Champion 8GCBC
Service difficulty reports · 194
Newest first. General aviation reporting is voluntary.
Query with SQL
duckdb -csv -c "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"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR CA061201004Tank · cracked(CAN) AIRCRAFT HAD RETURNED TO MAINTENANCE FACILITY FOR WINTER STORAGE. FUEL STAINS WERE NOTICED ON THE BOTTOM OF THE WING NEAR THE TRAILING EDGE. LT IB TANK WAS REMOVED AND A 1.5 INCH CRACKED WAS FOUND ON THE RADIUS OF THE LATERAL RE-ENFORCEMENT INDENT OF TANSDR CA060424006Spar · damaged2 HOLES FOR MOUNTING INBD FLAP HINGE BRACKET LWR ATTACH AND INBD BOLT FOR SHIM PLATE BOTH FOUND CRUDELY DRILLED AND VERY OVAL.SDR CA060424005Frame · crackedDURING THE COMPANY STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), THE RIGHT SIDE OF THE FUSELAGE FRAME WAS FOUND CRACKED IN THE AREA WHERE THE RIGHT MAIN GEAR LEG RESTS AGAINST THE AIRFRAME. THE CRACK WAS LONGITUDINAL AND WAS ABOUT 1 1/8" LONG.SDR CA060421021Crankshaft · corrodedCORROSION FOUND UNDER PID FWD ID.SDR CA060421020Crankshaft · corrodedCORROSION FOUND UNDER PID AT FWD ID.SDR CA060421019Crankshaft · corroded(CAN) FWD INNER DIA CRANKSHAFT CORRODED BEYOND LIMITS IAW AWD 98-02-08. (TC NR 20060421019)SDR CA060127006Landing Gear · cracked(CAN) 2 SMALL CRACKS UNDER UPPER RADIUS OF LANDING GEAR.SDR CA060124002Rudder Pedal · cracked(CAN) DURING THE COMPANY STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), THE AIRCRAFT RUDDER PEDALS WERE SENT FOR NDT INSPECTION WHERE IT WAS DISCOVERED THAT BOTH LT AND RT REAR RUDDER PEDALS WERE CRACKED. THESE PEDALS ARE AN OLDER STYLE PEDAL AND ARE NO LONSDR CA060116006Crankshaft · corrodedTHE CRANKSHAFT A/C WAS INSPECTED DUE TO A FAILURE OF A CRANKSHAFT ON ANOTHER AIRCRAFT IN THE FLEET (INTERNAL CORROSION). UPON REMOVAL OF THE FRONT CRANK PLUG AND CLEANING OF THE CRANKSHAFT, IT DISCOVERED THAT URETHABOND COATING WAS BLISTERING. URETHABOND REMSDR CA051205007Crankshaft · corroded(CAN) THE CRANKSHAFT OF THIS AIRCRAFT WAS INSPECTED DUE TO A FAILURE OF A CRANKSHAFT OF ANOTHER AIRCRAFT IN THE FLEET (INTERNAL CORROSION). UPON REMOVAL OF THE FRONT CRANK PLUG AND CLEANING OF THE CRANKSHAFT. IT WAS DISCOVERED THAT THE URETHABOND COATING WAS PSDR CA051101003Crankshaft · corroded(CAN) ENGINE WAS REMOVED FROM THE AIRCRAFT AND SENT TO AN OVERHAUL FACILITY FOR AN INSPECTION DUE TO A PROP STRIKE. DURING THE INSPECTION OF THE CRANKSHAFT, IT WAS NOTICED THAT THE URETHANE INTERNAL COATING (PID) WAS BLISTERING. FURTHER INSPECTION OF THE AREA SDR CA050927002Control Cable · frayed(CAN) ELEVATOR UP CONTROL CABLED FRAYED AT AFT PULLEY.SDR CA050819012Control Cable · frayed(CAN) LT AND RT FLAP CABLES FRAYED AT WING ROOT PULLEYS.SDR CA050819011Control Cable · frayed(CAN) RT FLAP CABLE FRAYED AT WING ROOT PULLEY.SDR CA050819010Control Cable · frayed(CAN) LT RUDDER CABLE FRAYED AT CABIN PULLEY.SDR CA050819009Control Cable · frayed(CAN) LT RUDDER CABLE FRAYED AT CABIN PULLEY.SDR CA050819008Control Cable · frayed(CAN) LT RUDDER CABLE FRAYED AT CABIN PULLEY.SDR CA050819007Control Cable · frayed(CAN) RT FLAP WING ROOT CABLE FRAYED AT PULLEY.SDR CA050819006Leaf Spring · broken(CAN) MAIN LEAF SPRING BROKEN AT ALIGNMENT DIMPLE.SDR CA050812003Mount · cracked(CAN) ON THE