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 IXXA0400066SSkin · dentedDURING A ROUTINE C-CHECK INSPECTION, FOUND DENTS ON RT WING STATION 660. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1 ALSO REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER 57-2-1 FIG 24 PG 15. CLEANED, TREATED AND PRIMED AREA IAW SRM 51SDR AALA20040503Skin · corrodedTUL LEFT HAND UPPER WING SKIN PANEL NUMBER 2 HAS A CRACK FROM FASTNER AT RIB 4, INBOARD FASTNER THIRD ROW AFT OF JOINT. CRACK LENGTH IS 0.821 AND 0.255 AT A DEPTH OF 0.167. INSTALLED DOUBLER PER AIR BUS DRAWING R57340132. CRACK REPAIRED PER ESO 30595 DATED 0SDR 04FDEA01128Panel · missingPANEL ON TOP OF RIGHT WING MISSING. REPLACED WING PANEL USING APPROVED PARTS AND METHODS USING EA 1-5710-78268. PART NUMBER OF PANEL INSTALLED IS ARC0629-502 AND IS INK-STAMPED ACCORDINGLY REF MM CHAP 51 SRM. OK FOR SERVICE. INST ON A/C ONLY, NO REMOVAL OSDR UIEA200400072Skin · corrodedFOUND WING TOP SIDE SKIN CORROSION WSTA 440.62 STRINGER 19. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400075Skin · corrodedFOUND LEFT WING TOP SIDE SKIN CORRODED WSTA 1392 STRINGER 15. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400076Skin · corrodedFOUND LEFT WING LOWER SKIN CORROSION AROUND SURGE TANK SUMP DRAIN VALVE AT WS 1487. CORROSION BLENDED OUT AND REPAIRED AS PER FAA FORM 8110-3 DATED 19 JAN 2004, COPY ATTACHED FOR DETAILS OF HFEC INSPECTION REF COPY OF ATTACHED SJC A00064. (M)SDR UIEA200400073Skin · corrodedFOUND LEFT WING TOP SIDE SKIN CORROSION WS 1434 STRINGER 13. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400071Skin · corrodedFOUND LEFT WING TOP SIDE SKIN CORROSION WSTA 697 STRINGER 27. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400074Skin · corrodedFOUND LEFT WING TOP SIDE SKIN CORRODED WSTA 1454 STRINGER 15. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1. AREA WAS REPROTECTED AND PRIMER APPLIED IAW SRM 57-30-01. (M)SDR UIEA200400080Angle · crackedFOUND RT WING T/E UPPER FIXED PANEL LONGITUDINAL SUPPORT BEAM FORWARD L-ANGLE CRACK AT WBL 130.0. REPLACED CRACKED SUPPORT ANGLE WRT SRM 51-30-02. (M)SDR AUS20040291Skin · corroded(AUS) WING STRUCTURE CONTAINED LEVEL 3 CORROSION IN THE FOLLOWING AREAS: CORROSION FOUND ON FORWARD FACE OF FORWARD MAIN SPAR AT RIB STATION 129752. ACCESS PANEL Z536FB MOUNTING FLANGE HAD EVIDENCE OF SURFACE AND DEEPER CORROSION AT RIB 11974-12795. FORWARD FSDR DHL2004803544Skin · corrodedLT WING OUTBOARD L/E INNER SECTION CORRODED, STA XFS 710.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-1, DWG V4SDR DHL2004803540Skin · corrodedOUTER PLATING CORROSION DAMAGE TO RT INNER WING CENTER L/E SLOT UPPER SIDE AROUND STA XFS 422.750 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DSDR DHL2004803543Skin · corrodedLT WING OUTBOARD L/E INNER SECTION CORRODED, STA XW 485.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR. REMOVED FASTENERS. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. TRIMMED OUT DAMAGED SECTION IAW ED EDV43-6, DWG V43SDR DHL2004803542Skin · corrodedRIGHT WING CTR L/E UPPER SURFACE SHOWS CORROSION AT STA XW 257.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW ED EDV43-7, DWG V43-R07. REMOVED FASTENERS IAW SRM 51-1-21 PG 1, SRM 51-1-20D, SRM 51-3-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18, FOUND OUSDR DHL2004803537Skin · corrodedRT WING CTR L/E EXTERIOR SURFACE SHOWS CORROSION AT STA. XW 257.500. PERFORMED MAJOR REPAIR IAW ED NR EDV43-5, DWG V43-R05. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-SDR DHL2004803536Skin · corrodedLT WING OB L/E OUTER SECTION CORRODED, STA. XFS 710.000. REMOVED FASTENERS IAW SRM 51-1-21 PG.1, SRM 51-1-20D PG. 9, SRM 51-3-0 PG.1. REMOVED CORROSION IAW SRM 51-1-8 PG. 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG.9. TRIMMED OUT DAMAGED SECTION IAW ED EDV4SDR UIEA200400059Skin · corrodedFOUND LT WING TOP SKIN CORROSION WS 1280 STRINGER 14. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M)SDR UIEA200400061Skin · corrodedFOUND LEFT WING TOP SKIN CORROSON WS 323.82.00 STRINGER 27. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M)SDR UIEA200400058Panel · corrodedFOUND LEFT WING STATION 715, WBL 433, BULGE ON THE T/E F/G PANEL RABBET AREA AT REAR SPAR WING TOP SKIN. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPROTECTED AND PRIMER APPLIED IAW 57-30-01. SDR UIEA200400057Panel · corrodedFOUND LEFT WING STATION 715, WBL 433, BULGE ON THE T/E F/G PANEL RABBET AREA AT REAR SPAR WING STOP SKIN. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPORTECTED AND PRIMER APPLIED IAW 57-30-01.SDR UIEA200400060Skin · corrodedFOUND LEFT WING TOP SKIN CORROSION WS 1280 STRINGER 18. SKIN CORROSION WAS BLENDED OUT WITHIN LIMITS OF SRM 57-30-01 FIG 1 AREA WAS REPROTECTED AND PRIMED IAW SRM 57-30-01. (M)SDR COMA0460289Skin · crackedCRACK INDICATION NOTED AT RIGHT HAND LOWER WING PLANK ACCESS PANEL CUTOUT 650 AB. REPAIRED IN ACCORDANCE WITH REO 601R-57-21-030.SDR AALA20040492Skin · corrodedTUL - TWO INCH BY FOUR INCH AREA OF CORROSION ON RIGHT HAND LOWER WING SKIN UPPER SURFACE AT NUMBER NINE SLAT TRACK OPENING. CORROSION HAS DEPTH OF 50+ PERCENT. REPAIRED NUMBER NINE SLAT TRACK OPENING LOWER WING SKIN PER ESO 40-572000-3322 DATED 4/21/2004.SDR AALA20040491Skin · corrodedTUL - TWO INCH BY FOUR INCH AREA OF CORROSION ON RIGHT HAND LOWER WING SKIN UPPER SURFACE AT NUMBER 10 SLAT TRACK OPENING. CORROSION HAS A DEPTH OF 50 PLUS PERCENT. REPAIRED NUMBER 10 SLAT TRACK OPENING LOWER WING SKIN PER ESO 40-572000-3322 DATED 4/21/2004SDR ASAA0480325Access Panel · corrodedOKC - DURING HV CHECK, FOUND LOEWR SRFC OF FUEL ACCESS PANEL 1454 IS CORRODED. REMOVED AND REPLACED FUEL ACCESS PANEL PER SRM 51-22-2A. (M)SDR ASAA0480324Access Panel · damagedOKC - DURING HV CHECK, FOUND FUEL ACCESS PANEL 1355C HAS ONE ELONGATED HOLE. REMOVED AND REPLACED FUEL ACCESS PANEL PER SRM 51-22-2A. (M)SDR ASAA0480326Access Panel · corrodedOKC - DURNG HV CHECK, FOUND FRETTING CORROSION ON FUEL ACCESS PANEL 1456C. REMOVED AND REPLACD FUEL ACCESS PANEL PER 51-22-2A. (M)SDR UIEA200400056Panel · corrodedFOUND LEFT WING TOP SKIN FIXED T/E FIBERGLASS PANEL BULGING AT RABBET AREA AFT OF REAR SPAR BETWEEN WBL 198.6 TO 204.6. CORROSION FOUND ON WING TOP SKIN AFT OF REAR SPAR CORROSION BLENDED OUT WITHIN LIMITS OF SRM 57-30-01. AREA REPROTECTED AND PRIMER APPLIEDSDR UIEA200400053Cap · crackedFOUND RT WING LEADING EDGE NOSE CAP AT LES 1042 FOUND 4.25 INCH LONG SPANWISE CRACK PROPERGATED FROM WING ANTI-ICE DUCT. RIGHT WING LEADING EDGE NOSE BEAM CRACKED WEB REPAIRED AS PER FAA FORM 8110-3 REF SJC NR A00063. (M)SDR CA040709005Skin · crackedUPPER SKIN ON RT WING FOUND TO HAVE HAIR LINE CRACKS AT STA 174.50 AND STA 160.50 ONE RIVET FORWARD OF STRINGER IMMEDIATELY FORWARD OF MAIN SPAR.SDR ASAA0480291Panel · corrodedOKC - DURING HV CHECK, FOUND FUEL PANEL IS CORRODED. REPLACED PANEL PER SRM 51-22-2A. (M)SDR AWXA200400444Skin · delaminatedUPPER SURFACE