JASC 5740
Service difficulty reports · 3,003
Reports filed under 5740 · Wing, Attach Fittings, 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 = '5740' 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 = '5740' 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 YENA2023031400236None · noneDURING HEAVY MAINTENANCE: CRACK ON FIXED LEADING EDGE BTW RIB 19/20 AT LH WING; CRACK ON FIXED LEADING EDGE BTW 19/20 AT LH WING WAS REPAIRED PER EMB190 SRM 57-49--1. REPAIR 51P AND SDR ARE REQUIRED. O REF TOMX WO 2162 NR 00015 FOR WORK PERFORMED).SDR V0XR20230426AV1Bracket · crackedLH AILERON I/B HINGE FITTING UPPER SURFACE FWD NUTPLATE HOLE CRACKED AT THE 12:00 POSITION. REMOVED AND REPLACED L/H AILERON I/B HINGE FITTING IAW EMB 145 SRM 5140-02 AND SRM 51-20-03SDR SWAA2023031512987Channel · brokenL/H WING AFT C CHANNEL BROKEN UNDER PANEL 561AB MARKED<[01] REMOVED AND REPLACED C CHANNEL BRACKET PER SRM 51-40-02SDR UIEA2023022300188None · noneLH WING #6 L/E SLAT (P/N 114T3100-401G, S/N 000010) SKIN BIRD STRIKE DENT DAMAGE - TIME LIMIT REPAIR(<P>IT WAS REPAIRED IN ACCORDANCE WITH ATLAS EO 1957A609 / SRM 57-43-01-2R-2 REPAIR 2</P>)SDR R61A2023021900156Spar · cracked170EO-57-20-0050MA_1 RIGHT-OUTBOARD-MAIN WING SPAR 1 INSPECTION AND REWORK SB57-73G1P2. ROUTINE TASK CARD COMPLIED WITHSDR R61A2023021900155Spar · cracked170EO-57-20-0050MA_1 RIGHT-OUTBOARD-MAIN WING SPAR 1 INSPECTION AND REWORK SB57-73G1P2. ROUTINE TASK CARD COMPLIED WITHSDR SWAA2023031304213Panel · crackedLT WING L/E PANEL 521ZB O/B FWD CORNER IS CRACKED<[01] IDENTIFIED PANEL 521ZB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 2; SHEET1; TABLE 2; ITEM [1]. <BR><BR>CLEANED PANEL AND REMOVED FINISH ON TOOL SIDE TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C. ANSDR DALA2023021401155None · noneSHIP 3307 DURING HCK AT SAL, THE L/H RIB 6 FITTING FORWARD LUG WAS FOUND CORRODED. A REPAIR WAS ACCOMPLISHED PER SECT I OF ERA 605358-14AD. CORRECITVE ACTION: REF ER/A 605358-14AD. (2623515)SDR ASAA2023020742593Skin · unknownL/WING SLAT 5 HAS THREE BURN MARKS ON TOP SKIN APPROX. 9" AND 7.5" OUTBD. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MAJOR REPAIR ON L/WING SLAT 5 L/E SKIN AT TRACK 11 IAW EA CMPT-57EA-01716 AND SRM 57-40-00-300-216.SDR ASAA2023020742592Skin · damagedL/WING SLAT 5 HAS ONE BURN MARK ON TOP SKIN L/E APPROX. 1.5" OUTBD OF TRACK 11. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MAJOR REPAIR ON L/H WING SLAT 5 L/E SKIN AT TRACK 11 IAW EA CMPT-57EA-01716 AND A320 SRM 57-40-00-300216.SDR SWAA2023030298025Panel · debondedPANEL 521CB IS DISBONDED AT CORNER<[01] IDENTIFIED PANEL 521QB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 5; TABLE 5; ITEM [3]. <BR>CLEANED PANEL AND REMOVED FINISH AS NEEDED TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C. AND D. <BR><BR>VISUAL INSPECTIONSDR SWAA2023030298026Panel · debondedPANEL 521WB IS DISBONDED AT CORNER<[01] IDENTIFIED 521WD PANEL IAW SRM 57-41-01-0I-4 PARA FIGURE 2; ITEM 1; TABLE 2.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 51-41-01-1A-1 PARA 4.A.(5)<BR><BR>REMOVED BONDED ALUMINUM FOIL TO FACILITATE REPAIR.<SDR SWAA2023030298027Panel · debondedPANEL 521JB IS DISBONDED AT CORNER<[01] IDENTIFIED PANEL 521JB MATERIAL IAW SRM 57-41-01-0I-4; FIGURE 4; TABLE 4; ITEM [1].