# Service difficulty reports: Champion 8GCBC

A list on [Champion 8GCBC](https://openairdocs.org/model/champion-8gcbc.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 194 reports

- [SDR 2026FA0000424](https://openairdocs.org/sdr/2026FA0000424.md): Air Box · seized · Nov 10, 2025 · N565T · Bbavia 8GCBC · Engine Air Intake System
  > 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 NOTICED ON ANNUAL INSPECTION. PILOT ONLY NOTICED RESISTANCE IN THE CABLE. OEM OPINION: RARE OCCU
- [SDR 2023FA0000289](https://openairdocs.org/sdr/2023FA0000289.md): Blade · broken · May 29, 2023 · N559BC · Bbavia 8GCBC · Propeller Blade Section
  > PROPELLER BLADE SEPARATED FROM HUB ON TAKEOFF CAUSING ENGINE INBALANCE/FAILURE. PILOT MADE PRECAUTIONARY LANDING IN SOYBEAN FIELD ADJACENT TO RUNWAY. NO AIRFRAME DAMAGE FROM LANDING. NO INJURIES TO PILOT. DAMAGE TO ENGINE MOUNT, COWLING AND ENGINE DUE TO PROP
- [SDR CA190718001](https://openairdocs.org/sdr/CA190718001.md): Spar · cracked · Jul 16, 2019 · Bbavia 8GCBC · Wing Spar
  > (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.md): Cylinder · cracked · Jun 27, 2019 · Bbavia 8GCBC · Reciprocating Engine Cylinder Section
  > (CAN) HIGHER THAN EXPECTED CYLINDER HEAD TEMPERATURE (CHT), FOLLOWED BY DECREASING RPM AND A KNOCKING NOISE THAT PROGRESSIVELY GOT LOUDER. ON INSPECTION IT WAS FOUND THAT THE #3 CYLINDER WAS CRACKED STARTING FROM THE BOTTOM SPARK PLUG HOLE HEADING TOWARD AND
- [SDR CA190315010](https://openairdocs.org/sdr/CA190315010.md): Tab · cracked · Feb 12, 2019 · Bbavia 8GCBC · Elevator Tab Control System
  > (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 TO QUARANTINE. A NEW TRIM TAB WAS INSTALLED ON AIRCRAFT.
- [SDR CA190315008](https://openairdocs.org/sdr/CA190315008.md): Tab · cracked · Feb 1, 2019 · Bbavia 8GCBC · Elevator, Tab Structure
  > (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 QUARANTINE. NEW TRIM WAS INSTALLED.
- [SDR 2016FA0000282](https://openairdocs.org/sdr/2016FA0000282.md): Spar · cracked · Jun 8, 2016 · N7630S · Bbavia 8GCBC · Wing Spar
  > 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 MUCH WING OTBD OF STRUT AND ACFT TOTAL LOAD WEIGHT. THIS ACFT IS ON FLOATS PART OF THE TIME. WE A
- [SDR 2016FA0000381](https://openairdocs.org/sdr/2016FA0000381.md): Spark Plug · broken · May 2, 2016 · N64PZ · Bbavia 8GCBC · Spark Plug/Igniter
  > 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 GROUND LUG PORTION OF THE ELECTRODE. INSPECTION FOR MISSING PART INCLUDED BORESCOPE OF ALL CYLIN
- [SDR CA160301026](https://openairdocs.org/sdr/CA160301026.md): Switch · failed · Mar 1, 2016 · Bbavia 8GCBC · Emergency Locator Beacon
  > (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 ACTIVATION. THIS WAS REPEATED A THIRD TIME WITH THE SAME RESULTS. A NEW SWITCH WAS INSTALLED AND THE SYS
- [SDR CA151020002](https://openairdocs.org/sdr/CA151020002.md): Handle · failed · Oct 18, 2015 · Bbavia 8GCBC · Trailing Edge Flap Control System
  > (CAN) FLAP HANDLE MATERIAL FAILED JUST FWD OF CABLE ATTACHMENT.
