JASC 5330
Service difficulty reports · 79,329
Reports filed under 5330 · Fuselage Main, 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 = '5330' 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 = '5330' 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 CALA2024102802741Skin · crackedCRACK FOUND ON SECOND LOWER FASTENER HOLE ON RH #3 WINDOW FRAMESDR CALA2024102802740Skin · crackedCRACK FOUND ON SECOND LOWER FASTENER HOLE ON LH #3 WINDOW FRAME (REF: AAR NR 1000020520)SDR R61A2024102800488Skin · ground damageJET BBIDGE DAMAGE BELOW CAPT,S DV WINDOW BETWEEN FRA 10 AND FRA 11 AT STR 17L. REPAIRED IAW EMB 170/175 SRM 53-10-01 REPAIR 15 ALSO REF VP-044779-2024 N/R #3 FOR WORK ACCOMPLISHED.SDR N6WA2024102602Doubler · corrodedANTENNA DOUBLER AT FS300 , STGR27 CORRODED. REPLACED ANTENNA DOUBLER AT FS300 , STGR27 IAW CRJ SRM 51-42-06.SDR 2024F00261Skin · corrodedREPAIRED CORROSION OF TAILCONE L/H, R/H, AND MIDDLE LOWER SKIN ASSEMBLIES UNDER AFT CHIN FAIRING PER AQRD ERO-981949 REV. IR TITLED "N389QS AFT TAILCONE SKIN CORROSION REPAIR" DATED OCT 24, 2024. SUPPORTED BY FAA FORM 8110-3 DATED 10/24/2024.SDR IPXA2024110620506Skin · dentedNOSE LOWER FUSEIAGE SKIN HAS A DENT NOT IN THE ADM MAPPING AT STA 380 BETWEEN LONGERON 51R AND 52 . MARK MM001. ACCOMPLISHED REPAIR PER MD11 53-00-01-2R-1 REPAIR #1 FIGURE 201 REV 71.SDR DALA2024102810432Doubler · corrodedCORROSION AROUND FASTENERS HOLES OF 2 WASTE BOX DOUBLER FASTENERS. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0516:5300-2019/004 00468 COMPLIED WITH ER/A 598701-14 REV B PRI REV 0, REV 1, REV 2 AND FINAL ER/A 5987SDR DALA2024102810431Doubler · corrodedWASTE BOX DOUBLER HAS MULTIPLE AREAS OF CORROSION AT I/B FWD CORNER. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0516:5300-2019/005 00469 COMPLIED WITH ER/A 598701-14 REV B PRI REV 0, REV 1, REV 2 AND FINAL ER/A 59SDR HNAA2024120401155Skin · corroded53-2015 FUSELAGE SKIN CORRODED AROUND HEATED WATER DRAIN AT BTW FR60-61. REPAIRED IAW ETD2024-145-029497 AND TRACKED WITH EO1-05-24-0650SDR HNAA2024112501128Skin · cracked53-2013 EXTERNAL SKIN CRACKED AROUND FASTENER AT FR77 BELOW STR8R. REPAIRED IAW EO 1-53-24-0683SDR SWIA20241115023Skin · gougedMULTIPLE GOUGES/SCRATCHES FOUND ON THE EXTERIOR, AFT OF FS559.00 +112 BETWEEN STRG 22R AND STRG 23R, JUST AFT OF THE LOW AIR GROUND CONNECTION ACCESS DOOR. (MARKED WITH TAPE) (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8244 DATED: 2024-10-26 REV - TEMPOSDR SWIA2024110823Skin · gougedMULTIPLE GOUGES/SCRATCHES FOUND ON THE EXTERIOR, AFT OF FS559.00 +112 BETWEEN STRG 22R AND STRG 23R, JUST AFT OF THE LOW AIR GROUND CONNECTION ACCESS DOOR. (MARKED WITH TAPE) (FILED OPEN) COMPLIED WITH REO 601R-53-61-8244 DATED: 2024-10-26 REV - TEMPORASDR CALA2024110102771Skin · unknownRH FUS SKIN FND PREVIOUS DOUBLER REPAIR AT BS 347-368 STR 33R REFER HX NR WO.3882226 AND . EEN STA 246-434 AT STR 33R NO LATER THAN 37,500 TOTAL FLIGHT CYC VE INTERNAL HFEC INSPECTION AND DETAILED VISUAL INSPECTION PER P OF EC/RA 5310- 08447". LES PER PART 2 ISDR SWAA2024103052342Skin · crackedREF 24-153-02913 WP 2; STEP 8. RII INSPECTION REQUIRED. 