JASC 5754
Service difficulty reports · 17,344
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 SWAA022198Wedge · delaminatedDURING SCHEDULED D CHECK, FOUND NR 5 L/E SLAT WEDGE DELAMINATED AT BOTH INBD AND OTBD ENDS. REPAIRED NR 5 L/E SLAT WEDGE PER MM.SDR GTIA021123Skin · crackedRIGHT NR 1 SLAT OUTBOARD LEADING EDGE METAL STRIP UPPER SIDE IS CRACKED. FORMED NEW MATERIAL STRIP, INSTALLED NEW SLAT METAL STRIP.SDR ASAA0240117Skin · delaminatedPAE - DURING C-CHECK, FOUND LEFT NR 2 SLAT UPPER AND LOWER TRAILING EDGE WEDGE SKIN IS DELAMINATED AT OUTBOARD END. REPAIRED IAW SRM. (M)SDR ASAA0240113Skin · crackedPAE - DURING C-CHECK, FOUND NR 6 SLAT EXTERNAL SKIN IS CRACKED ON LOWER L/E AT FASTENERS AT OUTBOARD END. REPAIRED IAW SRM. (M)SDR GTIA021058Rib · crackedLT WING UNDERSIDE OF NR 3 SLAT ACCESS AREA, RIB CRACKED AT FIXED LEADING EDGE, STA XRS 267. FABRICATED FILLERS AND REPAIR ANGLES/DOUBLERS STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER ON RIB.SDR GTIA021057Skin · crackedLEFT WING, NR 5 SLAT, EXTREME OUTBOARD END CAP, UPPERSIDE CRACKED NEXT TO RIVETS. LOCATED, DRILLED AND DEBURRED REPAIR PART INSTALLED REPAIR PART.SDR DL76L021055Beam · damagedNR 5 LEADING EDGE SLAT NOSE BEAM WAS FOUND DAMAGED. DAMAGE CONSISTED OF THE NOSE BEAM WEB BEING SEVERED ON OSS481. REPAIRED PER ER/A 417610-14.SDR GTIA020972Horn · dentedRIGHT SLAT 0 HAS 2 DENTS IN LEADING EDGE. NR 1 15 INCH FROM INBOARD END. NR 2, 18 INCH FROM INBOARD END. SKIN HAS SCRATCHES BETWEEN THE 2 DENTS. REMOVED RIGHT WING SLAT HORN. INSTALLED RIGHT WING SLAT HORN NUMBER ZERO SLAT.SDR 2002UALA01702Skin · delaminatedLOWER SURFACE DELAMINATED ON WEDGE T/E INBOARD END. SKIN REPAIRED/REPLACED PER AUTOCLAVE REPAIR.SDR 2002UALA01700Skin · delaminatedDELAMINATED TRAILING EDGE WEDGE SKIN. SLAT 1A. SKIN REPAIRED/REPLACED PER AUTOCLAVE REPAIR.SDR F3LA200200253Skin · crackedDURING C-2 CHECK, INSPECTION REPORTED LT WING NR 1 SLAT LOWER SKIN CRACKED AT LAST ROW OF RIVETS, OUTBOARD OF MAIN TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER SRM 57-43-01.SDR CALA0200445Skin · crackedINSPECTION FOUND A 2" CRACK IN #6 LEADING EDGE SLAT SKIN AT EDGE OF RIVET HOLE ON SLAT LOWER SIDE BY I/B AUX TRACK. A REPAIR WAS INSTALLED IAW SRM 57-43-01, FIGURE 206.SDR SWAA021950Slat · crackedDURING SCHEDULED C4 CHECK, FOUND NR 3 L/E SLAT CRACKED IN AFT ROW OF RIVETS. REMOVED AND REPLACED NR 3 L/E SLAT PER MM.SDR 2002F01002Structure · damagedHOLE IN 7 RT SLAT OUTBD END LOWER SIDE. REPAIRED AREA IAW SRM 57-51-00. WING STATION, FROM OWS 