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 DL72K972708Rib · crackedFOUND ON B2 LETTER CHECK, 1.25 INCH CRACK IN RADIUS OF NOSE RIB I/B SIDE OF ACTUATOR ATTACH NR 7 SLAT. REPAIRED PER MM 57-54-0.SDR MWEA97877Vane · chafedDURING C CHK, FOUND RT WING NR 3 FLAP FIXED VANE LEADING EDGE CHAFFED AND GOUGED. MX REPAIRED IAW SRM 51-70-2.SDR DL72S980055Bracket · crackedBRACKET CRACKED, ACT ATTACH BRACKET NR 3 KRUEGER FLAP OUTBD SIDE. BEGAN MANUFACTURING ANGLE REPAIR DOUBLER AS PER M/M 57-20-21 FIGURE 807. FINISH MFG ANGLE REPAIR DOUBLER PER MM 57-20-21 FIG 807. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER M/M 57-20-21 FISDR DLL19972665Skin · crackedLT WING NR 4 SLAT UPPER SKIN CRACKED 4PLS SRM REPAIR REF 57-51-00 FIG808 MAJOR REPAIR.SDR DL757980024Wedge · delaminatedTHE NR 9 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 2 BY 2 AREA OF DELAMINATION. THE DAMAGE WAS REPAIRED PER B757 SRM 51-70-10 AND DOCUMENTED PER ER/A 363471-14AD.SDR DL757972695Wedge · delaminatedTHE NR 3 SLAT WAS FOUND WITH A 4 BY 2 AREA OF DELAMINATION ON THE TRAILING EDGE WEDGE. A COMPOSITE REPAIR WAS INSTALLED PER THE B757 SRM AND DOCUMENTED PER ER/A 363470-14AD.SDR DL72S972667Rib · crackedFOUND F2 LETTER CHECK, 1 IN CRACK NR 3 SLAT NOSE RIB AT SLAT ACT ROD END ATTACH I/B END. REPAIRED PER M/M 57-54-0 FIG 804.SDR DL72L972666Rib · crackedO/B ACTUATOR RIB CRACKED. REPAIRED RIB PER SRM 57-54-0.SDR DL72S972660Skin · crackedFOUND DURING B-2 LETTER CHECK, 1 IN CRACK NR 5 L/E FLAP SKIN AT I/B HINGE CUTOUT. REPAIRED PER M/M 57-53-0 AND ERA 363467-14.SDR DL72S972652Skin · cracked.75 IN CRACK AT NR 2 LE FLAP SKIN AT INBD LIP HINGE CUTOUT. REPAIRED PER ERA 363453-14 AND M/M 57-30-0.SDR EISA97279Slat · malfunctionedNR 2 SLAT LIGHT CAME ON IN-FLIGHT. AMBER LIGHT INDICATION ON FLAP UP NR 2 SLAT DID NOT RETRACT. REPOSITIONED AT 2 DEGREES AND UP LIGHT DID NOT EXTINGUISH. REMOVED AND REPLACED NR 2 LEADING EDGE SLAT PER MM 27. OPS CHECK NORMAL. (X)SDR DL72L972678Rib · crackedRIB NR 18 CRACKED. REPAIRED PER MM 57-54-0.SDR DL72S972608Rib · crackedNR 2 L/E FLAP O/B ACTUATOR ATTACH RIB CRACKED. INSTALLED DOUBLER PER M/M 57-20-21 NR 12.SDR AALA972524Mount · corrodedTUL - KRUEGER FLAP OUTBOARD CARRIER MOUNT CORRODED. REMOVED OUTBOARD CARRIER MOUNT. REPLACED WITH NEW MOUNT. A-300 MM 27-87-14-4. TST: 26,718.41 HOURS. CYCLES: 10,861. (X)SDR TWAA9804014Skin · delaminatedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LEFT WING NR 5 LE SLAT DELAMINATED TOP SURFACE INBOARD END AT TE. REPAIRED PER SRM 57-43-02 FIG 201 DETAIL III ITEM D, AND SRM 51-70-10 FIG 4 SHEET 1 TABLE 1, AND 51-70-10 FIG 9. (M)SDR CALA9701736Bracket · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 8 SLAT OUTBOARD UPSTOP BOLT BRACKET AND LOWER LEADING EDGE SKIN FLANGE BROKEN. THE BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR P2EA97095Skin · crackedSJO - DURING C-CHEC, FOUND NR 5 L/E SLAT HAS A LOOSE RIVET AND A CRACK IN THE SLAT SKIN, LOWER SURFACE LEADING EGE AT OUTBOARD AUXILLARY TRACK. REPAIRED NR 5 SLAT LEADING EDGE LOWER SKIN CRACK AND LOOSE RIVET IAW COOPESA EO COO-3-57-557-97, DATED 12-10-97 ANDSDR DL72S972540Stiffener · crackedA 1.5 INCH CRACK IN 2 EA SPAR STIFFENERS AT NR 6 SLAT OUTBD TRACK. REPAIRED PER MM 57-20-21.SDR DL72S972538Skin · crackedA .25 INCH