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 DHL2001801513Angle · crackedCENTER WING BEAM LOWER SUPPORT ANGLE CRACKED 1 INCH AT STA 683 XCW 23 RT. REMOVED CRACKED SUPPORT ANGLE PER SRM 51-1-20 D. FABRICATED NEW ANGLE PER SRM 53-20-0. INSTALLED NEW ANGLE PER SRM 51-1-20D PG 21.SDR UPS01837089Fitting · crackedINSPECTION TYPE:SV RIGHT WING NR 3 MAIN TANK STRINGER 51 END FITTING ON I/B SIDE IS CRACKED. REMOVED STRINGER 51 END FITTING ON I/B SIDE IAW DC8 SRM 51-3-2. LOCATED DRILLED AND INSTALLED NEW END FITTING IAW DAC DWG 5613423.SDR UPS01837088Fitting · crackedINSPECTION TYPE:SV RIGHT WING NR 3 ALT TANK STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DWG 56SDR UPS01837062Fitting · crackedINSPECTION TYPE:SV LT WING NR 2 MAIN STRINGER 51 FWD I/B SIDE HAS A CRACKED STRINGER END FITTING. PERFORMED HFEC TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-001. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.SDR UPS01837061Fitting · crackedINSPECTION TYPE:SV LT WING NR 2 ALT STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED AND RPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.SDR UPS01837060Fitting · crackedINSPECTION TYPE:SV LT WING NR 2 MAIN STRINGER 51 AFT I/B STRINGER END FITTING IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 06-10-01-0 01. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0.SDR UPS01837059Fitting · crackedINSPECTION TYPE:SV LT WING NR 2 ALT STRINGER 51 END FITTING ON O/B SIDE IS CRACKED. PERFORMED HFEC INSPECTION TO VERIFY CRACK IAW DAC NDT SPM 060101. REMOVED CRACKED FITTING. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24 AND DAC DWG 5613423. INSTALLESDR SWIA200110349Bolt · corrodedRIGHT WING TRAILING EDGE NEAR AILERON POSITIONING TRANSMITTER HAS 3 CORRODED BOLTS. NEW HARDWARE INSTALLED IAW CRJ MM 27-15-01.SDR DHL2001801522Channel · crackedNR 4 MAIN TANK CHANNEL ASSY CRACKED (REF 505D ACCESS DOOR). REMOVED AND REPLACED CHANNEL ASSY PER S/B 57-65 PG 1-5. LEAK CHECK COMPLIED WITH.SDR ASOA01183Bracket · crackedDURING SCHEDULED MAINTENANCE IN TXK, THE LEFT WING RIB NR 6 LOWER MID SKIN SUPPORT BRACKET WS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE LEFT WING RIB NR 6 LOWER MID SKIN SUPPORT BRACKET. MAINTENANCE REINSTALLED THE LEFT WING DEFUEL PANEL IAW SDR ASOA01176Bracket · crackedDURING SCHEDULED MAINTENANCE IN TXK, RIB 8 WAS FOUND WITH CRAKES SKIN SUPPORT BRACKET AFT OF THE NR 1 FUEL PANEL ON THE LEFT WING. MAINTENANCE REMOVED AND REPLACED THE SKIN SUPPORT BRACKET AT RIB 8 ON THE AFT SIDE OF THE NR 1 FUEL PANEL ON THE LEFT WING. MAISDR UPS01836867Attach Fitting · crackedINSPECTION TYPE:C2 STGR 64 TO FRONT SPAR ATTACH FTG CRACKED ON I/B SIDE OF NR 4 PYLON NR 4 ALT. REMOVED AND REPLACED W/NEWLY