# Champion 8GCBC

- Type: Aircraft model (FAA registry)
- Registry code: 2110301
- Manufacturer (registry): CHAMPION
- Model: 8GCBC
- Aircraft type: Fixed wing single engine
- Category: Airplane
- Engines: 1 · Reciprocating
- Seats: 3
- Weight class: Up to 12,499 lb
- Certification: Type certificated
- Data sheet: [TCDS A21CE](https://openairdocs.org/tcds/A21CE) (OpenAirDocs)
- Holder: American Champion Aircraft Corp.
- Registered aircraft: 0
- Page: https://openairdocs.org/model/champion-8gcbc

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 2006-03-08](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 79-22-01](https://openairdocs.org/ad/79-22-01): Exhaust System · American Champion 7ECA, 8GCBC and 8KCAB. Effective Oct 29, 1979
- [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 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 75-04-12](https://openairdocs.org/ad/75-04-12): Markings on Tachometer · American Champion 8GCBC. Effective Feb 21, 1975
- [AD 74-15-07](https://openairdocs.org/ad/74-15-07): Propeller Mounting · American Champion 8GCBC. Effective Jul 26, 1974

Historical (superseded or no longer in force):

- [AD 98-05-04](https://openairdocs.org/ad/98-05-04) (historical): Wood Spar Wing · American Champion 8GCBC. Effective Apr 17, 1998
- [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

None registered with this model now.

## NTSB investigations (2)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ANC01FAMS1](https://openairdocs.org/ntsb/ANC01FAMS1), Dec 27, 2000: Champion 8GCBC (N7100C), Juneau, AK, destroyed, 2 fatal. Probable cause: Undetermined. Missing airplane.
- [NTSB BFO87FA003](https://openairdocs.org/ntsb/BFO87FA003), Oct 8, 1986: Bellanca 8GCBC (N7100C), Keysville, VA, substantial damage

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 20001227027899A](https://openairdocs.org/incident/20001227027899A), Dec 27, 2000: Bbavia 8GCBC (N7100C), Juneau, AK, No damage, 2 fatal. (-23) On 12-27-00, Mr. Stephen zecker, private pilot, went to do a biannual flight review in his belanca scout, N7100C. He was flying with edgar burch, a…

