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 06FDEA2301Skin · unknownLEFT WING SLAT NR 2, FOUND EXTERNAL REPAIR DOUBLER AT STA XORS 264 ON THE INTERNAL SKIN LOWER SIDE 12 X 10 INCHES. REMOVED EXISTING REPAIR TO EVALUATE DAMAGE IAW SRM 51-30-01 VOL 2. FABRICATED PART IAW DETAIL PART TRAVELER N01197 AND IAW SRM 51-30-01 VOL 2. SDR ABXA060240Attach Angle · crackedTWO EA NOSE RIB TO LEADING EDGE ATTACH ANGLES CRACKED AT NR 8 SLAT OUTBOARD DRIVE CUTOUT. REMOVED AND REPLACED RIB IAW B767 SRM 51-40-02.SDR ASAA0640693Structure · crackedNUMBER 2 SLAT LOWER TEE CHORD CRACKED AT ACTUATOR. REMOVED DAMAGED TEE CHORD, FABRICATED NEW TEE CHORD. DRILLED, TREATED, PRIMED AND INSTALLED IAW SRM 51-40-02, 51-30-01 FIG 7, 51-40-05 AND 51-21-21 PG 705.SDR SWAA062068Slat · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 3 L/E SLAT DELAMINATED AT OUTBOARD T/E WEDGE. REPAIRED SLAT PER SRM.SDR USAA200606006Skin · delaminated3.5" L BY 1.4" W DELAMINATION AT OUTBD AFT UPPER SKIN AT NR 5 SLAT TRAILING EDGE. REPAIRED PER EA 82529.SDR AWXA200601077Skin · crackedDURING C17 CHECK DISCOVERED 4 CRACKS, .063 INCHES, ON THE BOTTOM OF THE NR 1 SLAT SKIN OUTBOARD OF THE INBOARD MAIN TRACK. MAINTENANCE REPAIRED THE BOTTOM SKIN OF THE NR 1 SLAT OUTBOARD OF THE INBOARD MAIN TRACK IAW BOEING 737-300 SRM 57-43-01-2R6 FIG 201.SDR AWXA200601068Skin · crackedDURING C17 CHECK DISCOVERED 3 CRACKS, .250 INCHES, LOCATED ON THE BOTTOM OF THE NR 2 SLAT SKIN BELOW THE OUTBOARD AUX TRACK AT SLAT STATION 189.0L. MAINTENANCE CUT OUT DAMAGED AREA IAW B737-300 SRM 57-43-01-2R6 FIG 201. FABRICATED SPLICE PLATE AND FILLER IAWSDR MWEA060057Attach Fitting · corrodedLEFT NR 2 LEADING EDGE SLAT, OUTBOARD ATTACH FITTING HAS CORROSION AT RETAINER SCREW HOLE. FABRICATED AND INSTALLED PLUG.SDR USAA060787Skin · crackedLT WING LEADING EDGE, JUST O/B OF PYLON CRACKED. INSTALLED NEW PNL IAW TR 57-41-02, DEFECT SIZE: .500 INCH.SDR CALA0600202Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN THE LT WING NR 1 SLAT LOWER SKIN AT FASTENER AREA O/B OF I/B AUX TRACK. THE CRACKED AREA WAS REMOVED AND FILLER AND A SPLICE PLATE WERE INSTALLED IAW SRM 57-43-01, FIGURE 201.SDR PIDR2006004Skin · crackedINSPECTION NOTED A GOUGE ON THE NR 5 SLAT UPPER LEADING EDGE SURFACE 28 INCHES FROM THE INBOARD END (SS169.0). REPAIRED DAMAGED AREA IN ACCORDANCE WITH PACE AIRLINES REPAIR PROCEDURE REPORT EA 57-140 DATED 05/20/06 WITH FAA DER APPROVED 8110-3 DATED MAY 20, 2SDR PIDR2006005Skin · crackedINSPECTION NOTED CRACKS AT SEVERAL FASTENER LOCATIONS IN THE NR 5 SLAT LOWER TRAILING EDGE SKIN PANEL UNDER THE SLAT ACTUATOR. REPAIRED DAMAGED AREA IN ACCORDANCE WITH SRM 57-43-01.SDR PIDR2006006Skin · crackedINSPECTION NOTED SEVERAL CRACKS IN THE NR 3 SLAT LOWER TRAILING EDGE SKIN BELOW THE SLAT ACTUATOR. REPAIRED DAMAGED AREA PER SRM 57-43-01.SDR HALA0600532Skin · damagedRIGHT WING FIXED LEADING EDGE SKIN IS DAMAGED AT NR 9 SLAT IB ROTARY ACTUATOR AND IB MAIN TRACK CUTOUT RESIDUE MOTOR.