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 UPS05443919Skin · crackedINSPECTION TYPE: C, LT WING REAR SPAR UPPER SPLICE FITTING AT BS 1241 HOLE NR 11 FOUND CRACKED AT WING SKIN APPROX 0.060 INCH. HOLE REWORKED AT BSB 747-57A2314.SDR QXEA200500418Panel · corrodedYYC - LEFT WING, FUEL PANEL 522CT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-57-428.SDR QXEA200500413Access Panel · corrodedYYC - RIGHTHAND WING, RIGHTHAND FUEL PANEL 622CT, BOTTOM SURFACE OF PANEL, PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD -8/4-57-438, ISSUE 1 Q400 SRM 51-21-00-350-001 AND HORIZON AIR EA 6-57-312.SDR QXEA200500221Panel · corrodedPDX - LEFT WING PANEL 523AT COUNTER SINKS HAVE FRETTING. REPAIRED IAW RD 8-57-1715.SDR QXEA200500222Panel · corrodedPDX - RIGHT WING PANEL 623AT COUNTER SINKS HAVE FRETTING. REPAIRED IAW RD 8-57-1715.SDR 05FDEA00256Access Panel · crackedLEFT HAND WING LEADING EDGE SKIN CRACKED AT STATION XORS 530, AROUND REFUELING STATION ACCESS PANEL INBOARD CORNER. COMPLIED WITH EA 8-5710-8352, WINGS- LEFT HAND LEADING EDGE TEE CRACK AT REFUELING DOOR CUTOUT- REPAIR.SDR QXEA200500407Access Panel · corrodedYYC - RIGHTHAND WING, RIGHTHAND FUEL TANK PANEL 622CT, PANEL REBATED WS 117.50 TO WS 157.825, FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q400 SRM 57-10-30-320-002 AND RD 8/4-57-435, ISSUE 1.SDR QXEA200500419Panel · corrodedYYC - LEFT WING PANEL 522BT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-87-422.SDR QXEA200500412Panel · corrodedYYC - LEFTHAND WING, LEFTHAND FUEL TANK PANEL 522CT, PANEL REBATE WS 117.50 TO WS 157.825, FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q400 SRM 57-10-30-320-002, RD 8/4-57-429, ISSUE 1 AND HORIZON AIR EA 6-57SDR CALA0500041Panel · crackedINSPECTION FOUND A 2 INCH CRACK IN UPPER TRAILING EDGE PANEL LOCATED FORWARD OF O/B SIDE OF GROUND SPOILER, LEFT UPPER WING, XRS 91.0 TO 111.5. A NEW PANEL WAS INSTALLED IAW SRM 51-30-2.SDR QXEA200500415Panel · corrodedYYC - RIGHTHAND WING, RIGHTHAND FUEL PANEL 623AT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-57-420.SDR QXEA200500396Shroud · chafedYYC - LEFTHAND OUTBOARD FLAP HAS A CHAFING MARK SEVERAL FEET LONG FROM CONTACT WITH THE UPPER WING SHROUD. REPAIRED IAW RD 8/4-57-423 AND HORIZON AIR EA 6-57-296.SDR QXEA200500423Panel · corrodedYYC - RT WING ANCHOR NUTS AROUND PANEL 622AT ARE CORRODED AND BROKEN AT ALL LOCATIONS. REPAIRED IAW Q400 SRM 51-42-05-330-001.SDR QXEA200500420Panel · corrodedYYC - LEFTHAND WING, LEFTHAND WING FUEL PANEL 522BT PANEL ATTACH DOMED ANCHOR NUT WS 114.50 AND STRINGER 4L ANCHOR NUT HAS UN-REMOVEABLE FOD. REPAIRED IAW Q400 SRM 51-42-05-330-001.SDR QXEA200500416Panel · corrodedYYC - RIGHTHAND WING, RIGHTHAND FUEL PANEL 622BT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-57-419.SDR UPS05243877Skin · crackedSUSPECT CRACK ON LT WING DOOR, ON INNER SKIN AT UPPER FWD END. REPAIR CARRIED OUT IAW SRM 51-40-2.SDR ASAA0580080Skin · gougedOKC - DURING C-CHECK, FOUND LEFT WING OUTBOARD FLAP VANE LEADING EDGE IS GOUGED. REMOVED DAMAEGD AREA. INSTALLED REPAIR FILLER AND DOUBLER. (M)SDR QXEA200500424Panel · corrodedYYC - RIGHT WING PANEL 622AT HAS FRETTING CORROSION ON BOTTOM SIDE OF PANEL. REPAIRED IAW Q400 SRM 57-10-35-992-801 AND 57-10-30-940-002.SDR QXEA200500408Panel · corrodedYYC - RIGHTHAND