JASC 5754

Service difficulty reports · 17,348

Reports filed under 5754 · Leading Edge Devices, newest first.

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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"

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SDR DL757951855Skin · dentedDURING INSPECITON, RT WING NR 8 SLAT WAS FOUND WITH WEDGE UPPER SKIN DENTED BEYOND LIMITS. REPLACED WEDGE PER SRM 57-43-02.May 1, 1995 · N676DL · Boeing 757232SDR DL72S951838Web · crackedFOUND ON F1 LTR CK, NR 6 SLAT OTBD ACT ROD END WEB CRACKED AFT SIDE. REPAIRED PER M/M 57-54-0 PAR 3.May 1, 1995 · N490DA · Boeing 727232SDR DL76S952252Skin · damagedDURING SHOP INSPECTION, NR 9 L/E SLAT T/E WEDGE WAS REPAIRED FOR HAIL DAMAGE. REPAIRS ACCOMPLISHED PER SMR 57-43-55.Apr 30, 1995 · N135DL · Boeing 767332SDR DL76S951907Skin · dentedSLAT T/E WEDGE HAIL DAMAGED. REPAIRED PER CMM 57-43-61, FOR NR 3 L/E SLAT DURING SHOP VISIT.Apr 30, 1995 · N135DL · Boeing 767332SDR DL76S951885Wedge · dentedDURING INSPECITON NR 1 SLAT WEDGE WAS FOUND DENTED FROM HAIL. REPLACED WEDGE PER SRM 57-43-61.Apr 30, 1995 · N135DL · Boeing 767332SDR DL76S951884Te Wedge · dentedRT WING NR 7 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED WEDGE PER CMM 57-43-61.Apr 30, 1995 · N135DL · Boeing 767332SDR DL76S951882Te Wedge · damagedNR 5 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED T/E WEDGE PER CMM 57-43-61.Apr 30, 1995 · N135DL · Boeing 767332SDR DL76S951879Te Wedge · dentedNR 2 L/E SLAT FOUND TO HAVE DENTS APPARENTLY CAUSED BY HAIL. REPLACED TRAILING EDGE WEDGE AS PER CMM 57-43-61.Apr 30, 1995 · N135DL · Boeing 767332SDR DL76S951872Te Wedge · dentedRT WING NR 8 SLAT TRAILING EDGE WEDGE UPPER SURFACE DENTED. REPLACED TRAILING EDGE WEDGE PER CMM 57-43-61.Apr 30, 1995 · N135DL · Boeing 767332SDR DL757951967Skin · damagedDURING INSPECTION, NR 2 SLAT PANEL WAS FOUND WITH NUMEROUS DENTS IN T/E WEDGE DUE TO HAIL DAMAGE. REPLACED WEDGE PER SRM 57-43-002.Apr 30, 1995 · N676DL · Boeing 757232SDR DL757951877Skin · dentedNR 7 SLAT T/E HAS MANY DENTS. REPLACED T/E WEDGE PER SRM 57-43-02 FIG 202.Apr 30, 1995 · N676DL · Boeing 757232SDR DL757951874Wedge · dentedNUMBER 1 SLAT T/E WEDGE HAS MANY DENTS. REPAIRED PER SRM 57-43-02 FIGURE 202.Apr 30, 1995 · N676DL · Boeing 757232SDR DL757951859Wedge · dentedDURING INSPECITON, LEFT WING NR 5 L/E SLAT WEDGE WAS FOUND DENTED BEYOND LIMITS. REPLACED PER SRM 57-43-02.Apr 30, 1995 · N676DL · Boeing 757232SDR DL72S952484Ribs · crackedAT HMV, FOUND NR 5 L/E SLAT WITH 2 CRACKED RIBS INBD AND OTBD OF SLAT ACTUATOR ATTACH FITTING. REPAIRED PER SRM 57-54-0.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952111Ribs · crackedRIB CRACKED NR 2 SLAT O/B ACTUATOR MARKED NR 11 LOWER AFT CORNER. RIB CRACKED NR 2 SLAT I/B ACTUATOR MARKED NR 12 LOWER AFT CORNER. REMOVED DOUBLER AND INSTALLED NEW DOUBLER PER MM 57-54-0 FIG 805. REMOVED DOUBLER FABRICATED NEW DOUBLER PER MM 57-54-0 PAGE Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952086Rib · crackedAT HMV, FOUND NR 8 SLAT WITH CRACKED RIBS INBD OF TAI DUCT AND IB RIG AT W/P. REPAIRED PER SRM 57-54-0.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952084Rib · crackedAT HMV, FOUND NR 1 SLAT PANEL WITH CRACKED RIB JUST O/B OF ACTUATOR ATTACH FITTING. REPAIRED PER SRM 57-54-0 FIG 804.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952080Rib · crackedRIB CRACKED, NR 2 SLAT, RIB MARKED NR 10 CRACKED LOWER AFT CORNERBY N/P. REPAIRED PER MM 57-54-0 FIG 814.