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 SCNA20250717264Skin · dentedFOUND DENT BETWEEN STA. 1006 AND 1013 BETWEEN STRINGERS 12L AND 13L. DENT IS OUT OF LIMITS PER SRM 53-00-01 TABLE 2 NO CRACKS NOTED IN PAINT. REPAIRED DAMAGED FUSELAGE SKIN @STA 1006-1013 STR 12L TO 13L PER ER 25-02325 REV. P1 AND ENG-53SCA-11709 REV 00.SDR IPXA2025071295380Bear Strap · crackedCRACK, FWD ENTRY DOOR AFT LOWER CORNER BEAR STRAP. INSTALLED INSULATION BLANKET IAW AMM 25-80-00-400-803 REV. 145, JOB COMPLETED AND CONDITION CHECK NORMAL. IAW AMM 20-11-00-910-802 REV 145 INSTALLED THE E/E COOLING DUCT AT MEC P31. IAW AMM 24-22-00-862-001 RESDR DALA2025071105228Skin · damaged(LOG 1068562) FOUND DAMAGE AT STA 807 BY S-2R. ACCOMPLISHED REPAIR INSTRUCTIONS 4 A-E PER SRM 53-00-01-2R-35.SDR AALA202507106493Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT AFT LAVATORY SERVICE PANEL BETWEEN BS 847 AND BS 867, BETWEEN S24L AND S25L. REPAIRED SKIN PER EA 365990.SDR COEA2025071002921Skin · ground damageDURING UNLOADING OF FLIGHT 7820, THE BELT LOADER MADE CONTACT WITH THE AIRCRAFT. DISCREPANCY: LOWER L/H LATERAL SKIN PANEL BETWEEN FRAMES 36-37 AND STRINGERS 16-17L HAS DENT FROM BELT LOADER. REPAIR COMPLETED PER SRAS ES_00264336_01-25790, ISSUE B.SDR N6WA2025071009Skin · damagedFUSELAGE SKIN FWD LOWER SKIN PANEL BETWEEN STRG20R-21R AT FS453.00-FS469.00 IS DAMAGED. REPAIRED FUSELAGE SKIN LOWER SKIN PANEL BETWEEN FS453-FS469 AT STGR20R IAW GOJET EO-C550-53MR-076SDR DALA2025070805149Skin · damagedSHIP 3415 AIRCRAFT SKIN ABOUT 3" FWD OF FRAME 63 TOOLING DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 627461-14 REV ORIG. (1069231)SDR DALA2025070805148Skin · damagedSHIP 3415 AIRCRAFT SKIN ABOUT 4" AFT OF FRAME 63 BETWEEN L1 AND R1 RIDGE IN PAINT TOOLING DAMAGE. REPAIRED PER ERA 627461-14 REV ORIG. (1069223)SDR DALA2025070805108Skin · dentedSHIP 6711 DTA MONITOR INSPECTION LOG REF ERA 627037-14, THE FUSELAGE SKIN WAS FOUND DENTED (3 EA PROTRUDING) BETWEEN BSTA 1380 & BSTA 1400 AND BETWEEN S-28R & S-30. CORRECTIVE ACTION: REF ERA 627037-14. (1068906)SDR CALA2025070806348Skin · damagedLIGHTNING STRIKE FOUND AT STATION 410 BELOW STRINGER 15L - REF L P 5171918 (REF AAR NR 1000048418) ALL WORK PERFORMED ON RFD AAR N/R 1000048418.SDR CALA2025070806347Skin · damagedLIGHTNING STRIKE FOUND ON FASTNER AT STATION 188 AND WATER LINE 220 LH SIDE-REF LP NO.4936294 (REF AAR NR 1000048412). COMPLIED