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 ASAA12711104Bracket · crackedLEFT WING T/E CAVITY AT WS 289 SEAL RETAINER BRACKET CRACKED AFT SIDE. REMOVED AND REPLACED IAW B737 700 51 40 02.SDR USAA2012012300003Support Fitting · corrodedRIB 5 INSPECTION - CORROSION ON FORWARD LUG RIGHT MAIN LANDING GEAR RIB 5 SUPPORT FITTING. REPAIRED OVERSIZED AFT LUG BORE ON FORWARD LUG RIGHT MAIN LANDING GEAR RIB 5 SUPPORT FITTING IAW EA 201678 AND EO 5707Y085.SDR QXEA2012012300017Shroud · damagedLEFT WING LOWER T/E SHROUD HAS 5 WORKING RIVETS AT APPROX STA YW 317.019. R & R 5 RIVETS ON LT WING LOWER T/E SHROUD IAW SRM 51-42-05-02-01.SDR QXEA2012012300016Shroud · damagedLEFT WING LOWER T/E SHROUD JUST INBD OF NACELLE HAS 3 WORKING RIVETS. R & R 3 RIVETS ON LT WING LOWER T/E SHROUD INBD OF NACELLE IAW SRM 51-42-05-02-01.SDR A6WA201240236Angle · crackedLEFT WING UPPER ANGLE CRACKED AT OTBD CORNER. REMOVED AND FABRICATED ANGLE IAW SRM 51-40-11, 51-31-06.SDR A6WA201240295Shroud · debondedOTBD END OF INNER SHROUD DISBONDED AND RIVET IS PULLED THROUGH. COMPLIED WITH STEPS 1-4 OF REO 601R-57-41-161.SDR IPXA2M71724Angle · corrodedINSPECTION TYPE: 4C, RT WING T/E TEE ANGLE BETWEEN XW 311-373 AT FWD EDGE OF PANEL 641JB HAS INTERGRANULAR AND EXFOLIATION CORROSION. REPAIRED RT WING T/E BEAM ASSY LOWER CAP AT XW311-373 REF STA, EA 011-5720-01-A3659 AND UPS EO MD11-5720-46034-A.SDR DALA1517300174Fitting · not reportedWINGS DIAGONAL BRACE AFT PITCH LOAD FITTING, LWR WIN IAW EA 01-451812-03.SDR CA120112001Angle · cracked(CAN) THE AME WAS PERFORMING A 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 ANGLE PN:601R10SDR A6WA201240233Angle · crackedLEFT WING AT WS 143.189, INBD ANGLE IS CRACKED UNDER PANEL 520ML. R & R IAW SRM 51-41-02.SDR DALA1203116303Thrust Bearing · worn35/681 WING T/E NR 8: THRUST BEARING WORN. REPLACED WITH NEW THRUST BEARING.SDR IPXA2671140Stiffener · crackedINSPECTION TYPE:C, WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 RBL 10.94. STIFFENER REPAIRED IAW SRM 57-10-10-2R2 REPAIR 2, FIG 201, REV 52. JUST AT STA 785.9, RBL 10.94, ORG MATL IS BAC1518-912-2024T3511, CRACK LENGSDR SWAA120230Web · damagedDURING SCHEDULED 14Y CHECK, FOUND RT MLG SUPPORT BEAM VERTICAL WEB DAMAGED. REPAIRED WEB PER EA.SDR DALA1209390668Fill Port · corrodedRT WING OVERWING FILL PORT FAILED BONDING CHECK BETWEEN ADAPTER AND UPPER SKIN. REMOVED FILL PORT. REMOVED CORROSION ON MATING SURFACE IAW SRM 57-20-01 FIG10. HFEC INSPECTION IAW NDTM