JASC 5730
Service difficulty reports · 27,269
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 ASOA2013071708713Skin · crackedLT FUEL ACCESS HOLE 540EB FAILS NDT WITH AN INDICATION ON INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.SDR ASOA2013071708712Skin · crackedRT FUEL ACCESS HOLE 650CB FAILS NDT WITH INDICATIONS GREATER THAN 50 PERCENT SCREEN HEIGHT ON FWD SIDE OF HOLE. REPAIRED IAW REO 601R-57-21-030, REV J.SDR ASOA2013071708711Skin · crackedRT FUEL ACCESS HOLE 650DB FAILS NDT WITH INDICATIONS ON FWD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.SDR ASOA2013071708710Skin · crackedRT FUEL ACCESS HOLE 640DB FAILS NDT WITH AN INDICATION ON INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.SDR ASOA2013071708709Skin · crackedRT FUEL ACCESS HOLE 650BB FAILS NDT WITH AN INDICATION ON FWD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.SDR ASOA2013071708708Skin · crackedRT FUEL ACCESS HOLE 650AB FAILS NDT WITH AN INDICATION ON FWD INBD SIDE OF HOLE GREATER THAN 50 PERCENT SCREEN HEIGHT. REPAIRED IAW REO 601R-57-21-030, REV J.SDR ASOA2013070308555Panel · dentedRT WING L/E DENTED. REMOVED R/T OTBD L/E ASSY IAW AMM 57-41-01-000-806 AND ACCESS PANEL 630BL IAW TASK 57-41-01-000-808. INSTALLED OTBD L/E ASSY QC 44 (630KL) IAW AMM 57-41-01-400-806. RECEIVED SERVICEABLE LEADING EDGE PN 601R12062-4 LOCATED AND TRANSFERESDR DALA13028321402Skin · crackedNR 2 PYLON, CRACK INDICATION FOUND ON RT UPPER WING SKIN LOAD FITTING AT MOST OTBD AFT FASTENER HOLE. WORK CARRIED OUT IAW PRI 514654-14AD, REV 0, REV 1 AND REV 2 AND REV 3.SDR ABXA20130605440Skin · corrodedCORROSION AT FASTENERS AND AFT SKIN EDGE OF LT WING UPPER SKIN WS 798. REMOVED CORROSION IAW SRM 57-20-01, DETAIL I AREA WAS REPAIRED ON REA NR B657-60562.SDR ABXA20130605438Skin · corrodedCORROSION ON LT UPPER WING SURFACE LOCATED AT REAR SPAR APPROX WBL 710. REMOVED CORROSION IAW SRM 57-20-01, DETAIL I AREA WAS REPAIRED ON ABX REA NR B657-60562-MR; ACFT WAS GROUNDED.SDR DALA13027221402Skin · corrodedFOUND ON RT WING UPPER SURFACE, WITHIN FILLET AREA AT WBL 102 TO WBL 106 AND 11" FWD OF RT WING REAR SPAR. REPAIR COMPARED AND COMPLIED WITH FINAL ER/A 514645-14.SDR DALA13027211402Skin · corrodedRT WING UPPER FILLET AREA-CORROSION FOUND ON WING UPPER SURFACE BELOW BRACKET, WITHIN FILLET AREA AT WBL 101 TO WBL 102.5 AND FWD OF RT WING REAR SPAR 22.5" TO 23.5". REPAIR CARRIED OUT IAW PRI 514645-14.SDR ASOA2013062403901Skin · corrodedRIGHT WING PLANK ACCESS HOLE FOR PANEL 640BB HAS AREAS OF PITTING. REPAIR IS CLASSIFIED AS MAJOR REPAIR. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV J.SDR ASOA2013062403900Skin · corrodedRIGHT WING PLANK ACCESS HOLE FOR PANEL 610AB HAS AREAS OF PITTING. REPAIR IS CLASSIFIED AS MAJOR. REPAIRED IAW EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV J.SDR ASOA2013062403899Skin · corrodedLEFT WING PLANK ACCESS HOLE FOR PANEL 540BB HAS AREAS OF PITTING. REPAIRED IAW EC/TC EO 600-57-81 C/W IAW REO 601R-57-21-030, REV J. REPAIR CLASSIFIED AS MAJOR.SDR IPXA13M78932Doubler · crackedINSPECTION TYPE:1C, RT WING BEADED DOUBLER CRACKED NEAR XOS 634. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 633-648 IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA13M78862Skin · crackedINSPECTION TYPE:2C, RT WING L/E IS CRACKED ON PANEL SUPPORT AT STA XOS 547. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PANEL SUPPORT RT WING L/E IAW SRM51-33-01, 51-35-01, AND DWG ARB2933.SDR DALA13028231402Skin · corrodedLEFT WING UPPER FILLET AREA-CORROSION FOUND ON LT WING UPPER SURFACE AT WBL 101 TO WBL 104.5 AND FWD OF LT WING REAR SPAR 14" TO 18.5" AS MARKED. REPAIR CARRIED OUT IAW ER/A 514644-14, REV ORIGINAL.SDR DALA13028221402Skin · corrodedCORROSION FOUND LT WING UPPER SURFACE AT WBL 101.5 TO WBL 104.5 AND 8.5 INCHES TO 12 INCHES FWD OF LT WING REAR SPAR CORRODED AREA. REPAIR CARRIED OUT IAW PRI 514644-14, REV 0.SDR ASOA2013060603773Skin · burnedLEFT WING LOWER WING PLANK HAS LIGHTNING BURN AT OTBD AFT SKIN EDGE OF FUEL TANK ACCESS PANEL 610AB CUTOUT. BLENDED BURN ON LT WING LOWER WING PLANK REF SRM 51-12-00. DETERMINED TO BE OUT OF LIMITS (LIGHTNING STRIKE NOT ALLOWED TO WING PLANK). ROTO-PEENEDSDR DALA13027443753Panel · crackedDURING INSPECTION, FOUND LT WING UPPER T/E PANEL BY DEFLECTOR RIB CENTER ANGLE CRACKED. MX R & R LT WING DEFLECTION RIB UPPER PANEL CENTER ATTACH ANGLE IAW SRM 51-40-02, PG 1-4 AND IPC 57-50-00-25.SDR DALA13027201402Skin · corrodedLT WING UPPER FILLET AREA-CORROSION FOUND ON LT WING UPPER SURFACE BELOW BRACKET, AT WBL 101 TO WBL 103.5 AND FWD OF LT WING REAR SPAR 22" TO 24". REPAIR CARRIED OUT IAW PRI 514644-14, REV 0 AND REV 1.SDR FDEA201306041188Skin · corrodedLT WING T/E LOWER ACCESS PANEL 541JB CUTOUT FORWARD EDGE LOWER CAP SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5710-T0300678A, PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR ASOA2013071708707Skin · corrodedLEFT WING LOWER WING PLANK ACCESS HOLE AT WS 54.897, HOLE NR 1 AT PANEL LOCATION 540BB HAS PITTING CORROSION AT FORWARD AND AFT ENDS IN THE CRITICAL REGIONS. DEEPEST AREA IS APPROXIMATE .003" DEEP. REPAIRED IAW REO 601R-57-21-030.SDR SWIA201333818Cleat · crackedTWO CRACKED SKIN CLEATS IN LT WING BETWEEN NR 4 & NR 5 FUEL CELLS UPPER. C-CHECK TWO NEW SKIN CLEATS INSTALLED ON LT WING BETWEEN FUEL PANELS NR 4 & NR 5 IAW AMM.SDR SWIA201333817Cleat · crackedCRACKED SKIN CLEAT IN LT WING NR 5 FUEL CELL UPPER INBD. C-CHECK NEW SKIN CLEAT INSTALLED ON LT WING AT NR 5 FUEL CELL UPPER INBD IAW SRM.SDR SWIA201333816Cleat · crackedCRACKED SKIN CLEAT IN LT WING NR 4 FUEL CELL OTBD UPPER FORWARD. C-CHECK NEW SKIN CLEAT INSTALLED ON LT WING OTBD UPPER FORWARD NR 4 FUEL PANEL IAW SRM.SDR SWIA201333815Cleat · crackedCRACKED SKIN CLEAT LT WING NR 3 FUEL CELL OTBD LOWER. C-CHECK NEW SKIN CLEAT INSTALLED ON LT WING NR 3 FUEL CELL OTBD LOWER IAW SRM.SDR SWIA201333814Cleat · crackedRT WING NR 5 FUEL PANEL UPPER OTBD SKIN CLEAT CRACKED. C-CHECK NEW UPPER OTBD SKIN CLEAT ON RT WING AT NR 5 FUEL PANEL IAW SRM.SDR ASMF201306004Skin · damagedDURING TRANSIT CHECK, DETECTED RIVETS BROKEN IN RT UPPER INBD FIXED L/E SKIN PANEL. MX PERSONNEL PERFORMED REVISION DETECTING 18 RIVETS VIBRATED AT STATION WS 190 TO 204 IN RT WING UPPER INBD FIXED L/E SKIN PANEL; SO THE RIVETS WERE REPLACED IAW SRM 51-40-02 SDR U2RA201306020002Skin · crackedLT WING L/E UPPER FIXED PANEL FOUND CRACKED BETWEEN WING STATIONS 730 TO 862. CRACK LENGTH 38" REF NRCMOL0209. GENERATED FROM TASK CARD 57-806-01-01.SDR USAA2013061900015Access Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RT WING LOWER FUEL ACCESS PANEL 640NB BETWEEN STRINGERS 8 TO 11 & BETWEEN RIB 18 TO RIB 19. REPLACED RT WING LOWER FUEL ACCESS PANEL NR 640NB IAW AMM 57-27-11-400-002-A.SDR USAA2013061900014Access Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON RT WING LOWER FUEL ACCESS PANEL 640KB BETWEEN STRINGERS 8 TO 11 & BETWEEN RIB 15 TO RIB 16. REPLACED RT WING LOWER FUEL ACCESS PANEL 640KB IAW AMM 57-27-11-400-002-A.SDR USAA2013061900013Access Panel · corroded2S CHECK - LEVEL 2 GALVANIC CORROSION ON LT WING LOWER FUEL ACCESS PANEL NR 