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 ZB0R201100003Fitting · corrodedDURING ANNUAL INSP, FOUND LT WING AFT ATTACH POINT STEEL FITTING SEVERELY CORRODED. REPLACED PART WITH NEW.SDR UALA2011050502202Cotter Pin · missingRIGHT O/B FOREFLAP ATTACH POINT TO NR 8 FLAP TRACK, FOUND COTTER PIN MISSING FOR THE ATTACH NUT. NUT TIGHTENED AND PIN INSTALLED BY MECH.SDR UALA2011050502201Attach Fitting · gougedNR 7 FLAP TRANSMISSION LOWER ATTACH FITTING HAS 4 GOUGES.1- .5 INCHES LONG X .10" DEEP & MAX. .20" WIDE. 2 = .6" LONG X .150" DEEP & MAX DEPTH .20".3= .9" LONG X .150" DEEP & MAX WIDE= .20". 4 = 1.1" LONG X MAX. DEPTH .20" & MAX. WIDE= . 450". ACP HFEC OF ARESDR CA110421002Channel · misinstalled(CAN) UPON REMOVAL OF LT WING L/E THROTTLE CABLE PULLEY BRACKET AT BS 445.5 FOR ACCESS, FOUND SUPPORT CHANNEL WRONGLY INSTALLED IAW IPC 76-11-44-02. AFT ATTACHMENT SAFETY BOLT, BACB30DX6-18 AND WASHER, BACW10P95A, MISSING. THE ASSY COULD HAVE DETACHED AND DISDR LR7A2011041900187Fitting · crackedDURING SCHEDULED C-9 CHECK, FOUND RT UPPER CW FWD CORNER FITTING HOLE CRACK CWS 217. REPAIR ACCOMPLISHED BY REPLACING FITTING IAW SMP583 CHAP 51-60 & 51-70.SDR LR7A2011041900177Attach Angle · crackedDURING SCHEDULED C-9 CHECK, FOUND LT OTBD TO INBD WING T/E UPPER ATTACH ANGLE WITH MULTIPLE CRACKS. REPAIR ACCOMPLISHED BY REPLACING FORMER IAW SMP583 CHAP 51-60 & 51-70.SDR HNAA2011050600125Clamp · corroded2 ADEL CLAMPS ON LT L/E DEICE LINE BETWEEN FUSELAGE AND NACELLE ARE CORRODED. R & R 2 ADEL CLAMPS,SDR FDEA201103231143Attach Fitting · corrodedRIGHT WING OUTBOARD FLAP INBOARD FORWARD HINGE ACTUATOR INBOARD HOLE FOUND CORRODED REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08 REV 69. ORIGINAL DIAMETER = 1.228 INCH, FINAL DIAMETER = 1.250 INCH, MAX ALLOW DIAMETER = 1.220 INCH. ACCOMPLISHED SDR FDEA201103020812Bracket · crackedLT WING T/E CTR AND OTBD FLAP ATTACH AREA FOUND 2 ANGLE GOT BROKEN. REPLACED DAMAGED BRACKET BY NEW BRACKET WITH RIVET REF TO AB6 STM 51-40-21.SDR ASOA201100365Attach Bracket · crackedHINGE ARM ASSEMBLY AT WS.220.0 LT, CRACKED FWD O/B ATTACH BRACKET. REMOVED UNSERVICEABLE BRACKET AND REPLACED WITH NEW SERVICEABLE BRACKET IAW SRM 51-42-06.SDR AALA20110225AFW01Fitting · wornWEAR WAS FOUND ON THE RIGHT WING UPPER KICK LOAD FITTING, OUTBOARD OF RIGHT BUTTLINE 97.42. REMOVED DEEP GOUGES, ACCOMPLISHED HFEC INSPECTION TO ENSURE NO CRACKS EXIST. ALODINED AND PRIMED. REFERENCE EA B767-57-015098.SDR TRBACPCP2011002Support Bracket · corrodedRT WING SPOILER BRACKET SUPPORT SHOWS INTERGRANULAR CORROSION. R & R RT WING SPOILER BRACKET SUPPORT IAW SRM:57-70-00.SDR USAA2011020890603Attach Fitting · corrodedSAL - MAJOR REPAIR - S4 CHECK - CORROSION ON LEFT WING INTERCONNECT STRUT UPPER ATTACHMENT FITTING. REPLACED LEFT WING INTERCONNECT STRUT UPPER ATTACHMENT FITTING IAW A320 SRM 51-72-11.SDR USAA2011020890602Attach Fitting · corrodedSAL - MAJOR REPAIR - S4 CHECK - CORROSION ON RIGHT WING INTERCONNECT STRUT UPPER ATTACHMENT FITTING. REPLACED RIGHT WING INTERCONNECT STRUT UPPER ATTACHMENT FITTING IAW A320 SRM 51-72-11.SDR DALA1108059884Attach Bracket · crackedLT WING T/E REAR SPAR FWD OF INBD SPOILER ACTUATOR ATTACH BRACKET CRACKED. REMOVED ATTACH BRACKET IAW SRM 51-30-5. LOCATED, DRILLED AND INSTALLED NEW ATTACH BRACKET IAW SRM 51-10-4, 51-30-5. REQUIRED INSP COMPLETED.SDR FOTR2021700212Attach Bracket · crackedLT WING NR 2 SLAT ACTUATOR, INBD ATTACH BRACKET IS CRACKED. SLAT STA 291.0 REMOVED SLAT ACTUATOR SUPPORT STRUCTURE IAW SRM 51-30-2. FABRICATED NEW STIFFENER FROM BAC1503-100145 PO NR 20217147 DIM 9" X 4.5" AND SHIM FROM 7075T6 .032" PO NR 9006027 DIM 5" X SDR IXXA11SMN016SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING NR 1 STUB WING FITTING INTERNAL PART CRACKED AT STA XW 454.000. REMOVED CRACKED FITTING. CLEANED, TREATED, PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3SDR DHLA201100036Fitting · crackedRT WING TO FUS FAIRING. FITTING CRACKED 1" STA 920.000, L24R. PERFORMED MAJOR REPAIR IAW FORM 8110-3, DATED 02-28-11, EVA D853-00390 REV IR DATED 02-03-11, DWG ES-D85300390-001-D, REV B, DATED 2-15-11. REMOVED FASTENERS IAW SRM 51-1-20D. CUT OUT DAMAGED ARSDR DALA1109790178Fitting · crackedRT WING FRONT SPAR UPPER LINK PITCH LOAD FITTING FASTENER HOLE CRACK. REPAIR ACCOMPLISHED IAW ER/A 487054-14AD.SDR USAA2011021490737Attach Bracket · excess playSAL - MAJOR REPAIR - S4 CHECK - LEFT WING INTERCONNECT STRUT ATTACH BRACKET HAS EXCESSIVE PLAY. REPLACED LEFT WING INTERCONNECT STRUT ATTACH BRACKET IAW A319 SRM 51-72-11.SDR KPVA201101Bolt · brokenWHILE INSPECTING FOR POSSIBLE HYDRAULIC LEAK AT THE RT WING ROOT, MAINTENANCE DISCOVERED THAT ONE OF THE WING BOLTS FOR THE REAR SPAR STEEL SUPPORT STRUTS HAD FAILED. THE BOLT HEAD HAD SEPARATED FROM THE SHANK OF THE BOLT AND WAS DANGLING FROM THE SAFETY WIRE.SDR EE4Y20110021Structure · corrodedRT WING REAR SPAR AREA, MACHINING JACK ANCHORAGE WITH CORROSION AROUND THE BORE UPPER AND LOWER SURFACE AND AT THE BORE INNER SURFACE. REQUIRES MAJOR REPAIR.SDR DALA1103019855Attach Angle · crackedMAIN CABIN STA 756 LBL 44 WEB TO CTR WING TANK ATTACH ANGLE CRACKED. CUTOUT CRACKED AREA 1" X 12" IAW SRM 53-01, FIG 2, FABRICATED 1EA FILLER, 2EA REPAIR ANGLES IAW SRM 53-01, FIG 2. REMOVED & INSTALLED NEW T ANGLE AND 2EA SHIMS IAW DWG NR 9919689. INSTALLSDR SWAA110208Fitting · crackedDURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 