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 FDEA201211274188Fitting · corrodedCORROSION WAS FOUND ON RT RIB5 FWD LUG BORE AND BOTH SIDE OF THE SPOTFACE OF RIB 5 FWD LUG. 1 IAW EA 6-5740-149078 ACCOMPLISHED THE CORROSION REPAIR. 2 EA 6-5740-149078.SDR ASOA2012121302645Attach Angle · crackedRT L/E 630JL ATTACHMENT ANGLE AT INBD TRANSITION CRACKED. R & R DAMAGED L/E 630JL ATTACHMENT ANGLE AT INBD TRANSITION IAW SRM 51-40-11 AND AMM 20-21-80-910-801.SDR DALA1256950183Tee Fitting · damagedLT WING SIDE LINK FITTING INBD AND OTBD LOWER TEE CLIPS FASTENER HOLES SHORT EDGE MARGIN. REPAIRED IAW ERA 507544-14AD, REV ORIG SECTION I.SDR HYIA20121121001Attach Fitting · corrodedDURING A SCHEDULED MAINTENANCE EVENT, AT REMOVAL OF LT WING TO FACILITATE OTHER MX, THE LT AFT LOWER FUSELAGE FITTING WAS FOUND TO BE SEVERELY CORRODED. FITTING, PN IS 5011024-2, ASSUMED TO BE ORIGINAL FROM ACFT MFG WITH 31,645.5 HOURS TT IN SERVICE. REMOVEESDR DALA1256940183Tee Fitting · damagedRT WING SIDE LINK FITTING INBD AND OTBD LWR TEE CLIPS FASTENER HOLES SEM. REPAIRED IAW ERA 507545-14AD, REV ORIG SECTION I.SDR SWAA2012112609850Bolt · corrodedLEFT WING NR 3 SLAT OUTBOARD TRACK AFT UPPER BOLT IS CORRODED AND MISSING PLATING. REMOVED AND REPLACED BOLT AT LEFT WING NR 3 SLAT O/B MAIN TRACK AFT UPPER IAW B737 AMM 57-54-01.SDR DALA1256530183Fitting · crackedRIGHT WING UPPER LINK PITCH LOAD FITTING AND WING UPPER SKIN PANEL HOLE CRACKED. REPAIRED IAW ERA 507538-14AD, REV ORIG.SDR REXA2012111201517Structure · chafedRIGHT INBOARD IS CHAFED SEVERAL AREAS BETWEEN SLAT TRACK 1-1 AND TRACK 1-3. REPAIRED IAW SRM 57-41-01.SDR REXA2012111201516Structure · crackedLEFT INBOARD IS CHAFED SEVERAL AREAS BETWEEN SLAT TRACK 1-1 AND TRACK 1-3. REPAIRED IAW SRM 57-41-01.SDR HYIA20121108001Attach Fitting · crackedDURING REPLACEMENT OF WING SPAR STRAP ON RT WING, OTBD ENGINE BEAM FITTING WAS DISCOVERED TO BE CRACKED IN TWO LOCATIONS. OPENSDR AALA20121030003Attach Fitting · crackedLEFT WING WINGLET ADAPTER PLUG ATTACH FLANGE CRACKED. REMOVED DAMAGE AND INSTALLED ANGLE, FILLER AND NUT PLATE CHANNEL PER EA 757-57-026567 REVISION A.SDR FDEA201210263755Bracket · crackedRT WING AFT OF REAR SPAR AT NR 2 ENG PYLON INTERFACE PANEL ATTACH WEB TO BOTTOM WING SKIN CRACKED 2EA.PLACES. MEASURED 2", AND 1.8" IN LENGTHS. R & R RT WING NR 2 PYLON AFT ATTACH WEB (BRACKET) REF TO SRM 51-72-10. PERFORMED OPS CHECK AND LEAK CHECK REF TO SDR FDEA201210263754Bracket · crackedLEFT WING AFT OF REAR SPAR AT ENG PYLON INTERFACE ATTACH WEB TO BOTTOM WING SKIN CRACKED AT ATTACH FASTENERS. MEASURED 1.5", 1.2", AND .7" IN LENGTHS. R & R LT WING NR 1 PYLON REAR SPAR AT AFT ATTACH WEB REF TO SRM 51-72-10. LEAK AND OPS CHECKED GOOD IAW AMMSDR FDEA201210233726Fitting · damagedRIGHT WING, SIDE LINK FITTING HOLE "H" FOUND TO BE OVERSIZED. REPAIRED IAW EA F5740-162444. MAJOR REPAIR.SDR DALA1251310924Attach Angle · crackedLEFT WING ATTACH ANGLE CRACKED IN TWO PLACES LWS 993. REPAIRED IAW ER/A 507061-14 REV 0.SDR EE4Y2012102500316Anchor Fitting · corrodedDURING THE INSPECTION, FOUND THE RT AND LT MLG RETRACTION JACK ANCHORAGE FITTING CORRODED. THE FITTINGS WERE REPAIRED IAW 70568467/005 SRM, UNDER NON ROUTINE ITEM : WO A1A166, SUB JOB 5 ITEM 3 AND SUB JOB 6 ITEM 5.SDR FDEA201210173647Attach Fitting · crackedLEFT WING T/E LOWER ATTACH FITTING AT APPROX XORS 433 FOUND CRACKED. REPLACED IAW SRM 51-31-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 115.SDR DALA1250300182Fitting · mismanufacturedRT WING SIDE LINK FITTING FASTENER HOLES FOUND FOUND INTERFERING WITH RADIUS OF MILL STEP. SIDE LINK REWORKED IAW ERA 503735-16.SDR DALA12009823271Bracket · damagedDURING INSPECTION, FOUND RT OTBD FLAP CUSHION SEAL UPPER RETAINING SCREW HOLE MISDRILLED ON NR 1 FLAP RIB. R & R RIB 1 BRACKET IAW SRM 51-42-11.SDR EE4Y2012100900293Fitting · corrodedDURING INSPECTION, FOUND THE RT AND LT MLG RETRACTION JACK ANCHORAGE FITTING CORRODED. THE FITTING WAS REPAIRED IAW 70567813/007.SDR 6CBA20121005122Adapter · faultyTRIM RUNAWAY AURAL WARNING, NO YOKE MOVEMENT. THE KTA-2810 TRIM ADAPTER, PN 065-00195-0100 WAS FOUND TO BE FAULTY. IT WAS R & R WITH A NEW UNIT IAW THE AMM 12-B-22-10-07-00A-920A-A. THE AUTO PILOT SYS OPERATIONALLY TESTED GOOD IAW 12-B-22-10-00-00A-903A-A.SDR HNAA2012100100991Bolt · rustedLEFT AFT STEEL STRUT TO WING RIB BOLT IS RUSTED AND BORE OF STRUT. REAMED HOLE TO .541 IAW DWG 85320229. CLEANED CORROSION AND R & R BOLT AND NEW PLI WASHERS.SDR FDEA201209203372Bracket · corrodedLT WING AILERON OTBD BONDING WIRE ATTACHMENT, HINGE BRACKET RIB CORRODED. REMOVED AND REPLACED RIB ASSY, WS 817.27, IAW SRM 51-40-02 AND DWG 113N1501 DUE TO OUT OF LIMITS PER SRM 57-51-09, FIG 101, DETAIL IV. REPAIR IS CLASSIFIED AS A MAJOR REPAIR.SDR FDEA201209203361Attach Fitting · corrodedRT WING T/E PANEL NR 641JB SUPPORT ATTACHMENT FOUND CORRODED. REPAIRED IAW EA1-5710-162382. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201209203360Attach Fitting · corrodedLEFT WING PANEL ATTACHMENTS FOUND CORROSION. REPAIRED IAW EA 1-5710-162381. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.SDR FDEA201209133309Fitting · corrodedRIB 5 FWD LUG CORRODED. REPAIRED IAW EA 6-5740-149059.SDR ASOA20120909101Bushing · migratedDURING C-CHECK, LT GROUND SPOILER OTBD ATTACHMENT BRACKET INBD HAT BUSHING MIGRATED ON WING. MX R & R LT GROUND SPOILER OTBD ATTACHMENT BRACKET IAW AMM 57-51-02 AND EC5740-01288. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20120909099Bushing · migratedDURING C-CHECK RT GROUND SPOILER INBD ATTACHMENT FITTING, OTBD HAT BUSHING IS MIGRATED (ON WING). MX R & R RT GROUND SPOILER INBD ATTACHMENT FITTING IAW AMM 57-51-02 AND EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120909098Attach Fitting · migratedDURING C-CHECK RT GROUND SPOILER OTBD ATTACH FITTING INBD HAT BUSHING IS MIGRATED (ON WING). MX R & R RT GROUND SPOILER OTBD ATTACHMENT FITTING (ON WING) IAW AMM 57-51-02 AND EC5740-01288. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ASOA20120909097Bushing · migratedDURING C-CHECK, LT GROUND SPOILER INBD ATTACH BRACKET OTBD HAT BUSHING MIGRATED. MX R & R ATTACH BRACKET IAW AMM 57-51-02 AND EC5740-01288. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASOA20120909096Bushing · migratedDURING C-CHECK, LT GROUND SPOILER CENTER ATTACH BRACKET INBD HAT BUSHING MIGRATED ON WING. MX R & R ATTACHING BRACKET ON WING IAW AMM 57-51-02 AND EC5740-01288. ACFT APPROVED FOR RETURN TO SERVICE.SDR ASAA2012090792881Attach Angle · crackedLEFT WING FIXED T/E SEAL RETAINER ATTACH ANGLE CRACKED, WS ORSS274. R & R ATTACH ANGLE.SDR ASOA20120905136Bracket · gougedACFT CURRENTLY IN A C-CHECK STATUS WHEN INSPECTION FOUND THE RT AILERON PCA BRACKET WITH DAMAGE TO THE LOBES OF THE BRACKET. MX R & R THE PCA BRACKET IAW EC 5750-01077. ALL WORK ACCOMPLISHED AND WILL BE RELEASED AT THE END OF THE CHECK.SDR IPXA2M75290Fitting · crackedINSPECTION TYPE: 3C, RT LOWER WINGLET FWD MOUNT FITTING CRACKED. REPLACED BOTH ATTACH FITTINGS ON RT LWR WINGLET WITH KIT SB11570063-5, APPX E. (MAJOR)SDR ASOA20120904093VAttach Bracket · wornDURING C-CHECK THE LT SPOILER ACTUATOR ATTACHMENT BRACKET WAS FOUND TO BE WORN AND WOULD NOT RETAIN THE HAT BUSHINGS. MX R & R THE SPOILER IAW AMM 27-62-05. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.SDR ABXA20120830251Splice Plate · corrodedRIGHT WING LOWER ATTACH FLANGE FOR LEADING EDGE JUST O/B OF PYLON UPPER SURFACE POTTING COMPOUND BOWED UP POSSIBLE CORROSION. COMPOUND WAS REMOVED AND NOTICED CORROSION FOUND AND REMOVED, ENGINEERING EVAL AND WORK ACCOMPLISHED ON REA B657-60316-MR. RIGHT WINSDR ASOA2012082902127Attach Angle · crackedRIGHT UPPER WING UNDER FUSELAGE TO WING ACCESS PANEL 162EL VERTICAL ATTACHMENT ANGLE IS CRACKED FS 469.53. REMOVED DAMAGED RT UPPER WING VERTICAL ATTACHMENT ANGLE & REPLACED W/NEW SERVICEABLE ANGLE PN IAW SRM 51-42-13 & 51-42-06.SDR ASOA2012082902126Attach Angle · crackedLEFT UPPER WING UNDER FUSELAGE TO WING ACCESS PANEL 161EL VERTICAL ATTACHMENT ANGLE IS CRACKED. LOCATED & DRILLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET IAW SRM 51-40-11, INSTALLED NEW SERVICEABLE VERTICAL ATTACHMENT BRACKET UNDER ACCESS PANEL 161EL ON LSDR 2012FA0000548Angle · crackedRIGHT WING ROOT FAIRING ATTACHMENT