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 C2XA98IA204Support · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT WING NUMBER TWO UPPER SKIN SUPPORT AT RIB 21 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE EFFECTED SKIN SUPPORT IAW EMB-120 SRM 51-40-02 AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR ABXA9800523Angle · crackedDURING C-CHECK, FOUND FRAME STATION 718 SUPPORT ANGLE CRACKED ON LONGERON 20. REPLACED ANGLE IAW DC9 SRM 51-30-1 AND DACO DWG 9958209.SDR SWAA981148Angle · crackedDURING SCHEDULED 1/4 D-CHECK, FOUND CRACKED I/B FLAP WELL LWR SURFACE SUPPORT ANGLE AND WORN JUST ABOVE CANOE. REPAIRED PER BOEING SRM.SDR 99ZZZM537Stiffener · crackedRIGHT WING TE SHROUD LOWER SKIN STIFFENER CRACKED INBOARD OF RIB 10. REMOVED AND REPLACED LOWER SKIN STIFFENER PER SRM. (M)SDR CALA9801060Bracket · crackedINSPECTION FOUND TWO CRACKS IN RT WING FLAP LEADING EDGE SUPPORT BRACKET AT XRS 332 TO 232. THE SUPPORT BRACKET WAS REMOVED, A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-20-0, 51-10-2, 51-10-1, AND 51-10-3.SDR UPS98826926Doubler · crackedINSPECTION TYPE-C, LT WING INBD SLOT, OTBD CLOSE OUT RIB DOUBLER IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER PER DWG 5769859 AND SRM 57-3-1 FIG 6.SDR 99ZZZM543Stiffener · crackedLT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB NR 10. REPLACED LEFT TE WING SHROUD TOP SKIN STIFFENER INBOARD OF NR 10 RIB AT THIS TIME. (M)SDR 99ZZZM542Stiffener · crackedLT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END, OUTBOARD OF RIB NR 8. REPLACED LEFT WING TE SHROUD TOP SKIN STIFFENER OUTBOARD OF RIB NR 8.SDR 99ZZZM540Stiffener · crackedLEFT WING TE SHROUD LOWER SKIN STIFFENERS, TWO HAVE TAG ANGLE CRACKED AT AFT END, BETWEEN RIBS 8/9. REPLACED TWO ANGLES ON TE SHROUD LOWER SKIN STIFFENERS BETWEEN RIBS 8/9 AT THIS TIME.SDR 99ZZZM538Stiffener · crackedLEFT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB NR 6. REPLACED TOP SKIN STIFFENER BETWEEN RIBS 5 AND 6 JUST INBOARD OF RIB 6 AT THIS TIME. (M)SDR 99ZZZM433Angle · crackedRIGHT WING TE TOP SKIN STIFFENER AFT TAG ANGLE CRACKED AT LOWER FLANGE BETWEEN RIBS 5 AND 6 OF SHROUD. REMOVED AND REPLACED AFT TAG ANGLE BETWEEN RIBS 5/6 FOR THE TOP SKIN STIFFENER. (M)SDR 98ZZZX2353Doubler · crackedRIGHT FORWARD WING WALK HAS BROKEN/CORRODED DOUBLER PLATE. THIS SECTION CRACKED FULL LENGTH ON BOTH INNER AND OUTER OF DOUBLER PLATE. SUBMITTER STATED THIS WAS THE SECOND ARROW THAT WAS FOUND IN THIS CONDITION.SDR CALA9801029Angle · crackedINSPECTION FOUND A 1 CRACK ON METAL STRIP AND A 1 CRACK ON SUPPORT ANGLE IN LT WING LEADING EDGE CAVITY AT XORS 562. REPAIRS WERE INSTALLED IAW SRM 57-00-01, 51-31-01, 57-31-01, FIGURE 1, AND 51-21-01.SDR CALA9801024Angle · corrodedINSPECTION FOUND SUPPORT ANGLES CORRODED IN CAVITY OF TRAILING EDGE FIXED FAIRING BETWEEN INBOARD AILERON AND OUTBOARD TRAILING EDGE FLAP, LT WING. THE ANGLES WERE REMOVED. NEW PARTS WERE FABRICATED AND INSTALLED IAW SRM 51-20-00 AND 51-31-01.SDR CA980707059Bracket · cracked(CAN) THE RIGHT HAND FORWARD REAR SPAR CARRY THROUGH BRACKET FOUND CRACKED 1.50 INCHES AND LEFT BRACKET CRACKED .50 INCH. RIGHT HAND BRACKET REPLACED, AND LEFT BRACKET REINFORCED.SDR 99ZZZM541Stiffener · crackedLT WING TE SHROUD TOP SKIN STIFFENER CRACK AT FORWARD END (BETWEEN RIBS 7/8). REPLACED LEFT WING TE SHROUD TOP SKIN STIFFENER BETWEEN RIB 7/8 AT THIS TIME.SDR 98ZZZX2438Nut · crackedDURING AN ANNUAL INSPECTION TWO OF THE