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 030520Attach Fitting · elongatedREAR SPAR ATTACH FITTING BOLT HOLE IS ENLARGED ON BOTH WINGS. FITTINGS ARE BEING REPLACED.SDR 030521Fitting · crackedUPPER WING ATTACH FITTINGS ON BOTH WINGS ARE CRACKED. THE CRACKS APPEAR ON THE FACE OF THE LEFT FITTING AND THE INSIDE CORNER OF THE RIGHT FITTING, THE FACES OF WHICH GO AGAINST THE SPAR CARRY THRU. FRETTING IS PRESENT BETWEEN THE FITTING AND SPAR ON THE RIGHSDR AWXA200300706Fitting · arcedDURING C-04 CHECK A HOLE WAS FOUND BURNT INTO THE INBOARD EDGE OF NR 2 PYLON TO WING ATTACH FITTING, ARCING CAUSED FROM NR 2 IDG FEEDER CABLE. MAINTENANCE REMOVED SPIGOT FITTING AND FORWARD INBOARD PYLON ATTACH FITTING; FABRICATED A NEW REPLACEMENT INBOARD PYSDR 2003FA0000439Fitting · deformedDURING INSPECTION OF THE WING FITTINGS AND BOLTS THE RIGHT REAR WING ATTACH BOLT WAS FOUND TO BE BENT AND THE FITTING WAS DEFORMED. IN THE MFG STRUCTURAL INSPECTION AND REPAIR MANUAL COVERS THE INSTPECTION OF THE BOLTS AND FITTING AREA. THE BOLT AND A CASTINGSDR DHL2003801007Fitting · crackedRT STUB WING UPPER SURFACE ZEE PAN AT STA XS 250.089 WITH 2.000 INCH CRACK. REMOVED AND REPLACED RT STUB WING UPPER SURFACE ZEE PAN FITTING AT XS 250.089 IAW SRM 51-1-21 PG 1 AND SRM 51-1-21D PG 9.SDR UPS03840678Fitting · crackedINSPECTION TYPE: C1, LT WING AT STA. XRS 74 OB SIDE STRINGER 51 END FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3704841, AND SRM. 51-1-20DSDR DHL2003801030Fitting · crackedLT STUB WING UPPER SURFACE ZEE PAN WITH 2.000 INCH CRACK STA XS 250.089. REMOVED DAMAGED ZEE PAN FITTING IAW SRM 51-3-0 PG 1, SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW ZEE PAN FITTING IAW SRM 51-3-SDR UPS03840637Fitting · crackedINSPECTION TYPE: C1, LT WING FITTING AT REAR SPAR AT XRS 446 AT REAR SPAR REMOVED,FABRICATED AND REPLACED FITTING I.A.W. DWG. 4640309 AND SRM. 51-1-20DSDR DHL2003801028Fitting · crackedRT WING CTR L\E ZEE PAN CRACKED 3.500, STA XS 520.168. REMOVED AND REPLACED DAMAGED ZEE PAN FITTING AT STA XS 520.168 (RT WING CTR L\E IAW 51-1-21 PG 1 AND SRM 51-1-20D PG 9 AND 21.SDR 03FDEA00610Fitting · crackedRIGHT WING FOUND L/E NR 16 TRACK INBOARD SUPPORTING FITTING CRACKED. RT WING LEADING EDGE NR 16 TRACK INBOARD SUPPORTING FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II AND DWG ARB2850.SDR MWEA030166Bushing · damagedFOUR HI-LOKS REQUIRED REMOVAL IN THE LEFT WING FUEL TANK APPROXIMATELY XCW 67 AND XCW 69 DUE TO FUEL LEAKS. FABRICATED AND INSTALLED BUSHINGS.SDR SWAA030590Rib · crackedDURING SCHEDULED D CHECK, FOUND LH WING UPPER RIB CHORD CRACKED AT STA 114, STR 2. REPAIRED UPPER RIB CHORD PER BFG ER.SDR AUS20030369Fitting · damaged(AUS) WING FORWARD