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 SWAA2023091992044Skin · corrodedCORROSION ON OUTER FUSELAGE CROWN SKIN COMMON TO FASTENER ROWS FROM STATION 1016 TO 1016+17; STRINGER 0; STRINGER S-1R; STRINGER S-1L; AND BL 12 LEFT AND RIGHT. CORRECTION TO FAULT NAME LOCATION SHOULD BE STR 1 AND STR 2L AND STR 2R LBL 12 AND RBL 12<[01] VERISDR IPXA2023091994197Skin · corrodedINSPECTION TYPE:2C*MAJOR REPAIR* WASTE TANK AREA STA Y=1997.750 AND Y=2007.00 LONGERON 43L - 44L FUSELAGE SKIN HAS CORROSION.REPAIRED CORRODED SKIN AT THE WASTE TANK AREA STA Y=1997.750 AND Y=2007.00 LONGERON 43L - 44L FUSELAGE IAW VTSAA EA 011-5330-01-B0088 ISDR YENA2023082400970Unknown · unknownDURING HEAVY MAINTENANCE: WINGS / CENTER WING BOX / TOP SKIN PANEL / UPPER SURFACE / BETWEEN FR41-42 AT BEAM Y1292 / CORROSION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR FDEA202308221476Panel · corrodedNOSE WHEEL WELL PANEL 117AL HAS MINOR SURFACE CORROSION. BLENDED CORROSION FROM PANEL, ORG MATERIAL WAS .100, REMOVED .009 OF MATERIAL, .091 REMAINS, FOUND TO BE IN LIMITS PER B757 SRM 53-10-14-1A DETAIL IV. ALODINED PANEL PER B757 AMM 51-21-04. PRIMED PANESDR DALA2023082306870Unknown · unknown(LOG 2930763) DURING MAINTENANCE OF THE A/C B737-900ER SHIP NUMBER 3826 ON MXA MRO AT MEX, RE-EVALUATING 5 DENTS ON LH FUSELAGE SKIN BTWN STA 303.9 AND 380 & STGRS WITH TASK CARDS 2020-9002/002, /003, /004, /005 & /006, IT WAS DETERMINED THAT, FOUR (4) DENTS WSDR IPXA2023082293994Skin · dentedINSPECTION TYPE:CDENT AT FR 92 BETWEEN STR 16R AND 19RREPAIRED AREA IAW SRM 53-12-12SDR SWIA2023110100821Unknown · chafedRH AILERON UPPER LEADING EDGE SKIN SHROUD CHAFFING FROM INBOARD TO OUTBOARD SIDES (C-CHECK RO 11/4/2023) REPLACED RH AILERON UPPER LEADING EDGE SKIN REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DWG: CC670-13000 REV D. COMPLIESDR SWIA20231023821Unknown · damagedSTUCK SCREW IN A DAMAGED DOME NUT ON PANEL 195BB (CAMP# 27055473) (C-CHECK RO 10/21/2023) REMOVED AND INSTALLED 1 EA NEW DOME NUT AT FUSELAGE SKIN USED FOR ATTACHING PANEL 195BB PER CRJ 200 SRM 51-42-06COMPLIED WITH STEPS 1 TO 4 OF MHIRJ REO 601R-53-61-807SDR DALA2023082306856Unknown · unknownSHIP 3413 DAMAGE TOLERANCE EVALUATION (DTE) IS REQUIRED. ERA 607822-14 WAS ISSUED FOR LIGHTNING STRIKE REPAIRS TO THE FUSELAGE SKIN AND WINDOW FRAMES, FR 19 TO 22 RHS. CORRECTIVE ACTION: SECTION II PERMANENT REPAIR INSTRUCTIONS ADDED IN ER/A 607822-14. (292956SDR DALA2023082306850Unknown · unknownSHIP 3274 PULLING UP ON FUSELAGE LOC. FR 52 TO FR 70 BTW STR 19 L/H TO STR 19 R/H. CORRECTIVE ACTION: REPAIRED PER A320 SRM 53-41-11. (2929766)SDR HNAA2023091800330Unknown · unknownE991907 : FUSELAGE EXTERNAL SKIN PREVIOUS REPAIR DOUBLER BETWEEN FR 6/7 AND STR 2L/2R HAS NO REPAIR INFORMATION. RE-ACCOMPLISHED REPAIR ON FWD FUSELAGE II SKIN FR 6-7 STGR 2L-2R IAW ETD2023-145-021605 REV. A, EO1-53-23-0276SDR SIMA20230820001Unknown · unknownSUSPECT CORROSION ON AFT POTABLE WATER DRAIN MAST INTERNAL SKIN SUPPORT DOUBLER. (LEVEL 2 CORROSION)-C/A-REMOVED AND REPLACED AFT POTABLE WATER DRAIN MAST INTERNAL SKIN SUPPORT DOUBLER IAW EMB 170 SRM 51-40-08.SDR DALA2023082106800Unknown · unknownSHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN FROM FRAMES FR26 TO FR26.1 AND BETWEEN STRINGERS 1R/1L ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 610895-14, VALIDATE ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING