JASC 5730
Service difficulty reports · 27,262
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 FDEA202111102810Access Panel · crackedDURING HIGH FREQUENCY EDDY CURRENT SURFACE INSPECTION FOUND CRACK INDICATION APPROXIMATELY 0.2" IN LENGTH AT LEFT HAND WING CORNER NUMBER 5 SLAT ACTUATOR ACCESS DOOR AT FORWARD INBOARD CORNER AT STATION XOS 490.85. LEFT HAND WING CORNER NUMBER 5 SLAT ACTUSDR AALA202201079316Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TOP SKIN PANEL #2 AT WX 4010.2 BETWEEN RIB 6 AND RIB 9. REPAIRED SKIN PANEL PER EA EA 332257.SDR AALA202111307157Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE REAR SPAR UPPER SURFACE SKIN AT RIB 24. REPAIRED SKIN PER SRM 57-21-11-283-026 AND REPAIR INSTRUCTION R572-58998.SDR FDEA202111082906None · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON L/H WING LWR SURFACE L/E PANEL 513AB CUTOUT FWD O/B AREA POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FASDR FDEA202111082905None · unknownAIRCRAFT REPAIR ASSESSMENT :EXISTING EXTERNAL DOUBLER FOUND ON R/H WING LWR SURFACE L/E PANEL 613AB CUTOUT FWD O/B AREA POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA SDR AALA202111179801Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING UPPER TRAILING EDGE SKIN PANEL LOWER SURFACE AT WS 5512 AND RIB 10. REPAIRED SKIN PANEL PER EA 329846.SDR DALA2021111006933None · noneSHIP 6823 MIGRATED SHIM ON DRAG FITTING/FRONT SPAR OUTBOARD ID# 1D, AT LH ENG DRAG FTG CLAMP-UP. IN REF CARD 5720-01100-02A STEP 16. CORRECTIVE ACTION: SUMMARY OF NRC 00197 MIGRATED SHIM ON DRAG FITTING/FRONT SPAR OUTBOARD ID# 1D, AT LH ENG DRAG FTG WAS REPLACSDR DALA2021111006932None · noneSHIP 6823 A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP, SECTION 4, AS FOLLOW: HOLE #11 CORROSION ON FITTING AND SKIN, BTW 10 OCLOCK POSITION AND SCRATCHES ON SKIN BTW 7 TO 8 OCLOCK POSITION, HOLE #12 CORROSION ON FITTING AND SKIN, BTW 12 ASDR DALA2021111006931None · noneSHIP 6823 A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP, SECTION 4, AS FOLLOW: HOLE #12 CORROSION ON SKIN AND FITTING, BTW 7 AND 4 OCLOCK POSITION; HOLE #13 CORROSION ON SKIN AND FITTING, BTW 10 AND 2 OCLOCK POSITION; HOLE #14 CORROSION ON SDR DALA2021111006930None · noneSHIP 6823 A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP, SECTION 4, AS FOLLOW:HOLE #1 CORROSION ON SKIN, BTW 3 AND 5 OCLOCK POSITION AND SCRATCH ON SKIN BTW 7 OCLOCK POSITION, HOLE #2 CORROSION ON FITTING AND SKIN, BTW 1 AND 10 OCLOCK POSITSDR FDEA202111072791Former · crackedRIGHT HAND WING FIXED LEADING EDGE COMPARTMENT FORMER CRACKED AT STATION XOS 584. RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT CRACKED FORMER AT STATION XOS 584 REMOVED AND REPLACED AS PER SRM 51-31-01-OG . FORMER FABRICATED AS PER DOUGLAS DRAWING ARB2SDR DALA2021110906904None · noneSHIP 6823 A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP, SECTION 4, AS FOLLOW: HOLE #1 CORROSION ON SKIN AND FITTING, BTW 8 AND 5 OCLOCK POSITION; HOLE #2 CORROSION ON SKIN AND FITTING, BTW 12 AND 3 OCLOCK POSITION AND 11 OCLOCK POSITION; HSDR DALA2025102207740Skin · damagedREPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 595215-14. REPETIVE BHEC INSPECTION WAS PERFORMED PER AMDS 5720-0100-03A IN REF ER/A 595215-14AD REV B SECC IV DISCREPANCE SURFACE CONDITION FOUND ON FASSDR 2022F00114Skin · corrodedRT WING O/B L/E LWR SKIN HAS MULTIPLE AREAS OF CORROSION AT STA. XFS 566.250. REF NRC # B000092.SDR 2021F00332Skin · corrodedR/H WING L/E SKIN UPPER SURFACE BETWEEN STA XOLD 67.750 TO STA XW 485, HAS CORROSION ON EXISTING REPAIR DOUBLER. REF NRC B000104SDR 2021F00331Skin · corrodedRT WING UPPER FORWARD SKIN HAS CORROSION AT STA.XRS= 74.869. REF NRC B000098.SDR DALA2021110406800None · noneSHIP 1604 ON MEET AND GREET FOUND 0.40 INCH HOLE ON LT WING LOWER PANEL 511FB, CORRECTIVE ACTION: HOLE IS 0.40 INCHES IN DIAMETER . FWD TO MON PER B767-300 SRM 57 -20*-01-1A PROCEDURE 1. FIGURE 101 SHEET 3 H & J. INSPECT EVERY A CK AND REPAIR NO LATER THAN 120SDR EE4Y2021110314204Plate · corrodedLH WING FIXED TRAILING EDGE REAR FALSE SPAR OVERHANG WITH CORROSION BETWEEN WING RIB 7 AND 8. NOTE: THE TOP SKIN PANEL 2 WAS REPAIRED AS PER AIRBUS DOSSIER NO: 80981761 GUIDELÑINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2021-14151 INSTRUCTIONS (FOR SDR FDEA202111022721Doubler · unknownAGING AIRCRAFT - EXISTING BEADED DOUBLER REPAIR FOUND AT LEFT HAND WING FIXED LEADING EDGE INNER COMPARTMENT XOS 649. EXISTING BEADED DOUBLER REPAIR AT LEFT HAND WING FIXED LEADING EDGE INNER COMPARTMENT XOS 649 EVALUATED AND FOUND REPAIRED IN ACCORDANCE WSDR ASMF2021120800323Skin · dentedDENT ON LH WING FIXED LEADING EDGE SKIN.DURING TRANSIT CHECK, IT WAS DETECTED A DENT ON LH WING FIXED LEADING EDGE SKIN. MAINTENANCE PERSONNEL PERFORMED A REVISION, DETECTING A DENT OF 1.9" LENGTH, 1.022" WIDTH AND 0.051" DEPTH ON LH WING FIXED LEADING EDGE SKSDR FDEA202110312689Fitting · noneRIGHT HAND WING-OUTBOARD FLAP VANE ASSEMBLY. FITTING (E) ECCENTRIC HOLE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY FITTING (E) ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5. FIGURE 201. RESDR FDEA202110312688Fitting · noneRIGHT HAND WING-OUTBOARD FLAP VANE ASSEMBLY. FITTING (B) ECCENTRIC HOLE CORROSION. CORROSION AT RIGHT HAND WING - OUTBOARD FLAP VANE ASSEMBLY FITTING (B) ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5. FIGURE 201. OVSDR FDEA202110312687Fitting · noneLEFT HAND WING-OUTBOARD FLAP VANE ASSEMBLY. FITTING (D) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY FITTING (D) ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5. FIGURE 201. OVERSDR FDEA202110312686Fitting · noneLEFT HAND WING-OUTBOARD FLAP VANE ASSEMBLY. FITTING (C) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY FITTING (C) ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5. FIGURE 201. OVERSDR FDEA202110312685Fitting · noneLEFT HAND WING-OUTBOARD FLAP VANE ASSEMBLY. FITTING (E) ECCENTRIC HOLE CORROSION. CORROSION AT LEFT HAND WING - OUTBOARD FLAP VANE ASSEMBLY FITTING (E) ECCENTRIC HOLE REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 SRM 57-50-02-2R REPAIR 5. FIGURE 201. REPAIRSDR DALA2021110106710None · noneSHIP 3256 WEAR ON LOWER SKIN SLAT 2 IB POSITION ON LH WING. CORRECTIVE ACTION: PERFORMED REPAIR PER ER/A #594929-14 PRI REV.0 AND ER/A #594929-14 REV.ORIGINAL. (2001347)SDR AALA202111175160Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING UPPER SURFACE TRAILING EDGE SKIN PANEL #2 AT WS 3758 AND RIB 7 AT STIFFENER 5. REPAIRED SKIN PER EA 329847SDR IPXA2021110775670Doubler · puncturedINSPECTION TYPE:A300LT WING TOP SURFACE JUST FWD OF #1 SPOILER WING WING FIXED T/E PANEL PUNCTUREDREPAIRED PER SRM 57-51-12SDR IPXA2021110775669Doubler · puncturedINSPECTION TYPE:A300LT WING TOP SURFACE JUST FWD OF #1 SPOILER WING FIXED T/E PANEL PUNCTUREDREPAIRED PER SRM 57-51-12SDR LR7A2021091102980None · noneDURING SCHEDULED C-4 CHECK UNDER JOB CARD HC5701, FOUND CENTER WING SKIN CORRODED UNDER #2 BREAD PAN AT CWS178, FS579, WL256. / REPAIRED IAW LAC MEA 382-57-21-080. NR# 1000567514.SDR EE4Y2021102514137Plate · corrodedRH WING BETWEEN RIB #5 AND RIB #6 BOTTOM SKIN UPPER SURFACE WITH CORROSION. NOTE: THE BOTTOM SKIN PANEL 3 WAS REPAIRED AS PER AIRBUS DOSSIER NO: 80973153 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2021-14041 INSTRUCTIONS (FOR ADDTIONAL DETAISDR EE4Y2020110251413Plate · corrodedRH WING, TOP SKIN LOWER SURFACE OVERHANG WITH CORROSION BETWEEN RIB #7 AND RIB #9. NOTE: THE TOP SKIN PANEL 2 WAS REPAIRED AS PER AIRBUS DOSSIER NO: 80972366 GUIDELINES AS STATED IN COOPESA ENGINEERING ORDER NO: COO-EO-2021-14014 INSTRUCTIONS (FOR ADDITIONAL DSDR FDEA202110232597None · noneLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 731. LEFT HAND WING FIXED LEADING EDGE INTERNAL DOUBLER AT STATION XOS 731 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PERSDR FDEA202110232598None · noneRIGHT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 645. RIGHT HAND WING FIXED LEADING EDGE INTERNAL DOUBLER AT STATION XOS 645 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PSDR FDEA202110232596None · noneLEFT HAND WING FIXED LEADING EDGE INTERNAL BEADED DOUBLER FOUND CRACK AT STATION XOS 610. LEFT HAND WING FIXED LEADING EDGE INTERNAL DOUBLER AT STATION XOS 610 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJOR PESDR DALA2021102606635None · noneSHIP 6823 CORROSION ON FUEL ACCESS PANELS EXTERIOR SIDE 541MB AND 641MB. CORRECTIVE ACTION: SUMMARY OF NRC 00554: TANK ACCESS DOOR PANELS 541MB AND 641MB WERE REPLACED AND EFFECTIVITY WAS VERIFIED PER B757-200 IPC:28-11. (1992911)SDR IPXA2021102275212None · noneINSPECTION TYPE:SEG3LEFT WING DRY BAY PANEL 432FZ HAS EDGE DAMAGE.REPAIRED PANEL IAW B757 SRM 51-70-07-0G PER SRM 57-20-09-2R, FIG. 201, TABLE 1.SDR DALA2021102206574None · noneSHIP 187 CRACK FOUND ON THE END FITTING OF THE FRAME WHICH IS ATTACHED TO THE CENTER WING UP SURFACE AT STA927 S22R. CORRECTIVE ACTION: REPLACED THE FITTING ON THE CENTER WING UP SURFACE AT STA927 S22R AS PER B767-300 SRM51-40. (1992323)SDR DALA2021102106511Not Reported · not reportedSHIP 678 AD:A.A. DAMAGES WERE FOUND ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP & DIAG BRACE AS FOLLOW: HOLE #2 CORROSION ON SKIN AND FITTING BTW 1 