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 USAA2011031791097Panel · overweightSAL - S5 - MAJOR REPAIR - LOWER LEFT WING FUEL PANEL 540EB WEIGHT IS OUT OF LIMITS BETWEEN WS 5512 TO WS 6132 & BETWEEN RIB 10 TO RIB 11. REPLACED LOWER LEFT WING FUEL PANEL 540EB WEIGHT IS OUT OF LIMITS BETWEEN WS 5512 TO WS 6132 & BETWEEN RIB 10 TO RIB 11 ISDR USAA2011031791096Panel · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION ON LOWER LEFT WING FUEL PANEL 540LB BETWEEN WS 8744 TO WS 9235 & BETWEEN RIB 16 TO RIB 17. REPLACED LOWER LEFT WING FUEL PANEL 540LB BETWEEN WS 8744 TO WS 9235 & BETWEEN RIB 16 TO RIB 17 IAW A320 SRM 57-27-SDR USAA2011031691068Panel · corrodedSAL - S5 - MAJOR REPAIR - LEVEL 2 GALVANIC CORROSION IN COUNTERSINK HOLE OF LEFT WING FUEL PANEL 540HB AT WS 7316 BETWEEN RIB 13 TO RIB 14. REPLACED LEFT WING FUEL PANEL 540HB AT WS 7316 BETWEEN RIB 13 TO RIB 14 IAW A320 CMM 28-12-46.SDR FDEA201102250763Skin · crackedLEFT WING LEADING EDGE LOWER SURFACE SKIN FOUND CRACKED AT STATION XORS 616, NR 5 SLAT MAIN TRACK CUTOUT OUTBOARD CORNER. REPAIR CARRIED OUT AT LT WING LOWER LEADING EDGE SKIN AREA AT STATION 616 NR 5 SLAT MAIN TRACK CUTOUT OUTBOARD CORNER AS PER SRM 57-40-SDR FDEA201102250762Skin · crackedRIGHT WING LEADING EDGE LOWER SKIN FOUND CRACKED AT STATION XORS 507, REFUELING STATION ACCESS PANEL, INBOARD HINGE CORNER. REPAIR CARRIED OUT AT RT WING LEADING EDGE LOWER SKIN AT STATION XORS 50. REFUELING STATION ACCESS PANEL INBOARD HINGE CORNER AS PER SSDR FDEA201102250761Skin · crackedLEFT WING LEADING EDGE LOWER SURFACE SKIN FOUND CRACKED AT STATION XORS 507, REFUELING STATION ACCESS PANEL, INBOARD HINGE CORNER. REPAIR CARRIED OUT AT LT WING LEADING EDGE LOWER SKIN AT STATION XORS 507 REFUELING STATION ACCESS PANEL INBOARD HINGE CORNER SDR EE4Y20110117Doubler · crackedDOUBLER CRACKED LOCATED LT WING UPPER SURFACE AT STA XCW110 MLGSDR SWIA201125704Skin · crackedCRACK ON THE LOWER WING SKIN NEAR WS 148.018 IN THE AREA OF THE REAR SPAR. (SERVICE) REPAIRED PER REO.SDR FDEA201102210652Skin · crackedRT WING FIXED L/E SKIN UPPER CUTOUT FOR NR 2 SLAT INBD JACKSCREW, FOUND CRACKED. REPAIRED AS PER SRM 57-41-12 FIGURE 203, REVISION 19. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112. REPAIR CLASSIFIED CATEGORY B. TO PERFORMED DETAILED VISUAL INSPESDR FDEA201102210656Skin · crackedRT WING LOWER SKIN PANEL INBD OF RIB 9 OF REAR SPAR NEAR ACCESS PANEL 675FE FOUND CRACKED, APPROX 0.250 INCH LONG DURING HIGH FREQUENCY EDDY CURRENT INSPECTION. REPAIRED AS PER EA 6-5710-143870 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112SDR FDEA201102210654Skin · crackedLT WING LOWER SKIN PANEL INBD OF RIB 9 OF REAR SPAR NEAR ACCESS PANEL 575FE FOUND CRACKED APPROX 0.375 IN LONG DURING HIGH FREQUENCY EDDY CURRENT INSP. REPAIRED AS PER EA 6-5710-143871 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REVISION 112.SDR FDEA201102180628Skin · crackedLT WING FIXED T/E PANEL UPPER SURFACE AT APPROX STA 1270, FOUND CRACKED. REPAIRED AS PER SRM 57-51-12 FIGURE 210 REV 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.SDR FDEA201102180629Skin · crackedLT FIXED T/E PANEL UPPER SURFACE AT APPROX STA 1260, FOUND CRACKED. REPAIRED AS PER SRM 57-51-12 FIGURE 210 REV 74. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 REV 111.SDR DALA1115900136Skin · crackedHFEC OPEN HOLE INSP CARRIED OUT ON RT WING UPPER LINK PITCH LOAD FITTING, COMMON TO WING IN REF TO SB B767-54-0081, FIG 38, REV 1 AND FOUND 03EA HOLES WITH CRACK INDICATION ON UPPER SKIN. 03 EA HOLES ON RT WING UPPER SKIN REPAIRED IAW ER/A 488787-14AD, REV SDR IPXA1M65050Skin · crackedINSPECTION TYPE:3C, LT WING L/E UPPER SKIN CRACKED AT OTBD CORNER OF SLAT DEICE DUCT CUT-OUT, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-01. REPAIR 10, FIG 201 ON WING SKIN STA XOS464-470.SDR FDEA201102170602Skin · cracked07 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND STA XORS 713.65. ACCESS DOOR CUTOUT REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. REPSDR FDEA201102170601Skin · cracked09 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS 683.4 AND XORS 713.65. ACCESS DOOR CUTOUT REPAIR CARRIED OUT AS PER DRAWING SG11570004 REVISION A. SDR AALA20110217DWH01Skin Panel · damagedLEFT WING LOWER SKIN PANEL DAMAGED. ACCOMPLISHED EXTERNAL DOUBLER REPAIR PER EA MD80-57-015247.SDR DALA1121126904Skin · corrodedAFTER REMOVAL OF OVERWING FILLER CAP FOUND SKIN CORRODED AROUND EDGE CUTOUT, LEFT WING. COMPLIED WITH ERA 490329-14 REV ORIG AT SAA DURING HMV ON NR CARD 172786.SDR SWIA201125769Skin · crackedBOTH WING LOWER PLANKS AT WS 148 CRACKED AT AFT AREA. (C-CHECK) REPAIRED PER REO.SDR ASAA1199038Skin Panel · wornWING LEADING EDGE SKIN PANEL WORN UNDER NR 2 PYLON PANEL 441CL MATING SURFACE. REMOVED DAMAGED SKIN PANEL FABRICATED REPLACEMENT PANEL AND INSTALLED IAW BOEING DRAWING 116A4411 REV B AND B737 900 SRM 57 41 01.SDR EE4Y20110104Skin · corrodedDURING THE INSPECTION, WING CTR SECTION, FOUND THE UPPER SKIN BETWEEN XCW 42 AND XCW 58.688 AND BETWEEN STR 6 AND 9 LT SKIN CORRODED.SDR ASAA1149194Skin Panel · dentedRT FIXED WING PANEL UPPER SURFACE (FWD OF NR 5 SPOILER) HAS A CLUSTER OF DENTS. REPAIRED PANEL IAW B737 400 SRM 51 70 10 REPAIR 4.SDR IPXA11664857Panel · elongatedINSPECTION TYPE:C, LT WING NR 5 SLAT LWR CLOSURE PANEL RIVET HOLE ELONGATED. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5K, FIG 16,
REV 49 .SDR REXA201100094Skin · corrodedRIGHT WING LOWER PLANK ACCESS HOLES AT WS 54.897, WS 76.161, WS 116.366 AND WS 209.040 HAVE CORROSION NOT IN CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR REXA201100091Skin · corrodedLEFT WING LOWER PLANK ACCESS HOLES AT WS 12.245, WS 54.897, WS 76.161, WS 188.040, WS 209.040 AND WS 230.415 HAVE CORROSION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR QXEA2011021000132Panel · chafedC6 CHECK - RT SLAT LOWER T/E IS CHAFED INTO PANEL 622CB. BLENDED CHAFE DAMAGE, PERFORMED FPI ON AREA IAW NDTM 51-20-08, NO EVIDENCE OF CRACKS FOUND. SENT ENGINEERING REQUEST TO MFG. RECEIVED ENGINEERING REO 670-57-42-288, AREA IS OK AS BLENDED. TREATED, PRSDR IPXA1564947Skin · chafedINSPECTION TYPE:MOD, RT WING LOWER SKIN AT FSS 295 IS CHAFED FROM 7-14 INCHES AFT OF THE SKIN L/E. REPAIRED IAW SRM 57-20-01-1A1, EO B757-5730-41559-A, DATED 23 FEB 2011, AND ATS ER 11-01575 DATED 23 FEB, 2011.SDR IPXA1564946Skin · chafedINSPECTION TYPE:MOD, LT WING LOWER SKIN IS CHAFED AT FSS 295, FROM 2-14 INCHES AFT OF THE SKIN L/E. REPAIRED IAW SRM 57-20-01-1A1, ATS ER 11-01575, DATED 23, FEB 2011, EO B757-5730-41559-A DATED 23, FEB 2011.SDR IPXA11M64843Doubler · crackedINSPECTION TYPE:3C, THRU ACCESS 619CB, RT WING L/E COMPARTMENT, BEADED DOUBLER FOUND CRACKED AT 2 LOCATIONS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.SDR IPXA11M64842Doubler · crackedINSPECTION TYPE:3C, RT WING L/E COMPARTMENT INBD OF SLAT TRACK NR 12, BEADED DOUBLER FOUND WITH SUSPECTED CRACK. REMOVE DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.SDR IPXA11M64840Doubler · crackedINSPECTION TYPE:3C, RT WING L/E COMPARTMENT, OTBD OF SLAT TRACK NR 9, BEADED DOUBLER FOUND CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.SDR IPXA1M64810Doubler · crackedINSPECTION TYPE:3C, IN LT WING L/E COMARTMENT CEILING DOUBLER IS CRACKED AT 2EA FASTENERS AT XOS669 APPX CUT