ALTERATION INSTASDR DALA2023082106796Unknown · unknownSHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN FUSELAGE A T FR84, STR2A LH ON TAIL. CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING MODIFICATION INSTALLED AS PER EM 5330-SDR DALA2023082106795Unknown · unknownSHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN FUSELAGE AT FR84, STR2A RH ON TAIL. CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING MODIFICATION INSTALLED AS PER EM 5330-0SDR DALA2023082106794Unknown · unknownSHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR 4L OUTER SKIN LOWER AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING REPAIR INSTALLED PER A330 SRM 53-13-0SDR DALA2023082106793Unknown · unknownSHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR DOOR 4L OUTER SKIN LOWER AFT EDGE AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: COMPLIED WITH ER/A PRI 610895-14, VALIDATED ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING REPAIR INSTALLED PER DELTA ESDR DALA2023082106790Unknown · unknownSHIP 3357 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN FR53 AND FR54 BTW STR1L AND STR1R ON UPPER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH PRI 610895-14, VALIDATE ER/A 610895-14 MATCHES WITH PRI 610895-14. EXISTING ALTERATION INSTALLED PER 2330-01325-0SDR DALA2023082106788Unknown · unknownCONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN FROM FRAMES FR30 TO FR31, AND BTW STR1L AND STR1R ON UPPER FUSELAGE. COMPLIED WITH PRI 610895-14, VALIDATE ER/A 610895-14 MATCHES WITH PRI 600895-14. EXISTING ALTERATION INSTALLED PER 2325-01059-03. INSTALLASDR DALA2023082106780Unknown · unknown(LOG 2925391) CORROSION ON BELLY UNDER FWD AIR PHONE ANT BETWEEN FS 747-767. C/W ALL STEPS PRI 611386-14 REV 2.SDR VNAA202308190014Skin · corrodedAFTER REMOVAL OF THE TCAS OMNIDIRECTIONAL ANTENNA: CORROSIÓN WAS FOUND ON FUSELAGE SKIN(SETTLEMENT AREA) OF ANTENNA BTW FS 295.00 AND FS 310.00 AND STGR 26LH TO STRG 26RH. CORROSIÓN ON SETTLEMENT AREA OF ANTENNA BTW FS 295.00 AND FS 310.00 AND STGR 26LH TO SSDR WX0A1900010031852Unknown · unknownXTERNAL FUSELAGE BTW FR79-FR80 AND STGR2-3 L/H NEED PERMANENT REPAIR WITHIN 500 FC- ACCOMPLISHED STS EA 72-2023-018 PERM REPAIR REQ, SRM TASK 53-51-11-300-064. / EXTERNAL FUSELAGE BTW FR79-FR80 AND STGR2-3 L/H PERMANENTLY REPAIRED AS PER SRM TASK 53-51-11-SDR SWIA202308280018Unknown · gougedTRANSFER FROM EAML 1194655 : FOUND GOUGE IN THE FORWARD FUSELAGE SKIN LH SIDE JUST FWD OF THE MCD, LOCATED BETWEEN FRAMES FR 10-11 AND STRG 15L-17L. THE DEPTH OF THE SCRATCH IS 1/32€?. THE AREA SCRATCH IS DENTED. THE DENTED AREA IS 2.5L€? X 1.5W€? X .05€?DSDR DALA2023082106775Unknown · unknown(LOG 2924099) WHILE ON THE LINE IN DTW, MTC REPORTED DAMAGE COMMON TO THE FUSELAGE SKIN UNDERLYING THE FWD TFTS AIRPHONE ANTENNA AT BS 747 - 767 AND BL0. THE ANTENNA WAS REMOVED AND MTC FOUND CORROSION TO THE FUSELAGE SKIN UNDERNEATH THE BASE OF THE ANTENNA. DSDR REXA2022082100680Skin · corroded"FUSELAGE SKIN IS CORRODED UNDER AFT CARGO DOOR PROTECTOR PLATE BETWEEN F.S. 1031 TO F.S. 1051. REMOVED CORROSION IN FUSELAGE SKIN UNDER AFT CARGO DOOR PROTECTOR PLATE, STRG 19L BETWEEN FS. 1031.0 TO FS. 1051.0, IAW CRJ900 SRM 51-21-06-001-001-A01. ORIGINAL THSDR REXA2022082100679Skin · corroded"AFT BAGGAGE BAY DOOR SILL CORRODED BETWEEN FS 1000 AND FS1047 AT STRG17L AFT BAGGAGE BAY DOOR SILL CORRODED BETWEEN FS 