ANGLE CRACKED. R & R RIGHT WING ROOT FAIRING ATTACHMENT ANGLE.SDR FDEA201208042843Attach Fitting · corrodedLT WING AFT SPAR AT W STA 820 , RIB ATTACHMENT TO BONDING JUMPER CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 57-51-09 FIG 101 DETAIL VI PG 106.. REMOVED AND REPLACED RIB WITH NEW RIB, IAW SRM 51-40-02, SRM 51-40-05, AND DWG 113N1511 SH.1. SDR IPXA2B74897Support Fitting · crackedINSPECTION TYPE: 1C, LEFT WING SPOILER ACTUATOR NR 6 SUPPORT FITTING INBD LWR LUG AREA FOUND CRACKED. LT WING SPOILER NR 6 SPOILER SUPPORT FITTING INBD LOWER LUG AREA REPAIRED SRM 57- 51-13, REPAIR 1 R.22. REPAIR CLASSIFIED AS MAJOR.SDR IPXA2B74896Support Fitting · crackedINSPECTION TYPE: 1C, RT WING SPOILER ACTUATOR NR 7 SUPPORT FITTING OTBD LWR LUG AREA FOUND CRACKED. RT WING SPOILER ACTUATOR NR 7 SPT FITTING OTBD LWR LUG AREA IS REPAIRED IAW SRM 57-51-13, REPAIR 1 R.22. MAJOR REPAIR.SDR QXEA2012072500727Attach Bracket · crackedLEFT NR 3 HYD SYS ELEVATOR PCU AIR FRAME STRUCTURE ATTACH BRACKET IS BROKEN (CRACKED). ACFT CURRENTLY DOWN FOR REPAIRS.SDR CA120823006Attach Bracket · unsecure(CAN) AN ACFT EXPERIENCED AN AILERON SYS LIMITED TRAVEL EVENT. UPON INSPECTION, THE AILERON QUADRANT AFT SECONDARY STOP BRACKET ATTACHING HARDWARE WAS FOUND UNSECURED AND IN CONTACT WITH THE AILERON QUADRANT CABLE GUIDE BRACKET, IPC 27-12-01 ITEM 190. THE STOSDR QXEA2012062800562Tee Fitting · damagedRIGHT WING TEE FITTING BETWEEN PANELS 622BT AND 622CT HAS AREA OF FRETTING. REMOVED AREAS OF FRETTING IAW RD 8/4-57-441. BLENDED AREAS FOUND WITHIN LIMITS IAW RD 8/4-57-441. MINIMUM THICKNESS REMAINING .212" REF NTM 51-00-04-910-801. CONFIRMED BLENDED AREASDR FDEA201206082144Attach Bracket · corrodedLEFT WING OTBD FLAP, INBD FORWARD BRACKET SIDE ATTACH LOWER HOLE SPOT FACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 73. SHIM FABRICATED AND INSTALLED IAW CMM 57-44-08, REV 73. REPAIR EVALUATED AND FOUND SIDE LOAD MATING SURFACE REMAINING THICKNESS UPSDR CA120605012Link · cracked(CAN) WHILE CARRYING OUT A DETAILED INSPECTION OF THE RT WING ATTACHMENT LINK IAW TASK RJ2-53-160-501, THE AME FOUND WHAT LOOKED LIKE CRACKS ON THE UPPER SPHERICAL BEARING IN THE LINK. THIS WAS CONFIRMED BY HAVING A EDDY CURRENT INSPECTION PERFORMED IN-SITU. SDR GR4D20120530013Lug · corrodedRT AFT LUG ON SPONSON RIB HAS PITTING IN BORE.SDR IPXA2M73940Fitting · crackedINSPECTION TYPE: 4C, LT LOWER WINGLET FWD MOUNT FITTING CRACKED. R & R LT LOWER WINGLET FWD AND AFT MOUNT FITTINGS REF EO MD11-5720-27680-C, APPX D.SDR A6WA201240561Attach Bracket · crackedRT WING INBD L/E OTBD ATTACH BRACKET CRACKED. REMOVED UNSERVICEABLE BRACKET AND INSTALLED SERVICEABLE BRACKET IAW SRM 51-41-02/ 51-40-11.
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