54.6. REMOVED AND REPLACED SHEAR FITTING PER SRM.SDR WRLA20110103460Attach Fitting · crackedRIGHT WINGLET AFT FITTING CRACKED,SDR WRLA20101230459Attach Fitting · crackedLEFT WINGLET AFT FITTING SPACER CRACKED. REPLACED THE DAMAGED PART WITH NEW PART IAW MD-11-1F SRM 51-33-01 REV 45. COND CHECK SATISFACTORY.SDR V0XR201012300012Attach Angle · delaminated(V0XR) LT FWD BOTTOM WING-FAIRING ATTACHMENT ANGLE IS CRACKED. R & R ANGLE. W/C 5069SDR V0XR201012280013Attach Fitting · damaged(V0XR) RT TOP WING-FAIRING ATTACHMENT STRIP CRACKED. R & R STRIP. W/C 6020SDR V0XR201012280012Attach Fitting · damaged(V0XR) RT TOP WING-FAIRING ATTACHMENT STRIP CRACKED. R & R STRIP. W/C 6018SDR V0XR201012280011Attach Fitting · damaged(V0XR) RT INBD L/E WING-FAIRING ATTACHMENT STRIP CRACKED. R & R STRIP. W/C 6017SDR V0XR201012270021Attach Angle · cracked(V0XR) LT FWD BOTTOM WING-FAIRING ATTACHMENT ANGLE IS CRACKED. R & R ANGLE. W/C 5068SDR DALA1107360175Fitting · damagedLT WING INBD MIDSPAR UNDERWING FITTING INBD HOLE FOUND DIAMENTER SIZE = 0.902" WHICH IS GREATER THAN 0.8750"-0.8770". REPAIR CARRIED OUT IAW PRI 487833-14AD, REV.2, DATED 01/04/11.SDR SWIA201025338Mount · damagedFLT 3071, ON APPROACH, WITH AUTOPILOT OFF, CONTROL COLUMN FROZE AND TOOK ABOUT 25 POUNDS OF FORCE TO BREAK FREE. REPLACED ELEVATOR SERVO MOUNT.SDR DALA1036239864Fitting · brokenDURING M-CHECK, FOUND RT WING OTBD FLIGHT SPOILER TORSION BAR INBD FITTING IS BROKEN AT WING AFT SPAR. R & R OTBD SPOILER INBD FITTING IAW SRM 51-30-2 51-30-5.SDR CALA2010102100491Structure · corrodedRT WING RT MLG O/B STAB LWR I/B HOLE AT SECOND OVERSIZE OF.3432 -.3442 & STILL HAS INDICATION. REPAIRED PER ECRA 5740-02276. INITIATED DIP #57-DIP CONTROL #07 526 READS: ACCOMPLISH PERMANENT REPAIR BEFORE 18-OCT-2011 PER ECRA 5740-02276 PART 3. PLANNING TOSDR FDEA201010114001Attach Bracket · looseRT WING T/E FIXED PANEL, PANEL SUPPORT BEAM NEAR WS 231.5 ATTACH BRACKET LOOSE. RT WING T/E FIXED PANEL SUPPORT BEAM AT WS 231.5 R & R IAW SRM 51-40-02 REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010114000Attach Bracket · looseRT WING T/E FIXED PANEL, PANEL SUPPORT BEAM NEAR WS 220 ATTACHING BRACKET LOOSE. RT WING T/E FIXED PANEL SUPPORT BRACKET AT WS 220 CRACKED THROUGH. BRACKET R & R IAW SRM 51-4002 REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201009303802Fitting · corrodedLT WING RIB 5 MLG FWD LUG CORROSION EXCEED LIMIT COMPLIED WITH EA 6-5710-141613.SDR FDEA201009203565Attach Fitting · crackedCRACK FOUND LT WING INTERNAL LOWER STRINGER 36 BUTTERFLY CLIP AT XORS 402.00. REMOVED AND REPLACED BUTTERFLY CLIP IAW DWG ARB2176 AND EA 8-5710-123558.SDR IXXA10SMN088SFitting · crackedDURING