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 AALA20120305013Vapor Barrier · crackedLEFT VAPOR BARRIER CRACKED BETWEEN BAYS 2 AND 4 LEFT. INSTALLED REPAIR STRAPS, ANGLES AND JOINT ANGLES FOR BAYS 2 AND 4 LEFT PER SRM - WINGLET SUPPLEMENT 57-10-10-2R 2.SDR AALA20120305011Stiffener · crackedLEFT VERTICAL STIFFENER CRACKED AT LOWER END JUST OUTBOARD OF PACK EXHAUST CUTOUT, AFT SIDE OF BULKHEAD. INSTALLED VERTICAL STIFFENER PER AARD 51-00-05-1 AND BOEING DRAWING NUMBERS 111A1000 AND 111A1308.SDR IPXA2672229Stiffener · crackedINSPECTION TYPE: 9C, WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 LBL 10.94. REPAIRED IAW 57-10-10-2R2, REPAIR 2, FIG 201, REV 52, JUST AT STA 785.9, LBL 10.94, ORIG MATL: BAC1518-912-2024T3511, CRACK LENGTH: 3", CUTOFSDR IPXA2672228Stiffener · crackedINSPECTION TYPE:9C, WING CENTER TANK FRONT SPAR VERTICAL STIFFENER TOP AREA FOUND CRACK JUST AT STA 785.9 RBL 10.94. REPAIRED IAW SRM 57-10-10-2R2, REPAIR2, FIG 201, REV 52 JUST AT STA 785.9 RBL10.94, ORIG MATL: BAC1518-912-2024T3511, CRACK LENGTH: 2.5",CUTOFSDR AALA20120302003Stiffener · crackedRIGHT VERTICAL STIFFENER OUTBOARD OF RIGHT PACK EXHAUST CUTOUT CRACKED AT LOWER END. REPLACED STIFFENER PER AARD 51-10-05-1 AND BOEING DRAWING 111A1000 AND 111A1308.SDR EE4Y20120302083Fitting · corrodedLEFT WING REAR SPAR AFT FACE RETRACTION JACK ANCHORAGE FITTING CORRODED AROUND BORE AND LOWER SURFACE. DAMAGED PART GOING TO BE REPAIRED FOLLOWING REPAIR INSTRUCTIONS.SDR EE4Y20120302081Fitting · corrodedRIGHT WING REAR SPAR AFT FACE RETRACTION JACK ANCHORAGE FITTING CORRODED AROUND T BORE AND LOWER SURFACE. DAMAGED PART GOING TO BE REPAIRED FOLLOWING REPAIR INSTRUCTIONS.SDR HNAA2012030200640Fastener · corrodedFASTENER CORRODED ON LT WING TO FUSELAGE REAR SPAR LOWER FITTING. R & R REAR SPAR LOWER FITTING IAW AMM 20-14-01.SDR FOTR0301201225306Stiffener · crackedRIGHT WING FRONT SPAR VERTICAL STIFFENER CRACKED, WS 200.SDR CWQR20120229008Closeout Panel · crackedDURING A SCHEDULED MX CHECK, FOUND THE RT WHEEL WELL AFT SPAR CLOSE-OUT PANEL TO BE CRACKED AT 3 LOWER INBD RIVET LOCATIONS THAT ATTACH IT TO THE LOWER WING SKIN. UPON DISASSEMBLE IT WAS FOUND THAT 1 OF THE CRACKS WENT FROM RIVET TO RIVET. THE PANEL ALSO HOLDSSDR AALA20120229001Doubler · crackedAFT RIGHT AIR CONDITIONING BAY PACK EXHAUST DUCT CUTOUT DOUBLER IS CRACKED AT LOWER INBOARD ATTACH FLANGE. INSTALLED PACK EXHAUST DUCT CUTOUT DOUBLER AT AFT RIGHT AIR CONDITIONING BAY PER AARD 51-10-05-1, REPAIR 1.SDR SWAA2012030201849Attach Angle · crackedRT WING O/B UPPER T/E BEAM TO SPAR ATTACH ANGLE IS CRACKED AT RSS 240. REMOVED ANGLE IAW SRM AND DWG.SDR HNAA2012022700626Panel · corrodedCORROSION FOUND AT MANY PLACES ON LADDER PLATE OF STRESS PANEL 