WING, RIGHTHAND FUEL PANEL 623AT, PANEL REBATE WS 157.825 TO WS 190.0, FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q400 SRM 57-10-30-320-002, RD 8/4-57-418, ISSUE 1 AND HORIZON AIR EA 6-57-297SDR QXEA200500392Skin · erodedYYC - LEFTHAND WING TIP LEADING EDGE HAS EROSION DAMAGE TO COMPOSITE STRUCTURE. REPAIRED IAW Q400 SUB TASK 51-80-00-340-802, 51-25-26-370-801 AND RD 8/4-57-415, PAGE 4.SDR QXEA200500409Panel · corrodedYYC - LEFTHAND WING, LEFTHAND WING FUEL TANK PANEL 522BT, PANEL REBATE WS 79.700 TO WS 117-500, FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q400 SRM 57-10-30-320-002, RD 8/4-57-424, ISSUE 1 AND HORIZON AIR EASDR QXEA200500406Panel · corrodedYYC - RIGHT WING RIGHT FUEL TANK PANEL 622BT, PANEL REBATE WS 79.700 TO WS 117.500 FRETTING CORROSION ON TOP SURFACE OF REBATE AROUND PANEL. REPAIRED IAW Q400 SRM 57-10-30-320-002, 51-21-10-380-001 AND 51-25-40-370-001.SDR QXEA200500411Panel · corrodedYYC - LEFTHAND WING, LEFTHAND FUEL PANEL 523AT, PANEL REBATE WS 157.825 TO WS 190.00, FRETTING CORROSION ON TOP OF REBATE AROUND PANEL ANCHOR NUT ATTACH HOLES. REPAIRED IAW Q00 SRM 57-10-30-320-002, 51-21-10-380-001, 51-25-40-370-001, RD 8/4-57-424, ISSUE 1 ASDR QXEA200500393Skin · erodedYYC - RIGHTHAND WING TIP LEADING EDGE HAS EROSION DAMAGE TO COMPOSITE STRUCTURE. REPAIRED IAW DHC-8 Q400 SUB TASK 51-80-00-340-802, 51-25-26-370-801, 51-25-31-370-801 AND RD 8/4-57-415, PAGE 4.SDR A6WA200540039Panel · corrodedRT WING PLANK HAS CORROSION UNDER THE FOLLOWING FUEL PANELS 640BB AND 650HB. REMOVED MINOR CORROSION FROM RIGHT WING LOWER PLANK AT FUEL TANK ACCESS PANELS 340BB AND 650 HB IAW BOMBARDIER, INC REO 601R-57-21-030 REV C. (M)SDR A6WA200540037Access Panel · corrodedLT WING PLANK HAS CORROSION UNDER THE FOLLOWING FUEL TANK PANELS 550BB, 540ED, 540BB, 510AB. REMOVED MINOR CORROSION FROM LT WING LOWER PLANK AT FUEL ACCESS PANELS 550BB, 540FB, 540EB, 540BB AND 510AB IAW MFG REO 601R-57-21-030 REV C. (M)SDR 05FDEA00205Skin · corrodedDURING AIRPLANE PASSENGER TO FRIGHT CONVERSION: FOUND MANY SEVERE CORROSION ON UPPER SKIN OF THE CTR BOX WING LT SIDE STA 1199;1219 AND 1229 X= 100 RH SIDE STA 1199;1219 AND 1229 X=-100. REMOVE FASTENERS IN THE AFFECTED AREA, REMOVED CORROSION PER SRM 57-20-SDR QXEA200500427Panel · corrodedYYC - LEFTHAND WING, LEFTHAND FUEL PANEL REBATE AT 522AT HAS CORROSION AROUND SCREW HOLES, TOP SURFACE. REPAIRED IAW Q400 SRM SUB TASK 57-10-30-940-002.SDR QXEA200500428Panel · corrodedYYC - LEFT WING FUEL PANEL AT 522AT, BOTTOM SURFACE HAS AREAS OF CORROSION AROUND SCREW HOLES. REPAIRED IAW Q400 SRM SUB TASK 57-10-35-910-001.SDR QXEA200500417Panel · corrodedYYC - LEFTHAND WING LEFTHAND PANEL 523AT BOTTOM SURFACE OF PANEL PITTING AND FRETTING CORROSION AROUND PANEL ATTACH HOLES. REPAIRED IAW RD 8/4-57-421.SDR QXEA200500429Panel · corrodedYYC - RIGHT WING FUEL PANEL AT 621AT LOWER SURFACE HAS AREA OF CORROSION, AROUND SCREW HOLES. REPAIRED IAW Q400 SRM SUB TASK 57-10-35-940-001.SDR QXEA200500426Panel · corrodedYYC - LEFTHAND WING LEFTHAND FUEL TANK AT 521BT HAS CORROSION AROUND PANEL REBATE TOP SURFACE. REPAIRED IAW Q400 SRM 57-10-35-940-001.SDR USAA050216Skin Panel · crackedPIT - FOUND SKIN PANEL CRACKED 1 INCH, LEFT LEADING EDGE LOWER SKIN PANEL AT SLAT STATION 3.25. FILLER AND DOUBLER INSTALLED PER TYPICAL REPAIR 