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 07FDEA04367Skin · chafedFOUND SCRATCHES ON NOSE SKIN OF SLAT NR 2 RT WING, RIB 24-27. NOSE SKIN REPAIR PERFORMED IAW SRM 57-43-11/FIG 202/SHEET 11. REFER TO NON ROUTINE DR0399, AT RIB 27 OTHER ASNA0081A FASTENERS ARE INSTALLED ACC TO DRW A578-44242/SHEET 16, IAW AI-STATEMENT 942-03SDR 07FDEA04334Doubler · corrodedCORROSION ON KRUEGER FLAP DOUBLER AT FRAME 38, STGR 28-33 LT. REPAIR PERFORMED BY BLEND OUT CORROSION, NDT INSPECTION FOR CRACK FREE CONDITION IAW EA 6-5314-92161 AND RAS/DATLS/0002692/2005 ISSUE A.SDR SWAA074810Skin · debondedDURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 2 L/E SLAT OUTBOARD UPPER SURFACE DISBONDED. REPAIRED SLAT PER SRM.SDR 07FDEA04288Angle · crackedLEFT WING LE NR 2 SLAT, ACTUATOR LWR FAIRING SUPPORT ANGLE CRACKED ON INBD SIDE FWD FASTENER LOCATION. REMOVED CRACKED ANGLE ON L/E NR 2 SLAT ACTUATOR FAIRING SUPPORT IAW SRM 51-30-02 PG 1. LOCATED DRILLED, TREATED, PRIMED AND PAINTED IAW SRM'S 51-10-1 PG 10SDR 07FDEA04281Skin · dentedFOUND DENT ON NOSE SKIN OF RT KRUEGER FLAP (70MMX50MM, DEEPNESS 2.7MM). REPAIR PERFORMED BY DRESSING OUT THE PANEL, HFEC-ROTOTEST INSPECTION AND OVERSIZING RIVETS IN DENTED AREA IAW EA 6-5745-92141 AND RAS/AS/0160/2005 ISSUE A.SDR 07FDEA04268Skin · damagedFOUND OLD DAMAGE (DENTS AND BULGES) ON LEADING EDGE SKIN BETWEEN RIB 15-16 OF SLAT NR 2 LT. REPAIR PERFORMED BY CUT OUT SKIN AND INSTALLING EXTERNAL PATCH REPAIR IAW TD FOK/158/2005 ISSUE A, APPROVED BY EA 6-5743-92143 AND RAS/FOK/158/2005 ISSUE A.SDR MALA070125Skin · dentedTWO DENTS IN THE LT FLAP SKIN PANEL WS 192.71. REPAIRED PER EO NR S57060.SDR 07FDEA04203Skin · dentedFOUND ABRASION AT SLAT NR 1 RT TRAILING EDGE LOWER SKIN RIB 21 REPAIR PERFORMED BY INSTALLING AN EXTERNAL DOUBLER AND BONDING THE INTERNAL STRUCTURE IAW EA 6-5742-7034 AND RAS/FOK/173/2003 ISS A.SDR 07FDEA04202Beam · corrodedFOUND CORROSION AT BEAM C 38-39 KRUEGER FLAP FWD FAIRING RT REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 57-45-11.SDR 07FDEA04201Skin · dentedFOUND DENT AT SLAT NR 1 LT ON LOWER TRAILING EDGE SKIN NEAR RIB 23 REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR AND NDT FOR CRACK FREE IAW EA 6-5742-70345 AND RAS/FOK/197/2003 ISS A.SDR 07FDEA04199Skin · chafedFOUND ABRASION AT SLAT NR 1 LT ON TRAILING EDGE LOWER SKIN RIB 21. REPAIR PERFORMED BY INSTALLING A EXTERNAL DOUBLER AND BONDING THE INTERNAL STRUCTURE IAW EA 6-5742-70335 AND RAS/FOK172/2003 ISS A.SDR SWAA074721Slat · delaminatedDURING SCHEDULED C4 CHECK, FOUND RIGHT WING NR 5 L/E SLAT DELAMINATED AT T/E. REMOVED AND REPLACED SLAT PER MM.SDR 2007UALA03802Skin · damagedCRACK FOUND IN RIGHT WING LEADING EDGE SKIN PANEL OUTBOARD OF LANDING LIGHT LENS RUNNING THROUGH 4 RIVETS TO EDGE OF SKIN. 10-19-07 ACCOMPLISH EDDY CURRENT INSPECTION OF CUTOUT REPAIR AND SURROUNDING STRUCTURE OUTBOARD OF RH OUTBOARD LANDING LIGHT PER SRSDR 2007UALA03793Skin · crackedNR 1 SLAT L/E LOWER SURFACE JUST INBOARD OF SLAT ACTUATOR SKIN AND RIVET HEAD CRACKED. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED DOUBLER REPAIR TO EXTERIOR LOWER SKIN.SDR 07FDEA03972Skin · dentedDENT ON OUTER SKIN LOWER GIRDER AREA AT OUTBOARD BAY OF RT SLAT NR 3. THE DEPTH OF DENT IS 2, 4MM, SPAN WISE WIDE OF 30MM AND CHORD WISE WIDE OF 38MM. REPAIR PERFORMED BY FILLING DENT WITH FILLERALU (MAT 05-051) OR HYSOL EA9394 AS PER SRM 51-73-10 / PARA.3.CSDR 07FDEA03959Skin Panel · chafedFOUND CHAFING MARKS ON LT SLAT NR 2 ON LEADING EDGE BETWEEN SLAT TRACK 5 AND TRACK 6. REPAIR PERFORMED BY FLUSH DOUBLER SKIN INSERT IAW SRM 57-41-12/FIG 204.SDR 07FDEA03950Skin · misrepairedFLUSH REPAIR ON L/E OF NR 5 SLAT DOES NOT COMPLY WITH SRM. REMOVED AND REPLACED REPAIR ON NR 5 L/E SLAT IAW SRM 57-43-01, FIG 201. FABRICATED REPAIR FILLER, HEAT TREATED TO T6 ON MAE TRAVELER T7/696092. FABRICATED DOUBLER AND SPLICES, HEAT TREATED ON MAE SDR 2007UALA03746Structure · corrodedFLT DIVERTED DUE TO RIGHT L/E SLAT MATERIAL LIBERATION. THE RIGHT SLAT BETWEEN THE ENGINE AND THE FUSELAGE WAS DISINTEGRATING. AT THE TIME OF THE RADIO PATCH THE AIRCRAFT HAD A 12 X 8 X 2 INCH PIECE MISSING FROM THE SLAT. MAJOR REPAIR ACCOMPLISHED. THE PRISDR 2007UALA03750Skin · crackedRIGHT WING NR 6 SLAT LOWER LEADING EDGE SKIN CRACKED AT 2EA FASTENERS LOCATED AT INBOARD AUXILLARY TRACK. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED LOWER SKIN EXTERNAL DOUBLER REPAIR.SDR 07FDEA03683Skin Panel · chafedCHAFING MARKS ON RT WING LEADING EDGE D-NOSE SKIN BETWEEN TRACK 5 AND 6 AND AREA AROUND JACK 3, OUT OF SRM LIMITS. PARTIAL SKIN REPLACMENT BETWEEN TRACK 5 AND 6 AND AROUND JACK 3 IAW SRM 57-41-12/FIG 203, 204 SRM REQUIRES MATERIAL DTD5070 TO ACCOMPLISH REPAIRSDR SWAA074542Slat · crackedDURING SCHEDULED A1 CHECK, FOUND RIGHT WING NR 4 L/E SLAT CRACKED AT OUTBOARD END. REPAIRED SLAT PER SWA EA.SDR SWAA074570Slat · crackedDURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT INBOARD LOWER END. REPAIRED SLAT PER SRM.SDR SWAA074571Slat · crackedDURING SCHEDULED 22Y CHECK, FOUND RT WING NR 5 L/E SLAT CRACKED AT INBOARD LOWER END. REPAIRED SLAT PER SRM.SDR USAA920070824Attach Fitting · crackedCLT - MAJOR REPAIR - NR 6007656, CRACKED LEFT WING NR 2 KRUEGER FLAP ATTACH FITTING, LEADING EDGE STATION 106.5 - LEADING EDGE STATION 118.47. REPLACED LEFT WING NR 2 KRUEGER FLAP ATTACH FITTING, LEADING EDGE STATION 106.5 - LEADING EDGE STATION 118.47 IAW USSDR 2007UALA03653Slat · damagedDAMAGE TO RIGHT LEADING EDGE SLAT BEYOND SRM LIMITS. 