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.

SDR USAA2011020890590Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING ACCESS PANEL 640JB. REPLACED RIGHT WING ACCESS PANEL 640JB IAW A319 SRM 57-27-11 AND TASK CARD 26C60057091.Feb 1, 2011 · N714US · Airbus A319112SDR A6WA201140159Access Panel · corrodedFUEL CELL ACCESS PANEL OPENING FOR PANEL 640CB IS CORRODED. REPAIRED FUEL CUT OUT 640CB REO 601R-57-21-030, REV H.Jan 31, 2011 · N456ZW · Cndair CL6002B19SDR A6WA201140160Access Panel · corrodedFUEL CUT OUT 640BB HAS FRETTING CORRODED. REPAIRED FUEL CUT OUT 640BB IAW REO 601R-57-21-030, REV H.Jan 31, 2011 · N456ZW · Cndair CL6002B19SDR A6WA201140161Access Panel · corrodedFUEL CELL ACCESS PANEL OPENING 640DB IS CORRODED. REPAIR FUEL CUT OUT 640DB REO 601R-57-21-030, REV H.Jan 31, 2011 · N456ZW · Cndair CL6002B19SDR GUUA92757013111APanel · debondedDURING SCHEDULED ROUTINE INSP DISCOVERED LT WING INBD EDGE PANEL CORROSION AND DEBOND. REMOVED DAMAGE AND INSTALLED A FILLER AND AN EXTERNAL DOUBLER REPAIR.Jan 31, 2011 · N46AR · Beech 1900DSDR USAA2011020890586Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING ACCESS PANEL 540LB. REPLACED LEFT WING ACCESS PANEL 540LB IAW TASK CARD 26C50057092.Jan 31, 2011 · N714US · Airbus A319112SDR DALA1111810691Skin · damagedMISLOCATED HOLES ON LT WING LWR SKIN WSTA 730 COMMON TO FUEL PNL PN 112N62002-7 DUE TO USING FUEL PNL PN 112N6002-8 (FOR RT WING) TO PICK UP HOLES/COMPLIED ERA 489459-14 REV ORIGINAL ON LT WING LOWER SKIN PANEL ON HMV AT SAA ON NRC 180986.Jan 29, 2011 · N900PC · Boeing 75726DSDR IPXA1M64738Skin · crackedINSPECTION TYPE:4C, LT WING ANTI-ICE TELESCOPIC DUCT UPPER DOOR CUTOUT CRACK AT OTBD CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-01, REPAIR 10, FIG 201.Jan 28, 2011 · N283UP · Doug MD11FSDR FDEA201101280397Skin · cracked13 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT RT WING SKIN ACCESS DOOR CUT OUT BETWEEN STATION XORS= 683.4 AND STATION XORS= 713.6. REPAIR CARRIED OUT PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MINOR AS PERJan 28, 2011 · N596FE · Doug MD11FSDR FDEA201101280396Skin · cracked15 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING SKIN ACCESS DOOR CUT OUT BETWEEN STA XORS= 683.4 AND XORS= 713.6. REPAIR CARRIED OUT PER DRAWING SG11570004 REVISION A. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-Jan 28, 2011 · N596FE · Doug MD11FSDR DHLA201100014Skin · misrepairedREMOVED NON STANDARD REPAIR IAW SRM 51-3-0, SRM 51-1-20D. FABRICATED EXT REPAIR DOUBLER & INTERNAL DOUBLER IAW SRM 57-2-1A FIG. 1. HEAT TREATED INTERNAL DOUBLER IAW SRM 51-1-1 PG 1-13-17, DPS 7.00-1 REV "BL". CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAWJan 27, 2011 · N873SJ · Doug DC873FSDR IPXA1M64761Doubler · crackedINSPECTION TYPE:4C, RT WING L/E INNER SKIN CRACKED AT 2 EA RIVETS ABOUT THE OUTBD REFUEL/DEFUEL RECEPTACLE, APPROX STA XOS 635. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR IPXA1M64760Doubler · crackedINSPECTION TYPE:4C, RT WING L/E INNER SKIN CRACKED AT 3 EA RIVETS, ABOUT THE SLAT CABLE PULLEY JUST INBD OF THE NR4 SLAT OTBD TRACK, APPROX STA XOS 645. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR IPXA1M64759Doubler · crackedINSPECTION TYPE:4C, RT WING L/E INNER SKIN CRACKED AT 2 EA RIVETS, ABOVE THE INBD REFUEL/DEFUEL RECEPTACLE, APPROX STA XOS 610. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR IPXA1M64743Doubler · crackedINSPECTION TYPE:4C, RT WING L/E INNER SKIN CRACKED AT 2 EA RIVETS, APPROX. STA XOS 567 JUST OTBD OF SLAT OTBD TRACK. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR IPXA11M64689Doubler · crackedINSPECTION TYPE:4C, LT WING FIXED L/E BEADED DOUBLER CRACK RT ALONG SUPPORT STRAP AT STA XOS 669. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR IPXA11M64688Doubler · crackedINSPECTION TYPE:4C, CRACK ON LT WING FIXED L/E BEADED DOUBLER AT STA XOS 673. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR IPXA11M64687Doubler · crackedINSPECTION TYPE:4C, CRACK ON LT WING FIXED L/E COMPT BEADED DOUBLER AT APPROX STA XOS 692. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR IPXA11M64686Doubler · crackedINSPECTION TYPE:4C, CRACK ON LT WING FIXED L/E COMPT. BEADED DOUBLER AT APPROX STA XOS 708. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR IPXA11M64685Doubler · crackedINSPECTION TYPE:4C, BEADED DOUBLER CRACK AT LT WING FIXED L/E COMPT AT APPROX STA XOS 587. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR IPXA11M64684Doubler · crackedINSPECTION TYPE:4C, BEADED DOUBLER CRACK ON LT WING FIXED L/E COMPT AT APPROX STA XOS 647. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 27, 2011 · N283UP · Doug MD11FSDR FDEA201101270394Skin · corrodedWING CENTER SECTION UPPER EXTERIOR SURFACE BS 820, LBL 12 HAS CORROSION. ACCOMPLISHED REMOVAL OF CORROSION FROM WING CENTER SECTION SKIN AT BS 820 LBL 12 IAW EA 7-5730-123577.Jan 27, 2011 · N223FE · Boeing 727233SDR UALA2011012700453Seal · damagedRT FUEL ACCESS PANEL 3RD FROM WING ROOT LEAKING OUT OF LIMITS. FOUND ALL SCREWS LOOSE TIGHTENED NO HELP. REMOVED PNL 631CB FOUND RUBBER SEAL DAMAGED, RPL SEAL,CLEARED AND REINSTALLED 631CB, LEAK CHECK PASSED.Jan 27, 2011 · N206UA · Boeing 777222SDR FDEA201101270390Skin · corrodedLT WING LWR SURFACE, WS 177.50, STRINGER L-6 TO L-8, 3 EA SPOTS OF CORROSION. COMPLIED WITH/ACCOMPLISHED REPAIR ON EA F-5730-143248 MAJOR REPAIR.Jan 27, 2011 · N997FD · Boeing 757200SDR FDEA201101260363Skin · misrepairedLT WING FIXED L/E FOUND WITH EXISTING REPAIR AT FORWARD OF FUEL PANEL AREA. LT WING FIXED L/E REPAIR AT FWD OF REFUEL PANEL AREA EVALUATED AND FOUND NOT IAW APPROVED DATA. LT WING FIXED L/E FWD OF REFUEL PANEL CARRIED OUT REPAIR IAW EA 1-5730-143848 & EO 1-5Jan 26, 2011 · N596FE · Doug MD11FSDR DALA1106279857Skin · chafedLT WING L/E SKIN AFT OF NR 2 SLAT INBD AND OTBD OF CTR TRACK CUTOUT EXISTING REPAIR IS CHAFED. REMOVED OLD REPAIR NR 2 SLAT BROKE CABLE TENSION, REMOVED NR2 SLAT PULLEY AND BRACKET FAB NEW REPAIR DOUBLER INSTALLED NR2 SLAT EXTENSION CABLE PULLEY AND BRACKET Jan 26, 2011 · N766NC · Doug DC951SDR QXEA2011012600082Skin · corrodedC5 CHECK - RT WING SKIN