57-41-02. (M)SDR A6WA200540028Skin · corrodedMWC 170 CORROSION EXISTS ON LOWER WING PLANK UNDER FUEL PANEL 510AB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K)SDR A6WA200540027Skin · corrodedFOUND CORROSION ON RT LOWER WING PLANK UNDER THE FOLLOWING FUEL PANELS 640BB AND 650GB. PERFORMED A MAJOR REPAIR BY REMOVING CORROSION IAW REO. (K)SDR CA050125016Panel · loose(CAN) DURING ROUTINE MAINTENANCE INSPECTION VISUALLY NOTICED SCREW HEADS PROTRUDING ABOVE WING SURFACE ON WING STRESS PANEL (DRYBAY ACCESS). APPROXIMATELY 50 PERCENT OF THE ATTACH SCREWS (CSP318-5) WERE FOUND LOOSE ON ACESS PANEL NR 522AT, ALSO SOME LOOSE SCRESDR IXXA0500163SSkin · crackedDURING ROUTINE C-CHECK FOUND LEFT WING JUST ABOVE NUMBER 2 PYLON UPPER SKIN CRACKED. REPLACED UPPER SLOT DOOR WITH NEW, IAW DC8MM 20-12-0, AND 27-81-02.SDR QXEA200500135Panel · corrodedPDX - 523AT COUNTERSINKS HAVE FRETTING CORROSION. REPLACED PANEL 857/3043-003.SDR QXEA200500134Panel · corrodedPDX - 522BT COUNTERSINKS HAVE FRETTING CORROSION. REPLACED PANEL.SDR 05FDEA00124Panel · damagedPANEL LAND ON RIGHT WING ACCESS HOLE 650JB HAS 1 EACH ELONGATED HOLE. COMPLIED WITH EA 6-5710-85600 BY INSTALLING REPAIR BUSHING.SDR 05FDEA00123Panel · damagedPANEL 550GB HAS 1 EACH ELONGATED HOLE ON PANEL LAND, LEFT WING. COMPLIED WITH EA 6-5710-85600 BY INSTALLING REPAIR BUSHING.SDR 05FDEA00122Panel · damagedPANEL 550JB HAS 2 EACH ELONGATED HOLES. COMLIED WITH EA 6-5710-85600 BY INSTALLING 2 EACH REPAIR BUSHINGS.SDR DHL2004809527Skin · delaminatedLT WING - REMOVE AND INSTALL NR 1 SPOILER FOR DELAMINATION ON UPPER SKIN, XW 5.000 TO XW 90.000. REMOVED AND REPLACED NR 1 SPOILER (O/H CONDITION) ON LT WING XW 5.000 TO XW 90.000 (LT WING) IAW MM 27-61-1 PG 201-205.SDR SWAA050079Skin · crackedDURING SCHEDULED C1 CHECK, FOUND RT WING LOWER SURFACE SKIN OUTBOARD OF NR 2 ENGINE PYLON MID SPAR FITTING, CRACKED. REPAIRED SKIN PER EA.SDR 05FDEA00063Skin · corrodedRT WING, CORROSION FOUND BETWEEN XOS= 680 TO XOS= 725 UPPER SURFACE SPAR AREA. COMPLIED WITH FEDEX EA 1-5710-81591, CORROSION REMOVAL AND REPAIR. CORROSION REMOVED AT XORS STA 714 AS PER SRM 51-21-01 VOL. II FOUND WITHIN LIMITS AS PER SRM 57-10-00 FIG. 32 VOSDR USAA050209Skin Panel · crackedPIT - FOUND SKIN PANEL CRACKED .5 INCH LONG, OUTBOARD SIDE OF PYLON ABOVE MID SPAR FITTING LOWER SKIN PANEL SLAT STATION 3.25. STOP DRILLED, INSTALLED FILLER AND DOUBLER FREEZE PLUG PER TR 57-41-02, SRM 51-20-10 AND EA 79764. (M)SDR 05FDEA00053Skin · dentedINNER LT WING LOWER SKIN AT XORS= 85 FOUND WITH 3.5 INCH DENT. COMPLIED WITH FEDEX EA 1-5710-81592.SDR 05FDEA00035Skin · dentedACCOMPLISH MAINTENANCE C-CHECK, NON-ROUTINE, RT WING - DENTS AND DEBONDS AT LOWER SKIN SURFACE OF T/E OF FLAP INBOARD. REPAIRED IAW AIRBUS REF: 001-57-01-2005-A1B AND IAW EA 6-5750-81828. PAINTED IAW SRM 51-75-10-8.SDR 05FDEA00039Skin · corrodedRT WING - CORROSION FOUND ON UPPER SURFACE STA 1659 RIB 27 TO STA 1713 RIB 28 INTERSECTION WITH STRINGER 12. CORROSION REMOVED AND REPAIRED IAW EA 6-5710-81827.SDR 05FDEA00037Skin · corrodedACCOMPLISH MAINTENANCE C-CHECK, ORIGINAL PLAN DATE WAS ENTERED ON: 23JUL04. NON-ROUTINE LT WING - CORROSION FOUND ON UPPER SURFACE STA 813 RIB 13 TO STA 874 RIB 14 INTERSECTION WITH STRINGER 7. REPAIRED IAW FAX REF 942-034715/005/2004 DATED 12/27/2004 AND FE
Back to JASC 5730