540NB BETWEEN STRINGERS 8 TO 11 & BETWEEN RIB 18 TO RIB 19. REPLACED LT WING LOWER FUEL ACCESS PANEL 540NB IAW AMM 57-27-11-400-002-A.SDR FDEA201306011163Skin · crackedSEVEN FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 690 AND XORS 700. REAMED IAW SRM 57-20-02, FIG 201, REPAIR 5. REPAIR BUSHINGS FABRICATED AND ISDR FDEA201306011164Skin · crackedEIGHT FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS 690 AND XORS 700. HOLES REAMED IAW SRM 57-20-02, FIG 201, REPAIR 5. REPAIR BUSHINGS FABRICATEDSDR UALA2013060303850Skin · dentedON WALK-AROUND. FOUND A 3 INCH DENT ON L/E OF LT WING JUST ABOVE AND LT OF ENGINE. SUP: DENT IS .070" DEEP AND 3.5" WIDE AND HEIGHT IS 1.35" DENT HAS PREVIOUS REPAIR AND WILL NEED PERM REPAIR IN 150 HR IAW ECRA 5720-02391. REPAIRED LT OTBD L/E IAW REF SRM.SDR UALA2013041702628Skin · damagedLEFT & RIGHT LWR WING SKINS HAD DAMAGED FASTENER HOLES AT MOUNTING FLANGE OF PANELS 540NB, 540PB, & 540NB.1EA HOLE AT EACH PANEL. PANEL IS 540RB PER AIRBUS RAS-BAE-1005046-200 7. ACP INSPECTION PER ECRA 5720-02377. FOUND NO DAMAGE,ALL FASTNERS SECURED. (ORISDR DALA13026870950Access Panel · corrodedCORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF FUEL TANK ACCESS DOOR NR 1361C. CORROSION WAS REMOVED, COUNTERSINK WERE MEASURED AND WERE FOUND OUT OF LIMITS. CONDITION II MAXIMUM DIAMETER ALLOWABLE IS 0.554", 0.585", 0.554", 0.567", AND 0.0602". THEREFORE ACSDR DALA13026701812Skin · crackedUPPER WING SKIN PITCH LOAD FITTING CRACKED. REPAIRED IAW PRI 515434-14AD, REV O, VERIFIED PRI 515434-14AD, REV O MATCHES ERA 515434-14AD, REV A.SDR DALA13026711812Skin · crackedLT WING SKIN UPPER LOAD FITTING ULTRASOUND CRACK INDICATION AFT FASTENER INBD ROW. REMOVED FASTENER, REAMED HOLE IAW WC 5724-01005-10. . REPAIRED COMPLETE ON PRI 515424-14AD REV 0.SDR REXA2013060300689Skin · damagedFUEL PANEL 5650EB ACCESS HOLE AT WS 253.022 HAS NICKS ON FWD INNER SIDE 0.010" DEEP IN NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.SDR REXA2013060300688Skin · damagedFUEL PANEL 550CB ACCESS HOLE AT WS 209.040 HAS NICKS ON FWD INNER SIDE 0.010" DEEP IN NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.SDR FDEA201305291121Access Panel · corrodedLT WING -T/E LOWER ACCESS PANEL 541JB CUT-OUT FWD EDGE LOWER CAP LOWER SURFACE FOUND CORROSION. REPAIRED IAW EA 1-5710-166134. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305291126Skin · crackedTHREE FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA. XORS = 683.4 AND STA. XORS=713.6. REPAIRED AS PER SRM 57-20-02 REPAIR 5 FIGURE 201 REVISION 52. SDR REXA2013060200687Skin · damagedFUEL PANEL 510AB ACCESS HOLE LANDING CORRODED AT WS12.245 IN NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.SDR FDEA201305291127Skin · crackedTHREE FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN-HOLE HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS =683.4 AND STA XORS=713.6. REPAIRED IAW SRM 57-20-02, REPAIR 5, FIG 201, REV 52. SDR FDEA201305291124Doubler · crackedRT WING FIXED L/E BEAD DOUBLER FOUND CRACKED AT XOS 666. REPAIRED IAW SRM 57-40-02, REPAIR 15, FIG 203, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201305291120Skin · crackedRT WING T/E LOWER ACCESS PANEL 641JB CUT-OUT FORWARD EDGE LOWER CAP SURFACE, FOUND CRACK ABOUT 2" AT XW 339. REPAIR CARRIED OUT IAW EA 1-5710-166135, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR WX0A071597Skin · damagedLEFT WING MAIN FUEL TANK CUTOUT SCREW WHOLE OBLONGED. REAMED DAMAGE HOLE AND INSTALLED FREEZE PLUG.
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