JASC 5754
Service difficulty reports · 17,344
Reports filed under 5754 · Leading Edge Devices, 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 jasc_code = '5754' 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 jasc_code = '5754' 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 2002UALA01180Filler · missingFILLER WAS MISSING FROM THE SPANWISE BULB SEAL ON SLAT NR 14 AND 15 INCHES OF THE OUTBOARD END OF THE FILLER WAS MISSING FROM THE NR 1 SEAL. MAJOR REPAIR ACCOMPLISHED. FILLER INSTALLED.SDR 2002UALA01064Skin · crackedNR 1 SLAT LOWER SKIN CRACKED AT FASTENER BETWEEN ACTUATOR AND ANTI-ICE TUBE, ALSO CRACKED BELOW INBOARD AUXILIARY TRACK. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.SDR DL72S020691Spar · crackedFOUND ON B2 LETTER CK 1 IN CRACK NR 7 SLAT SPAR AT TAI DUCT CUTOUT UPPER INBD CORNER. REPAIRED PER MM 57-54-000-8 AND ERA.SDR SWAA021374Slat · crackedDURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT CRACKED ON LOWER SKIN. REMOVED AND REPLACED NR 6 L/E SLAT PER MM.SDR CALA0200351Skin · crackedINSPECTION FOUND #6 SLAT SKIN CRACKED. REPAIRED IAW SRM 57-43-01.SDR AUS20020872Roller · worn(AUS) LEADING EDGE SLAT ROLLERS WORN.SDR UPS02238614Slat · crackedINSPECTION TYPE:AS NR 5 SLAT CRACKED OUTBOARD OF FENCE JUST OUTBOARD OF UPSTOP. REMOVED AND REPLACED NR 5 SLAT PER MM 27-81-11, RIG AND OPS CHECK GOOD.SDR USAA020215Skin · crackedPIT - FOUND SKIN CRACKED 4 INCH BY 8 INCH, UNDERSIDE OF NR 2 SLAT 24 INCHES FROM OUTBOARD END. INSTALLED 4 INCH BY 8 INCH DOUBLER PER SRM 57-43-01 FIG 206. (M)SDR MWEA020390Fitting · worn#5 SLAT INBOARD SADDLE FITTING BUSHINGS WORN. -- REMOVED AND REPLACED RIB.SDR GTIA020583Slat · crackedDTW - FOUND RIGHT WING LEADING EDGE THE NR ZERO SLAT TRACK THE SLAT IS CRACKED ON THE INBOARD SIDE. REPAIRED IAW MD80. (M)SDR 0201919951Door · damagedDURING APPROACH FOR LANDING WHEN SLATS EXTENDED, THE AIRCRAFT ROLLED TO THE LEFT. THE SLAT DISAGREEMENT LIGHT WAS ON AND THE SLATS RETRACTED LIGHT WAS OUT. CREW CYCLED THE SLAT EXTENSION PROCEDURES AND THE SLATS AGREED AND NO TENDENCY TO ROLL. ALL INDICATIOSDR 2002UALA00932Slat · crackedLT WING NR 1 SLAT HAS CRACKS IN AFT ROW OF RIVETS, NR 29 THROUGH NR 33 FROM INBOARD SIDE FROM BLACK STRIP. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED HFEC INSPECTION ON CUTOUT AFTER DAMAGE REMOVAL. DOUBLER REPAIR ACCOMPLISHED.SDR A6WA200260016Panel · crackedCRACK IN UPPER LANDING ANGLE OF LEFT FLAP LEADING EDGE ACCESS PANEL BETWEEN STATION WRX 311.4 AND WRX 323.0. FABRICATED A REPAIR STRIP. REPAIRED IAW MFG.SDR 2002UALA00915Slat · crackedLEFT HAND WING NR 2 SLAT HAS CRACK IN AFT ROW OF RIVETS. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.SDR 2002UALA00914Skin · crackedNR 4 LEADING EDGE SLAT LOWER SURFACE 6-8 INCHES OUTBOARD OF SLAT ACTUATOR SKIN IS CRACKED AT TWO FASTENERS. MAJOR REPAIR ACCOMPLISHED REINFORCEMENT DOUBLER.SDR AUS20021034Hinge · corroded(AUS) LEADING EDGE FLAP LH HINGE FITTING CONTAINED SEVERE EXFOLIATION CORROSION AROUND BUSH. FOUND DURING CPCP INSPECTION.SDR C1HA200292016Skin · delaminatedRT WING FORE FLAP INBRD LOWER SKIN HAS AREA OF DELAMINATION JUST AFT OF CENTER ATTACH ARM. (AREA 12 INCHES X 6 INCHES)SDR C1HA200292017Skin · debondedLT INBRD TRAILING EDGE AFT FLAP LOWER SURFACE AT INBRD END HAS REPAIR DISBONDINGSDR SWAA021087Slat · crackedDURING SCHEDULED C4 CHECK, FOUND NR 1 L/E SLAT CRACKED UNDER PREVIOUS REPAIR. REMOVED AND REPLACED NR 1 L/E SLAT PER MM.SDR 2002F00613Skin · dentedAT C-CHECK, FOUND DENT IN OUTER SKIN OF NR 4 SLAT, LEFT WING STATION 410. (M)SDR IXXA0200061SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACKED WAS DETECTED ON THE RIGHT WING OUTBOARD LEADING EDGE PANEL AT THE INBOARD AREA AT STATION XRS 634. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A FILLER AND REPAIR DOUBLER IN ACCSDR IXXA0200060SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE RIGHT WING LEADING EDGE AT WING STATION XES710, UPPER CHORD MOUNTS. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBSDR IXXA0200059SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, CORROSION AND A CRACK WAS DETECTED ON THE LEFT WING OUTBOARD LOWER LEADING EDGE AT STATION XFS 566. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR FILLER AND EXTERNAL DOUBLER IN ACCOSDR IXXA0200058SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LT WING OUTBOARD UPPER LEADING EDGE AT STATION XFS 705. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF A REPAIR DOUBLER AND FILLER IN ACCORDANCE WITH THE DOUGLAS SSDR IXXA0200057SStructure · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RT WING OUTBOARD LEADING EDGE AT STATION XFS 705. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER AND INTERNAL FILLER IN ACCORDANCE WITH SDR 2002F00657Flap · corrodedAT C-CHECK, FOUND RIGHT WING NUMBER FOUR LEADING EDGE FLAP CORRODED ON INBOARD UPPER CORNER. (M)SDR TSAA0251130Slat · corrodedFOUND CORROSION ON THE RIGHT WING AFT OF THE NR 5 SLAT FITTING. BLENDED OUT CORROSION. FABRICATED AND INSTALLED PARTS. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.SDR USAA020175Skin · crackedPIT - FOUND SKIN CRACKED IN 13 SMALL CONTINUOUS PLACES, RIGHT WING, NR 6 SLAT, LOWER SURFACE SLAT STATION 299.10-314. REMOVED DAMAGED SKIN PER SRM 57-43-01. (M)SDR SWAA020947Slat · delaminatedDURING SCHEDULED 1/4D CHECK, FOUND NR 4 L/E SLAT DELAMINATED AT UPPER INBD CORNER. REPAIRED L/E SLAT PER SRM.SDR 2002F00625Skin · dentedAT C-CHECK, FOUND NR 3 SLAT OUTER SKIN DENTED AT WING STATION 570L. (M)SDR DHL2002726520Skin · dentedDURING C-CHECK, NR 5 LEADING EDGE SLAT HAS A DENT AT SLAT AT STA 355. CUT OUT DENTED SECTION OF SLAT SKIN IAW B-727 SRM 57-50-1 FIG 1, FABRICATED REPAIR PARTS IAW B-727 SRM 57-50-3 FIG 1, AND INSTALLED DOUBLER AND FILLER REPAIR ON NR 5 LEADING EDGE SLAT IAW BSDR 2002F00677Skin · dentedAT C-CHECK, FOUND NR 5 SLAT OUTER SKIN UPPER SURFACE DENTED AT STATION 380R. (M)SDR UPS02438334Rib · crackedINSPECTION TYPE:C DURING LHW NR 9 L/E FLAP GREASE LUBE AS NR 3 ROTARY ACTUATOR (COUNT FROM O/B) REMOVED, L/E RIB O/B FWD AREA FOUND CORROSION AT ILES 800. L/E RIB AT ILES 800 IS REPLACED AS PER