## Service difficulty reports (194, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2026FA0000424](https://openairdocs.org/sdr/2026FA0000424), Nov 10, 2025: AIR BOX. SEIZED. 8GCBC WITH IO-390-A1B6 FRONT FACING AIR BOX. ACTUATING ARM FOR ALTERNATE AIR SEIZED AND STUCK IN 'OFF' POSITION. SINCE ALTERNATE AIR IS RARELY NEEDED, WAS ONLY 
- [SDR 2023FA0000289](https://openairdocs.org/sdr/2023FA0000289), May 29, 2023: BLADE. BROKEN. PROPELLER BLADE SEPARATED FROM HUB ON TAKEOFF CAUSING ENGINE INBALANCE/FAILURE. PILOT MADE PRECAUTIONARY LANDING IN SOYBEAN FIELD ADJACENT TO RUNWAY. NO AIRFRAM
- [SDR CA190718001](https://openairdocs.org/sdr/CA190718001), Jul 16, 2019: SPAR. CRACKED. (CAN) ROUTINE INSPECTION BEFORE A/C WAS DEPARTING ON LONG CONTRACT AWAY BASE. CRACKS EMANATING FROM NAIL HOLES ON SPAR DOUBLER. (TC# 20190718001)
- [SDR CA190723008](https://openairdocs.org/sdr/CA190723008), Jun 27, 2019: CYLINDER. CRACKED. (CAN) HIGHER THAN EXPECTED CYLINDER HEAD TEMPERATURE (CHT), FOLLOWED BY DECREASING RPM AND A KNOCKING NOISE THAT PROGRESSIVELY GOT LOUDER. ON INSPECTION IT WAS 
- [SDR CA190315010](https://openairdocs.org/sdr/CA190315010), Feb 12, 2019: TAB. CRACKED. (CAN) ON A 100HR INSPECTION OF THE ELEVATOR TRIM TAB, THE TAB WAS OBSERVED TO BE CRACKED AT THE TOP RIVET OF THE BELL CRANK. THE TRIM TAB WAS REMOVED AND SENT T
- [SDR CA190315008](https://openairdocs.org/sdr/CA190315008), Feb 1, 2019: TAB. CRACKED. (CAN) ON A 100HR INSPECTION OF THE ELEVATOR TRIM TAB, THE TAB WAS FOUND TO BE CRACKED AT TOP RIVET ON THE BELL CRANK. THE TRIM WAS REMOVED AND SENT TO QUARANTIN
- [SDR 2016FA0000282](https://openairdocs.org/sdr/2016FA0000282), Jun 8, 2016: SPAR. CRACKED. CRACK IN REAR LT REAR SPAR 2ND BAY PAST STRUT FITTING. CRACK IS NEAR A GLUE JOINT ABOUT A FOOT LONG AND .333 THE WAY DOWN THE SPAR. ACFT PROBABLE CAUSE IS TOO M
- [SDR 2016FA0000381](https://openairdocs.org/sdr/2016FA0000381), May 2, 2016: SPARK PLUG. BROKEN. SPARK PLUGS CHANGED AS REGULAR SERVICE INTERVAL. MAY 2016 PILOT REPORTED ROUGH ENGINE WITH LOSS OF POWER. FOUND LOWER POSITION PLUG IN NR 4 CYLINDER HAD MISSING
- [SDR CA160301026](https://openairdocs.org/sdr/CA160301026), Mar 1, 2016: SWITCH. FAILED. (CAN) ELT REMOTE SWITCH FAILED TO ACTIVATE THE ELT WHEN SWITCHED TO THE ON POSITION. THE SWITCH WAS RETURNED TO THE ARMED POSITION AND TRIED AGAIN WITH NO ACTIV
- [SDR CA151020002](https://openairdocs.org/sdr/CA151020002), Oct 18, 2015: HANDLE. FAILED. (CAN) FLAP HANDLE MATERIAL FAILED JUST FWD OF CABLE ATTACHMENT.
- [SDR CA151020001](https://openairdocs.org/sdr/CA151020001), Oct 18, 2015: HANDLE. FAILED. (CAN) FLAP HANDLE MATERIAL FAILED JUST FWD OF CABLE ATTACHMENT. THIS IS OUR 3RD FAILURE OF THIS PART ALONG WITH 1 CRACKED AND REMOVED FROM SERVICE.
- [SDR CA150817023](https://openairdocs.org/sdr/CA150817023), Aug 17, 2015: SWITCH. FAILED. (CAN) DURING THE 100 HR INSPECTION THE MAINTENANCE PERSONAL WENT TO TEST THE ELT FOR PROPER FUNCTION. THE REMOTE ELT SWITCH WAS ATTEMPTED TO BE ACTIVATED AND FO
