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.

SDR LR7A2011041900179Former · crackedDURING SCHEDULED C-9 CHECK, FOUND RT OTBD TO INBD WING T/E UPPER ATTACH ANGLE WITH MULTIPLE CRACKS AT OWS0. REPAIR ACCOMPLISHED BY REPLACING FORMER IAW SMP583, CHAP 51-60 & 51-70.Apr 11, 2011 · N405LC · Lkheed 382GSDR UALA2011040701681Screw · looseFUEL LEAKING FROM RT WING OUTBOARD FIXED FLAP TRACK PORTION AT A RATE OF 2 DROPS PER MINUTE. LOWERING FLAPS DRAINED APPROX 1 CUP OF FUEL. REMOVED FWD END OF CANOE. FOUND MULTI SCREWS LOOSE. SECURED, NO FURTHER LEAKAGE.Apr 7, 2011 · N407UA · Airbus A320232SDR FDEA201104061337Control Panel · corrodedRT WING, FUELING CONTROL PANEL P28 FOUND WITH CORROSION. RT WING RE-FUELING CONTROL PANEL P28 REPLACED BY FABRICATION IAW DWG 344N5120-4, SHT 2, REV A. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Apr 6, 2011 · N948FD · Boeing 757236SDR 2011FA0000236Structure · corrodedDURING REPAIR OF THE LT WING L/E, FOUND CORROSION IN AN AREA THAT IS NOT ACCESSIBLE WITHOUT REMOVING RIVETS AND THE DIFFUSER TUBE. THESE AREAS WERE BLENDED AND PRIMERED USING REPAIR DATA FROM MFG. THIS SITUATION WOUDL HAVE CONTINUED TO CORRODE WITHOUT ANY INMar 30, 2011 · N323QS · Cessna 680CESDR IPXA1665736Panel · delaminatedINSPECTION TYPE:C, RT WING INBD AILERON L/E LWR PANEL FOUND DAMAGE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5, REV 49.Mar 18, 2011 · N319UP · Boeing 76734AFSDR UIEA2011031400208Structure · crackedCRACK ON THE CHORD OF LT WING FIXED T/E LOWER SUPPORT STRUCTURE AT WS 1185.40. (REPAIR IAW NR T2011A57B-615, REV 00 AND REV 01)Mar 14, 2011 · N499MC · Boeing 74747UFSDR GLBA20110304FStructure · damagedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RT OB WHEEL WELL KEEL ATTACHING HOLES FOR OB FENDER BRACKET HAS ELONGATED HOLES. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-54Mar 4, 2011 · N100UX · Beech 1900DSDR FDEA201102230696Structure · damagedLT WING T/E THROUGH HOLES FOR HYD LINES ARE ELONGATED AT WS OWS 1083.Feb 23, 2011 · N430FE · Airbus A310203SDR IPXA1M65046Doubler · crackedINSPECTION TYPE:3C, BEADED DOUBLERS CRACKED INSIDE LT WING L/E NEAR STA XOS670. FABRICATED AND INSTALLED REPAIR REF IAW SRM 57-40-02 REPAIR 9, FIG 203.Feb 17, 2011 · N260UP · Doug MD11FSDR IPXA1M65045Doubler · crackedINSPECTION TYPE:3C, BEADED DOUBLERS CRACKED INSIDE LT WING L/E ON EA SIDE OF RIB AT STA XOS706. REMOVED RIB FOR ACCESS, FABRICATED AND INSTALLED REPAIR BETWEEN XOS692 & XOS 703 REF SRM 57-40-02, REPAIR 9, FIG 203, 51-35-01, DWG ARB2894, RE-INSTALLED RIB.Feb 17, 2011 · N260UP · Doug MD11FSDR IPXA1564785Plate · crackedINSPECTION TYPE:C2, RT WING T/E LOWER SURFACE HAS CRACKED WIGGLE PLATE AT RSS 328. R & R WITH NEW WIGGLE PLATE IAW SRM 51-40-02-0G.Feb 16, 2011 · N414UP · Boeing 75724APFSDR GR4D20110207001Structure · corrodedWING T/E CORRODED.Feb 7, 2011 · N489QS · Gulstm GIVG400SDR IPXA1M64474Structure · crackedINSP TYPE:1C LT WING L/E COMP CEILING HAS CRACKS AT 3 EA FASTENERS, 12" INBD OF NR10 SLAT TRACK XOS 637-647. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR IAW SRM 57-40-02, REPAIR 9, FIG 203.Jan 18, 2011 · N278UP · Doug MD11FSDR DALA1107900178Skate Angle · chafedLT WING OTBD SKATE ANGLE INTERIOR CHAFED AREA REPAIRED IAW ER/A 487057-14.Jan 17, 2011 · N178DN · Boeing 767332SDR DALA1103280909Guard · misinstalledDURING LINE MX CHECK FOUND A FLIGHT CONTROL CABLE GUARD INCORRECTLY INSTALLED AND WITH HARDWARE MISSING. 4 CONTROL CABLES THAT RUN NEXT TO THE LT SIDE CATWALK ON THE AFT 48 SECTION. WERE ROUTED THRU THE OUTSIDE OF THE CABLE GUARD INSTEAD OF THE INSIDE. THE Jan 17, 2011 · N909DL · Doug MD88SDR EE4Y20110020Structure · corrodedLEFT WING REAR SPAR AREA, MACHINING JACK ANCHORAGE WITH CORROSION AROUND THE BORE UPPER AND LOWER SURFACE AND AT THE BORE INNER SURFACE. REQUIRE A MAJOR REPAIR.Jan 14, 2011 · N502NK · Airbus A319132SDR DALA1100323721Vapor Barrier · crackedTHE LT VAPOR BARRIER WAS FOUND CRACKED AND REPAIRED IAW SRM 57-10-10. REPAIR 2 OF APB SUPPLEMENT.Dec 23, 2010 · N391DA · Boeing 737832SDR DALA1100313721Vapor Barrier · crackedRT WHEEL WELL VAPOR BARRIER FOUND CRACKED AND REPAIRED IAW SRM 57-10-10 REPAIR 2 OF APB SUPPLEMENT.Dec 23, 2010 · N391DA · Boeing 737832SDR UALA2010122104677Doubler · leakingRT WING FIRST FLAP TRACK FAIRING OTBD OF ENG HAS FUEL LEAKING OUT OF WEEP HOLE. LEAK EXIT POINT IS BETWEEN AFT MOUNT DOUBLER PLATE AND WING. AFT INBD CONNER OF THE RT WING NR3 FLAP TRACK BEAM. ALSO LOWER HI-LOCK IN AFT SPAR JUST BEHIND NUT OF AFT CENTERING PDec 20, 2010 · N410UA · Airbus A320232SDR X7PA20101215001Unknown · vibrationACFT EXPERIENCED A WINGTIP VIBRATION OF APPROX 24" AMPLITUDE AND 3-PER-SECOND FREQUENCY AT BOTH WINGTIPS. THIS EVENT LASTED FOR A DURATION OF APPROX 15-20 SECONDS DURING DESCENT THROUGH FL330 AT MACH 0.78 AND RELATIVELY LIGHT ACFT LOAD. THIS EVENT WAS INDUCED Dec 15, 2010 · N585VC · Raythn HAWKER800XPSDR FDEA201012154679Shear Tie · crackedREF EO F-5710-7-5002, PT 4, RT WING PANEL SUPPORT BEAM CLIP CRACKED AT IRSS 164.95. CRACKED RT WING PANEL SUPPORT BEAM CLIP AT IRSS 164.95. R & R IAW EO F-5710-7-5002 PT 4 (WING T/E FIXED UPPER PANEL SUPPORT BEAM CLIP INSP AND REPLACEMENT). REPAIR IS CLASSIFDec 