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.

SDR DL72S960667Rib · wornDURING INSPECTION, NR 8 L/E SLAT WAS FOUND WITH DAMAGED INTERNAL SUPPORT RIB. ACCOMPLISHED REPAIRS PER SRM 57-50-3.Mar 27, 1996 · N469DA · Boeing 727232SDR 9607506614Skin · crackedDURING LINE CHECK (AMS), FOUND A CRACK IN THE NR 11 KRUEGER FLAP INNER SKIN. REPAIRED FLAP PER EA 66-99604.Mar 26, 1996 · N614US · Boeing 747251BSDR DL757961967Skin · damagedL/E SKIN DAMAGED FROM 70 TO 80 INCHES FROM I/B END. REPAIRED PER SRM 57-43-01.Mar 25, 1996 · N667DN · Boeing 757232SDR DL72L960642Skin · crackedA .25 INCH CRACK IN COVE SKIN LOWER ATTACH ANGLE BELOW NR 2 SLAT ACTUATOR ROD. FOUND DURING D-1 LETTER CHECK. REPAIRED PER MM 57-54-0.Mar 22, 1996 · N506DA · Boeing 727232SDR DL72L960641Rib · crackedFOUND DURING D-1 LETTER CHECK, NR 3 L/E SLAT NOSE RIB CRACKED 1 INCH ON I/B AND O/B SIDES. REPAIRED PER MM 57-54-0.Mar 22, 1996 · N506DA · Boeing 727232SDR UPS96205792Bearing · corrodedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 6 K-FLAP BULLNOSE I/B BEARING HAS CORROSION ON O/B SIDE. REPLACED K-FLAP NR 6 IAW MM 27-81-01.Mar 21, 1996 · N907UP · Boeing 72727CSDR DL72S960687Skin · crackedINNER SKIN CRACKED BETWEEN RIB NR 9 AND NR 10. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT.Mar 21, 1996 · N515DA · Boeing 727232SDR DL72S960650Web · crackedFROM MV-2 ATL, I/B WEB IS CRACKED ON NR 8 SLAT. FABRICATED AND INSTALLED DOUBLER PER M/M 57-54-0 FIG 814.Mar 21, 1996 · N520DA · Boeing 727232SDR DL72S960634Angle · crackedDURING LETTER CHECK, NR 5 L/E SLAT AFT ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PAR 12.Mar 21, 1996 · N499DA · Boeing 727232SDR DL72S960631Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 7 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.Mar 21, 1996 · N499DA · Boeing 727232SDR DL72S960630Angle · crackedFOUND DURING A-1 LETTER CHECK, NR 5 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.Mar 21, 1996 · N499DA · Boeing 727232SDR DL72S960605Angle · crackedFOUND ON A1 LETTER CHECK - REWRITE FROM N/R 50 - ANGLE CRACKED .50 INCH AT NR 7 SLAT ANTI-ICE 'T' DUCT CUTOUT - REPAIR, INSTALL DOUBLER PER M/M 57-54-0, PG 807.Mar 18, 1996 · N515DA · Boeing 727232SDR DL72S960604Rib · crackedFOUND ON F1 LETTER CK, 1 INCH CRACK AT NR 2 L/E SLAT INBOARD NOSE RIB AT ACTUATOR ROD END ATTACH. REPAIRED PER MM 57-54-0.Mar 18, 1996 · N400DA · Boeing 727232SDR DL72K960623Rib · crackedFOUND ON MV1 CHECK, NR 2 SLAT (S/N BN1110) HAS .5 CRACKS IN INBD AND OUTBD NOSE RIBS ADJACENT TO ACTUATOR ROD END. REPAIRED PER M/M 57-54-0 PG 805.Mar 18, 1996 · N412DA · Boeing 727232SDR DL72K960612Attach Angle · crackedFOUND ON MV-1 CHECK, .3750 INCH CRACK IN COVE