TO 4 AND 8 TO 10 OCLOCK POSITION, HOLE #3 CORROSION ON SKIN AND FITTING BTW 9 TO 5 OCLOCK POSITION, HOLE #4 CORROSSDR DALA2021102006500Not Reported · not reportedSHIP 6816 LH ENG DRAG FTG CLAMP UP SECTION 04 DAMAGES FOUND ON OPEN HOLES AS FOLLOWS: HOLE#1 CORROSION ON SKIN BTW 5 -7 HRS POSITION; HOLE #2 CORROSION ON SKIN/FITTING BTW 4 - 1 CLOCK POSITION, GOUGE ON SKIN BTW 7 - 10 CLOCK POS, GOUGE ON FITTING BTW 12 - 2 CLSDR DALA2021102006499Not Reported · not reportedSHIP 6816 A.A. DAMAGES WERE FOUND ON OPEN HOLES AT RH ENG DRAG FTG CLAMP-UP, SECTION 4, AS FOLLOW: HOLE #2 CORROSION ON FITTING AND SKIN, BTW 2 AND 5 OCLOCK POSITION, HOLE #3 CORROSION ON SKIN AT 3 OCLOCK POSITION, HOLE #4 CORROSION ON FITTING AT 2 OCLOCK POSISDR FDEA202110192571Doubler · noneWORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00331 MAJOR REPAIR, REQUIRED INSPECTION ITEM, JOB PROGRESS FORM ITEMS 3 TO 4 AND 8 TO 11 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. EXISTING REPAIR REMOVED AT LEFT HAND WING FIXED LEADINSDR FDEA202110192570Doubler · unknownWORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00328 MAJOR REPAIR, REQUIRED INSPECTION ITEM, JOB PROGRESS FORM ITEMS 4 TO 5 AND 7 TO 10 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. EXISTING DOUBLER REMOVED AS PER SRM 51-33-01-0G AT LEFSDR FDEA202110192569Doubler · unknownWORK ORDER 69707 SPECIAL/NONROUTINE MAINTENANCE FORM NUMBER N00585 MAJOR REPAIR, REQUIRED INSPECTION ITEM, JOB PROGRESS FORM ITEMS 2 TO 6 DO NOT HAVE REQUIRED INSPECTION ITEM BLOCK MARKED. REMOVED EXISTING DOUBLER AT LEFT HAND WING FIXED LEADING EDGE LOWESDR DALA2021101906439None · noneSHIP 3265 ELONGATED HOLE FUEL TANK BOTTOM SKIN BTW RIB 18 AND RIB 19 ON RH WING. CORRECTIVE ACTION: PERFORMED REPAIR ON HOLE FUEL TANK BOTTOM SKIN PER A320 SRM 57-21-11. (1988130)SDR FDEA202110172556Doubler · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER CRACKED AT STATION XOS 498. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT STATION XOS 498 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS SDR IPXA2021103075465Doubler · crackedINSPECTION TYPE:4CRT WING FIXED L/E SKIN SPLICE DOUBLER IS CRACKED O/B OF #12 SLAT TRACK.REMOVED AND REPLACED CRACKED RT WING FIXED L/E SKIN SPLICE DOUBLER O/B OF #12 SLAT TRACK IAW SRM 51-33-01. (MINOR)SDR IPXA2021102975443Doubler · crackedINSPECTION TYPE:4CRT WING FIXED L/E SKIN SPLICE DOUBLER IS CRACKED O/B OF SLAT TRACK #10.REMOVED AND REPLACED CRACKED RT WING FIXED L/E SKIN SPLICE DOUBLER O/B OF SLAT TRACK #10 IAW SRM 51-33-01. (MINOR)SDR DU4R2021102100097None · corrodedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H WING OB JACK POINT HAS CORROSION AT REAR SPAR AND LOWER SKIN LAYERS. S/O 193125 N/R 008838651 / 32087SDR DALA2023110209030Unknown · unknownAIRCRAFT 3714, DURING HCK AT QRO, A CRACK WAS FOUND EMANATING FROM A FASTENER HOLE OF RH WING SURFACE, STA 553, S-9R. AFFECTED ELEMENTS ARE SKIN 112A4102-208 (M/F 2324-T39 MACHINED PLATE PER BMS 7-254) & STRINGER 112A4205-208 (M/F 2224-T3511 EXTRUSION PER BMS
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