JASC 5710
Service difficulty reports · 4,462
Reports filed under 5710 · Wing Main, Frame Structure, 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 = '5710' 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 = '5710' 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 DALA1207530923Doubler · crackedRT WING LEADING EDGE COMPT XFS 397 DOUBLER ON FORMER IS CRACKED (NRC 191871).SDR DALA1207480923Former · crackedRT WING L/E COMPT XOS 461 FORMER IS CRACKED AT FASTENER HOLE (NRC 191413).SDR FDEA201202030453Skin · chafedLEFT WING FIXED L/E ANTI-ICE DUCT CUTOUT FOUND CHAFED. CUTOUT AREA IAW SRM 51-31-01, REV 48. DOUBLER FABRICATED IAW SRM 57-40-01. REPAIR 10, FIG 201, REV 48. FABRICATED DOUBLER INSTALLED IAW SRM 57-40-01. REPAIR 10, FIG 201, REV 48. REPAIR CLASSIFIED MASDR FDEA201202030450Structure · corrodedRIGHT WINGLET T/E INBD STATIC DISCHARGER HAS CORROSION EXTENDING FROM UNDERNEATH THE BASE ESTIMATED DEFECT MEASURES 4 SQ IN, REMOVED LEVEL 1 CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-30-11. FABRICATED DOUBLER AND FILLER AND INSTALLED REPAIR IAW SRM 5SDR ANZY20120201Plate · crackedPRIOR TO RAISING INBD SLATS, A CAVITY CHECK FOR FOD AND CLEARANCE OF AREAS WAS CARRIED OUT. DURING THIS CHECK IT WAS FOUND THAT THE RT KRUGER FLAP SEAL ACTUATOR MOUNTING SIDE PLATE STRUCTURE HAD SNAPPED IN HALF. S/O RAISED TO REPLACE SIDE PLATE STRUCTURE ANDSDR GR4D20120125012Winglet · corrodedLT WINGLET CORRODED.SDR FDEA201201190268Retainer · crackedRT WING L/E RIB 8 HAS A .75 INCH CRACK EXTENDING FROM RECEPTICAL. REPAIRED LANDING ON RT WING L/E RIB 8 RECEPTICAL IAW SRM 57-41-12, SECTION 3 H,J,K, AND N.SDR FDEA201201190252Support · corrodedLEFT WING T/E ACCESS PANEL 541JB FWD SUPPORT AT XORS 380 TO XORS 433, FOUND CORRODED. R & R IAW SRM 51-31-01, REV 48 AND DWG ARC0293, REV T. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.SDR FDEA201201110084Structure · crackedCRACK INDICATION FOUND ON 3RD LAYER FROM BELOW OF HOLE 'F' DURING HFEC OPEN HOLE INSPECTION ON RT SIDE CENTER WING BOX REAR SPAR BOTTOM PANEL AT FRAME 47. REPAIR CARRIED OUT AT RT SIDE CENTER WING BOX FRAME 47 HOLE 'F' IAW EA 6-5710-155862 PART 1. REPAIR CLASDR A6WA201240174Bearing · crackedLT WING HINGE PANEL 594JB OTBD ROLLER BEARING WORN AND HINGE PIN TAB CRACKED AND BENT. R & R OTBD LT WING HINGE PANEL ROLLER BEARING IAW RIL R26 NR2114. R & R HINGE, PN 601R10394 IAW SRM 51-42-06.SDR TRBA201136301Structure · corrodedLT WING FUEL PUMP CUT OUT AREA CORRODED. COMPLIED WITH EO E2-5700-476.SDR A6WA201240091Structure · chafedRT APRON CHAFED FROM WING PANELS AT AFT WING STUB FAIRING, COMPLIED WITH REO 601R-53-41-341.SDR A6WA201240122Structure · chafedRIGHT AFT WING APRON CHAFED. REMOVED CHAFE IAW REO 601R-53-41-341.SDR A6WA201240131Panel · chafedPANEL 699CB CHAFED. REMOVED CHAFE IAW REO 601R-57-60-020.SDR QXEA2011121901410Shroud · looseRT WING UPPER T/E SHROUD HAS NUMEROUS LOOSE RIVET AND SCREWS BETWEEN STA YW335.019 AND YW371.019. R & R LOOSE RIVETS ON RT WING T/E SHROUD IAW SRM 51-42-45-02-01. R & R LOOSE SCREWS ON RT WING UPPER T/E SHROUD IAW SRM 51-45-00-00-01.SDR A6WA201240116Beam · chafedLEFT FLAP INBD VANE ACTUATOR INBD BEAM CHAFED BLENDED IAW REO 601R-57-52-1824.SDR DALA1255770183Tee Fitting · damagedRT WING UPPER PITCH LOAD FITTING INBD TEE FITTING HAS SHORT EDGE MARGIN ON FASTENERS