ADAPTER PLATE DAMAGED. FASTENER HOLES ELONGATED. FRETTING AND CORROSION ALSO EVIDENT.SDR ASAA0380246Mount · gougedOKC - FOUND DURING 30K CHECK, RIGHT WING NR 1 INBOARD SLAT CLOSE OUT MOUNT BROKEN. REPLACED BRACKET PER SRM. (M)SDR 03FDEA00359Hinge Bracket · corrodedRT WING, O/B FLAP, I/B HINGE BRACKET ACTUATOR UPPER ATTACHMENT HOLES 2 EACH CORRODED. WINGS - RIGHT O/B FLAP, I/B HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORROSION REWORKED AND BUSHING REPAIRED AS PER FEDEX EA 1-5740- 68589.SDR 03FDEA00358Bracket · corrodedLT WING OUTBOARD FLAP INBOARD HINGE BRACKET ACTUATOR UPPER ATTACHMENT HOLE AND LUG CORRODED. WINGS- LEFT O/B FLAP- I/B HINGE BRACKET ASSY FOR ACTUATOR INSTALLATION CORRODED HOLE REWORKED AND BUSHING REPAIRED AS PER FEDEX EA 1-5740-68588.SDR 1387SMount · crackedDICOVERED DURING INSPECTION FOUND A CRACK IN THE RT TIP TANK MOUNTING FLANGE. REPAIRED PER MFG. DRAWING.SDR UPS03840191Fitting · crackedINSPECTION TYPE: C1, RT WING STRINGER 51 END FITTING IS CRACKED OUTBOARD SIDE AT XRS 74. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.SDR DHL2003804889Fitting · corrodedRT WING CTR L/E UPPER PART CORRODED, STA XW 257.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030106, ED-3212. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. REMOVED CORROSION ON RT WING CTR L/E UPPER PART IAW SRM 51-1-8B PG 17-18, FOUND OUT OF LIMITS IAW SRSDR UPS03840190Fitting · crackedINSPECTION TYPE: C1, RT WING STRINGER 51 END FITTING IS CRACKED AT XRS 74 INBOARD SIDE. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.SDR DHL2003804887Fitting · crackedRT WING L/E ZEE PAN CRACKED 2.000 INCHES AT STA XW 223.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED FITTING ZEE PAN CRACKED IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW FITTING ZEE PAN ON RSDR 2003F00113Attach Fitting · chafedDURING A ROUTINE SERVICE INTERNAL CUSTOMER REQUESTED THE 1000 HOUR INSPECTION DETAILED IN AIRWORTHY LIMITATIONS OF MM. ON ALL FOUR STRUT ATTACH FITTINGS. BOTH FITTINGS WERE REJECTED ON LEFT WING DUE TO CHAFING ON EDGES WHERE FITTINGS PASS THROUGH LEADING EDGSDR SWAA030214Beam · crackedDURING SCHEDULED D CHECK, FOUND LT MLG BEAM REAR SPAR CHORD CRACKED. REPAIRED BEAM PER SWA ACO.SDR 030130Fitting · crackedUPPER WING ATTACH FITTING IS CRACKED. THE CRACKS APPEAR ON THE FACE OF THE FITTINGS THAT GO AGAINST THE SPAR CARRY THRU. IN SOME CASES THE CRACKS CAN BE DETECTED INSIDE THE BARREL NUT BORE. WE HAVE BEGUN CHECKING SPARE WINGS IN STORAGE AS WELL AS FLIGHT LINSDR LR7A03003Fitting · crackedDURING SCHEDULED B1 INSPECTION PER JOB CARD HB0521 FOUND RH FLAP TRACK RIB STIFFENER FITTING CRACKED 2.0 IN. IN LOWER FLANGE AT RH OWS 28, FS 598, WL 257.REPLACED FITTING