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 V0XR2012042700007Plate · corrodedLADDER PLATE FOR PANEL 624CT HAS PITTING. REPAIRED LADDER PLATE BETWEEN STATIONS YW=333-423 IAW REPAIR DWG 8-57-984.SDR CALA2012042600301Stiffener · crackedLT WING LES 679.8 FRONT SPAR UPPER STIFFER FOUND CRACKED. LT WING LES 679.8 FRONT SPAR UPPER STIFFER REPLACED IAW SRM 51-10-02 AND FASTENER INSTALLED IAW SRM 51-40-02. (NEW STIFFER FABRICATED DETAIL (REF NRC 5327522 (500-0070).SDR FDEA201204261610Angle · corrodedLEFT WING T/E ACCESS PANEL 541JB FORWARD SUPPORT TEE ANGLE FOUND WITH CORROSION. R & R IAW SRM 51-31-01, REV 49 AND SRM 51-33-01, REV 49. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.SDR FDEA201204241547Fitting · crackedPERFORMED NDT IAW E6-5710-7-3324 A PT2 , CRACKS WERE FOUND AT HOLE NR 1 AND HOLE NR 2 OF FRAME 40 RT UPPER CORNER FITTING.SDR FDEA201204241546Fitting · crackedPERFORMED NDT IAW E6-5710-7-3324 A PT1, CRACKS WERE FOUND AT HOLE NR 1 AND HOLE NR 2 OF FRAME 40 LT UPPER CORNER FITTING.SDR AALA20120510001Vapor Barrier · crackedCRACK ON VAPOR BARRIER IN BAY 2 ON LEFT SIDE. REPAIRED PER SRMS 57-10-10-2R 2.SDR AALA20120509015Vapor Barrier · crackedCRACK TO RIGHT VAPOR BARRIER IN BAYS 2R AND 4R. INSTALLED REPAIR DOUBLERS TO BAYS 2 AND 4 RIGHT VAPOR BARRIER PER SRM 57-10-10-2R 2.SDR SWAA2012050803762Angle · crackedRIGHT WING TRAILING EDGE ANGLE CRACKED. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.SDR R61A201204180249Attach Bracket · crackedWHILE AIRCRAFT WAS IN HEAVY CHECK MAINTENANCE FOUND THE ATTACH BRACKET CRACKED ON THE FORWARD LEFT WHEEL WELL FORWARD BULKHEAD. MAINTENANCE REMOVED AND REPLACED THE ATTACH BRACKET FOR THE LEFT WHEEL WELL FORWARD BULKHEAD IAW EMB 170-175 SRM 51-40-02 AND 51-43SDR AALA20120413039Support · corrodedNR 3 SLAT ANTI-ICE DUCT SUPPORT IS CORRODED. REMOVED AND REPLACED THE SUPPORT PER AARD 51-00-05.SDR ABXA20120412330Fitting · damagedRIGHT WING BACK UP FITTINGS FWD OF RIB 8 I/B AND O/B HAS TOOLING MARKS. REMOVED TOOLING MARKS PER ENGINEERING REQUEST IAW B767 SRM 51-10-02, ACFT WAS GROUNDED.SDR ABXA20120412331Fitting · damagedRIGHT WING BACK UP FITTING BETWEEN RIB 8 AND 9 AT FWD SPAR HAS TOOLING MARKS. REMOVED TOOLING MARKS PER ENGINEERING REQUEST IAW B767 SRM 51-10-02, ACFT WAS GROUNDED.SDR UIEA2012041200121Web · crackedWHILE DOING AN "A" CHECK INSPECTION OF THE RT WING FIXED T/E INBD SPOILERS SUPPORT RIBS, A 1.5 INCHES LONG CRACK WAS FOUND ON THE WEB OF THE INBD SUPPORT RIB ASSY AT WBL 255.692. THE DAMAGE EXCEEDED THE LIMITS OF THE SRM 