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 DHL2002806856Skin · corrodedLT WING OUTBOARD L/E UPPER SKIN CORRODED (STA 578.000-603.750, 628.750-653.750). PERFORMED MAJOR REPAIR IAW SRM 57-2-1 PG 2 FIG 38. REMOVED CORROSION FROM LT OUTBOARD LEADING EDGE UPPER SKIN IAW SRM 51-1-8 PG 17-18 FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. SDR CA020708001Fitting · misinstalled(CAN) WHILE CARRYING OUT ALERT SB A8-28-33, IT WAS DISCOVERED THAT ONE OF THE WIGGINS FITTING UNDER ACCESS PANEL 624CT(RT WING OUTBOARD PANEL) WAS INSTALLED BACKWARDS. THERE WAS NO DAMAGE TO THE STIFFNERS ON THE UNDERSIDE OF THE PANEL, WIGGINS FITTING WAS REPOSDR 2002F00953Fairing · crackedAT C-CHECK, FOUND LEFT WING OUTBOARD MID FLAP, OUTBOARD JACK SCREW FAIRING CRACKED. (M)SDR GTIA020741Panel · crackedACY - RIGHT WING LOWER TRAILING EDGE PANEL CRACKED BOTTOM SIDE INBOARD. PERFORMED MULTIPLE LAMINATION REPAIR ON RIGHT LOWER TRAILING EDGE PANEL BOTTOM INBOARD IAW 57-70-1 OF THE DC9/MD80 SRM. (M)SDR GTIA020740Panel · crackedACY - FOUND LEFT WING LOWER TRAILING EDGE PANEL CRACKED BOTTOM SIDE. PERFORMED MULTIPLE LAMINATION REPAIR ON LEFT LOWER TRAILING EDGE PANEL BOTTOM INBOARD IAW DC9/MD80 SRM 57-70-1. (M)SDR DHL2002806839Skin · corrodedREMOVED CORROSION FROM RT WING OUTBOARD L/E UPPER SURFACE IAW SRM 51-1-8 PG 17-18, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT OUT DAMAGED AREA IAW SRM 57-2-1 PG 2 FIG 38. FABRICATED AND INSTALLED FILLER & DOUBLER IAW SRM 57-2-1 PG 2 FIG 38, SRM 51-1-21 PGSDR DHL2002806532Skin · corrodedRT WING OUTBOARD LEADING EDGE UPPER SURFACE SKIN CORRODED XFS 566.000 TO XFS 660.000. REMOVED CORROSION, FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16 ,CUT OUT DAMAGED AREA. FABRICATED FILLER AND DOUBLER IAW SRM 57-2-1 PG 2 FIG 38.SDR QXEA0201006Plate · corrodedPDX - LADDER PLATE FOR PANEL 622AT HAS FRETTING CORROSION AROUND ONE BOLT HOLE. REPAIRED IAW DHC-8-200 RD 8-57-1471.SDR DHL2002806838Skin · corrodedRT WING CENTER LEADING EDGE UPPER SURFACE SKIN SHOWS CORROSION XFS 304.000 - 335.250. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 57-2-0 PG 16. CUT CORRODED AREA IAW SRM 57-2-1 PG 2 FIG 38. FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 57-21-1 PG 2 SDR COOSDR02200Panel · delaminatedRIGHT WING, TRAILING EDGE - LOWER PANEL (PN 6521652616) DELAMINATED.SDR COOSDR02197Panel · delaminatedRIGHT WING, TRAILING EDGE-UPPER PANEL (PN 6521657242) DELAMINATED.SDR COOSDR02185Skin · corrodedRIGHT WING, LOWER SKIN - LOWER SURFACES CORRODED AT WS 637, BETWEEN STIFFENER NR 8 AND STIFFENER NR 9.SDR COMA0260405Skin · corrodedL/H WING LOWER PLANK ACCESS HOLE 540FB HAS APPROX .008" DEEP CORROSION PIT ON FLAT HORIZONTAL SURFACE, FWD SIDE @ W.S. 136.676.BLENDED OUT DAMAGED AREA, PERFORMED NDI TO ENSURE COMPLETE DAMAGE REMOVAL, ROTO-PEENED REPAIR AREA AND APPLIED CONVERSION COATING. WOSDR DHL2002806520Skin · crackedFOUND DURING C-CHECK, RT WING O/B LEADING EDGE LWR SURFACE .375 INCH CRACK STA XFS 597.000. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER PER EO DHL020608, DWG EO3104 EO SEMAN2002693.SDR P5CA0200688Panel · crackedCRACK 15" LONG FOUND RH WING UPPER SKIN LE FIXED PANEL AT WS 834 TO WS 862. PANEL SHOWS 15 X 30 IN. SQ AREA DELAMINATED. LEADING EDGE FIXED PANEL AT WS 834 TO WS 862 REMOVED & NEW PANEL INSTALLED IAW SRM 51-10-01, PG 8, SECT 6, PARA A-B-C. ALSO SRM 51-30-02.SDR JGV2002F00006Panel · damagedPERFORMING FASTENER LEAKAGE REPAIR ON THE RIGHT WING LOWER REMOVABLE PLANK AND DISCOVERED AND INCORRECT FASTENER LOCATED IN THE FORWARD/INBOARD CORNER OF THE PLANK. UPON REMOVAL OF THE FASTENER, THE MECHANIC DISCOVERED THE FASTENER TO BE INCORRECT IN LENGTH ASDR JGV2002F00005Fastener · wrong partLEAKING FASTENERS LOCATED ON THE RIGHT WING LOWER SURFACE REMOVABLE PLANK, CAME UPON INCORRECT FASTENER INSTALLED. FASTENER WAS A 6 MM DIAMETER RATHER THAN A 5 MM DIAMETER AND SHORT IN LENGTH. FOUND THAT NUTPLATE, LOCATED INSIDE WING FUEL TANK, WAS MISSING SDR UPS02838711Skin · crackedINSPECTION TYPE:C2, RIGHT WING CENTER LEADING EDGE LOWER SKIN IS CRACKED INBOARD OF XW408. STOP-DRILLED CRACKED, NDT VERIFIED CRACK TERMINATES AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087 FIG 1 APPX C.SDR DHL2002806510Panel · delaminatedDURING C-CHECK FOUND RT WING T/E UPPER PANEL SKIN DELAMINATED STA XA 681.000-613.000. REMOVED AND REPLACED PANEL PER SRM 51-3-0 PG 1.SDR DHL2002806503PanelDURING C CHECK FOUND L/H WING T/E LWR PANEL EXTERNAL SKIN DELAMINATED BETWEEN XF 339.000 TO XF 409.000.REMOVED AND REPLACED DELAMINATED PANEL PER SRM 51-1-21 PG 7.SDR DHL2002806502PanelDURING C CHECK FOUND R/H WING LWR PANEL EXTERNAL SKIN DELAMINATED (STA XF 339.000-409.000)REMOVED AND REPLACED EXTERNAL SKIN PANSL PER SRM 52-3-0 PG 1.SDR DHL2002806518Skin · damagedDURING C-CHECK, FOUND RT WING T/E UPPER SKIN DEFECT XW 761.695. REMOVED DAMAGED SKIN PANEL. FABRICATED AND INSTALLED NEW SKIN PANEL PER EODHL 020601, EO3082, EO SEMAN2002679.SDR QXEA0201360Skin · chafedCKB - LEFT HAND SIDE LEADING EDGE CHAFED AND INBOARD LOWER SIDE OF MID SLAT, INBOARD CHAFED AT WS 199.66. REPAIRED IAW WVAC EO 610R-57-4033 AND HORIZON AIR EA R-57-05.SDR DHL2002806501Panel · delaminatedDURING C CHECK FOUND R/H WING T/E LWR PANEL DELAMINATED.REMOVED AND REPLACED R/H WING LWR PANEL FROM STA XF219.000-339.000, PER SRM 51-3-0 PAGE 4.SDR DHL2002806511Panel · delaminatedDURING C-CHECK FOUND RT WING T/E LWR PANEL INNER AND EXTERNAL SKIN DELAMINATED BETWEEN XW 5.000 TO XW 33.000. REMOVED AND REPLACED DELAMINATED PANEL PER SRM 51-3-0 PG 7 AND SRM 51-31 PG 1.SDR GTIA020803Panel · crackedFTW - FOUND LEFT WING LOWER L/E PANEL 1166C APPROX 2 INCH CRACK AND TOOL MARKS ON SIN, BARE METAL ON BACK. DAMAGE CUT OUT, FORMED DOUBLER REPAIR AND FILLER. INSTALLED DOUBLER REPAIR AND FILLER. (M)SDR GTIA020839Panel · delaminatedFTW - FOUND LEFT WING UPPER SURFACE PANEL DELAMINATED NEXT TO INBOARD SPOILER. REMOVED PANEL. LOCATED AND DRILLED NEW PANEL. INSTALLED PANEL. (M)SDR GTIA020858Skin · dentedFTW - FOUND RIGHT WING HAS DENT/DAMAGE AT OUTER SKIN FUELING PANEL 1249C. STOP DRILLED CRACK FOUND IN DENT. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)SDR GTIA020848Panel · delaminatedFTW - FOUND LOWER WING SURFACE TRAPEZOID (SHAPE) PANEL DELAMINATED NEXT TO MLG WHEEL. REPAIRED RIGHT LOWER WING TRAPEZOID PANEL. (M)SDR GTIA020847Panel · delaminatedFTW - FOUND LEFT LOWER WING SURFACE TRAPEZOID (SHAPE) PANEL DELAMINATED NEXT TO MLG WHEEL. REPAIRED LEFT LOWER WING SURFACE TRAPEZOID PANEL. (M)SDR GTIA020878Panel · damagedFTW - FOUND RIGHT WING HAD DENT/DAMAGE AT OUTER SKIN FUELING PANEL. STOP DRILLED CRACK FOUND IN DENT. FABRICATED DOUBLER. INSTALLED DOUBLER. (M)SDR UPS02838732Skin · crackedINSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN IS CRACKED AT XFS 360.25. STOP-DRILLED CRACK, NDT VERIFIED STOPDRILLS TERMINATES CRACK. INSTALLED CONICAL WASHERS, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-7767-A AND SRM 51-1-26.SDR SIMA200217321Skin · gougedLEFT NR 1 LEADING EDGE GOUGED 11 INCH INBOARD OF LANDING LIGHT LENS COVER. BLENDED GOUGE, PERFORMED NDT, NO DEFECTS. ACCEPTED AS IS IAW MFG GST.SDR DHL2002745502Skin · corrodedDURING C-CHECK, LT WING LWR WING SKIN AT STR 9 FROM WING STA 519 TO STA 421.50 IS CORRODED. REMOVED CORROSION ON LT WING LWR IN SPAR SKIN, FOUND TO BE BEYOND ALLOWABLE LIMITS IAW B-727 SRM 57-30-1 FIG 1. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DWG FSDR OZI2002F00000Skin · chafedDURING SCHEDULED INSPECTION CHECK, WING LOWER SURFACE OF BOTH THE LT AND RT WING SKINS, WERE SEVERLY CHAFED AT EACH FLAP TRACK FAIRING. ALL THE DAMAGE APPEARS TO BE CAUSED BY CONTACT BETWEEN THE WING LOWER SKIN AND THE (BLADE SEAL), WHICH IS ATTACHED TO THE ESDR ASAA0270007Skin · damagedSEA - DURING C-CHECK, THE RIGHT WING FAIRING OUTBOARD BONDING JUMPER ATTACHMENT SCREW HOLE WAS ENLARGED. REPAIRED SKIN PER EA 5750-01696. (M)SDR GTIA020760Panel · delaminatedFTW - FOUND LEFT TRAPEZOID PANEL DELAMINATED, LEFT WING. REMOVED DELAMINATED PANEL. REPAIRED LEFT TRAPEZOID PANEL USING 181 GLASS CLOTH. INSTALLED TRAPEZOID PANEL. (M)SDR AALA20020921Skin · crackedTUL - FOUND 3 INCH CRACK IN FIXED LEADING EDGE SKIN ABOVE NR 8 SLAT TRACK. REPAIRED CRACK PER SRM 57-01 FIG 3 SHEET 2 PAGE 8. (M)SDR COMA0260341Skin · crackedCRACK FOUND ON LT LOWER WING PLANK AT PANEL 540CB.REPAIRED I/A/W 601R-57-21-030.SDR COMA0260340Skin · crackedCRACK FOUND ON RT LOWER WING PLANK AT PANEL 650AB.REPAIRED I/A/W 601R-57-21-030.SDR COMA0260339Skin · crackedCRACK FOUND ON RT LOWER WING PLANK AT PANEL 640EB.REPAIRED I/A/W 601R-57-21-030.SDR COMA0260338Skin · crackedCRACK FOUND ON LT LOWER WING PLANK AT PANEL 550CB.REPAIRED I/A/W 601R-57-21-030.SDR COOSDR020168Panel · delaminatedRIGHT WING TRAILING EDGE LOWER FIX PANEL OUTER SKIN DELAMINATED AND HONEYCOMB CORE CORRODED.SDR COOSDR02132Skin · crackedLEFT WING, UPPER SURFACE, TRAILING EDGE SKIN AT XRS 267.0 INCHES, CRACKED.SDR COOSDR02104Panel · delaminatedLEFT WING, OUTER WING TRAILING EDGE, UPPER FIXED PANEL DELAMINATED.SDR COOSDR02105Skin · corrodedRIGHT WING, LOWER SKIN PANEL, INBOARD BOOST PUMP-CUTOUT, CORRODED.SDR COOSDR02124Panel · delaminatedLEFT WING, TRAILING EDGE LOWER PANEL WITH DELAMINATION.SDR COOSDR02122Panel · delaminatedRIGHT WING MAIN LANDING GEAR TRAILING EDGE UPPER PANEL WITH DELAMINATION.SDR COOSDR02121Panel · delaminatedLEFT WING, TRAILING EDGE UPPER PANEL WITH DELAMINATION.SDR COOSDR02120Panel · delaminatedLEFT WING, MAIN LANDING GEAR PANEL WITH DELAMINATION.
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