- [SDR CA150106010](https://openairdocs.org/sdr/CA150106010), Jan 5, 2015: FRAME. CRACKED. (CAN) DURING THE DND STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), THE STABILIZER WAS REMOVED AND STRIPPED OF ITS FABRIC AND PAINT. AT THAT POINT A CRACK WAS
- [SDR CA130722007](https://openairdocs.org/sdr/CA130722007), Jul 22, 2013: PEDAL. BROKEN. (CAN) THE FRONT RT RUDDER PEDAL BROKE INTO 2 PEICES. THIS RESULTED IN THE REAR PILOT TO BE UNABLE TO ACTIVATE THE RT BRAKE.
- [SDR CA130117013](https://openairdocs.org/sdr/CA130117013), Jan 14, 2013: CAMSHAFT. MAKING METAL. (CAN) DURING A 100 HR INSPECTION, METAL FILINGS WERE DISCOVERED IN THE OIL FILTER. CYLINDER 2 AND CYL NR 4 WERE REMOVED AND THE CAMSHAFT INSPECTED. MISSING META
- [SDR CA120710013](https://openairdocs.org/sdr/CA120710013), Jul 6, 2012: INDICATOR. INACCURATE. (CAN) DURING FUELING PROCEDURES, IT WAS NOTICED BY THE PILOT THAT THE LT FUEL GUAGE WAS READING INACCURATE. A DIP OF THE FUEL TANK CONFIRMED THAT THE FUEL INDIC
- [SDR CA111115013](https://openairdocs.org/sdr/CA111115013), Nov 15, 2011: FUEL TANK. CRACKED. (CAN) DURING THE IN HOUSE REQUIRED 10 YEAR STRUCTURAL INSPECTION & REPAIR PROGRAM, SIRP, THE FABRIC WAS REMOVED FROM THE WINGS & A CRACK APPROX 1 1/4" LONG WAS 
- [SDR CA110826003](https://openairdocs.org/sdr/CA110826003), Aug 24, 2011: SOLENOID. LOOSE. (CAN) DURING A 100 HR INSPECTION, IT WAS DISCOVERED THAT ONE OF THE TERMINAL ENDS OF THE STARTER SOLENOID THAT IS RIVETED INTO POSITION BECAME LOOSE AND HAD APP
- [SDR CA110629004](https://openairdocs.org/sdr/CA110629004), Jun 23, 2011: CYLINDER. CRACKED. DURING THE 100HR INSPECTION, A .5" TO 1" CRACK WAS DISCOVERED COMMING FROM THE LOWER SPARK PLUG HOLE ON NR 4 CYLINDER. CYLINDER WAS REPLACED. THIS ENGINE IS USE
- [SDR CA110531006](https://openairdocs.org/sdr/CA110531006), May 26, 2011: CONTROL HANDLE. FAILED. PILOT WAS GOING FROM 2 ND TO 4 TH NOTCH OF FLAP AND THE HANDLE FAILED. TT ON PART 1502 HRS.
- [SDR CA110512002](https://openairdocs.org/sdr/CA110512002), May 11, 2011: CYLINDER HEAD. CRACKED. DURING A 100HR INSP, A CRACK WAS DISCOVERED COMING FROM THE LOWER SPARK PLUG HOLE PROCEDING TOWARDS THE EXHAUST VALVE. IT IS COMMON PRACTICE IN THE FACILITY TO 
- [SDR CA110222006](https://openairdocs.org/sdr/CA110222006), Feb 18, 2011: CRANKSHAFT. CORRODED. (CAN) DURING A COMPANY DIRECTED 2 YEAR INSPECTION OF THE ID OF THE CRANKSHAFT IAW SB 505B, PITTING WAS DISCOVERED AND FOUND TO BE 0.082" DEEP. CRANKSHAFT HAS BE
- [SDR CA110222004](https://openairdocs.org/sdr/CA110222004), Feb 15, 2011: CRANKSHAFT. CORRODED. (CAN) THE FRONT PLUG WAS REMOVED FOR A COMPANY DIRECTED 2 YEAR CORROSION INSPECTION OF THE ID OF THE CRANKSHAFT IAW SB 505B. THIS INSPECTION WAS BEING COMPLETED
- [SDR CA110204005](https://openairdocs.org/sdr/CA110204005), Feb 3, 2011: REMOTE SWITCH. FAILED. (CAN) DURING THE TROUBLESHOOTING OF ANOTER ELT SYSTEM. IT WAS DISCOVERED THAT THE ELT REMOTE SWITCH WOULD TURN THE ELT ON PROPERLY BUT WOULD NOT RESET THE SYSTE
