N687AL, cancelled Sep 25, 2020
Service difficulty reports · 45
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 = 'N687AL' AND deregistration_id = 'N687AL-2020-09-25' 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 = 'N687AL' AND deregistration_id = 'N687AL-2020-09-25' 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 ALGA2012071801Shaft · damagedUPON COMPLIANCE WITH A 3000 HR INSPECTION, FOUND SHAFT DAMAGED BEYOND REPAIR.SDR ALGA2012061412Step · corrodedFLOAT STEP, CORROSION BEYOND REPAIRABLE LIMITS.SDR ALGA2012061411Step · corrodedFLOAT STEP, CORROSION BEYOND REPAIRABLE LIMITS.SDR ALGA2012061201Rotor · damagedONE TRUNNION, PN 407-312-100-101, SN LKFS3425, HAS ELASTOMERIC EXTRUSION, FOUR WORN BEARINGS, PN 406-312-100-101 AND TWO PITCH HORNS PN 406-012-108-107, PITTING. CORROSION BEYOND LIMITS.SDR ALGA2012052214Panel · corrodedPANEL CORRODED BEYOND LIMITS.SDR ALGA2012052213Channel · corrodedCHANNEL CORRODED BEYOND LIMITS.SDR ALGA2012052212Frame · crackedFRAME CRACKED BEYOND REPAIRABLE LIMITS.SDR ALGA2012052211Skin · corrodedSKIN CORRODED BEYOND LIMITS.SDR ALGA2012052210Shelf · corrodedSHELF CORRODED BEYOND LIMITS.SDR ALGA2012052209Support · corrodedSUPPORT CORRODED BEYOND LIMITS.SDR ALGA2012052208Angle · corrodedANGLE CORRODED BEYOND LIMITS.SDR ALGA2012052207Skin · corrodedSKIN CORRODED BEYOND LIMITS.SDR ALGA2012052206Angle · corrodedANGLE CORRODED BEYOND LIMITS.SDR ALGA2012052205Angle · corrodedANGLE CORRODED BEYOND LIMITS.SDR ALGA2012012500022Skin · corrodedCORROSION FOUND ON BELLY SKIN DURING CORROSION INSPECTION. AREA FOUND TO BE OUT OF LIMITS.SDR ALGAR919115682Crosstube · corrodedCROSS TUBE CORRDED BEYOND LIMITS IAW AA00061 PAGE 19, FIG 2, TABLE 8.SDR ALGA070711687ALMount · corrodedTRANSMISSION DECK, TRANSMISSION PYLON MOUNT POINT CORRISION, RT FWDSDR ALGA070611687ALMount · corrodedTRANSMISSION DECK. TRANSMISSION PYLON MOUNT POINT CORRODED.SDR ALGA100000Pitch Link · wornBINDING; AXIAL PLAY BEYOND LIMITS; ROUGH / REPLACED WITH NEW PART BY FIELD MAINT.SDR ALGA099285Bearing · roughROUGH, BINDING AND AXIAL PLAY, REPLACED W/NEW.SDR ALGA099284Bearing · roughROUGH, BINDING AND AXIAL PLAY, REPLACED W/NEW.SDR ALGA099280Bearing · roughROUGH, BINDING AND AXIAL PLAY, REPLACED W/NEW.SDR ALGA099278Bearing · roughROUGH, BINDING AND AXIAL PLAY, REPLACED W/NEW.SDR ALGA087760Bearing · failedTAIL ROTOR TRANSMISSION REMOVED FOR METAL IN OIL, FOUND BEARING BREAKING DOWN. SUBMITTED BY: PRESTON BARZARESDR ALG2003F00066Hmu · leakingDURING REFUELING. AFTER A/C WAS REFUELED OFFSHORE AT WC-560. THE MECHANIC NOTICED A STEADY FLOW OF FUEL FROM THE OVERFLOW DRAIN LINE. HE INSPECTED THE LEAK AND FOUND THE HMU LEAKING. HE REMOVED AND REPLACED THE HMU AND COMPLIED WITH A LEAK CHECK AND AIRCRASDR ALGA079856Shaft · looseFOUND T/M GEAR, BEARING JOURNAL SHAFT AND SUPPORT LOOSE IN COVER ASSEMBLY. FOUND ALL 4 STUDS ON JOURNAL SUPPORT PULLED OUT AND 1 EACH WITH NO THREADS LEFT IN WORN BORE. THIS ALLOWED GEAR TO WEAR IN AN UNUSUAL MANNER, WHICH COULD HAVE RESULTED IN A CATASTROPHSDR ALGA079855Gearshaft · galledDUE TO T/M JOURNAL SUPPORT STUDS BACKING OUT OF COVER AN UNUSUAL WEAR PATTERN OF SPALLING AND GALLING OCCURRED ON GEAR TEETH.SDR ALG2002F00044Cover · wornENGINE HAD CHIP LIGHTS. UPON DISASSEMBLY OF GEARBOX FOUND T/M JOURNAL SUPPORT STUDS BACKED OUT OF COVER. FOUND T/M GEAR, BEARING JOURNAL SHAFT AND SUPPORT LOOSE IN COVER ASSEMBLY. FOUND ALL 4 STUDS ON JOURNAL SUPPORT PULLED OUT AND 1 EACH WITH NO THREADS LESDR ALG2002F00043Gear · galledENGINE WAS REMOVED DUE TO CHIP LIGHTS. UPON VISUAL INSPECTION FOUND CAUSE OF METAL DUE TO GALLING T/M AND PTO GEARS. DUE TO T/M JOURNAL SUPPORT STUDS BACKING OUT OF COVER AN UNUSUAL WEAR PATTERN OF SPALLING AND GALLING OCCURRED ON GEAR TEETH. THIS COULD HAVSDR ALG2002F00033Shaft · wornDURING REPAIR FOR LEAKING OUTPUT SEAL, FOUND SPLINES ON OUTPUT SHAFT WORN BELOW LIMITS, READING 1.3025, MIN 1.3035 (SHAFT SPLINES SOFTER METAL THAN TRUNNION SPLINES.)SDR ALG2002F00002Pitch Horn · corrodedAFTER DISASSEMBLY, CLEANING AND STRIPPING PAINT FOR OVERHAUL. CORROSION ON ENTIRE SURFACE BEYOND LIMITS DUE TO POOR METAL QUALITY AND POOR PRIME AND PAINT. BETTER QUALITY ALUMINUM AND PAINTING PROCEDURES RECOMMENDED.SDR 2001F00578Blade · missingTURBINE RECEIVED FROM FIELD FOR HOWLING NOISE. REMOVED COMBUSTION SECTION AND FOUND SULFADATION ON 1ST STAGE WHEEL. WHEEL HAS MISSING AND BROKEN BLADES DUE TO SULPHADATION. (M)SDR 2001F00574Turbine Wheel · corrodedTURBINE RECEIVED FROM FIELD FOR HOWLING NOISE. REMOVED COMBUSTION SECTION AND FOUND SULFADATION ON 1ST STAGE WHEEL. THIS TURBINE HAD A ROLLS ROYCE COMBUSTION LINER. WHEEL HAS MISSING AND BROKEN BLADES DUE TO SULFADATION. (M)SDR 20001206SH008Drive Shaft · failedIN-FLIGHT, PILOT HEARD A LOUD POP. LANDED AT THE NEAREST PLATFORM AND AFTER SHUT DOWN, FOUND FORWARD FLEXURE ON INPUT DRIVESHAFT HAD FAILED. ONE OF THE FORWARD FLEXURES FAILED AT THE BOLT HOLE AND A PORTION OF THE FLEXURE WENT THROUGH THE TRANSMISSION DECK/CSDR 20000912SH012Disc Pack · crackedDURING 25-HOUR AD INSPECTION, FOUND AFT SEGMENT CRACKED ACROSS THE SPAN. (X)SDR 20000912SH011Disc Pack · crackedDURING 25-HOUR AD INSPECTION, FOUND AFT SEGMENT CRACKED IN 3 PLACES ACROSS THE SPAN. (X)SDR 20000807SH019Bearing · crackedDURING REPAIR/REPLACEMENT OF CRACKED HOUSING, BEARINGS ROUGH. (X)SDR 20000807SH018Bearing · crackedDURING REPAIR/REPLACEMENT OF CRACKED HOUSING, BEARINGS ROUGH. (X)SDR 20001026SH001Gear · brokenCHIP LIGHT WAS DETECTED ON AIRCRAFT. CHIP DETECTORS WERE PULLED AND INSPECTED. LARGE PIECE OF GEAR TOOTH WAS FOUND ON PLUG. LARGE PIECE OF GEAR TOOTH BROKE OFF DURING FLIGHT. CAUSE FOR BROKEN GEAR TOOTH WAS DUE TO EXCESSIVE GALLING EXTENDING UP TO FORWARD SDR 20000518SH006Bearing · leakingDURING RECURRING 25-HOUR INSPECTION AND BEARING LUBRICATION (PER ASB 407-00-35/AD 2000-02-12), ACCUMULATED GREASE EXPELLED FROM AROUND THE SEAL IS BLACK DETERMINING BEARING IS DAMAGED. (X)SDR 20000518SH005Bearing · leakingDURING RECURRING 25-HOUR INSPECTION AND BEARING LUBRICATION (PER ASB 407-00-35/AD 2000-02-12), DURING LUBRICATION, ACCUMULATED GREASE EXPELLED FROM AROUND THE SEAL IS BLACK DETERMINING BEARING IS DAMAGED. (X)SDR 20000518SH004Bearing · damagedDURING RECURRING 25-HOUR INSPECTION AND BEARING LUBRICATION (PER ASB 407-00-35/AD 2000-02-01), DURING LUBRICATION, ACCUMULATED GREASE EXPELLED FROM AROUND THE SEAL IS BLACK DETERMINING BEARING IS DAMAGED. (X)SDR 20000518SH003Bearing · damagedDURING RECURRING 25-HOUR INSPECTION AND BEARING LUBRICATION (PER ASB 407-00-35/AD 2000-02-12), ACCUMULATED GREASE EXPELLED FROM AROUND THE SEAL IS BLACK DETERMINING BEARING IS DAMAGED. (X)SDR 20000719SH004Bearing · damagedRECURRING 25-HOUR INSPECTION AND BEARING LUBRICATION (PER ASB 407-00-35 AND AD 2000-02-01), FOUND ACCUMULATED GREASE EXPELLED FROM AROUND THE SEAL IS BLACK DETERMINING BEARING IS DAMAGED. (X)SDR 2000ZZZX6Housing · crackedDURING DAILY INSPECTION, FOUND CRACKED BLOWER HOUSING.
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