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 UALA2009081802534Bolt · shearedNR 4 LEADING EDGE SLAT OTBD AUX TRACK GUIDE ROLLER BOLT SHEARED. REPLACED ROLLER AND BOLT AND ALL RELATED HARDWARE. INSPECTED AFT BOLT FOR NR 4 AUX TRACK. LEADING EDGE SLAT PANEL 521CB.SDR IPXA09557144Skin · chafedINSPECTION TYPE:C2 LEFT WING NR 3 SLAT LWR T/W WEDGE SKIN IS CHAFED, ABOVE INBOARD MAIN TRACK. MARKED WITH TAPE REPAIRED IAW SRM 51-70-10 2R.SDR FDEA200908163024Skin · damagedLEFT WING NR 8 SLAT INTERIOR SURFACE SKIN INBOARD TOP CORNER FOUND CHIPPED-OFF AT XOS 1005. CARRIED OUT REPAIR IAW SRM 57-40-01 FIG 201 REPAIR 3, REV 41. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR USAA2009090892407Slat · crackedCLT - Q3 - MAJOR REPAIR - CRACK ON NR 1 SLAT ON LOWER TRAILING EDGE. REPAIRED NR 1 SLAT ON LOWER TRAILING EDGE IAW B737 SRM 57-43-01 REPAIR 6.SDR SWAA095431Slat · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT NR 2 SLAT DELAMINATED. REPAIRED NR 2 SLAT PER SRM.SDR SWAA095341Wedge · delaminatedDURING SCHEDULED MV2 CHECK, FOUND LT WING NR 2 SLAT I/B TRAILING EDGE WEDGE DELAMINATED. REPAIRED WEDGE PER SWA EA.SDR USAA2009081792145Skin · debondedPHX - DVI - MAJOR REPAIR - DISBONDING SURFACE ON LEFT WING NR 5 SLAT UPPER SURFACE LEADING EDGE WEDGE AT PREVIOUS REPAIR LOCATION BETWEEN ISS152 TO ISS169. REPAIRED LEFT WING NR 5 SLAT UPPER SURFACE LEADING EDGE WEDGE BETWEEN ISS152 TO ISS169 IAW B757 SRM 51-SDR AALA20090814TUL02Rib · crackedRIGHT WING NUMBER 5 SLAT RIB IS CRACKED AT NUMBER 14 SLAT TRACK ATTACHMENT. REPLACED RIB UNDER SRM 57-50-13.SDR AALA20090814TUL01Rib · crackedRIGHT WING NUMBER 5 SLAT OUTBOARD RIB IS CRACKED AT NUMBER 15 SLAT TRACK ATTACHMENT. REPLACED RIB UNDER SRM 57-50-13.SDR FDEA200908132997Skin · misrepairedEXISTING EXTERNAL REPAIR DOUBLER FOUND AT RT WING NR 5 SLAT L/E EXTERIOR SKIN. EXISTING EXTERNAL REPAIR DOUBLER AT RT WING NR 5 SLAT L/E EXTERIOR SKIN EVALUATED AND FOUND NOT IAW SRM REPAIR. REPAIR CARRIED OUT IAW EA NR 1-5750-133822, TITLE: WINGS - FLIGHTSDR SWAA095248Skin · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA095230Wedge · delaminatedDURING SCHEDULED SPV CHECK, FOUND LT WING NR 3 SLAT T/E WEDGE UPPER SURFACE DELAMINATED. REMOVED AND REPLACED WEDGE PER SRM.SDR SWAA095219Skin · crackedDURING SCHEDULED 22Y CHECK, FOUND RT WING NR 6 L/E SLAT CRACKED AT I/B SIDE OF ACTUATOR. REPAIRED SLAT SKIN PER SRM.SDR UALA2009081302474Panel · damagedLEFT WING NR 5 LEADING EDGE SLAT HAS 2 SLAT CLOSURE PANELS WITH DAMAGE, 2ND FROM INBOARD PANEL HAS A 4 INCH CRACK THAT RUNS FROM THE AFT EDGE OF THE PANEL THROUGH 4 RIVET HOLES AND TERMINATES IN THE AFT HOLE, 3RD FROM INBOARD PANEL HAS SOME DELAM IN THE OUTBOASDR SWAA095267Skin · crackedDURING SCHEDULED 10Y CHECK, FOUND LT WING NR 4 L/E SLAT I/B