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 IPXA09M56126Doubler · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ 250-W3-01 LT WING FIXED L/E EXISTING REPAIR DOUBLER AT TELESCOPIC DUCT CUTOUT GOUGED. REMOVED DOUBLER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43 SHT 1-5.SDR FDEA200905131649Skin · puncturedLEFT WING, LEADING EDGE UPPER SKIN AT STA XOS 1142 FOUND PUNCTURED. REPAIRED AS PER EA 1-5730-129225.SDR IPXA09855839Skin · damagedINSPECTION TYPE:SV SURVEY SEQ 852-W3-06 LT WING L/E SURFACE EDGE DOUBLER XFS 300-341 SEVERAL FASTENERS ARE LESS THAN 1.5 DIAMETERS FROM EDGE OF REPAIR MARKED XFS 320. REPAIR ACCOMPLISHED PER TIMCO REO-G12705 AND EO DC8-5730-33332.SDR IPXA09855859Skin · misrepairedINSPECTION TYPE:SV SURVEY SEQ 852-W4-11, RT CTR LE LWR SKIN STA XFS 303 PREVIOUS REPAIR DID NOT PASS APPENDIX H. REMOVED EXISTING REPAIR, INSTALLED NEW REPAIR IAW REO-G12763 AND UPS EO DC8-5710-33325-A.SDR KCSA091040Skin · corrodedRT WING LOWER SKIN SPLICE FWD OF FRONT SPAR CORRODED A WS 1500.SDR IPXA09M55929Skin · misrepairedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W3-14 EXISTING REPAIR ON LT WING FIXED LE UPPER SKIN BETWEEN XIS 168-178 AT WING SPAR NOT PER SRM AND NOT ON MRCSSR. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW IPXA EO MD11-5720-33511-ASDR FDEA200905041531Skin · crackedRIGHT WING LEADING EDGE UPPER SURFACE AT WING ANTI-ICE TELESCOPIC DUCT CUT-OUT FOUND CRACKED. CUT-OUT CRACKED AREA AS PER SRM 57-10-00 FIGURE 43 VOLUME I, REVISION 40. REPAIR DOUBLER AND FILLER FABRICATED AS PER SRM 57-10-00 FIGURE 43 VOLUME I, REVISION 4SDR FDEA200905041498Skin · corrodedFOUND CORROSION ON LT WING TIP UNDER LOWER STATIC DISCHARGER REPAIR PERFORMED BY BLEND OUT THE CORROSION AND APPLY FILLING COMPONENT IAW RAS/FOK/059/2009 ISS A, APPROVED BY EA 6-5720-129117.SDR IPXA09M55885Skin · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQUENCE W4-12 RT WING FIXED L/E UPPER SKIN BETWEEN XIS 242- XIS 252 REPAIR IS GOUGED. REMOVED DOUBLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG 24.SDR ASAA0945495Skin · damagedFIXED L/E SKIN DAMAGED AT 31 SLAT I/B AUX TRACK CUTOUT. DAMAGE REPAIRED.SDR MZZA2009050500060Skin · corrodedRIGHT WING CENTER SECTION CORROSION FOUND UNDER DRAG BRACE BETWEEN SR 20 TO SR21 AT STATION 540 (WBL52). REPAIR CARRIED OUT PER EC/RA NR5710-02162.SDR MZZA2009050500059Skin · corrodedLEFT WING CENTER SECTION CORROSION FOUND UNDER DRAG BRACE BETWEEN SL 20 TO SL 21 AT STATION 540 (WBL52). REPAIR CARRIED OUT PER EC/RA NR 5710-02162.SDR FDEA200905021492Doubler · corrodedRT WING TRAILING EDGE LOWER WING DOUBLER BELOW NR 1 SPOILER ACTUATOR AREA FOUND WITH SEVERAL AREA CORROSION. COMPLIED WITH EA 1-5710-127841. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 107.SDR IPXA09M55928Skin · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W4-03 EXISTING REPAIR ON RT WING FIXED LE BETWEEN XOS 882-896 AT SLAT TRACK CUT OUT IS NOT PER SRM, HAS A GOUGE .071 AND HAS BLIND RIVETS. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW MD-SDR ASOA200900510Skin · crackedCRACK FOUND ON RT LEADING EDGE OF WINGLET TIP APPROX 7 INCHES FROM BOTTOM OF TIP.SDR SWAA092821Skin · crackedDURING SCHEDULED HC2 CHECK, FOUND LT WING L/E SKIN CRACKED. REPAIRED SKIN PER MM.SDR UIEA200900031Panel · delaminatedLT WING LEADING EDGE UPPER SURFACE FIXED PANEL A PREVIOUS REPAIR AT ILES 865.5 AND 18.0 INCHES FROM PANEL TRAILING EDGE, AN AREA OF 7.0 INCHES BY 11.0 INCHES IN DIAMETER IS DELAMINATED. PERMANENT REPAIR ACCOMPLISHED AS PER 747-200 SRM 51-40-09, FIG 18 SHEET 3SDR UIEA200900030Panel · delaminatedRT WING LEADING EDGE UPPER SURFACE FIXED PANEL A PREVIOUS REPAIR AT ILES 857.5 AND 13.0 INCHES FROM TRAILING EDGE, AN AREA OF 5.0 INCHES IN DIAMETER IS DELAMINATED. PERMANENT REPAIR ACCOMPLISHED AS PER 747-200 SRM 51-40-09, FIG 18 SHEET 3 AND 5. PREPREG 250 SDR UIEA200900029Panel · delaminatedRT WING LEADING EDGE UPPER SURFACE FIXED PANEL A PREVIOUS REPAIR AT ILES 897.5 AND 26.0 INCHES FROM PANEL TRAILING EDGE, AN AREA OF 6.0 INCHES IN DIAMETER IS DELAMINATED. PERMANENT REPAIR ACCOMPLISHED AS PER 747-200 SRM 51-40-09, FIG 18 SHEET 3 AND 5. PREPRESDR AALA20090430TUL06Skin · wornRIGHT WING LOWER SKIN FORWARD AND AFT OF TANK PLATE 632BB OUTBOARD SIDE WORN .015. REPAIRED PER EA B737-57-006-127 DATED 4/24/09.SDR IPXA09M55895Skin · damagedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W4-01 EXISTING REPAIR DOUBLER ON RT WING FIXED LE BETWEEN XOS 461-473 HAS A GOUGE. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPLACEMENT REPAIR IAW IPXA EO MD11-5730-33489-A AND SAA EA 011-5730-01-A1754.SDR IPXA09M55888Skin · gougedINSPECTION TYPE:2C REPAIR SURVEY SEQ NR 286-W3-02, EXISTING REPAIR DOUBLER ON LT WING FIXED L/E BETWEEN XOS461-473 HAS A GOUGE. REMOVED EXISTING REPAIR FABRICATED NEW REPAIR AND INSTALLED REF SRM 57-10-00 FIG 43.SDR IPXA09555776Skin · crackedINSPECTION TYPE:C4 RIGHT WING LEADING EDGE HAS A CRACK AT WS 419.5, 9 TO 15 INCHES ABOVE NOSE OF LEADING EDGE, ABOVE NR 7 SLAT. REPAIRED PER SRM 51-70-07-0G.SDR ZZDA2009127Skin · damagedLEFT WING LEADING EDGE STA 15.136 HAS DEEP GROOVE WORN. REMOVED OLD REPAIR, INSTALLED NEW DOUBLER IAW B717 SRM 57-00-00 FIG 101.SDR IPXA09M55762Skin · crackedINSPECTION TYPE:1C LT WING L/E SKIN CRACKED AT OPENING FOR SLAT DEICE TELESCOPE DUCT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW MD-11 SRM 57-10-00 FIG 43 SHT 1-5.SDR DL738090779Skin · damagedWINGLET MOD RT WINGTIP. MAINTENANCE MISDRILLED OF THE HOLE LOCATIONS AT APPROX OF SS725 COMMON TO THE UPPER FRONT SPAT CHORD, THE SPAR WEB AND THE SLAT TRACK SUPPORT FITTING FOR THE SLAT TRACK AT OFSS 730.SDR IPXA09M55903Doubler · crackedINSPECTION TYPE:C RT WING L/E LOWER ACCESS NR 619DB