- [SDR CA151020001](https://openairdocs.org/sdr/CA151020001.md): Handle · failed · Oct 18, 2015 · Bbavia 8GCBC · Trailing Edge Flap Control System
  > (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.md): Switch · failed · Aug 17, 2015 · Bbavia 8GCBC · Emergency Locator Beacon
  > (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 FOUND TO BE EXTREMELY STIFF. AN ABNORMAL AMOUNT OF PRESSURE WAS APPLIED AND THE SWITCH FINALLY MOVED
- [SDR CA150106010](https://openairdocs.org/sdr/CA150106010.md): Frame · cracked · Jan 5, 2015 · Bbavia 8GCBC · Horizontal Stabilizer, Spar/Rib
  > (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 DISCOVERED PROCEEDING FROM THE END OF THE FWD. ATTACHMENT TUBE TOWARDS THE ATTACHMENT BOLT HOLE. JU
- [SDR CA130722007](https://openairdocs.org/sdr/CA130722007.md): Pedal · broken · Jul 22, 2013 · Bbavia 8GCBC · Rudder Control System
  > (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.md): Camshaft · making metal · Jan 14, 2013 · Bbavia 8GCBC · Reciprocating Engine Power Section
  > (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 METAL WAS DISCOVERED ON THE NR 2 CYL EXHAUST LOBE. IN ADDITION WERE AND PITTING HAVE BEEN OBSERVED ON T
- [SDR CA120710013](https://openairdocs.org/sdr/CA120710013.md): Indicator · inaccurate · Jul 6, 2012 · Bbavia 8GCBC · Fuel Quantity Indicator
  > (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 INDICATOR WAS READING.5 TANK MORE FUEL THAT WHAT WAS ACTUALLY ON BOARD THE ACFT. UPON REMOVAL OF THE F
- [SDR CA111115013](https://openairdocs.org/sdr/CA111115013.md): Fuel Tank · cracked · Nov 15, 2011 · Bbavia 8GCBC · Fuel Storage
  > (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 DISCOVERED ON THE TOP OF THE INBD FUEL TANK. THE FABRIC HAD LAST BEEN REMOVED OVER THE WINTER OF 20
- [SDR CA110826003](https://openairdocs.org/sdr/CA110826003.md): Solenoid · loose · Aug 24, 2011 · Bbavia 8GCBC · Engine Starter
  > (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 APPROX.1250" PLAY AT THE END. IN THE PAST, THIS PROBLEM HAS LEAD TO INTERMITTENT STARTING.
- [SDR CA110629004](https://openairdocs.org/sdr/CA110629004.md): Cylinder · cracked · Jun 23, 2011 · Bbavia 8GCBC · Reciprocating Engine Cylinder Section
  > 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 USED FOR GLIDER TOWING AND IS O/H EVERY 2000 HRS.
- [SDR CA110531006](https://openairdocs.org/sdr/CA110531006.md): Control Handle · failed · May 26, 2011 · Bbavia 8GCBC · Trailing Edge Flap Control System
  > 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.md): Cylinder Head · cracked · May 11, 2011 · Bbavia 8GCBC · Reciprocating Engine Cylinder Section
  > 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 BORESCOPE THE CYLINDERS AT EACH 100 HR INSP TO LOOK FOR SUCH CRACKS AS PREVENTITIVE MX TO REDUCE TH
- [SDR CA110222006](https://openairdocs.org/sdr/CA110222006.md): Crankshaft · corroded · Feb 18, 2011 · Bbavia 8GCBC · Reciprocating Engine Power Section
  > (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 BEEN INSPECTED AND PITTING REMOVED AND STILL FOUND TO BE IN LIMITS. THE OPTIONAL REAR PLUG HAS BEEN
- [SDR CA110222004](https://openairdocs.org/sdr/CA110222004.md): Crankshaft · corroded · Feb 15, 2011 · Bbavia 8GCBC · Reciprocating Engine Power Section
  > (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 DUE TO PITTING PROBLEMS FOUND IN THE PAST, DESPITE THE CRANKSHAFT BEING COATED AND LABLED PID. TH
- [SDR CA110204005](https://openairdocs.org/sdr/CA110204005.md): Remote Switch · failed · Feb 3, 2011 · Bbavia 8GCBC · Emergency Locator Beacon
  > (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 SYSTEM WHEN SWITCHED BACK TO "ARM". THE REPLACEMENT OF THE ORIGINAL PROBLEM SWITCH WITH A NEW ONE IDEN
- [SDR CA110204004](https://openairdocs.org/sdr/CA110204004.md): Remote Switch · failed · Feb 3, 2011 · Bbavia 8GCBC · Emergency Locator Beacon