END LOWER SKIN CRACKED. REPAIRED SKIN PER SRM.SDR SWAA095234Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT SKIN LOWER T/E CRACKED. REPAIRED SLAT SKIN PER SRM.SDR UIEA201000115Wedge · damagedLT WING INBD AFT FLAP LWR SURFACE T/E WEDGE FOUND HOLE AS MARKED. LTW AND INBD ALT FLAP LOWER SURFACE T/E WEIGHT REPAIRED IAW SRM 51-70-02. FIG 5 AND REF TO PROCESS CARD. CONTROL SEQ NO CHW 505020-1.SDR SWAA095181Skin · crackedDURING SCHEDULED 22Y CHECK, FOUND LT WING NR 2 SLAT L/E SKIN CRACKED. REPAIRED SKIN PER SRM.SDR FDEA200908102966Structure · damagedRH KRUEGER FLAP DAMAGED AT L/E AND TOP SKIN PANEL AFTER IMPACT WITH GROUND EQUIPMENT. KRUEGER FLAP TOP SKIN PANEL REPAIRED WITH AN EXTERNAL DOUBLER AS PER AIRBUS PROPOSAL. KRUEGER L/E SKIN REPLACED.SDR USAA2009090392344Slat · delaminatedSAL - Q6 - MAJOR REPAIR - DELAMINATION ON NR 2 SLAT 10 INCHES FROM OUTBOARD END OF TRAILING EDGE WEDGE AT SS246 TO SS254.5. REPAIRED NR 2 SLAT TRAILING EDGE WEDGE AT SS246 TO SS254.5 IAW B737 SRM 51-70-10.SDR USAA2009081892161Wedge · delaminatedSAL - Q6 - MAJOR REPAIR - DELAMINATION ON NR 2 SLAT TRAILING EDGE WEDGE AT INBOARD END BETWEEN SS124.4 TO SS130.4. REPAIRED NR 2 SLAT TRAILING EDGE WEDGE AT INBOARD END BETWEEN SS124.4 TO SS130.4 IAW B737 SRM 51-70-10.SDR AALA20090806TUL26Bushing · wornRIGHT NUMBER 5 SLAT INBOARD KNUCKLE FITTING WORN. REMOVED AND REPLACED BUSHINGS (272A103-1) ON RIGHT NUMBER 5 SLAT INBOARD KNUCKLE.SDR IPXA09M57234Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ 258-W4-01 RT NR 2 SLAT BETWEEN STA XIS 323-342 REPAIR DOUBLER NOT IN SRM. REMOVED EXISTING REPAIR FROM RT NR 2 SLAT LOWER SKIN BETWEEN XISS 325.37 0 AND 342.520. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF EO MD1 1-57SDR AALA20090805TUL14Rib · crackedHIGH FREQUENCY EDDY CURRENT- RIGHT WING NUMBER FIVE SLAT OUTBOARD SLAT RIB FITTING HAS CRACK INDICATION. REMOVED AND REPLACED NUMBER FIVE OUTBOARD SLAT RIB FITTING PER ESO 80117.SDR IPXA09M57244Skin · dentedINSPECTION TYPE:1C RT WING FIXED L/E SKIN DENTED AND CHIPPED AT CUTOUT FOR NR 1 SLAT TRACK. SLAT MUST BE EXTENDED. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW 57-40-02 REPAIR 7 SHT 2 AND 3.SDR IPXA09656992Support · crackedINSPECTION TYPE:C LEFT WING L/E LES 675 FIXED FAIRING SUPPORT AFT UPPER FRONT SPAR ANGLE FOUND CRACKED. CRACK LENGTH 0.75 INCH. LEFT WING L/E LES 675 FIXED FAIRING SUPPORT AFT UPPER FRONT SPAR ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 REVSDR SWAA095051Skin · crackedDURING SCHEDULED 12Y CHECK, FOUND LT WING NR1 SLAT SKIN CRACKED. REPAIRED SKIN PER SRM.SDR IPXA09657019Skin · crackedINSPECTION TYPE:C LEFT WING NR 4 SLAT O/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. LEFT WING NR 4 SLAT O/B AREA OSS641.6 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJSDR IPXA09657018Skin · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT O/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. LEFT WING NR 3 SLAT O/B AREA OSS792.25 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MASDR IPXA09657017Skin · crackedINSPECTION TYPE:C RIGHT WING NR 10 SLAT I/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. RIGHT WING NR 10 SLAT I/B AREA OSS 724.24 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MATERSDR IPXA09657016Skin · crackedINSPECTION TYPE:C RIGHT WING NR 9 SLAT I/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT I/B AREA OOS 573 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MASDR IPXA09657015Skin · crackedINSPECTION TYPE:C LEFT WING NR 4 SLAT I/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. LEFT WING NR 4 SLAT I/B AREA OSS 573 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR IS CLASSIFIED AS MAJOSDR IPXA09657006Skin · crackedINSPECTION TYPE:C LEFT WING NR 3 SLAT I/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. LEFT WING NR 3 SLAT I/B AREA OSS 724.24 NOSE SKIN REPAIRED AS PER SRM 57- 43-01-2R2 FIG 201, REV 44. THIS REPAIR CLASSIFIED AS MASDR IPXA09657005Skin · crackedINSPECTION TYPE:C RIGHT WING NR 9 SLAT O/B LOWER EXTERNAL SKIN RIVET HEAD SURROUNDING AREA FOUND CRACK. CRACK LENGTH 0.125 INCH. RIGHT WING NR 9 SLAT O/B AREA OSS 641.5 NOSE SKIN REPAIRED AS PER SRM 57-43-01-2R2 FIG 201 REV 44. THIS REPAIR CLASSIFIED AS MAJSDR IPXA09656989Panel · misrepairedINSPECTION TYPE:C RIGHT WING NR 7 SLAT CLOSURE PANEL I/B AREA THE EXISTING REPAIR PATCH NON-STANDARD REPAIR. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PAR 5H FIG 15 REV 44.SDR UALA2009080302333Structure · damagedLEFT WING METAL PROTRUDING 1 INCH BY 6 INCHES AFT OF SLAT. REMOVAL OF NR 2 LEFT SLAT COMPLETED UP TO STEP 11-L. REMOVED NR 2 SLAT UP TO STEP (12) (P/N 65C26602-223, S/N 957). SLAT IS ON GROUND PLANE SIDE. STARTED INSTALLATION OF NR 2 SLAT P/N 65C26602-301,SDR AALA20090803TUL01Rib · crackedHIGH FREQUENCY EDDY CURRENT INDICATES CRACKS ON RIGHT WING LEADING EDGE NUMBER FIVE SLAT AT BOTH OUTBOARD AND SECOND FROM OUTBOARD MOST SLAT RIBS. REPLACED BOTH NUMBER FIFTEEN OUTBOARD AND NUMBER FOURTEEN SECOND FROM OUTBOARD DAMAGED RIBS WITH NEW RIBS ON SLASDR IPXA09557040Doubler · missingINSPECTION TYPE:C1 RIGHT WING NR 9 SLAT UPPER SURFACE PREVIOUS REPAIR 24 INCHES FROM I/B EDGE AND 15 INCHES FROM LEADING EDGE IS MISSING REPAIR DOUBLER. REPAIRED PER SRM 51-70-10-2R3, SRM 51-70-10-2R.SDR USAA2009080492012Skin · delaminatedMCN - C22 - MAJOR REPAIR - DELAMINATION ON LOWER SKIN OF NR 3 SLAT WEDGE BETWEEN SLAT STATION 12 TO 19. REPLACED NR 3 SLAT WEDGE LOWER SKIN IAW B737 SRM 51-70-10-2R4 & 57-43-02-1A1.SDR ASAA0946344Wedge · chafedLEFT WING NR 3 L/E SLAT