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 FDEA201210293767Structure · corrodedRT WING OTBD FIXED T/E RIB 26 TO RIB 29 HAS 3" AREA OF CORROSION AT 2ND FROM INBD END STATIC WICK BELOW BASE WITH 60 PERCENT WORKING FASTENERS AND DISBONDED EDGES ALONG ENTIRE LENGTH. R & R RT WING FIXED T/E WEDGE IAW FSRM 51-72-10.Oct 29, 2012 · N660FE · Airbus A300F4605RSDR FDEA201210243740Structure · damagedLT WING OTBD FLAP ACCESS PANEL 566AL CUT OUT HAS ELONGATED/DOUBLE DRILLED HOLES LOC NR 2 FROM INBD LOWER CORNER AT LT WING OTBD FLAP ACCESS PANEL 566AL CUTOUT A REPAIR WAS ACCOMPLISHED ON MAE NR 47749920001 AND MAE EA 757-5754-16-F3851. REV - DATED AUG 21, 20Oct 24, 2012 · N964FD · Boeing 757200SDR QXEA2012101901325Structure · corrodedWING DRY BAY PANEL LANDING 621BT HAS CORROSION. REMOVED PANEL LANDING 621BT NUTPLATE CHANNELS IAW SRM 51-42-05-02-01. REMOVED CORROSION IAW REF RD 8/4-57-441. MIN REMAINING THICKNESS .155" FOUND OUT OF LIMITS IAW RD 8/4-57-441. HFEC INSPECTED BLENDS, NO CRACKSOct 19, 2012 · N407QX · Bombdr DHC8402SDR QXEA2012101701302Structure · corrodedWING DRY BAY PANEL LANDING 521BT HAS AREAS OF CORROSION. REMOVED CORROSION REF RD 8/4-57-441 MIN REMAINING THICKNESS NOTED .156" REF NTM 51-00-04-910-801 PT 1. HFEC INSPECTED BLENDS, NO CRACKS NOTED REF NDTM 51-00-06-910-801 PT 1. MATERIAL LOSS FOUND TO BE OUOct 17, 2012 · N407QX · Bombdr DHC8402SDR UIEA2012110600517Beam · crackedCRACK ON THE LOWER SECTION OF LT WING NOSE BEAM NEAR WS 1093. REPAIR IAW EI NR T2012A57B-2496, REV 00.Oct 15, 2012 · N249BA · Boeing 747409SDR ASOA20121010146Structure · crackedCRACK AT CENTER HINGE POINT OF LT WING GROUND SPOILER ON WING. DRILLED OUT DAMAGED HOLE, PERFORMED EDDY CURRENT INSPECTION OF HOLE, PERFORMED ROTO PEENING ON THE INNER AND OUTER AREAS OF SPAR 3 AROUND DRILL HOLE, FABRICATED A PLUG FOR DRILLED HOLE IN SPAR 3, Oct 9, 2012 · N12934 · Emb EMB145EPSDR ASAA2012100793186Torque Tube · crackedLEFT WING TORQUE TUBE IS CRACKED. R & R CRACKED BUMPER IAW CMM 57-53-22. REMOVED AND REINSTALLED BALLSCREW AND GIMBLE ASSY IAW CMM 57-53-22 AND AMM 27-51-73. OPS CHECKED GOOD IAW AMM 27-51-00.Oct 7, 2012 · N760AS · Boeing 7374Q8SDR GLBA2012100500076Structure · damagedBIRD STRIKE ON LT OTBD WING FROM WS 192.74 TO APPROX 201.74, APPROX .5" IN DEPTH. REPAIRED IAW EO 12-1900-57-011. MAJOR REPAIROct 5, 2012 · N153GL · Beech 1900DSDR 2012F00172Winglet · corrodedRIGHT WINGLET CORRODED IN ATTACH BORE, REF W/O 2142.23.3-23.6 FOR REPAIR.Oct 5, 2012 · N452QS · Gulstm GIVSDR HNAA2012100300995Bolt · corrodedRT WING TO FUSELAGE STRUT HAD RUSTED BOLT AND BORE INSIDE OF PANEL 264CR. CLEANED BORE WITH BARREL BRUSH. CORROSION WAS TRANSFERED FROM CORRODED BOLT. INSTALLED NEW BOLT AND PLI WASHER.Oct 3, 2012 · N907HA · Dhav DHC8102SDR HNAA2012100300994Bolt · corrodedAFT OTBD BOLT AND BORE IF LT AFT WING TO FUSELAGE STRUT IS RUSTED INSIDE OF PANEL 263CL. REAMED HOLE IAW DWG 85320339. CLEANED CORRSION, R & R BOLT AND PLI WASHER.Oct 3, 2012 · N907HA · Dhav