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 UALA2013011600270Panel · unsecurePOSSIBLE FUEL LEAK ON LEFT WING. SECURED PANEL 540JB. NO LEAKS NOTED.SDR QXEA2013011400033Access Panel · corrodedLT WING FUEL PANEL LANDING 524AT HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND TO BE WITHIN LIMITS IAW SRM 57-20-35-02-05. ORIGINAL THICKNESS .080" REMAINING THICKNESS .075". ALL BLENDED RIVETS MEASURE MORE THAN .179. VERIFIED BLENDS CRACK FREE IAW NTM SDR QXEA2013011400034Access Panel · corrodedRT WING FUEL PANEL LANDING 624FT HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND WITHIN LIMITS IAW SRM 57-20-35-02-05. ORIGINAL THICKNESS .080" AND .074 REMAINING. ALL BLENDED RIVETS MEASURE MORE THAN .179". PERFORMED HFEC OF BLENDS VERIFIED BLENDS ARE CSDR QXEA2013011400035Access Panel · corrodedRT WING FUEL PANEL LANDING 624ET HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND BLENDED AREAS TO BE IN LIMITS IAW SRM 57-20-35-02-01. ORIGINAL THICKNESS .080" REMAINING .075". ALL BLENDED RIVETS MEASURE MORE THAN .179". PERFORMED HFEC AND VERIFIED BLENSDR QXEA2013011400036Access Panel · corrodedRT WING FUEL PANEL LANDING 624BT HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND BLENDED AREAS TO BE IN LIMITS IAW IAW SRM 57-20-35-02-01. ORIGINAL THICKNESS .080" REMAINING .074". ALL BLENDED RIVETS MEASURE MORE THAN .179". VERIFIED BLENDS ARE CRACK FRSDR QXEA2013011400037Access Panel · corrodedRT WING FUEL PANEL LANDING 624AT HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND BLENDED AREAS TO BE IN LIMITS IAW SRM 57-20-35-02-05. ORIGINAL THICKNESS .080" REMAINING .075". ALL BLENDED RIVETS MEASURE MORE THAN .179". PERFORMED HFEC AND VERIFIED BLESDR QXEA2013011400038Access Panel · corrodedLEFT WING FUEL PANEL LANDING 524BT HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND BLENDED AREAS TO BE IN LIMITS IAW SRM 57-20-35-02-05. ORIGINAL THICKNESS .080" REMAINING .075". ALL BLENDED RIVETS MEASURE MORE THAN .179". VERIFIED BLENDS ARE CRACK FRESDR QXEA2013011400045Access Panel · corrodedRT WING FUEL PANEL LANDING 624CT HAS AREAS OF CORROSION. REMOVED CORROSION AND FOUND BLENDS TO BE WITH IN LIMITS IAW SRM 51-20-35-02-05. ORIGINAL THICKNESS .080" REMAINING THICKNESS .0705". ALL BLENDED RIVETS MEASURE MORE THAN .179". PERFORMED HFEC OF BLENDSSDR QXEA2013011400031Access Panel · corrodedLT WING ACCESS PANEL 524BT HAS LIGHT SURFACE CORROSION ON MATING SURFACE. REMOVED CORROSION, NOMINAL THICKNESS 0., REMAINING THICKNESS 0.110 AND WITHIN LIMITS IAW RD 8/4-57-442. INSPECTED SURFACE IAW RD 8/4-57-442 REPAIR ITEM 3 AND NDT MANUAL 8.2.1.2. MATINGSDR QXEA2013011400030Access Panel · corrodedLT WING ACCESS PANEL 524AT HAS LIGHT SURFACE CORROSION ON MATING SURFACE. REMOVED CORROSION, NOMINAL THICKNESS 0.120" REMAINING 0.110 WITHIN LIMITS IAW RD 8/4-57-442. INSPECTED IAW RD 8/4-57-442, REPAIR ITEMS 3 AND NDT MANUAL 8.2.1.2. MATING SURFACE IS CRACK SDR SWAA2013011611472Plate · crackedWIGGLE PLATE CRACKED AT RIGHT WING PANEL 651GB. REMOVED AND REPLACED REF AMM, AND SRM 51-40-02.SDR A6WA20134644Panel · gougedLEFT BUTE DOOR PANEL 594PB IS GOUGED. REMOVED UNSERVICEABLE PANEL AND INSTALLED SERVICEABLE PANEL IAW CRJ 200 SRM 51-42-06, 51-40-11.SDR IPXA3M76942Skin · corrodedINSPECTION TYPE:4C, CENTER WING UPPER SKIN CORRODED ALONG S10 BETWEEN XCW-101 & XCW-118. REPAIRED CORRODED SKIN IAW STASA EA 011-5730-01-A4428 REV IR AND EO MD11-5730-49658-A.SDR DALA13003049242Skin · corrodedWHILE IN SERVICE, CORROSION WAS FOUND ON THE EXTERNAL SURFACE OF THE LT LOWER WING SKIN PANEL OTBD OF XRS=545.380 AT THE T/E. REPAIR WAS ACCOMPLISHED IAW ER/A 510483-14 SECTION I.SDR USAA2013021500004Access Door · corroded2S CHECK - CORROSION ON LEFT WING