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 COMA0460162Skin · corrodedFRETTING DAMAGE NOTED ON LEFT LOWER WING ACCESS HOLE CUTOUT AT 550CB. ALL DAMAGE REPAIRED BY BLENDING AND ROTO-PEENING IAW REO 601R-57-21-030.SDR MWEA040017Panel · crackedTOP PANEL IS CRACKED ON HORIZONTAL FLANGE. REMOVED AND REPLACED WITH FABRICATED TRAPEZOID PANEL.SDR IXXA0400060SSkin · corrodedDURING C CHECK INSP FOUND LT WING IB LE UPPER SKIN SURFACE CORRODED STA XFS 207.00-212.00. REPAIR WAS ACCOMPLISHED. DAMAGED SKIN ALONG WITH FASTENERS AND CORROSION WERE REMOVED AND FOUND OUT OF LIMITS IAW DC8 SRM. AN NDT INSPECTION WAS PERFORMED IAW DC8 NDT SSDR IXXA0400022SSkin · damagedDURING ROUTINE C-CHECK INSPECTION FOUND L/E HOLES ELONGATED ON UPPER SKIN SURFACE, STA XFS 526.000. REPAIR ACCOMPLISHED PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-1 PG 1, DC8 SRM 57-3-3. REMOVED UPPER SKIN SURFACE OF LT WING CTR L/E STA SXF 526.00 IAW DC8 SRM 5SDR IXXA0400049SPlate · corrodedDURING A ROUTINE C-CHECK INSPECTION FOUND CORROSION ON RT OUTER WING IB L/E OUTER PLATING AROUND STA XFS 710.00. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS IAW SRM 51-1-20D PG 21, 51-1-21 PG. 1,51-3-0 PG 1. THE CORROSION AND DAMAGED SKIN WAS REMOVED AND FOUNDSDR IXXA0400063SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND LT OB WING LE OB SECTION SKIN CORRODED STA XW 761.000. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS AND CORROSION ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-20D PG 21, 51-1-21 PG.1, 51-3-0 PG.1SDR IXXA0400058SPlate · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RT INNER WING CTR. LE SLOT OUTER PLATING CORRODED. STA.XW257.000-XFS 310.250. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA AND FOUND OUT OF LIMITS IAW DC8 SRM 51-1-21 PG. 1, 5SDR IXXA0400057SSkin · corrodedDURING A ROUTINE C CHECK RT WING OB L/E OUTER SECTION UPPER SKIN SURFACE CORRODED, STA. XW 761.000. REPAIR WAS ACCOMPLISHED. FASTENERS AND CORROSION WERE REMOVED ALONG WITH THE DAMAGED AREA IAW SRM 51-1-20D PG 21., 51-3-0 PG. 7, 51-1-21 PG 1. AN NDT INSPECTIONSDR IXXA0400052SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED , STA. XW 485.000. REPAIR WAS ACCOMPLISHED. CORROSION, FASTENERS AND THE DAMAGED AREA WAS REMOVED IAW DC8 SRM 51-1-21 PG1, 51-1-20D PG21,51-3-0 PG.1, 51-1-8 PG 17-SDR IXXA0400027SSkin · corrodedDURING ROUTINE C-CHECK FOUND RT WING OUTBOARD L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STATION XW 485.000- XFS 710. REPAIR IS ACCOMPLISHED. REMOVED FASTENER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 57-2-1 FIG 44. REMOVED CORROSION FROM UPPER SKIN SURFACE OF SDR IXXA0400026SSkin · corrodedDURING C-CHECK INSPECTION FOUND LEFT OUTBOARD WING L/E INBOARD SECTION WITH CORROSION