COMPT FOUND BEADED DOUBLER CRACKED AS MARKED, STA XORS 573 APPROX OTBD OF SLAT TRACK NR 10. DAMAGE AREA AT BEADED DOUBLER TRIM OFF PER SRM 57-10-00, FIG 27, VOL I REV40. HFEC INSPECTION C/O ON TRIMMED EDGE SDR IPXA09M55902Doubler · crackedINSPECTION TYPE:C LT WING L/E LOWER ACCESS NR 519CB COMPT FOUND BEADED DOUBLER CRACKED AS MARKED, STA XORS 528 APPROX. DAMAGED AREA AT BEADED DOUBLER TRIM OFF AS PER SRM 57-10-00, FIG 27, VOLI, REV40. HFEC INSP C/O ON TRIM OUT EDGE AND FOUND NO CRACK EVIDENTSDR IPXA09M55846Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W4-016, RT WING, FIXED L/E ACCESS PANEL NR 615DB, NEEDS VALIDATION FOR REPAIR. BASE ON INFO COLLECTED IN EO MD11-5100-30530-B, REPAIR SEQ NBR 285-W4 -016 DOES NOT CORRELATE WITH SRM REPAIR. EXISTING REPAIR AT ACCESS SDR IPXA09M55913Doubler · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-011 LWH REPAIR DOUBLER AT FIXED LEADING EDGE STA XORS 402-433 NEEDS VALIDATION. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W3-011 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING REPAIR AT LHW FIXED L/E REMOVED. SDR IPXA09M55900Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NUMBER 285-W4-007, RT WING, INBD TOP FIXED L/E AT XFS 231, NEEDS VALIDATION FOR REPAIR. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W4-007 DOES NOT CORRELATE TO SRM 57-10-00, FIG 24, VOL I, REV 40. EXISTING REPAIR AT DISCRSDR IPXA09M55864Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-004 LHW FIXED LEADING EDGE TOP SURFACE STA 247 REPAIR DOUBLER NEEDS VALIDATION. BASED UPON COLLECTED INFO, REPAIR SEQ NBR 285-W3-004 DOES NOT CORRELATE TO SRM 57-10-00 FIG 24, VOLI, REV40. EXISTING REPAIR REMOVED.SDR IPXA09M55831Skin · misrepairedINSPECTION TYPE:C REPAIR SEQUENCE NBR 285-W3-001 LHW UPPER WINGLET LEADING EDGE TOP END REPAIR DOUBLER NEEDS VALIDATION. BASE ON EO MD11-5100-30530-B, REPAIR SEQ NR 285-W3-001 DOES NOT CORRELATE TO ANY SRM REPAIR. EXISTING REPAIR AT LHW UPPER WINGLET L/E REMSDR IPXA09M55828Skin · gougedINSPECTION TYPE:1C REPAIR SURVEY SEQUENCE NR 272-W3-01, EXISTING REPAIR DOUBLER ON LT WING FIXED L/E LWR SKIN BETWEEN XDLE 330-XW344 NR 1 PYLON HAS GOUGED FASTENER HEADS, AS WELL CAN NOT CORRELATE TO THE SRM AND IS NOT ON MRCSSR REPORT. REMOVED DOUBLER ,TRIMMSDR IPXA09M55813Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY DWQ 272-W4-01, EXISTING REPAIR DOUBLER ON RT WING FIXED L/E LWR SKIN BETWEEN XOLE 330- XW 344 HAS SHEARED FASTENER HEADS AND GOUGED, AS WELL CAN NOT BE CORRELATED TO THE SRM AND IS NOT ON THE MRCSSR REPORT. REMOVED DOUBLER, FASDR FDEA200904221380Skin · crackedFIVE FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN HOLE HFEC INSPECTION AT RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-127836, THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-SDR FDEA200904221379Skin · crackedFIVE FASTENER HOLES FOUND