WITH ECRA 5310-08636. MAINTENANCE C/WSDR CALA2025070806346Skin · damagedLIGHTNING STRIKE AT STA 440, STRINGER 9R-REF LP NO.5180618. COMPLIED WITH EC/RA 5330-07558. REPAIR COMPLETED ON ELB 5180618. NO FURTHER ACTION REQUIRED.SDR AALA202507108624Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT AFT LAVATORY OVERBOARD VENT AT BS 907 BETWEEN S21L AND S22L. REPAIRED SKIN PER SRM 53-70-01-2R-3.SDR DALA2025070805132Skin · damagedSHIP 3412 TOOLING DAMAGE ON SKIN 6" AFT OF C63 1" I/B OF P2 RIGHT. CORRECTIVE ACTION: REPAIRED PER ERA 627461-14 REV ORIG. (1067261)SDR EE4Y2025070622637Skin · canningDURING THE STRUCTURE INSPECTION WAS REPORTED IN THE CENTER FUSELAGE III, AT FR 82+357MM, STR-23R+100MM AN EXISTING REPAIR WITH OIL CAN IN THE EXTERNAL SKIN. SINCE THAT THE DAMAGE REPORTED IS WITHIN GRAY ZONE AREA IAW ERJ190 PART II SRM 53-23-01, REPAIR 61, FIGSDR EE4Y2025070622642Skin · dentedDURING THE STRUCTURE INSPECTION, DENTS WERE FOUND CONTROLLED AS PER PREVIOUS OPERATOR RECORDS UNDER ETD2015-190-078115 GUIDELINES, HOWEVER, FOLLOWING INSPECTION INSTRUCTIONS REQUIRED OIL CAN EFFECT WAS FOUND LOCATED BTWN FR25/26, BTWN STR-28L/28R. THIS CONDITISDR EE4Y2025070622639Skin · no discrepancyDURING THE STRUCTURE INSPECTION, AN EXISTING REPAIR WAS FOUND INSTALLED AS PER PREVIOUS OPERATOR RECORDS UNDER IC2007-190/04024A DTD JUN 20 2007 GUIDELINES, HOWEVER, THE RECORDS DOES NOT SHOWN MATERIAL TRACEABILITY. THE DAMAGE WAS EVALUATED AND FOUND ON GREY ZSDR EE4Y2025070622634Repair · misinstalledDURING THE STRUCTURE INSPECTION, AN EXISTING REPAIR WAS FOUND INSTALLED AS PER PREVIOUS OPERATOR RECORDS UNDER ETD2010-190-10955 GUIDELINES, HOWEVER, THE RECORDS DOES NOT SHOWN MATERIAL TRACEABILITY. DUE TO THIS FACT, THE REPAIR WAS REMOVED, AND A NEW PROPOSALSDR I5PA2025070575701Skin · corrodedMAJOR REPAIR: LEVEL 2 CORROSION FOUND AT BSTA 680-700 BETWEEN STRINGERS 26R/28R. REPAIRED CORROSION PER EO APA-0043-001 REV 1 DTD 28JUN2025 AND PER SRM 53-00-01 REPAIR 28.SDR DALA2025070705034Skin · gougedSHIP 3412 SKIN GOUGED AT FRAME 63 BETWEEN P-1R AND P-2R. CORRECTIVE ACTION: REPAIRED PER ERA 627461-14 REV ORIG. (1064177)SDR DALA2025070805083Skin · damaged(LOG 1062480) FWD CARGO DOOR CUTOUT SKIN DAMAGE AFT SIDE STA 492.4 BETWEEN S22R AND S23R. INSTALLED REPAIR PER B737 AMM SRM 53-00-01-2R PROC 24 AND ERA 627564-14 REV 0.SDR EE4Y2025070422631Skin · corrodedDURING THE INSPECTION WAS REPORTED