VISIBLE CRACK IN COVE SKIN ANGLE AT NR 1 SLAT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0.SDR DL72S972514Skin · crackedFOUND ON D1 LETTER CK, ONE 3 AND ONE 3.5 INCH CRACK IN SLAT LOWER SKIN OF NR 6 L/E SLAT AT O/B T/E. REPAIRED PER MM 57-54-0.SDR CALA9701695Skin · crackedINSPECTION FOUND A .125 AND .0937 INCH CRACK AT FASTENER OF NR 6 SLAT SKIN UPPER LEADING EDGE, IN FORWARD ROW OF FASTENERS 50 FROM INBOARD END. THE FASTENERS WERE REMOVED, THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A DOUBLER WAS FABRICATED AND INSTALLED ISDR DL76G972464Wedge · delaminatedWING, NR 1 LE SLAT/TRAILING EDGE WEDGE : REPAIR FOR DELAMINATION. THE UPPER SKIN OF THE NR 1 LEADING EDGE SLAT TRAILING EDGE WAS FOUND WITH A 6 X 1.5 AREA OF DELAMINATION. THE AREA WAS REPAIRED IN ACCORDANCE WITH SRM 57-43-02 PER ER/A 363288 14AD.SDR DL72W972457Baffle · crackedA .75 INCH CRACK NR 3 L/E FLAP HEAT BAFFLE AFT SIDE BELOW ACT AND .5 INCH CRACK NR 2 L/E FLAP HEAT BAFFLE AFT SIDE BELOW ACTUATOR. REPAIR PER MM 57-54-0.SDR DL72S972626Rib · crackedNR 6 SLAT RIB CRACKED LOWER SURFACE. REMOVED RIVETS FORM RIB, BEGAN FABRICATION OF REPAIR DOUBLERS PER M/M 57-40-0 FIG 814. DRILLED AFT DOUBLER, STOP DRILLED PER SRM 57-54-0. ROUTED OUT DAMAGE PER SRM. INSTALLED REPAIR PER SRM.SDR DL72S972625Rib · crackedNR 7 SLAT RIB CRACKED JUST OUTBD OF ACTUATOR ROD END AREA. FABRICATED REPAIR PER MM 57-54-0 FIG 814. INSTALLED REPAIR PER MM 57-54-0 FIG 814.SDR DL72S972624Rib · crackedNR 6 SLAT RIB CRACKED ON INBD END. MADE DOUBLER IAW MM. DRILLED UP AND TREATED AND PAINTED. INSTALLED DOUBLER PER M/M 57-54-0 FIG 814. INSTALLED SEAL.SDR DL72S972623Stop · wornNR 4 SLAT INBD STOP WORN, 2ND WEB FROM INBD END CRACKED OUT UNDER N/P. FABRICATED REPAIR PER MM 57-54-0 FIG 814. OK TO TREAT AND PAINT. TREATED AND PAINTED PER PS 900-2 NR 5. INSTALLED REPAIR PER MM 57-54-0 FIG 814. WEAR WITHIN LIMITS PER MM 27-87-0 FIG 5SDR DL757972467Wedge · delaminatedWING NR 5 AND 7 SLATS TRAILING EDGE WEDGES : REPAIR FOR DELAMINATION. THE NR 5 AND 7 SLATS WERE FOUND WITH AREAS OF DELAMINATION ON THE TRAILING EDGE WEDGES. THE DAMAGES WERE REPAIRED IN ACCORDANCE WITH THE B757 SRM 51-70-10 PER ER/A 363247-14AD.SDR DL72S972393Angle · crackedA 3 INCH CRACK IN NR 7 SLAT AT INBD TRACK UPSTOP PAD COVE ANGLE. REPAIRED PER M/M 57-54-0 AND ERA 363224-14.SDR ABXA9701835Fitting · crackedDURING C-CHECK, FOUND RT WING NR 5 SLAT OUTBD FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-2.SDR CALA9701626Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN LOWER SURFACE OF LT WING NR 4 SLAT SKIN, OUTBOARD OF INBOARD TRACK. THE CRACK WAS STOP DRILLED, A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-5, 51-40-2, AND 51-10-2.SDR DL72S972341Stiffener · crackedFOUND DURING F-1 LETTER CHECK, 1.25 INCH CRACK NR 4 L/E SLAT I/B TRACK ROLLER BOX I/B STIFFENER. REPLACED STIFFENER PER M/M 57-20-21.SDR CKSA97570Rib · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND CRACKS NOTED IN RIB 3 AND 4 EMANATING FROM RIB WEB CUTOUT DOWN WEB AND INTO THE LOWER RIB FLANGE, CRACKS APPEAR TO TERMINATE AT 4TH FASTENER HOLE FWD FROM END OF FLANGE. INSTALLED REPAIR IAW L1011 SRM 57-51-00 FIG 812.SDR CKSA97569Rib · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND CRACKS NOTED IN RIB 5 AND 6 EMANATING FROM