15, 2010 · N946FD · Boeing 757236SDR 2010FA0001194Link · corrodedLT WING SHROUD BOX FWD INBD SUPPORT LINK CORRODED. NO CORROSION REMOVAL LIMITS AVAILABLE. SUPPORT LINK IS LISTED AS PRIMARY/ FATIGUE CRITICAL STRUCTURE.Nov 22, 2010 · N508JL · Airbus A320232SDR QXEA2010111200733Structure · damagedON APPROACH, RECEIVED A BIRD STRIKE TO THE RT WING OTBD TO THE NACELLE. BIRD STRIKE DAMAGED THE FWD WING SPAR AND PENETRATED INTO THE FUEL TANK. ACFT IS CURRENTLY DOWN FOR REPAIRS.Nov 8, 2010 · N422QX · Bombdr DHC8402SDR FOTR2016910895Structure · cracked(FOTR) RT WING FIXED L/E STA XW300 CRACKED. NR10895, WO20169 FASI.Oct 18, 2010 · N831US · Doug MD83SDR IPXA10M63553Bulkhead · crackedINSP TYPE:4C, LT WING L/E COMPT AT XORS1070 OTBD BULKHEAD RIB AT L/E OTBD CORNER IS CRACKED AND MISSING A PIECE OF MATERIAL. TRIMMED OUT DAMAGE ON LT WING L/E BULKHEAD HORZONTAL FLANGE AT XORS 1093. FABRICATED AND INSTALLED REPAIR REF EO 5720-40434-A AND STAOct 11, 2010 · N284UP · Doug MD11FSDR FDEA201010113993Doubler · crackedCRACKED BEADED DOUBLER INBD OF SLAT TRACK NR11 AT LT WING FIXED L/E COMPARTMENT. CRACKED BEADED DOUBLER INBD OF SLAT TRACK NR11 AT LT WING FIXED L/E COMPARTMENT REPAIRED IAW SRM 57-40-02 FIG 203, REPAIR 9 REV 44. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, Oct 11, 2010 · N625FE · Doug MD11FSDR IPXA10163558Wing · dentedINSPECTION TYPE:10YR, RT ASA HAS A DENT IN OTBD LOWER CORNER. ACCOMPLISHED REPAIR ON RT ASA OTBD LOWER CORNER IAW EO A300-5750-40464-A.Oct 7, 2010 · N137UP · Airbus A300F4622RSDR CA101005002Beam · cracked(CAN) CRACKED BEAM ASSY.Oct 5, 2010 · Lakeac 250LAKESDR FDEA201010013859Structure · crackedRIGHT INBD MID FLAP INBD ACTUATING MECHANISM PUSH ROD CUTOUT CRACK. CUT OUT DAMAGED AREA OF R/H INBD MIDFLAP T/E CHORD 47 1/2" LONG IAW FED EX B727 SRM REV 103 51-10-1 FABRICATED REPAIR FROM BAC1503-100046 7075 T6 DIM 47 1/2" LONG AND SPLICE FROM BAC1503-Oct 1, 2010 · N490FE · Boeing 727227SDR REXA201000169Seal · missingRIGHT WING TRAILING EDGE P/N 601R10336-130 RAZOR SEAL UNDER THE FLIGHT SPOILER WAS FOUND WITH A PORTION MISSING. THE MISSING PORTION MEASURES 7.88 INCHES IN LENGTH WITH NO OBVIOUS ORIGIN FOR THE DISCREPANCY VISIBLE. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-Sep 30, 2010 · N8839E · Cndair CL6002B19SDR UIEA2010092900169Wing · damagedDURING TAXI IN, TOP AND RT WING WINGLET CAME IN CONTACT WITH PARKED ACFT (EO 4457A308 ISSUED. PART 1 TIME LIMITED REPAIR ACCOMPLISHED. PART 2 REPEAT INSPECTIONS TO BE ACCOMPLISHED. PART 3 PERMANENT REPAIR TO BE ACCOMPLISHED PRIOR TO THE ACCUMULATION OF 10 FLIGSep 29, 2010 · N263SG · Boeing 747481SDR DALA1023679868Bolt · crackedDURING M-CHECK FOUND CRACK IN RT WING WEB OTBD OF RT BOTTLE BOLT. REPAIRED IAW SRM 57-21-00, SRM 51-30-2, SRM 51-30-5 PAGE 226.Sep 23, 2010 · N777NC · Doug DC951SDR CA101027010Structure · damagedBIRD STRIKE IN DECENT AT 6000 FEET, RESULTING IN THE RT WING ROOT BEING DAMAGED. FAIRING REMOVED AND ANOTHER FAIRING INSTALLED. DAMAGED FAIRING SUBSEQUENTLY REPAIRED IAW THE SRM.Sep 21, 2010 · Dhav DHC8102SDR IPXA10M62995Structure · chafedINSPECTION TYPE:2C, LT WING L/E AT NR 10 SLAT TRACK CAVITY OPENING, INBD EDGE IS CHAFED AND REPAIR PATCH IS CHAFED. REMOVED PATCH, FABRICATED AND INSTALLED REPAIR DOUBLER IAW STA-SA EA 011-5750-01-A2703 I/R AND EO MD11-5730-40040-A.Sep 10, 2010 · N296UP · Doug MD11FSDR CA100907008Strut · crackedWING STRUT FITTING, LT, UPPER PN D3081-6L. DURING A SCHEDULED INSP, A SUSPECTED CRACK WAS NOTED ON THE UPPER LINK, INNER FACE, EMANATING FROM BUSHING HOLE. AN EDDY CURRENT INSP WAS PERFORMED ON THE SUSPECTED AREA AND IT WAS CONFIRMED THAT THE AREA WAS CRACKEAug 22, 2010 · Dhav DHC3SDR V0XR201008190016Seal · deterioratedLT WING INBD FLAP BUTTE DOOR SEAL DETERIORATED. R & R LT WING INBD FLAP BUTTE DOOR SEAL.Aug 19, 2010 · N851HK · Emb EMB145LRSDR FDEA201008193046Skin · crackedLT WING FIXED L/E TELESCOPIC DUCT CUTOUT FOUND CRACKED. LT WING FIXED L/E TELESCOPIC DUCT CUTOUT CRACKED AREA ACCOMPLISHED REPAIR IAW EA NR 8-5710-143715, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.Aug 19, 2010 · N562FE · Doug MD1010FSDR GLBA20100819FFastener · looseSIG EVENT - PILOT REPORTED THAT AN OVERWHELMING ODOR OF FUEL ENTER THE CABIN AND COCKPIT. MAINTENANCE FOUND LOOSE FASTENERS JUST OUTBOARD OF RT NACELLE AT FORWARD SPAR, REPLACED FASTENERS AND SEALED AREA, REFUELED, NO LEAKS OR ODOR PRESENT IAW SRM 51-10-00, CAug 18, 2010 · N210GL · Beech 1900DSDR IPXA10M62263Structure · crackedINSPECTION TYPE:1C, IN LT WING L/E COMPARTMENT, 6" OTBD OF SLAT TRACK NR10 CEILING HAS 2 EA LONG CRACKS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02, REPAIR 9, FIG 203.Aug 14, 2010 · N275UP · Doug MD11FSDR IPXA10M62262Structure · crackedINSPECTION TYPE:1C, IN LT WING L/E COMPARTMENT, 13" INBD OF SLAT TRACK NR10 CEILING HAS CRACKS AT FASTENERS AT SEVERL LOCATIONS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER,AND ANGLES IAW SRM 57-40-02 REPAIR 9, FIG. 203.Aug 14, 2010 · N275UP · Doug MD11FSDR VGQY2010081200083Beam · crackedRIGHT WING L/E BULLNOSE SKIN ADJACENT TO NR 16 KRUEGER FLAP O/B LINKAGE FOUND CRACKED. COMPLIED WITH EN1180-10.Aug 12, 2010 · N815SA · Boeing 7472L5BSDR