CORROSION DAMAGE AFFECTING THE FUSELAGE SKIN, LOCATED AROUND THE EXISTING HOLE CUT OUT, BETWEEN FRAME 63 AND 64 AND BETWEEN STRINGER 1L AND 2L. SINCE THE CORRODED AREA REQUIRE A SKIN TRIM OUT AND A REPAIR, THE DOUBLER P/N: 19SDR EE4Y2025070422630Skin · damagedDURING THE STRUCTURE INSPECTION, IT WAS FOUND THE CENTER FUSELAGE I – AT FR29+365MM, S-20R+14MM EXTERNAL SKIN WITH LIGHTNING STRIKE. THE DAMAGE WAS REMOVED BY DRILLING A HOLE (Ø3.17MM). PER ERJ 190 SRM 53-21-01 / AD53 IT WAS NOT POSSIBLE TO REPAIR IT, DUE TO TSDR SWIA2026030475631Doubler · unknownCOMPLY WITH SCHEDULED MAINTENANCE WIFI PCS/TIMING ANTENNA SDI 700 - COMPLY WITH INSPECTION OF THE PCS/TIMING ANTENNA SDI & DI IAW STC ST02541CH ICA DOCUMENT D12454-20110 SEC 4 (LATEST REVISION) 1. INTERNAL A/C SKIN - DOUBLER OUTER EDGE FASTENER HOLES - SDI2.SDR SWAA2025072988004Doubler · corrodedWIFI ANTENNA AREA; EXTERIOR FUSELAGE CROWN SKIN DOUBLER FOUND CORROSION AT STA 727C BTWN STGR 1 AND 2 RH AT SEVERAL FASTENERS. RESOLVE FAULT ON TTG8Q013J793 WHERE EA 25-153-01827.SDR N6WA2025070306Lap Joint · corrodedCORROSION ON CIRCUMFERNTIAL JOINT AT FS280 BETWEEN STRINGER 25R AND 25L. PERFORMED REPAIR ON STRAP AT FS280 BETWEEN STRINGER 25R AND 25L IAW STS EA139-2025-122.SDR KY7A202507030038Skin · corrodedA/B/E CHECK FOUND BELLY CORROSIONSDR F3LA202507030263Skin · dentedC4 CHECK REF LOGPAGE 444741 ITEM 1 & EAR INC0061624 FOR DENT ON SKIN FUSELAGE BETWEEN 13 & 14. REPAIRED DENT ON SKIN FUSELAGE BETWEEN FRAME 13 &14 IAW A320NEO SRM 53-11-11-300-04. CATEGORY B REPAIR CURRENT RC/FH IS 10,758/23,964.08 INSPECTION THERSHOLD FROMSDR REXA2026072901293Skin · wornWEAR ON EXTERNAL FUSELAGE SKIN STR 27L, BTW BS 900 - 920 WEAR ON FUSELAGE SKIN WAS EVALUATED SKIN BTW BS 913 - 927, STR 27L, FOUND OUT LIMITS AND SKIN AT BS 900 IS WITHIN LIMITS IAW SRM 53-00-01-101-001-A01 AND AREA WAS REPAIRED IAW EA CRJ953-19697, REV IR.SDR SWIA20250702Landing · crackedRIGHT HAND TRU BAY, LAND HAS A SUSPECTED CRACK JUST ABOVE THE AFT LATCH RECEPTACLE. PERFORMED PERMANENT REPAIR (PART REPLACEMENT). COMPLIED WITH M-337. SEE CAMP 30869266 FOR RVSM MAPPING REFERRAL. REF. CRJ 900 SRM 51-40-11-001-001-A01.SDR SWAA2025072987675Doubler · crackedDURING OK TO INSTALL RT BS 663 RBL 6-32 LWR DOUBLER; FOUND DOUBLER CRACKED AT THE CORNER. REMOVED AND REPLACED ON FAULT TTG8Q013CQB6.SDR IPXA2025071525054Skin · corrodedMAJOR REPAIR, CORROSION-SKIN, AFT CGO COMPT FWD SIDE LWR SKIN, NEAR STA 1081 S-39L~S-39R. ACCOMPLISHED REPAIR I.A.W UPS EO NO:EO-94375-REQ1 REV.1 AND BOEING DWG NO.140T0130 SH.16 REV.C;140T0130 SH.7 REV.C;146T1201 SH.1 REV.H AND 146T3261 SH.3 REV.