JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous 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 = '5720' 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 = '5720' 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 ABXA201011190158Support Fitting · corrodedAREA OF CORROSION AT APPROX WS 450 WHERE LT AILERON DROOP MECHANISM - TO AFT SPAR ATTACH ANGLE. REMOVED AND REPLACED VERTICAL SUPPORT FITTING IAW B767 AMM 51-40-02. LEAK CHECK GOOD IAW B767 AMM 28-11-00.SDR FDEA201011044253Support · crackedRT WING ALL SPEED AILERON ACTUATOR UPPER PANEL SUPPORT IS CRACKED ON THE OTBD SIDE. PARTIALLY REMOVED OTBD UPPER AILERON PANEL AND REMOVED CRACKED LANDING. INSTALLED NEW PANEL LANDING PN A5724275920300, PO 691739.5 AND RE-INSTALLED OTBD UPPER AILERON PANELSDR CA101115018Lug · worn(CAN) BOTH UPPER AND LOWER ATTACH LUGS WERE REPLACED DUE TO WEAR AT THE STRUT ATTACH BOLT HOLE. THE WEAR WAS NOTICEABLE IF YOU MOVED THE WING TIP FOR AND AFT WHILE THE FLOAT EQUIPPED AIRCRAFT WAS ON THE HARD.SDR ABXA201011170155Panel · crackedNR 4 SLAT I/B DRIVE ROD CUTOUT I/B NOSE RIB CLOSING PANEL CRACKED. REMOVED, FABRICATED NR 4 SLAT I/B DRIVE ROD CUTOUT I/B NOSE RIB CLOSING PANEL IAW DWG 114T25-12. INSTALLED RIB IAW B767 SRM 51-40-02 REMOVED AND REPLACED SLAT TRACK CURTAIN FOR NR 4 SLAT I/B SDR SWAA106710Stiffener · crackedDURING SCHEDULED HC2 CHECK, FOUND RT WING VERTICAL STIFFENER CRACKED AT REAR SPAR STA 545. REMOVED AND REPLACED STIFFENER PER SRM.SDR FDEA201010234152Angle · damagedREFER TO EO 6-5710-3322 A3 PT3 & 4, FOUND THE FASTENER HOLES IN THE INTERNAL ANGLES ON THE CENTER WING BOX HAVE BEEN SECOND OVERSIZED AT PREVIOUS MAINTAINANCE CHECK PERFORMED ROTO-TEST INSPECTION REQUIREMENTS OF EO 6-5710-7-3322 A3 PT3 & 4, FOR THE HOLES WITH SDR CA101021012Washer · missingDURING A 200 HR INSP ON 2 OTHER ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS NON CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMAINSDR CA101021011Washer · missingDURING A 200 HR INSP ON 2 OTHER ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS A NON CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMASDR CA101021010Washer · missingDURING A 200 HR INSP ON 2 OTHER ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS A NON CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMASDR CA101021009Washer · missingDURING A 200 HR INSP ON 2 OTHER ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS A NON CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMASDR CA101021008Washer · missingDURING A 200 HR INSP ON 2 OTHER ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS A NON CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMASDR CA101021007Washer · missingDURING A 200 HR INSP ON 2 OTHER ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS A NON CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMAINSDR CA101021006Washer · missingDURING A 200 HR INSP ON 2 OTHER ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS A NON CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMAISDR CA101021003Washer · missingDURING A 200 HR INSP ON 2 OTHER ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS A NON CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMAISDR CA101021014Washer · missingDURING A 100 HR INSP ON ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS A NON-CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMAINDER OFSDR CA101021013Washer · missingDURING A 200 HR INSP ON ACFT, MSB 1121-109/1 WAS BEING CARRIED OUT AS REQUIRED WHEN IT WAS NOTED THAT THE WASHERS WERE MISSING. THE MFG WAS CONTACTED AND DETERMINED THAT THIS WAS A NON CONFORMANCE TO THE TYPE CERTIFICATE. IT WAS