKED. WHILE INSPECTING WING SPARS IN COMPLIANCE WITH AD, THE FRONT SPAR IN THE RIGHT WING WAS FOUND TO HAVE A COMPRESSION CRACK AT THE BUTT END AND THE REAR SPAR IN T - [SDR 2002FA0000237](https://openairdocs.org/sdr/2002FA0000237), Aug 13, 2001: FASTENER. LOOSE. RIGHT WING: 16 LOOSE NAILS, 3 VERY LOOSE, 1 MISSING LEFT WING: 9 LOOSE NAILS, 0 VERY LOOSE, 0 MISSING. - [SDR 2002FA0000251](https://openairdocs.org/sdr/2002FA0000251), Jul 17, 2001: SPAR. CRACKED. DETECTED COMPRESSION CRACK AT TOP OF AFT SPAR ON THE OUTBOARD END OF LIFT STRUT DOUBLER PLATE. CRACK PROGRESSED DOWN AFT SIDE ABOUT 1 INCH. LONGITUDINAL CRACK W - [SDR 20010613CW006](https://openairdocs.org/sdr/20010613CW006), May 26, 2001: ARM. WORN. AN4 BOLT ACTS AS TERMINAL END OF CARBURETOR HEAT CABLE AND IS FREE TO ROTATE IN HOLE DRILLED NEAR END OF SHAFT ASSY ARM OF CARB HEAT BUTTERFLY VALVE IN CARB AIR - [SDR LAO2002F00000](https://openairdocs.org/sdr/LAO2002F00000), Apr 1, 2001: SPAR. CRACKED. DURING AN ANNUAL INSPECTION AD (WING SPAR CRACKING) WAS COMPLIED WITH IAW SB PER AD. A LONGITUDINAL CRACK WAS FOUND IN THE FRONT LEFT HAND WING SPAR THAT STARTE - [SDR 20010419CW005](https://openairdocs.org/sdr/20010419CW005), Feb 20, 2001: NUT. MISMANUFACTURED. FOUND NEW AXLE NUTS TO HAVE CHAMFER CUT ON INSIDE DIAMETER, WHERE NUT CONTACTS BEARING. CONTACTED MFG., CONFIRMED THAT NO CHAMFER SHOULD BE PRESENT ON INSIDE DI - [SDR 20000731SH003](https://openairdocs.org/sdr/20000731SH003), Jul 6, 2000: BOLT. BROKEN. LEFT SIDE, LANDING GEAR DEPARTED AIRCRAFT. (X) - [SDR 20000731SH002](https://openairdocs.org/sdr/20000731SH002), Jul 6, 2000: BOLT. BROKEN. LEFT SIDE, LANDING GEAR DEPARTED AIRCRAFT. (X) - [SDR CA000530027](https://openairdocs.org/sdr/CA000530027), Apr 11, 2000: AXLE. CRACKED. (CAN) CRACK FOUND IN BEND JUST BELOW FORWARD UPPER BOLT HOLE - [SDR 99ZZZX3094](https://openairdocs.org/sdr/99ZZZX3094), Aug 5, 1999: SPAR. CRACKED. WHILE C/W AD 98-05-04 INSPECTING WING SPARS FOR CRACKS, FOUND A CRACK ON THE RT FORWARD INBOARD SPAR ATTACH POINT. THE CRACK PROTRUDED OUT FROM UNDERNEATH A PLY - [SDR 97ZZZX4812](https://openairdocs.org/sdr/97ZZZX4812), Aug 31, 1997: P LEAD. SHORTED. FORCED LANDING DUE TO ENGINE STOPPAGE. INVESTIGATION DETERMINED ENGINE STOPPAGE DUE TO WIRE BETWEEN MASTER SWITCH LOCATED ABOVE AND LEFT OF PILOT'S HEAD AND THE - [SDR 97ZZZX2902](https://openairdocs.org/sdr/97ZZZX2902), Jun 12, 1997: SPAR. CRACKED. WHILE C/W AMERICAN CHAMPION SL 406 RE: CRACKED SPARS. BOTH MAIN SPARS FOUND TO HAVE HAIRLINE CRACKS OPPOSITE THE UPPER INBOARD ATTACH BOLT FOLLOWING THE SPAR GR - [SDR 97ZZZX2901](https://openairdocs.org/sdr/97ZZZX2901), Jun 12, 1997: SPAR. CRACKED. WHILE C/W AMERICAN CHAMPION SL 406 RE: CRACKED SPARS. BOTH MAIN SPARS FOUND TO HAVE HAIRLINE CRACKS OPPOSITE THE UPPER INBOARD ATTACH BOLT FOLLOWING THE SPAR GR - [SDR 97ZZZX539](https://openairdocs.org/sdr/97ZZZX539), Jan 17, 1997: FITTING. CRACKED. DURING INVESTIGATION OF FATAL ACCIDENT (MIA97FA047), THE LEFT FORWARD LIFT STRUT TO WING SPAR FITTING WAS FOUND CRCKED IN 2 PLACES AT THE OUTBOARD WELD TERMINAL - [SDR AU960856](https://openairdocs.org/sdr/AU960856), Apr 25, 1996: SHAFT. WORN. (AUS) ENGINE CRANKSHAFT LH IDLER GEAR SHAFT ATTACHMENT HOLES ELONGATED,LOCKWIRE BROKEN, BOLTS NECKED AND SHAFT LOOSE - [SDR CA960320003](https://openairdocs.org/sdr/CA960320003), Feb 15, 1996: SPAR. CRACKED. (CAN)SUBJECT SPAR INDICATED IRREGULAR LINES ACROSS THE GRAIN AT 14 INCHES AND 92 INCHES FROM THE ROOT END, BOTH FORE AND AFT FACES. REFERENCE MATERIAL ENCYCLOPE - [SDR CA960320001](https://openairdocs.org/sdr/CA960320001), Feb 15, 1996: BOLT. CORRODED. (CAN)DURING SPAR REPLACEMENT ON THE WING, ALL BOLTS WERE FOUND TO BE CORRODING WHERE THEY CONTACT THE WOOD. THE HEAD AND THREAD OF THE BOLTS WAS FOUND TO BE CLE - [SDR