-.SDR CALA2025070706259Skin · corrodedLAV PAN SERVICE PANEL SKIN STRUCTURE AROUND PAN HAS SIGNS OF CORROSION AT HYLOCK AREA, REF 002741809 FUSELAGE SKIN AT LAVATORY SERVICE PAN BS 847-867 AT S-25L REPAIRED PER ECRA -5331-03169 REF BAM N/R002731809 FOR WORKED PERFORMED AND REQUIRED INSPECTION SIGNSDR DALA2025070805074Skin · corrodedCORROSION FOUND ON FUSELAGE SKIN FWD OF THE WASTE BOX AND FRAME 75. (P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0549:0500-2020/004 00354 COMPLIED WITH ER/A PRI 597330-14 REV 0, REV 1, AND FINAL ERA 597330-14ADSDR DALA2025070304991Skin · damagedSHIP 3416 AFTER PAINT REMOVAL FROM C60-C64 IN VIASAT MOD AREA FOUND MULTIPLE AREAS WITH TOOLING DAMAGE. CORRECTIVE ACTION: REPAIRED PER ERA 627461-14 REV ORIGINAL. (1057514)SDR JR2R20250701244Skin · corrodedUPON REMOVAL OF AFT WIFI ANTENNA DOUBLER, FOUND UNDERLYING SKIN TO HAVE LIGHT CORROSION.SDR SWIA2026022575333Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA71070-670-53-21-2078 N613SK MXCODEID57339-PR - 6 EACH DENTS FOUND ABOVE REPLACED STR 21L BETWEEN FS421 AND FS453. COMPLIED WITH MHIRJ REO 670-53-21-2078, REV--, DATED 2021-07-07. THIS IS A TEMPORARY DISPOSITION VASDR DALA2025100807329Skin · damagedAFT CARGO DOOR AND DOOR FRAME: FUSELAGE SKIN DOOR CUTOUT AREA AFT EDGE DAMAGED. C/W AFT CARGO CORROSION ERA 627055-14 REV A. (1055785)SDR SIMA20250630007Doubler · corrodedCENTER FUSELAGE III INTERNAL DOUBLER BETWEEN FR 76-77 AND STGR 28R-27R IS CORRODED. (MAJOR REPAIR) (LEVEL 2 CORROSION). ACCOMPLISHED PERMANENT REPAIR ON CENTER FUSELAGE III INTERNAL DOUBLER BETWEEN FR 76 AND FR 77 AND BETWEEN STRINGERS 28 R AND 27 R IAW ERS-EJSDR SWIA20250630Skin · dentedADM# N430SY-8907 - DENT LOCATED BETWEEN FR19 AND FR20, STGR 27R AND 28R BEHIND FWD DRAIN MAST ABOUT 3 FEET AFT OF NOSE GEAR DOOR AND SLIGHTLY RIGHT OF CENTER MEASURING APROX. 