522AT. COMPLIED WITH HFEC INSPECTION ON REWORKED AREAS IAW RD8-57-114. NO CRACK INDICATION FOUND. REPAIRED IAW RD8-57-114.SDR UALA2012022801200Structure · leakingFUEL LEAKING FROM CENTER TANK SEAM JUST AFT OF THE RIGHT INBD TANK SUMP (PREVIOUSLY REPAIRED). CLEANED AND RESEALED AREA INSIDE TANK. SEALANT APPLIED 0200 OF FEB 26. OUTSIDE FITTING AND SEAM NEEDS TO BE RESEALED. RESEALED SEAM.SDR UALA2012022801199Structure · leakingFUEL LEAKING FROM LEFT LOWER WING ATTACH FITTING SEAM NEAR THE LEFT INBD CENTER TANK SUMP (SEALANT REMOVED). CLEANED AND RESEALED AREA INSIDE TANK. APPLIED SEALANT AT 0200 OF 26 FEB. OUTSIDE FITTING AND SEAM NEEDS TO BE RESEALED. RESEALED SEAM.SDR USAA2012032600005Plate · worn2S CHECK - ELONGATED HOLE ON RIGHT WING LOWER SURFACE MOUNTING PLATE BETWEEN WS376 TO WS 407 & BETWEEN RIB 7 & RIB 8. REPLACED RIGHT WING LOWER SURFACE MOUNTING PLATE IAW A319 SRM 51-72-11.SDR A6WA201240393Support Angle · crackedUPPER ANGLE SUPPORT FOR PICCOLO TUBE TRANSITION DUCT BETWEEN L/E 520JL AND 530JL IS CRACKED. REMOVED, FABRICATE4D AND INSTALLED IAW FORM 412, SRM 51-41-29, 51-41-02, 51-42-06, 51-42-15, 51-24-16, 51-21-11, 51-25-06.SDR A6WA201240395Support Angle · crackedUPPER SUPPORT ANGLE FOR PICCOLO TUBES TRANSITION 620JL AND 630JL IS CRACKED. REMOVED UPPER SUPPORT ANGLE, FABRICATED AND INSTALLED IAW FORM 412, SRM`S 51-41-21, 51-41-02, 51-42-15, 51-24-16, 51-21-11, 51-25-06.SDR A6WA201240277Fairing · chafedRT STUB FAIRING CHAFED. REPLACED RT STUB FAIRING WITH SERVICEABLE STUB FAIRING.SDR ABXA20120224209Splice Plate · crackedLEFT WING OUTBD UPPER L/E SPLICE PLATE CRACKED AT APPOX LWS 564. REPAIRED IAW REA B651-59661, AIRCRAFT WAS GROUNDED.SDR AALA20120223028Vapor Barrier · crackedCRACK IN VAPOR BARRIER AT WING CENTER SECTION AFT BULKHEAD. INSTALLED PERMANENT DOUBLER REPAIR PER AARD 57-10-10-2R 2.SDR R61A201202220153Bolt · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LT WING CANOE FAIRING NR 2 523BB ATTACHING LINK THAT ATTACHES TO AIRCRAFT, BOLT & PIN/BUSHING CORRODED & SEIZED. MAINTENANCE REMOVED AND REPLACED THE SEIZED LT WING CANOE FAIRING NR 2 5SDR R61A201202220152Bushing · corrodedWHILE AIRCRAFT WAS IN FOR HEAVY CHECK, LEVEL 2 CORROSION WAS FOUND ON THE LT WING CANOE FAIRING NR 2 523BB ATTACHING LINK THAT ATTACHES TO AIRCRAFT, BOLT & PIN/BUSHING CORRODED & SEIZED. MAINTENANCE REMOVED AND REPLACED THE SEIZED LT WING CANOE FAIRING NR 2 5SDR FDEA201202220637Access Panel · corrodedLEFT WING INBD T/E ACCESS PANEL 541JB ATTACHMENT SUPPORT TEE FOUND SURFACE CORROSION ON SEVERAL LOCATION. R & R IAW EA 1-5710-157949, REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 114.SDR AALA20120319002Angle · crackedAFT RIGHT AC BAY UPPER HORIZONTAL ANGLE CRACKED AT SECOND RIVET