JASC 5754
Service difficulty reports · 17,348
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 97UAL900265Slat · crackedDURING L-CHECK, 8 BY 12 INCH PIECE OF THE LT NR 1 SLAT WAS FOUND MISSING. THE MISSING SECTION WAS LOCATED ON THE UNDERSIDE OF THE SLAT ALONG THE TRAILING EDGE WEDGE, EXTENDING FROM THE INBOARD EDGE APPROX 12 INCHES. CAUSE OF DAMAGE UNKNOWN. REPAIRED PER SRMSDR UPS97222481Rib · crackedINSPECTION TYPE:SI, RIB CHORD ON NR 2 SLAT, AT SLAT STATION 313.136. REMOVED DAMAGED PORTION OF RIB, PROCURED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW SRM 51-30-2, 57-50-3.SDR CALA9700601Bracket · crackedLEFT WING KRUEGER FLAP ACTUATOR ATTACH BRACKET LOWER OUTBOARD CORNER HAS CRACK .75 INCH. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED REPLACEMENT IN ACCORDANCE WITH SRM 51-20-1 AND 51-30-2.SDR CALA9700509Angle · crackedINSPECTION FOUND A 2 INCH CRACK AT AFT END OF LT WING LEADING EDGE SLAT STA 0 RIB UPPER ATTACH ANGLE. THE ANGLE WAS REMOVED AND A REPLACEMENT ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR TWAA9804704Skin · disbondedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DISBONDING ON UPPER SKIN OF NR 4 LE SLAT. INSTALLED TWO EACH FIELD REPAIR PATCHES PER SRM 51-70-10. (M)SDR TWAA9804703Skin · disbondingMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DISBONDING ON TOP SKIN OF NR 2 LE SLAT. INSTALLED TWO REPAIR DOUBLERS PER SRM 51-70-10. (M)SDR MZZA97087Slat · dentedLEFT WING SLAT NR 4 DENT AT 2 POINTS APPROXIMATELY 2 INCHES BY 4 INCHES AND 2 INCHES BY 2 INCHES. TOP LEADING EDGE DEPTH ABOUT .25 INCH. REPAIRED DENTS ON NR 4 SLAT IAW SRM 57-50-3. (X)SDR MZZA97086Slat · dentedLEFT WING NR 1 SLAT DENTED APPROXIMATELY 2 INCHES BY 6 INCHES, DEPTH APPROXIMATELY .1875 INCH, TOP SURFACE. REPAIRED DENTS IN NR 1 SLAT IAW SRM 51-50-2. (X)SDR DL757970635Skin · delaminatedTHE LEADING EDGE OF THE TRAILING EDGE WEDGE ON THE NR 7 SLAT WAS FOUND DELAMINATED. THE DAMAGE WAS 24 INCHES LONG. THE SLAT WAS REPAIRED PER THE B757 SRM 51-70-10, FIGURE 11.SDR DL72W980605Rib · crackedFOUND ON B2 LETTER CK, .25 INCH CRACK BEYOND PREVIOUS STOP DRILLED CRACK, OUTBD NOSE RIB AT NR 5 SLAT ACTUATOR ROD END. REPAIRED PER MM 57-54-0.SDR DL72S970487Angle · crackedFOUND ON F2 LETTER CHECK, NR 8 SLAT CRACKED AT THE LOWER COVE SKIN ATTACH ANGLE AT THE OUTBOARD STOP. REPAIRED PER MM 57-54-0.SDR P5CA9700430Skin · damagedGOUGE IN L/E OF LT SIDE OUTBOARD FOREFLAP. REPAIRED PER BOEING SRM 51-40-09.SDR DL76S970698Skin · delaminatedTHE NR 8 SLAT WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED. THE DELAMINATION IS A 3 INCH DIA CIRCLE, APPROX 4 FROM THE AFT EDGE OF THE TRAILING EDGE WEDGE. THE WEDGE IS MANUFACTURED WITH 0.016 5052-H38 FACE SHEETS WITH A METALLIC HONEYCOMB CORE PER BMS 4-6, SDR DL757970471Wedge · delaminatedDELAMINATION WAS FOUND ON THE TRAILING EDGE WEDGE OF THE NR 2 SLAT. THE DAMAGE MEASURED 8 INCHES FORWARD-AFT, 5 INCHES INBD/OTBD, AND IS LOCATED 3 INCHES FROM THE OUTBOARD EDGE OF THE SLAT. THE DAMAGE WAS REPAIRED PER B757 SRM 51-70-10.SDR EISA970505Flange · crackedNR 1 KRUEGER FLAP OUTBOARD OF UPPER MIDDLE FLANGE ATTACHMENT CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-2. (M)SDR DL76S970470Slat · delaminatedTHE OUTBOARD END OF