SKIN ATTACH ANGLE BELOW TIA DUCT OF NR 2 L/E SLAT. REPAIR: REPAIRED PER M/M 57-54-0, PG 807A.Mar 18, 1996 · N412DA · Boeing 727232SDR AWXA960150Skin · crackedPAE - FLT 3812 - DURING ROUTINE SCHEDULED C-9 MAINTENANCE CHECK, FOUND NR 6 SLAT CENTER AUXILIARY TRACK CUT OUT ON FIXED LEADING EDGE HAS CRACK CONTINUING PAST PREVIOUS BLEND OUT. CUT OUT DAMAGED SKIN SECTION. FABRICATED NEW SKIN AND REPAIR DOUBLER AND INSTAMar 18, 1996 · Boeing 737275SDR UPS96205740Bonding Jumper · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 2 K-FLAP OUTBOARD BULLNOSE BONDING JUMPER UPPER HAS PITTING ON OUTBOARD SIDE OF RIB. REMOVED DAMAGED AREA FAB REPAIR PARTS AND INSTALLED IAW SRM 57-50-3.Mar 16, 1996 · N907UP · Boeing 72727CSDR DL72E960730Rib · crackedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 11 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0 FIG 804.Mar 15, 1996 · N830WA · Boeing 727247SDR DL72E960728Rib · crackedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 8 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0.Mar 15, 1996 · N830WA · Boeing 727247SDR DL72E960726Rib · crackedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, THE NR 10 RIB WAS FOUND TO BE CRACKED. THE RIB WAS REPAIRED PER M/M 57-54-0 FIG 814.Mar 15, 1996 · N830WA · Boeing 727247SDR DL72E960725Heat Shield · dentedDURING INITIAL INSPECTION OF THE NR 7 LEADING EDGE SLAT, A DENT WAS FOUND IN THE HEAT SHIELD BETWEEN THE NR 11 AND NR 12 RIB. THE DENT WAS REPAIRED PER M/M 57-50-3 FIG 4.Mar 15, 1996 · N830WA · Boeing 727247SDR DL72E960677Rib · crackedDURING SHOP INSPECTION, THE NINTH AND SIXTEENTH RIBS FROM THE OUTBOARD END OF NR 7 SLAT WERE FOUND TO BE CRACKED. THE DAMAGE WAS REPAIRED PER 727 M/M 57-54-0.Mar 15, 1996 · N830WA · Boeing 727247SDR DL72E960662Rib · crackedDURING SHOP INSPECTION, THE SECOND AND SIXTH RIBS FROM THE OUTBOARD END OF NR 7 SLAT WERE FOUND TO BE CRACKED. THE DAMAGE WAS REPAIRED PER 727 M/M 57-54-0.Mar 15, 1996 · N830WA · Boeing 727247SDR 96FDEA00564Bullnose · corrodedNR0323 AND 004, CORROSION ON NR 4 K-FLAP O/B BONDING JUMPER LOWER ATTACH POINT.Mar 15, 1996 · N154FE · Boeing 72725SDR 96FDEA00527Bullnose · corrodedCORROSION ON NR 4 K-FLAP O/B BONDING JUMPER LOWER ATTACH POINT. REMOVED CORROSION ON NR 4 K-FLAP BULLNOSE O/B BONDING JUMPER, FOUND TUBE OUT OF LIMITS PER SRM 57-50-1. BLENDED TO LIMITS PER DRAWING SR 27-57-010. CLEANED AND TREATED AREA AND REINSTALLED BONDMar 15, 1996 · N154FE · Boeing 72725SDR DL76S960572Te Wedge · delaminatedTHE RT WING NR 12 SLAT TE WEDGE WAS FOUND WITH THE UPPER SKIN DELAMINATED. THE DAMAGE LOCATION IS 3.5 INCHES FROM THE TE EDGE, 10 INCHES FROM THE I/B EDGE COVERING 3.5 DIA. ACCOMPLISHED REPAIRS