CUTOUT FOR PANEL 624BT HAS FRETTING ON THE OTBD END. COMPLIED WITH RD8/4-57-445. FOUND WITHIN LIMITS OF RD 8/4-57-445. TREATED AND PRIMED AS REQUIRED IAW RD8/4-57-445.Jan 25, 2011 · N412QX · Bombdr DHC8402SDR QXEA2011012600081Skin · corrodedC5 CHECK - RT WING SKIN CUTOUT FOR PANEL 624AT HAS FRETTING ON THE INBD END. COMPLIED WITH RD8/4-57-445. FOUND WITHIN LIMITS OF RD 8/4-57-445. TREATED AND PRIMED AS REQUIRED IAW RD8/4-57-445.Jan 25, 2011 · N412QX · Bombdr DHC8402SDR QXEA2011012600080Skin · corrodedC5 CHECK - LT WING SKIN CUTOUT FOR PANEL 524AT HAS FRETTING ON THE INBD END. COMPLIED WITH RD8/4-57-445. FOUND WITHIN LIMITS OF RD 8/4-57-445. TREATED AND PRIMED AS REQUIRED IAW RD8/4-57-445.Jan 25, 2011 · N412QX · Bombdr DHC8402SDR QXEA2011012600079Panel · corrodedC5 CHECK - RT WING PANEL 624BT HAS FRETTING ON THE OTBD END. COMPLIED WITH RD8/4-57-442. FOUND WITHIN LIMITS OF RD 8/4-57-442. TREATED AND PRIMED AS REQUIRED IAW RD8/4-57-442, SRM 51-21-10-02-01 AND 51-25-10-02-01.Jan 25, 2011 · N412QX · Bombdr DHC8402SDR QXEA2011012600078Panel · corrodedC5 CHECK - RT WING PANEL 624AT HAS FRETTING ON THE INBD END. COMPLIED WITH RD 8/4-57-442. TREATED AND PRIMED AS REQUIRED IAW RD 8/4-57-442, SRM 51-21-10-02-01 AND 51-25-10-02-01.Jan 25, 2011 · N412QX · Bombdr DHC8402SDR QXEA2011012600077Panel · corrodedC5 CHECK - LT WING PANEL 524AT HAS FRETTING ON THE INBD END. COMPLIED WITH RD8/4-57-442. TREATED AND PRIMED AS REQUIRED IAW SRM 51-21-10-02-01 AND 51-25-10-02-01.Jan 25, 2011 · N412QX · Bombdr DHC8402SDR IPXA1564733Panel · chafedINSPECTION TYPE:C4, 2" LONG CHAFE IN THE LT WING FIXED L/E, 1" OTBD OF THE NR1 ENGINE PYLON. REPAIRED FIXED L/E IAW ER 11-01203.Jan 24, 2011 · N417UP · Boeing 75724APFSDR EE4Y20110034Door · delaminatedLT WING T/E BUTE DOOR P/N: 5919572-512 DELAMINATED. DELAMINATED BUTE DOOR WAS REPAIRED BY LOCAL DER.Jan 24, 2011 · N573SH · Doug DC982SDR DHLA201100012Skin · misrepairedREMOVED PLATING WITH EXISTING NON STANDARD REPAIR IAW SRM 57-1-0 PG 1, SRM 51-1-21. FABRICATED NEW PLATING IAW SRM 57-3-3 FIG 8 ITEM "A", SRM 51-1-4. CLEANED, TREATED AND PRIMED AREA & NEW PLATING INNER FACE IAW SRM 51-1-8B. INSTALLED NEW PLATING IAW SRM 51-1-Jan 21, 2011 · N873SJ · Doug DC873FSDR DHLA201100011Skin · misrepairedREMOVED EXISTING REPAIR IAW SRM 51-1-21, SRM 51-1-20D. CUT OUT DAMAGED AREA & FABRICATED FILLER & DOUBLER IAW DWG ES-D85700391-001-D REV IR. VISUALLY INSPECTED CUT OUT AREA & REPAIR PARTS IAW NDT SPM PART 09, NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION FJan 21, 2011 · N873SJ · Doug DC873FSDR USAA2011021790787Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING ACCESS PANEL 640QB, RIB 20 - RIB 21. REPLACED RIGHT WING ACCESS PANEL 640QB, RIB 20 - RIB 21 IAW TASK CARD 26C50057091.Jan 21, 2011 · N714US · Airbus A319112SDR USAA2011021790786Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING ACCESS PANEL 540HB, RIB 13 - RIB 14. REPLACED LEFT WING ACCESS PANEL 540HB, RIB 13-RIB 14 IAW TASK CARD 26C50057092.Jan 21, 2011 · N714US · Airbus A319112SDR USAA2011020890607Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING ACCESS PANEL 540MB. REPLACED LEFT WING ACCESS PANEL 540MB IAW TASK CARD 26C50057092.Jan 21, 2011 · N714US · Airbus A319112SDR USAA2011020890606Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING ACCESS PANEL 540RB. REPLACED LEFT WING ACCESS PANEL 540RB IAW TASK CARD 26C50057092.Jan 21, 2011 · N714US · Airbus A319112SDR USAA2011020890605Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING ACCESS PANEL 640NB. REPLACED RIGHT WING ACCESS PANEL 640NB IAW A319 SRM 57-27-11.Jan 21, 2011 · N714US · Airbus A319112SDR USAA2011020790534Panel · corrodedSAL - S4 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL PANEL 640MB BETWEEN WS 9235 TO WS 9704 & BETWEEN RIB 17 TO RIB 18. REPLACED RIGHT WING LOWER FUEL PANEL 640MB BETWEEN WS 9235 TO WS 9704 & BETWEEN RIB 17 TO RIB 18 IAW A319 SRM 57-2Jan 21, 2011 · N714US · Airbus A319112SDR FDEA201101210324Skin · damagedLT WING - WING TIP T/E SEVERAL RIVET HOLES ELONGATED. REMOVED AS PER SRM 51-40-21 REVISION 19. ELONGATED HOLES REWORKED AS PER DRAWING A57247017 ISSUE M AND NEW RIVETS INSTALLED AS PER SRM 51-40-21 REVISION 19. REPAIR CLASSIFIED MINOR PER GMM 6-2-100 REVISJan 21, 2011 · N663FE · Airbus A300F4605RSDR QXEA11012100058ASkin · corrodedC5 CHECK - LT WING SKIN CUTOUT FOR PANEL 524BT HAS FRETTING. REMOVED FRETTING CORROSION IAW RD 8/4-57-442. FOUND WITHIN LIMITS IAW RD 8/4-57-442. TREATED AND PRIMED AREA IAW RD 8/4-57-442.Jan 20, 2011 · N421QX · Bombdr DHC8402SDR QXEA2011012100057Skin · corrodedC5 CHECK - LT WING PANEL 524BT HAS FRETTING. REMOVED FRETTING CORROSION IAW RD 8/4-57-442. FOUND WITHIN LIMITS IAW RD 8/4-57-442. TREATED, PRIMED AND REPLACED INNER AND OUTER SEALS IAW RD 8/4-57-442.Jan 20, 2011 · N412QX · Bombdr DHC8402SDR CA110201008Skin · cracked(CAN) VISUAL INSPECTION REVEALED CRACKED OUTBOARD SKINS P/N 100-110068-15 AND 16. THESE ARE THE OUTER SKINS ON THE OUTER WINGS LH AND RH. CRACKS WERE LOCATED AT ABOUT 12 O`CLOCK POSITION OF THE OUTBOARD FUEL CAPS. CRACKS UNDOUBTEDLY RELATED TO ABNORMAL LOADS AJan 19, 2011 · Beech B200SDR WX0A070752Access Panel · chafedRT WING LEADING EDGE ACCESS PANEL DEEP AREAS OF CHAFING. TRIMMED OUT DAMAGE, HEFC INSPECTED, NO CRACKS NOTED, FABRICATED, LOCATED, DRILLED AND INSTALLED REPAIR DOUBLER AND FILLERS IAW AAR EA 14275.Jan 19, 2011 · N401NV · Doug MD83SDR DHLA201100028Skin · damagedRT WING UPPER PANEL DELAMINATED AND HOLES ELONGATED (STA XW 0.000 - 47.000) R & R RT WING UPPER PANEL (STA XW 0.000 - 47.000) IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Jan 18, 2011 · N873SJ · Doug DC873FSDR DHLA201100024Panel · delaminatedLT WING UPPER PANEL DELAMINATED STA XA 566.000 - 586.000. R & R LT WING UPPER PANEL WITH SAME FASTENERS IAW SRM 51-3-0, SRM 51-3-1 (TORQUE).Jan 18, 2011 · N873SJ · Doug DC873FSDR IXXA11SMN011SSkin · corrodedDURING ROUTINE C CHECK INSPECTION FOUND LEFT WING UPPER SKIN CORRODED AT STATION XRS 360.000 STRINGER 6. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY FOUNJan 18, 2011 · N799AL · Doug DC862F
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