10-11-07 CREW REPORTED BIRD STRIKE ON RIGHT LEADING EDGE OF AIRCRAFT. CHK'D ENGINE FOR EVIDENCE OF INGESTION. NO DISCREPANCIES NOTED. NR 8 SLAT REMOVED FOR REPLACEMENT. AFTER CHECK, AIRCRAFT OK FORSDR USAA920070825Attach Fitting · crackedCLT - MAJOR REPAIR, CRACKED WING NR 2 KRUEGER FLAP ATTACH FITTING, LEADING EDGE STATION 106.5 - LEADING EDGE STATION 118.47. REPLACED WING NR 2 KRUEGER FLAP ATTACH FITTING, LEADING EDGE STATION 106.5 - LEADING EDGE STATION 118.47 IAW USAIRWAYS EA 98873.SDR UIEA200700348Frame · crackedAFT REMOVAL OF L/E NOSE CAP FOUND THAT "D" SECTION CRACKED. CARRY OUT REPAIR AS PER SRM 57-20-03.SDR SWAA074417Skin · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LEFT WING NR 2 L/E SLAT DELAMINATED AT OUTBOARD END. REPAIRED L/E SLAT PER SRM.SDR 07FDEA03373Skin · misrepairedFOUND OLD FLUSH REPAIR ON LT SLAT NR 2 LOWER SKIN, BETWEEN TRACK 5-6 WITH POOR EDGE MARGIN. FLUSH DOUBLER REPAIR PERFORMED IAW EA 6-5743-95844 AND RAS/FOK/264/2005 ISSUE C.SDR 07FDEA03372Skin · crackedSLAT NR 5 RT : INSTALLING EXTEND CABLE ASSY FOUND NUT PLATE OF BOLT ASSY TRACK CABLE RETAINER ON TRACK SLAT, MISSING. REPAIRED SLAT SKIN IAW SRM 57-00-01 VOL I FIG 4 SHT 2.SDR 07FDEA03368Skin · damagedFOUND TWO OLD REPAIRS ON RT SLAT NR 1 IN BAD CONDITION, BETWEEN RIB 10-13, L/E AREA. ONE FLUSH DOUBLER REPAIR BETWEEN RIB 10-13 PERFORMED IAW EA 6-5740-95838 AND RAS/FOK/265/2005 ISSUE A.SDR 07FDEA03367Skin · unknownUNKNOWN REPAIR FOUND AT LT SLAT NR 2 NEAR JACKSCREW NR 3 ATTACH FITTING. REPAIR WAS RENEWED WITH DOUBLER IAW EA 6-5743-92228 AND RAS/FOK/279/2005 ISSUE A.SDR 07FDEA03360Skin · damagedON OLD REPAIR ON NOSE SKIN, INNER RIB 7-9 OF SLAT NR 2 FOUND MISDRILLED HOLE. AFTER REMOVAL OF SKIN INSERT FOUND THREE RIBS DAMAGED. FLUSH SKIN REPAIR RENEWED IAW EA 6-5740-95837 AND RAS/FOK/267/2005 ISSUE A.SDR 07FDEA03341Skin · damagedDENT WITH A CHAFING MARK WAS FOUND ON THE RT SLAT NR 1, LOWER SKIN T/E HONEYCOMB TAIL, NEAR RIB 21-23. REPAIR PERFORMED BY SKIN INSERT AND REPAIR PATCH IAW TD FOK/273/2005 ISS B, APPROVED BY EA 6-5742-95845 AND RAS/FOK/237/2005 ISS. B.SDR 07FDEA03337Rib · damagedLT SLAT 1 TRAILING EDGE LOWER SKIN DAMAGE AT INNERRIB 23, AREA AT T/E PROFILE. REPAIR IS PERFORMED WITH SKIN INSERT AND REPAIR PATCH IAW TD FOK/262/2005 ISSUE B.SDR 07FDEA03325Skin · misrepairedOLD FLUSH DOUBLER REPAIR FOUND ON SLAT NR 2 RT THAT REQUIRES REWORKING. REPAIR RENEWED IAW TD FOK/065/2006 ISSUE C, APPROVED BY EA 6-5740-99182A AND RAS/FOK/065/2006 ISSUE A.SDR 2007UALA03534Wedge · delaminatedRIGHT WING, 10 SLAT T/E WEDGE IS DELAM ALONG TRAILING EDGE FOR APPROX 20 INCHES.SDR 2007UALA03476Skin · dentedSLAT NR 4 & 5 ARE DAMAGED ON LEADING EDGE. REMOVED NR 4 SLAT AND INSTALLED REPAIRED UNIT. REWORKED DENT ON NR 5 LE SLAT AND FIXED