JASC 5730
Service difficulty reports · 27,269
Reports filed under 5730 · Wing, Plate/Skin, 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 = '5730' 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 = '5730' 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 IXXA10SMN022SDoubler · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 MAIN TANK TOP ACCESS DOOR NR 506C DOUBLER CRACKED AT STA XRS 22.750 STR 13. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED INTERNAL AND EXTERNAL DSDR ASOA201000089Skin · crackedFOUND RT LOWER WING PLANK FUEL ACCESS HOLE 640FB HAS MULTIPLE INDICATIONS NOTED INBD SIDE OF LANDING IN NON CRITICAL AREA APPROX .5" IN LENGTH 90 PERCENT AND 50 PERCENT FSH FAILED NDT INSPECTION. MARKED ON ACFT. COMPLIED WITH EC/TC EO 600-57-81 C/W IAW REO 601SDR P5CA2010012201627Panel · crackedDURING WALK AROUND CHECK THE LEFT LOWER LEADING EDGE PANEL IN FRONT OF THE FUELING PANEL DOOR WAS FOUND CRACKED. TIME LIMITED REPAIR ACCOMPLISHED IAW EO 4457A227 AND FAA 8110-3 DATED 22JAN10. DVI REQUIRED EVERY A-CHECK WITH PERMANENT REPAIR TO BE ACCOMPLISHESDR CALA2010012500017Skin · corrodedBS 984 RIGHT UPPER SURFACE OF CENTER TANK HAS EXFOLIATION UNDER STUB BEAM. PERFORMED REPAIR TO CORROSION AT BS 984 RIGHT UPPER SURFACE OF CENTER TANK UNDER STUB BEAM COMPLYING WITH STEPS 1-12 OF EC/RA 5730-02583.SDR CA100119012Skin · damaged(CAN) DURING A PREFLIGHT INSP, A PORTION OF SKIN WAS FOUND TORN FWD OF THE LT REAR SPAR, ON A SECTION OF SKIN THAT FORMS PART OF THE FAIRING THAT COVERS THE AFT PORTION OF THE LANDING GEAR WELL. THERE IS A PREVIOUS REPAIR ON THE RT SIDE OF THIS SAME ACFT. THSDR ASOA201000068Skin · corrodedINDICATIONS OF CORROSION NOTED AT WS 231.0 (650BB) ON THE FLAT LANDING SURFACE OF LOWER WING PLANK APPROX 70 PERCENT FULL SCREEN HEIGHT. AREAS MARKED ON ACFT. C/W EC/TC EO 600-57-81, C/W IAW REO 601R-57-21-030 REV G AND FWDED ALL REQUIRED FORMS TO STRUCTURE SDR 2010FA0000055Skin · corrodedCTR WING SKIN CORRODED AT STRINGER 3C, LBL 17 INSIDE LT RAM AIR DUCT.SDR 2010FA0000054Skin · corrodedLOWER CTR WING SKIN CORRODED AT STRINGER 6C, LBL 30 INSIDE LT RAM AIR DUCT.SDR UIEA201000066Skin · corrodedDURING C-CHECK, MAINTENANCE FOUND CORROSION ON THE INTERSPAR SKIN AFT OF REAR SPAR. CORROSION WAS BLENDED OUT AS PER EO 4757A493 AND FAA 8100-9 DATED 1 FEB 2010.SDR AALA20100115AFW01Skin Panel · damagedFIVE UPPER SKIN PANEL 666KT FASTENER HOLES ON THE RIGHT OUTBOARD TRAILING EDGE FLAP WERE DAMAGED DURING MAINTENANCE. REPAIRED UNDER ENGINEERING AUTHORIZATION COMP-57-008495.SDR ZZDA2010086Rub Strip · corrodedRIGHT WING UPPER ACCESS PANEL 620FT RUB STRIP, CORROSION. ACCOMPLISHED WING UPPER ACCESS PANEL 620FT RUB STRIP REPLACEMENT PER B717 SRM 57-10-01.SDR FDEA201001140128Skin · crackedRT WING LOWER SKIN SURFACE IS CRACKED AT ACCESS PANEL 613 AB. REMOVED ACCESS PANEL ADJACENT TO THE REPAIR ON THE FWD SPAR IAW SRM 51-40-02, PARA 5. FABRICATED -1 AND -3 REPAIR DOUBLERS IAW SRM 53-15-63, FIG 201. ALODINED REPAIR IAW SRM 51-21-10, PARA 2-B(C)SDR FDEA201001140126Skin · cracked14 EACH FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT IAW EA NR 1-5710-137539. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100, REVISION 109.SDR FDEA201001140125Skin · cracked13 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 690 AND STA XORS = 700. REPAIR CARRIED OUT IAW EA NR 1-5710-137538. REPAIR CLASSIFIED MINOR IAW GMM 6-2-100 REVISION 109.SDR HALA2010011300046Skin · corrodedCORROSION ON TOP OF THE RT WING SKIN, VARIOUS PLACES. FASTENERS REMOVED IAW SRM 51-40-02, CORROSION BLENDED OUT IAW SRM 57-20-01, ROTOR PEENED IAW SOPM 20-10-03, FPI IAW SOPM 20-10-02, FIFEC INSPECTED, ALODINE AND PRIMED IAW SRM 51-20-01, INSTALLED FASTNERS, SDR ZZDA2010018Rub Strip · corrodedLEFT WING UPPER ACCESS PANEL 520DT RUB STRIP, CORROSION. ACCOMPLISHED WING UPPER ACCESS PANEL 520DT RUB STRIP REPLACEMENT PER B717 SRM 57-10-01. SEE NR 1070.SDR IPXA10M58172Skin · misrepairedINSPECTION TYPE:2C, REPAIR SURVEY SEQUENCE NR 290-W3-03 LT WING FIXED L/E PREVIOUS REPAIR DOUBLER DOES NOT CORRELATE TO SRM 57-40-01 REPAIR 5, FIG. 201 DUE TO FASTNER PATTERN. REMOVED DOUBLER, FABRICATED AND INSTALLED NEW REPAIR DOUBLER AND SHIMS IAW SRM 57-SDR FDEA201001110076Skin · crackedRT WING L/E FOUND CRACKS ON SKIN DOUBLER UPPER INT SKIN L/E. REPAIRED BEADED DOUBLER IAW SRM 57-10-00 FIG.71 VOL.1.SDR FDEA201001110075Skin · crackedRT WING L/E FOUND CRACK ON DOUBLER UPPER INT SKIN L/E. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110074Skin · crackedRT WING L/E FOUND CRACK ON SKIN DOUBLER UPPER INT SKIN. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110073Skin · crackedRT WING L/E FOUND CRACK ON DOUBLER UPPER INT SKIN. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110072Skin · crackedRT WING L/E FOUND CRACK ON SKIN DOUBLER UPPER INT SKIN L/E. REPAIRED DOUBLER IAW SRM 57-10-00, FIG 71, VOL I.SDR FDEA201001110071Skin · crackedRT WING LWR SURFACE FOUND CRACK ON SKIN OF WING TIP. REPAIRED SKIN IAW SRM 57-00-01 FIG.4 SH.2 VOL.1SDR FDEA201001110070Skin · crackedRT WING L/E FOUND CRACK ON LWR EXT SKIN L/E. REPAIRED SKIN IAW SRM 57-10-00, FIG 68, SHT 2, VOL I.SDR GLBA20100113FSkin · damagedMAJOR REPAIR - DURING ROUTINE TOWING OF ACFT ON 01/10/2010 THE RT WING CAME INTO CONTACT WITH ANOTHER ACFT RESULTING IN DAMAGE TO THE RT WING BETWEEN WS 183 & WS 236. UPON EVALUATION OF THE DAMAGE, THE AREA WAS DETERMINED TO REQUIRE A MAJOR REPAIR. MX REPAIRESDR IXXA10SMN011SSkin · corrodedDURING ROUTINE C CHECK INSP FOUND RT WING INBD L/E SLANT PANEL UPPER SKIN CORRODED AT STA XFS 70.000 - 160.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. CLEANESDR TRBACPCP2010002SUSkin · corrodedRT WING AT RIB 13 LOWER SURFACE FWD SKIN HAS CORROSION. TEMPORARY REPAIR, REMOVED CORROSION AND BLENDED OUT OF SKIN IAW SRM 51-21-58. PERFORMED A PERMANENT REPAIR AREA UNDER THIS EO E2-57 MR-360 AT NEXT SCHEDULED C-CK. PENDING FINAL REPAIR EMBODIMENT OR REPAIRSDR TRBACPCP20100002Skin · corrodedRT WING AT RIB 13 LOWER SURFACE FWD SKIN HAS CORROSION. AWAITING NRWC FOR DETAILS.SDR VNAA2010011200004Panel · damagedPITTING WAS FOUND ON THE RADIUS OF FUEL PANEL 510AB. REPAIRS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.SDR QXEA2010010800017Buttstrap · corrodedC-CHECK - CORROSION ON RT LOWER WING BUTT STRAP AT RBL 45.00. REMOVED THE CORROSION IAW SRM 51-21-06-001-001-A01. BLENDS ARE WITHIN LIMITS IAW REO 670-57-21-435. PERFORMED LPI ON BLEND NO CRACKS OR CORROSION AT THIS TIME IAW LPI NDTM 51-20-008. TREATED, PRSDR ABXR0210072000024Panel · broken(ABXR) DURING A MX INSP EVENT, FOUND PANEL 621ZB , RT L/E HAD (2) DOUBLERS BROKEN AND MISSING. REMOVED (2) DOUBLERS ON PANEL 621ZB IAW DWG 114T2400.SDR ABXA201007090100Doubler · brokenPANEL 621ZB RT LEADING EDGE HAS TWO DOUBLERS BROKEN AND MISSING. REMOVED AND REPLACED TWO DOUBLERS ON PANEL 621AZB IAW BOEING DRAWING 114T2.SDR IPXA10M58165Skin · crackedINSPECTION TYPE: 2C, LT WING