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952078Rib · crackedRIB CRACKED, NR 2 SLAT, RIB MARKED NR 8 CRACKED LOWER AFT CORNER BY N/P. REPAIRED PER MM 57-54-0 FIG 814.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952077Rib · crackedRIB CRACKED, NR 2 SLAT, RIB MARKED NR 19 CRACKED AT LOWER AFT END BY CUT OUT. REPAIRED PER MM 57-54-0 FIG 805.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952076Spar · crackedSPAR CRACKED, NR 8 SLAT-TOP I/B CORNER OF CUTOUT FOR TAI DUCT INSIDE OF SLAT, BN525. REPAIRED PER MM 57-54-0 FIG 802A.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952049Spar · crackedSPAR CRACKED, TOP I/B CORNER OF CUTOUT FOR TAI DUCT. NR 7 SLAT. REPAIRED PER MM 57-54-0 FIG 810. FOUND AT HMV.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952048Angle · crackedANGLE CRACKED, ANGLE BELOW TAI DUCT CRACKED AT BOTTOM OF CUTOUT FOR TAI DUCT. REPAIRED PER MM 57-54-0 FIG 805A, FOR NR 7 L/E SLAT AT HMV.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952047Rib · crackedRIB CRACKED, NR 6 SLAT RIB MARKED NR 11 CRACKED LOWER AFT CORNER BY N/P (1 RIB OUTBOARD OF ACTUATOR). REPAIR PER MM 57-54-0 FIG 814.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952046Rib · crackedRIB CRACKED, NR 6 SLAT-RIB MARKED NR 7 O/B OF TAI DUCT. REPAIR IS CRACKED AFT LOWER CORNER OF RIB. REPLACED REPAIR AS PER MM57-54-0 FIG 805. FOUND AT HMV.Apr 29, 1995 · N545DA · Boeing 727232SDR DL72S952001Rib · crackedRIB NR 19 CRACKED AND WAS REPAIRED PER M/M 57-54-0 FIG 814, FORNR #7 L/E SLAT, DURING SHOP INSPECTION.Apr 25, 1995 · N8875Z · Boeing 727225SDR DL72S952000Slat · crackedTHE TOP I/B CORNER OF THE ANTI-ICE DUCT CUTOUT IS CRACKED. REPAIRED PER M/M 57-54-0 FIG 801 FOR NR 7 L/E SLAT.Apr 25, 1995 · N8875Z · Boeing 727225SDR 95ZZZW658Slot Door · corrodedON 'A' CHECK, FOUND LEFT WING INBOARD SLOT DOOR HAS LEVEL II CORROSION AROUND FASTENERS HEADS AND INBOARD SIDE.Apr 25, 1995 · N1804 · Doug DC862SDR 95ZZZW657Slot Door · corrodedON 'A' CHECK, FOUND RIGHT INBOARD SLOT DOOR HAS LEVEL II CORROSION AT INBOARD AND OUTBOARD ENDS AROUND FASTENERS HEADS. (W)Apr 25, 1995 · N1804 · Doug DC862SDR 95ZZZM5Skin · creasedDURING ROUTINE MAINTENANCE CHECK, GROUND DAMAGE OCCURRED TO THE FOLDING NOSE SKIN OF THE NR 4 LEADING EDGE VARIABLE CAMBER FLAP. FLAP REPAIRED PER 747 SRM 57-50-03. REPAIR DEVIATED FROM SRM. DER APPROVED REPAIR FOR 50 HOUR LIMIT. FOLDING NOSE ASSY REPLACEDApr 25, 1995 · N832FT · Boeing 747121SDR 9507199977Fitting · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE NR 5 SLAT TO TRACK OUTBOARD ATTACH FITTING. REPLACED SLAT PER CITEXT 09-2782-1-9802.Apr 24, 1995 · N9341 · Doug DC931SDR UPS203065K Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 5 K-FLAP AND BULLNOSE. MAINTENANCE REMOVED AND REPLACE WITH A NEW K-FLAP AND BULLNOSE IAW OHM 20-50-01 AND MM 27-81-01.Apr 23, 1995 · N904UP · Boeing 72751CSDR UPS203049K-Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE OUTBOARD HINGE LOG OUTBOARD UPPER BOLT OF THE NUMBER 2 K-FLAP OUTBOARD BONDING JUMPER. MAINTENANCE REMOVED THE CORROSION THEN REPLACED THE K-FLAP IAW MM 27-81-01.Apr 23, 1995 · N920UP · Boeing 727180CSDR UPS203048K-Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND PITTING CORROSION ON THE ATTACH POINTS OF THE NUMBER 5 K-FLAP BULLNOSE. MAINTENANCE REMOVED AND REPLACED THE K-LFAP IAW OHM 20-50-03 AND MM 27-81-01.Apr 23, 1995 · N920UP · Boeing 727180CSDR UPS203047Hinge Fitting · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 4 K-FLAP ON ALL LUGS. MAINTENANCE REMOVED AND REPLACED CENTER HINGE FITTING