IAW SRM SMP 583 51-70 AND DWG 3325706. NR 0115.SDR CA030107003Fitting · cracked(CAN) DURING A ROUTINE INSPECTION, AME NOTICED AN OILY STREAK ON THE FITTING. AFTER CLEANING, IT APPEARED TO BE A DEEP SCRATCH. THE AREA WAS CLEANED WITH SOLVENT AND REEXAMINED, WHICH LOOKED LIKE A CRACK. AN NDT. (LIQUID PENETRANT) WAS PERFORMED TO CONFIRM THESDR ARWA20030101Spar CapLOG PAGE # 503179. DISCREPANCY: DURING 1A CHECK THE FOLLOWING WAS FOUND; ITEM # 128M: L/H WING AUXILIARY SPAR INBD. UPPER LOG WITH CRACK. GENERATED BY J/C # 51-020-04-06-1. CORRECTIVE ACTION: ACCOMPLISHED TEMPORARY REPAIR IN ACCORDANCE WITH BOEING MESSAGE ISDR CA021220011Fitting · nicked(CAN) NICKS FOUND DURING INSPECTION. LOCATED ON UPPER LUGS OF WING SPAR CARRY THROUGH FITTINGS ON LT & RT SIDES OF MAIN & REAR STUB WING SPAR ASSY'S.SDR CA021220010Fitting · nicked(CAN) NICKS ON UPPER LUGS OF WING CARRY THROUGH FITTINGS ON FWD & REAR SPARS.SDR 56724Fitting · mismanufacturedWHILE PERFORMING AND NDT INSPECTION IT WAS BROUGHT TO OUR ATTENTION THAT THERE APPEARED TO BE MORE THAN NORMAL SPACING BETWEEN THE WING CLOTHESPIN FITTING AND THE DOUBLER PLATE THAT WERE MODIFIED IAW ASC. UPON INSPECTION WE DETERMINED THAT THERE WAS A GAP BESDR 2003FA0000024Attach Fitting · misinstalledDURING ROUTINE 24-MONTH ULTRASONIC EXAMINATION NOTED ASC-426 (3 PIECE WING ATTACH FITTING) MODIFICATION WAS IMPROPERLY INSTALLED. NOTED THAT DOUBLER WAS TRIMMED TO FIT WING PLANK CUT OUT INSTEAD OF WING PIN DIAMETER. RECOMMEND ALL OPERATORS VISUALLY INSPECT SDR Q2A2003F00000Fitting · crackedWHILE PERFORMING NDT INSPECTION OF WING ATTACH FITTINGS, LEFT LOWER FORWARD FITTING FOUND CRACK IN RADIUS OF BOLT HOLE. SPAR WAS THEN REPLACED.SDR 0203729984Slat · crackedDuring Shop Visit in ATL, a crack and elongated hole were found on the lower skin of the subject slat at the aft otbd corner. Repaired per EA 99-190789.SDR SWAA022546Fitting · corrodedDURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG WALKING BEAM FITTINGS CORRODED. REMOVED AND REPLACED BOTH LT AND RT MLG WALKING BEAM FITTINGS PER MM.SDR CA021015010Bolt · cracked(CAN) DURING INSPECTION OF WING AND BOLTS, IN CONJUNCTION WITH AD. DYE PENETRANT INSPECTION FOUND CRACK IN LOWER FORWARD LT WINGBOLT. CRACK FOUND ON BOLT SHAFT/FLANGE AREA. NO OTHER CRACKS FOUND DURING INSPECTION. BOLT REPLACED. ORIGINAL FAILED BOLT INSSDR SWAA022362Fitting · corrodedDURING SCHEDULED SERVICE CHECK, FOUND BOTH LT AND RT MLG FWD STABILIZER BAR SUPPORT FITTINGS CORRODED. REPAIRED FITTINGS PER SWA EA'S.SDR TIM2002F00016Attach Fitting · crackedCRACK FOUND IN RIGHT WING ATTACH FITTING. (BATH TUB FITTING) LOCATION CENTER SECTION UPPER FORWARD ATTACH FITTING. RECURRING INSPECTION INTERVAL (STANDARD