DHC8102SDR HNAA2012100300993Bolt · corrodedFORWARD INBD BOLT IS PITTED ON AFT STRUT, LT WING TO FUSELAGE ATTACH POINT. R & R BOLT AND PLI WASHERS.Oct 3, 2012 · N907HA · Dhav DHC8102SDR FXGA201210011274Structure · corrodedCORRODED EXTRUSION WS 75R AT REAR INSPECTION DOOR 123 EO 1274.Oct 1, 2012 · N100CE · Doug C118ASDR 2012F00203Structure · corrodedLT WINGLET HAS CORROSION IN VERTICAL AND HORIZONTAL BORE. REPAIRED.Sep 26, 2012 · N441QS · Gulstm GIVSDR DXTA2012F00202Structure · corrodedCORROSION ON RT WINGLET ATTACH BORE, REPAIRED.Sep 26, 2012 · N441QS · Gulstm GIVSDR FDEA201209253432Tee Fitting · corrodedLT WING T/E LOWER ACCESS PANEL 541JB CUTOUT FORWARD TEE FOUND CORRODED AT XW317. CUTOUT FORWARD AREA REMOVED AS PER SRM 51-31-01 REVISION 50 AND REPLACED WITH NEW TEE AS PER SRM 51-35-01 REVISION 50 AND SRM 51-33-01 REVISION 50. REPAIR CLASSIFIED AS MAJOR Sep 25, 2012 · N618FE · Doug MD11FSDR FDEA201209233402Hinge · corrodedRT OTBD FLAP, INBD FORWARD (WING) HINGE ACTUATOR OTBD HOLE FOUND CORRODED. REPAIRED IAW EA 1-5750-162587 PART 1. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 115Sep 23, 2012 · N585FE · Doug MD11FSDR FDEA201209233400Hinge · corrodedRT OTBD FLAP, INBD FORWARD (WING) HINGE ACTUATOR, INBD HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 REVISION 74. EXISTING HOLE DIAMETER 1.249", FINAL HOLE DIAMETER 1.254", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED AS PESep 23, 2012 · N585FE · Doug MD11FSDR FDEA201209213377Hinge Fitting · corrodedRT OTD FLAP, OTBD FORWARD WING HINGE ACTUATOR OTBD HOLE CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 74 EXISTING HOLE DIAMETER 1.215", FINAL DIAMETER 1.221", MAXIMUM ALLOWABLE DIAMETER 1.220". REPAIR ACCOMPLISHED IAW EA 1-5750-162586, PASep 21, 2012 · N585FE · Doug MD11FSDR HYIA20120910003Spar · corrodedDURING A REGULARLY SCHEDULED MX, DAMAGE WAS DISCOVERED TO THE RT SPAR STRAP. DAMAGE WAS A MISDRILL AND INTERGRANULAR CORROSION. BASED ON THE DAMAGE NOTED, REMOVED DAMAGED PART AND INSTALLED NEW PART.Sep 10, 2012 · N120PC · Cessna 402CSDR ASAA2012090792880Bracket · crackedRT WING INBD FIXED T/E LOWER SUPPORT BRACKET CRACKED, WS ORSS 274R. REMOVED AND REPLACED.Sep 7, 2012 · N309AS · Boeing 737990SDR TRBA20120905001Structure · corrodedDURING MX INSPECTION, FOUND THE LT WING ELECTRIC FUEL PUMP SURROUNDING AREA CORRODED. ACFT REMOVED FROM SERVICE. REMOVED CORROSION IAW 51-21-42, BLEND OUT REF 51-21-58. PERFORMED EDDY CURRENT INSPECTION ON BLENDED AREA IAW NTM MANUAL 51-60-00, NO DEFECTS Sep 5, 2012 · N425MJ · Aerosp ATR72SDR FDEA201208233133Structure · damagedRT WING TIP L/E FOUND ONE LIGHTNING STRIKE, COMPLIED WITH EA 6-5730-149056.Aug 23, 2012 · N741FD · Airbus A300B4622RSDR QXEA2012081800821Fairing · dentedLEFT FWD WING TO FUSELAGE TOUCHDOWN FAIRING HAS MULTIPLE DENTS BETWEEN STATIONS X301.000 AND 341.000. DENTS FOUND TO EXCEED LIMITS OF RD 8/4-53-2231. CONFIRMED DENTS IN ALUMINUM PORTION OF FAIRING, CRACK FREE REF NTM 51-00-06-910-801 PT 1. INSPECTED