24-153-02907-WIP2 (N7864B - SWA - REPAIR - SECTION 46 - FUSELAGE CROWN SKIN CRACKS STA 727B - STA 727D AT S-4L) <[01] PERFORM RII VERIFYING STEP 8 OF TTG8Q00WMBUU INSTALLED REPAIR WASHERS PER SRM 51-40-08SDR CALA2024102502726Skin · misrepairedWHILE LAYING OUT NEW FASTENER LOCATIONS FOR L-1 DOOR SURROUND PREVENT MOD DOUBLER EA 5330-04213 REV D IT WAS DISCOVERED THAT SEVERAL INITIAL FASTENER LOCATIONS ON THE REPAIR DRAWING DO NOT MATCH UP WITH THE CONFIGURATION ON THE AIRCRAFT. ALSO, ONE FASTENER WILSDR AALA202410240135Doubler · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN EXTERNAL POWER DOOR LOWER CUTOUT SURROUND DOUBLER LOCATED FROM STA 229 TO STA 235.8, FROM S21R TO S22R. REPAIRED DOUBLER PER SRM 53-10-15-2R-4.SDR DALA2024102310322Doubler · corrodedEXFOLIATION ON UPPER DOUBLER ON INTERNAL CANTED KEEL STA Y=685 APROX BTW LONGERON 30-29R AT FUSELAGE (FUS). SUMMARY OF NRC 00523: CORROSION LEVEL 2. EXFOLIATION ON UPPER DOUBLER ON INTERNAL CANTED KEEL STA Y=685 APROX BTW LONGERON 30-29R AT FUSELAGE, WAS REPAISDR DALA2025011300287Skin · dentedRAMP REPORTS DENT ON UPPER RT FUSELAGE AREA/CANOPY. FND DENT TO BE NEAR FRAME 15, DENT IS 4 3/16" BY 2 3/4" WITH A DEPTH OF .038". OUT OF LIMITS PER A220 ASRP 53-11-01-05AAA- 661A-A (314041) PERFORMED A DVI OF EXTERNAL AREA AT DAMAGE LOCATION PER ANDTP BD500-ASDR SWAA2024112052063Intercostal · crackedINTERCOSTAL CRACKED IN PAX CABIN AT BS294.5+2 WL216 LBL56<[01] REMOVED AND REPLACED INTERCOSTAL BS 294.5- BS 303; AT STR 16L I.A.W SRM 51-40-02-0G-0 AND DWG 141A8180.;[02] CORRECTION TO ACTION 1: REMOVED AND REPLACED INTERCOSTAL BS 294.5 - BS 303; AT STR 16L ISDR AALA202411069419Skin · corrodedAIRCRAFT WAS GROUNDED: LARGE AREA OF SEVERE CORROSION APROX 2" X 1" AT BS 887 STR 27L. RIVET HEAD MISSING AN D SKIN CRACKED APROX 1" LENGTHWISE OF AC. MX FOUND CORROSION ON FUSELAGE SKIN UNDER SPLICE STRAP AT BS 887, FROM S24L TO S27R. ACCOMPLISHED DOUBLER RESDR SWIA20241021Skin · damagedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA84067-ETD2023-170-011676 MXCODEID67641-PR - DAMAGE ON FORWARD UPPER SKIN ADJACENT LH WINDSHIELD WIPER FROM FRAME 04 TO: FRAME 06 FROM STRINGER 01 TO: STRINGER 03. COMPLIED WITH TEMP REPAIR PER ETD2023-170-011676. PERMASDR VNAA202411240014Skin · corrodedCORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT. CORROSION ON INTERNAL SKIN CUT OUT, (SEAL SEATLEMENT AREA), DOOR SURROUND STRUCTURE, MAIN AVIONICS COMPARTMENT WAS REPAIRED PER REO 690-53-21-032 RSDR IPXA2024102452020Skin · ground damageLOAD CREW STRUCK AIRCRAFT WITH CAN CAUSING PUNCTURE DAMAGE NEAR STA 2020 BETWEEN STRINGERS 38L & 39L. COMPLETED/ VERIFIED ALL STEPS OF EO-91798-REQ1 LISTED ARE C/W. THIS IS A MAJOR REPAIR, CAT B REPAIR. REFEO-91798-REQ1 (SECTION 46 LEFT FUSELAGE SKIN PUNCTURE SDR VNAA202410210031Skin · dented" SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH.WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-580 REV."SDR VNAA202410210030Skin · dented"SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH. SEVERAL DENTS ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING LH WERE REPAIRED PER REO 670-51-00-085 REV -A AND PER REO 690-53-00-579 REV."SDR VNAA202410210025Doubler · corrodedCORROSION ON PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW STA 1000-1015 AND STRINGERS 25RH-26RH AT AFT CARGO COMPARTMENT. PRODUCTION DOUBLER OF ANTENNA AND ATTACH ANLGES BTW STA 1000-1015 AND STRINGERS 25RH-26RH AT WERE EVALUATED OUT OR LIMITS PER CRJSDR DALA2024102110254Skin · dentedSHIP 3159 ON A/C ARRIVAL NOTICE DENT AFT LOWER FUSELAGE JUST BEFORE APU INLET. CORRECTIVE ACTION: REPAIRED PER ER/A: 621756-14. (5845718)SDR VNAA2024101630034Skin · corrodedEXTERNAL FUSE SKIN BETWEEN F.S.855 - F.S.977 20L-16L HAS CORROSION.SDR IPXA2025050244800Skin · dented*** MAJOR REPAIR *** RIGHT SIDE FUSELAGE SKIN DENT AND CREASE REPAIR AT STA 139 ABOVE S-21R REVIEW COMPLETE.SDR DALA2024102110249Access Door · crackedSHIP 3143 CRACK ACCESS DOOR 172AR AROUND AFT HINGE AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 615217-14. (0619050)SDR CALA2024102102699Skin · corrodedIT WAS FOUND CORROSION ON THE SKIN (P/N 146T3241-12) AT THE DRAIN HOLE AREA LOCATED BETWEEN STA 1540 AND 1562 & STR 39LH AND 39RH. MANENT SOLUTION WITH INSPECTION REQUIREMENTS THAT MUST BE ACCOMP ON OR BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. ACSDR SWAA2024112550872Intercostal · corrodedPASSENGER AREA STA 947; LBL 24 UNDER AFT LAV MOUNT HAS EVIDENT OF CORROSION.<[01] FOUND INTERCOSTAL TO BE OUT OF LIMITS PER SRM 53-70-51-1A-1. INTERCOSTAL TO BE REMOVED AND REPLACED ON [TTG8Q00WJ9TR].SDR CALA2024102502728Skin · damagedREMOVED DAMAGE SKIN AREA ON AFT CARGO DOOR LOWER FWD CORNER, AND INSTALLED REPAIR STA 796.98-811 REF AAR ESR-WI NO. 2022816- 29-109935 REV IR AND UNITED EC/RA NO. 5231-01158. WORK ACCOMPLISHED BY V894534.REFER LP9607861SDR YENA2024102201389Skin · damagedDURING HEAVY MAINTENANCE: MISSING MATERIAL ON EXTERNAL SKIN LOCATED BTW FRAME 78 TO FRAME 80 PLUS 4 INCH AND BTW STRINGER 1 LH TO 1RH THS COMPARTMENT; (RESOLVED ON W/O: 1289680 TASKCARD: NR-00036) PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED BTW FRAME 7SDR DALA2024102110242Skin · corrodedSHIP 3143 CORROSION INTERNAL SKIN MACHINED AREA AT LEVEL STR 42L AND BTW FR60 TO FR61 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH ER/A 557100-14AD. (0617562)SDR SWIA202501061018Skin · dentedDENT LOCATED BETWEEN FS 1015.00 - FS 1031.00 AND BETWEEN STR 27 AND STR 26L(C-CHECK RO 12/21/2024) (FILED CLOSED)REPAIRED DENTED LOCATION BETWEEN FS1015.00-FS1031.00 BETWEEN STR 27 AND STR 26L REF REO 670-53-61-2397 REV.-- DATED 2024-10-29. LEAK CHECK. COMPLIESDR SWIA2024122401018Skin · dentedDENT LOCATED BETWEEN FS 1015.00 - FS 1031.00 AND BETWEEN STR 27 AND STR 26L(C-CHECK RO 12/21/2024) (FILED OPEN)REPAIRED DENTED LOCATION BETWEEN FS1015.00-FS1031.00 BETWEEN STR 27 AND STR 26L REF REO 670-53-61-2397 REV.