DECIDED THAT THE REMAINDER OFSDR UALA2010101903873Angle · brokenANGLE ASSEMBLY 65B12724-3 IS BROKEN OFF AT THE AFT END. MID SUPPORT BRACKET (ON SAME ASSEMBLY) CRACKS AT THE FWD HOLE. DRILLED TO FIT ANGLE ASSEMBLY 65B12724-3, MANUFACTURED REPAIR STRAP FOR MID SUPPORT BRACKET. INSTALLED BRACKET.SDR AALA20101018TUL02Strip · looseRIGHT WING STAINLESS WEAR STRIP LOOSE AT INBOARD END OF NUMBER 2 SLAT. RIGHT WING FILLED WORN AREA WITH DEVCON F, INSTALLED TITANIUM DOUBLER AND REINSTALLED STRIP PER EA MD60-27-013560 DATED 10-15-10.SDR FDEA201010144069Retainer · corrodedRT MLG CUTOUT SEAL RETAINER UNDER DOOR WARNING LIGHT AFTER REMOVING SEAL FOUND CORROSION. CORRODED SEAL RETAINER AT RT MLG CUTOUT REPLACED IAW SRM 51-40-02, REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010144068Retainer · corrodedRT MLG CUTOUT SEAL RETAINER UNDER DOOR WARNING LIGHT AFTER REMOVING SEAL FOUND CORROSION. CORRODED SEAL RETAINER AT RT MLG CUTOUT REPLACED IAW SRM 51-40-02, REV 100. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR HNAA2010110800240Panel · misrepaired623AT INBD STRESS PANEL FLANGE BLENDED BELOW MINIMUM LIMITS IAW RD8-57-455. REPAIRED 623AT LADDER PLATE FLANGE IAW EO8-57-10-0611.SDR HNAA2010110800238Panel · corroded623AT INBD STRESS PANEL FLANGE PITTED AND FRETTED ALONG INBD FLANGE. LOCALLY BLEND PITTING AND FRETTED AREA ON LADDER PLATE. COMPLIED WITH HIGH FREQUENCY EDDY CURRENT INSP CRACK CHECK, NO DEFECTS NOTED. REPAIRED IAW EO8-57-10-0611.SDR ASAA1058372Retainer · crackedLEFT WING BULKHEAD BULB SEAL RETAINER IS CRACKED. REMOVED AND REPLACED.SDR ASAA1058370Retainer · crackedLEFT WING UPPER T/E BULB SEAL RETAINER IS CRACKED AT THE ATTACH ANGLE. REMOVED AND REPLACED.SDR FDEA201010124007Shim · misalignedLT WING T/E NR 5 TRACK CARRIAGE UPPER BRIDGE INBD SHIM GOT MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR HNAA2010110800239Plate · corrodedOTBD LADDER PLATE FOR PANEL 623AT HAS FRETTING INBD. LOCALLY BLENDED FRETTING ON LADDER PLATE. COMPLIED WITH HIGH FREQUENCY EDDY CURRENT INSP CRACK CHECK, NO DEFECTS NOTED. REPAIRED IAW EO8-57-10-0611.SDR A6WA201040829Bracket · wornSTUB FAIRING (RT) ATTACH BRACKET ON WING IS WORN. R & R RT STUB FAIRING ATTACH BRACKET ON WING IAW SRM 51-42-21.SDR CA101007011Heat Shield · crackedDURING TROUBLESHOOTING OF A RT WING OVERHEAT IN CLIMB, WE FOUND DURING ACCESS THAT THE RT INBD L/E HEAT SHIELD WAS CRACKED ON THE LOWER SECTION APPROX 42 INCHES LONG. REMAINING RT WING HEAT SHIELD WERE INSPECTED, NO DEFECT FOUND. WE ALSO INSPECTED THE LT WINGSDR GLBA20101008GAngle · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP, MX FOUND A 3.5" CRACK AROUND THE RADIUS OF THE ANGLE INSIDE THE FUEL BAT AT WS YA-5021, RT WING, LOWER, JUST OTBD OF PRESSURE FUELING ACCESS PANEL. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUISDR GLBA20101008JAngle · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A 3" CRACK AROUND THE RADIUS OF ANGLE INSIDE FUEL BAY AT WS YA-4342, RT WING, LOWER SIDE, JUST AFT OF PRESSURE FUELING ACCESS PANEL.SDR SWIA201025731Angle · crackedLEFT WING AUXILIARY SPAR AT INBOARD LEADING EDGE UPPER ANGLE CRACKED. (C-CHECK)REPAIRED LEFT WING SPAR PER SRM.SDR K11A2010121372611Pin · damagedRT AFT BOTTLE PIN DAMAGED.SDR FDEA201010013861Support Bracket · crackedCRACK ANGLE CHORD AT NUMBER 7 SPOILER ACTUATOR SUPPORT BRACKET FALSE SPAR. CUT OUT SECTION OF L/H FALSE SPAR WEB 9 1/2" X 12 1/4" AND LOWER CHORD 20.33" IN LENGTH IAW FED EX B727 DWG NO. SR27-57-038 REV C. FABRICATED CHORD SPLICE ANGLES (2)EA, USING 7075-0,SDR FDEA201009273736Spacer · crackedRIGHT MLG W/W - SPACER WITH CRACK LOCATED AT FR54 AND AT Y-450 AND Z-1357. AFTER HFEC AND ROTOTEST THE CRACKS REPORTED BY THE VISUAL INSP WERE NOT CONFIRMED. IT WAS JUST A FLAW IN THE SURFACE PROTECTION SYS.SDR ASAA1048440Intercostal · crackedLT WING I/B LEADING EDGE HAS CRACKED INTERCOSTAL ON LOWER SURFACE. REMOVED SUPPORT ANGLE AND INSTALLED REPAIR PARTS.SDR IXXA10SMN093SSupport Angle · corrodedDURING ROUTINE C-CHECK INSP, FOUND RT WING UPPER PANEL SUPPORT ANGLE CORRODED AT STA XW 5.