1.5" LONG AND .05" WIDE. RE EVALUATE DAMAGE AND IMPROVE APPEARANCE IF POSSIBLE. (C-SDR SWIA2025070700630Skin · gougedFOUND 2 GOUGES (GOUGE 1: L=1.6 IN X W=0.080 IN. D=0.023. GOUGE 2: L=0.25 IN X W=0.090. D=0.020) BETWEEN FR21 & FR22 AND STGR15L & STGR16L ON PREXISTING DENT THAT HAS BEEN ENTERED INTO ALLOWABLE DAMAGE MAPPING. (FILED CLOSED)REPAIRED FUSELAGE BETWEEN FR21 & FSDR DALA2025070705010Skin · gouged(LOG 1054860) FWD CARGO DOOR CUT OUT, FUSELAGE INTERNAL DOUBLER AND SKIN GOUGED APPROX 18IN ABOVE AFT LOWER CORNER. INSTALLED REPAIR INNER & OUTER DOUBLERS AND SKIN AND INTERNAL DOUBLER FILLERS IAW B737-900 SRM 53-00-01 REPAIR 24.SDR UIEA2025062300797Skin · crackedDURING HFEC OPEN HOLE INSPECTION ON RH FWD ENTRY DOOR CUTOUT AFT LOWER CORNER. FOUND SECOND HOLE FROM BOTTOM WITH CRACK INDICATION AT 1 O'CLOCK POSITON VIEW LOOKING INBOARD. REPAIR CARRIED OUT IAW SRM 53-10-01 REPAIR 1 REV. 52. NO FURTHER DEFECTS NOTED.SDR UIEA2025062300798Skin · crackedDURING HFEC OPEN HOLE INSPECTION ON LT FWD ENTRY DOOR CUTOUT AFT LOWER CORNER FOUND SECOND HOLE FROM BOTTOM WITH CRACK INDICATION AT 10 O'CLOCK & 4 O'CLOCK POSITION VIEW LOOKING INBOARD. REPAIR CARRIED OUT IAW SRM 53-10-01 REPAIR 1 REV. 52. NO FURTHER DEFECTSSDR AALA202507045446Skin Panel · deformedAIRCRAFT IN BASE MAINTENANCE: DERFORMATION ON EXTERNAL SKIN LOCATED BTW FR73 TO FR74 AND STR 32R TO STR 32L. MAINTENANCE PERFORMED PERMANENT REPAIR EXTERNAL SKIN LOCATED BTW FR73 TO FR74 AND STR 32R TO STR 32L AT LOWER FUSELAGE IAW A319 SRM 53-51-29-300-002 RESDR SWIA2025070100629Skin · damagedFUSELAGE SUSTAINED SKIN DAMAGE FROM LADDER ON RT AFT SIDE OF FUSELAGE, BETWEEN HYDRAULIC SYSTEM #3 ACCUMULATOR SERVICING ACCESS PANEL AND AFT EQUIPMENT BAY MAJOR REPAIR, COMPLIED WITH PERMANENT REPAIR OF RT AFT SIDE OF FUSELAGE SKIN, BETWEEN HYDRAULIC SYSTEMSDR CALA2025070106108Skin · crackedEXT PWR RECEPTACLE CUT OUT INNER DOUBLER CRACKED AT LWR END. ACCOMPLISHED REPAIR AT EXT PWR RECEPTACLE CUT OUT INNER DOUBLER REF SRM 53-10-15-2R-4.SDR SWIA2025063000029Skin · ground damageFUSELAGE SUSTAINED SKIN DAMAGE FROM LADDER ON RT AFT SIDE OF FUSELAGE, BETWEEN HYDRAULIC SYSTEM #3 ACCUMULATOR SERVICING ACCESS PANEL AND AFT EQUIPMENT BAY (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESSSDR SWIA2025090200628Skin · gouged3 GOUGES TO FUSELAGE SKIN BETWEEN FS589.00 - FS605.00 AND STR 23R-24R (C-CHECK RO 08/29/2025)BLENDED 3 GOUGES TO FUSELAGE SKIN BETWEEN FS589.00 - FS605.00 AND STR 23R-24R WITH REFERENCE TO REO 601R-53-61-8350 REV-- DATED 2025-06-28. REFERENCE CP 30398090 FORSDR SWAA2025071486304Doubler · crackedEGPR DOOR CUTOUT LOWER DOUBLER IS CRACKED. ACCOMPLISHED REPAIR ON EGPR DOOR CUTOUT LOWER DOUBLER IAW SRM 53-10-15-2R-4.
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