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 FDEA200908263090Skin · crackedRT WING INTERNAL L/E FOUND 1EA CRACK 3 INCHES LONG ON INTERNAL SKIN DOUBLER UPPER AT STA XOS 667. REPAIR BEADED DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1.SDR C2XA09IA214Skin · corrodedIAH - FLIGHT 2140, DURING POST FLIGHT INSPECTION THE CREW REPORTED A PIECE OF THE LT WING LEADING EDGE TWO TO BE CORRODED AND MISSING. IAH MAINTENANCE INSPECTED THE LEADING EDGE AND FOUND WHAT APPEARED TO BE DISSIMILAR METAL CORROSION ADJACENT TO A FASTENER FSDR GUUA95257082309ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED LT WING TOP SKIN SURFACE BETWEEN WS 147.74 AND WS 159.51 AT REAR SPAR HAS AREA OF BUCKLING SKIN SUSPECT CORROSION. REMOVED DAMAGED SKIN FABRICATED AND INSTALLED REPAIR STRAP TO REAR SPAR CAP FLANGE FILLERS AND AN EXTERSDR Q2S2010F00007Skin · corrodedLT WING L/E CAVITY FRONT SPAR LOWER CHORD AT OLES 1042 FOUND CORROSION. REPAIR CARRIED OUT IAW EN NR 1379-09.SDR ABXR200908240016Skin · damagedDURING A C-CK INSP, THE LT WING SKIN AT THE NR 1 SLAT OTBD TRACK CUT-OUT WAS HEAVYILY DAMAGED AND CRACKED DUE TO THE UPPER FWD SLAT ROLLER NOT BEING CAPTURED BY THE ROLLER BOLT. THE DAMAGED AREA WAS CUT-OUT AND A NEW SKIN SECTION WAS FABRICATED WITH 2024 T-3 SDR KCSA091094Skin · corrodedLEFT WING L/E CAVITY HAS CORROSION ON LOWER WING SKIN WS 1336.SDR Q2S2010F00006Skin · corrodedRT WING FRONT SPAR L/E CAVITY LOWER CHORD AT APPROX OLES 1500 FOUND CORROSION. REPAIR CARRIED OUT IAW EN NR 1362-09.SDR COEA2009081909900Panel · delaminatedFOUND IN COE HEAVY CHECK: MAJOR REPAIR - LT WING INBOARD TRAILING EDGE DROP DOWN PANEL 531AB HAS AREA WHERE COMPOSITE IS DELAMINATING. REMOVE INBOARD TRAILING EDGE PANEL 531AB, PERFORM NDT, FABRICATED AND INSTALLED DOUBLERS, REINSTALLED LOWER TRAILING EDGE PSDR GUUA94253081809BSkin · chafedDURING SCHEDULED ROUTINE INSP DISCOVERED SKIN CHAFE AT LT CTR WING L/E AREA APPROXFS 256 TO 265. REPAIRED LEFT CENTER WING SKIN CHAFE INSTALLED REPAIR DOUBLER.SDR GUUA94253081809ASkin · chafedDURING SCHEDULED ROUTINE INSP DISCOVERED SKIN CHAFE AT RT CTR WING L/E AREA APPROX FS 256 TO 265. REPAIRED BY INSTALLING REPAIR DOUBLER TO CHAFE AREA.SDR FDEA200908132996Skin · misrepairedEXISTING EXTERNAL REPAIR DOUBLER FOUND AT RT WING SLAT NR 7 L/E EXTERIOR SKIN. EXISTING EXTERNAL REPAIR DOUBLER AT RT WING SLAT NR 7 L/E EXTERIOR SKIN EVALUATED AND FOUND NOT IAW SRM REPAIR. RT WING NR 7 SLAT ASSY REMOVED AND REPLACED IAW AMM 27-80-30-4, RSDR UALA2009081302479Blowout Panel · missingON WALK AROUND, FOUND BLOWOUT PANEL MISSING ON BOTTOM OF LEFT WING, LEADING EDGE WING ROOT. CHECKED AREA IN LEADING EDGE AND FOUND NO DEFECTS. LOGISTIC PURCHASED PANEL PER SAMC PLNR. INSTALLED PANEL.SDR A6WA200940520Skin · gougedRT WING LWR PLANK FUEL TANK ACCESS DOOR CUTOUT 650EB EDGE OF FLANGE FOUND