CA951027007](https://openairdocs.org/sdr/CA951027007), Oct 19, 1995: SPAR. CRACKED. (CAN)SUBJECT SPAR INDICATED IRREGULAR LINES ACROSS THE GRAIN AT 163 INCHES FROM THE ROOT END. FORE AND AFT SPAR FACES CLEANED AND SANDED & THE VERTICAL LINES RE - [SDR 95ZZZX6808](https://openairdocs.org/sdr/95ZZZX6808), Sep 21, 1995: ELT. ANTENNA DETACHED. THE AUXILIARY ANTENNA THAT IS ATTACHED TO THE ELT BODY HAS FALLEN OFF TWICE AND DISAPPEARED INTO THE BELLY OF THE AIRCRAFT. THE OWNER HAS FOUND IT EACH TIME. HO ## STCs that may be installed (OpenAirDocs) (183, first 50) Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has. - [STC SA01233SE](https://openairdocs.org/stc/SA01233SE): Fabrication and installation of Alaskan Bushwheel LLC tail wheel and fork assembly. ABI, LLC - [STC SA02571SE](https://openairdocs.org/stc/SA02571SE): Installation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display). Garmin International Inc - [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC - [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC - [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC - [STC SA04652CH](https://openairdocs.org/stc/SA04652CH): To allow use of 100R grade aviation fuel meeting Swift Fuel, LLC specification. Swift Fuels LLC - [STC SA02636SE](https://openairdocs.org/stc/SA02636SE): Installation of Garmin GPS 175 Navigation System and GNX 375 Navigation System with ADS-B In/Out Transponder. Garmin International Inc - [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc - [STC SA800EA](https://openairdocs.org/stc/SA800EA): Installation of Whelen Anti-Collision, Position, or Anti-Collision/Position Light System, and applicable associated power supplies. Whelen Aerospace Technologies - [STC SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc - [STC SA33CE](https://openairdocs.org/stc/SA33CE): If Champion Part Number 7-480 door is installed, remove two of AN 380-2-2 cotter pins and two of AN 393-3 flat head pins as necessarry to remove one door. If American Champion Part Number 7-1265 door is installed, remove quick release pins to remove one door. Weight change --10lb at +21.06 arm. National Aeronca Association - [STC SA00081NY](https://openairdocs.org/stc/SA00081NY): Installation of Iceman Aviation Supplies, Inc. Carburetor Ice Detector. Alcor LLC - [STC SA04046CH PAGE 1](https://openairdocs.org/stc/SA04046CH%20PAGE%201): Installation of L-3 GENESIS (TM) Electronic Standby Instrument System (ESI-500/MAG-500). Acron Aviation Inc - [STC SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC - [STC SA2699CE](https://openairdocs.org/stc/SA2699CE): Installation of aileron spades. Rainbow Flying Services - [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd - [STC SA02594SE](https://openairdocs.org/stc/SA02594SE): SkyView HDX Instrumentation and Autopilot System manufactured. Dynon Avionics - [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc - [STC SA01899WI](https://openairdocs.org/stc/SA01899WI): Installation of Garmin G3X Touch Electronic Flight Instrument System. Garmin International Inc - [STC SA02576AK](https://openairdocs.org/stc/SA02576AK): Installation of Cleveland and ABI, LLC Wheel and Brake Kits. ABI LLC - [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC - [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation - [STC SA04776NY](https://openairdocs.org/stc/SA04776NY): The HIPEC Covering and Finishing System must be performed and maintained. HIPEC Aircraft Coatings Inc - [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC - [STC SA03819NY](https://openairdocs.org/stc/SA03819NY): Installation and maintenance of Oratex 6000 Covering and Coating System. Lanitz-Prena Folien Factory GmbH - [STC SA01015SE](https://openairdocs.org/stc/SA01015SE): Installation of eligible Alaska Bushwheel, Inc. wheels