IAW SRM 51-30-2, 51-30-8, 51-10-1 AND MM 27-81-01.Apr 23, 1995 · N920UP · Boeing 727180CSDR UPS203046K-Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 6 K-FLAP ON ALL LUGS AT FASTENER HOLES. MAINTENANCE REPLACED THE K-FLAP PER MM 27-81-01 AND OHM 20-50-02.Apr 23, 1995 · N920UP · Boeing 727180CSDR UPS203037K Flap · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 3 K-FLAP OUTBOARD LUG UPPER OUTBOARD BOLT HOLE. MAINTENANCE REMOVED THE OUTBOARD LUG UPPER INBOARD AND BOTH LOWER BOLT HOLES TO HAVE CORROSION AND FOUND TO BE OUT OF LIMITS. REMOVED CORRODED K-FLAP Apr 23, 1995 · N920UP · Boeing 727180CSDR UPS203024Lug · corrodedWHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON THE NUMBER 1 K-FLAP INBOARD BULLNOSE LINKAGE ROD LUG. MAINTENANCE BLENDED THE CORROSION AND REPLACED THE NUMBER 1 K-FLAP IAW SRM 57-50-1 AND MM 27-81-01.Apr 23, 1995 · N920UP · Boeing 727180CSDR UPS202960Flange · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND NR 2 K-FLAP O/B LOWER BONDING JUMPER HAS CORROSION ON BULLNOSE FLANGE. REPLACED PER MM 27-81-01.Apr 20, 1995 · N920UP · Boeing 727180CSDR UPS202959Rib · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND NR 2 K-FLAP I/B LOWER BONDING JUMPER HAS CORROSION ON RIB. REPLACED PER MM 27-81-01.Apr 20, 1995 · N920UP · Boeing 727180CSDR UPS202958Flange · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND NR 2 K-FLAP I/B LOWER BONDING JUMPER HAS CORROSION ON BULLNOSE FLANGE. REPLACED PER MM 27-81-01.Apr 20, 1995 · N920UP · Boeing 727180CSDR DL757951757Te Wedge · crackedTHE UPPER SKIN OF THE TRAILING EDGE WEDGE OF THE NR 5 L/E SLAT IS DELAMINATED AT ISS 109.00. THE DELAMINATION MEASURES 1 INCH ALONG THE EDGE OF THE PANEL AND PROGRESSES 0.25 INCH FORWARD FROM THE EDGE OF THE PANEL. DAMAGE FOUND AT LETTER CHECK, REPAIRS WERE Apr 20, 1995 · N604DL · Boeing 757232SDR DL72W951750Rib · crackedNR 13 RIB CRACKED AT LOWER ANGLE LOCATION. REPAIRED PER B-727 M/M 57-54-0 FIG 814, FOR RT WING NR 6 L/E SLAT. FOUND AT SHOP INSPECTION.Apr 20, 1995 · N2819W · Boeing 727247SDR DL72W951748Spar · crackedDURING SHOP INSPECTION, RT WING NR 6 L/E SLAT WAS FOUND WITH THE SPAR CRACKED AT THE CUTOUT FOR THE ANTI-ICE T-DUCT. REPAIRED PER MM 57-54-0 FIG 810.Apr 20, 1995 · N2819W · Boeing 727247SDR DL72W951746Rib · crackedDOUBLER FOR O/B ACTUATOR RIB CRACKED. REPLACED DOUBLER PER B-727 M/M 57-54-0 FIG 804, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION.Apr 20, 1995 · N2819W · Boeing 727247SDR DL72W951745Rib · crackedDOUBLER FOR I/B ACTUATOR RIB CRACKED. REPLACED DOUBLER PER B-727 M/M 57-54-0 FIG 804, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION.Apr 20, 1995 · N2819W · Boeing 727247SDR DL72W951744Angle · crackedRIB NR 11 CRACKED AT LOWER ANGLE. REPAIRED PER B-727 M/M 57-54-0 FIG 814, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION.Apr 20, 1995 · N2819W · Boeing 727247SDR DL72W951743Angle · crackedLOWER ANGLE CRACKED AT RIB NR 7 LOCATION. REPAIRED PER B-727 M/M 57-54-0 FIG 805A, FOR RT WING NR 6 L/E SLAT. FOUND DURING SHOP INSPECTION.Apr 20, 1995 · N2819W · Boeing 727247SDR DL72W951742Angle · crackedRIB NR 7 CRACKED AT LWR ANGLE. REPAIRED PER B-727 M/M 57-54-0 FIG 814, FOR RT WING NR 6 L/E SLAT DURING SHOP INSPECTION.Apr 20, 1995 · N2819W · Boeing 727247SDR DL72S951613Bracket · crackedNR 2 L/E FLAP I/B ACT ATTACH BRKT CRACKED UPPER AND LWR ENDS. FOUND DURING E-2 LTR CK. TPA MM. REPAIRED PER MM 57-20-21 PG 811.Apr 19, 1995 · N401DA · Boeing 727232
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