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 IPXA13M77041Doubler · crackedINSPECTION TYPE:1C, LT WING FIXED L/E BEADED DOUBLER CRACKED NEAR XOS695. REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 692-698 IAW EO MD11-5730-48222-A.(MAJOR)SDR IPXA13M76985Doubler · crackedINSPECTION TYPE:1C LT WING FIXED L/E INNER BEADED DOUBLER CRACKED NEAR XOS 732 REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 728-734 IAW EO MD11-5730-48222-A. (MAJOR)SDR REXA2013020400090Skin Panel · chafedRIGHT WING FORWARD LOWER WING PLANK PANEL AT WS 54.897 ON FUEL DOOR LANDING IS PITTED AND CHAFED IN THE NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR SPUY201302020009Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING UPPER SKIN NEAR REAR SPAR SHOWS CORROSION WS 601.5, REF NR 0258.SDR SPUY201302020008Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING UPPER SKIN T/E NEAR OTBD AILERON CORRODED WBL 492.0, REF NR 0257.SDR SPUY201302020006Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, LT WING LOWER SURFACE SHOWS CORROSION WS 491.5 REF NR 0249.SDR SPUY201302020005Skin · corrodedDURING ROUTINE C-CHECK INSPECTION, RT WING UPPER SKIN L/E SHOWS CORROSION L/E STA 130.7, REF NR 0183.SDR DALA13007540941Skin · wornWEAR ON LT WING LOWER SKIN LOWER SKIN DUE TO INTERFERENCE WITH FLAP FWD HINGE FAIRING STA XW=99 AND XW=111 APROX (LW)(REF.NRC: T0 270112). DAMAGE WAS ATTENDED IAW ER/A 509661-14, REV ORIG AND SRM 51-30-5 AND 51-10-3, FAIRINGS WAS INSTALLED CORRECTLY AND INTESDR MTNA020120130001Panel · separatedAFTER LANDING AND DURING PREFLIGHT THE RIGHT WING INBOARD SECTION OF TKS PANEL WAS FOUND TO BE SEPARATING FROM THE WING.SDR ASOA2013022603078Access Panel · crackedFOUND LT FUEL ACCESS HOLE 540CB HAS MULTIPLE INDICATIONS NOTED AT AFT SIDE LANDING APPROX 6.0" LENGTH BY .250" W 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030, REV J.SDR ASOA2013022603077Access Panel · crackedFOUND RT FUEL ACCESS HOLE 640FB HAS MULTIPLE INDICATIONS NOTED AT INBD SIDE LANDING APPROX 8.0" LENGTH BY .250 W 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030, REV J.SDR SIMA20130130003Tape · peelingON FLIGHT 3728 THE CREW REPORTED THE RIGHT WING EMERGENCY EXIT PATH ON TOP OF WING WAS PEELING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE SAFETY TAPE IAW PT B OF EO-CR-5700-147. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR QXEA2013012900200Skin · corrodedWHILE INVESTIGATING THE MAGNASTICK BONDING CHECK FAILURE, FOUND PITTING CORROSION ON THE BONDING SURFACE OF THE LOWER WING. REMOVED CORROSION IAW SRM 51-21-00-00-02. MIN THICKNESS NOTED .198", CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-91SDR QXEA2013012800198Access Panel · corrodedRT WING FUEL PANEL 624DT HAS LIGHT SURFACE CORROSION ON MATING SURFACE. BLENDED CORROSION IAW RD 8/4-57-442. FOUND TO BE IN LIMITS IAW RD 8/4-57-442. PANEL FOUND TO BE CRACK FREE IAW RD 8/4-57-442. APPLIED