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 DL72E952082Flange · crackedFOUND ON A1 LTR CK, NR 7 SLAT CRACKED FLANGE TWO PLACES UNDER ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0 P 802.May 12, 1995 · N2826W · Boeing 727247SDR DL72S952333Bracket · crackedAT HMV, FOUND UPPER/LOWER CORNERS CRACKED FOR NR 2 LE FLAP ACT MOUNT BRACKET. INSTALLED DOUBLER PER M/M 57-20-21 PG 811.May 11, 1995 · N497DA · Boeing 727232SDR DL72S952081Angle · damagedTOOLMARKS ON INNER CLOSE OUT SKIN ATTACH ANGLE INSIDE AT 8TH RIB IN FROM OUTBD END OF NR 2 SLAT. REPAIRED PER MM 57-54-0 FIG 805A.May 11, 1995 · N545DA · Boeing 727232SDR DL72S952043Rib · crackedFOUND DURING E-1 LETTER CHECK, NBR 7 L/E SLAT NOSE RIB HAS .25 INCH CRK AT FWD SIDE RT SIDE OF ACTUATOR ATTACH POINT. REPAIRED PER MM 57-54-0 PG 803.May 11, 1995 · N404DA · Boeing 727232SDR CAL950385Rib · corrodedGSO - INSPECTION FOUND THE OUTBOARD RIB/WEB AND BOLT HOLE BUSHINGS CORRODED AT NR 3 LEADING EDGE SLAT OUTBOARD TRACK TO SLAT ATTACH POINT. THE CORROSION WAS REMOVED AND REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 57-30-3 AND 51-30-2. (W)May 10, 1995 · N17773 · Boeing 727227SDR CAL950383Intercostal · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT SLAT TRACK ATTACH FITTING AREA OF NR 2 SLAT INBOARD SLAT TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-30-3 AND 51-30-02. (W)May 10, 1995 · N17773 · Boeing 727227SDR CAL950381Intercostal · crackedGSO - INSPECTION FOUND THE NR 6 SLAT INTERIOR WITH A CRACK IN EACH OF TWO INTERCOSTALS AT INBOARD SLAT TRACK ATTACH FITTING. THE CRACKS WERE 1.2 INCHES LONG. A DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-50-3. (W)May 10, 1995 · N17773 · Boeing 727227SDR DL767952026Te Wedge · dentedT/E WEDGE OF NR 7 SLAT HAS DENTED BY HAIL STORM CHANGED T/E WEDGE PER CMM 57-43-37.May 9, 1995 · N114DL · Boeing 767232SDR DL767951994Skin · dentedDURING INSPECTION, NR 11 L/E SLAT PANEL UPPER T/E WEDGE WAS FOUND DENTED. REPAIRED PER SRM 57-43-61.May 9, 1995 · N114DL · Boeing 767232SDR DL757951964Skin · delaminatedDURING INSPECTION, LEFT WING SLAT PANEL WAS FOUND WITH DELAMINATION OF THE T/E WEDGE AT THE SLAT SPAR. REPLACED WEDGE PER SRM 57-43-02.May 9, 1995 · N659DL · Boeing 757232SDR UPS203188Slat · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 SLAT. REPLACED NR 1 SLAT PER MM 27-81-32.May 8, 1995 · N949UP · Boeing 72725CSDR UPS203187Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP ASSY. REPLACED K-FLAP ASSY PER MM 27-81-01.May 8, 1995 · N949UP · Boeing 72725CSDR UPS203185Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP ASSY. REPLACED K-FLAP ASSY PER NMM 27-81-01.May 8, 1995 · N949UP · Boeing 72725CSDR UPS203184Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION NR 1 K-FLAP ASSY. REPLACED K-FLAP ASSY PER NMM 27-81-01.May 8, 1995 · N949UP · Boeing 72725CSDR UPS203183Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 5 K-FLAP ASSY. REPLACED K-FLAP ASSY PER NMM 27-81-01.May 8, 1995 · N949UP · Boeing 72725CSDR DL76S951930Skin · dentedDURING SHOP VISIT, NR 6 L/E SLAT WEDGE WAS REPLACED DUE TO HAIL DAMAGE PER CMM 57-43-61.May 8, 1995 · N135DL · Boeing 767332SDR DL757951938Skin · delaminatedDURING SHOP INSP, THE T/E WEDGE WAS FOUND TO BE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02 FIG 202.May 8, 1995 · N653DL · Boeing 757232SDR DL757951997Skin · delaminatedDURING SHOP INSPECTION, NR 2 SLAT T/E WEDGE WAS FOUND DELAMINATED. REPLACED WEDGE PER SRM 57-43-03.May 7, 1995 · N659DL · Boeing 757232SDR DL757951925Skin · dentedHAIL DAMAGE OCCURED, T/E WEDGE HAS MANY DENTS. REPLACED T/E WEDGE PER SRM 57-43-02, FOR NR 4 L/E SLAT.May 7, 1995 · N620DL · Boeing 757232SDR DL757951924Skin · dentedHAIL DAMAGE TO NUMBER 5 SLAT. REPLACED WEDGE PER SRM 57-43-02.May 7, 1995 · N620DL · Boeing 757232SDR DL76S952287Te Wedge · dentedT/E WEDGE DENTED TOP SURFACE. INSTALLED WEDGE PER CMM 57-43-55, FOR NR 4 L/E SLAT AT SHOP INSPECTION.May 6, 1995 · N135DL · Boeing 767332SDR DL757951918Te Wedge · dentsHAIL DAMAGE ON NR 8 SLAT T/E WEDGE. REPLACED T/E WEDGE PER SRM 57-43-02.May 6, 1995 · N620DL · Boeing 757232SDR DL757951917Skin · dentedDURING SHOP INSPECITON, NR 1 L/E SLAT, T/E WEDGE WAS REPAIRED FOR HAIL DAMAGE PER SRM 57-43-02.May 6, 1995 · N620DL · Boeing 757232SDR DL757951908Skin · dentedDURING SHOP VISIT, NR 6 L/E SLAT WAS REPAIRED FOR HAIL DAMAGE, PER SRM 57-43-02.May 6, 1995 · N620DL · Boeing 757232SDR DL767953159Te Wedge · delaminatedDURING SHOP INSPECTION, NR 4 L/E SLAT PANEL WAS FOUND WITH DELAMINATION TO T/E WEDGE. WEDGE WAS REPLACED PER SRM 57-43-55.May 5, 1995 · N114DL · Boeing 767232SDR DL757951903Te Wedge · dentedHAIL DAMAGE ON NR 10 SLAT. REPLACED T/E WEDGE PER SRM 57-43-02.May 5, 1995 · N620DL · Boeing 757232SDR DL72S951902Rib · crackUPON INSPECTION, FOUND CRACK IN RIB OF NR 6 L/E SLAT. REPAIRED ITEM PER MM 57-54-0 FIG 814. FOUND DURING SHOP VISIT.May 5, 1995 · N522DA · Boeing 727232SDR DL757951880Te Wedge · dentedLEFT WING SLAT PANEL TRAILING EDGE WEDGE WAS FOUND WITH HAIL DAMAGE. REPLACED WEDGE PER SRM 57-43-02.May 4, 1995 · N676DL · Boeing 757232SDR DL76S951861Te Wedge · dentedDURING SHOP INSPECTION, RT WING L/E SLAT PANEL WAS FOUND WITH HAIL DAMAGE TO T/E WEDGE. REPLACED WEDGE PER MM 57-43-55.May 3, 1995 · N135DL · Boeing 767332SDR DL757952054Te Wedge · damagedRT WING NR 9 L/E SLAT TRAILING EDGE WEDGE, WAS FOUND WITH HAIL DAMAGE. REPLACED WEDGE PER SRM 57-43-02.May 3, 1995 · N620DL · Boeing 757232SDR DL757952053Te Wedge · damagedLEFT WING NR 3 L/E SLAT TRAILING EDGE WEDGE, WAS DAMAGED BY HAIL. REPLACED WEDGE PER SRM 57-43-02.May 3, 1995 · N620DL · Boeing 757232SDR DL757952052Te Wedge · damagedLEFT WING NR 1 L/E SLAT TRAILING EDGE WEDGE, WAS FOUND DAMAGED FROM HAIL. WEDGE WAS REPLACED PER SRM 57-43-02.May 3, 1995 · N620DL · Boeing 757232SDR DL757951894Te Wedge · damagedLEFT WING NR 5 SLAT PANEL TRAILING EDGE WEDGE WAS FOUND WITH DENTS FROM HAIL. REPLACED T/E WEDGE PER SRM 57-54-02.May 3, 1995 · N620DL · Boeing 757232SDR DL757951858Wedge · dentedDURING INSPECTION, RT WING NR 6 L/E SLAT WEDGE WAS FOUND DENTED BEYOND LIMITS. REPLACED WEDGE PER SRM 57-43-02.May 3, 1995 · N676DL · Boeing 757232SDR DL757952039Te Wedge · delaminatedT/E WEDGE DELAMINATED NR 4 SLAT. REPLACED WEDGE PER SRM 57-43-02 FIGURE 202. REPAIRED DURING SHOP INSPECTION.May 2, 1995 · N651DL · Boeing 757232SDR DL757951968Te