CHAFED AT I/B SIDE OF TRAILING EDGE WEDGE LOWER SFT CORNER. FABRICATED DOUBLER AND BONDED.SDR ASAA0946342Slat · delaminatedLEFT WING LEADING EDGE SLAT TRAILING EDGE WEDGE DELAMINATED AT O/B EDGE. FABRICATED DOUBLER AND BONDED.SDR C8GA20090232Skin · crackedWHILE IN HEAVY MX PERFORMING INSPECTIONS IT WAS NOTED THAT THE NR 3 SLAT INBD TRACK L/E CRACKED. STOP DRILLED CRACK, PERFORMED HFEC FOR VERIFICATION OF CRACK CONTAINMENT. FABRICATED REPAIR DOUBLER AND FILLER. INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ASDR C8GA20090231Skin · crackedWHILE IN HEAVY MX PERFORMING INSPECTIONS, IT WAS NOTED THAT THE NR 3 SLAT OTBD TRACK L/E CRACKED. STOP DRILLED CRACK, PERFORMED HFEC FOR VERIFICATION OF CRACK CONTAINMENT. FABRICATED REPAIR DOUBLER FROM .063" 2024 T3 DIM 10.5" X 9.250" AND FILLER FROM .063" SDR C8GA20090227AAngle · crackedWHILE IN HEAVY MX INSP IT WAS NOTED THAT THE NR1 K FLAP ACTUATOR INBD MOUNT ANGLE IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED NEW ANGLE FROM 2024 T3 DIM 8" X 3.5" .063", DOUBLER FROM 2024 T3 DIM 4.875" X 2" .125". INSTALLED REPAIR, NO OTHER DEFECTS WERE NOSDR C8GA20090216Skin · misrepairedWHILE IN HEAVY MAINTENANCE PERFORMING INSPECTIONS IT WAS NOTED THAT THE EXISTING REPAIR ON THE NR 6 SLAT I/B EDGE IS NON-COMPLIANT WITH SRM. REMOVED EXISTING REPAIR, FABRICATED REPAIR DOUBLER. INSTALLED REPAIR, NO OTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE.SDR USAA2009081792148Wedge · delaminatedSAL - Q6 - MAJOR REPAIR - DELAMINATION ON INBOARD END OF NR 5 SLAT TRAILING EDGE WEDGE BETWEEN SS123.4 TO SS124.4. REPAIRED INBOARD END OF NR 5 SLAT TRAILING EDGE WEDGE BETWEEN SS123.4 TO SS124.4 IAW SRM 51-70-10.SDR FDEA200907302847Skin · corrodedRT WING SLAT NR 7 T/E WEDGE TOP SKIN INTERNAL SURFACES FOUND WITH CORROSION AS MARKED. RT WING SLAT NR 7 REPAIRED IAW SRM 51-30-01 REV 97. REFER FORM 8130-3 TRACKING NR FA 2009/0327. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CITERIA.SDR FDEA200907302846Wedge · dentedMINOR DENT FOUND ON NR 7 SLAT UPPER SKIN AT OSS 333.3 AS MARKED. RT WING NR 7 SLAT T/E WEDGE REPLACED. REF TO FORM F8130-3 TRACKING NR SNF C187867 002. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200907302845Wedge · dentedMINOR DENT FOUND ON SLAT NR 7 UPPER SURFACE SKIN AT OSS 344.5 AS MARKED. RT WING NR 7 SLAT T/E WEDGE REPLACED. REFER TO REPAIR DIVISION FORM 8130-3 TRACKING NR NSF C187867 002. REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 CRITERIA.SDR FDEA200907302844Skin · corrodedRT WING SLAT NR 8 ANGLE FASTENER HOLES THRU ACCESS PANEL 623GB AT OSS 559.55 AND OSS 549.7 FOUND WITH MINOR CORROSION. SLAT NR 8 INTERIOR CORROSION AREA BETWEEN OSS 559.55 AND OSS 549.97 REPAIRED IAW SRM 51-10-02 REV 97. REFER TO FORM 8130-3 TRACKING NR FA 2
Back to JASC 5754