- [SDR CA110204004](https://openairdocs.org/sdr/CA110204004), Feb 3, 2011: REMOTE SWITCH. FAILED. (CAN) DURING A FUNCTION TEST IT WAS DISCOVERED THAT THE LED LIGHT FAILED TO WORK. AS WELL WHEN THE SWITCH WAS TURNED TO THE ON POSITION, THE ELT ACTIVATED PROPE
- [SDR CA110222005](https://openairdocs.org/sdr/CA110222005), Feb 1, 2011: CRANKSHAFT. CORRODED. (CAN) A COMPANY DIRECTED 2 YEAR INSPECTION OF THE ID OF THE CRANKSHAFT IAW SB 505B WAS COMPLETED AND PITTING WAS DISCOVERED. THE ID IS NOW AT MAX LIMITS AND PIT
- [SDR CA110225007](https://openairdocs.org/sdr/CA110225007), Jan 11, 2011: CRANKSHAFT. CORRODED. (CAN) DURING A COMPANY DIRECTED 2 YEAR INSPECTION OF THE ID OF THE CRANKSHAFT TO BE COMPLETED IAW SB 505B. DURING THE INSPECTION IT WAS DISCOVERED THAT THE ID W
- [SDR CA100816006](https://openairdocs.org/sdr/CA100816006), Aug 10, 2010: BRUSHES. BROKEN. FAA-PMA PART AM-3215 CARBON BRUSH AND SPRING WAS FOUND BROKEN OFF FLUSH WITH THE SPRING AND FELL INTO THE MAGNETO. CONTACT WAS MAINTAINED BY THE REMAINING PART 
- [SDR CA100816003](https://openairdocs.org/sdr/CA100816003), Aug 9, 2010: MOUNT. CRACKED. (CAN) THE ENGINE MOUNT WAS FOUND CRACKED ON THE LT SIDE ON THE ARM GOING FROM THE FIRE WALL TO THE UPPER LORD MOUNT JUST ABOVE THE WELD LOCATED AT THE FIRE WALL
- [SDR CA090225003](https://openairdocs.org/sdr/CA090225003), Feb 24, 2009: TRANSFER TUBE. CRACKED. (CAN) DURING THE REPAIR OF CORROSION PITTING IN THE CRANKSHAFT BORE, A CRACK WAS DISCOVERED COMING FROM THE CUTOUT ON THE OIL TRANSFER TUBE. THE CRACK APPEARS T
- [SDR CA090223015](https://openairdocs.org/sdr/CA090223015), Feb 23, 2009: CRANKSHAFT. CORRODED. UPON REMOVAL OF THE EXPANSION PLUG TO FACILITATE SLUG REMOVAL IT WAS DISCOVERED THAT THEIR WAS BUBBLING IN THE PID. BASED UPON PREVIOUS EXPERIENCE WITH THIS PRO
- [SDR 2009FA0000059](https://openairdocs.org/sdr/2009FA0000059), Jan 23, 2009: BLADE. CRACKED. PROP BLADE CRACKED FROM TIP INWARD. CRACK IS APPROX .5 INCHES FROM L/E. CRACK IS APPROX .7 INCHES LONG ON FWD. FACE AND APROX 1.2 INCHES LONG ON AFT FACE. ALSO,
- [SDR CA090121005](https://openairdocs.org/sdr/CA090121005), Jan 19, 2009: CRANKSHAFT. CORRODED. (CAN) UPON DESLUGING THE INNER BORE OF THE CRANKSHAFT, IT WAS DISCOVERED THAT THE PID COATING HAD BEGUN TO BUBBLE AND CHIP OFF. THE PID WAS REMOVED AND SURFACE 
- [SDR CA090112002](https://openairdocs.org/sdr/CA090112002), Jan 8, 2009: CRANKSHAFT. CORRODED. (CAN) UPON REMOVAL OF THE EXPANSION PLUG TO FACILITATE SLUG REMOVAL IT WAS DISCOVERED THAT THERE WAS BUBBLING IN THE PID. BASED UPON PREVIOUS EXPERIENCE WITH TH
- [SDR CA081204008](https://openairdocs.org/sdr/CA081204008), Nov 27, 2008: HINGE PIN. RUSTED. (CAN) AN ATTEMPT TO REMOVE THE ENTRANCE DOOR USING THE EMERGENCY EXIT HANDLE FOUND THAT THE SYS HAD BECOME SEIZED. UPON CLOSER INSP, IT WAS FOUND THAT THE HINGE
- [SDR CA080806012](https://openairdocs.org/sdr/CA080806012), Aug 1, 2008: CYLINDER HEAD. CRACKED. (CAN) DURING CLIMB OUT WITH GLIDER IN TOW, THE PILOT REPORTED AN ENGINE VIBRATION. THEY IMMEDIATELY INSTRUCTED THE GLIDER TO RELEASE AND THEN PREFORMED A DOWN W