MANUFACTURED PART IAW DC8 SRM 51-1-20D.SDR UPS01836950Splice · crackedINSPECTION TYPE: C2, REMOVE INTERCOSTAL AT LEFT WING STA 340 TO ACCESS FWD DRIVE LINK BOLT. REMOVED INTERCOSTAL & WEB IAW DC8 SRM 51-1-21. MAT ID FOR ANGLE DOUBLER DMS 1592 TITANIUM .040 PO 300420 IAW REO G08396 & SHIMS 7075-T6 .040 PO 362742 & 7075-T6 .06SDR AUS20010993Tape · separated(AUS) LH WING ROOT SEALING TAPE SEPARATED. CARBON MONOXIDE FUMESENTERED COCKPIT.SDR QXEA0101485Clip · corrodedPDX- CORROSION FOUND ON CLIPS AT LOWER END OF NR 2, NR 3 NR 4 RIBS ON INBOARD WALL OF LEFT SIDE OF COLLECTOR FUEL TANK. REMOVED CORROSION AND REPLACED HI LOCKS AND TREATED AREA IAW F28 SRM 51-01-01 AND SRM 51-10-04.SDR QXEA0101494Bracket · crackedPDX - LEFT WING ISOLATION VALVE LOWER ATTACH BRACKET HAS A CRACK. REPLACED IAW DASH-8 200 SRM 51-40-11.SDR C2XA01BT164Fitting · damagedYUL- DURING 4C INSPECTION YUL MAINTENANCE, AS PER COEX 5710-01025, INSPECTED AND REWORKED THE RT REAR WING SPAR FITTINGS BETWEEN WING RIBS 7/8 AND RIB 12. AIRCRAFT RETURNED TO SERVICE.SDR DHL2001727509Retainer · crackedREAR SPAR PRESSURE SEAL RETAINER CRACKED AT STA 849L WL 208. REMOVED AND INSTALLED NEW SEAL RETAINER PER SRM 51-30-2.SDR 0104099868Rib · crackedDuring Mck in ATL, a 3" crack was found on the leading edge rib at station xrs 129. Material 7075-t6, repaired per EA 98-185067 and SRM 57-02.SDR 01FDEA00762Splice · crackedFWD RT WING ROOT, SPLICE FITTING AT FUSELAGE TO WING FRONT SPAR LWR CHORD IS CRACKED BETWEEN TWO FASTENER HOLES. NDT VERIFIED STA 1156 XCW 118. REMOVED AND REPLACED DOUBLER PER EA 58-5710-59060.SDR AUS20010960Bracket · corroded(AUS) LH WING LEADING EDGE TOP FORWARD ATTACHMENT BRACKET CORRODED.SDR DHL2001727534Retainer · damagedNR 1 SPOILER DOWN STOP O/B BRACKET AT WING T/E HAS ATTACHED RETAINER WITH NICK AND DENTS. REPLACED RETAINER ON NR 1 SPOILER DOWN STOP O/B BRACKET AT WING LT TRAILING EDGE.SDR DHL2001727535Gusset · crackedLEFT WING I/B END, COVE PNL TO NR 7 SPOILER ACTUATOR CASTING, I/B GUSSET CRACKED AT LOWER BOLT HOLE. REMOVED AND REPLACED I/B GUSSETS AT NR 7 SPOILER PER SRM 51-30-2.SDR 2002FA0000232Flange · looseFOUND LOOSE NAILS LESS THAN .1250 OUT ON SECOND RIB OUTBOARD OF STRUT AFT SPAR. FIRST AND SECOND RIB INBOARD OF STRUT AND FIRST RIB OUTBOARD OF STRUT AND FRONT SPAR ALL ON RIGHT WING. LEFT WING, FOUND LOOSE NAILS MORE THAN .1250 OR MISSING ON 1ST AND 2ND RIBSDR DHL2001727533Angle · crackedAPU EXHAUST TOP COVE PANEL AT T/E FOR APU EXHAUST LOUVERS, FWD O/B SUPPORT ANGLE IS CRACKED JUST AFT OF SPAR. REMOVED AND REPLACED THE APU EXHAUST TOP COVE PANEL AT T/E FWD O/B SUPPORT ANGLE PER SRM 51-30-2 AND 57-10-2. HEAT TREATED AND AGED PART PER GPS988MSSDR SWAA012250Structure · crackedDURING SCHEDULED SERVICE