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.

SDR UPS02839290Skin · crackedINSPECTION TYPE:C1 RIGHT WING L/E UPPER SKIN IS CRACKED AT XFS 610. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-7767-A.Aug 20, 2002 · N708UP · Doug DC871FSDR UPS02839289Doubler · crackedINSPECTION TYPE:C1 RIGHT WING CENTER L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335.25. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-21.Aug 20, 2002 · N708UP · Doug DC871FSDR 2002F00970Skin · crackedDURING CURRENT C-CHECK AT SIAEC, FOUND RT WING L/E STATIONS NR ILES 378, 400, 446, 467, AND 546 NOSE CAP POSITIONS CRACKED AND CORRODED AT TOP ROW OF RIVETS. SIX CRACKED/ CORRODED AREAS TRIMMED OUT. ALL AREAS HFEC INSPECTED FOR ADDITIONAL CRACKS. NONE FOUNDAug 19, 2002 · N517MC · Boeing 747243BSDR QXEA0201262Panel · scratchedPDX - LEFT HAND WING DRY BAY PANEL 523 AT LADDER PLATE HAS SCRATCH DAMAGE TO TOP SURFACE WHERE PANEL EDGE SEALANT GOES. REPAIRED IAW RD 8-57-499.Aug 19, 2002 · N363PH · Dhav DHC8202SDR UIEA200200032Panel · crackedDURING CURRENT (C) CHECK AT SIAEC FOUND CRACKED CLOSURE PANEL ON LT WING LE NR12 KRUGER FLAP FOLDING NOSE SECTION OF THE CENTER ATTACH BRACKET AT ILES 480. TRIMMED OUT CRACKED SECTION OF CLOSURE WEB. FABRICATED NEW SECTION OF WEB AND ASSOCIATED SLICE DOUBLERAug 19, 2002 · N517MC · Boeing 747243BSDR DHL2002363506Skin · corrodedC-CHECK, BOTTOM SKIN LEFT WING BETWEEN RIB 10 AND 13 JUST OUTBOARD OF ACCESS PANEL 543BB LIGHT CORROSION ON WING PLANK. REMOVED CORROSION IAW A300 SRM 51-40-11. REMOVED CORROSION IAW A300 SRM 51-40-11, AREA WITHIN LIMITS IAW A300 SRM 57-33-11.Aug 15, 2002 · N363DH · Airbus A300B4203SDR DHL2002363512Skin · corrodedC-CHECK, RT WING FWD OF NR 6 FLAP TRACK ASSY HAS EXFOLIATION ON LOWER WING PLANK AT DRAIN HOLE. REMOVED CORROSION IAW A300 SRM 51-40-11. REMOVED DAMAGED FASTENER AND COUNTERSUNK HOLE PER A300 SRM 51-30-43 AND REINSTALLED NEW FASTENER IAW A300 SRM 51-30-35. Aug 10, 2002 · N363DH · Airbus A300B4203SDR AWXA200200717Panel · missingA 6 X 8 INCH PORTION OF PANEL 621FB FOUND MISSING AFT OF L/E O/B END, JUST I/B OF NR 2 ENG PYLON. A 4 INCH GOUGE TO HONEY COMB OF NR 2 ENG NOZZLE AT 10 O'CLOCK POSITION. UPON REMOVAL OF PANEL 621FB DAMAGE FOUND TO RT I/B L/E SLAT O/B TRACK FAIRING, I/B & MIDAug 9, 2002 · N653AW · Airbus A320232SDR AAL2002F00008Skin · groovedWING SKIN, GROVE IN BOTTOM OF WING IN BOARD AND AFT OF NR1 SLOT TRACK ON PANEL LANDING. DEPTH, OUT OF LIMITS, .5000 INCH X 10 INCHES, LEFT WING. REPAIRED IAW ESO. (2002-1167 AMC4)Aug 7, 2002 · N7549A · Doug DC982SDR QXEA0201401Skin · crackedCKB- ALL 4 CORNERS CRACKED ON LEFT HAND WING INBOARD LEADING EDGE. REPAIRED IAW HORIZON AIR EA 6-57-47A AND WVAC EO DH8S-57-0506A.Aug 6, 2002 · N404QX · Bombdr DHC8401SDR 