- [SDR CA080806015](https://openairdocs.org/sdr/CA080806015), Jul 28, 2008: TIRE. DAMAGED. (CAN) TAIL WHEEL TIRE FOUND FLAT DURING TAXI, UPON DISASSEMBLY IT WAS FOUND THAT THE INNER CORDS WERE FOUND LET GO AND CUT THE TUBE.
- [SDR CA080806013](https://openairdocs.org/sdr/CA080806013), Jul 28, 2008: TIRE. DAMAGED. (CAN) TAIL WHEEL FOUND FLAT DURING TAXI, UPON DISASSEMBLY IT WAS FOUND THAT THE INNER CORDS WERE FOUND LET GO AND CUT THE TUBE. TIRE, BATCH NR WAS EITHER 032167
- [SDR CA080806014](https://openairdocs.org/sdr/CA080806014), Jul 27, 2008: TIRE. DAMAGED. (CAN) TAIL WHEEL FOUND FLAT DURING TAXI, UPON DISASSEMBLY IT WAS FOUND THAT THE INNER CORDS WERE FOUND LET GO AND CUT THE TUBE. TIRE, BATCH NR WAS EITHER 032167
- [SDR CA080806017](https://openairdocs.org/sdr/CA080806017), Jun 25, 2008: SPAR. CORRODED. (CAN) PART FOUND CORODED AT SPAR ATTACHMENT BOLT HOLE.
- [SDR CA080806016](https://openairdocs.org/sdr/CA080806016), Jun 25, 2008: SPAR. CORRODED. (CAN) PART FOUND CORRODED AT SPAR ATTACHMENT BOLT HOLE.
- [SDR CA080123008](https://openairdocs.org/sdr/CA080123008), Jan 15, 2008: FUEL TANK. CRACKED. (CAN) GAS FUMES WERE DETECTED AROUND AC. WHEN THE RT IB FUEL TANK WAS REMOVED A CRACK WAS FOUND AROUND THE FUEL VENT INTERCONNECT WELD. (TC NR 20080123008)
- [SDR CA080123007](https://openairdocs.org/sdr/CA080123007), Jan 15, 2008: FUEL TANK. CRACKED. (CAN) GAS FUMES WERE DETECTED AROUND AC. WHEN RT OB FUEL TANK WAS REMOVED A CRACK WAS FOUND ON A REPAIRED RADIUS OF THE LATERAL RE-ENFORCEMENT INDENT OF THE TAN
- [SDR CA080111002](https://openairdocs.org/sdr/CA080111002), Jan 7, 2008: HINGE. CRACKED. (CAN) ON INSPECTION, 4 CRACKS FOUND IN CORNERS (TC NR 20080111002)
- [SDR CA080111003](https://openairdocs.org/sdr/CA080111003), Jan 2, 2008: HINGE. CRACKED. (CAN) CRACK FOUND DURING SIRP INSP (TC NR 20080111003)
- [SDR CA071122004](https://openairdocs.org/sdr/CA071122004), Nov 23, 2007: TANK. CRACKED. (CAN) AIRCRAFT WAS IN FOR A 50 HR INSPECTION. AFTER ENGINE RUN UP, MECHANIC DETECTED GAS FUMES AND LOOKED ON THE RT SIDE ON THE AC WINGS NEAR TRAILING EDGE NOTI
- [SDR CA070320008](https://openairdocs.org/sdr/CA070320008), Feb 26, 2007: CONTROL CABLE. FRAYED. (CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN RT WING GAP AREA. (TC NR 20070320008)
- [SDR CA070320006](https://openairdocs.org/sdr/CA070320006), Feb 26, 2007: CONTROL CABLE. FRAYED. (CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN LT WING GAP AREA. (TC NR 20070320006)
- [SDR CA070227004](https://openairdocs.org/sdr/CA070227004), Feb 21, 2007: TRANSFER TUBE. LOOSE. (CAN) CRANKSHAFT FWD CAVITY OIL TRANSFER TUBE LOOSE LATERALLY AND ROTATIONALLY. CRANKSHAFT WAS REPAIRED APPROX 500 HOURS AGO. (TC NR 20070227004)
- [SDR CA061220001](https://openairdocs.org/sdr/CA061220001), Dec 20, 2006: CABLE. FRAYED. (CAN) CABLE FOUND FRAYED AT FWD END WHERE CABLE BENDS HARD OFF OF HANDLE TRACK TO FWD CABLE ATTACH POINT. (TC NR 20061220001)

