JASC 5730

Service difficulty reports · 27,262

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 IPXA2016032100983Skin · corrodedINSPECTION TYPE:C3, CORROSION, SKIN, BETWEEN WS 724 AND WS 807, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.Mar 11, 2016 · N578UP · Boeing 74745ESDR IPXA2016032100981Skin · corrodedINSPECTION TYPE:C3, CORROSION SKIN, BETWEEN WS 944 AND WS 972, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR. REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.Mar 11, 2016 · N578UP · Boeing 74745ESDR IPXA2016032100980Skin · corrodedINSPECTION TYPE:C3, CORROSION, SKIN , BETWEEN WS 834 AND WS 858 , RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR, REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.Mar 11, 2016 · N578UP · Boeing 74745ESDR DALA2016031201889Skin · corrodedCORROSION WAS FOUND ON FASTENER HOLES COMMON TO THE LT LOWER ACCESS DOOR CUTOUT, AT THE XRS 199- 200 AND BETWEEN STR 12 AND 15. CORROSION WAS REPAIRED IAW ER/A 543177-14AD, REV ORIG.Mar 11, 2016 · N993DL · Doug MD88SDR DALA2016031201888Skin · corrodedCORROSION WAS FOUND ON FASTENER HOLES COMMON TO THE RT LOWER ACCESS DOOR CUTOUT, AT THE XRS=191-211 BETWEEN STR 12 AND 15. CORROSION WAS REPAIRED IAW ER/A 543177-14AD, REV ORIGINAL.Mar 11, 2016 · N993DL · Doug MD88SDR IPXA2016032100979Skin · corrodedINSPECTION TYPE:C3, CORROSION-SKIN, WS 1028, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR REPAIR IAW SRM 57-20-01-2R, REPAIR 1, REV 35.01.Mar 10, 2016 · N578UP · Boeing 74745ESDR IPXA2016032100978Skin · corrodedINSPECTION TYPE:C3, CORROSION, SKIN , WS 655, RT WING UPPER INSPAR SURFACE NEAR FRONT SPAR REPAIR IAW SRM 57-20-01-2R. REPAIR 1, REV 35.01.Mar 10, 2016 · N578UP · Boeing 74745ESDR MTNA20160314001Skin · chafedFLAP FAIRING 553AB CHAFED INTO WING. PERFORMED BLENDOUT, SMOOTHING OF CHAFED AREAS AT 553AB IAW SRM 512158-02-001-A01 AND SRI CE-861/16-27126. ALODINED IAW SRM 512117-02-001-A01. REQUIRES NDT. PERFORMED EDDY CURRENT OF AFFECTED AREA IAW NDTM 51-00. NO CRAMar 10, 2016 · N914FX · Aerosp ATR42300SDR SWAA2016041550958Skin · crackedRIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 237.5, AFT OF REAR SPAR. REPAIRED SKIN IAW EA.Mar 9, 2016 · N648SW · Boeing 7373H4SDR SWAA2016041550957Skin · crackedLEFT WING UPPER SKIN CRACKED AT FASTENER HOLE AT RSS 255 AFT OF REAR SPAR. REQUIRED SKIN IAW EA.Mar 9, 2016 · N648SW · Boeing 7373H4SDR SWAA2016041450904Skin · crackedRIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 264, AFT OF REAR SPAR. REPAIRED SKIN IAW ER & EA.Mar 9, 2016 · N648SW · Boeing 7373H4SDR SWAA2016041450903Skin · crackedRIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 253, AFT OF REAR SPAR. REPAIRED SKIN IAW ER & EA.Mar 9, 2016 · N648SW · Boeing 7373H4SDR SWAA2016041450902Skin · crackedRIGHT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 249, AFT OF REAR SPAR. REPAIRED SKIN IAW ER & EA.Mar 9, 2016 · N648SW · Boeing 7373H4SDR SWAA2016041450901Skin · crackedLEFT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 269, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.Mar 9, 2016 · N648SW · Boeing 7373H4SDR SWAA2016041450900Skin · crackedLEFT WING UPPER SKIN CRACKED, AT FASTENER HOLE AT RSS 268, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.Mar 9, 2016 · N648SW · Boeing 7373H4SDR SWAA2016041450899Skin · crackedLEFT WING UPPER SKIN CRACKED AT FASTENER HOLE, AT RSS 251, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.Mar 9, 2016 · N648SW · Boeing 7373H4SDR SWAA2016041450898Skin · crackedLEFT WING UPPER SKIN CRACKED, AT FASTENER HOLE AT RSS 239, AFT OF REAR SPAR. REPAIRED SKIN IAW EA & ER.Mar 9, 2016 · N648SW · Boeing 7373H4SDR COEA2016030903819Panel · corrodedHEAVY CHECK COE & MINOR REPAIR. RT WING, PANEL 623GT, HAS LEVEL 2 SURFACE CORROSION ON EDGE NEXT TO RUBBER SEAL. REPLACED PANEL WITH OEM PART.Mar 9, 2016 · N819FX · Aerosp ATR72212SDR ASOA2016030914639Access Panel · corrodedLOWER WING PLANK ACCESS HOLE 650AB HAS CORROSION. COMPLIED WITH ECTC REO 600-57-81 C/W IAW REO 601R-57-21-030, REV L. BLENDED AREA WHERE PITTING CORROSION WAS STILL PRESENT, IAW EO 600-57-81. COMPLIED WITH ECTC EO 600-57-81 C/W REV K.Mar 9, 2016 · N855AS · Cndair CL6002B19SDR FDEA201603090869Skin · crackedLEFT LOWER WING SKIN OTBD AFT CORNER OF SLAT TRACK 10 HAS .200 IN CRACK. TRIMMED OUT CRACK & INSTALLED FILLER & DOUBLER.Mar 9, 2016 · N303FE · Doug MD1030FSDR DALA2016031001827Skin · crackedCRACK ON FIXED L/E LOWER SURFACE LT WING BS XRS=218. FIXED L/E LOWER LT WING WAS REPAIRED IAW ER/A 380953-14MA, REV A.Mar 9, 2016 · N993DL · Doug MD88SDR COEA2016030827911Panel · corrodedHEAVY CHECK COE/MAJOR REPAIR: LT UPPER WING OTBD REMOVABLE PANEL HAS LEVEL 2 CORROSION AT RIB 21 NEXT TO VORTEX GENERATOR. REPAIRED IAW SRAS CE-1347/15, 10273, DATED 5/30/2016.Mar 8, 2016 · N911FX · Aerosp ATR42300SDR COEA2016030826911Vortex Gen · corrodedHEAVY CHECK COE/MINOR REPAIR: RT UPPER OTBD WING HAS 2 EA VORTEX GENERATORS WITH LEVEL 2 CORROSION. REPLACED VORTEX GENERATORS WITH OEM PARTS.Mar 8, 2016 · N911FX · Aerosp ATR42300SDR COEA2016030825911Skin · corrodedHEAVY CHECK, COE/MAJOR REPAIR. RIGHT UPPER WING SKIN HAS AREAS OF LEVEL 2 CORROSION AROUND AND UNDER THE VORTEX GENERATORS BETWEEN RIBS 23 AND 29. REPAIR IAW SRAS S572R0357.Mar 8, 2016 · N911FX · Aerosp ATR42300SDR COEA2016030820911Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. LT UPPER WING OTBD PANEL HAS AREAS OF LEVEL 2 CORROSION OTBD OF RIBS 23 - 29 UNDER VORTEX GENERATORS. REPAIRED IAW SRAS S572R0357 10305 DATED 6 3 2016.Mar 8, 2016 · N911FX · Aerosp ATR42300SDR COEA2016030819911Skin Panel · corrodedHEAVY CHECK COE & MAJOR REPAIR. LT UPPER WING OTBD PANEL HAS AREAS OF LEVEL 2 CORROSION ALONG FWD EDGE OF SKIN, BETWEEN RIBS 23 - 26. REPAIRED IAW SRAS S572R0357 10305 DATED 6 3 2016.Mar 8, 2016 · N911FX · Aerosp ATR42300SDR SWAA2016041250814Skin · crackedLEFT WING UPPER SKIN CRACKED AT FASTENER HOLE AFT OF RSS 239. REPAIRED SKIN IAW ER & EA.Mar 8, 2016 · N656SW · Boeing 7373H4SDR SWAA2016032850267Skin · crackedRIGHT