PER DL ERA 273469-14 REV A.Mar 13, 1996 · N128DL · Boeing 767332SDR DL76S960570Te Wedge · delaminatedTHE NR 5 LEADING EDGE SLAT ON THE LT WING WAS DELAMINATED ON THE T/E WEDGE. THE DAMAGE IS AT THE AFT, I/B CORNER WITH 3.5 INCH DIA COVERAGE. IN ADDITION, THE NR 5 SLAT WAS FOUND WITH AN UNIDENTIFIED PREVIOUS REPAIR EXTENDING FROM THE I/B EDGE OF THE TRAILINGMar 13, 1996 · N126DL · Boeing 767332SDR DL76S960569Skin · delaminatedTHE NR 4 LEADING EDGE SLAT WAS FOUND WITH THE UPPER SKIN DELAMINATED AT THE T/E WEDGE. THE DAMAGE IS ON THE LT WING WITH THE LOCATION OF THE DAMAGE 4 INCHES FROM TE, 81 FROM I/B EDGE AND 3 INCHES IN DIA. ACCOMPLISHED REPAIRS PER DL ERA 273469-14 RA.Mar 13, 1996 · N126DL · Boeing 767332SDR DL72S960680Angle · crackedA CRACK WAS FOUND 32.5 FROM I/B END ON LOWER AFT COVE SKIN ATTACH ANGLE BELOW ANTI-ICE DUCT. REPAIRED AS PER MM 57-54-0 FIG 805A, FOR NR 8 L/E SLAT.Mar 13, 1996 · N532DA · Boeing 727232SDR AWXA960125Skin · dentedPAE - FLT NR 3791 - DURING ROUTINE SCHEDULED C-4/S-1 MAINTENANCE CHECK, FOUND DENT ON RIGHT NR 4 SLAT ON L/E, 1540 MM C/B FROM THE SLAT I/B END. REPAIRED DENT IAW ER 32-27-83-02C. (M)Mar 13, 1996 · N637AW · Airbus A320231SDR DL72S960562Skin · crackedFOUND ON E1 LETTER CHECK, 2 CRACKS IN OUTBD SURFACE OF NR 4 L/E FLAP, 1.5 INCH AND 2 INCH. REPAIRED AND REPLACED L/E FLAP.Mar 12, 1996 · N478DA · Boeing 727232SDR CAL960350Slat · delaminatedGSO - INSPECTION FOUND THE OUTBOARD END OF NR 5 SLAT TOP SURFACE DELAMINATED IN AN AREA APPROXIMATELY 10 INCHES SQUARE. THE DELAMINATED SKIN AND CORE WERE REMOVED. THE AREA WAS REPAIRED BY REPLACING CORE AND APPLYING WET FIBERGLASS OVERLAYS IAW SRM 51-40-6. Mar 12, 1996 · N14209 · Boeing 737130SDR 96FDEA00548Bullnose · corrosionCORROSION (097-562-01-2) NR 4 K-FLAP BULLNOSE O/B BONDING JUMPER, UPPER ATTACH POINT. REMOVED CORROSION PER FEDEX SRM 57-50-03 AND 27-57-010.Mar 11, 1996 · N194FE · Boeing 72722SDR UPS96205693Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE REPORTED NR 6 SLAT HAS CRACK ON FIRST RIB I/B FROM O/B END. REMOVED AND REPLACED RIB IAW SRM 57-50-3.Mar 9, 1996 · N907UP · Boeing 72727CSDR 96FDEA00477Skin · crackedSNRM (0270). NR 4 SLAT, 01B GUIDE HOOK CUT-OUT, CRACKED. C/A STOP DRILLED CRACK AND FABRICATED AND INSTALLED REPAIR PARTS PER FEDEX SRM 57-30-4.Mar 8, 1996 · N275FE · Boeing 727233SDR DL72W960519Angle · crackedFOUND DURING B-2 LETTER CHECK - NR 8 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED AT OUTBOARD UPSTOP PAD. REPAIRED PER M/M 57-54-0, PAR 5A.Mar 7, 1996 · N2821W · Boeing 727247SDR DL72W960518Angle · crackedFOUND DURING B-2 LETTER CHECK - 1 INCH CRACK NR 1 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 PAR 12.Mar 