SPAR WITH STAP) 500 HOURS OR 1 YEARS WHICHEVER OCCURS FIRST. (CONTROL NUMBER 005)SDR TIM2002F00015Attach Fitting · crackedCRACK FOUND IN RT WING ATTACH FITTING. (BATH TUB FITTINGS) LOCATION CENTER SECTION UPPER FORWARD ATTACH FITTING. RECURRING INSPECTION INTERVAL (SUPER SPAR) 1000 HOURS OR 3 YEARS WHICHEVER OCCURS FIRST. (CONTROL NUMBER 004)SDR TIM2002F00014Attach Fitting · crackedCRACK FOUND IN RIGHT WING, CENTER SECTION UPPER FORWARD ATTACH FITTING.SDR 2002FA0001146Fitting · damagedREMOVED WING LOWER ATTACH FITTING COVERS IN PREPARATION FOR EDDY-CURRENT INSPECTION IAW T34 REPORT. BEFORE BEGINNING EDDY-CURRENT INSPECTION NOTED DEEP TOOL MARKS/GOUGES IN RIGHT WING LOWER AFT BATHTUB FITTING INTERIOR. ALSO NOTED SIMILAR MARKS IN LEFT WING SDR UPS02839248Fitting · crackedCRACK IN STEEL STRAP UNDER R/T ADF PNL. MILLED STEEL STRAP UNDER RT ADF (FWD) PANEL CRACKED AT STA 82.7 WHERE WING MEETS CENTER TANK BUT T L7ORT VERIFIED WITH EDDY CURRENT (SKI FITTING). R&R'D FITTING IAW DWG J060095 SRM 51-1-20D, 51-1-21,51-3-0 & 53-1-0. CSDR SWAA021982Fitting · corrodedDURING SCHEDULED SERVICE CHECK, FOUND RT MLG BEAM STABILIZER BAR FWD ATTACH FITTING ON REAR SPAR AT WBL 113.895 CORRODED IN BUSHING BORE. REPAIRED LUG BORE PER SWA EA.SDR MWEA020495Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 18&19 ALSO EXTENDING UNDER STRINGER 18 FORWARD AND AFT. -- FABRICATED AND INSTALLED SHIM.SDR MWEA020483Stringer · damagedREPAIR CLIPS REQUIRED BETWEEN STRINGERS 15&14 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.SDR MWEA020484Stringer · damagedREPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGERS 14&13 ON THE INBOARD AND OUTBOARD SIDE OF XCW 58 WING.SDR MWEA020485Stringer · damagedREPAIR CLIP REQUIRED INSTALL BETWEEN STRINGERS 13&12 ON THE INBOARD AND OUTBOARD SIDES OF XCW 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.SDR MWEA02505Stringer · damagedREQUESTING BOEING AGREEMENT OF FASTENER PLACEMENT IN UPPER PORTION OF REPAIR CLIPS BETWEEN STRINGER 14,15&16 THERE ARE TWO CLIPS AND TWO FASTENERS PER CLIP. -- BOEING APPROVES OF THE PLACEMENT OF THE FASTENERS.SDR MWEA020491Stringer · corrodedLEFT WING TEE OUTBOARD LOWER LEG HAS PITTING/EXFOLIATION CORROSION ON UPPER SURFACE BETWEEN STRINGER 14&15 ALSO EXTENDING UNDER STRINGER 14&15 AND ONE SPOT ON VERTICAL LEG. -- FABRICATED AND INSTALLED SHIMSDR MWEA020509Stringer · damagedREPAIR CLIPS REQUIRED INSTALL BETWEEN STRINGER 17&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.SDR MWEA020508Stringer · damagedREPAIRED CLIPS REQUIRED INSTALL BETWEEN STRINGER 15&16 ON THE INBOARD AND OUTBOARD SIDES OF XWC 58 WING TEE. -- DRILLED UP AND INSTALLED CLIPS.
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