57-51-02, FIGURE 101. CRACK REPAIREDSDR COEA2012041104900Attach Angle · crackedHEAVY CHECK / MAJOR REPAIR: LT WING TRAILING EDGE ANGLE FOR DROP DOWN PANEL AT RIB 15 FOUND CRACKED DURING REMOVAL. FABRICATED AND INSTALLED LT WING REAR SPAR ANGLE ATTACHMENT BETWEEN RIBS 16 & 17 LT IAW ATR42 SRM.SDR AALA20120410005Vapor Barrier · crackedWING CENTER SECTION VAPOR BARRIER (GFRP) HAS 26 INCH LONG CRACK WITH INTERM REPAIR INSTALLED. INSTALLED CROSS BRACE REPAIRS TO BAYS 1L, 2L AND 4L PER SRM - WINGLET APB SUPPLEMENT 57-10-10-2R 2.SDR AALA20120410004Doubler · crackedLEFT PACK EXHAUST DUCT CUTOUT DOUBLER CRACKED AT ATTACH ANGLES. REMOVED CRACKED DOUBLER AND INSTALLED EXHAUST CUTOUT DOUBLER PER AARD 51-00-05-1 AND IPC 57-11-00-02B.SDR AALA20120406001Angle · crackedUPPER ANGLE AT THIRD FASTENER HOLE OUTBOARD FROM KEEL BEAM IN A/C BAY CRACKED. INSTALLED REPAIR ANGLE PER EA B737-57-022773 AND SRM 51-70-11-2R.SDR 7AHR201204062249Retainer Seal · corrodedCORROSION ON NR 2 L/E SLAT LOWER RUB SEAL RETAINER OTBD OF SLAT ACTUATOR ATTACH POINT. REMOVED CORRODED SEAL RETAINER, FABRICATED REPAIR PARTS AND INSTALLED SEAL RETAINER IAW SRM.SDR 7AHR2012040600003Rub Strip · gougedLT INBD ENGINE TO WING FLAP SUPPORT FITTING RUB STRIP IS GOUGED. REMOVED RUB STRIP, FABRICATED REPAIR STRIP AND INSTALLED STRIP IAW SRM.SDR IPXA2M73181Strap · crackedINSPECTION TYPE: 4C, LEFT WING L/E SPLICE STRAP AT XFS 908 IS CRACKED. FABRICATED AND REPLACED LT WING L/E SPLICE STRAP AT XFS908 REF DWG ARB3954 AND SRM 51-33-01.SDR UALA2012040402081Rub Strip · damagedLEFT WING RUB STRIP STICKING UP ON INBOARD FLAP. REPLACED RUB STRIP IAW SRM.SDR CA120403006Support Angle · cracked(CAN) WHILE PERFORMING AN INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION IAW TASK RJ2-57-900-320, THE AME FOUND A CRACK EMINATING FROM 1 OF THE RELIEF CUTOUTS FOR THE STR IN THE WEB OF THE SUPPORT ANGLE, PN: 601R10011-13. THE ACFT IS CURRENTLY DOWN FOR ASDR USAA2012040300007Strut · wornC9 CHECK - LEFT WING FLAP INTERCONNECTING STRUT HAS INTERNAL DAMAGE. NORMAL INSERVICE WEAR. FAILED WEAR CHECK. REPLACED LEFT WING FLAP INTERCONNECTING STRUT IAW A319 AMM 27-51-44.SDR UALA2012040202060Seal · damagedFOUND RT WING UPPER WING TO BODY FAIRING SEAL VIBRATING AGAINST AIRFRAME AT WS 955 AND WS WBL 97.9566 AND WS 977. REPLACED AFT SECTION OF SEAL AND SEAL GAP.SDR UALA2012040202050Hinge · brokenDOOR AFT HINGE BROKEN. LOCATED OTBD OF NR 2 ENGINE. DOOR REMOVED.SDR UALA2012032901975Panel · damagedRIGHT MLG WW LOWER TRIANGLAR PANEL DAMAGED. REMOVED DAMAGED PANEL.SDR