  > (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 PROPERLY. BUT WHEN TURNED BACK TO "ARM" THE ELT FAILED TO RESET. A MANUAL RESET WAS POSSIBLE AT THE UNIT
- [SDR CA110222005](https://openairdocs.org/sdr/CA110222005.md): Crankshaft · corroded · Feb 1, 2011 · Bbavia 8GCBC · Reciprocating Engine Power Section
  > (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 PITTING REMAINS AND AN NDT INSPECTION WAS COMPLETED AND WILL BE COMPLETED EVERY 100 HRS AS REQUIRED IA
- [SDR CA110225007](https://openairdocs.org/sdr/CA110225007.md): Crankshaft · corroded · Jan 11, 2011 · Bbavia 8GCBC · Reciprocating Engine Power Section
  > (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 WAS CORRODED. THE SB FOR A CORRODED CRANKSHAFT WAS COMPLETED AND THE PITTING WAS THEN REMOVED. THE
- [SDR CA100816006](https://openairdocs.org/sdr/CA100816006.md): Brushes · broken · Aug 10, 2010 · Bbavia 8GCBC · Magneto/Distributor
  > 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 OF THE BROKEN BRUSH. DURING THE PREINSPECTION RUN UP, THERE WERE NO INDICATIONS OF A PROBLEM. TH
- [SDR CA100816003](https://openairdocs.org/sdr/CA100816003.md): Mount · cracked · Aug 9, 2010 · Bbavia 8GCBC · Engine Mount Section
  > (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 END.
- [SDR CA090225003](https://openairdocs.org/sdr/CA090225003.md): Transfer Tube · cracked · Feb 24, 2009 · Bbavia 8GCBC · Reciprocating Engine Power Section
  > (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 TO BEGIN AT THE CORNER OF THE CUTOUT PROCEEDING AROUND THE CIRCUMFERENCE OF THE TUBE TOWARD THE OPPO
- [SDR CA090223015](https://openairdocs.org/sdr/CA090223015.md): Crankshaft · corroded · Feb 23, 2009 · Bbavia 8GCBC · Reciprocating Engine Power Section
  > 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 PROBLEM ON OTHER AIRCRAFT THE PID COATING WAS REMOVED AND PITTING SIMILAR TO THAT FOUND IN SERVICE BUL
- [SDR 2009FA0000059](https://openairdocs.org/sdr/2009FA0000059.md): Blade · cracked · Jan 23, 2009 · N326JH · Bbavia 8GCBC · Propeller Blade Section
  > 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, AFT FACE IS BLISTERING IN SEVERAL LOCATIONS. DEFECT WAS FOUND DURING PRE-FLIGHT. ACFT TT IS SA
- [SDR CA090121005](https://openairdocs.org/sdr/CA090121005.md): Crankshaft · corroded · Jan 19, 2009 · Bbavia 8GCBC · Reciprocating Engine Power Section
  > (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 CORROSION WAS DISCOVED UNDER THE PID SIMMILAR TO THAT REFERENCED IN AD 980208 AND SB 505B. IT SHOULD
- [SDR CA090112002](https://openairdocs.org/sdr/CA090112002.md): Crankshaft · corroded · Jan 8, 2009 · Bbavia 8GCBC · Reciprocating Engine Power Section
  > (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 THIS PROBLEM ON OTHER AIRCRAFT, THE PID COATING WAS REMOVED AND PITTING SIMILAR TO THAT FOUND IN SERV
- [SDR CA081204008](https://openairdocs.org/sdr/CA081204008.md): Hinge Pin · rusted · Nov 27, 2008 · Bbavia 8GCBC · Passenger/Crew Doors
  > (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 PIN (DISPITE PERIODIC LUBING) HAD BECOME RUSTED TO THE AIRFRAME PIN TABS. THE DOOR CONTINUED TO O
- [SDR CA080806012](https://openairdocs.org/sdr/CA080806012.md): Cylinder Head · cracked · Aug 1, 2008 · Bbavia 8GCBC · Reciprocating Engine Cylinder Section
  > (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 WIND LANDING AND RETURN TO HANGER. UPON SHUTDOWN AND INSP IT WAS FOUND THAT CYL NR1 HEAD HAD CRACKED
- [SDR CA080806015](https://openairdocs.org/sdr/CA080806015.md): Tire · damaged · Jul 28, 2008 · Bbavia 8GCBC · Tire
  > (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.md): Tire · damaged · Jul 28, 2008 · Bbavia 8GCBC · Tire
  > (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 0321672 OR 0422043.