ROUTINE C-CHECK INSP, FOUND LT WING T/E UPPER FITTING CRACKED AT STATION XRS 409.000. R & R CRACKED FITTING IAW SRM 51-1-21.SDR UALA2010091603448Attach Angle · crackedFOUND PNEU DUCT LOWER SUPPORT ATTACH ANGLE CRACKED-BROKEN AT APPX WS670.25, INSIDE TOP WING AREA AS SEEN THROUGH PANEL 511CT. (THIS IS CAUSE FOR PNEU DUCT MISALIGN, PREVENTING PROPER SEAL CLAMP INSTALLATION JUST OTBD OF NR2 PYLON THROUGH L/E. KRUEGER FLAP IN SDR FDEA201009103343Attach Angle · crackedLT WING FALSE SPAR ATTACH ANGLE IS CRACKED WBL 118. REMOVED DOUBLER AND CUT OUT LOWER CHORD IAW DRAWING SR27-57-038 REV C. FABRICATED REPAIR ANGLES, NEW WEB, NEW I/B CHORD SECTION, NEW STRAP, RADIUS FILLERS, AND NEW WEB IAW DRAWING SR 27-57-038 REV C. INSSDR FDEA201009063302Attach Fitting · crackedRT WING T/E FIXED PANEL, PANEL SUPPORT BEAM ATTACHING BRACKET TO PANEL FOUND CRACKED AT WS 220 NEAR OTBD SIDE OF AFT LANDING TRUNNION FITTING. EVALUATE AND RECTIFY. RT WING T/E FIXED PANEL, PANEL SUPPORT BEAM ATTACHING CRACKED BRACKET REPLACED BY FABRICATISDR FDEA201008313210Bracket · crackedRT WING REAR SPAR LOWER T/E FIXED PANEL TO PANEL STIFFENER, ATTACHING BRACKET AT WS170, NEAR FUEL PUMP CRACKED. CRACKED BRACKET AT WS 170 R & R IAW SRM 51-40-02 REV. 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR CA100818001Attach Fitting · mismanufacturedDURING 10 YR/11000 HR INSP OF THE WING TO FUSELAGE ATTACHMENT FITTINGS, BOLTS AND BUSHINGS, THE AFT UPPER BOLT BORE ON THE WING FITTING (PART OF REAR SPAR) WAS FOUND TO HAVE TOOLING MARKS IN THE BORE. THIS WAS FOUND ON BOTH LT AND RT WINGS. THIS IS THE SECONSDR FDEA201008173030Fitting · damagedRT WING INBD SIDE LOAD FITTING OTBD LEG 2EA CODE 'C' FASTERNER HOLES ELONGATED WHILE REMOVING TO COMPLY WITH SIP MOD. REPAIR ACCOMPLISHED ON STAM EA 757-5724-16-F2734. REV- ISSUED 06/29/10. EA F5720-139218 WINGS- ATTACH FITTINGS-(AD2004-12-07) NR2 ENGINE PYLOSDR ABXR2010081100032Bracket · misalignedDURING A HEAVY MX, THE NR 7 SLAT ACTUATOR NOT ALIGNING WITH NR 7 SLAT MOUNT POINT DUE TO SLAT ACTUATOR MOUNTING BRACKET HOLE LOCATIONS WITH INCORRECT DIMENSIONS. R & R BRACKET. ITEM RETURNED TO SERVICE.SDR DALA1018950186Attach Fitting · crackedRT WING AFT PITCH LOAD FITTING ATTACHED AREA (2EA) CRACKS FOUND AT THE INBD ROW MOST FWD BOLT HOLE CRACKED AT LOWER SKIN. FREEZE PLUG REPAIRED IAW ERA 482265-14AD REV 0.SDR SWAA104701Fitting · crackedDURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR TIE FITTING CRACKED AT BS 540, RBL 14. REMOVED AND REPLACED FITTING PER SRM.SDR SWAA104700Fitting · crackedDURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR TIE FITTING CRACKED AT BS 540, RBL 7. REMOVED AND REPLACED FITTING PER SRM.
Back to JASC 5740