ALODINE IAW RD 8/4-57-442. COMPLIED WITH RD 8/4-5SDR USAA2013021100016Fuel Door · damaged3S CHECK - ELONGATED HOLE IN LEFT WING FUEL DOOR 540KB BETWEEN WS 8268 TO WS 8744 & BETWEEN RIB 15 TO RIB 16. REPLACED LEFT WING FUEL DOOR 540KB IAW A320 SRM 51-72-11 & AMM 57-27-11-400-002-A.SDR USAA2013021100015Fuel Door · damaged3S CHECK - ELONGATED HOLE IN LEFT WING FUEL DOOR 540JB BETWEEN WS 7792 TO WS 8268 & BETWEEN RIB 14 TO RIB 15. REPLACED LEFT WING FUEL DOOR 540JB IAW A320 SRM 51-72-11 & AMM 57-27-11-400-002-A.SDR DALA13004487105Panel · damagedWING EXTENSION T/E CLOSEOUT PANEL DAMAGED. C/A REMOVED PANEL AND ROUTED TO 382 FOR REPAIR(312579). REPAIRED PANEL IAW SHOP ORDER FZ9480 NDS INSTALLED. (134146) OK TO INSTALL CLOSEOUT PANEL FOR LT WING T/E EXTENSION. INSTALLED PANEL (204965) PANEL PAINT COMSDR IPXA3M76979Doubler · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT BEADED DOUBLER CRACKED NEAR XOS.499, REPAIRED RT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS 494-500, SRM 57-40-02. REPAIR 15 FIG 203.SDR IPXA3M76948Doubler · crackedINSPECTION TYPE: 1C, LT WING INNER BEADED DOUBLER CRACKED NEAR XOS 670. REPAIRED LT WING FIXED L/E INNER BEADED DOUBLER BETWEEN XOS667-673 IAW EO MD11-5730-48222-A (MAJOR).SDR R61A201301240507Skin · damagedWHILE ACFT WAS IN FOR HEAVY CHECK, FOUND RT WING FUEL TANK (WING PLANK) UNDER ACCESS 622AT APPROX WS RT YW-42.0-YW-79.7 L/E OF FASTENER HOLES HAS 1 EA HOLE WITH HIGH METAL AROUND THE HOLE ON THE INSIDE OF THE TANK, BOTTOM SURFACE OF THE TANK. MX COMPLIED WITHSDR QXEA2013012400175Skin · wornRT WING SKIN PANEL LANDING FOR PANEL 624DT HAS WEAR MARKS FROM PANEL BOTH INBD AND OTBD RADIUS OF CUTOUT. REMOVED WEAR MARKS IAW RD 8/4-57-445. ACCOMPLISHED FPI ON PANEL LANDING AND FOUND TO BE CRACK FREE REF RD 8/4-57-445 AND NDT MANUAL 8.2.0. MIN THICKNESS SDR QXEA2013012400174Skin · wornRT WING SKIN PANEL LANDING FOR PANEL 624CT HAS WEAR MARKS FROM PANEL BOTH INBD AND OTBD RADIUS OF CUTOUT. REMOVED WEAR MARKS IAW RD 8/4-57-445. ACCOMPLISHED FPI ON PANEL LANDING AND FOUND TO BE CRACK FREE REF RD 8/4-57-445 AND NDT MANUAL 8.2.0. MIN THICKNESSSDR QXEA2013012400172Skin · wornRT WING SKIN PANEL LANDING FOR PANEL 624ET HAS WEAR MARKS FROM PANEL BOTH INBD AND OTBD RADIUS OF CUTOUT. REMOVED WEAR MARKS IAW RD 8/4-57-445. ACCOMPLISHED FPI ON PANEL AND FOUND TO BE CRACK FREE REF RD 8/4-57-445 AND NDT MANUAL 8.2.0. VERIFIED MIN REMAINISDR SWAA2013020112225Skin · crackedLEFT WING FIXED LEADING EDGE SKIN CRACKED AT O/B END OF NR 1 K-FLAP. REPAIRED SKIN IAW SRM.SDR QXEA2013012400139Access Panel · corrodedRT WING FUEL PANEL 624DT HAS AREAS OF CORROSION ON MATING SURFACE. BLENDED CORROSION, ORIGINAL THICKNESS .120 REMOVED .002" REMAINING THICKNESS .118" WITHIN LIMITS IAW RD 8/4-57-442. INSPECTED AREAS BLENDED WITH HFEC, NO CRACKS NOTED REF NDTM PT 1 51-00-06-9SDR REXA2013012700081Skin · chafedFUEL PANEL 510AB LANDING ON LEFT WING LOWER SKIN IS CHAFED AND PITTED AT WS 12.245. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR REXA2013012700080Skin · chafedFUEL PANEL 640BB LANDING ON RIGHT WING LOWER SKIN IS CHAFED AND PITTED AT WS 54.897. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR REXA2013012700079Skin · chafedFUEL PANEL 540BB LANDING ON LEFT WING LOWER SKIN IS CHAFED AND PITTED AT WS 54.897. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR UHLA2013012300731Skin · crackedCRACK ON UPPER RT WING SKIN T/E AT RIB 10. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER IAW ETD2011-170/02998, REV A.SDR SWIA201332797Skin Panel · crackedLEFT LOWER WING PLANK WS 65.75 STR 14-15 DRAIN VALVE HOLE CRACK INDICATION NOTED. (C-CHECK) REPAIRED LEFT LOWER WING PLANK DRAIN VALVE HOLE AT WS 65.75 STR 14-15 IAW REO.SDR FDEA201301230163Doubler · crackedLEFT WING FIXED L/E BEAD DOUBLER AT XOS 666 FOUND CRACKED DURING OTBD SLAT DRIVE CABLES INSPECTION. REPAIRED IAW SRM 57-40-02 FIGURE 203 REPAIR 15 REVISION 51. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 116.SDR SWAA2013012811893Access Panel · crackedLEFT WING FUEL TANK ACCESS PANEL 520CB DOME NUT CHANNEL HAS A CRACK. REMOVED AND REPLACED DOME NUT CHANNEL AT LEFT WING FUEL TANK ACCESS PANEL 520CB IAW B717 SRM 57-10-01.SDR DALA13003295652Panel · crackedSLAT 2, COVE SKIN PANEL IS CRACKED. INBD SIDE AREA OF INBD MAIN TRACK. (093-02) CUT OUT DAMAGE AREA FABRICATED REPAIR DOUBLER AND FILLER, INSTALLED REPAIR DOUBLER AND FILLER AT SLAT NR 2 COVE SKIN PANEL INBD SIDE AREA OF INBD MAIN TRACK IAW ER/A NR 509318-1SDR SWIA201332739Skin Panel · corrodedLEFT WING FUEL ACCESS 540BB WING PLANK ACCESS HOLE HAS FRETTING CORROSION. (C-CHECK) REPAIRED FUEL ACCESS HOLE 540BB IAW REO.SDR SWIA201332733Skin Panel · corrodedRIGHT WING FUEL ACCESS 650 DB WING PLANK ACCESS HOLE HAS FRETTING CORROSION. (C-CHECK) REPAIRED FUEL ACCESS HOLE 650DB IAW REO.SDR SWAA2013021412680Fairing · delaminatedRIGHT WING NR 2 IFOT FAIRING HAS AREA OF DELAMINATION ON UPPER SURFACE WHERE BUBBLE FAIRING ATTACHES. REPAIRED THE NR 2 IFOT FAIRING DELAMINATED AREA ON UPPER SURFACE IAW SRM 51-70-04.SDR QXEA2013011700181Access Panel · corrodedRT WING FUEL PANEL 624DT HAS AREAS OF CORROSION ON MATING SURFACE. REMOVED CORROSION FROM LANDING AND FOUND BLENDS TO BE IN LIMITS IAW SRM 57-20-35-02-05. ORIGINAL THICKNESS .80", REMAINING THICKNESS .0715, BLENDED RIVETS MEASURE GREATER THAN .179" HFEC INSPECSDR QXEA2013011700180Access Panel · corrodedRT WING FUEL PANEL 624ET HAS AREAS OF CORROSION ON MATING SURFACE. REMOVED CORROSION IAW RD 8/4-57-442. ORIGINAL THICKNESS .120 REMAINING THICKNESS .115, WITHIN LIMITS IAW RD 8/4-57-442. HFEC INSPECTED AREA, NO CRACKS NOTED REF NDTM 51-00-06-910-801 PT 1. SDR QXEA2013011700068Access Panel · corrodedRIGHT WING FUEL PANEL 624FT HAS AREAS OF CORROSION ON MATING SURFACE. BLENDED CORROSION, ORIGINAL THICKNESS .120 REMOVED .005", REMAINING THICKNESS .115" WITHIN LIMITS IAW RD 8/4-57-442. INSPECTED BLENDED AREA WITH HFEC, NO CRACKS NOTED, REF NDTM 51-00-06-910SDR QXEA2013011700067Access Panel · corrodedRIGHT WING FUEL PANEL 624AT HAS AREAS OF CORROSION ON MATING SURFACE. BLENDED CORROSION, ORIGINAL THICKNESS .120 REMOVED .002", REMAINING THICKNESS .118" WITHIN LIMITS IAW RD 8/4-57-442. INSPECTED BLENDED AREA WITH HFEC, NO CRACKS NOTED REF NDTM PT 1 51-00-06SDR QXEA2013011700058Access Panel · corrodedRT WING FUEL PANEL 624BT HAS AREAS OF CORROSION ON MATING SURFACE. BLENDED CORROSION, ORIGINAL THICKNESS .120 REMOVED .003", REMAINING THICKNESS .117" WITHIN LIMITS IAW RD 8/4-57-442. INSPECTED BLENDED AREA WITH HFEC, NO CRACKS NOTED REF NDTM PT 1 51-00-06-91SDR REXA2013011800070Skin · corrodedRIGHT WING LANDING FOR FUEL ACCESS PANEL 540BB BETWEEN WS 45 AND WS 65.75 PITTED FROM FRETTING AT INBOARD AND OUTBOARD EDGES MEASURING 0.007" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR REXA2013011800069Skin · corrodedLEFT WING LANDING FOR FUEL ACCESS PANEL 540BB BETWEEN WS 45 AND WS 65.75 PITTED FROM FRETTING AT INBOARD AND OUTBOARD EDGES MEASURING 0.006" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.SDR FDEA201301160103Access Panel · corrodedLEFT WING - T/E LOWER ACCESS PANEL 541JB CUT-OUT FORWARD EDGE LOWER CAP, LOWER SURFACE FOUND CORROSION. FOUND WITHIN LIMITS IAW SRM 57-00-00, FIG 202, REV 51. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 116.SDR FDEA201301160101Access Panel · corrodedRT WING - T/E LOWER ACCESS PANEL 641JB CUT-OUT FORWARD EDGE LOWER CAP, LOWER SURFACE FOUND CORROSION. CORROSION REMOVED AND REPROTECTED IAW SRM 51-21-01, REV 51. ORIGINAL THICKNESS: 0.120", MATERIAL REMOVED: 0.004", REMAINING THICKNESS: 0.0116" AND FOUND WISDR SWAA2013021412679Fairing · crackedRIGHT WING BUBBLE FAIRING ON TOP OF NR 2 CRACKED. R & R FAIRING IAW SOPM SRM.SDR UALA2013011600279Skin · dentedDENTED RIGHT WING LEADING EDGE RIGHT WING BETWEEN ENGINE AND WINGTIP. REPAIRED IAW SRM 57-40-00.SDR QXEA2013011500047Access Panel · wornRT WING SKIN PANEL LANDING FOR PANEL 624BT HAS WEAR MARKS FROM PANEL BOTH INBD AND OTBD RADIUS OF CUTOUT. REMOVED WEAR MARKS AND CORROSION IAW RD 8/4-57-445. MIN THICKNESS NOTED .073" CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT SDR QXEA2013011500046Access Panel · corrodedRT WING SKIN PANEL LANDING FOR PANEL 624AT HAS SURFACE CORROSION ON INBD AND OTBD AREAS OF CUT OUT. REMOVED SURFACE CORROSION IAW RD 8/4-57-445. MIN THICKNESS NOTED .070, CONFIRMED CRACK FREE REF NTM 51-00-04-910-801 PT 1 AND 51-00-06-910-801 PT 1. MATERIAL SDR CA130116016Skin · cracked(CAN) DURING COMPLETION OF A CORROSION INSPECTION ON THE INTERNAL STRUCTURE OF THE WING A 28" CRACK OF THE LOWER WING SKIN WAS DISCOVERED. LOCATED APPROXIMATELY 8" INBD OF RT RIB BS 6. RUNNING FORE AND AFT. 2 PHOTOS ADDED TO THE SDR DEPICTING REPORTED CRACK
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