COMPOSAug 18, 2012 · N405QX · Bombdr DHC8402SDR 2012FA0000538Structure · corrodedRIGHT WINGLET ATTACH HOLES CORRODED, REFERENCE BP SE5809903 REV. C FOR REPAIR.Aug 3, 2012 · N424QS · Gulstm GIVSDR 2012FA0000537Structure · corrodedLEFT WINGLET ATTACH HOLES CORRODED, REF BP SE35809903, REV C FOR REPAIR.Aug 3, 2012 · N424QS · Gulstm GIVSDR A6WA201240748Beam · damagedLT INBD FLAP VANE ACTUATORS SLIDING BEAMS HAVE DAMAGE ON UPPER AND LOWER SURFACES FROM ROLLERS. REPAIRED BY BLENDING IAW REO 601R-57-52-1942.Jul 30, 2012 · N447AW · Cndair CL6002B19SDR DXTA201207200554Structure · corrodedLT GEAR WW HAS CORROSION ON SPAR AND LOWER SKIN. REPAIRED IAW S-680-0113/02RD.Jul 9, 2012 · N388QS · Cessna 680CESDR HNAA2012062700837Panel · corrodedFOUND CORRODED HARDWARE ON L/E PANEL 513AL. REMOVED OLD HARDWARE AND INSTALLED NEW HARDWARE.Jun 27, 2012 · N330EN · Dhav DHC8103SDR IPXA2M74170Frame · crackedINSPECTION TYPE: 4C, RT WING L/E FORMER AT XFS1026 IS CRACKED AT AFT END. REPAIRED RT WING L/E FORMER AT XFS1026, REF DWG ARB2920, SRM 51-33-01, PG 1-30, SRM 51-35-01, PG 1.Jun 20, 2012 · N288UP · Doug MD11FSDR FDEA201206142243Support · corrodedLEFT WING AT WS 165-204 UPPER T/E SKIN & PANEL SUPPORT CORRODED. REPAIRED IAW EA F-5710-159945 STEPS 1-12. MAJOR REPAIR.Jun 14, 2012 · N964FD · Boeing 757200SDR UALA2012060803161Shim · migratedRIGHT WING RETRACT ACTUATOR SUPPORT, (RSS 292) HAS SHIM MIGRATION AT LOWER CORNER. SUPPLEMENTAL DATA UPDATE, REPLACED MIGRATED SHIM WITH SOLID SHIM PER ECRA 5750-04451.Jun 6, 2012 · N505UA · Boeing 757222SDR TRBA20120524003Drain · corrodedDURING MX INSP FOUND CORRSION AT RT INBD AFT WATER DRAIN. THE ACFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO E2-5700-490, PART A. THE ACFT WAS RETURNED TO SERVICE.May 24, 2012 · N417AT · Aerosp ATR72SDR ASAA12511588Structure · chafedAIRCRAFT WAS FOUND WITH ECS DOOR FORWARD WEARING THROUGH THE STRIKER PLATE INTO THE LOWER CHORD. ACFT GROUNDED. ACCOMPLISHED REPAIR IAW REO G14956, REV A.May 24, 2012 · N588AS · Boeing 737890SDR TRBA20120522004Structure · corrodedDURING MX INSPECTION, FOUND THE RT WING BTW RIB 5-6 MAGNETIC FUEL IND. WITH CORROSION. COMPLIED WITH CORROSION BLEND OUT EO E2-5700-486. THE ACFT WAS RETUNRED TO SERVICE.May 22, 2012 · N447AM · Aerosp ATR72SDR TRBA20120522006Structure · corrodedDURING MX INSPECTION, FOUND THE LT WING BETWEEN RIBS 4 AND 5 WATER DRAIN VALVE CUTOUT WITH CORROSION. PERFORM PERMANENT REPAIR IAW PART B OF EO E2-5700-488 AT PRIOR TO THE NEXT SCHEDULE C CHECK. TEMPORARY DISPOSITION FOR CORROSION DAMAGE TO THE LOWER LT WINMay 22, 2012 · N447AM · Aerosp ATR72SDR UALA2012052402912Structure · damagedLEFT WINGLET OTBD SIDE HAS LIGHTNING STRIKE ON ONE FASTENER LOCATED 1-3 UP ON VERTICAL ROW OF REAR SPAR. LOCATED WITHIN CRITICAL AREA REF CF987 AND 989 REMOVED LEFT WINGLET. NEW WINGLET UP AND TORQUED. BUT MID FAIRING FWD SECTION DOES NOT FIT. TRIED SWAPPIMay 21, 2012 · N122UA · Boeing 747422SDR ABXA20120430344Beam · wornLEFT WING O/B FLAP I/B HINGE CARRIER