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 C8GA20090047Mount · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 6 SLAT OTBD HOOK AFT MOUNT HAS A CRACK BETWEEN FASTENERS. REMOVED HOOK AND FASTENERS, PERFORMED HFEC, FABRICATED DOUBLER FROM 2024 T3 .125 INCH DIM 7 INCH BY 3.125 INCH. INSTALLED REPAIR, NO OTHER DEFECTS WSDR C8GA20090046Mount · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 8 SLAT INBD HOOK AFT MOUNT HAS CRACK BETWEEN RIVETS. REMOVED FASTENERS AND PERFORMED HFEC. FABRICATED DOUBLER FROM 2024 T3 .125 INCH DIM 8.75 INCH BY 3.15 INCH. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTESDR C8GA20090038Mount · crackedWHILE IN HEAVY MAINTENANCE IT WAS NOTED THAT THE NR 6 K-FLAP UPPER MOUNT IS CRACKED AT THE OUTBOARD UPPER CORNER. REMOVED ASSY MOUNT, FABRICATED TWO WEB'S INBD AND OTBD. INSTALLED REPAIR PARTS IAW DWG NR 65-16275. NO OTHER DEFECTS NOTED. AIRCRAFT WAS RETURSDR C8GA20090035Rib · crackedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 3 SLAT HAS AN INTERNAL ATTACH FITTING CRACKED. THE SLAT ACTUATOR INBD AND OTBD RIBS WERE REMOVED AND REPLACED. NO OTHER DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.SDR ASAA0944389Skin · chafedNR 4 SLAT CHAFFING ON TE LOWER SURFACE AT IB SIDE CORE WITH INTERNAL DOUBLER AND EXTERNAL DOUBLER BONDED REPAIR. REPAIRED NR 4 SLAT TE WEDGE IB END BY ACCOMPLISHING FULL DEPTH BOND.SDR FDEA200902050465Skin · misrepairedRT WING SLAT NR 7 SKIN BETWEEN STA OSS 404.80 AND OSS 427.85 MISREPAIRED. REPAIRED IAW SRM 57-43-01, REPAIR 1, MAJOR REPAIR, CATEGORY "A".SDR SWAA090869Wedge · delaminatedDURING SCHEDULED 12Y CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA090868Wedge · delaminatedDURING SCHEDULED 12Y CHECK, FOUND LT WING NR 2 SLAT T/E WEDGE DELAMINATED. REPAIRED WEDGE PER SRM.SDR SWAA090867Skin · crackedDURING SCHEDULED 12Y CHECK, FOUND RT WING NR 6 SLAT LOWER L/E SKIN CRACKED. REPAIRED SKIN PER SRM.SDR UPS09M54793Skin · misrepairedINSPECTION TYPE:C LT WING L/E UPPER SURFACE XORS 130 TO 139 FOUND FASTENER (REPAIR) SIZE NOT AS PER SRM. DAMAGED BEADED DOUBLER TRIM OFF AT LT WING L/E XORS 130-139. HFEC C/O & FOUND NO CRACK EVIDENT. REPAIR DOUBLER & FILLER OF BEADED DOUBLER REPAIR FAB. RSDR ASAA0944466Skin · crackedRT WING LEADING EDGE NR 6 SLAT HAS 2 CRACKS AT THE INBD AUX TRACK LOWER SKIN. CUT OUT DAMAGED AREA FABRICATED FILLER AND SPLICE PLATE AND INSTALLED REPAIR DOUBLER IAW B737 400 SRM 57 43 01 51 40 02.SDR CNMA20090107Skin · corrodedLT WING, SLAT 2, OTBD GAP STRAP HAS SURFACE CORROSION AND MISSING RIVETS. DAMAGED AREA TRIMMED OUT REINFORCED AREA WITH NEW SLAT SEAL REPAIR IAW SRM VOL 1, 57-10-00, FIG 32. INSTALLED FASTENERS IAW SRM VOL 2, 51-31-01.SDR SWAA090774Slat · delaminatedDURING SCHEDULED 14Y CHECK, FOUND LT WING NR 2 L/E SLAT O/B UPPER CORNER DELAMINATED. REPAIRED