252TR0001PAPanelreturn to departure point due to high a/c vibration. insp complete exterior of a/c all panels & flight controls to include doors,found several loose & missing screws on panel # 6537. replaced & retorqued screws on panel # 6537,no other defects noted.Aug 5, 2002 · N252TR · Boeing 737228SDR QXEA0201105Access Panel · dentedPDX - DENT NOTED AT FIXED ACCESS PANEL 521AT, LEFT HAND WING. INSTALLED LEADING EDGE 521AT ON THE LEFT HAND WING IAW CRJ-700 MM 57-41-05, PAGES 426-428.Aug 3, 2002 · N611QX · Cndair CL6002C10SDR IXXA0200117SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK ALONG WITH CORROSION WAS DETECTED ON THE LT WING UPPER AFT SKIN ABOVE THE LT GEAR TRUNNION AREA. REAPIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IN ACCORDANCE WITH THE DOUAug 2, 2002 · N828BX · Doug DC871FSDR UPS02839257Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 9. CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED FREEZE PLUG AND DOUBLER IAW SRM 57-2-1 FIG 10.Aug 1, 2002 · N806UP · Doug DC873FSDR UPS02839256Skin · crackedINSPECTION TYPE:C2 RIGHT WING UPPER SKIN IS CRACKED AT XRS 74 AT STRINGER 11. CUTOUT DAMAGED AREA, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER AND FREEZE PLUGS IAW SRM 57-2-1 FIG 10.Aug 1, 2002 · N806UP · Doug DC873FSDR ABXA020180Skin Panel · delaminatedDELAMINATION AREA ON OUTBOARD TRAILING EDGE BONDED PANEL LOCATED ON WING UPPER SURFACE AND FORWARD OF AILERON. REPLACED OUTBOARD TRAILING EDGE BONDED PANEL IAW DC-9 SRM 51-30-2 AND 51-30-1.Jul 31, 2002 · N953AX · Doug DC941SDR AWXA200200804Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK .25 INCH CRACKS WERE FOUND ON RT WING LEADING EDGE AT THE NR 6 SLAT CENTER STOP FITTING CUTOUT, WS 557. MAINTENANCE BLENDED OUT CRACKS ON RT WING LEADING EDGE NR 6 SLAT CENTER STOP CUTOUT IAW AWA ER 15-5741-02232-SS1.Jul 31, 2002 · N183AW · Boeing 737277SDR UPS02839249Skin · corrodedINSPECTION TYPE:C2 LEFT WING CENTER L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 366.5. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 57-2-0 FIG 7, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-2- 1 FIG 38.Jul 30, 2002 · N806UP · Doug DC873FSDR UPS02839241Skin · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER SKIN IS CRACKED AT DRAIN HOLE AT XFS 597.5. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER IAW EO DC8-5720-4087.Jul 29, 2002 · N806UP · Doug DC873FSDR UPS02839238Skin · corrodedINSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION IB OF XFS 710. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-2-1 FIG 2H.Jul 29, 2002 · N806UP · Doug DC873FSDR QXEA0201400Skin · crackedCKB- RIGHT HAND CENTER WING LEADING EDGE CRACKED AT 4 CORNERS. REPAIRED IAW HORIZON AIR EA 6-57-47 AND WVAC EO DH8S-57-0506.Jul 28, 2002 · N404QX · Bombdr DHC8401SDR COMA0260453SkinL/H WING, LOWER SKIN FUEL PANEL LANDING @ WS95.950 HAS CORROSION .008" DEEP.REMOVED CORROSION BY BLENDING. PERFORMED EDDY CURRENT INSP TO ENSURE COMPLETE DAMAGE REMOVAL. FLAP PEENED REWORKED AREAS, AND REAPPLIED PROTECTIVE FINISH. ALL WORK WAS PERFORMED I/A/W Jul 28, 2002 · N936CA · Cndair CL6002B19SDR IXXA0200087SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT OUTBOARD SLOT LEADING EDGE AREA ON THE MOUNTING SURFACE WING STATION XFS422.750. REPAIR ACCOMPLISHED, REMOVAL OF CORROSION, FABRICATION AND INSTALLATION OF REPAIR DOUBLERS AND SHIMS IAW THEJul 24, 2002 · N825BX · Doug DC871FSDR TSAA0257184Skin · corrodedLEFT LOWER OUTBOARD WING TRAILING EDGE CORRODED AT WSL 453. BLENDOUT TO REMOVE ALL CORROSION CONFIRMED USING 10X VISUAL INSPECTION NO DEFECTS NOTED, OBTAINED A SURFACE FINISH OF 125 MICROINCHES RADIUS OR SMOOTHER, FLAT PEENED REWORKED AREA, ALODINED AND PRIMEJul 24, 2002 · N818AL · Boeing 737230SDR COMA0260450SkinI/H WING LOWER SKIN FUEL PANEL LANDINGS @ W.S. 106.40, 127.25, 264.00 AND 294.50 HAVE CORROSION FROM 0.010" - 0.012" DEEP.REMOVED CORROSION BY BLENDING. PERFORMED EDDY CURRENT INSP TO ENSURE COMPLETE DAMAGE REMOVAL. FLAP PEENED RE-WORKED AREAS, AND REAPPLIED PJul 24, 2002 · N713CA · Cndair CL6002B19SDR AWXA200200799Skin · damagedYVR - MAJOR REPAIR - DURING C-20 THE RT WING LOWER SURFACE NR 5 SLAT TROMBONE CUTOUT HAS SMALL PIECE OF SKIN MISSING AT OUTBOARD END. MAINTENANCE REMOVED DAMAGED AREA OF SKIN RT WING LOWER SURFACE NR 5 SLAT TROMBONE CUTOUT, FABRICATED A NEW SECTION OF SKIN, AJul 23, 2002 · N182AW · Boeing 737277SDR DHL2002806859Skin · damagedPERFORMED MAJOR REPAIR IAW EO DHL 020621, ED-3095, EO SEMAN 2002684. BLENDED DAMAGED AREAS. FABRICATED REPAIR DOUBLER IAW EO DHL 020621, ED-3095, EO SEMANS 2002684. INSTALLED DOUBLER ON RT WING L/E LOWER SURFACE STA XFS710.000 IAW EO DHL 020621, ED-3095, EOJul 22, 2002 · N806DH · Doug DC873FSDR DHL2002806841Skin · corrodedLT WING CENTER L/E LWR SKIN SHOWS CORROSION XFS 420.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT AFFECTED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER ON LT WING CENTER L/E LWR SKIN.Jul 21, 2002 · N806DH · Doug DC873FSDR QXEA0201092Skin · gougedPDX- TWO GOUGES NEXT TO EACH OTHER ON THE TOP CENTER INBOARD SIDE OF OUTBOARD WINGS. REPAIRED IAW DHC-8 RD 8-57-1734 AND RD 8-57-1549.Jul 20, 2002 · N361PH · Dhav DHC8202SDR DHL2002806860Skin · damagedLT WING OUTBOARD LEADING EDGE UPPER SKIN HOLES ELONGATED XFS710.000. PERFORMED MAJOR REPAIR IAW EO DHL 020614, ED-3086, EO SEMAN 2002675. TRIMMED OUT DAMAGED SKIN AREA. FABRICATED A REPAIR DOUBLER, A TRIPLER AND A FILLER IAW EO DHL 020614, ED-3086, EO SEMANJul 18, 2002 · N806DH · Doug