ON SEVERAL AREAS OF UPPER SKIN SURFACE (STA XW 485.000-XPS 710.000). PERFORMANCE MAJOR REPAIR IN ACCORDANCE WITH DC8 STRUCTURAL REPAIR MANUAL 56-2-1 FIG 44. REMOVED CORROSISDR IXXA0400051SSkin · corrodedDURING A ROUTINE C CHECK INSPECTION FOUND LT WING OB L/E INNER SECTION UPPER SKIN SURFACE CORRODED, STA.XW. 485.000. REPAIR WAS ACCOMPLISHED. REMOVED DAMAGED AREA IAW DWGV22-R01 INCLUDING FASTENERS AND CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-21 PG.1, 5SDR UPS04441990Skin · corrodedINSPECTION TYPE: C, RIGHT WING UPPER SURFACE T/E RABBET AREA STRAP PNL BULGED UP AT 20 INCHES O/B OF ROOT AREA. CORROSION BLEND OUT 11.5 X 1, DEPTH .115 TO .62, ORI .332 TO .328. FPI C/O SOPM 20-20-02 AT REWORK AREA CORROSION FREE NDT INSPECTED, NIL FINDINGSDR CALA0400095Skin · crackedINSPECTION FOUND MULTIPLE CRACKS IN LT WING L/E SKIN AT O/B END OF NR 4 SLAT, OSS 430. THE LONGEST CRACK WAS SIX INCHES. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D, SEQ 399.SDR AUS20040092Skin · delaminated(AUS) LT WING INNER LEADING EDGE SKIN DELAMINATING IN AREA LOCATED ABOVE THE BYPASS DUCT.SDR P5CA0401035Panel · crackedLT WING UPPER LE PANEL CRACKED ON UPPER SURFACE (APPROX 30 INCHES,) LWR OB SURFACE HAS A 25 INCHES CRACK AND IS DISBONDED. PANEL REPLACED DURING FA-06 CHECK - NON-ROUTINE WORKCARD (T-160) NR 0034 REF.SDR COMA0460103Skin · corrodedLEFT WING LOWER SKIN PLANK HAS CORROSION AT FUEL TANK ACCESS DOOR 540DB, WS 95.950. PERFORMED A MAJOR REPAIR BY BLENDING OUT CORROSION, PERFORMED NDT TO ENSURE COMPLETE REMOVAL OF DAMAGE. ROTO-PEENED REWORKED AREAS, SANDED REWORKED AREAS TO 63 MICRO INCHES. SDR UIEA200400009Skin · corrodedDURING (D) CHECK, WING LOWER SKIN CORROSION FOUND AROUND SURGE TANK SUMP DRAIN VALVE AT WING STA 1487, BETWEEN STRINGERS S-5 AND S-6 LT SIDE. CORROSION DAMAGE IS REPAIRED BY BLEND OUT. REPAIR AREA IS SHOP PEENED AND HFEC INSPECTED. APPLIED ALODINE 1200 AND SDR UPS04841843Doubler · crackedINSPECTION TYPE: C3, RT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED AND REPLACED INTERNAL DOUBLER IAW DWG 5760545 AND SRM 51-1-21, 51-1-20D.SDR DHL2004806583Skin · corrodedLEFT WING CTR L/E CORRODED AT STA XW 257.000 (EXTERNAL SKIN). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW EDSDR DHL2004806578Skin · corrodedLT WING INBOARD OUTER L/E CORRODED, STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA ISDR 04FDEA00254Skin · corrodedRT WING UPPER SURFACE AREA BETWEEN XORS 317 TO XORS 346 FOUND WITH CORROSION. CORROSION ON RH WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 317 TO XORS 346 REMOVED AS PER SRM 51-21-01 VOL. II AND FOUND WITHIN LIMITS AS PER SRM 57-10-00 FIG. 32 VOL. I.SDR 04FDEA00253Skin · corrodedRT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 231 TO XORS 264 FOUND WITH CORROSION. CORROSION ON RT WING UPPER SURFACE IN SPAR AREA BETWEEN XORS 231 TO XORS 264 REMOVED AS PER SRM 51-21-01 VOL. II AND FOUND WITHIN TOLERANCES OF DWG ARB7113.SDR DHL2004806581Skin · corrodedLEFT WING OUTBOARD L/E LOWER PART CORRODED STA XFS 710.000. PERFORMED MAJOR REPAIR. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DSDR DHL2004806577Skin · corrodedLEFT WING OTBD L/E UPPER & LOWER PART CORRODED AT STA XW 761.695. PERFORMED MAJOR REPAIR. REMOVED EXISTING REPAIRS (3EA). REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 2G. TRIMMED OUT AND REMOVED DAMAGED AREA IAW ED-EDUSDR QXEA200400107Panel · corrodedPDX - LEFT WING PANEL 522AT COUNTER SINKS HAVE FRETTING FROM SCREWS AT INBOARD AND OUTBOARD ENDS. REPAIRED IAW DHC-8-200 SRM 51-20-16.SDR DHL2004806579Skin · corrodedRIGHT WING UPPER SKIN CORRODED AT STA XRS 202.000 S-12 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-12, DWG U80-R12. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. BLENSDR DHL2004806582Skin · corrodedRIGHT WING TOP PANEL PLATING CORROSION, STA XRS 204.000 S-9 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDU80-11, DWG U80-R11. REMOVED FASTENERS IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. SDR SWIA200412837Panel · crackedSTRINGER ON LT WING FORWARD OF NR 2 FUEL PANEL CRACKED. DISCOVERED DURING LINE INSPECTION. REPAIRED LEFT WING FORWARD STRINGER AT NR 2 FUEL PANEL IAW SRM 120 57-20-03 PG 205 TO 211, FIG 202 & IAW RII CARD 28-301.SDR COMA0460110Drain Valve · crackedCRACK INDICATION AT RT COLLECTOR VALVE AFT ATTACH HOLE BORE. OPENED HOLE TO .3125 INCH AND FABRICATED FREEZE PLUG FROM 7075-T6 BAR MATERIAL, LIQUID PENETRANT INSPECTION ON AREA OF DAMAGE PRIOR TO INSTALLING FREEZE PLUG. INSTALLED FREEZE PLUG AFTER CLEANING ASDR CALA0400060Skin · gougedINSPECTION FOUND LT WING LEADING EDGE SKIN GOUGED AT CENTER AUX TRACK ICE DOOR CUTOUT (UNDER NR 1 SLAT). REPAIRED IAW SRM 51-70-16.SDR ASAA0580041Access Panel · corrodedOKC - HV-CHECK, LEFT WING FUEL PANELS 1363 AND 1367 ARE CORRODED ON LANDINGS. REPLACED PANELS, AT XRS 267-295 AND XRS 295-353 RESPECTIVELY. (M)SDR ASAA0580040Access Panel · chafedOKC - HV-CHECK, LEFT WING FUEL PANELS 1307, 13333, AND 1379 ARE WORN AND CHAFED AT EDGE. REPLACED PANELS AT XFS 70-196, XCW58-70, AND XRS 445-447 RESECTIVELY. (M)SDR ASAA0580043Access Panel · corrodedOKC - HV-CHECK, RIGHT WING FUEL PANEL AT HEAT BLANKET IS CORRODED. REPLACED PANEL. (M)SDR ASAA0580042Access Panel · corrodedOKC - HV-CHECK, RIGHT WING FUEL PANELS 1436 AND 1464 ARE CORRODED. REPLACED PANELS, AT XFS 58-70 AND XRS 324-353 RESPECTIVELY. (M)SDR ASAA0580026Access Panel · corrodedOKC - HV CHECK, RIGHT WING FUEL ACCESS PANEL, FOR BOOST PUMP, IS CORRODED AROUND