// REPAIRED THE RT WING L/E SKIN AT NR 9 SLAT I/B ROTARY ACTUATOR AND I/B MAIN TRACK CUTOUT IAW SRM 57-41-01 AND SRM 51-70-07.SDR HALA0600571Panel · damagedFIXED LEADING EDGE COMPOSITE PANEL IS DAMAGED OB OF NR 9 SLAT IB CONTROL ROD AND IB MAIN TRACK CUTOUT. REMOVED AND REINSTALLED FIXED LEADING EDGE COMPOSITE PANEL OB OF NR 9 SLAT BIG CONTROL ROD REPAIRED ON STRB CARD 5027 TO INCLUDE MISSING FASTENER REFERENCEDSDR 06FDEA2215Structure · corrodedNR 1 K-FLAP CORRODED AT O/B BONDING JUMPER ATTACH POINT. REPAIRED NR 1 K-FLAP PER FED EX EA 7-5710-100544.SDR USAA060755Wedge · damagedNR 2 SLAT T/E WEDGE HAS SMALL SECTION OF MISSING METAL SKIN ON LOWER I/B CORNER. REMOVED SKIN DAMAGE, INSTALL FILLER IAW SRM 51-70-10. DEFECT SIZE: .5 X .5 INCH.SDR 06FDEA2151Skin · scratchedLEFT WING, NR 2 SLAT INNER SURFACE FOUND WITH SCRATCH MARK. REPAIRED AS PER SRM 57 -10-00 FIGURE 10 VOLUME I. THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.SDR DHL2006873514Vane · corrodedLT WING INBD VANE SLOT CORRODED STA XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-19-2006, DWG AST060506 DATED 05-11-06. REMOVED CORROSION, FOUND OUT OF LIMITS. REMOVED FASTENERS, CUT OUT DAMAGED SECTION IAW DWG AST060506. PERFORMED NDT INSDR DHL2006873519Vane · damagedRT INBD VANE SLOT L/E UPPER PART HOLES ELONGATED STA XILD 7095 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-19-06, DWG AST060505 DATED 05-11-06. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION. PERFORMED NDT INSP, NO CRACKSDR DHL2006873516Structure · damagedRIGHT OUTBOARD VANE SLOT L/E HAS AN INTERIM REPAIR AT STA XOLDO 67.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001 (NO CRACK OR CORROSION FOUND). FABRICATED ESDR DHL2006873527Skin · damagedRT OUTBOARD VANE SLOT L/E HAS INTERIM REPAIR AT STA XOLDI 6.224 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. CUT OUT DAMAGED SECTION IAW DWG AST060503. PERFORMED NDT INSP IAW DC8 NDT SPM PART 06-10-01-001. NO CRSDR DL767060433Skin · corrodedTHE NR 7 SLAT (RT WING INBD SLAT) T/E WEDGE WAS FOUND WITH SKIN AND CORE CORROSION TOTALLING 151 SQ IN. REPAIRED PER ERA090851-14AD.SDR MWEA060051Doubler · crackedLEFT WING NR 2 SLAT OUTBOARD CENTER SLAT TRACK, APPROXIMATELY AT STATION XOS 240.0 EXISTING REPAIR DOUBLER CRACKED THROUGH 2 FASTENERS