AALA20120329005Vapor Barrier · crackedLEFT VAPOR BARRIER IS CRACKED BETWEEN VAPOR BARRIER BAYS 2L AND 4L, STARTS JUST INBOARD OF LEFT AIR CONDITIONER EXHAUST. INSTALLED FULL CROSSBRACE REPAIRS ON VAPOR BARRIER WEB BAYS 2L AND 4L PER SRM 57-10-10-2R.SDR REXA2012032100364Structure · corrodedACCESS OPENING FOR PANEL 640AT, 640BT, 640CT HAVE CORROSION. BLENDED 0.003" DEEP IAW SRM 57-21-32.SDR DALA1216700180Fitting · damagedLT WING SIDE UPPER LINK PITCH LOAD FITTING HAS SHORT EDGE DISTANCE AND IS BEING WORKED ON A PRI_(NRC 52691).SDR DALA1216690180Fitting · damagedRT WING SIDE UPPER LINK PITCH LOAD FITTING HAS SHORT EDGE MARGIN AND IS BEING WORKED ON A PRI_(NRC 52689).SDR KPVA2012031502Structure · debondedDISBONDING AT LT WING STA TO 387.0 TO LT WING STA 405.0.SDR ABXA20120314311Fitting · damagedRIGHT WING BACK UP FITTING AT RWS 385 HAS MULTIPLE TOOLING MARKS. BLENDED AREAS IAW B767 SRM 57-20-00 AND B657-59720-MR, ACFT WAS GROUNDED.SDR NSVA20120313475Screw · improper partJUST AFTER DEPARTING IAH, THE CREW REPORTED TO DISPATCH THAT THERE WAS AN AVIONICS ISSUE WITH THE HEADING FLAG. WITH NO PAX ON BOARD, THEY DECIDED THAT A RETURN TO IAH WOULD BE BEST OPTION AND TO PROCEED WITH ANOTHER AIRCRAFT AND CONTINUE THE FLIGHT. FOUND TSDR AALA20120312001Vapor Barrier · crackedRIGHT WHEEL WELL REAR SPAR VAPOR BARRIER HAS INTERIM REPAIR TO 22 INCH CRACK. INSTALLED REPAIR STRAPS AND ANGLES FOR BAYS 1R, 2R,4R PER SRM 57-10-10-2R, REPAIR 2.SDR UALA2012031301649Panel · damagedLT LOWER WING PNL 561AB IS DAMAGED. RMV'D PANEL & ROUTED TO SHOP FOR REPAIR R57160, PANEL RE-INSTALLED BY AMT.SDR UALA2012031301648Panel · damagedLEFT WING LOWER PANEL 552HB REMOVED FOR HEAT DAMAGE AND SENT TO SHOP 273. PART ROUTED TO SHOP 273 FOR PANEL REPAIR R57043, PANEL RE-INSTALLED BY AMT.SDR DALA1215121502Fitting · crackedCRACK INDICATION FOUND DURING AFT PITCH LOAD FITTING BOLT HOLE INSPECTION ON THE LEFT WING INBD BOLT HOLE. INDICATION WAS REMOVED WITHIN SP LIMITS BY OPENING HOLE TO 0.656. ERA BEING ISSUED TO ADDRESS LACK OF AVAILABLE SELF LEVELING WASHERS ERA 501250-14AD.SDR UALA2012031301647Panel · damagedLT WING LOWER PANEL 552KB REMOVED FOR HEAT DAMAGE AND SENT TO SHOP FOR REPAIR R57042, PANEL RE-INSTALLED BY AMT 024668.SDR UALA2012031301646Panel · damagedLEFT LOWER WING PNL 552LB IS DAMAGED. REMOVED PANEL AND ROUTED TO SHOP FOR REPAIR R57157, PANEL RE-INSTALLED BY AMT.SDR UALA2012031301644Panel · damagedLEFT WING LOWER PANEL 552JB REMOVED FOR HEAT DAMAGE AND SENT TO SHOP 273. PART ROUTED TO SHOP FOR PANEL REPAIR, PANEL