GOUGED. (DEPTH .012 INCH) NONE CRITICAL REGION. ACCESS DOOR CUTOUT 650EB REPAIRED IAW REO 601R-57-21-030, REV G. NON CRITICAL REGION. (K)SDR A6WA200940527Access Panel · corrodedCORROSION FOUND AROUND FUEL ACCESS PANEL CUTOUT 640CB. (NON CRITICAL REGION) CORROSION REMOVED AROUND FUEL ACCESS PANEL CUT OUT 640CB (NON CRITICAL REGION) IAW REO 601R-57-21-030 REV G AND EO NR E06/021/457 REV A. (K)SDR A6WA200940528Skin · corrodedCORROSION FOUND AROUND FUEL ACCESS PANEL CUT OUT 640DB (CRITICAL REGION). CORROSION REMOVED AROUND (CRITICAL REGION) FUEL ACCESS PANEL (640DB) IAW EO E06/021/457 AND REO 601R-57-21-030, REF G. (K)SDR IXXA09SMN089SSkin · corrodedDURING ROUTINE C-CHECK INSP FOUND RT WING L/E LWR SKIN CORRODED AT STA XFS 566.250. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK OR CORROSION. FABRICATED DOUBLER, AND FILLER. CLEANED, TREATED, AND PRIMED AREA ANSDR SWIA200922448Skin · corrodedFRETTING CORROSION AT RIGHT WING LOWER PLANK ACCESS. (C CHECK) REPAIRED PER REO.SDR SWIA200922447Skin · corrodedFRETTING CORROSION AT LEFT LOWER WING PLANK ACCESS. (C CHECK) REPAIRED PER REO.SDR I5PA20090804Skin · damagedDURING 5C CHECK AND INSP, CORROSION WAS FOUND ON THE SKIN INTERNAL SURFACE WHICH WAS UNDER THE PREVIOUS SKIN REPAIR DOUBLER FROM BS 1009 TO BS 1045 AND BETWEEN S-27L AND S-28R. REPAIRED IAW EI-727-090704.SDR IXXA09SMN069SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT WING LEADING EDGE UPPER SKIN CORRODED AT STATION XW 406.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORRODED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, AND SDR IXXA09SMN072SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HAND WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS 207.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL AND ESDR IXXA09SMN071SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND RIGHT HAND OUTER WING OUTBOARD LEADING EDGE UPPER SKIN CORRODED AT STATION XFS 730.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN INTSDR IXXA09SMN068SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HAND WING LEADING EDGE UPPER SKIN CORRODED AT STATION XFS 253.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDSDR IPXA09557052Clamp · corrodedINSPECTION TYPE:C1 FUEL PANEL CLAMP RINGS 631AB, 631BB, 631CB,641AB, 641BB, 641CB ARE CORRODED. REPLACED CORRODED FUEL PANEL CLAMP RINGS 631AB, 631BB, 631CB, 641AB, 641BB AND 641CB IAW AMM 28-11-01-4 AND AMM28-11-02-4.SDR IPXA09557051Clamp · corrodedINSPECTION TYPE:C1 FUEL PANEL CLAMP RINGS 531AB, 541BB, 541LB ARE CORRODED. REPLACED CORRODED FUEL PANEL CLAMP RINGS 531AB, 541BB, 541LB IAW AMM28-11-01-4.SDR IPXA09557050Panel · corrodedINSPECTION TYPE:C1 FUEL PANEL 542DB IS CORRODED. REPLACED CORRODED FUEL PANEL 542DB IAW AMM28-11-01-4.SDR IPXA09557049Panel · corrodedINSPECTION TYPE:C1 FUEL PANEL 542CB IS