Wedge · delaminatedDURING SHOP INSPECTION, 757 SLAT PANEL WAS FOUND WITH DELAMINATION TO TRAILING EDGE WEDGE. REPLACED WEDGE PER SRM 57-43-02.May 2, 1995 · N651DL · Boeing 757232SDR DL757951906Te Wedge · dentedREPLACED TRAILING EDGE WEDGE ON NUMBER 9 LEADING EDGE SLAT AS PER SRM REF 57-43-02, DURING SHOP VISIT FOR HAIL DAMAGE.May 2, 1995 · N620DL · Boeing 757232SDR DL757951893Te Wedge · hail damageTHE BOEING 757 NR 2 LEADING EDGE SLAT RECEIVED CONSIDERABLE HAIL DAMAGE TO THE TRAILING EDGE WEDGE. THE SLAT WAS RECEIVED INTO THE SHOP AND THE WEDGE WAS REPLACED PER SRM 57-43-02 FIG 202.May 2, 1995 · N620DL · Boeing 757232SDR DL757951849Skin · delaminatedUPPER OUTBOARD SECTION OF TRAILING EDGE WEDGE DELAMINATED. LOWER SKIN OF TRAILING EDGE WEDGE PUNCTURED. REPLACED TRAILING EDGE WEDGE AS PER SRM 57-43-02. FOUND AND REPAIRED DURING SHOP INSPECTION.May 2, 1995 · N653DL · Boeing 757232SDR DL757951845Skin · dentedDURING INSPECTION, FOUND RT WING NR 9 L/E SLAT WEDGE UPPER SKIN DENTED BEYOND LIMITS. REPLACED WEDGE PER SRM 57-43-02.May 2, 1995 · N676DL · Boeing 757232SDR DL757951841Skin · dentedDURING INSPECTION, LEFT WING NR 2 L/E SLAT T/E WEDGE UPPER SKIN WAS FOUND WITH NUMEROUS DENTS. REPLACED WEDGE PER SRM 57-43-02.May 2, 1995 · N676DL · Boeing 757232SDR DL757951840Te Wedge · dentedDURING INSPECTION LEFT WING NR 3 L/E SLAT WAS FOUND WITH NUMEROUS DENTS ON UPPER SURFACE OF WEDGE. REPLACED T/E WEDGE PER SRM 57-43-02.May 2, 1995 · N676DL · Boeing 757232SDR DL72W951993Angle · crackedFOUND ON LTR CK, NR 8 SLAT ANGLE CRACKED JUST I/B OF I/B STOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.May 2, 1995 · N2814W · Boeing 727247SDR DL72E951892Slat · crackedFOUND ON CV2 CHECK, NR 7 L/E SLAT CRACKED BELOW TAI DUCT SLAT S/N 1172. REPAIRED PER M/M 57-54-0 PAR 5A P807A.May 2, 1995 · N830WA · Boeing 727247SDR CAL950372Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN NR 3 SLAT RIB INBOARD OF TRACK. THE CRACK WAS STOP DRILLED. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-6 AND 57-50-3. (M)May 2, 1995 · N66734 · Boeing 727224SDR CAL950371Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN NR 7 SLAT RIB AT OUTBOARD SIDE ON OUTBOARD TRACK. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-3 AND 57-50-3. (M)May 2, 1995 · N66734 · Boeing 727224SDR CAL950369Skin · crackedGSO - INSPECTION FOUND A .125 INCH CRACK IN THE NR 2 LEADING EDGE FLAP INNER SKIN UNDER ACTUATOR. A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW EC 5720-01064 AND SRM 51-30-2. (M)May 2, 1995 · N66734 · Boeing 727224SDR 95FDEA00499Bonding Strap · corrodedNR 1 K-FLAP O/B LOWER BONDING VAMPER UPPER ATTACH POINT IS CORRODED. CLEANED AND TREATED PER EWO NR 95-2426, CORROSION ON NR 1K-FLAP O/B LOWER BONDING VAMPER ATTACH POINT AS WELL AS FEDEX EA 7-5750-24438.May 2, 1995 · N144FE · Boeing 72721CSDR DL76S951867Skin · dentedNR 11 SLAT T/E WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER CMM 57-43-61.May 1, 1995 · N135DL · Boeing 767332SDR DL757951919Slat · dentedNR 7 SLAT HAIL DAMAGE. REPLACED T/E WEDGE PER SRM 57-43-02, DURING SHOP VISIT.May 1, 1995 · N620DL · Boeing 757232
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