N172GA
Service difficulty reports · 31
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N172GA' AND registry_match = 'registration' 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 n_number = 'N172GA' AND registry_match = 'registration' 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 KGBR20200313001Tube · chafedFOUND FUEL TANK INTERCONNECT TUBES IN LEFT AND RIGHT MAIN LANDING GEAR WELLS TO BE CHAFED WHERE THE TUBES PASS THROUGH THE OUT BOARD KEEL BEAM. THE RIGHT HAND SIDE WORN TO OVER 90% OF THE WALL THICKNESS. THE LEFT HAND SIDE WAS WORN TO APPROX 75% OF THE WALL TSDR TIMA2018052230001Bolt · brokenRIGHT MAIN LANDING DRAG BRACE DISCONNECTED FROM WING ATTACH POINT. LANDING GEAR STRUT RETRACED THE AFT CONTACTING WING STRUCTURE. INVESTIGATION FOUND DRAG BRACE ATTACH BOLT BROKEN AT GREASE GALLEY.SDR TIMA20170223003Switch · failedDURING TAKEOFF ROLL BAGGAGE DOOR ANNUNCIATION ILLUMINATED. PILOT ABORTED TAKEOFF. INSPECTION REVEALED THE NOSE BAGGAGE DOOR SWITCH HAD FAILED.SDR TIMA20150915004Seat Track · corrodedDURING MX, THE RT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.SDR TIMA20150715003Seat Track · corrodedDURING MX INSPECTION, THE LT SIDE SEAT RAIL WAS FOUND TO BE CORRODED.SDR TIMA20140402018Spar Cap · corrodedINSPECTION REVEALED CORROSION DEVELOPING ON THE LT UPPER MAIN SPAR CAP UNDER THE VORTEX GENERATORS.SDR TIMA20140312017Skin · crackedSEVERAL CRACKS DEVELOPED IN THE SKIN OTBD OF THE LT NACELLE & AFT OF THE MAIN SPAR ORIGINATING FROM VARIOUS RIVETS.SDR TIMA20140312016Skin · debondedLEFT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.SDR TIMA20140312015Skin · debondedRIGHT WING DEBOND. UPPER SKIN OF BONDED PANEL IN AREA AROUND FUEL BAY ACCESS OVAL PANEL DEBONDED FROM FUEL ACCESS DISH & HONEYCOMB CORE.SDR TIMA20130617007Rib · crackedTWO CRACKS WERE DISCOVERED IN THE VERTICAL STABILIZER RIB AT CSS 69. REPAIRED IAW SRM 51-10-21.SDR TIMA20130605006Doubler · crackedA CRACK WAS DISCOVERED IN THE LT HORIZONTAL STABILIZER FWD SPAR DOUBLER. THE LT HORIZONTAL STABILIZER FORWARD SPAR DOUBLER WAS REPLACED WITH A NEW PART.SDR TIMA20130531005Spar Cap · crackedA CRACK WAS DISCOVERED IN THE LT FWD SPAR CAP OF THE VERTICAL STABILIZER ABOVE CSS 61. REPAIRED IAW FR-CO-02599, REV 1.SDR TIMA20130718004Tee Fitting · crackedDURING AN INSPECTION, A CRACK IN THE LT HORIZONTAL STABILIZER LOWER TEE EXTRUSION WAS DISCOVERED. REPAIRED THE CRACKED TEE EXTRUSION BY SPLICING IN A NEW SECTION IAW REPAIR FR-CO-02598. TWO REPAIR ANGLES WERE FABRICATED USING A SECTION OF A NEW TEE.SDR TIMA2010000010Actuator · crackedMAIN LANDING GEAR ACTUATOR ROD END CAP FOUND CRACKED DURING NDT INSPECTION TO C/W AD 2009-23-01.SDR TIMA20090002Skin · corrodedWHILE CLEANING LITE CORROSION ON SURFACE OF BELLY AFT OF WINGS, NOTICED SOME APPARENT BLISTERING OF THE SKIN. INVESTIGATION REVEALED THERE WAS CORROSION BETWEEN THE SKIN AND THE FUSELAGE FRAME. AFFECTED SKIN WAS CUT OUT AND REPLACED AS A COVER