WEB CUTOUT DOWN WEB AND ACROSS LOWER RIB FLANGE TO EDGE. INSTALLED REPAIR IAW L1011 SRM 57-51-00 FIG 812. C-CHECK WORK CARD NUMBER 05-57-1006. NON-ROUTINE TASK CARD NUMBER 0SDR DL72L980045Rib · crackedTHIRD FROM OUTBOARD RIB CRACKED, REPAIRED PER M/M 57-54-00.SDR DL72W972298Skin · crackedFOUND ON L/O CK, NUMBER 1 L/E FLAP CRACKED AT THE INBD HINGE CUTOUT. REPAIRED PER MM 57-30-0 AND ERA 363182-14.SDR RRXA97292Vane · crackedDURING A MAINTENANCE VISIT, FOUND RIGHT WING OTBD L/E VANE ASSY HAS NUMEROUS SMALL CRACKS AT T/E. *S/D* FABRICATED AND INSTALLED REPAIR STRAP IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-03704.SDR DL72S972388Skin · wornTHE NR 5 L/E SLAT EXTERNAL SKIN WORN AND CRACKED WHERE FENCE ATTACHES. BEGAN FABRICATED DOUBLER PER MM 57-54-0 FIG 8B, DRILLED DOUBLER PER MM 57-54-0 FIG 813, ROUTED OUT CRACKED AREA PER MM 57-54-0 FIG 813. DYE CHECK PER PS 900-6-3, SHOWS NO FURTHER DAMAGE. SDR DL72S972387Skin · wornTHE NR 4 L/E SLAT EXTERNAL SKIN AND ATTACHMENT HOLES WORN WHERE FENCE FAIRING ATTACHES. BEGAN REPAIR PER MM 57-40-0 PG 817, FABRICATED REPAIR PER MM 57-40-0 PG 817. COMPLETED INSTALL OF DOUBLER PER 57-54-0 PG 817.SDR DL72S972240Rib · crackedNR 2 SLAT RIB OUTBD OF ANTI-ICE DUCT CRACKED. REPAIR PER M/M 57-54-00.SDR CALA9701639Skin · dentedINSPECTION FOUND THE RT WING NR 7 SLAT DENTED .125 INCH DEEP AT XORS 827. THE DENTED AREA WAS CUT OUT, DOUBLERS AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 57-10-00, 51-21-01, AND 51-31-00.SDR ASAA9710108Track · gougedSEA - DURING C-CHECK, THE NR 4 SLAT INBOARD AUXILIARY TRACK AT STATION 41.29 WAS FOUND GOUGED. REPAIRED PER EA 5740-01130 AND BOEING TELEX ASA-SEA-97-0436RR. (M)SDR CALA9701516Skin · dentedINSPECTION FOUND RT WING NR 1 LEADING EDGE SLAT SKIN DENTED. THE DENTED AREA WAS CUT OUT. REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 57-06 AND 51-10-3.SDR DL72S972345Rib · crackedNR 6 SLAT HAS A CRACKED RIB ON INSIDE RADIUS, MARKED. DYE PENETRANT INSPECTED CRACK PER PS 900-6-3 NR 1, STOP DRILLED CRACK AND FABRICATED DOUBLER PER MM 57-40-0 FIG 814. OK TO INSTALL DOUBLER. INSTALLED DOUBLER ON NR 6 SLAT JUST O/B OF ANTI-ICE DUCT.SDR DL72S972344Frame · crackedNR 2 SLAT RACK FRAME CRACKED SECOND FROM RT END. REMOVED DAMAGE, FABRICATED DOUBLER PER MM 57-54-0 PG 818. INSTALLED DOUBLER PER MM 57-54-0 PG 818.SDR DL72L972151Support · crackedFROM MV1C, NR 7 SLAT ACTUATOR O/B SUPPORT STRUCTURE CRACKED. REPAIR PER M/M 57-42-0.SDR DL72K972145Rib · crackedFOUND ON B2 LETTER CK, NR 5 SLAT INBD AND O/B ACT ATTACH BRACKETS CRACKED. REPAIRED PER MM 57-54-0.SDR ASAA9780255Skin · creasedBFM - DURNG 30K CHECK, CREASE WAS FOUND ON RT WING OUTBOARD FLAP INBOARD FIXED VANE. REPAIRED WITH BONDED DOUBLER IAW ASA EA 5750-01254. TT: 29,023 HOURS. TC: 17,222. (X)SDR UPS97224761Hinge · corrodedINSPECTION TYPE:SI NR 6 K-FLAP CENTER HINGE FITING ON WING SIDE IS CORRODED. REMOVED AND REPLACED NR 6 K-FLAP CENTER HINGE FITTING AIRCRAFT SIDE IAW SRM 51-30-2, 51-30-8, 51-30-5.SDR MZZA97275Skin · corrodedKUL - NRC: 844134 - S-CHECK FOUND RIGHT HAND WING LEADING EDGE FLAP NR 4 OUTBOARD HINGE HAS HEAVY SURFACE CORROSION ON UPPER BRACKET. CORROSION REMOVED PER SRM 51-10-6, MATERIAL REMOVED 0.060 INCH FOUND OUT OF LIMITS PER SRM 57-50-1. TREATED, PRIMED, AND RE
Back to JASC 5754