FASTENERS. REPLACED PANEL. (M)SDR ASAA0580024Access Panel · corrodedOKC - HV-CHECK, LEFT WING FUEL PANEL 1303, CORRODED ON LANDING. REPLACED PANEL. (M)SDR ASAA0580002Access Panel · corrodedOKC - HV-CHECK, SEVEN LEFT WING FUEL PANELS, FROM XRS 189 TO XRS 445, WERE FOUND CORRODED. ALL PANELS WERE REPLACED. (M)SDR ASAA0580003Access Panel · corrodedOKC - HV-CHECK, NINE RIGHT WING FUEL PANELS, FROM XRS TO XRS 477, WERE FOUND CORRODED. ALL PANELS WERE REPLACED. (M)SDR CALA0400048Panel · crackedINSPECTION FOUND A .75 INCH CRACK IN RT WING NR 6 SLAT AUX TRACK AT I/B AUX TRACK CUTOUT (FIXED L/E PANEL). THE CRACK WAS STOP DRILLED IAW SRM 57-41-01, FIGURE 101, SHEET 4, NOTE O AND P. THE CRACK WAS PLACED ON DIP TO REINSPECT EVERY 400 HOURS AND REPAIR WISDR 04FDEA00199Skin · corrodedRIGHT WING - UPPER SURFACE, FASTENER (1 EA) POPPED UP AT XORS 230, STA 1413.SDR EAT2004F00001Skin · corrodedCORROSION WAS FOUND ON THE RT LEADING EDGE SKIN DURING A ROUTINE DE-ICE BOOT CHANGE. IT WAS FOUND ON THE OUTER PORTION LOWER SIDE OF THE SKIN. THE CORROSION WAS OF SUCH A DEPTH AFTER ITS REMOVAL THAT REPAIRS WERE REQUIRED. THE MOST LIKELY CAUSE IS POOR BOOTSDR DHL2004745008Panel · corrodedLT WING LOWER SURFACE OF PLANK BETWEEN PANELS 7213 AND 7212 WING STA 546 (APPROX) EXFOLIATED. CORROSION APPROX 1 X .75 INCH AT PLANK SEAM FWD PANEL.SDR CALA0400040Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN LT WING LEADING EDGE SKIN AT OSS 450.0. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D.SDR CALA0400039Skin · crackedINSPECTION FOUND A 9 INCH CRACK IN RT WING LEADING EDGE SKIN AT OSS 441.0. THE SKIN WAS REPAIRED IAW EA 5731-01010, REV D.SDR COMA0460094Skin · crackedLEFT HAND WING LOWER PLANK CRACKED AT WS 148.019. REPAIRED LEFT HAND LOWER WING PLANK AT WS 148.019 IN ACCORDANCE WITH BOMBARDIER REO 601R-57=21-138.SDR COMA0460093Skin · crackedRIGHT HAND WING LOWER PLANK CRACKED AT WS 148.019. REPAIRED RIGHT HAND LOWER WING, PLANK AT WS 148.019 IN ACCORDANCE WITH BOMBARDIER REO 601R-57-21-138.SDR COMA0460092Panel · corrodedFRETTING DAMAGE NOTED AT LOWER INBOARD END OF LEFT HAND LOWER WING ACCESS PANEL HOLE 540 DB. BLENDED DAMAGE AND ROTO-PEENED IN ACCORDANCE WITH REO 601R-57-21-030.SDR 04FDEA00174Skin · corrodedCENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK CORRODED. LOCATION FROM STA 1235 LT X =13 TO RT X =5. CENTER WING UPPER SKIN SURFACE ABOVE UPPER AUX TANK STA 1235 LH X = 13 TO RT X = 5. CORRODED AREA CARRIED OUT REPAIR IAW EA 1-5710-74294, WINGS - CENTERSDR 04FDEA00172Skin · crackedRIGHT WING LEADING EDGE PANEL INTERIOR SEVERAL CRACKS AT XOS 546 OUTBD OF REFUELING PANEL. RT WING LEADING EDGE XOS 546 INNER DOUBLER. REPAIRED AS PER SRM 57-10-00 FIG 25 V1.
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