HOLE FROM INBOARD END NEXT TO KEEL BEAM. INSTALLED REPAIR FILLER AND REPAIR ANGLE AT AFT RIGHT AC BAY UPPER HORIZONTAL ANGLE EA B737-57-022012.SDR AALA20120309002Stiffener · crackedAFT RIGHT A/C BAY MIDDLE HORIZONTAL STIFFENER IS CRACKED AT INBOARD END NEXT TO KEEL BEAM STATION 663 FORWARD SIDE. REMOVED CRACKED STIFFENER AND INSTALLED NEW HORIZONTAL STIFFENER AT AFT RIGHT A/C BAY PER AARD 51-10-05-1, REPAIR 1 AND BOEING DRAWING NUMBERS SDR SWIA201229727Angle · crackedRIGHT WING UPPER MID LEADING EDGE ANGLE CRACKED. REPLACED RIGHT WING UPPER MID LEADING EDGE ANGLE.SDR SWIA201229726Angle · crackedLEFT WING UPPER MID LEADING EDGE ANGLE CRACKED. REPLACED ANGLE AT LEFT WING UPPER MID AREA.SDR AALA20120216TUL02Angle · crackedRIGHT A/C BAY AFT UPPER ANGLE IS CRACKED AT INBOARD END AT SECOND FASTENER HOLE. INSTALLED SPLICE FILLER ANGLE AND REPAIR ANGLE PER EA B737-57-021884, SRM 51-70-11-2R AND BOEING DRAWING 111A1000.SDR AALA20120216TUL01Vapor Barrier · crackedWING CENTER SECTION REAR SPAR VAPOR BARRIER LOCATED IN RIGHT WHEEL WELL BETWEEN RIGHT BUTTLINES 6.15 AND 15.54 CRACKED. INSTALLED REPAIR ANGLES, SHIMS AND STRAPS AT BAY 1R, 2R AND 4R PER SRM 57-10-10-2R, REPAIR 2 AND EA B737-57-021884.SDR UALA2012021600948Panel · crackedLEFT TRAILING EDGE PANEL BEHIND WING BODY IS CRACKED, MOST FURTHEST PANEL P/N 65B11640-55. SUSPECT FLAP HITTING PANEL LEFT WING. REPAIRED PANEL REF SRM.SDR SWAA2012030902021Support Angle · crackedLT WING CRACKED ON SUPPORT ANGLE AT WS 537.806. REMOVED AND REPLACED ANGLE IAW SRM AND DWG.SDR HNAA201202200059Support · crackedLEFT WING AILERON TERMINAL QUADRANT SUPPORT BOX CRACKED. LT AILERON TERMINAL QUADRANT SUPPORT BOX REPLACED WITH MADE REPAIR PART FABRICATION COVERED BY WO9120.SDR DALA1208540923Fitting · crackedLT WING FIXED L/E RIB ANGLE CLIP IS CRACKED AT STA XOS 352. HFEC INSPECTION PER NDTSPM 06-10-01-001 VERIFIED CRACK EXIST AT DISCREPANT AREA. REPAIR TO BE PERFORMED ON NRC 191904.SDR UALA2012021400885Structure · leakingLEFT WING FUEL LEAK, FLIGHT DIVERTED. FUEL LEAKING FROM LT & RT WING BET LDG GR AND PYLON, DENTNK ENTRY CREW FOUND LT WING LEAKING, REPAIR IN PROGRESS WILL SEAL LT IN MORNING AND START RT LEAK. BOTH WING LEAKS ARE SEALED AND CURING.SDR AALA20120211TUL01Stiffener · crackedRIGHT HORIZONTAL STIFFENER CRACKED AT INBOARD END ABOVE PACK EXHAUST DUCT ON FORWARD SIDE OF BULKHEAD. REPLACED STIFFENER PER AARD 51-10-05-REPAIR 1 AND BOEING DWG 111A1301.SDR UALA2012021000804Screw · missingFOUR SCREWS MISSING IN SUCCESSION UNDER RT M WING INBOARD OF OUTBOARD FLAP RPL SCREWS AND MANY SURROUNDING SAME AREA WRONG LENGTH.SDR EE4Y201202060016Fitting · corrodedLEFT WING, INNER REAR SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING'S WITH CORROSION. THE