WITH CRACK INDICATIONS DURING OPEN-HOLE HFEC INSPECTION AT LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT AS PER EA 1-5710-127835, THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-SDR GLBA20090424FSkin · leakingDURING SCHEDULED MX A FUEL LEAK WAS FOUND ON THE LT WING LE ON A PREVIOUS REPAIR FROM APPROX WS 239 TO WS 249.75. MX REPAIRED THE LT WING LE PREVIOUS REPAIR IAW EO-09-1900-57-004. ALL RII INSP REQUIREMENTS COMPLIED WITH IAW EO-09-1900-57-004.SDR S9BA20090009Skin · corrodedRT BOTTOM WING HAS CORRISION IN SKIN AT STATION 135 AFT OF LEADING EDGE. REMOVED AND REPLACED RT WING ASSEMBLY IAW MM 57-00-00 PAGE 201-205SDR IPXA09855610Skin · damagedINSPECTION TYPE:SV SURVEY SEQ 852-W4-15 REPAIR DOUBLER HAS FASTENERS WITH SHORT EDGE DISTANCE, RT OTBD L/E LOWER SKIN XFS 712. REPAIR ACCOMPLISHED PER REO-G12675 REV A AND EO DC8-5720-33123-A.SDR IPXA09855608Access Panel · damagedINSPECTION TYPE:SV SURVEY SEQ 852-WS-35 LT WING L/E LOWER SURFACE ACCESS PANEL XFS 502 RE PAIR DOUBLER IS .071 BASE STRUCTURE IS .100. INSTALLED REPAIR PER DAC DWG 5761041-3.SDR IPXA09855607Access Panel · damagedINSPECTION TYPE:SV SURVEY SEQ 852-W3-34-LT WING L/E LOWER SURFACE ACCESS PANEL, XFS 476 EX EXISTING REPAIR DOUBLER IS .071 AND BASE MATERIAL IS .100. INSTALLED REPAIR PER DAC DWG 5761041.SDR FDEA200904201339Skin · crackedOLD EXTERNAL DOUBLER PATCH REPAIR WITH CRACKED HOLES. REPAIR PERFORMED IAW EA 6-5730-129153.SDR FDEA200904201336Skin · corrodedSEVERAL CORROSION SPOTS BETWEEN RIB 9 IN LEVEL OF CENTER SPAR TOP SKIN PANEL UPPER SURFACE REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS/BAE/1009557/2009.SDR FDEA200904201335Skin · corrodedSEVERAL CORROSION SPOTS BETWEEN RIB 14 AND 29 TOP SKIN PANEL UPPER SURFACE REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS/BAE/1009557/2009.SDR FDEA200904201334Skin · misinstalledIRREGULARLY BOLT HOLE AT LT WING TOP SKIN RIB 8 STRINGER 14 SKIN REINFORCING REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS/BAE/1009557/2009.SDR FDEA200904201333Skin · corrodedSEVERAL CORROSION SPOTS LT WING TOP SKIN PANEL BETWEEN RIB 1 AND 14 UPPER SURFACE REPAIR PERFORMED IAW EA 6-5730-129154 AND RAS /BAE/1009557/2009.SDR FDEA200904201332Skin · corrodedMULTIPLE CORROSION, TOP SKIN, TE OVERHANG, RIB 25-29, LEFT WING CORROSION REMOVED BY BLENDING AND NEW FASTENERS INSTALLED IAW EA 6-5720-129141. FABRICATION NEW PANEL IAW EA 6-5750-129151.SDR DL757090720Skin · wornCHAFING MARK (WORN) ON RIGHT WING LOWER SKIN SURFACE AT WS 321.5 DUE TO CONTACT WITH NR 2 PYLON ACCESS PANEL 445BR. C/W AT SAA, SAT ON N/R 127291 JBO 82638930001.SDR IPXA09855654Skin · misrepairedINSPECTION TYPE:SV 852-W4-13 REPAIR DOUBLER CRACKED. RIGHT L/E LOWER SKIN ABOVE NR 4 PYLON XFS 530 35 INCHES FWD OF WING FRONT SPAR. REPAIRED PER DC8 SRM 57-2-01A FIG 2.
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