PT6 51-00-19, NO CRACKS OR CORROSION. FPI PER SOPM 20-20-02 NO CORROSIOSDR HNAA2012010900467Angle · crackedRT CANOE NR 5 FAIRING AFT BRACKET IS CRACKED ON FLAP CARRIAGE. REPLACED BRACKET ON RT NR 5 CANOE FAIRING WITH SOLID RIVETS IAW SRM 51-42-05.SDR HNAA2012010900465Support Angle · crackedLT WING BLEED AIR DUCT SUPPORT ANGLES CRACKED AT STA YW49.0 AND YW69.0. REMOVED BLEED AIR DUCT AND REPLACED WITH MADE PART, INSTALLED WITH SOLID RIVETS IAW SRM 51-42-05. FABRICATION COVERED BY WORKCARD 9084.SDR SWIA201229312Structure · damaged(C-CHECK) RIGHT CENTER LEADING EDGE DAMAGED BETWEEN WS 158.52 AND 167.46. REPAIRED RIGHT CENTER LEADING EDGE BETWEEN WS 158.52 AND 167.46.SDR AALA20120105TUL11Vapor Barrier · crackedBULKHEAD (STATION 663) VAPOR BARRIER WEB CRACKED. INSTALLED REPAIR STRAPS, ANGLES AND JOINT ANGLES PER SRM 57-10-10-2R 2.SDR AALA20120105TUL04Vapor Barrier · crackedVAPOR BARRIER CRACKED AT RIGHT WING CENTER SECTION, BAYS 1, 2 AND 4. INSTALLED PERMANENT REPAIR PER SMR 57-10-10-2R REPAIR 2.SDR DALA1200203768Fitting · corrodedDURING TRIPLE GEAR CHANGE, EA 12-487906-12 REV A ME 03 OPN 0301 WAS WORKED. STEP 3 WAS WORKED TO REPAIR CORROSION ON FITTING. REF EO CARD E27 THROUGH E29. (CONTROL # C12311121)SDR NSVA2011341Boot · damagedWHILE A/C WAS PARKED AT GATE 9A IT WAS HIT BY A VAN ON THE RIGHT WING CAUSING DAMAGE TO THE BOOT.SDR CA111222009Angle · cracked(CAN) WHILE PERFORMING A DETAILED INSPECTION OF THE LT SIDE AND RT SIDE CENTER FUEL TANK FOR TASKS RJ2-57-510-502 AND RJ2-57-610-502, RESPECTIVELY, THE AME NOTED CRACKS EMINATING FROM EACH OF THE 2 RELIEF CUTOUTS FOR THE STRINGERS IN THE WEB OF THE SUPPORT ANGSDR UALA2011122107047Fastener · looseCREW REPORT: FUEL SEEPAGE ON RIGHT WING BY ACCESS PANEL JUST OTBD OF FUELING PANE. SAMC TEXT: FUEL ACCESS PLATE. TORQUED FASTENERS FOR PANEL 640NB, NO LEAKS NOTED.SDR P5CA2011122100511Scoop · damagedTHE LEFT WING VENT SCOOP INLET AREA WAS FOUND TO BE DAMAGED. (PRELIMINARY INSPECTION REVEALED FATIGUE CRACKS ON VENT SCOOP ASSEMBLY WHICH ARE NOT REPAIRABLE. THE VENT SCOOP ASSEMBLY WILL BE REPLACED ONCE PARTS BECOME AVAILABLE. AIRCRAFT IS AOG. ).SDR 7SSA20120102Panel · crackedRT WING TRAILING EDGE INBOARD PANEL ADJACENT TO FUSELAGE (WS 48.30) HAS A CRACK 1.25 INCH LONG AND HAD THREE SCREWS PULLED THROUGH.SDR REXA201100932Fitting · chafedLEFT WING AFT SPAR FLAP ROLLER GUIDE FITTING CHAFED APPROX .025 DEEP AND WING PLANK LOWER SKIN CHAFED APPROX .010 DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-51-143 