SLAT PER SRM.SDR UIEA200800356Skin · crackedNR 7 VC FLAP EXTERIOR SURFACE CRACKED. NR 7 VC FLAP REPLACED IAW 27-81-02. RIGGING AND OPS CHECKED IAW 27-81-00.SDR SWAA090674Wedge · delaminatedDURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE IS DELAMINATED AT I/B END. REPAIRED WEDGE PER SRM.SDR SWAA090673Wedge · delaminatedDURING SCHEDULED 12Y CHECK, FOUND RT WING NR 4 SLAT T/E WEDGE IS DELAMINATED AT I/B END. REPAIRED WEDGE PER SRM.SDR FDEA200901310407Skin · crackedRIGHT WING NR 8 SLAT OTBD TRACK SKIN IS CRACKED. STOP DRILLED CRACK IAW DRAWING SR27-57-034 REV A AND SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 2024-T3 0.071 DIM 9 1/2" BY 6" IAW DRAWING SR27-57-034 REV A. INSTALLED DOUBLER IAW DRAWING SR27-57-034 REV A ASDR UPS09M54614Slat · misrepairedINSPECTION TYPE:3C REPAIR SURVEY SEQ W4-006, RT WING NR 2 SLAT INBOARD SIDE, ANGLE P/N ARB1640-5 HAS AN EXISTING STACKED ANGLE REPAIR NOT PER SRM AND NOT ON UPS MRCSSR. REPAIRED RT WING NR 2 SLAT INBOARD SIDE, ANGLE P/N ARB1647-5 REF EO MD11-5740-32188-A AND SDR UPS09M54613Skin · misrepairedINSPECTION TYPE:3C REPAIR SURVEY SEQ W3-013, LT WING DROOPED L/E SKIN HAS EXISTING REPAIR NOT PER SRM AND NOT ON UPS MRCSSR. SKIN P/N ARB2312-1. REPAIRED LT WING DROOPED L/E SKIN REF. EO MD11-5720-32187-A AND EA 011-5730-01-A1624.SDR UPS09554731Wedge · dentedINSPECTION TYPE:C RT WING NR 9 SLAT T/E WEDGE HAS 1 (EA) DENT OUT OF LIMITS DUE TO PROXIMITY, 9.5 INCHES FROM I/B END, 8.4 INCHES FROM T/E, .50 INCH DIA. REMOVED SURFACE FINISH, FABRICATED AND BONDED 1 EA DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIG 201 PAGE 201/SDR UPS09554701Skin · dentedINSPECTION TYPE:C LT WING-35 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY-15.25 INCH FROM INBD END, 5.6 INCH FROM T/E, 2.0 INCH DIA. REMOVED TOPCOAT PREP FOR BOND DOUBLER IAW SRM 57-43-02/51-70-10 REPAIR NR 2 E(C) PG203 FIG 201. CLEANED/PREP FORSDR UPS09554700Wedge · dentedINSPECTION TYPE:C- LT WING, NR 5 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY 71.75 INCH FROM INBD END, 4.5 INCH FROM T/E, 1.8 INCH DIA. REMOVED TOPCOAT PREP FOR BOND OF DOUBLER IAW SRM 57-43-02/51-70-10, REPAIR NR 2 E(C) PG 203 FIG 201. CLEANEDSDR UPS09554699Skin · dentedINSPECTION TYPE:C LT WING NR 5 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY 69.0 INCHES FROM OTBD END, 1.6 INCH FROM T/E, 1.7 INCH DIA. REMOVED TOPCOAT TO PREP FOR BOND DOUBLER IAW SRM 57-43-02/51-70-10 REPAIR NR 2 E(C) PG 203 FIG 201. CLEANED/SDR UPS09554698Skin · dentedINSPECTION TYPE:C LT WING NR 5 SLAT T/E WEDGE HAS 2 DENT INCH DIA. REMOVED TOPCOAT PREP FOR BOND DOUBLER IAW SRM 57-43-02/51-70-10 REPAIR NR 2 E,(C) PAGE 203M FIG 201. CLEANED AND PREP FOR BOND IAW SRM 57-43-02/51-70-10 REPAIR NR 2, (C) PG 203 FIG 201. FABRSDR UPS09554697Skin · dentedINSPECTION TYPE:C LT WING, NR 