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED ANGLE. FABRICATED NEW ANGLE. CLEANED, TERATED, AND PRIMED AREA. ISDR IPXA10M62969Stiffener · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT OUTBD OF SLAT TRACK NR10 FOUND STIFFENER WITH SU SPECTED CRACK AS MARKED. REMOVED DAMAGE AND REWORKED RT WING FIXED L/E STRINGER INBD OF STA XOS 667.6. FABRICATED REPAIR STRAP AND FILLER AND INSTALLED REF EA 011- 5SDR IPXA10M62966Stiffener · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT OTBD OF SLAT TRACK NR 12 FOUND STIFFENER CRACKED AS MARKED. REMOVED DAMAGE AND REWORKED RT WING FIXED L/E STRINGER INBD OF XOS 789.6. FABRICATED REPAIR STRAP AND FILLER AND INSTALLED REF EA 011-572 0-01-A2697 REV I/SDR COEA2010091635803Strip · chafedHEAVY CHECK / CHAFING DAMAGE / LT WING FRONT SPAR UPPER SLAT STRIP LOWER SURFACE, ANTI-CHAFE BONDING STRIP HAS AREAS OF WEAR BETWEEN RIBS 2 AND 5. MAJOR REPAIR.SDR SWAA105549Support Angle · crackedDURING SCHEDULED SPV CHECK, FOUND RT WING UPPER T/E SUPPORT ANGLE CRACKED. REMOVED AND REPLACED ANGLE PER SRM AND BAC DWG.SDR ASAA1058276Bracket · crackedLT WING TRAILING EDGE SEAL RETAINER BRACKET CRACKED. REMOVED AND REPLACED BRACKET.SDR LR7A2010103100124Hinge · wornDURING SCHEDULED C-10 CHECK PER JOB CARD HC5712 FOUND RT OUTER WING LEADING EDGE FRONT BEAM OWS310 TO OWS368 LOWER HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.SDR LR7A2010103100123Hinge · wornDURING SCHEDULED C-10 CHECK PER JOB CARD HC5712 FOUND RT OUTER WING LEADING EDGE FRONT BEAM OWS0.0 TO OWS72 LOWER HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.SDR LR7A2010103100122Hinge · wornDURING SCHEDULED C-10 CHECK PER JOB CARD HC5712 FOUND RT CENTER WING LEADING EDGE FRONT BEAM LOWER HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.SDR LR7A2010103100121Hinge · wornDURING SCHEDULED C-10 CHECK PER JOB CARD HC5711 FOUND LT CENTER WING LEADING EDGE FRONT BEAM LOWER INBOARD HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.SDR LR7A2010103100120Hinge · wornDURING SCHEDULED C-10 CHECK PER JOB CARD HC5711 FOUND LT OUTER WING LEADING EDGE FRONT BEAM OWS201 TO OWS255 LOWER HINGE LOBES WORN. REPLACED LOWER HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.SDR LR7A2010103100119Hinge · wornDURING SCHEDULED C-10 CHECK PER JOB CARD HC5711 FOUND LT CENTER WING LEADING EDGE FRONT BEAM LOWER OUTBOARD HINGE LOBES WORN. REPLACED HINGE IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.SDR LR7A2010103100118Fitting · corrodedDURING SCHEDULED C-10 CHECK IN RELATION TO NR 2003 FOUND RT INBOARD WING FWD LOWER CORNER FITTING WITH DEEP PITTING CORROSION AT MAIN BOLT HOLE / NODE FACE. REPLACED LOWER RT CORNER FITTING IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.SDR LR7A2010103100117Fitting · corrodedDURING SCHEDULED C-10 CHECK IN RELATION TO NR 2003 FOUND RT INBOARD WING FWD UPPER CORNER FITTING WITH DEEP PITTING CORROSION AT MAIN BOLT HOLE / NODE FACE. REPLACED CORNER FITTING IAW LOCKHEED SMP583 CHAPTER 51-60 & 51-70.SDR LR7A2010103100107Attach Angle · crackedDURING SCHEDULED C-10 CHECK PER JOB CARD HC5711 FOUND LT OUTER WING JOINT ANGLE CRACKED AT BOLT HOLES IN 5 PLACES AT TRAILING EDGE ATTACH ANGLE. REPAIRED IAW LOCKHEED SMP583 FIG 57-40-08.
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