PATCH IN ACCORSDR 2006FA0000837Fire Loop · brokenPILOT EXPERIENCED A FIRE WARNING ANNUNCIATION DURING TAKEOFF ROLL. PILOT ABORTED TAKEOFF. MAINTENANCE FOUND THAT ONE FIRELOOP HAD FAILED AND CAUSED THE FALSE FIRE INDICATION. (K)SDR TIMR74Skin · crackedLEADING EDGE OF STABILIZER DISBONDED ON LOWER SIDE AND A CRACK FORMED JUST OFF THE END CAP AND COMPOSITE JOINT. (CONTROL NR 74)SDR TIM2002F00010Angle · brokenANGLE LOCATED ABOVE THE ICE DOOR HINGE. THIS ANGLE HOLDS THE LOWER FIRE SEAL BULK HEAD WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK.SDR TIM2002F00009Bolt · corrodedBOLT PN 908200115, CONNECTING NOSE GEAR DRAG BRACE TO NOSE STRUT, AND BOLT PN 908200111 CONNECTING THE TWO DRAG BRACE HALVES WAS FOUND WITH PITTING TYPE CORROSION.SDR TIM2002F00004Cable · brokenAIRSTAIR DOOR CABLE BROKE, ALLOWING ONE SIDE OF THE DOOR TO REMAIN UNLOCKED.SDR TIM2001F00011Wire · brokenTHE ICE VANE CONTROL WIRE NUMBER 20A20 BROKE AT THE TERMINAL END UNDER THE PANEL AT INST ZONE 245 CAUSING A SHORT WHICH CAUSED SMOKE IN THE COCKPIT.SDR 2001F00623Shaft · defectiveINSPECTION OF FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE RIGHT OUTBOARD FLAP CABLE DEFECTIVE. THE INNER SHAFT RETAINER WAS NOT ATTACHED TO THE FERRULE AS REQUIRED. (M)SDR TIM2001F00006B-Nut · looseOIL LINE TO THE TORQUE MANIFOLD, B-NUT CAME LOOSE, OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER MM, LOW OIL PRESSURE PROCEDURE. NO DAMAGE FOUND - OIL SERVICED AND ENGINE TEST RUN PER P/W CHECK.SDR 20010613CW015B-Nut · looseOIL LINE TO THE TORQUE MANIFOLD B-NUT CAME LOOSE. OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER PWA MM. LOW OIL PRESSURE PROCEDURE, NO DAMAGE FOUND. OIL SERVICED AND ENGINE TEST RUN, PER PWA CHECK.SDR 20010507CW013Cap · corrodedLOWER CAP LEFT STABILIZER OUTER 6 IS CORRODED.SDR 20010507CW011Trim Tab · corrodedLEFT AILERON TRIM TAB HORN CORRODED.SDR 20010509CW006Spar Cap · corrodedFOUND THE OUTBOARD 6 INCHES LOWER RIGHT REAR SPAR CAP EXTRUSION CORRODED. CORROSION WAS FOUND WHILE REPLACING A CORRODED OUTBOARD ELEVATOR HINGE BRACKET.SDR 20010509CW005Intercostal · crackedP43 INSPECTION FOUND A .8 INCH CRACK IN THE OUTDBOARD FLANGE RADIUS OF THE INTERCOSTAL AT THE UPPER CARGO DOOR FRAME AT FS 494.SDR 20010509CW004Hinge Bracket · corrodedDURING INSPECTION, THE RIGHT OUTBOARD AND THE RIGHT MIDDLE ELEVATOR HINGE BRACKET WERE FOUND TO BE CORRODED.SDR 20001103AP007Block · wornFLT 9410 - MIA/EYW - AFTER ROTATION, RIGHT PROP RPM DROPPED TO APPROXIMATELY 1200 RPM. RETURNED TO MIA. DETERMINED RIGHT BETA BLOCK TO BE WORN. REPLACED RIGHT BETA BLOCK AND RIGGED. (M)SDR 20000619AP012Nozzle · looseFLT 9209 - ON CLIMB-OUT FROM TAMPA, RIGHT T-HANDLE FIRE WARNING ILLUMINATED. PILOT SHUT DOWN ENGINE, DECLARED EMERGENCY AND RETURNED TO TAMPA. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED RIGHT ENGINE. NO EVIDENCE OF FIRE. DETERMINED TO BE HOT AIR LEAKING
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