5 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY-16.25 INCH FROM OTBD END, 2.8 INCH FROM T/E 1.5 INCH DIAMETER. REMOVED TOPCOAT FOR BOND OF DOUBLER IAW SRM 57-43-02/57-70-10, REPAIR NR 2 E(C) PG 203, FIG 201. CLEANED/SDR UPS09554696Skin · dentedINSPECTION TYPE:C RT WING, NR 6 SLAT T/E WEDGE HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY-58.0 INCH FROM OTBD END, 4.8 INCH FROM T/E 1.5 INCH DIA. EVAL DENT DUE TO HAIL DAMAGE IAW SRM 57-43-03-A1 FIG 101 SHT 4. REMOVED SURF FINISH PREP FOR BOND IAW SRM 57-43SDR UPS09554695Wedge · dentedINSPECTION TYPE:C RT WING, NR 6 SLAT T/E WEDGE HAS 1 WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY-36.5 INCHES FROM OTBD END,1.45 INCH FROM T/E .050 INCH DIA. REMOVED SUR FINISH AND PREP FOR BOND IAW SRM 57-43-02 REP 1 FIG 201/SRM 51-70 10 REP NR 2, E(C) PSDR UPS09554694Wedge · dentedINSPECTION TYPE:C LT WING, NR 4 SLAT T/E WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY 73 INCHES FROM OTBD END, 1.7 INCH FROM T/E. REMOVED TOPCOAT TO PREPARE BOND DOUBLER IAW SRM 57-43-02/51-70-10, REPAIR NR 2 E(C) PG 203, FIG 201. CLEANED AND PREPPED FOR SDR UPS09554691Wedge · dentedINSPECTION TYPE:C LT WING-NR 4 SLAT T/E WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY-97.5 INCH FROM OTBD END, 2.1 INCH FROM T/E (MARKED GRP 3). REMOVED TOPCOAT TO PREPARE FOR BOND OF DOUBLER IAW SRM 57-43-02 AND SRM 51-70-10 PRE NR 2,E, (C)PG203, FIG201. SDR UPS09554673Skin · dentedINSPECTION TYPE:C RT WING, NR 9 SLAT T/E EDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY 57.1 INCH FROM INBD END, 8.3 INCH FROM T/E, .70 INCH DIA. REMOVED SURFACE FINISH, FABRICATED AND BONDED 1 DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIG 201 PAGE 201 SRM 51-70-1SDR UPS09554672Skin · dentedINSPECTION TYPE:C RT WING, NR 9 SLAT T/E HAS 2 DENTS OUT OF LIMITS DUE TO PROXIMITY 19.9 INCH FROM OTBD END, 6.4 INCH FROM T/E, 1.8 INCH DIA (MARKED GROUP 3). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1 DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIG 201 PAGE 2SDR UPS09554665Wedge · dentedINSPECTION TYPE:C RT WING NR 10 SLAT T/E WEDGE HAS 2 (EA) DENTS OUT OF LIMITS DUE TO PROXIMITY 36.75 INCHES FROM T/E, 2.0 INCHES DIA (MARKED GROUP 2). REMOVED SURFACE FINISH FAB AND BONDED 1(EA) DOUBLER IAW SRM 57-43-02 & SRM 51-70-10-R2 FIG 201.SDR UPS09554664Wedge · dentedINSPECTION TYPE:C RT WING NR 8 SLAT T/E WEDGE HAS 1 (EA) DENT OUT OF LIMITS DUE TO PROXIMITY 46.7 INCHES FROM O/B END, 8.25A INCHES FROM T/E .60 DIA (MARKED GROUP 2). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-53-02 REPAIR 1 FIG 201 SDR UPS09554663Wedge · dentedINSPECTION TYPE:C RT WING NR 8 SLAT T/E WEDGE HAS 1 (EA) DENT OUT OF LIMITS DUE TO PROXIMITY 36.5 INCHES FROM O/B END, 1.2 INCH FROM T/E, .65 INCH DIA (MARKED GROUP 1). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-43-02 REPAIR NR 1 FIGSDR UPS09554662Wedge · dentedINSPECTION TYPE:C RT WING - NR 7 SLAT T/E WEDGE HAS 1(EA) DENT OUT OF LIMITS DUE TO PROXIMITY 100.26 INCHES FROM O/B END, 1.6 INCH FROM T/E, .50 INCH DIA (MARKED GROUP 1). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-43-02, REPAIR 1 FISDR UPS09554661Wedge · dentedINSPECTION TYPE:C RT WING - NR 7 SLAT T/E WEDGE HAS 1EA DENT OUT OF LIMITS DUE TO PROXIMITY 46.7 INCHES FROM O/B END, 4.55 FROM T/E IN A 1.7 DIA (MARKED AS GROUP 2). REMOVED SURFACE FINISH, FABRICATED AND BONDED 1EA DOUBLER IAW SRM 57-43-02 REPAIR 1 FIG 201 PSDR SWAA090660Wedge · delaminatedDURING SCHEDULED 12Y CHECK, FOUND RT WING NR 5 SLAT T/E WEDGE DELAMINATED AT I/B END. REPAIRED WEDGE PER SRM.SDR SWAA090626Wedge · delaminatedDURING SCHEDULED 26Y CHECK, FOUND RT WING NR 5 SLAT DELAMINATED AT O/B TRAILING EDGE WEDGE. REPAIRED WEDGE PER SRM.SDR SWAA090605Wedge · delaminatedDURING SCHEDULED 20Y CHECK, FOUND LT WING NR 2 SLAT WEDGE I/B END DELAMINATED. REPAIRED SLAT PER SRM.SDR UPS09154622Skin · erodedINSPECTION TYPE:3/C RT WING I/B SLAT L/E ERODED AT PYLON. REPAIRED USING FIBERGLASS OVERLAY IAW A300-600 SRM 51-77-11, PARA 3 F.SDR UPS09M54561Slat · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 293-W3-07 EXISTING REPAIR DOUBLER ON LT WING NR 8 SLAT BETWEEN STA 1113-1125 IS NOT ON MRCSSR REPORT AND NOT PER SRM. REMOVED EXISTING DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND INTER DOUBLER IAW MD-11 SSDR UIEA200800352Structure · dentedNR 1 LEADING EDGE DEVICE BULLNOSE DENTED. REPAIRED AS PER SRM 57-43-02SDR UIEA200800351Skin · dentedNR 10 VC FLAP BULLNOSE HAS DENT. REPAIRED AS PER SRM 57-43-02.SDR UALA2009012100233Panel · damagedRT WING NR 7 LEADING EDGE SLAT CLOSURE PANEL DAMAGED. REINSTALLED REPAIRED PANEL. OPS CHECK NORMAL, FAIR GOOD. REPAIRED PER GN-MM 1-0-1-24.SDR UIEA200800355Skin · looseLEFT WING LEADING EDGE FAIRING AT OUTBOARD OF LANDING LIGHT FOUND LOOSE RIVETS. LEADING EDGE REPAIRED AS PER SRM 57-41-01-2R-5 REPAIR 5 FIG 201.SDR SWAA090453Skin · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER MM.SDR SWAA090452Slat · puncturedDURING SCHEDULED SPV CHECK, FOUND RT WING NR 5 SLAT PUNCTURED. REMOVED AND REPLACED SLAT PER MM.SDR UPS09554533Strap · brokenINSPECTION TYPE:C2 NR 9 SLAT L/E ACCESS PANEL (TAI ACCESS) LWR SUPPORT STRAP IS BROKEN. REPLACED WITH NEW STRAP.SDR UPS09554471Skin · crackedINSPECTION TYPE:C3 RT WING L/E SKIN UPPER SURFACE AT O/B END OF NR 7 SLAT, SKIN HAS 8 INCH CRACK. REPAIRED PER B757-5740-11855 AND SRM 51-40-02-0G.SDR IPXA09855256Door · misrepairedINSPECTION TYPE:SV LT WING L/E SLOT DOOR REPAIR STA XFS525 DOES NOT CORRELATE TO A SRM SS 752-W3-9. REPAIRED PER TIMCO REO-G12590 REV IR, AND UPS EO DC8-5720-32211-A.
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