RT WING IB MOST FLAP MOUNT THERE ARE SEVERAL SMALL CRACKS PROTRUDING OUT OF THE LOWER BOLT HOLE WHICH IS USED TO ATTACH THE BRACKET TO THE REAR SPAR OF THE WING.SDR CA050812004Mount · cracked(CAN) ON THE LT WING IB MOST FLAP MOUNT THERE ARE SEVERAL SMALL CRACKS AND ONE LARGE CRACK PROTRUDING OUT OF THE LOWER BOLT HOLE WHICH IS USED TO ATTACH THE BRACKET TO THE REAR SPAR OF THE WING.SDR CA050706005Control Cable · frayedRT FLAP CABLE FRAYED AT WING ROOT PULLEY. THIS CABLE WAS A GALVANIZED CABLE.SDR CA050211001Leg Assy · delaminated(CAN) AS INSTRUCTED BY INSPECTION REPORT C-12-B80-00/NF-001, AME 118, OUT OF PHASE TASKING (MAIN LANDING GEAR SPRING): COMPLIANCE BI-ANNUAL OR 700 HOURS WHICH EVER COMES FIRST. THE GEAR LEGS WERE REMOVED AND SENT FOR NDT. AT NDT THE SUBJECT GEAR LEG WAS FOUNSDR CA041104003Leaf Spring · brokenCENTER LEAF SPRING FOUND BROKEN AT ASSY ALIGNMENT DIMPLE. ALL FLEET A/C LEAF SPRINGS WHERE REPLACED APPROX JUNE 2003. THIS IS THE 4RTH A/C SPRING ASSY FAILURE IN 3 MONTHS. SUSPECT ALL FLEET AIRCRAFT LEAF SPRINGS ARE DEFECTIVE AND SPLAYING/STRAINING TO FAILURSDR CA041013004Leaf Spring · broken(CAN) MAIN LEAF SPRING BROKEN AT TOW BRIDLE CAGING BOLT. APPROX 4 INCHES AFT OF SPRING ASSY U BAR. THESE ARE RECENTLY PURCHASED NEW BATCH TYPE SPRINGS.SDR CA041013003Leaf Spring · broken(CAN) 4, MAIN LEAF SPRING, BROKEN APPROX 4 INCHES AFT OF U BAR. -5 AND -6 SPRINGS BROKEN AT AFT EDGE OF U BAR AND -6, TOP SPRING, PUSHING UP AGAINST BOTTOM OF RUDDER HORN. THESE ARE RECENTLY PURCHASED NEW BATCH TYPE LEAF SPRINGS.SDR CA041013002Leaf Spring · broken(CAN) MAIN LEAF SPRING BROKEN AT TOW BRIDLE CAGING BOLT. APPROX. 4 INCHES AFT OF SPRING ASSYU BAR. THESE ARE RECENTLY PURCHASED, NEW BATCH TYPE, LEAF SPRINGS.SDR CA040816001Control Cable · frayed(CAN) LT AND RT CABLES FRAYED AT WING ROOT PULLEYS. CABLES REPLACED WITH GALVANIZED.SDR CA040525002Control Cable · frayedSTAINLESS STEEL CABLES, LT AND RT, FLAP CONTROL AT WING ROOT PULLEYS FRAYED.SDR CA040525001Control Cable · frayedSTAINLESS STEEL CABLES, LT AND RT, FRAYED AT WING ROOT PULLEY. FLAP DOWN POSITION.SDR CA040323003Tube · broken(CAN) AS INSTRUCTED BY THE NATIONAL DEFENSE SPECIAL INSPECTION, THE VERTICAL TUBE, ON THE LT SIDE OF THE A/C JUST ABOVE THE LANDING GEAR TUBE STRUCTURE, WAS FOUND BROKEN JUST ABOVE THE WELD.SDR TZ02004F00000Hinge · crackedCONDUCTED ANNUAL INSPECTION ON AIRCRAFT. FOUND BOTH LEFT AND RT AILERON CONTROL ROD ATTACH POINTS TO CONTROL SURFACES TO BE CRACKED. SPECULATE DAMAGE MAY HAVE BEEN INDUCED BY WIND ACTION AND LACK OF USE OF CONTROL SURFACE LOCK.SDR 2004FA0000262Hinge · crackedCONDUCTED ANNUAL INSPECTION ON AIRCRAFT. FOUND BOTH LEFT AND RIGHT WING FLAP CONTROL ROD ATTACH POINTS TO CONTROL SURFACES TO BE CRACKED. SPECULATE DAMAGE MAY HAVE BEEN INDUCED BY WIND ACTION AND LACK OF USE OF CONTROL SURFACE LOCK.SDR CA031217001Control Cable · frayed(CAN) DURING THE COMPANIES STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), THE FLAP CABLE ATTACHED TO THE FLAP HANDLE WAS FOUND FRAYED AS IT STARTS TO ENTER AND TURN AROUND THE SECTOR (P/N 3-1128). THERE WAS NO INDICATION OF FRAYING UNTIL THE CABLE WAS REMOVSDR 2003FA0001241Guard · out of adjustTHE CABLE GUIDE ON THE AFT PULLEY (BEFORE ATTACHING TO THE ELEVATOR BELLCRANK) WAS INSTALLED AT AN ANGLE WHICH ALLOWED THE CABLE TO WEAR AGAINST THE GUIDE. TWO OF THE SEVEN STRANDS ON THE 7 X 19 CABLE WERE FOUND WORN THROUGH ON AN ANNUAL INSPECTION.SDR CA031203003Support · cracked(CAN) FUEL TANK SUPPORT BRACKETS FOUND CRACKED AT ENDS DIRECTLY OFF OF WELDS. 