VGQY2010081200082Beam · crackedRIGHT WING L/E BULLNOSE SKIN ADJACENT TO NR 14 KRUEGER FLAP O/B LINKAGE FOUND CRACKED. COMPLIED WITH EN1180-10.Aug 12, 2010 · N815SA · Boeing 7472L5BSDR QXEA2010080400471Structure · corrodedAFT CARGO BAY SUBFLOOR DECK LIGHTING HOLE AT APPROX X730-X734 AND Y17L HAS CORROSION FORMING AROUND EDGE GROOVE. REMOVED CORROSION AT LIGHTNING HOLE IAW SRM 51-21-00. HFEC IAW -8400 NDTM PART 6, 51-00-01 AT BLENDED AREAS. NO CRACKS NOTED. LIGHT CORROSION OAug 3, 2010 · N410QX · Bombdr DHC8402SDR FDEA201008032793Support Beam · crackedRT WING REFUELLING DOOR CUT OUT OTBD SUPPORT BEAM FOUND CRACKED. REPAIRED IAW EA 8-5710-140442, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.Aug 3, 2010 · N396FE · Doug MD1010FSDR 2010FA0000907Structure · corroded(SPUY) RT WING INBD L/E OUTER SECTION UPPER PART CORRODED AT STA XW 257.000.Jul 31, 2010 · N71CX · Doug DC862FSDR FDEA201007192589Tee Fitting · crackedLT TEE FITTING HOLE "C" SHOWS A CRACK INDICATION WHILE PERFORMING BHEC FOR NDT. CONTACT ENGINEERING. ENGINEER SHALL COORDINATE A REPAIR WITH ACFT MFG THAT IS ACCEPTABLE TO THE FAA OR DGAC. REPAIRED HOLE IAW EA 6-5710-136669, TITLE "WINGS - EO 5710-7-3322-CJul 19, 2010 · N417FE · Airbus A310222SDR UIEA2010071700114Structure · damagedDURING SPECIAL CHECK (TLW); A STORM DRAGGED A MX STAND IMPACTING THE LT WING - OTBD L/E AT OLES1580.95, OLES1606.95 & OLES1625.951. DENT AT OLES 1580.95 (11.0 IN. LONG X 1.750 IN. WIDE X 0.187 IN. DEEP) REFERENCE FIG 1. EXCEEDS THE LIMITS IAW SRM 57-41-01 FIGJul 17, 2010 · N412MC · Boeing 74747UFSDR 2010FA0000760Structure · tornPILOT REPORTED THAT DURING FLIGHT, NOTICED THAT WING TIP OF LT WING WAS NOT LEVEL WITH WING. ACFT WAS LANDED AT CLOSEST AIRPORT. INSP REVEALED THAT LOWER WING TIP HAD SHEARED AWAY FROM ATTACHMENT SCREWS ON THE LOWER SECTION OF FIBERGLASS WING TIP, IN MY VIEWJul 9, 2010 · N881FT · Piper PA44180SDR CA100804019Bolt · corroded(CAN) THE REAR WING STRUT RONY BRACKETS OF THIS 1991 ADVANCED ULTRALIGHT AIRCRAFT WERE REMOVED AND THE BOLTS THAT ATTACH THE BRACKETS TO THE FUSELAGE LONGERON WERE FOUND TO BE SEVERELY CORRODED. FACTORY WAS CONTACTED AND THEY ADVISED THAT THESE BOLTS ALONG WITJun 21, 2010 · Amtr CHALLENGER1SDR 2010F00128Diffuser · cracked((JGVR)) FOUND THE WING BLEED AIR HEATED L/E DIFFUSERS CRACKED OR DEFORMED ON NUMEROUS ACFT. THIS DISCREPANCY WAS FOUND WHILE PERFORMING A301001 WING/ HORIZ STABILIZER BLEED AIR ANTI-ICE SYS DETAIL INSP. TASK 30-10-00-220 AS PART OF INSP DOCUMENT 9. THE DOCJun 17, 2010 · N378QS · Cessna 680CE
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