WING UPPER SKIN COMMON TO SPLICE PLATE ON TE CRACKED AT RSS 239.5. REPAIRED SKIN IAW ER & EA.Mar 8, 2016 · N656SW · Boeing 7373H4SDR SWAA2016031449902Skin · crackedRIGHT WING REAR SPAR FASTENER HOLE CRACKED, COMMON TO UPPER SKIN & CHORD AT RSS 293. REPAIRED SKIN IAW EA & DWG.Mar 8, 2016 · N656SW · Boeing 7373H4SDR SWAA2016041851027Skin · crackedLEFT WING INBD LEADING EDGE SKIN CRACKED AT 208.00. REPAIRED SKIN IAW EA.Mar 7, 2016 · N394SW · Boeing 7373H4SDR SCNA20160307032Skin · damagedON WALK AROUND, FOUND PANEL 571FB ON LT WING LOWER SURFACE, HAVE ALUMINUM FOIL MESH PEELING. PERFORMED REPAIR ON PANEL 571FB IAW SRM. OK FOR SERVICE.Mar 7, 2016 · N711SY · Boeing 73773VSDR DALA2016030801753Access Panel · corrodedCORROSION AT FUEL ACCESS PANEL 2302C ON COUNTER SKIN. ACCESS IS OUT LIMITS AND IT WAS REPLACED IAW SRM 51-22-2A.Mar 7, 2016 · N904DE · Doug MD88SDR DALA2016030801752Access Panel · corrodedCORROSION ON COUNTERSUNK AT FUEL ACCESS PLATE NR 1307C. CORROSION ON COUNTERSINK WAS REMOVED AND MEASURED 3 HOLES ADJACENT WERE FOUND OUT LIMITS WITH 0.664", 0.671" AND 0.688". THEREFORE IT IS OUT LIMITS AND IT WAS REPLACED IAW SRM 51-22-2A.Mar 7, 2016 · N904DE · Doug MD88SDR FDEA201603070857Skin · crackedDURING ACCOMPLISHMENT OF HFEC INSPECTION ON LT WING FIXED LE, SKIN ADJACENT TO CUT OUT & ACCESS DOORS, FOUND CRACK INDICATION AT NR 10 SLAT TRACK, INBD SIDE CORNER NR 13, APPROX 0.20' IN LENGTH. REPAIRED CARRIED OUT AT LT WING FIXED LE SKIN CUT OUT AT NR 10 SMar 7, 2016 · N607FE · Doug MD11FSDR SWAA2016040150507Skin · crackedLEFT WING UPPER SKIN CRACKED AT RSS 217, APPROX 3.5 INCHES FWD FROM TE. REPAIRED SKIN IAW ER & EA.Mar 6, 2016 · N633SW · Boeing 7373H4SDR SWAA2016032850247Skin · crackedLEFT WING UPPER SKIN CRACKED AT TE, BETWEEN RSS 254 - 269. REPAIRED SKIN IAW ER & EA.Mar 6, 2016 · N633SW · Boeing 7373H4SDR DALA2016030701704Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AT WING ACCESS PLATE NR 1464C. CORROSION WAS REMOVED, COUNTERSINKS WERE MEASURED AND MAXIMUN DIAMETER ALLOWABLE IS .532" AND WAS FOUND 1 COUNTERSINK OUT OF LIMITS MEASURE .568", THEREFORE HOLE AND COUNTERSINK WAS REWORKMar 6, 2016 · N993DL · Doug MD88SDR DALA2016030701703Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AT WING ACCESS PLATE NR 1367C. CORROSION WAS REMOVED, COUNTERSINKS WERE MEASURED, MAXIMUN DIAMETER ALLOWABLE IS .532" AND WERE FOUND 2 COUNTERSINK OUT OF LIMITS MEASURED .551" AND .554" THEREFORE HOLES AND COUNTERSINKS Mar 6, 2016 · N993DL · Doug MD88SDR DALA2016030701701Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE 1363C. CORROSION WAS REMOVED, MEASURED SETTLEMENT WAS ACCOMPLISHED, ORIGINAL THICKNESS IS .150", REMAINING THICKNESS IS .137" THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED, MAXIMUN Mar 6, 2016 · N993DL · Doug MD88SDR DALA2016030701700Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE NR 1472C. CORROSION WAS REMOVED, MEASURED SETTLEMENT AREA WAS ACCOMPLISHED ORIGINAL THICKNESS IS .150", REMAINING THICKNESS .138" THEREFORE IT IS