-- DATED 2024-10-29. LEAK CHECK. COMPLIED SDR SWIA20241018Waste Box · corrodedCORROSION IN WASTE BOX DOUBLER AT DOOR HINGE. (C-CHECK RO 11/13/2024) REPLACED WASTE BOX DOUBLER. REF SRM 51-40-08. SEE CONTINUATION CARDS FOR DETAILED STEPSSDR ASAA2024101853458Skin · corrodedSECTION 47 RH AFT LOWER FUSELAGE SKIN AROUND WATER SERVICE PANEL CUTOUT HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATERGORY B MINOR REPAIR ON SECTION 47 RH LOWER FUSELAGE SKIN AROUND WATER SERVICE PANEL AT STA 907-927 STGR 25R TO STGR 27R P/N 147A34SDR ASAA2024101853419Skin · corrodedSECTION 46 EXTERNAL FUSELAGE SKIN LAP SEAM AT STA 727-727A STGR 10R HAS SIGNS OF CORROSION. GROUNDED - YES. ACCOMPLISHED CATEGORY A MINOR REPAIR ON SECTION 46 FUSELAGE SKIN LAP SEAM AT STA 727-727A STGR P/N 146A3151-94 IAW EA #800-53EA-27776 REV 00.SDR ASAA2024101853376Skin · corrodedSECTION 47 LOWER LAP SEAM BETWEEN STA 907-927 STGR 23L HAS SIGNS OF CORROSION. GROUNDED - YES. EVALUATE / REMOVE CORROSIONACCOMPLISHED CATEGORY A MINOR REPAIR M SKIN P/N: 147A3110-3 IAW EA NO.800-53EA-27764 REV 00 AT L/H LOWER LAP SEAM BETWEEN STA 907-927 AT SDR ASAA2024101853375Skin · corrodedSECTION 47/48 AFT LOWER FUSELAGE SKIN BUTT SPLICE AT STA 1016 STGR 24L-27R HAS SIGNS OF CORROSION. GROUNDED - YES. EVALUATE / REMOVE CORROSION ACCOMPLISH CATEGORY B MINOR REPAIR AT FUSELAGE SKIN BUTT-JOINT AT STA1016 BETWEEN S-24LTO S27R ON SKIN P/N 147A3400-SDR DALA2024102110243Skin · corrodedSHIP 3143 CORROSION DAMAGE WAS FOUND ON FUSELAGE SKIN PANEL BETWEEN FR58-61 AND STGR42-43LH. CORRECTIVE ACTION: REPAIR PER ERA 557100-14AD. (0615883)SDR AALA202410195418Skin Panel · corrodedAIRCRAFT IN BASE MAINTENNACE: CORROSION ON CENTER WING BOX TOP SKIN BETWEN FR 41 AND FR 42 AT STIFFENER 17 AND RIB 1. REPAIRED SKIN PANEL PER EA 357671.SDR SWAA2024112549565Former · crackedR/H FAIRING FORMER BS 500D BETWEEN STRINGER 18 R/H AND 19 R/H IS CRACKED<[01] EVALUATED CRACK ON FAIRING FORMER AT BS 500D BETWEEN STRINGER 18R/H AND 19R/H FOUND TO BE OUT OF LIMITS THEREFORE FAIRING FORMER WILL BE REPAIRED BY REPLACEMENT OF PART PER 53-30-71-SDR SWAA2024112550098Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS685 S-3L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 685 S-3L PER SRM 51-40-02-0G-0 AND BOEING DWG 144A1106 REV. A.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550099Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS706 S-2L. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 706 S-2L PER SRM 51-40-02-0G-0 AND BOEING DWG 144A1107 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550093Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727E S-5R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727E S-5R PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1112 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550094Stringer Clip · crackedCRACKED STR CLIP AT PAX CABIN BS727A S-3R. MARKED<[01] REMOVED AND REPLACED STRINGER CLIP AT BS 727A S-3R PER SRM 51-40-02-0G-0 AND BOEING DWG 146A1101 REV. -.;[02] VERIFIED CORRECTIVE ACTION STEP 1.SDR SWAA2024112550262Support Bracket · crackedCRACK ON SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN 2024-645563<[01] REPLACED SUPPORT BRACKET LOCATED BS 867 BTW STR 2R TO STR 3R AT PASSENGER CABIN IAW B737-800 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02 AND DWG-146A7901-88B REV A; LEN
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