SRM 51-10-01. CORROSION FOUND CRACKED THROUGH AT 2 LOCATIONS.SDR 2002F00528Former · crackedAT C-CHECK, FOUND CRACK ON RIGHT WING NR 5 KRUEGER FLAP, OUTBOARD INNER FORMER. (M)SDR UPS02238094Skin · crackedINSPECTION TYPE:C NR 3 KRUEGER FLAP ANTI ICE SKIN CRACKED 14 INCHES FROM I/B END. INSPECTED IAW NDTM PT 6 51-00-00 FIG 4, REPAIR CARRIED OUT IAW UPS EO B727-5750-3082-D.SDR SWAA020843Slat · crackedDURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT CRACKED (2 EA), 12 INCHES OTBD OF OTBD ACTUATOR STOP. REPAIRED L/E SLAT PER SRM.SDR 02FDEA00274Structure · corrodedNR 5 K-FLAP OUTBOARD LWR BONDING JUMPER UPPER ATTACH POINT IS CORRODED. REMOVED AND REPLACED FLAP PER DWG SR 27-97-010.SDR DL72S020459Rib · crackedL/E NOSE RIB ON NR 5 SLAT I/B SIDE OF ACTUATOR ROD END IS CRACKED. REPAIRED PER M/M 57-54-000-8 AND ERA 382989-14.SDR SWAA020812Slat · delaminatedDURING SCHEDULED C4 CHECK, FOUND NR 4 L/E SLAT T/E WEDGE DELAMINATED ON INBD EDGE. REMOVED AND REPLACED NR 4 L/E SLAT PER MM.SDR DL72S020426Angle · crackedA .375 INCH CRACK AT LWR SLAT COVE SKIN ATTACH ANGLE BELOW NR 6 SLAT TAI DUCT. REPAIRED PER M/M 57-54-000-8.SDR ASAA0210080Slat · delaminatedANC - DURING SCHEDULED A-CHECK, FOUND NR 2 LEADING EDGE SLAT DELAMINATING AT WING BODY LINE 329.75. REPAIRED PER EA. (M)SDR UPS02238047Flap · crackedINSPECTION TYPE:C NR 5 L/E FLAP HAS CRACK AT I/B LOWER BONDING WIRE ATTACH POINT (BULLNOSE). REPAIR CARRIED OUT IAW SMRO EO 2002-015-002 UPS ENGINEERING FILE 727-57-20052.SDR F3LA200200121Skin · crackedMAINTENANCE REPORTED SKIN CRACKED AT OUTBOARD END OF NR 6 SLAT. REMOVED DAMAGED AREA AND INSTALLED REPAIR PER SRM 57-43-01 FIG 206 AND SRM 51-40-02.SDR CALA0200162Fastener · crackedINSPECTION FOUND NR 1 LEADING EDGE SLAT FASTENERS CRACKED ON LOWER SKIN. INSTALLED REPAIR IAW SRM 57-43-01.SDR ASAA0280107Rib · gougedPAE - DURING 30K-CHECK, FOUND LEFT WING NR 1 SLAT INBOARD RIB GOUGED IN INTERCONNECTING PIN BORE. REPLACED INBOARD RIB PER SRM 51-30-2. (M)SDR C1HA200288005Slat Track · crackedCUTOUT FOR NR 4 SLAT OUTBOARD TRACK IS CRACKED IN FIXED LEADING EDGE. STOP, DRILLED CRACK, REPAIRED.SDR UPS02237937Skin · crackedINSPECTION TYPE:C NR 4 L/E FLAP ANTI-ICE SKIN ON PANEL O/B OF ACTUATOR ATTACH POINT CRACKED ON LWR O/B RIVET. REPAIR CARRIED OUT AS REQUIRED IAW UPS EO B727-5750-3082.SDR 2002F00398Hinge · wornDURING CURRENT D-CHECK AT SIAEC, FOUND L/W NR 11, 12 AND 13 L/E KRUGER FLAP HINGE FITTING ASSEMBLIES WITHWORN AND ELONGATED BORE HOLES. REAMED HOLES. PERFORMED DYE CHECK TO ENSURE CORROSION AND CRACK FREE CONDITION. NO DEFECTS FOUND. FABRICATED AND INSTALLESDR RIVA020308ASkin · brokenMQY - FOUND LEFT WING INBOARD FLAP INBOARD END OF FORE FLAP UPPER SURFACE SKIN IS WORN AND HAS PIECES BROKEN OFF WS 220. REMOVED DAMAGED SECTION. FABRICATED FILLER DOUBLER AND INSTALLED PER EO NR 01-298 WITH APPROVED 8110-3. APPRECIABLE WEIGHT ADDED BY THISSDR DL76S020257Beam · crackedNR 5 LEADING EDGE SLAT NOSE BEAM WAS FOUND DAMAGED AT STA 439. REPAIR PER ER/A 402159-14.
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