464.5 TO OWS 464.5SDR AWXA200200794Structure · brokenUNCOMMANDED FLT INPUT - ON APPROACH AFTER FLAPS SELECTED TO 30 DEG ACFT ROLLED HARD LT, REQUIRED ALMOST FULL RT AILERON TO KEEP STRAIGHT & LEVEL. SELECTED FLAPS TO 40 DEG & PROBLEM REMAINED, LANDED UNEVENTFULLY. MX PERFORMED VISUAL INSPECTION OF WINGS AND FSDR GTIA020971Skin · dentedFROM CARRY OVER LIST, 3 DENTS ON NR 2 SLAT R WING, 1ST DENT XOS 204 DEPTH .016, 2ND DENT XOS 235 DEPTH .039, 3RD DENT XOS 264 DEPTH .019. ALL THREE DENTS ARE OUT OF LIMITS, REPAIRED DENTS.SDR SWAA021903Slat · crackedDURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT CRACKED AT INBD MAIN TRACK CUTOUT ON T/E ROW OF RIVETS. REPAIRED SLAT PER SRM.SDR F3LA200200220Skin · crackedDURING C-7 CHECK, INSPECTION REPORTED LT WING NR 1 SLAT LOWER SKIN CRACKED AT LAST ROW OF RIVETS I/B OF CENTER AUX TRACK. FABRICATED AND INSTALLED REPAIR PER SRM 57-43-01.SDR SWAA021886Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND NR 1 L/E SLAT LOWER SKIN CRACKED AT AFT FASTENERS NEAR OTBD END. REPAIRED SKIN PER SRM.SDR SWAA021897Slat · delaminatedDURING SCHEDULED 1/2D CHECK, FOUND NR 5 L/E SLAT DELAMINATED AT T/E OTBD END. REPAIRED NR 5 L/E SLAT PER SRM.SDR UPS02239168Skin · crackedINSPECTION TYPE:C CRACK IN ANTI-ICE SKIN AT 5TH BAY O/B ON NO.4 KRUEGER FLAP. ANTI-ICE SKIN FOUND TO BE OUT OF LIMITS IAW SRM ADDENDIUM EO NO. B72 7-5750-3082-D. ANTI ICE SKIN REPLACED IAW DRAWING NO.65-16225 + SRM 51-30-02.SDR UPS02239166Skin · crackedINSPECTION TYPE:C #3 LE FLAP ANTI-ICE SKIN CRACKED AT MIDDLE O/B RIVET 3RD BAY FROM O/ B REPAIR CARRIED OUT IAW SRM ADDENDUM EO # B727-5750-3082SDR UPS02239165Skin · crackedINSPECTION TYPE:C RIVET PULLED THROUGH ANTI-ICE SKIN AT #4 KRUEGER FLAP AT 8TH BAY O/B SKIN REPAIRED IAW SRM ADDENDUM EO # B727-5750-3082SDR SWIA200211227Frame · crackedRIGHT INBOARD LEADING EDGE INBOARD FRAME CRACKED, MARKED. DISCOVERED DURING C-CHECK. REPLACED RIGHT INBOARD LEADING EDGE FRAME.SDR AWXA200200771Slat · delaminatedLCQ - MAJOR REPAIR - APPROXIMATELY 12" OF TRAIL EDGE WEDGE HAS SKIN AND CORE DAMAGE ON # 6 LEADING EDGE SLAT. REMOVED #6 LEADING EDGE SLAT; CLEANED, PREPARED, AND REPLACED TRAILING EDGE WEDGE IAW E.O. 57-55-10. REINSTALLED # 6 LEADING EDGE SLAT IAW BMM 27-81-SDR AMTA200201018Rib · cracked6R SLAT INBOARD RIB CRACKED AT AFT END CRACK LENGTH 0.500.SDR ABXA030222Structure · corrodedLT WING LEADING EDGE UPPER SECTION APPROXIMATELY, STA. XFS 126.250, CORROSION AROUND FASTENERS. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. REPAIRED IAW REA D857-43958MR.SDR AMTA200200997Rib · cracked6R SLAT 4TH RIB OUTBOARD FROM INBOARD END CRACKED.SDR AMTA200200998Rib · cracked6R SLAT 4TH RIB OUTBOARD FROM INBOARD END CRACKED.SDR CA020802001Slat · separated(CAN) ON APPROACH, LT INBD. FORE FLAP SEPARATED FROM A/C. AFTER LANDING,DISCOVERED THE A/C HAD LOST THE LT FOREFLAP TRAILING EDGE. (APPROX. 8FT) THE SEPARATED SECTION TRAVELLED AFT, AND CONTACTED THE NR 1 ENGINE INLET COWL AND FORWARD PYLON LEADING EDGE. SCUSDR C2XA02TY114Skin · dentedTYS, DURING A SCHEDULED INSPECTION THE LEFT, NR 2 LEADING EDGE WAS FOUND DENTED AROUND A SCREW HOLE ON THE LOWER CENTER SIDE. MAINTENANCE REPAIRED THE DENT IAW-EMB-GST2378/02, THE REPAIR WAS SATISFACTORY AND THE AIRCRAFT WILL BE RELEASED UPON COMPLETION OF THSDR CA020726021Bracket · cracked(CAN) DURING A ROUTINE STRUCTURAL INSPECTION A CRACK WAS FOUND IN THE NR 3 LEADING EDGE SLAT ACTUATOR INBOARD WING ATTACH FITTING. THE CRACK WAS FOUND ON A VISUAL INSPECTION AND CONFIRMED TO BE 3/4 OF A INCH USING NDT. THERE IS NO ALLOWABLE REPAIRS FOR THIS BRSDR 2002UALA01248Filler · missingAT C-CHECK MAINTENANCE, UAL DISCOVERED 20 INCHES OF OUTBOARD END OF FILLER WAS MISSING FROM THE NR 1 SLAT SEAL. THIS FILLER WAS INSTALLED PER THE MANUFACTURER. SUPPLEMENTAL DATA UPDATE UAL SUSPECTS THAT TENSION WAS INDUCED DURING THE INSTALLATION OF THE BULSDR AUS20020740Skin · delaminated(AUS) NR 3, NR 6 AND NR 9 LEADING EDGE SLATS DELAMINATED IN AREA OF AFT WEDGES. FOUND DURING INSPECTION IAW AD/B767/73.SDR DL72S020846Spar · crackedAT F-I LETTER CK FOUND .375 INCH CRACK NR 2 SLAT AT TAI DUCT CUTOUT, INBOARD CORNER. REPAIRED PER M/M 57-54-000-8 FIG 802A.SDR AAL2004F00002Rib · corrodedKRUEGER FLAP JACK RIB HORIZONTAL SUPPORT FITTING CORRODED ON AFT SIDE BETWEEN ACT ATTACH POINTS. REMOVED CORROSION, TREATED IAW ESO 30595.SDR GTIA020943Skin · damagedFTW - RIGHT LEADING EDGE SLAT NR 5 DAMAGED TO APPROX 6 INCHES FROM OUTBOARD TIP, TEMPORARY REPAIR INSTALLED. REMOVED RIGHT LE NR 5 SLAT. REMOVED INNER SKIN AND CRACKED RIB. FORMED NEW RIB. INSTALLED RIB AND INNER SKIN. (M)SDR UPS02638751Skin · crackedINSPECTION TYPE:N/A NR 7 SLAT LEADING EDGE INBD CORNER CRACKED. REMOVED AND REPLACED NR 7 SLAT INBD BOTTOM SKIN PER SRM 51-10-02 & SRM 51-40-02, OPS CHK LEADING EDGE SLAT PER MM 27-81-00.SDR DHL2002806845Fitting · crackedLT WING INBOARD SLOT ZEE PAN FITTING CRACKED 2 INCHES XS 250.000. REMOVED ZEE PAN FITTING IAW SRM 51-1-20D PG 21, PERFORMED ANTI CORROSIVE TREATMENT AND PRIMED EFFECTED AREA IAW SRM 51-1-8B, INSTALLED ZEE