7, 1996 · N2821W · Boeing 727247SDR DL72S960508Angle · crackedFOUND DURING C-2 LETTER CHECK - 2 INCH CRACK NR 4 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER MM 57-54-0 PAR 5A.Mar 6, 1996 · N531DA · Boeing 727232SDR DL72L960500Angle · crackedFOUND ON D1 LETTER CK, NR 7 SLAT LOWER ANGLE CRACKED AT THE ANTI-ICE DUCT CUTOUT. REPAIRED PER MM 57-54-0.Mar 5, 1996 · N505DA · Boeing 727232SDR 96FDEA00451Flap · corrodedNR 4 K-FLAP OUTBOARD LOWER BONDING JUMPER IS CORRODED AT UPPER ATTACH POINT. MATERIAL REMOVED DURING REWORK EXCEEDS LIMITS PER FEDEX SR 27-57-010, REV B. ****S/D*** COMING. C/A REMOVED CORRODED AREA AND REPAIRED OUTBOARD LOWER BONDING JUMPER ATTACH POINT Mar 5, 1996 · N275FE · Boeing 727233SDR DL72S960542Skin · crackedHMV/ATL - NR 4 SLAT TOP SKIN - CRACK AT OUTBOARD SIDE OF STALL FENCE MID-AREA SCREW ATTACH POINT. CORRECTION: REMOVED FENCE. INSTALLED DOUBLER REPAIR PER MM 57-40-0.Mar 3, 1996 · N546DA · Boeing 727232SDR DL757960476Skin · gougedDURING ROUTINE INSPECTIONS OF THE NR 3 SLAT, THE TRAILING EDGE WEDGE WAS FOUND DAMAGED. THE DAMAGE WAS A .25 INCH PUNCTURE THROUGH BOTH UPPER AND LOWER SKINS OF THE NR 3 SLAT TRAILING EDGE WEDGE. IN ACCORDANCE WITH B757 SRM 51-70-10, THE DAMAGE WAS REPAIRED Mar 1, 1996 · N650DL · Boeing 757232SDR DL72S960530Skin · wornDURING A ROUTINE HANGAR INSPECTION, NR 637 WAS WRITTEN DUE TO A GROOVE WORN IN INNER SKIN OF NR 5 SLAT. THE DAMAGE WAS REPAIRED PER MM 57-54-0.Mar 1, 1996 · N546DA · Boeing 727232SDR DL72S960501Angle · crackedFOUND ON C1 LETTER CK, FOUND 1.25 INCH CRACK AT NR 7 SLAT I/B TRACK BOX INBD ANGLE. REPAIRED PER MM 57-20-21.Mar 1, 1996 · N416DA · Boeing 727232SDR DL757960462Te Wedge · dentedDURING INSPECTION, NR 6 SLAT T/E WEDGE WAS FOUND DENTED. REPLACED WEDGE PER SRM 57-43-02.Feb 29, 1996 · N658DL · Boeing 757232SDR DL72W960469Angle · crackedNR 2 SLAT COVE SKIN ANGLE AT TAI DUCT CRACKED .5 INCH. FOUND DURING A-2 LTR CK, REPAIRED PER MM 57-54-0.Feb 29, 1996 · N291WA · Boeing 727247SDR DL72S960555Rib · crackedTHE I/B ACTUATOR RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL.Feb 29, 1996 · N419DA · Boeing 727232SDR DL72S960554Rib · crackedTHE NR 9 RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL.Feb 29, 1996 · N419DA · Boeing 727232SDR DL72S960553Rib · crackedTHE O/B ACTUATOR RIB WAS FOUND TO BE CRACKED IN 2 PLACES. REPAIRED PER M/M 57-54-0 FIGS 804 AND 814, FOR NR 6 L/E SLAT PANEL.Feb 29, 1996 · N419DA · Boeing 727232SDR DL72S960470Angle · crackedA .25 INCH CRACK AT NR 2 SLAT COVE SKIN ANGLE BELOW I/B TRACK. FOUND DURING C-1 LTR CK TPAMM AND REPAIRED PER MM 57-54-0.Feb 29, 1996 · N421DA · Boeing 727232
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