and TSO-C62d tires. ABI LLC - [STC SA01818WI](https://openairdocs.org/stc/SA01818WI): Installation of Garmin G5 Electronic Flight Instrument. Garmin International Inc - [STC SA02553AK](https://openairdocs.org/stc/SA02553AK): Fabrication and installation of a Tail Wheel Anti-Shimmy Dampener. Keller Engineering Group LLC - [STC SA11174SC PAGE 1](https://openairdocs.org/stc/SA11174SC%20PAGE%201): Installation of BendixKing by Honeywell KSN 770 and KSN 765 WAAS LPV approach capable nav/comm systems. Honeywell International Inc (Bendix King) - [STC SA1151NW](https://openairdocs.org/stc/SA1151NW): Installation of the Flight Grip Model 135 Control Stick Grip. Air Products & Parts LLC - [STC SA10822SC](https://openairdocs.org/stc/SA10822SC): Installation of EFD1000 Primary Flight Display. Aspen Avionics Inc - [STC SA220SO](https://openairdocs.org/stc/SA220SO): Tow bar, release mechanism, and safety tow link. Fliegen Works Inc. d/b/a Pacific Aerial Tow Hooks - [STC SA00401BO](https://openairdocs.org/stc/SA00401BO): Installation of a SkyTrax100B UAT receiver. Avidyne Corporation - [STC SA00410BO](https://openairdocs.org/stc/SA00410BO): Installation of an AV-30-C Multi-Mode Indicator. uAvionix Corporation - [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation - [STC SA04301CH](https://openairdocs.org/stc/SA04301CH): Attachment of fabric covering and wing leading edge. C William Pancake Jr - [STC SA2710WE](https://openairdocs.org/stc/SA2710WE): Installation of carburetor heat box bearings. Del-Air - [STC SA02529AK](https://openairdocs.org/stc/SA02529AK): Installation of the GSD Landing Gear System, Aeronca/American Champion 7 & 11 series airplanes. Mr. Ernie Broten - [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc - [STC SA33GL](https://openairdocs.org/stc/SA33GL): Installation of EDO Model 88A-1650 floats. Kenmore Air EDO Floats LLC - [STC SA04032CH](https://openairdocs.org/stc/SA04032CH): Install rocker switch assemblies. Electroair Acquisition Corporation - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies - [STC SA615EA](https://openairdocs.org/stc/SA615EA): Installation of a Whelen Anti-Collision Strobe Light System as replacement for originally installed anti-collision lights. Whelen Aerospace Technologies - [STC SA21NW](https://openairdocs.org/stc/SA21NW): Installation of a 70 pound baggage compartment in either or both EDO 89-2000, 89A-2000 or 689-2130 floats. Kenmore Air Harbor Inc - [STC SA04362CH](https://openairdocs.org/stc/SA04362CH): Installation of the uAvionix skyBeacon Automatic Dependent Surveillance-Broadcast (ADS-B) Out. uAvionix Corporation - [STC SA01435SE](https://openairdocs.org/stc/SA01435SE): Installation of J.P. Instruments (JPI) Primary Engine Data Management System. J. P. Instruments - [STC SA02153LA-D PAGE 2](https://openairdocs.org/stc/SA02153LA-D%20PAGE%202): Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Garmin International Inc - [STC SA513AL](https://openairdocs.org/stc/SA513AL): Installation of Hartzell model HC-C2YL-1BF/F8468A-8R constant speed propeller. Truby Proctor - [STC SA00024NY](https://openairdocs.org/stc/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. Airwolf Filter Corporation - [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc All 183: https://openairdocs.org/model/aeronca-7gcbc/stcs.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Bellanca 7GCBC](https://openairdocs.org/model/bellanca-7gcbc): 487 registered aircraft, registry code 1220601 - [American Champion 7GCBC](https://openairdocs.org/model/american-champion-7gcbc): 232 registered aircraft, registry code 21101PL - [Champion 7GCBC](https://openairdocs.org/model/champion-7gcbc): 144 registered aircraft, registry code 21101PK --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.