PAN FITTING IAW SRM 51-1-20D PAGE 9.SDR SWAA021485Slat · delaminatedDURING SCHEDULED RON, FOUND NR 3 LT L/E SLAT DELAMINATED ON UPPER INBD SURFACE. REMOVED AND REPLACED NR 3 LT L/E SLAT PER MM.SDR DHL2002754001Slat · bird strikeRTO DUE TO MULTIPLE BIRD STRIKES, RETURN TO BLOCKS FOR INSPECTION. PERFORMED BIRD STRIKE INSPECTION PER MM 05-51-41. NO DAMAGE OR STRIKE IN ENGINES. SOME STRIKES ON LEADING EDGE. NO DAMAGE A/C. OKAY FOR SERVICE.SDR CA020705003Panel · damaged(CAN) DURING WEEKLY CHECK, NR 2 RT SLAT ACTUATOR PANEL ASSY. FOUND DAMAGED. PART OF THE COMPOSITE PANEL WAS MISSING. AIRCRAFT WAS AOG. THE PANEL WAS FLOWN IN. MAINTENANCE REPLACED THE PANEL I.A.W. AMM 57-40-00.SDR AWXA200200669Skin · delaminatedDURING C-14 CHECK DELAMINATION WAS FOUND ON THE OUTBOARD TRAILING EDGE OF THE NR 2 SLAT. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED A DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW B737-300 SRM 51-70-10, FIG 13.SDR DHL2002806513Skin · crackedFOUND AT C-CHECK, LT INBOARD SLOT L/E INTERNAL SKIN CRACKED 4 INCHES AT STA XFS 250.000. PERFORMED MAJOR REPAIR PER SRM 57-3-3 PG 9-11. REMOVED DAMAGED SKIN PER SRM 51-1-21 PG 1. FABRICATED NEW SKIN PER SRM 57-3-3 PG 9-11. INSTALLED NEW INTERNAL SKIN PER SSDR COOSDR020192Structure · delaminatedRIGHT WING OUTBOARD FORE FLAP (PN 65-21631-274) (SN BN386) UPPER SKIN AND HONEYCOMB CORE DELAMINATED SECTION.SDR COOSDR020191Structure · delaminatedLEFT WING INBOARD FORE FLAP (PN 652130-188) (SN BN720) UPPER, LOWER SKIN AND HONEYCOMB CORE DELAMINATED SECTION.SDR DHL2002806519Structure · damagedDURING C-CHECK, FOUND LT WING I/B SLOT UPPER SURFACE SKIN HOLES ELONGATED XS 250.000. CUT OUT DAMAGED AREA. FABRICATED DOUBLERS AND FILLER PER EODHL020606, EO-3088, EO SEMAN2002671. INSTALLED FILLERS AND DOUBLERS PER EODHL020606, EO-3088, EO SEMAN2002671.SDR UPS02239013Structure · crackedINSPECTION TYPE:C PLS CARRY OUT PERMANENT REPAIR TO NR 2 L/E SLAT DENT (APPROX 1.5 FT O/B OF ACTUATOR). PERMANENT REPAIR CARRIED OUT ON NR 2 L/E SLAT IAW SRM 57-50-03 FIG 1.SDR DHL2002806514Structure · damagedDURING C-CHECK, FOUND RT INBOARD SLOT WITH ELONGATED HOLES AT STA XFS 250.000. TRIMMED OUT DAMAGED AREA. FABRICATED DOUBLERS AND A FILLER PER EODHL020620, EO3093, EO SEMAN 2002682. INSTALLED FILLER AND DOUBLER PER EODHL020620, EO3093, EO SEMAN 2002682.SDR 2002UALA01183Filler · missingSLATS NR 1 & 14 FILLERS WERE MISSING FROM SPANWISE BULB SEALS. MAJOR REPAIR ACCOMPLISHED. FILLERS INSTALLED.
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