<BR><BR>CLEANED PANEL AND REMOVED FINISH AS NEEDED TO EVALUATE DAMAGE IAW AMM 51-21-11-150-815 PARA. 17. C. AND D.<BR><BR>VISUAL INSPECTISDR SWAA2023031097736Panel · delaminatedPANEL 621PB HAS DELAMINATION AT FWD INBOARD CORNER<[01] IDENTIFIED PANEL MATERIAL IAW SRM 57-41-01-0I-4 FIGURE 3; TABLE 3; ITEM [1] AND DWG DOC: 116A9110 ID: 0026 <BR><BR>PANEL FWD INBOARD CORNER IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PAR. 4.ASDR YENA2023013100123None · noneDURING HEAVY MAINTENANCE: CRACK ON RIB 22 OF WING LEADING EDGE SKIN AT LH WING; REF TECH OPS WO: N187/ 2037 NR-00183 - RIB 22 OF WING LEADING EDGE SKIN OF LH WING WAS REPLACED PER EMB 190 SRM 51-43-04.SDR YENA2023013100122None · noneDURING HEAVY MAINTENANCE: CRACK ON RIB 17 OF WING LEADING EDGE SKIN AT RH WING; REF. TECH OPS WO: N187JB / 2037 NR-00184 - RIB 17 OF WING LEADING EDGE SKIN AT RH WING WAS REPLACED PER EMB 190 SRM 51-43-04, AND SRM 51-42-02.SDR YENA2023013100121None · noneDURING HEAVY MAINTENANCE: CRACK ON RIB 17 OF WING LEADING EDGE SKIN AT LH WING; REF TOMX W/O 2037 NR 00182. RIB 17 OF WING LEADING EDGE SKIN AT LH WING WAS REPLACED PER EMB 190-SRM 51-41-02, EMB-190 SRM 51-42-02, AND EMB-190 SRM 51-43-04.SDR YENA2023013100118None · noneDURING HEAVY MAINTENANCE: CRACK ON FIXED LEADING EDGE BTW RIB 19 TO RIB 20 (UPPER AREA) AT LH WING; REF TOMX W/O 2037 NR 00047. LEADING EDGE BTW RIB 17 TO RIB 22 (UPPER AREA) AT LH WING WAS REPLACED PER EMB 190 SRM 51-41-01, EMB-190 SRM 51-42-02, EMB-190 SRMSDR DALA2023013100791None · noneSHIP 3161 - CORROSION REMOVAL WAS REQUIRED ON THE L/H MLG ACHORAGE FITTING. CORRECTIVE ACTION: CORROSION REMOVAL WAS REQUIRED ON THE L/H MLG ACHORAGE FITTING AND WAS REPAIRED IAW A319 SRM 57 -26-13. (2595066)SDR SWAA2023011791173Attach Bracket · damagedRT WING /L/E AT FSS150 DUCT BRAKET ATTACH HOLES ELONGATED<[01] REMOVED AND REPLACED BRACKET PER SOPM 20-50-01;[02] REMOVED AND REPLACED BRACKET PER SOPM 20-50-01SDR HYIA20230113001Fitting · damagedDURING MAINTENANCE, A SPOT OF DAMAGE WAS VISUALLY IDENTIFIED ON THE RH FWD WING ATTACH FITTING (PN: 082550-46). THIS DAMAGE IS LOCATED ON THE TOP EDGE OF THE FITTING AS SEEN THROUGH THE WING GAP PANEL 611AT INBOARD OF RWS 58.94. THIS DAMAGE MEASURES APPROXIMASDR LR7A202301043260Splice · corrodedDURING SCHEDULED B-3 CHECK UNDER SB 382-57-82, FOUND RH OW UPPER FWD CORNER SPLICE FITTING WITH MULTIPLE FASTENER HOLES CORRODED AT OWS3-10R, FS517, WL287. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM CH. 51-70. NR# 1000796217. / PSE# 57-50-SDR LR7A2023010403259Splice · corrodedDURING SCHEDULED B-3 CHECK UNDER SB 382-57-82, FOUND CORRODED FASTENER HOLE ON LH OW UPPER FWD CORNER SPLICE FITTING AT OWS3L, FS517, WL287. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM CH. 51-70. NR# 1000796213. / PSE# 57-50-05, AD 2012-06-SDR LR7A2023010403257Attach Plate · crackedDURING SCHEDULED B-3 CHECK UNDER SB 382-57-82 , FOUND MULTIPLE DEFECTS IN RH OUTER WING LOWER PANEL ATTACH HOLES WITH MULTIPLE CRACKS AT FS517-579, OWS3.5-6.5L, WL255-260. / REPAIRED IAW LAC MEA 382-57-22-087. NR# 1000777936. / PSE# 57-50-02, AD 2012-06-09.SDR LR7A2023010403256Fitting · crackedDURING SCHEDULED B-3 CHECK UNDER SB 382-57-82 , FOUND MULTIPLE DEFECTS IN LH OUTER WING LOWER PANEL ATTACH HOLES WITH MULTIPLE CRACKS. REPAIRED IAW LAC MEA 382-57-22-086.SDR LR7A2023010403251Fitting · corrodedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTER WING LOWER AFT CORNER FITTING CORRODED AT FS597, OWS0R, WL265. REPAIR BY REPLACEMENT ACCOMPLISHED IAW SMP583 SRM, CH. 51-60 & 51-70.SDR LR7A2023010543250Fitting · corrodedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTER WING UPPER AFT CORNER FITTING CORRODED AT FS597, OWS0R, WL285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000796219. / PSE# 57-50-05, ASDR LR7A2023010543249Fitting · corrodedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND RH OUTER WING LOWER FORWARD CORNER FITTING CORRODED AT FS517, OWS0R, WL265. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000796218. / PSE# 57-50-04SDR LR7A2023010403247Fitting · corrodedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH OUTER WING LOWER AFT CORNER FITTING CORRODED AT FS597, OWS0L, WL265. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000796216. / PSE# 57-50-04, ASDR LR7A2023010543246Fitting · corrodedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH OUTER WING UPPER AFT CORNER FITTING CORRODED AT FS597, OWS0L, WL285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000796215. / PSE# 57-50-05, ADSDR LR7A2023010543245Fitting · corrodedDURING SCHEDULED B-3 CHECK WHILE PERFORMING OTHER MAINTENANCE, FOUND LH OUTER WING LOWER FORWARD CORNER FITTING CORRODED AT FS517, OWS0L, WL265. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SMP583 SRM, CH. 51-60 & 51-70. NR# 1000796214. / PSE# 57-50-04, SDR LR7A2023010403243Fitting · corrodedDURING SCHEDULED B-3 CHECK UNDER SB382-57-82, FOUND RH OUTER WING LOWER RAINBOW FITTING CORRODED AT FS517-596, OWS0R, WL263. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SB 382-57-95. NR# 1000777926. / PSE# 57-50-02, AD 2012-06-09SDR LR7A2023010403242Fitting · corrodedDURING SCHEDULED B-3 CHECK UNDER SB382-57-82, FOUND LH OUTER WING LOWER RAINBOW FITTING CORRODED AT FS517-596, OWS0L, WL263. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SB 382-57-95. NR# 1000777926. / PSE# 57-50-02, AD 2012-06-09SDR LR7A2023010403241Fitting · corrodedDURING SCHEDULED B-3 CHECK UNDER SB382-57-82, FOUND RH OUTER WING UPPER RAINBOW FITTING CORRODED AT FS517-596, OWS0R, WL285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SB 382-57-95. NR# 1000777926. / PSE# 57-50-01, AD 2012-06-09SDR LR7A2023010543240Fitting · corrodedDURING SCHEDULED B-3 CHECK UNDER SB382-57-82, FOUND LH OUTER WING UPPER RAINBOW FITTING CORRODED AT FS517-596, OWS0L, WL285. / REPAIR BY REPLACEMENT ACCOMPLISHED IAW LOCKHEED SB 382-57-95. NR# 1000777926. / PSE# 57-50-01, AD 2012-06-09SDR SWAA2023012682295Attach Bracket · crackedLEFT WING T/E BULB SEAL ATTACH BRACKET UNDER DEFLECTION CONTROL RIB AT ORSS 261+11 IS CRACKED.