All 194: https://openairdocs.org/model/champion-8gcbc/reports.md

## STCs that may be installed (OpenAirDocs) (167, 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 SA12428CH](https://openairdocs.org/stc/SA12428CH): Installation of the Lycoming Engines Electronic Ignition System (EIS). Lycoming Engines, An Operating Division of AVCO Corporation
- [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 SA12406WI](https://openairdocs.org/stc/SA12406WI): Installation of a Garmin AXIS Flight Display System. Garmin International Inc
- [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 SA02511SE](https://openairdocs.org/stc/SA02511SE): Installation of replacement fuel quantity indicator sending unit(s). CiES Inc
- [STC SA01866WI](https://openairdocs.org/stc/SA01866WI): Installation of Garmin GFC 500 Autopilot with Electronic Stability and Protection. Garmin International 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 SA02738CH](https://openairdocs.org/stc/SA02738CH): Installation of L-3 Communications Avionics Systems. Acron Aviation Inc
- [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 SA7965SW](https://openairdocs.org/stc/SA7965SW): Application of fabric and polyurethane finishing system. Shady Aviation LLC
- [STC SA01240SE](https://openairdocs.org/stc/SA01240SE): Installation of secondary voltage indication system. Visual Instruments LLC
- [STC SA04378CH](https://openairdocs.org/stc/SA04378CH): Installation of an engine modified per STC SE04349CH. SureFly Partners Ltd
- [STC SA39CH](https://openairdocs.org/stc/SA39CH): Installation of an Amphibian Landing Gear Position Advisory System/Laser Gear Advisory System. Wipaire Inc
- [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 SA02019WI](https://openairdocs.org/stc/SA02019WI): Installation of the Trig Avionics TX56, TX56A, TX57, or TX57A VHF Nav-Com Radio. Peregrine
- [STC SA00756DE](https://openairdocs.org/stc/SA00756DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT22 Transponder and an approved Global Positioning System (GPS) Position Sensor. Peregrine
- [STC SA11137SC](https://openairdocs.org/stc/SA11137SC): Installation of Plane-Power ALT-FLX alternator. Hartzell Engine Technologies, LLC
- [STC SA01606CH](https://openairdocs.org/stc/SA01606CH): Installation of alternate electro-hydraulic power pack system for operation of main wheel skis. F.Atlee Dodge Aircraft Services
- [STC SA3-423](https://openairdocs.org/stc/SA3-423): Installation of CT-3000 tail ski on airplanes equipped with Scott 3200 or 3400 tail wheels. F.Atlee Dodge Aircraft Services
- [STC SA666AL](https://openairdocs.org/stc/SA666AL): Installation of Wipaire Skis (Fluidyne Engineering Corporation) Main Wheel Skis Model C3000A. F.Atlee Dodge Aircraft Services
- [STC SA02987CH](https://openairdocs.org/stc/SA02987CH): Installation of the Electroair Electronic Ignition System. Electroair Acquisition Corporation
- [STC SA02990CH](https://openairdocs.org/stc/SA02990CH): Installation of MT Propeller model number MTV-15-B/210-58 or MTV-9-B/198-52 and corresponding spinner assembly. McFarlane Aviation LLC
- [STC SA02203AK](https://openairdocs.org/stc/SA02203AK): Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Genesys Aerosystems Inc
- [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 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 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 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 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 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 SA742NW](https://openairdocs.org/stc/SA742NW): Installation of Hartzell HC-C2YR-1BF/F7666A-O propeller on a Lycoming O-360-C1E engine. Kenmore Air Harbor LLC
- [STC SA743NW](https://openairdocs.org/stc/SA743NW): Installation of Bellanca 72 gallon fuel system. Kenmore Air Harbor LLC
- [STC SA00744DE](https://openairdocs.org/stc/SA00744DE): Installation of the Automatic Dependent Surveillance Broadcast (ADS-B) Out Equipment using a Trig Avionics TT31 Transponder and an approved position sensor. Peregrine

All 167: https://openairdocs.org/model/champion-8gcbc/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Bellanca 8GCBC](https://openairdocs.org/model/bellanca-8gcbc): 182 registered aircraft, registry code 1220803
- [American Champion 8GCBC](https://openairdocs.org/model/american-champion-8gcbc): 160 registered aircraft, registry code 2121004
- [American Champion 8GCBC](https://openairdocs.org/model/american-champion-8gcbc): 58 registered aircraft, registry code 2121005

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