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 UP202224Rib · crackWHILE IN 'D' CHECK MAINTENANCE FOUND NR 5 SLAT 2ND RIB FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9.SDR UP202223Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 5 SLAT THIRD RIB FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3 PAGE 26, FIGURE 9.SDR UP202222Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 8 SLAT 2ND RIB IN FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 51-30-2, UPS OHM 57-51-31 AND DWG 65-16224.SDR UP202208Flap · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP O/B UPPER ATTACH LUG I/B SIDE AROUND FASTENERS. INSTALLED REPAIR IAW SRM 57-50-1.SDR UP202207Flap · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP I/B LOWER BONDING JUMPER UPPER AND LOWER ATTACH POINTS. INSTALLED REPAIR IAW SRM 57-50-1.SDR UP202206Flap · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND DAMAGE DUE TO EXCESSIVE CORROSION, REMOVED AND REPLACED NR 2 K-FLAP. INSTALLED REPAIR IAW MM 27-81-1.SDR DL72S950611Rib · crackedDURING INSPECTION OF THE NR 4 LEADING EDGE SLAT, RIB MARKED NR 18 WAS FOUND TO HAVE A CRACK. THE RIB WAS REPAIRED PER MM 57-54-0 FIG 805.SDR SWAA950161Skin · crackedDURING SCHEDULED TRANSITION CHECK, FOUND NUMBER 6 SLAT CRACKED AT LOWER L/E OF SLAT. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR 95FDEA00122Skin · corrodedCORROSION (76C002-00) NR 6 K-FLAP DATAPLATE. REMOVED DAMAGE AROUND DATAPLATE, REPAIRED K-FLAP WEB AND RELOCATED DATAPLATE IAW SRM 5250-3, DWG SR 27-57-010 REV B.SDR DL757950515Skin · delaminatedDURING SHOP INSPECTION, NR 4 SLAT WAS FOUND WITH THE TRAILING EDGE WEDGE DELAMINATED. REPAIRED PER SRM 57-43-02.SDR DL72S950819Angle · crackedDURING CV-2 CK, FOUND CRACK ON NR 2 SLAT O/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER MM 57-20-21 PG 813.SDR DL72S950519Rib · crackedDURING SHOP INSPECTION, FOUND LEFT WING NR 3 SLAT WITH THE LOWER CHORD DAMAGED OUBOARD OF THE INBOARD UP STOP FITTING AND RIB NR 10 CRACKED AT ITS LOWER END, OUTBOARD OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0.SDR 95ZZZX878Skin · crackedJFK - DURING SPECIAL CHECK, FOUND A 4 INCH CRACK IN RT WING NR 5 LEADING EDGE SLAT, ON INBOARD LOWER SURFACE, RT SIDE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-50-3, FIGURE 1, PAGE 2A. AIRCRAFT TOTAL TIME: 37,178 HOURS; 24,066 CYCLES.SDR 95ZZZX1399Skin · crackedJFK - DURING SPECIAL CHECK, FOUND A 4 INCH CRACK IN RT WING NR 5 LEADING EDGE SLAT, ON INBOARD LOWER SURFACE, RT SIDE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-50-3, FIGURE 1, PAGE 2A. AIRCRAFT TOTAL TIME: 37,178 HOURS; 24,066 CYCLES.SDR DL72S950502Flap · crackedFOUND ON LETTER CHECK, 1 IN CRACK I/B END OF NR 6 L/E FLAP, REPAIR. INSTALLED DOUBLER PER M/M 57-53-0 PG 804.SDR DL72S950497Cover · crackedFOUND ON LETTER CK -1. .5 IN CRACK ON NR 5 L/E SLAT I/B TRACK COVER SKIN - 2. .5 IN CRACK ON NR 6 L/E SLAT I/B TRACK COVER SKIN - 1. AND 2. REPAIRED PER M/M 57-54-0 PG 820.SDR CAL950199Slat · cracked31J - INSPECTION FOUND A 1 INCH CRACK IN THE LEFT LEADING EDGE NR 3 SLAT NR 1 HINGE DOOR AREA. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW SRM 51-10-2, 57-30-4, AND 51-30-2. (X)SDR UPS202164Flap · corrosionWHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 K FLAP CORRODED ON VERY INBD SIDE AT FASTENERS FOR END BULB SEAL. INSTALLED REPAIR IAW UPS EO B727-5740-3980.SDR UPS202156Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 7 SLAT 12TH RIB FROM I/B IS CRACKED COMMON TO LWR CHORD. INSTALLED REPAIR IAW SRM 57-50-3, PAGE 26, FIGURE 9.SDR UPS202155Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RIB 12TH FROM I/B END IS CORRODED. INSTALLED REPAIR IAW SRM 51-10-2 AND 51-10-6 AND DWG 65-17296.SDR UPS202154Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 6 SLAT RIB 13TH FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3, FIGURE 9.SDR UPS202153Angles · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 1 SLAT I/B AND O/B TRACK TO SKIN ANGLES ARE CRACKED. INSTALLED REPAIR IAW SRM 51-30-2, UPS OHM 57-51-31 AND IPC 57-50-1.SDR UPS202152Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 3 SLAT I/B RIB AT I/B TRACK IS CRACKED AT FLANGE COMMON TO COVE PANELS AND IS NOT CONTAINED BY PREVIOUS REPAIR. INSTALLED REPAIR IAW BSRM 57-50-3.SDR UPS202151Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT RT (I/B) ACTUATOR RIB CRACKED BETWEEN FLANGES