AND HAS BEEN REPLACED IAW ERA 507545-14AD, REV ORG NR 52474.SDR CA111110007Adapter · damaged(CAN) FOUND A DRILL STRIKE HAS OCCURRED ON THE BOTTOM OF FITTING, PN C6WM1162-3/-4. DURING THE MFG OF NEW WINGS. MFG IS INVESTIGATING TO DETERMINE WHAT FURTHER ACTION IS REQUIRED.SDR EE4Y20110592Anchor Fitting · corrodedLOWER FUSELAGE, OUTER WING REAR SPAR AFT FACE, RT RETRACTION ANCHOR JACK FITTING WITH CORROSION. THE ANCHORAGE JACK FITTING REQUIRED A MAJOR REPAIR IAW MFG.SDR 2011FA0000706Structure · misinstalledON 1/2011 DURING A WALK AROUND PRIOR TO AN ANNUAL INSPECTION THE RT WING LE WAS FOUND LOOSE. INSPECTION OF THIS AREA DISCLOSED THAT THE LE WAS MISINSTALLED. THE DISCREPANCY WAS CORRECTED.SDR IPXA11M70119Doubler · crackedINSPECTION TYPE:2C, LT WING FIXED L/E SPLICE STRAP (DOUBLER) CRACKED AT XOS.786. REMOVED FABRICATED & INSTALLED REPLACEMENT DOUBLER IN LT WING L/E INTERIOR IAW DWG ARB3954, SRM 51-33-01, 51-35-01.SDR ASOA201101825Structure · gougedGOUGES FOUND ON ALL FLAP HINGE BOXES IN VARIOUS LOCATIONS. REPAIRED GOUGES IAW SRM 51-12-00. 09-28-2011.SDR ASOA201101824Structure · gougedGOUGES FOUND ON FWD AND AFT WING FITTINGS FOR FLAP HINGE BOXES AND FLAP ACTUATORS (REF ISE-STR-11-080 REV NC, DETAILED DAMAGE 6.4.) REPAIRED GOUGES FOUND ON FWD AND AFT WING FITTINGS FOR FLAP HINGE BOXES AND FLAP ACTUATORS IAW SRM 51-12-00. REPAIRED GOUGES FSDR FDEA201109193959Shim · looseLT WING BETWEEN OTBD NAC FITTING AND LOWER WING SKIN FOUND WITH SHIMS MIGRATION AT WS 303.5. SHIM MIGRATION DEFECT ON LT WING AT STA 303.5 REPAIRED IAW EA F-5740-152627 (AD 2004-12-07)- LT WING OTBD NAC ATTACH FITTING -SHIM MIGRATION. REPAIR IS CLASSIFIED ASDR FDEA201109173916Arm · corrodedDURING LT WING NR 3 SLAT ASSY REMOVAL, OTBD ATTACHMENT ARM HOLE AT STA XORS 455 FOUND CORRODED. REPAIRED IAW EA 1-5740-149880. CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.SDR UIEA2011091900512Structure · damagedDURING MX, RT OTBD WING - WBL 1131.2 SUSTAINED GROUND DAMAGE. LOCATED 4.0 IN. OTBD FROM FUEL JETTISON NOZZLE AT THE WING T/E WEDGE MEASURING 12.0 X 9.0 IN. (REF FIG 1). (DISPOSITION WAS MADE TO PERFORM AN INTERIM REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONSDR CA111005003Bulkhead · torn(CAN) A DIFFERENTIAL FLAP CONDITION WAS NOTED ON DURING TAKEOFF, THE ACFT LANDED AT THE MX FACILITY AND FURTHER INVESTIGATION REVEALED THE FOLLOWING: LOWER BULKHEAD ASSY 0512133 WAS TORN WERE RT FLAP BRACKET 0512128 INBD UPPER ATTACH POINT IS SECURED TO THE 0SDR CA110826006Bolt · corroded(CAN) HEAD OF BOLT CORRODED.SDR CA110822011Winglet · damaged(CAN) CREW REPORTED THEY HAVE BEEN STRUCK BY A LIGHTNING STRIKE ON THE LT WING DURING DESCENT. INITIAL INSPECTION REVEALED SOME DAMAGE TO THE LOWER LT WINGLET STATIC DISCHARGER. THE ACFT WAS REMOVED FROM SERVICE AND INSPECTED IAW THE ACT MM CHAP 05-51-05. ISDR QXEA2011081600668Panel · corrodedWING CUTOUT FOR PANEL 624BT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.SDR QXEA2011081600667Panel · corrodedWING CUTOUT FOR PANEL 624CT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.SDR QXEA2011081600666Panel · corrodedWING CUTOUT FOR PANEL 624DT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.SDR QXEA2011081600665Panel · corrodedWING CUTOUT FOR PANEL 624ET MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.SDR QXEA2011081600664Panel · corrodedWING CUTOUT FOR PANEL 624FT MATING SURFACE HAS CORROSION. REMOVED CORROSION IAW RD 8/4-57-445. FOUND TO BE WITHIN LIMITS. COMPLETED REPAIRS IAW RD 8/4-57-445.SDR GR4D20110802002Structure · corrodedRIGHT WINGLET CORRODED.SDR GR4D20110802001Structure · corrodedLEFT WINGLET CORRODED.SDR ASMF201107013Winglet · damagedDURING TRANSIT CHECK MX DETECTED A LIGHTNING STRIKE ON THE LT WINGLET, ACFT WAS SENT TO THE HANGAR FOR ATTENTION; A LIGHTNING STRIKE CONDITIONAL INSPECTION WAS PERFORMED IAW MM 05-51-19 FOUND DAMAGES OUT OF LIMITS OF 3.5" LONG AND 0.5" WIDE, SO LEFT WINGLET WASDR DU4R2011001ABeam · corrodedR & R CORRODED LEFT 517 BEAM, INTER CAP, REINFORCING STEEL DOUBLER AND MAIN LANDING TRACK.SDR 2011FA0000477Strut · crackedNEW REPLACEMENT REAR WING STRUT RECEIVED FROM MFG. WHEN RECEIVED THERE WERE 2 LONGITUDINAL CRACKS IN THE STRUT IN THE ELECTRICALLY WELDED SEAM OF THE SEAMLESS WELDED STRUT TUBING. LOCATION OF THE CRACKS ARE 1 FT FROM THE UPPER WING STRUT FITTING IN A VIRGIN SDR ASOA201101260Structure · crackedAFTER INITIAL INSP OF WING, IAW AD2002-03-14REP, AND SB A601R-57-031, FOUND SUSPECTED CRACK ON LT WING AT WS148.019. COMPLIED WITH HFEC INSP IAW NDTM 51-20-06 FOUND A .300" CRACK AT LT WING BOTTOM AT WS 149.58 JUST FWD OF REAR SPAR. PERFORMED LPI TO DETERMISDR UVVR2010060900015Structure · corrodedEXTERNAL WING SUPPORT STRUCTURE CASTING CORRODED ON NUMEROUS AREAS,LOCATED AT LT SPAR ADJACENT TO THE LT MLG ACTUATOR CYLINDER, FOUND DURING C INSPECTION.SDR HNAA2011061300170Doubler · corrodedMINOR SURFACE CORROSION AT THE UPPER SURFACE AT FUEL BOOST PUMP DOUBLER IN THE RT WING AT APPROX 1 O'CLOCK. REMOVED MINOR SURFACE CORROSION IAW RD8-57-1907. APPLIED ALODINE AND PRIMER TO ALL BARE METAL.SDR GLBA20110531FBulkhead · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE BULKHEAD WHERE THE HYD POWERPACK ATTACHES, LT INBD WING, 3.6" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-004. MATERIALS UTILISDR EE4Y20110299Fitting · corrodedRT WING, INNER REAR SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING'S BORE AND SPOTFACE WITH CORROSION. MAJOR REPAIR.SDR EE4Y20110298Fitting · corrodedLT WING, INNER REAR SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING'S BORE AND SPOTFACE WITH CORROSION. MAJOR REPAIR.SDR IPXA11M66840Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E BEADED DOUBLER CRACKED AT STA XOS 653 ABOVE SLAT NR 4 EXTEND PULLEY. REPAIRED LT WING L/E INTERNAL BEADED DOUBLER BETWEEN STA XOS653-657 IAW SRM 57-40-02, REPAIR 9, FIG 203.SDR DALA1404530191Structure · damagedLOWER WING SKIN TENSION BOLT HOLE. REPAIRED IAW AA 5700-01029.SDR 2011FA0000299Strut · mismanufacturedMECHANIC REPORTED TO FSDO THAT THEY HAD PURCHASED AIRFRAME SEALED FRONT LIFT STRUTS, STC NR SA02300AK, PN AF-MA-A815 REPLACEMENT STRUTS THAT SATISFY AD 2007-16-14, ACTION 4, REPLACEMENT AND AD 2008-04-09 BY USING AN FAA APPROVED EQUIVALENT SEALED STRUT. AFTESDR CA110426008Bolt · failed(CAN) SINGLE REPORT FROM A FOREIGN OPERATOR WITH A PICTURE SHOWING EVIDENCE OF SURFACES CRACKS IN BOLT, PN C6WM1411-029. THE BOLT HAS 2712.3 HRS/2182 LANDINGS SINCE NEW APRIL 2004, 7 YRS. OTHERWISE THE CONDITION IS UNKNOWN. BOLT IS PART OF THE PRIMARY LOAD SDR GR4D20110412002Winglet · corrodedLT WINGLET CORRODED.
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