RE-INSTALLED.SDR CA120309001Angle · cracked(CAN) THE AME WAS PERFORMING AN INTERNAL ZONAL INSPECTION OF THE CENTER WING SECTION FOR TASK RJ2-57-900-320, WHEN HE FOUND CRACKS EMINATING FROM EACH OF THE 2 RELIEF CUTOUTS FOR THE STRINGERS IN THE WEB OF THE SUPPORT ANGLE. PN: 601R10011-13 AND ANGLES, PN:60SDR FDEA201203080817Skin · corrodedLT WING LOWER SKIN DOUBLER EXTERIOR SURFACE CORRODED AT MLG RIB NR 5 LOCATION. REPAIRED IAW EA 6-5730-158253.SDR SWIA201229954Structure · crackedTHERE IS A 4 INCH CRACK IN THE RIGHT WING FIXED LEADING EDGE, JUST UNDERNEATH THE OUTBOARD END OF THE NR 1 SLAT. (SERVICE) REPAIRED RIGHT FIXED LEADING EDGE PER REO.SDR CA120309004Angle · cracked(CAN) CRACK FOUND IN THE CENTER WING FUEL TANK FWD OF THE COLLECTOR TANK, INSIDE FUEL PANEL NR 510AB, LT SIDE AT WS29.42 WHILE DOING INSPECTION RJ2-57-900-320. CRACK IS ON CLOSING ANGLE, PN: 601R10011-13. THE CRACKED ANGLE IS ATTACHED TO THE VERTICAL MEMBER SDR USAA2012030700008Angle · leakingS2 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-232 A/C'S, RIB 1/FR 42 OUTER ANGLES REPLACED. REPLACED OUTER ANGLE AT RIGHT RIB 1, FR42 IAW EA 103576A.SDR USAA2012030700007Angle · leakingS2 CHECK - BASED ON REPORTS OF FUEL LEAKS ON OTHER A330-232 A/C'S, RIB 1/FR 42 OUTER ANGLES. REPLACED OUTER ANGLE AT LEFT RIB 1, FR42 IAW EA 103576A.SDR IPXA2572624Support Fitting · corrodedINSPECTION TYPE: C, RIGHT WING FRONT SPAR INBD SUPPORT FITTING FOR TRUNNION BEARING HAS CORROSION AROUND LOWER FUSE PIN BUSHING. REMOVED CORROSION BY LINE REAM BORING AND INSTALLED OVERSIZED BUSHINGS. ALL WORK DONE IAW EA 120363 AND EO B757-5740-46395-A.SDR IPXA2572623Support Fitting · corrodedINSPECTION TYPE: C, RIGHT WING FRONT SPAR OTBD SUPPORT FITTING FOR TRUNNION BEARING HAS CORROSION AROUND LOWER FUSE PIN BUSHING. REMOVED CORROSION BY LINE REAM BORING AND INSTALLED OVERSIZED BUSHINGS. ALL WORK DONE IAW EA 120363 AND EO B757-5740-46395-A.SDR IPXA2572621Support Fitting · corrodedINSPECTION TYPE: C, LEFT WING FRONT SPAR OTBD SUPPORT FITTING FOR TRUNNION BEARING HAS CORROSION AROUND LOWER FUSE PIN BUSHING. REMOVED CORROSION BY LINE REAM BORING AND INSTALLED OVERSIZED BUSHINGS. ALL WORK DONE IAW EA 120364 AND B757-5740-46394-A.SDR IPXA2572620Support Fitting · corrodedINSPECTION TYPE: C, LEFT WING FRONT SPAR INBD SUPPORT FITTING FOR TRUNNION BEARING HAS CORROSION AROUND LOWER FUSE PIN BUSHING. REMOVED CORROSION BY LINE REAM BORING AND INSTALLED OVERSIZED BUSHINGS. ALL WORK DONE IAW EA 120364 AND EO.
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