AND SRM 51-12-00.SDR ASAA11410782Support Angle · crackedLEFT WING UPPER FIXED T/E PANEL SUPPORT ANGLE COMMON TO SIDE OF LEFT FAIRING CRACKED. REPLACED CRACKED ANGLE WITH NEW PER SRM 51 40 02.SDR QXEA2011122160136Shroud · looseRT WING T/E SHROUD HAS 6 LOOSE RIVETS JUST INBD OF NACELLE. REMOVED LOOSE RIVETS IAW SRM 51-42-05-02-01.SDR QXEA2011121601358Shroud · looseRT WING LOWER T/E SHROUD HAS 4 LOOSE RIVETS JUST OTBD OF NACELLE. R & R LOOSE RIVETS ON RT WING T/E SHROUD IAW SRM 51-42-05-02-01.SDR A6WA201141133Doubler · damagedDURING REMOVAL OF NUT PLATE ON RT INBD L/E FASTENER HOLE WAS DOUBLE DRILLED. REMOVED UNSERVICEABLE 601R12045-8 DOUBLER. FABRICATED NEW DOUBLER AND REPLACED TO SERVICEABLE CONDITION IAW SRM 51-42-06 AND 51-42-15.SDR ASAA11410764Support Angle · crackedRIGHT WING TRAILING EDGE AILERON AREA REAR SPAR/RIB AFT SUPPORT ANGLE IS CRACKED. REPLACED SUPPORT ANGLE.SDR AALA20120113TUL03Vapor Barrier · crackedRIGHT WHEEL WELL VAPOR BARRIER CRACKED. ACCOMPLISHED REPAIRS PER SRM 57-10-10.SDR ABXA20111205150Fitting · damagedSIDE LOAD FITTING TO BACK UP FITTING HAS TOOLING MARKS. BLENDED AREA AND REPAIRED IAW REA B657-59598, AWG.SDR UIEA2011120600703Retainer · damagedDURING EO 4457A391, PART 2, MX REPORTED DAMAGE TO THE RT INBD FIXED T/E WB135 - WBL155 SEAL RETAINER AND SEAL (REF FIG 1). PERFORMED A TIME LIMITED REPAIR.SDR AALA20111203TUL02Vapor Barrier · crackedLEFT VAPOR BARRIER CRACKED 16.5 INCHES, LEFT WING REAR SPAR AREA. INSTALLED REPAIR STRAPS AND ANGLES AT BAYS 5L, 7L, AND 8L, PER SRM 57-10-10-2R 2, AND EA B737-57-0174466 DATED 6/13/2011.SDR AALA20111203TUL01Vapor Barrier · crackedTHREE INCH CRACK IN LEFT VAPOR BARRIER BETWEEN BAYS L2 & L4, LEFT WING REAR SPAR. INSTALLED REPAIR STRAPS AND ANGLES PER SRM 57-10-10-2R 2.SDR A6WA201240130Shroud · crackedRT WING OTBD L/E SHROUD CRACKED. FABRICATED REPLACEMENT SHROUD IAW SRM 51-24-26 & 51-40-11.SDR ASOA201102262Bracket · crackedRT WING L/E INBD SECTION 620JL HAS CRACKED BRACKET AT OTBD END WS140.00. LOCATED, DRILLED AND DEBURRED NEW ANGLE IAW SRM 51-40-11. INSTALLED IAW SRM 53-00-47 AND CMM CGFP-02, REPAIR I.SDR CA111125005Support Angle · cracked(CAN) WHILE PERFORMING A DETAILED INSPECTION OF THE LT & RT CTR FUEL TANK FOR TASKS RJ2-57-510-502 & RJ2-57-610-502 RESPECTIVELY, THE AME NOTED CRACKS EMANATING FROM EACH OF THE TWO RELIEF CUT OUTS FOR THE STRINGERS IN THE WEB OF THE SUPPORT ANGLE, PN 601R-100SDR QXEA2011112801245Angle · corrodedCORROSION