WITHIN LIMITS, COUNTERSINK WERE MEASURED MAXIMUMMar 6, 2016 · N993DL · Doug MD88SDR DALA2016030701699Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA AT WING ACCESS PLATE NR 1478C. CORROSION WAS REMOVED, MEASURED SETTLEMENT WAS ACCOMPLISHED ORIGINAL THICKNESS IS .150", REMAINING THICKNESS IS .138", THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MMar 6, 2016 · N993DL · Doug MD88SDR DALA2016030701698Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE 1377C. CORROSION WAS REMOVED, MEASURED SETTLEMENT AREA WAS ACCOMPLISHED, ORIGINAL THICKNESS IS .150" REMAINING THICKNESS IS .140", THEREFORE IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MAXMar 6, 2016 · N993DL · Doug MD88SDR DALA2016030701697Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1414C. CORROSION WAS REMOVED, MEASURED ON SETTLEMENT WAS ACCOMPLISHED, ORIGINAL THICKNESS IS .180" REMAINING THICKNESS IS .172" THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MINMar 6, 2016 · N993DL · Doug MD88SDR COEA2016030512819Skin Panel · corrodedHEAVY CHECK COE & MINOR REPAIR. LT WING UPPER SURFACE PANEL 523GT, SURFACE CORROSION ON EDGE NEXT TO RUBBER SEAL. REPLACED WITH OEM PART.Mar 5, 2016 · N819FX · Aerosp ATR72212SDR COEA2016030510819Landing · damagedHEAVY CHECK COE & MAJOR REPAIR. FRETTING DAMAGE ON LANDING FOR PANEL 622CT. REPAIR IAW SRAS DO TS-531 06 3474 ISSUE E DATED 4 5 2016.Mar 5, 2016 · N819FX · Aerosp ATR72212SDR IPXA2016040501673Skin · corrodedINSPECTION TYPE:3C, LT WING UPPER SKIN CORRODED ALONG T/E XORS1042. REPAIRED NOTED CORROSION BTEWEEN BS 1057-1067 IAW EA 011-5710-01-A6174, REV IR AND EO 5730-60295-A.Mar 5, 2016 · N282UP · Doug MD11FSDR DALA2016030701693Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA OF WING ACCESS PLATE NR 2302C. CORROSION WAS REMOVED, MEASURED SETTLEMENT AREA WAS ACOMPLISHED ORIGINAL THICKNESS IS .172" THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE ISMar 5, 2016 · N993DL · Doug MD88SDR DALA2016030701691Access Panel · corrodedCORROSION ON COUNTERSINK AND SETTLEMENT AREA AT WING ACCESS PLATE 2301C. CORROSION WAS REMOVED, MEASURE SETTLEMENT WAS ACCOMPLISHED ORIGINAL THICKNESS IS .180" REMAINING THICKNESS IS .172", THEREFORE IT IS WITHIN LIMITS, COUNTERSINKS WERE MEASURED AND MAXIMUMMar 5, 2016 · N993DL · Doug MD88SDR DALA2016030701689Access Panel · corrodedCORROSION ON COUNTERSINK OF WING ACCESS PLATE 1365C. CORROSION WAS REMOVED, COUNTERSINKS WERE MEASURED MAXIMUM DIAMETER ALLOWABLE IS .532 AND FOUND COUNTERSINK OUT OF LIMITS IN .547, THEREFORE HOLE AND COUNTERSINK WERE REWORKED AND MEASURED WITH ID HOLE .330Mar 5, 2016 · N993DL · Doug MD88SDR DALA2016030601678Access Panel · corrodedCORROSION ON COUNTERSINK AT WING ACCESS PLATE 1373 C. CORROSION WAS REMOVED , COUNTERSINKS WERE MEASURED. MAXIMUM DIAMETER ALLOWABLE IS .532" AND WERE FOUND 2 COUNTERSINKS OUT OF LIMITS IN .540" AND .559" THEREFORE HOLES AND COUNTERSINKS WERE REWORKED AND WEMar 5, 2016 · N993DL · Doug MD88
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