CORRODED. REPLACED FUEL PANEL 542CB IAW AMM28-11-01-4.SDR IPXA09557048Panel · corrodedINSPECTION TYPE:C1 FUEL PANEL 541MB IS CORRODED. REPLACED PANEL 541MB IAW AMM28-11-01-4.SDR ASAA0946359Skin · gougedLEFT WING LOWER SURFACE TRAILING EDGE PANEL JUST OUTBOARD OF THE NR 3 FLAP TRACK FAIRING IS GOUGED ON INNER SURFACE OVER CONE AREA. REPAIRED GOUGE ON INNER SURFACE OVER CONE AREA ON LEFT WING LOWER SURFACE TRAILING EDGE JUST OUTBOARD OF THE NR 3 FLAP TRACK FASDR IPXA09M57109Doubler · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ 258-W3-02 LT WING FIXED L/E BETWEEN STA XOS461- 473 EXISTING DOUBLER GOUGED. REMOVED EXISTING REPAIR DOUBLER ON LT WING FIXED L/E BETWEEN STA XOS461 - 473. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF MD11 SRM VOL 1 57SDR IPXA09M57247Skin · corrodedINSPECTION TYPE:1C BULGING SKIN, EVIDENCE OF CORROSION UNDER SKIN PANEL, RT WING UPPER T/E NEAR STA XORS981. REMOVED CORROSION IAW UPS EO MD11-5710-34766-A AND EA 011-5710-01-A1994.SDR GUUA95657080209ASkin · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED CRACK ON AIRCRAFT LOWER SKIN SECTION BETWEEN LEFT WING AND CENTER WING BETWEEN FS 273.25 AND FS 288.00 BL 29.00 AND BL 0.00. STOP DRILLED CRACK AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA95657080209Skin · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED CRACK ON AIRCRAFT LOWER SKIN SECTION BETWEEN LEFT WING AND CENTER WING BETWEEN FS 273.25 AND FS 288.00 AND BL 29.00 AND BL 0.00. OPENSDR UALA2009080302330Panel · crackedLEFT WING FIXED T/E UPPER PANEL HAS A CRACK LOCATED 18 INCHES AFT OF LEADING EDGE OF PANEL AND 23 INCHES INBOARD OF THE OUTBOARD EDGE OF THE PANEL. PANEL RMV RR 43353 TO SHOP 273 INSTALLED & RIGGED WU K6404D AT SMB.SDR UALA2009080302329Panel · delaminatedLEFT WING FIXED T/E LWR PANEL HAS DELAMINATION. PANEL REPAIRED REF WU K640 4D.SDR FDEA200908022868Skin · cracked09 EA FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HFEC INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700 AS MARKED. REPAIR CARRIED OUT AS PER EA 1-5710-132734.SDR FDEA200908022867Skin · cracked10 EA FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HFEC INSP AT LTW LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700 AS MARKED. REPAIR CARRIED OUT AS PER EA 1-5710-132735. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV.SDR IPXA09556923Ring · corrodedINSPECTION TYPE:C1 LT WING FUEL PANEL CLAMP RINGS 531AB, 541AB, 541BB, 541CB, 541DB, 541EB, 541HB AND 542AB ARE CORRODED. REPLACED LT WING FUEL PANEL CLAMP RINGS 531AB, 541AB, 541BB, 541CB, 541DB, 541EB, 541HB 542AB THAT WERE CORRODED IAW AMM 28-11-01-4.SDR C8GA20090221ASkin · corrodedWHILE IN INSP, IT WAS NOTED THAT THE SKIN AT STR 26L AT BS 680 IS CORRODED. CUT OUT UPPER SKIN, . FABRICATED REPAIR DOUBLER, FILLER, INSTALLED REPAIR, NO OTHER DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.SDR COMA2009080450173Skin · crackedRIGHT WING MIDDLE LEADING EDGE SKIN IS CRACKED AROUND ONE FASTENER. REMOVED AND REPLACED RIGHT WING MID LEADING EDGE SKIN AS PER CRJ SRM51-40-11 PG 1-16, CRJ SRM 51-42-06 PG 1-20 AND CRJ SRM 51-42-13 PG 1-14.SDR DJFA2009032Access Panel · corrodedDURING SCHEDULED MAINTENANCE INSPECTION, TECHNICIANS FOUND SIGNIFICANT CORROSION ON THE INTERNAL SURFACE OF CERTAIN EXTERNAL FUEL ACCESS PANEL COVERS. IN MOST CASES, THE CORROSION WAS CORRECTABLE PER THE STRUCTURAL REPAIR MANUAL BUT FOUR PANELS HAD TO BE REPLSDR FDEA200907292820Skin · misrepairedLHW - EXISTING REPAIR FOUND ON I/B FLAP UPPER SURFACE AT STA. X1FH 137. LHW EXISTING REPAIR AT I/B FLAP UPPER SURFACE AT STA. XIFH 13 7 EVALUATED AND FOUND NOT IAW SRM REPAIR. SASCO 225. EXISTING REPAIR DOUBLER REMOVED AS PER SRM 51-31-01 VOL. 2 REV. 40 AND SDR FDEA200907292910Skin · corrodedRIGHT WING - SPOTS OF CORROSION AT UPPER SKIN SURFACE AT REAR SPAR LOCATION, BTW RIBS 4 AND 5. CORROSION WAS BLENDED OUT AND REMAINING THICKNESS FOUND ACCEPTABLE AS PER EA 6-5710-131042.SDR UALA2009072902279Skin · crackedRIGHT WING UPPER SURFACE HAS A CRACKED L/E FIXED PANEL JUST OUTBOARD OF NR 3 ENG PYLON. CRACK IS 4.25 INCHES LONG BY 1. CRACK IS 3 INCHES AWAY FROM EDGE, NO DELAMINATION. TAPED CRACK, TAPE NEEDS TO BE CHECKED EVERY FLIGHT AND REPAIRED BY NEXT A-CK. PANEL PSDR IPXA09556940Panel · chafedINSPECTION TYPE:1C13 RT WING PANEL 672HB FWD LWR EDGE IS CHAFED. REMOVED AND REPLACED IAW SRM 51-40-02, AMM 51-21-10-7.SDR FDEA200907282809Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT. FOUND 07 EA HOLES WITH CRACKED INDICATION AT LT WING LWR SKIN OUTER WING FUEL TANK PANEL CUT OUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIR CARRIED OUT AS PER E.A. 1-5710-132718, REPAIR CLASSIFIESDR FDEA200907282808Skin · crackedHIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP CARRIED OUT. FOUND 02 EA HOLES WITH CRACKED INDICATION AT RT WING LWR SKIN OUTER WING FUEL TANK PANEL CUT OUT BETWEEN XORS 683.400 AND XORS 713.600. REPAIR CARRIED OUT AS PER E.A. 1-5710-132717, REPAIR CLASSIFIEDSDR FDEA200907282794Skin · crackedLT WING L/E FOUND CRACKED ON LOWER EXT SKIN L/E. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I.SDR CA090728014Skin · crackedWHILE CARRYING OUT AD 2009-11-16 AND A SCHEDULED PHASE 3 INSP A LARGE CRACK AND SEVERAL SMALL CRACKS WERE DISCOVERD IN THE RT L/E, BEHIND NACELLE SKIN. AREA IS VERY DIFFICULT TO INSPECT AND WAS FOUND BY LOOKING FROM THE LANDING GEAR WELL. CRACK IS EMENATING FSDR FDEA200907272776Skin · crackedCRACK IN LT WING BOTTOM SKIN PANEL, JUST FWD OF OTBD FWD CORNER OF ACCESS PANEL 575FB. FOUND DURING HFEC INSPECTION. ACCOMPLISHED REPAIR ON WORK CARD E6-5710-7-5013 PT5; E.O. 6-5710-7-5013 PART 5.
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