MS21042L5 NUTS WERE FOUND CRACKED ALL THE WAY THROUGH TO THE BOLT ON THE RIGHT WING STRUT UPPER ATTACH FITTING. SUBMITTER STATED THE CAUSE IS UNKNOWN.SDR MWEA98654Doubler · crackedLEFT WING INTERNAL BEADED DOUBLER CRACKED AT STATION XO 198. MAINTENANCE ROUTED OUT CRACK AND INSTALLED REPAIR USING APPROVED DATA.SDR DL72W981233Stiffener · crackedOUTBOARD L/E SPAR STIFFENER CRACKED NR 6 SLAT I/B TRACK O/B SIDE. REPLACED SPAR STIFFENER PER M/M 57-20-21.SDR CALA9801008Support · crackedINSPECTION FOUND LT WING STA 280 FLAP LEADING EDGE SUPPORT CAP CRACKED AND CORRODED. THE SUPPORT CAP WAS REMOVED, A NEW SUPPORT CAP WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-4, AND 51-30-2.SDR IXXA9800092Doubler · corrodedDURING ROUTINE C CHECK INSPECTION, CORROSION WAS DETECTED ON CENTER WING UPPER JOINT DOUBLER AT FUSELAGE STATION 816, STRINGER 6. REPAIR ACCOMPLISHED BLENDED OUT CORROSION IN ACCORDANCE WITH FAA DER APPROVED DRAWINGS, COO-SJO-98-0393DDAC, COO-SJO-98-0394DAC, SDR CALA9800997Doubler · crackedINSPECTION FOUND A .5 INCH CRACK IN RT WING LEADING EDGE FRAME UPPER DOUBLER AT STA 438. THE ANGLE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-10-2 AND 51-10-3.SDR 99ZZZM435Stiffener · crackedRIGHT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8 OF SHROUD. REMOVED AND REPLACED STIFFENER PER SRM. (M)SDR 99ZZZM434Stiffener · crackedRIGHT WING TOP SKIN TE STIFFENER CRACKED AT FORWARD END, INBOARD OF RIB 9, SHROUD AREA. REMOVED AND REPLACED STIFFENER PER SRM. (M)SDR ABXA9800498Angle · crackedRIGHT WING INBOARD SLOT BOX, OUTBOARD AFT VERTICAL ANGLE IS CRACKED AT THE BOTTOM. REPAIRED IAW DC8 SRM 51-1-20D.SDR UPS98826952Intercostal · crackedINSPECTION TYPE:D, RT WING L/E I/B OF THE STA XFS201.25 RIB, THE INTERCOSTAL IS CRACK EDAT THE I/B END. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5769859 AND SRM 51-1-21.SDR UPS98826995Doubler · crackedINSPECTION TYPE-D, LT WING L/E LWR SKIN INTERNAL DOUBLER AT STA XOLDI 7 IS CRACKED. REMOVED DOUBLER, FABRICATED AND INSTALLED PER DWG 5769891 AND SRM 51-1-20D, 51-1-21.SDR UPS98826959Angle · crackedINSPECTION TYPE:D, LT WING I/B SLOT BOX, O/B AFT VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 69753293 AND SRM 51-1-20D.SDR CALA9800962Angle · crackedINSPECTION FOUND A 1 CRACK IN ANGLE OF LT WING FORWARD SIDE AT WING ROOT, WHERE FORWARD SPAR GOES INTO FUSELAGE. THE SEAL BRACKET AND ANGLE AT WING ROOT WERE REMOVED IAW SRM 51-30-3. AN ANGLE WAS FABRICATED IAW SRM 51-10-4. THE ANGLE AND SEAL BRACKET WERE ISDR UPS98826989Clip · crackedINSPECTION TYPE-D, RT WING L/E ABOVE THE NR 3 PYLON, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED AND INSTALLED CLIP PER DWG 9753294 AND SRM 51-1-21.SDR UPS98826988Angle · crackedINSPECTION TYPE-D, RT INBD SLOT BOX, O/B AFT VERTICAL ANGLE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED VERTICAL ANGLE PER DWG 9753293 AND SRM 51-1-21, 51-3-0.SDR UPS98826956Doubler · crackedINSPECTION TYPE:D, RT WING L/E LWR INTERNAL DOUBLER AT STA XOLDI7.00 IS CRACKED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769891 AND SRM 51-1-20D.SDR QXEA9800849Angle · crackedUPPER ATTACH ANGLE FOR LEFTHAND MAIN LANDING GEAR BACK-UP STRUCTURE CRACKED AT LOWER BOLT HOLE. REPAIRED IAW FOKKER SRM 57-02-09, PAGE 2, PARAGRAPH 3, FIGURE 5.SDR CALA9800942Bracket · crackedINSPECTION FOUND A .5 INCH CRACK IN BRACKET OF RT WING LEADING EDGE PANEL FRAME. THE BRACKET WAS REMOVED, A NEW ANGLE BRACKET WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-10-4, AND 51-30-5.SDR SWAA981048Angle · wornDURING SCHEDULED 1/4 D-CHECK, FOUND T-ANGLE WORN I/B UPPER FLAP WELL PANEL. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA981007Angle · crackedDURING SCHEDULED D-CHECK, FOUND CRACKED L-ANGLE ON TOP WING PANEL I/B OF NR 5 GROUND. REMOVED AND REPLACED PER BOEING SRM.SDR CA980707001Bracket · broken(CAN) AT FLAP SECONDARY DRIVE SHAFT LUBE AND INSPECTION, THE INBOARD RIGHT WING FLAP SHROUD SUPPORT STRUT BRACKET WAS FOUND BROKEN. PART TC: 23,946.SDR UPS98827061Fitting · crackedINSPECTION TYPE:C+S2 IN NR 3 MAIN TANK JUST OUTBD OF XRS74 LOWER STRINGER NR 51 IS CRACKED IN TWO SEPARATE PLACES ON THE FWD SIDE AND BETWEEN 3 FASTENERS ON THE AFT SIDE. REMOVED CRACKED END FITTING. DRILLED NEW FITTINGS IAW 51-3-2. INSTALLED FITTINGS IAW DSDR UPS98827060Fitting · crackedINSPECTION TYPE:C+S2 IN NR 3 MAIN TANK ON INBD SIDE AT APPROX STA XRS 66 TO APPROX XRS 61 LOWER STRINGER NR 51 IS CRACKED ON THE AFT SIDE. REMOVED END FITTING IAW DAC DWG 3704841 PART NR 3704841-501. DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED AND PRIMSDR CALA9800907Doubler · crackedINSPECTION FOUND A 1.5 CRACK IN RT WING LEADING EDGE FRAME UPPER DOUBLER AT WS 444.5. THE DOUBLER WAS REMOVED. A REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-2.SDR F3LA98071Doubler · crackedPAE - DURING C-CHECK, INSPECTION REPORTED LEFT WING FIXED LEADING EDGE SKIN DOUBLER CRACKED AT NR 3 SLAT OUTBOARD AUXILLIARY TRACK CUTOUT. MAINTENANCE REMOVED DAMAGED DOUBLER AND REPAIRED PER ER 98-0483 AND SRM 51-30-2. (M)SDR QXEA9800810Fitting · chafedNR 2 ENGINE INBOARD FRONT SPAR SUPPORT FITTING HAS CHAFING DAMAGE. REPAIRED IAW CONAIR EO 1998 AND HORIZON AIR EA 9-57-365.SDR UPS98827045Angle · corrosionINSPECTION TYPE:C+S2 CORROSION ON RIGHT WING TRAILING EDGE PANEL SUPPORT ANGLE AT XRS 558 .00. ORDER NEW ANGLE RECEIVED NEW ANGLE DRILLED HOLES AND INSTALLED ANGLE IAW DC8 SRM 51-1-21.SDR ABXA9800656Fitting · crackedATTACH FITTING AT CANTED STATION XRS 495 TO STRINGER 63 (UPPER SKIN) HAS CRACK AT LAST FASTENER HOLE. FABRICATED REPLACEMENT ATTACH FITTING IAW DWG 3648143 AND ABX REA 857-22859.SDR 99ZZZM457Stiffener · crackedRIGHT WING TE LOWER SHROUD SKIN STIFFENER CRACKED BETWEEN RIB 7/8. REPLACED STIFFENER IN RIGHT WING TE LOWER SHROUD SKIN BETWEEN RIBS 7/8. (M)SDR 99ZZZM464Stiffener · crackedRIGHT WING TE SHROUD TOP SKIN STIFFENER CRACKED AT FORWARD END BETWEEN RIBS 7/8. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 7/8. (M)SDR 99ZZZM459Stiffener · crackedLEFT WING TE SHROUD TO PSKIN STIFFENERS ARE CRACKED AT FORWARD END IN AREA BETWEEN RIBS 8/9. REPAIRED LEFT WING TE SHROUD TO SKIN STIFFENER BETWEEN RIBS 8/9. (M)SDR 99ZZZM458Stiffener · crackedLEFT WING TE TOP SKIN STIFFENER IS CRACKED AT FORWARD END IN AREA BETWEEN RIBS 7/8. REPAIRED LEFT WING TE TOP SKIN STIFFENER BETWEEN RIBS 7/8 IAW BAE FAX NR JM/RJO417-98. REF W/C 5022 FOR REINSPECTION. (M)SDR 99ZZZM454Stiffener · crackedLEFT WING TRAILING EDGE SHROUD TOP SKIN STIFFENER IN AREA BETWEEN RIBS 9/10 IS CRACKED AT FORWARD END. REPAIRED LEFT WITH TE SHROUD TOP SKIN STIFFENER BETWEEN RIBS 9/10 IAW BAE FAX NR JM/RJO417-98, REF REINSPECTION W/C 5020. (M)SDR 99ZZZM436Stiffener · crackedRIGHT WING TE TOP SHROUD SKIN STIFFENER CRACKED AT FORWARD END INBOARD OF RIB 9. REPAIRED RIGHT WING TE TOP SHROUD SKIN STIFFENER BETWEEN RIBS 8/9 IAW BAE FAX NR JM/RJ0417-98. (M)
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