3 IB BRACKETS CRACKED IN RT WING NONE IN LT WING. NUMBER OF CRACKS VARY FROM 2 TO ALL 4 POINTS OF EACH BRACKET.SDR CA031203002Support · cracked(CAN) FUEL TANK SUPPORT BRACKETS CRACKED AT ENDS DIRECTLY OFF OF WELDS. 5 OUT OF 6 BRACKETS CRACKED IN LT WING AND ONLY 1 FOUND CRACKED IN RT WING.SDR CA031203001Tube · broken(CAN) VERTICAL FRAME TUBE JUST ABOVE AND ATTACHING TO MLG TRUSS FITTING BROKEN JUST ABOVE WELD AT MLG FITTING.CRACK TRAVELS COMPLETELY AROUND AND SECOND CRACK GOES VERTICAL 2 INCHES FROM FIRST LOWER CRACK, THEN AROUND THE TUBE AGAIN APPROX 75 PERCENT.SDR CA031201004Wire · chafed(CAN) NAV WIRE IN LT WING FOUND ATTACHED WITH MASKING TAPE TO 2ND AND 3RD COMPRESSION TUBES FROM OB, AND RT WING FOUND ATTACHED WITH MASKING TAPE TO 3RD (FROM OB) COMPRESSION TUBE. WIRES CHAFFING ON TUBE AND EXPOSED WIRE CAUSING SHORT AGAINST COMPRESSION TUBESDR CA031201003Wire · chafed(CAN) NAV WIRE IN LT WING FOUND ATTACHED WITH MASKING TAPE TO COMPRESSION TUBE. WIRE WAS CHAFING ON TUBE AND EXPOSED WIRE CAUSING SHORT AGAINST COMPRESSION TUBE, BLOWING FUSE.SDR CA031201002Wire · chafed(CAN) NAV WIRE IN LT WING FOUND ATTACHED WITH MASKING TAPE TO COMPRESSION TUBE. WIRE WAS CHAFING ON TUBE AND EXPOSED WIRE CAUSING SHORT AGAINST COMPRESSION TUBE, BLOWING FUSE.SDR CA031128005Mount · cracked(CAN) ON THE COMPANY STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), FLAP MOUNT (LEFT WING ROOT POSITION) WAS INSPECTED AND CRACKS WERE FOUND ON THE MOUNTING FACE BOTTOM BOLT HOLE.SDR CA031128003Wire · misrouted(CAN) DURING COMPANY STRUCTURAL INSPECTION AND REPAIR PROGRAM (SIRP), FABRIC WAS REMOVED FROM THE WINGS. ON INSPECTION OF THE WIRES, IT WAS DISCOVERED THAT THE POWER WIRES FOR THE NAV AND STROBE LIGHTS WERE INCORRECTLY ROUTED ALLOWING THE WIRES TO RUB ON A RISDR CA031006002Control Cable · frayed(CAN) RT FLAP CABLE FRAYED AT WING ROOT PULLEY AT FLAP FULL DOWN POSITION.SDR CA030825002Pedal · cracked(CAN) AME WAS DOING A QUICK VISUAL OF THE COCKPIT AREA BEFORE THE AIRCRAFT WAS TO LEAVE FOR THE DAYS FLIGHT, WHEN HE NOTICED A CRACKED ON THE FACE OF THE PEDAL. ON FURTHER INPECTION OF THE PEDAL IT WAS DISCOVERED THAT THE CRACK CONTINUED AROUND THE BACK ON INTSDR CA030814003Control Cable · frayed(CAN) CABLES ARE STAINLESS STEEL. LT AND RT CABLES FRAYED AT CABIN PULLEY IN NEUTRAL POSTION.SDR CA030814002Control Cable · frayed(CAN) STAINLESS STEEL CABLE, RT FLAP CABLE FRAYED AT PULLEY WHEN FLAPS SELECTED DOWN.SDR CA030815001Mount · corroded(CAN) DURING THE 100 HR INSPECTION, A SMALL RUST LINE WAS DETECTED ON THE UPPER LT MOUNT LOCATION AT THE WELD. FURTHER INSPECTION WITH 10 POWER MAGNIFYING GLASS DETERMINED THAT THE AREA WAS CRACKED 1/2 INCH.SDR CA030723001Cable · frayed(CAN) LT & RT CABLES FRAYED AT CABIN PULLEYS. CABLES ARE STAINLESS STEEL AND REPLACED WITH GALVANIZED.SDR CA030716002Control Cable · frayed(CAN) LT AND RT RUDDER CABLES FRAYED AT FUSELAGE PULLEYS WITH RUDDER NEUTRAL.
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