OUT DAMAGE AT LT WING L/E COMPARTMENT BEADED DOUBLER. FABRICATED 1, 1EA FILLER, 3EA ANGLES AND 1EA DOUBLER AND INSTALLED AT LT WING L/E COMPARTMENT AT SDR DALA1109059864Panel · delaminatedRT WING T/E FIXED PANEL INBD OF AILERON IS DELAMINATED. APPROX 36 SQ INCHES. R & R PANEL IAW SRM 51-30-01 AND 51-30-2. REPAIRED UPPER T/E SPAR IAW ERA 488339-147. REQUIRED INSP COMPLETED.SDR IXXA110014SSkin · crackedDURING INSP FOR AD2008-26-07 AND SB DC8-57A102 FOUND LT WING LOWER SKIN CRACKED AT STRINGER 62 IN THE 14TH FASTENERS ROW OTBD FROM STA XW408 CENTERLINE PROPAGATING APPROX .300 FWD AND .050 AFT. REPAIR WAS ACCOMPLISHED IAW SRM 57-2-1 FIGURE 45 TR NUMBER 57-1SDR UIEA2011020500046Skin · damagedMAJOR REPAIR. DURING A-CHECK BEING PERFORMED, MX FOUND THE LT WING ILES 718.80; UPPER L/E PANEL - EXTERNAL SKIN WITH CRACK/DELAMINATION DAMAGE , MEASURING 24.0 INCHES LONG, LOCATED 4.5 INCHES FROM THE AFT END OF THE L/E PANEL. REF FIG 1. PERMANENT REPAIR PESDR USAA2011020890601Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING ACCESS PANEL 540QB. REPLACED LEFT WING ACCESS PANEL 540QB IAW A319 SRM 57-27-11.SDR IXXA11SMN025SSkin · dentedDURING ROUTINE C-CHECK INSP, FOUND RT WING OTBD FLAP UPPER SKIN SHOWS DENTS AT STA XF 380.000. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALSDR FDEA201102030460Skin · cracked05 EA FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT STA XORS= 683.4 TO XORS= 713.6. CARRIED OUT RECTIFICATION AS PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVSDR FDEA201102030459Skin · cracked08 EA, FASTENER HOLES FOUND CRACK INDICATION DURING OPEN HOLE HFEC INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT STA XORS= 683.4 TO XORS= 713.6. CARRIED OUT RECTIFICATION AS PER DRAWING SG11570004 REVISION A. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 RESDR A6WA201140156Access Panel · corrodedFUEL CUT OUT 540BB HAS FRETTING, CORROSION. REPAIRED FUEL CUT OUT 540BB IAW REO 601R-57-21-030, REV H.SDR USAA2011020890599Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING ACCESS PANEL 540PB. REPLACED LEFT WING ACCESS PANEL 540PB IAW A319 SRM 57-27-11.SDR USAA2011020890598Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING ACCESS PANEL 640KB. REPLACED RIGHT WING ACCESS PANEL 640KB IAW A319 SRM 57-27-11.SDR EE4Y1101034Access Panel · corrodedLT WING L/E SECTION , LOWER ACCESS PANEL NR 1144C UPPER SUFACE CORRODED. THE DAMAGE REQUIRED REPAIR APPROVAL.SDR IXXA11SMN017SSkin · crackedDURING ROUTINE C-INSP FOUND LT WING LOWER INNER SKIN CRACKED AROUND STRINGER 60 AT STA XW 408.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND FILLER. CSDR IPXA1M64742Skin · crackedINSPECTION TYPE:4C, RT TELESCOPIC DUCT CUTOUT XOS 464-470 HAS CRACK ON OTBD UPPER CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-01, REPAIR 10, FIG 201.SDR GUUA95157020111ASkin · corrodedDURING SCHEDULED ROUTINE INSP, DISCOVERED RT WING UPPER SKIN T/E CORROSION AND DEBOND BETWEEN WING STATIONS 127.00 THROUGH 174.00 JUST FWD OF NR4 FLAP. REMOVED DAMAGE AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR USAA2011020890593Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING ACCESS PANEL 540NB. REPLACED LEFT WING ACCESS PANEL 540NB IAW TASK CARD 26C50057092.SDR USAA2011020890592Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT WING ACCESS PANEL 540KB. REPLACED LEFT WING ACCESS PANEL 540KB IAW A319 SRM 57-27-11.SDR USAA2011020890591Access Panel · corrodedSAL - MAJOR REPAIR - S4 CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING ACCESS PANEL 640LB. REPLACED RIGHT WING ACCESS PANEL 640LB IAW A319 SRM 57-27-11.
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