FITTING'S REWORK REQUIRES A MAJOR REPAIR.SDR UALA2012020600692Seal · out of positionAIR LEAK NOISE ON RT SIDE OF A-C BY EXIT ROW BACK. PAX COMPLAINING. LOUD PRESSURE LEAK COMING FROM FWD RT OVER WING EMERG EXIT WINDOW DURING DESCENT. DEBRIEFED INBD CREW. SOUND LOUDEST IN SEAT NEAREST FWD OVERWING EXIT. CHKD FWD OVERWING EXIT, NO OBVIOUS SDR EE4Y201202030017Fitting · corrodedLT WING, INNER REAR SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING BORE AND SPOTFACE WITH CORROSION. THE FITTING REWORK REQUIRES A MAJOR REPAIR IAW GUIDELINES.SDR SWAA2012022001564Stiffener · crackedRT MAIN LANDING GEAR WHEEL WELL STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM AND DWG.SDR IPXA2M71689Angle · corrodedINSPECTION TYPE:4C, LT WING T/E T-CAP CORRODED AT FASTENER HOLE JUST FWD OF INBD AILERON ACCESS PANEL 541JB. GAINED ACCESS, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR IAW SRM 57-00-00, FIG 207, SHEET 7, RESTORED AREA.SDR AALA20120202TUL03Doubler · crackedRIGHT PACK EXHAUST CUTOUT DOUBLER IS CRACKED AT INBOARD MOUNT TABS. INSTALLED NEW RIGHT PACK EXHAUST CUTOUT DOUBLER PER AARD 51-00-05-1 REPAIR 1 AND BOEING DRAWING 11A1512.SDR AALA20120202TUL01Web · crackedLEFT AC BAY, STATION 663 BULKHEAD INBOARD OF PACK EXHAUST HAS TEMPERARY REPAIR. FABRICATED AND INSTALLED ALL REPAIR STRAPS, ANGLES AND JOINT ANGLES FOR BAYS 2L AND 4L. SEALED ALL FASTENERS AND APPLIED VAPOR BARRIER PER SRM -WINGLET APB SUPPLEMENT 57-10-10-2RSDR AALA20120208AFW08Fitting · crackedLEFT WING AFT PITCH LOAD FITTING OUTBOARD TENSION BOLT HOLE CRACKED. INSTALLED AFT PITCH LOAD FITTING PER EA B767-57-021103.SDR AALA20120208AFW07Fitting · crackedRIGHT WING AFT PITCH LOAD FITTING OUTBOARD TENSION BOLT HOLE CRACKED. INSTALLED AFT PITCH LOAD FITTING PER EA B767-57-021245.SDR QXEA2012020600151Shroud · damagedLEFT WING UPPER T/E SHROUD HAS 8 WORKING RIVETS AT OTBD SPOILER HINGE CUT-OUT. REMOVED REPLACED 8 RIVETS ON SHROUD IAW SRM 51-42-05-02-01.SDR AALA20120131TUL01Stiffener · crackedVERTICAL STIFFENER CRACKED AT STATION 663 AFT SIDE OF BULKHEAD OUTBOARD OF LEFT PACK EXHAUST CUTOUT. INSTALLED NEW STIFFENER PER AARD 51-10-05-1 AND DRAWING 149A7210 AND 111A1000.SDR NOCA201201290012Web · crackedLEFT WING LEADING EDGE, NOSE WEB CRACKED AT LOWER FLANGE INSIDE REFUEL PANEL INBOARD END. REMOVED FUELING DOOR FOR ACCESS REMOVED DOUBLER AND CLIP STOP DRILLED CRACKS AS PER SRM 57-41-13. VERIFIED CRACK CONTAINED PER NDT MANUAL 51-00-19 FABRICATED DOUBLER STSDR IPXA12M71544Stiffener · crackedINSPECTION TYPE:3C, STIFFENER CRACKED IN RT WING L/E INTERIOR AT XORS 562 (XOS667). REPAIRED STIFFENER IN RT WING L/E INTERIOR AT STA XOS667 IAW SRM57-40-03, REPAIR 2, FIG 202.
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