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"

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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.Dec 22, 1997 · N417DA · Boeing 727232SDR MWEA97877Vane · chafedDURING C CHK, FOUND RT WING NR 3 FLAP FIXED VANE LEADING EDGE CHAFFED AND GOUGED. MX REPAIRED IAW SRM 51-70-2.Dec 20, 1997 · N701ME · Doug MD88SDR 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 FIDec 20, 1997 · N403DA · Boeing 727232SDR DLL19972665Skin · crackedLT WING NR 4 SLAT UPPER SKIN CRACKED 4PLS SRM REPAIR REF 57-51-00 FIG808 MAJOR REPAIR.Dec 17, 1997 · N756DR · Lkheed 10113853SDR 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.Dec 17, 1997 · N615DL · Boeing 757232SDR 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.Dec 17, 1997 · N615DL · Boeing 757232SDR 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.Dec 17, 1997 · N526DA · Boeing 727232SDR DL72L972666Rib · crackedO/B ACTUATOR RIB CRACKED. REPAIRED RIB PER SRM 57-54-0.Dec 17, 1997 · N510DA · Boeing 727232SDR 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.Dec 16, 1997 · N515DA · Boeing 727232SDR 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.Dec 15, 1997 · N409DA · Boeing 727232SDR 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)Dec 13, 1997 · N315NE · Boeing 727223SDR DL72L972678Rib · crackedRIB NR 18 CRACKED. REPAIRED PER MM 57-54-0.Dec 13, 1997 · N510DA · Boeing 727232SDR DL72S972608Rib · crackedNR 2 L/E FLAP O/B ACTUATOR ATTACH RIB CRACKED. INSTALLED DOUBLER PER M/M 57-20-21 NR 12.Dec 11, 1997 · N8875Z · Boeing 727225SDR 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)Dec 11, 1997 · N14053 · Airbus A300B4605RSDR 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)Dec 9, 1997 · N610TW · Boeing 767231SDR 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.Dec 9, 1997 · N69736 · Boeing 727224SDR 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 ANDDec 5, 1997 · N209US · Boeing 737222SDR DL72S972540Stiffener · crackedA 1.5 INCH CRACK IN 2 EA SPAR STIFFENERS AT NR 6 SLAT OUTBD TRACK. REPAIRED PER MM 57-20-21.Dec 4, 1997 · N470DA · Boeing 727232SDR DL72S972538Skin · crackedA .25 INCH VISIBLE CRACK IN COVE SKIN ANGLE AT NR 1 SLAT I/B UPSTOP PAD. REPAIRED PER MM 57-54-0.Dec 4, 1997 · N470DA · Boeing 727232SDR 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.Dec 1, 1997 · N532DA · Boeing 727232SDR 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 INov 25, 1997 · N69736 · Boeing 727224SDR 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.Nov 24, 1997 · N153DL · Boeing 7673P6SDR 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.Nov 24, 1997 · N2821W · Boeing 727247SDR 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.Nov 24, 1997 · N401DA · Boeing 727232SDR 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.Nov 24, 1997 · N401DA · Boeing 727232SDR 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.Nov 24, 1997 · N401DA · Boeing 727232SDR 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 5Nov 24, 1997 · N401DA · Boeing 727232SDR 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.Nov 20, 1997 · N629DL · Boeing 757232SDR 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.Nov 17, 1997 · N8873Z · Boeing 727225SDR ABXA9701835Fitting · crackedDURING C-CHECK, FOUND RT WING NR 5 SLAT OUTBD FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-2.Nov 17, 1997 · N973AX · Doug DC941SDR 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.Nov 13, 1997 · N93738 · Boeing 727224SDR 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.Nov 12, 1997 · N467DA · Boeing 727232SDR 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.Nov 11, 1997 · N103CK · Lkheed 1011385115SDR 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 0Nov 11, 1997 · N103CK · Lkheed 1011385115SDR DL72L980045Rib · crackedTHIRD FROM OUTBOARD RIB CRACKED, REPAIRED PER M/M 57-54-00.Nov 10, 1997 · N507DA · Boeing 727232SDR 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.Nov 9, 1997 · N2813W · Boeing 727247SDR 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.Nov 4, 1997 · N791FT · Doug DC873FSDR 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. Nov 3, 1997 · N400DA · Boeing 727232SDR 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.Nov 3, 1997 · N400DA · Boeing 727232SDR DL72S972240Rib · crackedNR 2 SLAT RIB OUTBD OF ANTI-ICE DUCT CRACKED. REPAIR PER M/M 57-54-00.Nov 3, 1997 · N493DA · Boeing 727232SDR 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.Nov 3, 1997 · N533ND · Doug DC1030SDR 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)Oct 31, 1997 · N730AS · Boeing 737290CSDR 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.Oct 29, 1997 · N14524 · Doug DC932SDR 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.Oct 25, 1997 · N518DA · Boeing 727232SDR 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.Oct 25, 1997 · N518DA · Boeing 727232SDR DL72L972151Support · crackedFROM MV1C, NR 7 SLAT ACTUATOR O/B SUPPORT STRUCTURE CRACKED. REPAIR PER M/M 57-42-0.Oct 25, 1997 · N510DA · Boeing 727232SDR DL72K972145Rib · crackedFOUND ON B2 LETTER CK, NR 5 SLAT INBD AND O/B ACT ATTACH BRACKETS CRACKED. REPAIRED PER MM 57-54-0.Oct 24, 1997 · N414DA · Boeing 727232SDR 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)Oct 23, 1997 · N939AS · Doug DC983SDR 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.Oct 22, 1997 · N903UP · Boeing 72751CSDR 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 REOct 21, 1997 · N86426 · Boeing 727227
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