DC873FSDR DHL2002806537Skin · crackedLT WING STUB WING LEADING EDGE LWR SKIN CRACKED .5 INCH XFS 207.000. FABRICATED AND INSTALLED DOUBLER IAW EO DHL020622, ED-3100, EO SEMAN 2002688, SRM 51-1-21 PG 1, SRM 51-1-20D PG 9.Jul 18, 2002 · N806DH · Doug DC873FSDR DHL2002806536Panel · corrodedLT WING T/E SKIN UPPER PANEL SHOWS POINTS OF CORROSION XW47.000 - XW75.312. REMOVED CORROSION IAW SRM 57-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. REMOVED DAMAGED PANEL IAW SRM 51-3-0, INSTALLED NEW PANEL ON LT WING T/E UPPER SKIN IAW SRM 51-3-Jul 18, 2002 · N806DH · Doug DC873FSDR DHL2002806534Skin · corrodedRT WING L/E SHOWS SPOT OF CORROSION AT STA XW257. REMOVED CORROSION ON RT WING L/E, FOUND OUT LIMITS IAW SRM 57-2-0 PG 16. TRIMMED OUT DAMAGED AREA. FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO DHL 020615 , ED3091, EO SEMAN 2002678.Jul 17, 2002 · N806DH · Doug DC873FSDR IXXA0200108SSkin · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS DETECTED ON A SCREW HOLE ON THE LEFT WING OUTBOARD LEADING EDGE STA XFS 710. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF REPAIR FILLER AND DOUBLER IN ACCORDANCE WITH THE DOUGLAS STRUCTJul 16, 2002 · N41CX · Doug DC862FSDR IXXA0200098SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT WING LEADING EDGE AT XW 485. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGE, FABRICATION AND INSTALLATION OF FILLER AND EXTERNAL DOUBLER IAW THE DOUGLAS SRM.Jul 16, 2002 · N41CX · Doug DC862FSDR IXXA0200096SSkin · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE LEFT WING LEADING EDGE OUTBOARD XW488. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER IAW THE DOUGLAS SRM AND EA 28298-5269-02-129Jul 16, 2002 · N41CX · Doug DC862FSDR GTIA020892Panel · corrodedFTW - FOUND PANEL 1220C, EXFOLIATION CORROSION NEAR CORNER, SEVERAL OXIDIZED SCREW HOLES AND HEADS. MATERIAL LOSS OUT OF LIMITS. REPAIR DOUBLER FABRICATED. INSTALLED REPAIR DOUBLER. (M)Jul 16, 2002 · N819NK · Doug DC981SDR DHL2002806843Skin · corrodedRT STUB WING UPPER SURFACE SKIN CORRODED AROUND XILD42.000 - 257.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT AFFECTED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW EO DHL 020613, ED-3083 & EO SEMAN 2002680 SRM51-1-21 PG 1, SJul 16, 2002 · N806DH · Doug DC873FSDR DHL2002806842Skin · corrodedRT STUB WING UPPER SURFACE SKIN CORRODED AROUND XILD42.000 - 257.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT AFFECTED AREA. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW EO DHL 020613, ED-3083 & EO SEMAN 2002680 SRM 51-1-21 PG 1, Jul 16, 2002 · N806DH · Doug DC873FSDR 02FDEA00492Skin · corrodedRT WING LOWER SKIN CORRODED ON LWR SURFACE ON NR 2 PANEL AT AFT EDGE AT RIB 9. STRUCTURAL REPAIR PER E.A. 6-5710-64296.Jul 16, 2002 · N419FE · Airbus A310SDR 2002FA0001045Doubler · crackedDOUBLER FAILURE DUE TO IMPROPER MANUFACTURE PROCESS. DOUBLER BROKE AT MACHINE RADIUS AND CORNER OF FUEL ACCESS PANEL LOCATED IN LOWER INBOARD WING SKIN AREA. WING SKIN DEVELOPED CRACKS LOCALIZED TO CORNER OF ACCESS PANEL. REMOVED PAINT AND DYE PEN. INSPECTJul 15, 2002 · N14447 · Lkheed P2V7SDR UPS02438955Skin · corrodedINSPECTION TYPE: C RIGHT WING - FRONT SPAR LOWER CHORD FOUND CORROSION AT WS 1100 - 1110 AFTER LOWER PANEL, REMOVED JUST AT NR 4 PYLON AREA. CORROSION BLEND OUT 0.104 INCH X 2 INCH X 4 INCH EXCEED SRM LIMIT. WING LOWER SKIN REPAIRED AS PER HX RS R-57-26-3485Jul 15, 2002 · N677UP · Boeing 747123FSDR GTIA020891Panel · damagedFTW - FOUND PANEL 1171C BARE METAL ON BACK SIDE, NUMEROUS OXIDIZED SCREW HEADS AND SCREW HOLES, EXFOLIATION CORROSION IN TWO PLACES. FOUND MATERIAL TO BE OUT OF LIMITS IN 2 PLACES. FABRICATED TWO DOUBLERS. INSTALLED TWO DOUBLERS. (M)Jul 14, 2002 · N819NK · Doug DC981SDR GTIA020890Panel · dentedFTW - FOUND PANEL 1120C HAS A DENT, BARE METAL. DENT OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER. (M)Jul 14, 2002 · N819NK · Doug DC981SDR IXXA0200094SSkin Panel · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RIGHT WING UPPER LEADING EDGE PANEL BY THE NUMBER FOUR PYLON. REPAIR ACCOMPLISHED, REMOVAL OF DAMAGED AREA, FABRICATION AND INSTALLATION OF REPAIR DOUBLER IAW THE DOUGLAS SRM AND DRAWING 57-0249Jul 13, 2002 · N41CX · Doug DC862FSDR DHL2002806840SkinN/R:2477 LH WING UPPER SURFACE SHIN SHOWS CORROSION STRINGER 9 XRS396.000 ( MAJOR REPAIR)CORR: PERFORMED MAJOR REPAIR IAW SRM 57-2-1 SHEET 1.BLENDED OUT LH WING UPPER SKIN FOUND OUT OF LIMITS IAW SRM57-2-0 PG. 16 CUT CORRODED AREA IAW SRM 57-2-1 FIG. 32 CLEANEJul 12, 2002 · N806DH · Doug DC873FSDR AAL2004F00003Skin · corrodedINTERGRANULAR CORROSION IN WING SKIN BETWEEN RIBS 28-29 JUST AFT OF REAR SPAR. AREA WAS BLENDED, FLAP, PEENED AND TREATED IAW FSO 30595.Jul 11, 2002 · N14061 · Airbus A300B4605RSDR 2002FA0000994Doubler · crackedLOWER WING SKIN ACCESS PANEL DOUBLER CRACKED IN SEVERAL PLACES CWS 90 LEFT SIDE TO CWS 90 RIGHT SIDE. RIGHT WING LOWER SKIN CRACKED AT AN ACCESS PANEL AT CWS 94. (SW)Jul 9, 2002 · N140HP · Lkheed P2V7SDR 2002FA0000996Doubler · crackedLOWER WING SKIN ACCESS PANEL DOUBLER CRACKED IN SEVERAL PLACES CWS 90 LEFT SIDE TO CWS 90 RIGHT SIDE. RIGHT WING LOWER SKIN CRACKED AT AN ACCESS PANEL AT CWS 94. (SW)Jul 8, 2002 · N139HP · Lkheed P2V7SDR 2002FA0000993Doubler · crackedLOWER WING SKIN ACCESS PANEL CUTOUT DOUBLER CRACKED IN SEVERAL PLACES CWS 90 LEFT SIDE TO CWS 90 RIGHT SIDE. RIGHT WING LOWER SKIN CRACKED AT AN ACCESS PANEL CWS 94. (SW)Jul 6, 2002 · N139HP · Lkheed P2V7
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