NR 12 SLAT TRACK CUT-OUT IS CRACKED ON OTBD CORNER TRIMMED CRACK, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-40-02, REPAIR 7 FIG 201.SDR COMA2010010650009Skin · crackedLEFT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 65.75, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.SDR COMA2010010650008Skin · gougedLEFT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 0.0, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.SDR COMA20100650007Skin · crackedRIGHT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 65.75, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.SDR COMA2010010650006Skin · damagedRIGHT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 0.0, STRINGER 5. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.SDR USAA2010012090152Panel · debondedSAL - BC7 - MAJOR REPAIR - DEBOND ON LEFT WING CLOSING PANEL 540CZ. REPLACED LEFT WING CLOSING PANEL 540CZ IAW A320 AMM 57-27-11.SDR USAA2010010490009Skin · corrodedCLT - C2 - MAJOR REPAIR - CORROSION ON RIGHT WING UPPER SKIN AT WBL 136, S11. REPAIRED RIGHT WING UPPER SKIN AT WBL 136, S11 IAW EA 101632.SDR TRBACPCP20090026Skin · corrodedRT WING WATER DRAIN VALVE SURROUNDING SKIN FOUNDED WITH CORROSION. PERFORMED TEMPORARY REPAIR OF RT WING INNER DRAIN VALVE SKIN IAW EO NR E2-57MR-359 (BETWEEN RIB 4 AND 5) FOR 500FC.SDR IPXA10M58170Skin · damagedINSPECTION TYPE:2C, REPAIR SURVEY SEQUENCE NR 290-W4-10 RT WING FIXED L/E LWR SURFACE PREVIOUS REPAIR DOUBLER GOUGED, TOOLMARK, OVER COUTERSUNK. APPROX BTWN STA XOS836-867. REMOVED DOUBLER, REMOVED DAMAGE, AND FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBSDR IPXA10M58180Skin · crackedINSPECTION TYPE:2C, LT L/E TELESCOPIC DUCT CUTOUT UPPER INBD AND OTBD CORNER CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLERS AND DOUBLER IAW SRM 57-40-01 REPAIR 10 FIG 201.SDR IPXA10M58179Skin · crackedINSPECTION TYPE: 2C RT WING L/E SKIN CRACKED AT BOTH CORNERS OF SLOT FOR ANTI-ICE DUCT CUT OUT DAMAGE. FABRICATED & INSTALLED FILLERS AND DOUBLER REF SRM 57-40-01 REPAIR 10 FIG 201.SDR IPXA10M58167Skin · crackedINSPECTION TYPE:2C, LT WING L/E SLAT TRACK CUTOUT NR 12 CRACK ON LWR OTBD CORNER. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-40-02 REPAIR 7, FIG. 201.SDR IPXA10M58166Skin · crackedINSPECTION TYPE: 2C, LT WING SLAT TRACK CUT OUT NR 14 CRACKED ON LWR OTBD CORNER, REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW SRM 57-40-02 REPAIR 7, FIG 201.SDR IPXA10M58164Doubler · crackedINSPECTION TYPE: 2C, LT L/E SKIN BEADED DOUBLER AT XFS 667 CRACKED IN 4 SPOTS. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02 REPAIR 9, FIG. 203 SHT. 1-3.SDR IPXA10M58163Doubler · crackedINSPECTION TYPE:2C, POSSIBLE CRACKS AROUND BUCKED RIVETS IN BEADED DOUBLER RT WING L/E INTERIOR THRU PANEL 619DB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND ANGLES IAW SRM 57-40-02 REPAIR 9, FIG 203.SDR IXXA10WSAP012SPanel · crackedDURING ROUTINE C-CHECK INSP FOUND RT WING T/E PANEL NR 651WB CRACKED. ACCOMPLISHED REPAIR IAW MM 20-11-00 REV 79, AND SRM 51-70-06 REV 101, 51-21-10 REV 97, 51-40-05 REV 101.SDR KCSA091139Skin · corrodedLEFT WING UPPER SKIN CORRODED FWD OF FRONT SPAR AT WS 1485.SDR UIEA201000082Skin · gougedRT WING LOWER SURFACE HAS 2 AREAS WITH GOUGES ON SKIN EDGES STN 1551 & STN 1558. BOTH WITHIN SRM LIMITS. SRM 57-20-01-1A-1 DETAIL 1. GOUGE MARK SMOOTHED OUT IAW SRM 51-10-02. EO 4457A218, REV B.
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