BEAM (ATTACHED TO FLAP) -WHERE 3-10 LINK ATTACHS TO FLAP -O/B FLANGE I/B BUSHING LOOSE IN FLANGE. REPAIRED ON REA B653-59822-MR, ACFT WAS GROUNDED.May 7, 2012 · N739AX · Boeing 767281SDR ASAA2012052492336Structure · chafedACFT WAS FOUND WITH ECS DOOR FORWARD LATCH WEARING THROUGH THE STRIKER PLATE INTO THE LOWER CHORD. ACFT GROUNDED. ACCOMPLISHED REPAIR IAW REO-614956, REV A.May 2, 2012 · N588AS · Boeing 737890SDR FDEA201204301680Panel · crackedLT WING LOWER FIXED L/E AT REFUELING PANEL CUTOUT INBD FORWARD CORNER FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02, REPAIR 7, FIG 201, REV 49. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114.Apr 30, 2012 · N607FE · Doug MD11FSDR CA120420001Tip Cap · departed(CAN) WHILE IN CRUISE FLIGHT CONDITION, RT WING TIP SUDDENLY BROKE AWAY FROM ITS LOWER POINTS AND LIFTED TO A NEARLY VERTICAL POSITION. MINIMAL CHANGE IN CONTROLLABILITY WAS NOTED, WITH WINGS LEVEL MAINTAINED WITH ADDITIONAL AILERON TRIM. EMERGENCY LANDING WApr 19, 2012 · Amtr LANCAIRSDR NSVA20120412513Drain Valve · corrodedANGLE I/B WING SUMP DRAIN VALVE IS CORRODED AT STA 42.3 BETWEEN STRINGERS 14 AND 15. REPAIRED IAW TD 340-57-12-07.Apr 12, 2012 · N239CJ · Saab 340BSDR DALA1509809254Fitting · unknownMLG - INSPECTION, REPLACEMENT RETRACT ACTUATOR SUPPORT FITTINGS IAW EA 02-093855-03.Apr 4, 2012 · N954DN · Doug MD9030SDR ABXR2012033100031Housing · debondedRIGHT OVERWING FILL HOUSING DID NOT BOND CHECK PROPERLY. REPAIRED IAW AMES REA 46938REA15.Mar 31, 2012 · N363CM · Boeing 767338SDR FDEA201203211155Bonding Strap · corrodedRT WING, WING RIB OTBD, BOND STRAP ATTACH AREA CORRODED, WS 817.27.Mar 21, 2012 · N962FD · Boeing 7572G5SDR TRBA201206901Structure · corrodedDURING MX INSP FOUND LT WING FUEL ELECTRIC PUMP SURROUNDING AREA WITH CORROSION. LT WING LT MAGNETIC FUEL LEVEL SURROUNDING AREA WITH CORROSION. LT WING RIB 6 T/E WITH CORROSION. THE ACFT WAS REMOVED FROM SERVICE. REMOVED SURFACE CORROSION AT LT WING FUEL ELEMar 8, 2012 · N407AT · Aerosp ATR72212SDR UALA2012022101054Tip Cap · damagedLEFT WING TIP ASSY SUSTAINED DAMAGE. REPLACED WINGTIP PER AMM.Feb 20, 2012 · N415UA · Airbus A320232SDR UALA2012022001018Bolt · damagedLT WING BOLT LOCATED AT WS 416.2, STR 18L COMMON TO RIB NR 9 AND P-N 112T5373-9 FITTING HAS THREAD DAMAGE, REF EVA IMC-00713 AND IMC-00733 FOR HISTORY. REMOVED AND REPLACED BOLT WITH NEW ONE.Feb 19, 2012 · N641UA · Boeing 767322SDR FDEA201202090536Structure · gougedLT WING NR 3 SLAT TRACK IS RIDING/CUTTING INTO L/E SUPPORT STRUCTURE. FWD UPPER TRACK CORNERS. CLEARANCE CHECKED GOOD.Feb 9, 2012 · N367FE · Doug MD1010FSDR FDEA201202090535Structure · gougedLEFT WING NR 1 SLAT TRACK IS RIDING AND CUTTING INTO L/E SUPPORT STRUCTURE. FWD UPPER TRACK CORNERS. BURNISHED THE SLAT TRACK IAW CMM 57-55-04. ALODINE AND PAINT AND PRIMERED IAW SRM 51-21-01 AND 51-21-02. R & R NR 1 LT SLAT AND CLEARANCE AND OPS CHECK C/WFeb 9, 2012 · N367FE · Doug MD1010F
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