<[01] REMOVED AND REPLACED T/E BULB SEAL ATTACH BRACKET UNDER DEFLECTION CONTROL RIB ORSS 261+11 P/N 115A2953-1 IAW SRM 51-40-02 AND AIPC 57-50-00-25;[02] VERIFIED COSDR SWAA2022122979217Fitting · crackedCRACK ON FITTING LOCATED AL LEVEL ORSS 271 TRAILING EDGE AT RT WING 2022-688300<[01] REPLACED FITTING LOCATED AL LEVEL ORSS 271 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] CERTIFIED WORK PERFORMED.SDR FDEA202212072887Drag Fitting · corrodedHOLE #2 AND 5 ON UPPER SKIN AND DRAG FITTINGS PRESENT CORROSION RH WING. WORKS STEPS ACCOMPLISHED ON EA #: F5730-T0371761 MAJOR REPAIR.SDR FDEA202212072886Drag Fitting · corrodedHOLES 4 & 5 ON LT WING UPPER SKIN DRAG FITTINGS PRESENT CORROSION. WORKS STEPS ACCOMPLISHED ON EA F5730-T0371760 EA TITLE: WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, CORROSION FINDINGS* THIS EA DEVIATES FROM EO F-5730-E0340076. MAJORSDR FDEA202212072885Beam · corrodedRIGHT WING, AILERON BALANCE WEIGHT ATTACH BEAM IS CORRODED REMOVED AND REPLACED BEAM IAW BAC DWG 113N7100, SHEET 2, REVISION L AND B757 SRM 51- 40-02.SDR FDEA202212072884Bracket · crackedLEFT WING LEADING EDGE UNDER PANEL 511KT OUTBOARD SIDE L-BRACKET BROKEN/CRACKED REMOVED AND REPLACED CRACKED L-BRACKET ON LEFT WING LEADING EDGE UNDER PANEL 511KT OUTBOARD SIDE, WITH NEW BRACKET P/N 313N5004Y15, P.O # 1044727.1 IAW BAC DWG 313N5004, REV CSDR HYIA20221205001Fitting · corrodedDURING MAINTENANCE AN AREA OF CORROSION WAS VISUALLY IDENTIFIED ON THE TOP EDGE OF THE VERTICAL LEG OF THE FORWARD LEFT HAND LOWER AFT WING FITTING. CORROSION MEASURES APPROXIMATELY 1.25 INCHES LONG, WITH A MAX DEPTH OF APPROXIMATELY .017 INCHES DEEP AND IS CSDR FDEA202211212823Drag Fitting · corrodedLH WING DRAG FITTING HOLE 9 HAS CORROSION AND A CRACK INDICATION IN THE FITTING LAYER AT 3 O'CLOCK WINGS-PLATES AND SKINS-LH WING, UPPER SKIN AT PYLON DRAG FITTING, CORROSION FINDINGS THIS EA DEVIATES FROM EO F-5730-E0340076 . COMPLIED WITH EA F-5730-T037SDR AALA202211224833Strap · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING INBOARD LEADING EDGE LOWER ATTACH STRAP LOCATED FROM WS 94.24 TO WS 156.25. REPAIRED PER DWG 112A4402 AND EA 340171.SDR SWAA2022111670386Attach Angle · crackedRT WING; FWD ATTACH ANGLE CRACKED FOR PANEL 651AT ATTACH CHANEL RT WING FWD ATTACH ANGLE CRACKED FOR PANEL 651AT ATTACH CHANEL / [01] REMOVED AND REPLACED ANGLE BRACKET IAW SRM 51-40-04SDR HYIA20221114001Attach Fitting · corrodedDURING MAINTENANCE A SPOT OF CORROSION WAS VISUALLY IDENTIFIED ON THE LEFT HAND UPPER AFT OUTBOARD FORWARD WING ATTACH FITTING (P/N: 0822550-45). IT IS LOCATED ON THE BOTTOM FACE OF THE UPPER HORIZONTAL LEG OF THE FITTING AND MEASURES APPROXIMATELY .674 INCHESSDR IXXA2022110900002Bracket · corrodedRIGHT WING TRAILING EDGE SUPPORT BRACKET ATTACHING TO FUSELAGE FOR PANEL HAS CORROSION BL. 70.50 STATION 1158.SDR DALA2022110907229None · noneSHIP 3239 LH MLG RETRACT ACTUATOR ANCHORAGE FITTING HAS CORROSION/PITTING. CORRECTIVE ACTION: REPAIRED LH ANCHORAGE FITTING PER A320 SRM 57-26-13. (2488579)SDR DALA2022110907228None · noneSHIP 3239 R/H MLG RETRACT ACTUATOR ANCHORAGE FITTING HAS CORROSION. CORRECTIVE ACTION: REWORKED R/H MLG RETRACT ACTUATOR ANCHORAGE FITTING PER A320 SRM 57-26-13. OK FOR SERVICE. (2488562)SDR SWAA2022112968690Fitting · crackedCRACK SLAT ACTUATOR FITTING LOCATED SLAT STATION 202.45 AT LT WING 2022-635919EXACTLY LOCATION OF CRACK: CRACK IS LOCATED ON LOWER SKIN OF SLAT 3 AT SLAT STATION 202.45 (COMMON TO THE ACTUATOR RIB). PERFORMED REPAIR ON LOWER SKIN LOCATED ON SLAT #3 STATION 19
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