THE TRAILING EDGE OF THE NR 3 SLAT WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED. THE DELAMINATION IS 6 INCHES BY 8 INCHES. THE DAMAGE WAS REPAIRED PER B767-300 SRM 57-43-02, FIGURE 201.SDR ABXA9700075Fitting · crackedRIGHT WING INBOARD SLAT TRACK FITTING AT NR 2 TRACK CRACKED. REPLACED NR 2 SLAT TRACK FITTING, IAW DC9 SRM 51-30-01.SDR 97FDEA00148Bonding Strap · corrodedNR 0259 005. CORROSION (C57-562-01-2) NR 6 K-FLAP TO BULLNOSE JUMPER ATTACH POINT IS CORRODED AT UPPER ATTACH POINT. REMOVED CORROSION ON NR 6 K-FLAP BULL NOSE UPPER BONDING JUMPER ATTACH POINT IAW FED-EX E.A. NR 7-5740-32908.SDR 97FDEA00147Flap · corrodedCORROSION (C57-562-01-2) NR 4 K-FLAP TO BULLNOSE BONDING JUMPER ATTACH POINT IS CORRODED AT UPPER ATTACH POINT. REPAIRED NR 4 K-FLAP TO BULL NOSE BONDING JUMPER ATTACHED POINT IAW FED-EX SR DRAWING 27-57-010C AND SRM 57-50-3.SDR 97FDEA00143Flap · corrodedNR 260 001 CORROSION (C57-562-01-2) UNDERNEATH NR 6 K-FLAP DATA PLATE. REMOVED CORROSION AND REPAIRED K-FLAP IAW FED-EX SRM 57-30-3.SDR DHL9771261DRib · crackedAT D-CHECK, CRACK ON I/B AND O/B RIBS AT NR 3 SLAT O/B TRACK. STOP DRILLED CRACKS, ACCOMPLISH HFEC, INSTALLED RIB REPAIR DOUBLER 4 BY 3 ON O/B SIDE. INSTALLED RIB REPAIR DOUBLER ON I/B SIDE, 4 BY 3, PER SRM 57-50-3.SDR AU970325Fairing · failed(AUS) NO7 LEADING EDGE FLAP BULLNOSE FAIRING OPERATING RODS AND HINGES BROKEN AWAY - FLAP HANGING BY BONDING STRAPSSDR DHL9771262DCasting · corrodedAT D-CHECK, NR 3 SLAT OUTBOARD TRACK BOTH RIB CASTINGS ARE CORRODED. REMOVED RIBS AND CASTING PER SRM 51-10-6 . INSTALLED BOTH NEW RIBS AND CASTINGS PER SRM 51-30-2.SDR CALA9700532Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 2 RT SLAT SKIN AT UPPER SURFACE OUTBOARD END. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW ECRA 5750-02618.SDR DHL9771259DRib · corrodedAT D-CHECK, NR 7 SLAT I/B TRACK ATTACH CASTING CORROSION UNDER RIB. REPLACED CASTING PER SRM 51-50-3 AND 51-30-2.SDR DHL9771266DFitting · corrodedAT D-CHECK, NR 4 SLAT AND OUTBOARD TRACK INBOARD FITTING CORRODED. REPLACED INBOARD AND OUTBOARD FITTING AND INBOARD RIB PER SRM 51-10-1, 51-30-2 AND 57-50-2.SDR ABXA9700523Fitting · crackedDURING C-CHECK, THE RIGHT WING NR 2 INBOARD SLAT TRACK FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.SDR DHL9771269DFitting · corrodedAT D-CHECK, NR 2 SLAT O/B ATTACH CASTING FOR TRACK HAS CORROSION UNDER RIB SKIN. REMOVED AND INSTALLED NEW CASTING PER SRM 51-10-1.SDR CALA9700426Angle · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING ANGLE AT OUTBOARD SIDE OF LEADING EDGE NOSE RIB, SLAT STA 0. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-40-3.SDR ABXA9700525Fitting · crackedDURING C-CHECK, THE LEFT WING NR 1 OUTBOARD SLAT TRACK FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.SDR ABXA9700522Fitting · crackedDURING C-CHECK, THE RIGHT WING NR 1 INBOARD SLAT TRACK FITTING WAS FOUND CRACKED. THE FITTING WAS REPLACED IAW DC9 SRM 51-30-5.SDR DHL9771263DRib · crackedAT D-CHECK, NR 2 SLAT HAS THE 8TH RIB FROM I/B END CRACKED AT LOWER AFT END. ROUTED OUT CRACK, HFEC, INSTALLED RIB REPAIR PER SRM 57-50-3, 4 BY 2.SDR ABXA9700524Fitting · crackedDURING C-CHECK, THE LEFT WING NR 1 INBOARD SLAT TRACK FITTING WAS FOUND CRACKED. THE