CHECK, FOUND LT WING L/E CRACKED NEAR NR 1 KRUEGER FLAP, CRACK IS .4375. REPAIRED L/E PER SWA RA.SDR 2001FA0000187Angle · crackedDURING A SCHEDULED INSPECTION, THE LEFT CANTED RIB CAP P/N 5722206-1 WAS FOUND CRACKED APPROXIMATELY 1 INCH AFT OF THE FORWARD WING SPAR. WHILE REPAIRING THIS CRACK THE UPPER WING TO FUSELAGE CLOSEOUT ANGLE P/N 5720001-3 WAS FOUND CRACKED. THESE CLOSEOUT ANGSDR UPS01836702Angle · crackedINSPECTION TYPE:C2,3 LEFT WING L/E VERTICAL ATTACH ANGLE IS CRACKED AT XS 250. REMOVED,FABRICATED,AND REPLACED ANGLE IAW DWG 9753293,AND SRM 51-3-0,51-1-20D.SDR QXEA0101307Flange · corrodedPDX-CORROSION AROUND FASTENER HOLES ON FLANGE FOR PANEL 624BT FORWARD INBOARD CORNER. REPAIRED IAW DHC-8 SRM 51-00-06, RD8-57-529, AND RD8-57-633.SDR UPS01836627Fitting · crackedINSPECTION TYPE:C1,3 LEFT WING T/E SUPPORT FITTING IS CRACKED OUTBOARD SIDE OF FLAP HINGE 410 CANOE FITTING. REMOVED AND REPLACED FITTING IAW DWG 4649597, AND SRM 51-1-20D, 51-3-0.SDR AALA20011578Angle · corrodedTUL - FOUND LEADING EDGE WING SKIN BULGED AT UPPER SPAR ATTACH SCREWS 8 INCH - 9 INCH OUTBOARD OF FUSELAGE. REMOVED CORROSION TREATED AND PRIMED AREA AND INSTALLED A STRAP AND ANGLES WITH DOUBLER REPAIR PER ESO 11697 DATED 7/27/2001. (M)SDR DHL2001745006Bracket · crackedCOVE PANEL BRACKETS BELOW OUTBD END OF NR 13 SPOILER CRACKED LT WING LEADING EDGE VENT PANEL OUTER SKIN MISSING COVE PANEL BRACKETS BELOW OUTBD END NR 12 SPOILER BROKEN OUT. REMOVED & REPLACED 1 EA T/E COVE PNL SUPPORT CHANNEL PER B727 SRM 51-10-1 & 51-30-2. SDR DL72S011232Stiffener · crackedFOUND ON F-1 CK 1 INCH CRACK L/E WING VERTICAL SPAR STIFFENER O/B SIDE OF NUMBER 6 SLAT O/B TRACK.SDR 01FDEA00578Fitting · crackedDURING ROUTINE INSP FOUND SUPPORT FITTING FOR NR 6 LEADING EDGE SLAT UP STOP CRACKED. *S/D* REMOVED AND REPLACED FITTINGS PER IAW SRM 51-20-1.SDR 0104969922Spar · corrodedDuring Mck in ATL, corrosion was found in the left and right beaver tails. The beaver tails were removed to accomplish corrosion removal. After the beaver tail removal, it was noted that 11 fastener holes common to the pylon front spar were elongated on each sSDR RRXA11399Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H O/B L/E UPPER RIB STA XFS 710 CRACKED. *** CORRECTIVE ACTION *** INSTALLED DOUBLER PER SRM 57-2-0SDR RRXA11382Doubler · crackedDURING A MAINTENANCE VISIT FOUND R/H WING UPPER CUTOUTS FOR #1 SPOILER MID HINGES ARE DISTORTED/BENT UPWARD. ***CORRECTIVE ACTION *** FABRICATED DOUBLERS INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2ASDR RRXA010057Fairing · damagedUPON WALKAROUND, DISCOVERED DAMAGE TO WING FILLET FAIRING. PERFORMED TEMPORARY REPAIR PER BOECOM EAF-IND-01- 00059H. INSTALLED EXTERNAL DOUBLER AND COVERED WITH SPEED