FOUND ON WING BULKHEAD ANGLE OF THE BULKHEAD ASSY LOWER INBD EDGE. CORROSION BLENDED TO LIMITS IAW RD 8/4-25-262. COMPLIED WITH TASKCARD RD 8/4-25-262.SDR UALA2011112106350Beam · damagedRIGHT WING FIXED T/E BEAM UPPER CHORD LUG BORE DAMAGED AT WBL 235.2. REPAIRED IAW 747 EN-57-0187. REPAIR IS AN INTERIM REPAIR AND DVI FOR BEARING INSTALLATION AT WBL 235.20 MUST BE ACP AT 1C INTERVAL, NOT TO EXCEED 24 MONTHS. THIS CF CAN CLEAR ONCE EC IS CRSDR ASAA11410676Angle · crackedRIGHT WING LOWER FIXED L/E ANGLE CRACKED AT LES 198. REPLACED ANGLE AND CLIP.SDR ASAA11410672Fitting · crackedWHILE REMOVING CRACKED ANGLE ON CUST CARD 5351122 FOUND CRACKED CLIP FOR THE ANGLE (CHANNEL). REPLACED CLIP.SDR CA111117009Angle · cracked(CAN) WHILE CARRYING OUT TASK: RJ2-28-900-750 FOR FUNCTIONAL CHECK OF COLLECTOR TANK CHECK VALVES, CRACKS WERE FOUND ON THE OTBD SIDE OF ANGLE, PN 601R10011-14A IN THE RT SIDE COLLECTOR TANK. THE CRACKS ARE 1.495" AND 1.200" IN LENGTH AND WERE OBSERVED TO BE SDR CA111116010Angle · cracked(CAN) CRACKS FOUND ON THE OTBD SIDE OF LT SUPPORT ANGLE IN THE LT SIDE COLLECTOR TANK BY AN AME WHEN HE WAS IN THE FUEL TANKS CARRYING OUT TASK: RJ2-28-900-750 FOR FUNCTIONAL CHECK OF COLLECTOR TANK CHECK VALVES. THE CRACKS ARE APPROXIMATELY 2.300" EMINATING SDR CA111114011Fitting · damaged(CAN) DURING FIRST 5 YEAR WING BOLT REPLACEMENT & WING FITTING NDT INSPECTION, SOME MECHANICAL DAMAGE WAS NOTED ON THE SPOT FACE OF THE UPPER AFT RT OUTER WING ATTACH BATHTUB FITTING. DAMAGE WAS CAUSED BY IMPROPERLY INSTALLED CHAMFERED WASHER AT THE NUT OF THSDR USAA2011111400027Angle · crackedS2 CHECK - CRACKS ON LEFT WING ANGLE AT FASTENER HOLES NUMBERS 7, 8, 10, FR42, RIB 1. REPLACED LEFT WING ANGLE AT FR42, RIB 1 IAW EA 103364.SDR USAA2011111400010Angle · crackedS2 CHECK - CRACKS ON RIGHT WING ANGLE AT FASTENER HOLES NUMBERS 7, 8, 10, FR42, RIB 1. REPLACED RIGHT WING ANGLE AT FR42, RIB 1 IAW EA 103364.SDR UALA2011111106169Sealant · damagedFUEL LEAKING FROM LEFT WING OTBD FLAP INBD TRACK FAIRING. ONE DROP EVERY 90 SECONDS. FOUND FWD OUTBOARD BOLT ON LOWER ATTACH FITTING LEAKING. RESEALED AT 0600 ON 11-11-11.SDR UALA2011111106163Structure · wornREF DAMAGED BULKHEAD CONNECTOR, SMC7. IPC SHOWS A DOTTED CUTOUT OF STRUCTURE FOR ATTACHMENT OF CONNECTOR. ITEMS 135 AND 120 ARE USED TO SECURE CONNECTOR. THE STRUCTURE IS WORN AWAY. THERE IS NOTHING TO ATTACH TO. REMOVED 1 EA FWD HI-LOKS IN FUEL TANK. P
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