COMMON TO SPAR AND UPPER SKIN. INSTALLED REPAIR IAW EO 727-57-1077.SDR UPS202150Panel · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT COVE PANEL CRACKED AT O/B UP STOP. INSTALLED REPAIR IAW SRM 51-20-1 AND 51-30-02.SDR UPS202149Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 8 SLAT 1ST RIB FROM I/B IS CRACKED. INSTALLED REPAIR IAW SRM 51-30-2 AND DWG 65-16224.SDR UPS202147Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 3 SLAT 4TH FROM O/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3.SDR UPS202146Skin · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND TAI SKIN CRACKED 1 INCH O/B OF O/B TRACK TO SLAT ATTACH POINT. INSTALLED REPAIR IAW EO 727-57-1080.SDR UPS202145Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 3 SLAT 14TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3.SDR UPS202144Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 3 SLAT 13TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-3.SDR UPS202143Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 3 SLAT I/B END RIB IS CRACKED. INSTALLED REPAIR IAW SRM 51-10-1.SDR UPS202142Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND LT WING NR 4 SLAT, 6TH RIB FROM O/B END (JUST I/B OF O/B TRACK) IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-01.SDR UPS202141Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 4 SLAT, 7TH RIB FROM I/B END IS CRACKED. INSTALLED REPAIR IAW SRM 57-50-01.SDR UPS202140Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND LT NR 4 SLAT I/B END RIB CRACKED IN FWD RADIUS. INSTALLED REPAIR IAW SRM 51-30-02 AND OHM 57-51-61.SDR UPS202139Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND NR 7 SLAT FIRST RIB ON O/B END CRACKED. INSTALLED REPAIR IAW 51-10-1 AND DWG 65-16223.SDR DL72S950817Rib · crackedDURING CV-2 CK, FOUND RIB CRACKED 1 INCH ON NR 3 SLAT JUST OUTBD OF OUTER TRACK. REPAIRED PER SRM 57-50-3 FIG 9.SDR DL72S950689Rib · crackedAT HMV, FOUND NR 2 LEADING EDGE SLAT WITH CRACKED RIB AT 2ND LOCATION FROM THE OUTBD END OF SLAT. REPAIRED PER SRM 57-54-0 PG 819.SDR SWAA950124Skin · crackedDURING SCHEDULED D CHECK, FOUND NUMBER 2 SLAT SKIN CRACKED ADJACENT TO EXISTING REPAIR. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND DRAWING 65C30133.SDR DL72S950695Rib · crackedAT HMV, NR 3 L/E SLAT WAS FOUND WITH CRACKED RIBS JUST INBOARD OF THE INBOARD SLAT TRACK AND OUTBOARD OF TAI DUCT. REPAIRED PER MM 57-54-0 PG 807.SDR DL72S950694Rib · crackedAT HMV, FOUND NR 3 L/E SLAT WITH RIBS NR 1 AND NR 2 CRACKED. REPAIRED PER SRM 57-50-3 FIG 9 AND MM 57-54-0 PG 819.SDR DL72S950690Rib · crackedAT HMV, FOUND RT WING NR 6 SLAT WITH THE 2ND RIB FROM THE INBOARD END CRACKED AND 2 CRACKS IN RIB ON THE OUTBARD SIDE OF THE INBOARD TRACK. REPAIRED PER SRM 57-50-3 PG 25.SDR DL72S950596Rib · crackedRIB CRACKED, 3RD RIB OUTBOARD OF ACTUATOR MOUNT ON NR 6 L/E SLAT. FOUND DURING INSP AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 819.SDR DL72S950595Angle · crackedLOWER CHORD ANGLE CRACKED AT 2ND RIB O/B OF ACTUATOR FITTING ON NR 6 L/E SLAT. FOUND DURING INSP AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 816.SDR DL72S950593Rib · crackedOUTBOARD RIB CRACKED ON NR 5 L/E SLAT. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED PER MM 57-54-0 PG 819.SDR DL72S950592Stops · wornINBOARD AND OUTBOARD STOP WORN ON NR 5 L/E SLAT. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED STOPS PER MM27-81-11 PG 803.SDR DL72S950591Rib · crackedRIB CRACKED, 2ND RIB FROM OUTBOARD END OF NR 5 L/E SLAT. FOUND DURING INSPECTION AT HMV2 IN ATL. REPAIRED PER M/M 57-54-0 PG 819.SDR DL72S950586Le Rib · crackedDURING HMV, FOUND RIB CRACKED ON INBD SIDE OF INBD TRACK ON NR 7 L/E SLAT AND A RIB CRACKED ON OUTBD SIDE OF INBD TRACK NR 7 SLAT, REPAIRED PER MM 57-54-0 PG 805 ON INBD SIDE AND OUTBD SIDE PER MM 57-57-0 PG 805.SDR DL757950443Wedge · delaminatedDURING SHOP INSPECTION, LEFT WING NR 3 LEADING EDGE SLAT T/E WEDGE WAS FOUND TO BE DELAMINATED. REPAIRED BY PLACING WEDGE PER SRM 57-43-02.SDR DL72S950441Skin · crackedFOUND DURING C-1 LETTER CHECK, 1.375 INCH CRACK ON I/B LWR CORNER OF NR 2 L/E FLAP. ALSO, .5 INCH CRACK AT I/B LWR CORNER OF NR 3 L/E FLAP. REPAIRED PER B727 M/M 57-53-0 PG 804.SDR DL72W950413Panel · dentedDURING SHOP INSPECTION, RT WING SLAT PANEL WAS FOUND WITH DENTED UPPER SKIN. REPAIRED PER SRM 57-50-3 FIG 1.
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