LE WING DAMAGE REPAIRED AND INSPECTED FOR CRACKS. ALL ITEMS RETURNED TO SERVICE.SDR 2007UALA03468Skin · delaminatedNR 9 SLAT OUTBOARD EDGE DELAM ON UPPER AND LOWER SURFACE.SDR 07FDEA03221Skin · dentedOLD FLUSH DOUBLER REPAIR ON SLAT NR 3 LT, UPPER SKIN, BETWEEN RIB 44-46. BLIND RIVETS WITHOUT PIN, RIB 46 IS MISDRILLED AND RIVETS FORM IS NOT ADHERED. REWORK PER TD FOK/233/2005 ISSUE: C, APPROVED BY EA 6-5744-99139A AND RAS/FOK/2332005 ISSUE: A.SDR 07FDEA03210Skin · chafedABRASION FOUND NOSE SKIN OF RT SLAT NR 2 RIB 21-22. REPAIR PERFORMED BY BLEND OUT AND NDT INSPECTION FOR CRACK FREE IAW EA 6-5743-112508 AND RAS/FOK/189/2007 ISS "A".SDR USAA070686Wedge · debondedNR 3 SLAT UPPER OUTBOARD WEDGE DISBONDED. INSTALLED REPAIR PARTS PER SRM 51-70-17, 51-70-10, DEFECT SIZE: 1.5 X 2 INCHES.SDR USAA070685Skin · damagedNR 4 SLAT T/E WEDGE HAS ERODED SKIN & DISBOND ON LOWER SURFACE I/B SIDE OF SLAT. REMOVED DISBONDED AREA, INSTALLED REPAIR PARTS PER TR 57-42-03, SRM 51-70-10, DEFECT SIZE: 2 X 3 INCHES.SDR USAA070683Skin · gougedNR 2 SLAT O/B END UPPER SURFACE, SLAT WEDGE SKIN, GROOVE/GOUGE. INSTALLED NEW CORE FILLER & NEW UPPER SURFACE BONDED DOUBLER PER SRM 57-43-01, 51-70-10, DEFECT SIZE: 1.25 X .250 INCH.SDR USAA070679Skin · crackedNR 6 SLAT, LOWER T/E AT OUTBOARD END, CRACKED AT RIVET HOLES. INSTALLED FILLER/DOUBLER REPAIR PER SRM 57-43-01, DEFECT SIZE: .125 INCH.SDR UIEA200700325Skin · delaminatedON WALKAROUND AFTER FLIGHT OF GT5421, FOUND NR 11 L/E DEVISE DELAMINATED AT AFT I/B CORNER. PERFORMED INTERIM REPAIR PER XEO57-082707. REPETITIVE INSPECTIONS FOR CONDITION AND SECURITY TO BE ACCOMPLISHED EVERY OTHER FLIGHT CYCLE UNTIL PERMANENT REPAIR OR PARSDR 07FDEA03154Skin · dentedLEFT WING, NR 5 SLAT LEADING EDGE AREA FOUND WITH DENT. REPAIR CARRIED OUT AS PER SRM 57-10-00 FIG. 5 VOL.I. REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.SDR 07FDEA03135Fitting · crackedLEFT WING, OUTBOARD FLAP LEADING EDGE STOP BOLT FITTING FOUND CRACKED. 09-12-07 REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II. REPAIR CLASSIFIED AS MAJOR REPAIR AS PER FEDEX GMM 6-2-100.SDR TAMF20070031SSkin · wrinkledDURING (C) CHECKS INSPECTION WAS FOUND AN EXISTING REPAIR WRINKLED ON LEADING EDGE SLAT NR 2 UPPER SKIN. DAMAGED AREA WAS REPAIRED IAW EWO 767-57-029 AND MFG SERVICE REQUEST 1-527377149. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FORM 8100-9 WAS ISSUED APPROVINGSDR 07FDEA03130Slat Track · crackedLEFT WING, FIXED LEADING EDGE NR 10 SLAT TRACK CUTOUT INBOARD CORNER FOUND CRACKED. 09-11-07 REPAIR CARRIED OUT AT LEFT HAND WING : FIXED LEADING EDGE NR 10 SLAT TRACK CUTOUT INBOARD CORNER AREA AS PER SRM 57-10-00 FIG. 21 VOL I. CLASSIFIED AS MAJOR REP
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