FITTING WAS REPAIRED IAW REA D957-18609-MR.SDR UPS97222159Flap · corrodedINSPECTION TYPE-C, CORROSION ON NR 4 KREUGER FLAP FOUND TO BE BEYOND LIMITS OF SRM 57-50-1. KREUGER FLAP REPLACED IAW MM 27-81-01.SDR UPS97222158Flap · corrodedINSPECTION TYPE-C, NR 5 KREUGER FLAP CORRODED BEYOND SRM 57-50-1 LIMITS. NR 5 KREUGER FLAP ASSY REPLACED IAW MM 27-81-01.SDR UPS97222157Flap · corrodedINSPECTION TYPE-C, NR 6 KREUGER FLAP CORRODED BEYOND LIMITS OF SRM. NR 6 KREUGER FLAP ASSY REPLACED IAW MM 27-81-01.SDR DL76S970341Skin · delaminationTHE NR 10 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED AT THE INBD CORNER. THE DAMAGE CUTOUT MEASURES 8 FWD-AFT AND 6 INBD-OUTBD. DAMAGE REPAIRED PER ER/A 361270-14AD.SDR DL767970336Slat · damagedA/C DIVERTED INTO MCO WITH FLAP/SLATS LOCKOUT. ON ARRIVAL, FOUND NR 8 SLAT DAMAGED. REPLACED NR 8 SLAT, OPS CHECK NORMAL.SDR UPS97222103Skin · corrodedINSPECTION SI-CHECK, NR 6 K-FLAP INNER SURFACE IS CORRODED UNDER FASTENER ON RIB 6 FROM OUTBOARD END. CORROSION REMOVED, REWORK OUT OF LIMITS IAW SRM 57-50-1. REMOVED AND REPLACED NR 6 K-FLAP IAW MM 27-81-01.SDR UPS97222102Lugs · corrodedINSPECTION SI-CHECK, NR 2 K-FLAP HAS CORROSION ON OUTBOARD LUG OUTBOARD SIDE AROUND BOLTS. CORROSION FOUND TO BE OUT OF LIMITS IAW UPS EO B727-5750-5542. REMOVED AND REPLACED NR 2 K-FLAP IAW MM 27-81-01.SDR CALA9700322Skin · crackedINSPECTION FOUND THE NR 5 LEADING EDGE SLAT CRACKED AT THREE RIVETS UNDER INBOARD AUXILIARY TRACK. THE CRACKS WERE .25 INCH LONG. A DOUBLER AND FILLER REPAIR WAS INSTALLED IAW ECRA 5750-01159.SDR CALA9700321Skin · crackedINSPECTION FOUND A .25 INCH CRACK AT TWO RIVETS (SIX INCHES INBOARD OF ACTUATOR) ON NR 6 LEADING EDGE SLAT. THE SLAT WAS REPAIRED IAW ECRA 5750-01159.SDR P5CA9700323Skin · corrosionLEVEL 1CORROSION AND BUBBLING OF SKIN ON NR 24 LEADING EDGE DEVICE PANEL. REMOVED CORROSION AND TREATED AREA PER BAC SRM 51-10-01 AND 51-10-02.SDR DL72K970318Skin · crackedTHE LOWER SKIN SECTION WAS CRACKED IN TWO PLACES. INSTALLED SPLICE SECTION REPAIR PER M.M.57-54-O.SDR ABXA9700382Fitting · crackedLT OUTBOARD SLAT TRACK, NR 1 SLAT TRACK, FITTING CRACKED. REPLACED SLAT TRACK FITTING.SDR UPS97222117Skin · crackedINSPECTION TYPE-D, LT WING LE SLAT NR 3 CRACK AT RIVET HOLE ON LE SKIN CENTER. *S/D* HFEC INSPECTED PER NDT PT6 51-00-00 FIG4, CRACKS CONTAINED BY STOP DRILL HOLES. REPAIR CARRIED OUT IAW SRM 57-50-3 FIG 1.SDR TWAA9809508Skin · dentedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND NR 1 L/E SLAT WITH DENTS IN THE L/E. REPAIRED DENTS PER SRM 57-03, PAGE 18A PAR 12B, ITEM A, REFERENCE SRM 51-70-2 PAGE 3 FIG 1. ACFT TT: 51,723 HOURS. ACFT TC: 52,362. (X)SDR DHL9771253DSkin · crackedAT D-CHECK, NR 4 SLAT NR 2 RIB FROM OUTBOARD END IS CRACKED. STOP DRILLED CRACK, HFEC CRACK, INSTALLED RIB REPAIR PER SRM 57-50-3, 4.5 BY 3.SDR DHL9771252DSkin · dentedAT D-CHECK, PERFORM PERMANENT REPAIR TO DENT O/B L/E NR 8 SLAT. CUT OUT DAMAGED AREA, INSTALLED REPAIR PER SRM 57-50-3. REPAIR 6 BY 6.SDR UPS97222156Flap · corrodedINSPECTION TYPE-C, WIDE SPREAD PITTING CORROSION ON NR 2 KREUGER FLAP. CORROSION BEYOND REPAIRABLE LIMITS OF SRM 57-50-1. NR 2 KREUGER FLAP ASSY REPLACED IAW MM 27-81-01.
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