TAPE. TAPE TO BE INSPECTED EACH FLIGHT.SDR UPS01436251Tee Chord · bulgedINSPECTION TYPE:C LHW - UPPER SURFACE L/E FIXED PANEL BUTT JOINT AREA FOUND BULGE AT ILES 997 AFT OF NR 7 V.C. FLAP AS MARKED. L/E FIXED PANEL SUPPORT T-CHORD REPLACED AND RIB REINSTALLED AS PER SRM 51-30-02, 51-10-01 L/E PNEUMATIC DUCT TRUSS ROD AND TORQUE SSDR 01FDEA00499Bracket · crackedN 500 DUR ROUTINE INSP IB BRACKET ON THE #8 FLAP TRACK FOUND CRACKED. R&R & FAB BRACKET PER IAW BAC 727 SRM 51-20-1, 51-30-2.SDR CA010627053Bolt · failed(CAN) UPON MPI IT WAS FOUND THAT 2 OF 4 WING BOLTS FAILED INSPECTION. IT WAS THANDETERMINED TO CHANGE ALL THE BOLTS. LOG ENTRY INDICATES BOLTS WERE LAST CHANGED IN 1992. THER IS NO RECORD OF BOLT INSPECTION SINCE THAT TIME ALTHOUGH INSPECTION IS CALLED FOR AFTSDR DL767011056Fitting · crackedWHILE ACCOMPLISHING THE STRUT IMPROVEMENT PROGRAM MODIFICATION ON THE LT WING SUPPORT STRUCTURE, A CRACK INDICATION WAS FOUND IN THE O/B ROW 2ND HOLE FROM BOTTOM COMMON TO THE RIB NR 8 ENGINE SUPPORT FITTING, THE FRONT SPAR, AND THE FRONT SPAR WEB. ER/A 39765SDR ERKR200100134Beam · crackedCRACKED UPPER T-CHORD OF RT WING T/E BEAM AT WING 235.20. THE CRACK WAS FOUND IN THE UPPER T-WING TRAILING EDGE BEAM AT WBL 235.20. THE REPAIR WAS ACCOMPLISHED BY REMOVING AND REPLACING THE DAMAGED AREA OF THE CHORD WITH NEWLY FABRICATED CHORD, REPAIR STRAPSSDR ERKR200100132Fitting · crackedDURING A-CHECK INSPECTION FOUND THE LEFT HAND SWING LINK FITTING CRACKED. REMOVED AND REPLACED LEFT HAND SWING LINK FITTING PER BOEING 737 MM 57-20-01 AND BOEING DWR 65-46400 REV G SH:0001.SDR DHL2001803534Angle · crackedAT C CK, RT WING - WING TO FUSELAGE FILLET SUPPORT ANGLE CRACKED (2 INCHES) AT XW 908-XCW 69.5.SDR RRXA11279Panel · gougedDURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO L/H FLAP AT STA.410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0.SDR 0105079971Doubler · crackedDuring Hck in ATL, A crack was found on the upper fuel tank access panel doubler. Repaired per EA 99-181239.SDR QXEA0100947Guide · damagedYYC - LEFT-HAND STUBWING REAR GUIDE BLOCK IS WORN. REPLACED IAW HORIZON AIR EA 4-54-130, FOKKER FAX TS04.55321 AND FOKKER MM 54-10-02, PAGE 3.SDR 2001FA0000020Strut · defectiveWING STRUTS HAD FILLED WITH WATER FROM SITTING OUTSIDE. RUST STAINS VISIBLE FROM OUTSIDE OF STUT. WHEN POKED WITH AIR AWL IT PUSHED A HOLE INTO STRUT AND DRAINED WATER. DRILLED A .0312 HOLE IN BOTTOM OF OTHER 3 STRUTS AND WATER CAME OUT IN EXCESS OF 1 CUP ESDR UPS01836131Intercostal · crackedINSPECTION TYPE:C2,3 RIGHT WING CENTER L/E INTERCOSTAL IS CRACKED AT XS 454.976. REMOVED AND REPLACED INTERCOSTAL IAW DWG 5769857 AND SRM 57-1-0, 51-1-20D, 51-1-21.
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