OF RT FIXED WING LEADING EDGE DELAMINATED AT WS 421. MAINTENANCE REMOVED DAMAGED AREA OF SKIN ON UPPER SURFACE OF R/H FIXED WING LEADING EDGE AT WS 421; FABRICATED A FILLER, NEW SECTION OF SKIN, AND A SPLICE PLATE; INSTALLED REPAIR PART IAW AWA ESDR DHL2004803534Panel · corrodedRT WING L/E SLANT PANEL UPPER CAP CORRODED STA XFS 57.500 - XFS 82.500 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 PG 11. REMOVED CORRODED SLANT PANEL UPPER CAP ISDR AWXA200400376Skin · delaminatedRIGHT FIXED WING LEADING EDGE UPPER SURFACE DISBONDED AT WS 397. MAINTENANCE REMOVED DAMAGE ON RIGHT FIXED WING LEADING EDGE UPPER SURFACE WS 397 AND PERFORMED BOND REPAIR PER AWA ER 19-5700-00012-DD4 & 757-200 SRM 51-70-17.SDR P5CA0401074Panel · damagedLT WING ACCESS PANEL OB AND FWD OF NR 4 FLAP TRACK FIX FAIRING 3 X 3 INCH HOLE. REMOVED DAMAGED ACCESS PANEL FOR REPAIRS, INSTALLED SERVICEABLE PANEL IAW SRM.SDR CA040414002Skin · cracked(CAN) CRACKING OF RT WING LEADING EDGE SKIN AT STA 160.50 AND 174.50 FROM RIVETS 1 RIVET FORWARD OF STRINGER AHEAD OF THE SPAR. REVIEW OF AIRCRAFT RECORDS DID NOT SHOW ANY RECENT HISTORY OF HARD LANDINGS.SDR SWAA041051Skin · crackedDURING SCHEDULED C2 CHECK, FOUND RIGHT WING L/E SKIN AT WS 213, CRACKED. REPAIRED L/E SKIN PER ER.SDR CALA0400353Skin · crackedINSPECTION FOUND A 1.5 INCH CRACK IN LEFT WING SKIN JUST FORWARD OF PANEL 1196C UPPER LEFT WING AREA, STA XOS 286. REPAIRED IAW ECRA 5720-01946.SDR ASAA0480254Access Panel · corrodedOKC - DURING FUEL ACCESS PANEL UPPER WING NR 1409 MATTING FLANGE PITTED AND CORRODED. REMOVED AND REPLACED PANEL NR 1409 IAW MD80 SRM 51-22-2A. (M)SDR ASAA0480255Panel · corrodedOKC - DURING LEFT WING PANEL 1367 HAS CORROSION. REMOVED, ORDERED, AND REPLACED PANEL IAW MD80 SRM 51-22-2A. (M)SDR ASAA0480257Panel · corrodedOKC - FOUND LEFT WING PANEL 1472C CORRODED. REMOVED, ORDERED, AND REPLACED PANEL IAW MD80 SRM 51-22-2A. (M)SDR ASAA0480256Panel · corrodedOKC - FOUND LEFT WING PANEL 1361 HAS CORROSION. REMOVED, ORDERED, AND REPLACED PANEL 1361 IAW MD80 SRM 51-22-2A. (M)SDR ASAA0480258Access Panel · corrodedDURING HV CHECK, FUEL ACCESS PANEL NR 1414 IS CORRODED. REMOVED AND REPLACED ACCESS PANEL PER SRM 51-22-2A. (M)SDR ASAA0480259Access Panel · corrodedDURING HV CHECK, FUEL ACCESS PANEL NR 1410 IS CORRODED. REMOVED AND REPLACED ACCESS PANEL PER SRM 51-22-2A. (M)SDR IXXA0400064SPanel · corrodedDURING ROUTINE C-CHECK INSPECTION RT WING INBD L/E SLANT PANEL UPPER SKIN SURFACE CORRODED, STA XCW 69.000 AND XFS 207.000. REPAIR ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1, FAX TIN-N 043, BOEING MESSAGE DATE 03/31/2004. REMOVED CORROSISDR 04FDEA00833Panel · corrodedRIGHT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH SEVERAL BULGES. COMPLIED WITH FEDEX EA 1-5710-76644 - WINGS - LEFT AND RIGHT HAND WING AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR.SDR 04FDEA00832Panel · corrodedLEFT WING UPPER SURFACE FIXED T/E PANELS FWD OF OUTBOARD AILERON FOUND WITH BULGE. COMPLIED WITH FEDEX EA 1-5710-76644. LEFT AND RIGHT HAND WING - AFT UPPER SPAR CAP AFT TANG CORROSION REMOVAL AND REPAIR.SDR ASAA0480210Panel · corrodedOKC - FOUND HV CHECK, RIGHT WING LOWER FUEL PANEL 1460C IS CORRODED. REPLACED PANEL NR 1460C PER MM 28-40-02 AND SRM 51-30-5. (M)SDR ASAA0480211Panel · corrodedOKC - FOUND WING RIGHT LOWER FUEL PANEL NR 1454C CORRODED. ORDERED AND REPLACED WITH NEW PANEL IAW MD80 SRM 51-22-2A. (M)
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