AND SKIN CRACKED PAST REPAIR TERMINATING AT PANEL 1136C, CUTOUT ON LOWER SKIN. FABRICATED AND INSTALLED DOUBLER AND FILLER.SDR USAA200605003Skin · crackedMULTIPLE NUMBER OF CRACKS, TOT APPROX LENGTH 2 INCHES, AT LOWER TIE SURFACE AT ACTUATOR, NR 3 SLAT SKIN. INSTALLED FILLER AND DOUBLER PER SRM 57-43-01, REPAIR 06.SDR SWAA061769Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING NR 3 SLAT UPPER SURFACE SKIN CRACKED AT LEADING EDGE. REPAIRED SLAT SKIN PER CMM AND SRM.SDR 06FDEA1998Doubler · crackedRT WING FIXED L/E BEADED DOUBLER FOUND CRACK BETWEEN XORS 625 AND 629. REPAIRED AS PER FEDEX EA 1-5730-99657. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA1997Doubler · crackedRT WING FIXED L/E BEADED DOUBLER FOUND CRACK BETWEEN XORS 643 AND 649. REPAIRED AS PER FEDEX EA 1-5730-99657. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA1996Doubler · crackedFOUND RT WING FIXED L/E BEADED DOUBLER FOUND CRACK BETWEEN XORS 692 AND 698. CRACK ON RT WING FIXED L/EDGE BEADED DOUBLER BETWEEN STA XOS 692 AND 698 REPAIRED AS PER FEDEX EA 1-5730-99656, REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR 06FDEA1995Doubler · crackedLT WING FIXED L/EDGE BEADED DOUBLER FOUND CRACKED FROM STA XOS 610 TO XOS 616. REPAIR CARRIED OUT AS PER FEDEX EA 1-5730-99655.SDR 06FDEA1994Doubler · crackedFOUND LT WING FIXED L/EDGE BEADED DOUBLER FOUND CRACKED FROM STA XOS 667 TO XOS 673. REPAIRED AS PER FEDEX EA 1-5730-99654.SDR 06FDEA1993Doubler · crackedFOUND LT WING FIXED L/EDGE BEADED DOUBLER FOUND CRACKED FROM STA XOS 643 TO XOS 648. REPAIRED AS PER FEDEX EA 1-5730-99655.SDR 06FDEA1992Doubler · crackedFOUND LT WING FIXED L/EDGE BEADED DOUBLER FOUND CRACKED FROM STA XOS 636 TO XOS 643. REPAIRED AS PER FEDEX EA 1-5730-99655.SDR 06FDEA1990Doubler · crackedFOUND LT WING FIXED L/EDGE BEADED DOUBLER FOUND CRACKED FROM STA XOS 698 TO XOS 703. REPAIRED AS PER FEDEX EA 1-5730-99654.SDR 06FDEA1989Doubler · crackedFOUND LT WING FIXED L/EDGE BEADED DOUBLER FOUND CRACKED FROM STA XOS 734 TO XOS 740. REPAIRED AS PER FEDEX EA 1-5730-99653.SDR 06FDEA1988Doubler · crackedFOUND LT WING FIXED L/EDGE BEADED DOUBLER FOUND CRACKED FROM STA XOS 679 TO XOS 685. REPAIRED AS PER FEDEX EA 1-5730-99654.SDR 06FDEA1987Doubler · crackedFOUND LT WING FIXED L/EDGE BEADED DOUBLER FOUND CRACKED FROM STA XOS 728 TO XOS 734. REPAIRED AS PER FEDEX EA 1-5730-99653.SDR 06FDEA1985Skin · crackedFOUND LT WING FIXED L/E CRACK AT XOS 892 SLAT TRACK CUTOUT. REPAIRED AS PER SRM 57-10-00 FIGURE 21, VOLUME I. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.SDR DHL2006873523Skin · damagedLEFT OUTBOARD VANE SLOT HAS INTERIM REPAIR AT STA XOLDI 6.225 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 DATED 05-18-06, EO AST060501 DATED 05-06-06. REMOVED EXISTING REPAIR DOUBLER IAW SRM 51-1-21. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PSDR IXXA06SMN165SRepair · improperDURING ROUTINE C CHECK INSPECTION, LEFT HAND INNER WING EXTENDED LEADING EDGE SLOT OUTER PLATING LOWER SIDE EXISTING REPAIR IMPROPER AT STATION XFS 341.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NUMBER 06245 DATE 05-22-06, SEMAN DRAWING NUMBER ED 4220 DASDR IXXA06SMN164SSkin · misrepairedDURING INSPECT, FOUND LT INNER WING EXTENDED L/E SLOT OUTER SKIN EXISTING REPAIR IMPROPER AT STA XFS 310.000. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIR DOUBLER IAW DC-8 SRM 51-1-21. REMOVED DAMAGED AREA IAW SEMAN DWG NR ED 4233. PERFORMED NDT INSPECTSDR IXXA06SMN163SSkin · damagedDURING C CHECK, FOUND RT OUTER WING INBD EXTENDED L/E OUTER SKIN LWR SIDE, 3 EXISTING DOUBLER REPAIRS BETWEEN XW 485.000 AND XFS 591.250. REMOVED EXISTING REPAIR DOUBLERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED AREA IAW SEMAN DRAWING NUMBER ED 4228. PERFORMEDSDR HALA0600421Skin · debondedNR 11 SLAT LOWER SKIN DISBONDED O/B END T/E. REPAIRED NR 11 SLAT DISBOND ON LWR SKIN O/B END T/E PER SRM 51-70-10-2R-0.SDR USAA060705Wedge · debondedSKIN DISBONDING, COMPOUND LOST, NR 3 L/E SLAT, I/B UPPER END OF WEDGE. FABRICATED FILLER & DOUBLER, THEN BONDED PER SRM 51-70-10, DEFECT SIZE: 2.6"L X 3"W X .250"D.SDR USAA060706Skin · crackedNR 3 SLAT, I/B TRACK LWR AFT EDGE MISSING COMP MATERIAL & CRACKED. FABRICATED OVERLAY REPAIR AND BONDED PER SRM 51-70-06, MM 51-20-10, DEFECT SIZE: .5"L X .5"W X .090"D.SDR ASAA0640585Wedge · delaminatedNR 2 SLAT OB TE DELAMINATED. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 51 70 10.SDR ASAA0640584Wedge · dentedFOUND LT WING NR 2 SLAT IS DENTED AT OB AUX TRACK. REPAIRED DAMAGED AREA OF THE LT WING NR 2 SLAT PER SRM 51 70 10 PG 211 PARA 7 PG 213 PARA 8 PG 221 PARA 238 PARA 15 AND PAGE 249 PARA 20.SDR 06FDEA1873Wedge · damagedCOMPLY WITH AGING 9-AGING-INSP REV NR POS PT1, PREVIOUS REPAIR FOUND LOCATED ON THE LT OUTBD FLAP T/E WEDGE UPPER SURFACE OUTBD OF NUMBER THREE FLAP TRACK, WS 847-877. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN SRM REPAIR NEW REPAIR ACCOMPLISHESDR SWAA061610Skin · crackedDURING SCHEDULED C2 CHECK, FOUND RT WING NR 5 SLAT CRACKED AT LOWER L/E. REPAIRED NR 5 SLAT PER SRM.SDR SWAA061609Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND RT WING NR 4 SLAT DELAMINATED. REMOVED AND REPLACED NR 4 SLAT PER MM.
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