- [SDR CA080806014](https://openairdocs.org/sdr/CA080806014.md): Tire · damaged · Jul 27, 2008 · Bbavia 8GCBC · Tire
  > (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 0321672 OR 0422043.
- [SDR CA080806017](https://openairdocs.org/sdr/CA080806017.md): Spar · corroded · Jun 25, 2008 · Bbavia 8GCBC · Wing Spar
  > (CAN) PART FOUND CORODED AT SPAR ATTACHMENT BOLT HOLE.
- [SDR CA080806016](https://openairdocs.org/sdr/CA080806016.md): Spar · corroded · Jun 25, 2008 · Bbavia 8GCBC · Wing Spar
  > (CAN) PART FOUND CORRODED AT SPAR ATTACHMENT BOLT HOLE.
- [SDR CA080123008](https://openairdocs.org/sdr/CA080123008.md): Fuel Tank · cracked · Jan 15, 2008 · Bbavia 8GCBC · Fuel Storage
  > (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.md): Fuel Tank · cracked · Jan 15, 2008 · Bbavia 8GCBC · Fuel Storage
  > (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 TANK. 720 HOURS SINCE THE TANK WAS REPAIRED. (TC NR 20080123007)
- [SDR CA080111002](https://openairdocs.org/sdr/CA080111002.md): Hinge · cracked · Jan 7, 2008 · Bbavia 8GCBC · Ailerons
  > (CAN) ON INSPECTION, 4 CRACKS FOUND IN CORNERS (TC NR 20080111002)
- [SDR CA080111003](https://openairdocs.org/sdr/CA080111003.md): Hinge · cracked · Jan 2, 2008 · Bbavia 8GCBC · Ailerons
  > (CAN) CRACK FOUND DURING SIRP INSP (TC NR 20080111003)
- [SDR CA071122004](https://openairdocs.org/sdr/CA071122004.md): Tank · cracked · Nov 23, 2007 · Bbavia 8GCBC · Fuel Storage
  > (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 NOTICE FUEL STAINING. RT OB TANK WAS REMOVED AND 1 INCH CRACK WAS FOUND ON THE RADIUS OF THE LATERAL RE-
- [SDR CA070320008](https://openairdocs.org/sdr/CA070320008.md): Control Cable · frayed · Feb 26, 2007 · Bbavia 8GCBC · Trailing Edge Flap Control System
  > (CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN RT WING GAP AREA. (TC NR 20070320008)
- [SDR CA070320006](https://openairdocs.org/sdr/CA070320006.md): Control Cable · frayed · Feb 26, 2007 · Bbavia 8GCBC · Trailing Edge Flap Control System
  > (CAN) FLAP CABLE FOUND FRAYED AT ALLUMINUM PULLEY IN LT WING GAP AREA. (TC NR 20070320006)
- [SDR CA070227004](https://openairdocs.org/sdr/CA070227004.md): Transfer Tube · loose · Feb 21, 2007 · Bbavia 8GCBC · Reciprocating Engine Oil System
  > (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.md): Cable · frayed · Dec 20, 2006 · Bbavia 8GCBC · Trailing Edge Flap Control System
  > (CAN) CABLE FOUND FRAYED AT FWD END WHERE CABLE BENDS HARD OFF OF HANDLE TRACK TO FWD CABLE ATTACH POINT. (TC NR 20061220001)

Next page: https://openairdocs.org/model/champion-8gcbc/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '8GCBC'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/champion-8gcbc/reports

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