LOWER FUEL DOOR 540MD BETWEEN WS 9235 TO WS 9704 & BETWEEN RIB 17 TO RIB 18. REPLACED LEFT WING LOWER FUEL DOOR 540MD IAW A321 SRM 57-27-11.SDR IPXA3M76936Skin · corrodedINSPECTION TYPE:4C, CENTER WING UPPER SKIN CORRODED ALONG S15 BETWEEN STA XCW-81 & XCW-118. REPAIRED CORRODED CENTER WING UPPER SKIN IAW STASA EA 011-5730-01- A4427 REV.IR AND EO MD11-5730-49659-A.SDR IPXA3M76935Skin · corrodedINSPECTION TYPE:4C, CENTER WING UPPER SKIN CORRODED ALONG S15 BETWEEN XCW17 AND XCW-17. REPAIRED CORRODED WING SKIN IAW STASA EA 011-5730-01-A4427, REV IR AND EO MD11-5730-49659.SDR EPUA20130124003Skin · looseRIGHT WING TOP SKIN NEAR L/E HAS LOOSE RIVETS. REPAIRED RT WING IAW SRM 57-23-01, PARA 4 A-C, REV 4.SDR SWAA2013012111680Attach Angle · crackedLOWER WING SKIN TO PANEL ATTACH ANGLE CRACKED ON I/B SIDE FSS 222. REMOVED CRACKED ATTACH ANGLE ON RT WING I/B SIDE FSS 222 AND INSTALLED NEW FABRICATED ATTACH ANGLE IAW SRM 51-40-02-0G-0 PARA 4, 7 AND 9 2656U 18JAN13.SDR QXEA2013011000029Access Panel · damagedLT WING ACCESS PANEL 522BT HAS DAMAGE AROUND FASTENER HOLE AND MISSING PAINT. BLENDED OUT DAMAGE AROUND FASTENER HOLE. NOMINAL THICKNESS 0.225", REMAINING THICKNESS IS 0.220" AND IS WITHIN LIMITS IAW RD 8/4-57-425. PREPPED MISSING PAINT AREAS IAW SRM 51-25-4SDR USAA2013012400019Access Panel · corrodedS2 CHECK - LEVEL 2 GALVANIC CORROSION ON RIGHT WING LOWER FUEL DOOR 640JB BETWEEN RIB 14 TO RIB 15 & BETWEEN S8R TO S11R. REPLACED RIGHT WING LOWER FUEL DOOR 640JB IAW A321 SRM 57-27-11 PB104 & SRM 51-72-11.SDR SWAA2013011611494Door · cracked2 SCREW ON ACCESS PANEL RT WING BETWEEN 2 INNER FLAP ACTUATOR CRACKED IN METAL DOOR. REMOVED AND REPLACED DOOR PER AMM.SDR SWAA2013030813490Skin · crackedRIGHT WING FIXED L/E CRACKED ABOVE NR 4 FLAP NACELLE DOOR. REPAIRED LEADING EDGE PER EA.SDR FDEA201301080036Skin · corrodedLEFT WING LOWER T/E ACCESS 541JB CUT-OUT FORWARD FOUND CORROSION.SDR IPXA3M76932Skin · corrodedINSPECTION TYPE:4C, AREA OF CORROSION ON LT WING UPPER SKIN AT XORS315.9, STRINGER 15 AREA EXCEEDED ALLOWABLE SRM LIMITS AFTER CORROSION REMOVAL. REPAIRED LT WING UPPER SKIN CORROSION STA XORS 315.9 ABOVE S15 IAW STASA EA 011-5730-01-A4431, REV IR AND EO MD11SDR IPXA3M76817Skin · crackedINSPECTION TYPE: 4C, LT WING FIXED L/E SKIN CRACKED AT NR 14 SLAT TRACK CUT OUT. REPAIRED IAW SRM 57-40-02, REPAIR 7, FIG 201.SDR IPXA3M76928Doubler · corrodedINSPECTION TYPE: 4C, RT WING FIXED L/E LOWER SACRIFICIAL DOUBLER AT XFS925 IS CORRODED. REPAIRED RT WING FIXED L/E LOWER SACRIFICIAL DOUBLER AT XFS925 REF STA SA EA 011-5710-01-A4423 REV I/R, EO MD11-5710-49721-A AND 8100-9.SDR IPXA3M76891Skin · crackedINSPECTION TYPE:4C, RT WING FIXED L/E SKIN CRACKED AT NR 14 SLAT TRACK CUT OUT. REPAIRED RT WING FIXED L/E SKIN AT NR 14 SLAT TRACK CUT OUT REF SRM 57-40-02, REPAIR 7, FIG 201.SDR IPXA3M76890Skin · crackedINSPECTION TYPE:4C, RT WING FIXED L/E SKIN IS CRACKED AT INBD FWD CORNER OF PANEL 619CB CUT OUT. REPAIRED RT WING FIXED L/E SKIN AT INBD FWD CORNER OF PANEL 619CB CUT OUT REF SRM 57-40-02, REPAIR 7, FIG 202.SDR IPXA3M76796Skin · crackedINSPECTION TYPE:4C, RT WING FIXED L/E SKIN SPLICE STRAP IS CRACKED AT XFS 669. REPLACED RT WING FIXED L/E SKIN SPLICE STRAP AT XFS 669 SRM 51-31-01, PARA 3 AND PAGE 1 AND 36, SRM 51-33-01 PARA 8, PAGE 30.SDR FDEA201301040020Skin · crackedNR 8 SLAT COVE SKIN CRACKED AT OTBD MAIN TRACK. REMOVED NR 8 SLAT COVE SKIN IAW SRM 51-40-02. ROUTED TO FAB SHOP. FABRICATED NEW COVE SKIN ON STAM TRAVELER NR T12/976166. LOCATED AND DRILLED COVE SKIN IAW SRM 51-40-02. TREATED AND PRIMED IAW SRM 51-20-01. SDR IPXA13M76746Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 638. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS636-648 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)SDR IPXA13M76745Doubler · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 613. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS610-616 IAW EO MD11-5730-48222-A. (MAJOR)SDR IPXA13M76744Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 627. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS625-629 IAW EO MD11-5730-48222-A. (MAJOR)SDR IPXA13M76743Doubler · crackedINSPECTION TYPE: 2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 561. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS559-565 IAW EO MD11-5730-48222-A. (MAJOR)SDR IPXA13M76736Doubler · crackedINSPECTION TYPE:2C, RT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 700. REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 698-708 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR).SDR IPXA13M76726Doubler · crackedINSPECTION TYPE: 2C, LT WING L/E INNER BEADED DOUBLER CRACKED NEAR XOS 770. REMOVED EXISTING REPAIR DOUBLER BETWEEN XOS 763-768. INSTALLED NEW REPAIR TO INCORPORATE INTERNAL BEADED DOUBLER DAMAGES BETWEEN XOS 763- 772 IAW SRM 57-40-02, REPAIR 15, FIG 203.SDR IPXA13M76718Doubler · crackedINSPECTION TYPE: 2C, LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 670. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 667-673 IAW SRM 57-40-02, REPAIR 15, FIG. 202. (MAJOR).SDR IPXA13M76676Doubler · crackedINSPECTION TYPE: 2C, LEFT WING BEADED DOUBLER CRACKED NEAR XOS 645. REPAIRED LT WING FIXED L/E INTERNAL BEADED DOUBLER BETWEEN XOS 643-648 IAW SRM 57-40-02, REPAIR 15, FIG 203. (MAJOR)SDR RJEF2013010768201Cover · missingAT THE ARRIVAL OF THE AIRCRAFT AS FLIGHT TAI-9951 FROM SAP TO SAL, IT WAS FOUND THAT COVER 622WB ON PANEL 622AB ON RIGHT WING WAS MISSING. THE AIRCRAFT WAS INSPECTED AND NO OTHER DAMAGE WAS FOUND. AS PER AIRBUS REPAIR APPROVAL REF:70571449/003/2013 AND ENGINSDR SWIA201232666Access Panel · corrodedRIGHT WING ACCESS PANEL 650HB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) CORROSION AT LOWER WING PLANK COMMON TO PANEL 650HB REPAIRED IAW REO.SDR SWIA201232665Access Panel · corrodedRIGHT WING ACCESS PANEL 650BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 650BB REPAIRED IAW REO.SDR SWIA201232664Access Panel · corrodedRIGHT WING ACCESS PANEL 640FB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK CUTOUT COMMON TO PANEL 640FB REWORKED IAW REO.SDR SWIA201232663Access Panel · corrodedRIGHT WING ACCESS PANEL 640DB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK CUTOUT COMMON TO PANEL 640DB REWORKED IAW REO.SDR SWIA201232662Access Panel · corrodedRIGHT WING ACCESS PANEL 640AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) RIGHT LOWER WING PLANK ACCESS PANEL CUTOUT COMMON TO PANEL 640AB REWORKED IAW REO.SDR SWIA201232661Access Panel · corrodedRIGHT WING ACCESS PANEL 640BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK COMMON TO PANEL 640BB REPAIRED IAW REO.SDR SWIA201232660Access Panel · corrodedLEFT WING ACCESS PANEL 550HB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 550HB REPAIRED IAW REO.SDR SWIA201232659Access Panel · corrodedLEFT WING ACCESS PANEL 550AB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LEFT LOWER WING PLANK COMMON TO ACCESS PANEL 550AB REWORKED IAW REO.SDR SWIA201232658Access Panel · corrodedLEFT WING ACCESS PANEL 540EB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) LOWER WING PLANK CUTOUT COMMON TO PANEL 540EB REWORKED IAW REO.SDR SWIA201232657Access Panel · corrodedLEFT WING ACCESS PANEL 540BB HOLE HAS SIGNS OF CORROSION IN SEVERAL AREAS. (C-CHECK) MARKED AREAS OF LOWER WING PLANK COMMON TO PANEL 540BB REWORKED IAW REO.
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