1000 AND FS1047 AT STRG17L. REMOVED CORROSION ON AFT BAGGAGE BAY DOOR SILL BETWEEN FS1000 AND FS1047 AT STRG17L IAW CRJ900 SRM 53-61-23-201SDR VNAA202308180023Skin · dentedSEVERAL DENTS (16EAS) ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH. SEVERAL DENTS (16EAS) ON FUSELAGE SKIN SETTLEMENT AREA OF VENTRAL FIN FAIRING RH WERE REPAIRED PER EA 23-C9-53-0943 REV. IR SECTION III-PERMANENT REPAIR.SDR REXA2022081700666Skin · corroded"LH FLOOR SILL IS CORRODED AT FS 661+16. LH FLOOR SILL IS CORRODED AT FS 661+16. CORROSION REQUIRES REMOVAL REMOVED CORROSION AT FS 661+16 IAW CRJ900 SRM 53-00-45-201-001-A01 STEPS 6A-E UT REQUIRED FOR MRT PERFORMED UT THICKNESS OF LH FLOOR SILL FS661+16 REWOSDR VNAA202308180008Skin · wornWEAR ON FUSELAGE SKIN BTW STA 897.70 AND STA 913 STGR 27 ALSO WEAR ON SEVERAL FASTENER HEADS BTW STA. 913 AND STA 927 STGR 27. FUSELAGE SKIN BTW STA 897.70 AND STA 913 STGR 27 BTW STA 913 AND STA 927 STGR 27 WAS REPAIRED PER EA 23-C9-53-0988 REV. IR SECTION ISDR VNAA202308180007Skin · corrodedINITIAL INSPECTION: CORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT. CORROSION ON INTERCOSTALS (2 EAS) IN STA. FS= 349 TO FS= 364 NEAR STGR 27 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ/900 SRM 51-2SDR VNAA202308180006Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN BTW FS280.00 AND FS 295.00 AND STGR 26RH AND 25RH. INTERNAL FUSELAGE SKIN BTW FS280.00 AND FS 295.00 AND STGR 26RH AND 25RH WAS REPAIRED PER EA 23-C9-53-0904 REV. IR SECTION III - PERMANENT REPAIRSDR VNAA202308180005Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN BETWEEN FS 280.00 AND 295.00 AND STGR 25RH AND 24RH. INTERNAL FUSELAGE SKIN BETWEEN FS 280.00 AND 295.00 AND STGR 25RH AND 24RH WAS REPAIRED PER EA 23-C9-53-0904 REV. IR SECTION III - PERMANENT REPAIRSDR VNAA202308180001Skin · unknownBURN MARK BY LIGHTNING STRIKE IN TRAILING EDGE OF RH ELEVATOR LOCATED BETWEEN RIB NO. 19./ RIB NO. 20. LIGHTNING STRIKE IN TRAILING EDGE OF RH ELEVATOR LOCATED BETWEEN RIB NO. 19./ RIB NO. 20 WAS REPAIRED PER EA 23-C9-55-0930 REV IR SECTION III PERMANENT REPASDR SWIA2023082417Unknown · scratchedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA85373-SRM 53-10-01/AD01,MXCODEID68972-PR - FIRST OFFICER FOUND 2 SCRATCHES FORWARD OF MAIN CABIN DOOR BELOW CAPTAINS SIDE FORWARD FUSELAGE. INSPECTED 2 SCRATCHES ON LH FUSELAGE, FWD OF L1 DOOR. BLENDED DAMAGED AREA PERSDR VNAA202308170006Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (642BB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (642BB, 686AB, 692AB, 695AB, 697AB) AT RH WING LOWER SKIN WERE BLENDED OUT, EVALUATED WITHIN LIMITS AND REPAIRED PER EA 23SDR VNAA202308170005Skin · nickedSEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5. SEVERAL NICKS ON LOWER SKIN OF LH INBOARD FLAP FLS 15.00 TO FLS 65.5 WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND BTW FLS15.00 AND FLS42.00 WAS EVALUATED OUT OF LIMITS PER CRJ900 SDR VNAA202308170004Skin · wornWEAR ON AREA OF SETTLEMENT OF FAIRINGS (542BB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN. WEAR ON AREA OF SETTLEMENT OF FAIRINGS (542BB, 586AB, 592AB, 595AB, 597AB) AT LH WING LOWER SKIN WERE REPAIRED PER EA 23-C9-57-1085 REV IR, EA 23-C9-57-1084 REV SDR VNAA202308170003Skin · nickedSEVERAL NICKS ON FUSELAGE SKIN, ON STA 1000 TO STA 1096.75 AND BTW STGR 17LH TO STGR 11LH. SEVERAL NICKS ON FUSELAGE SKIN, ON STA 1000 TO STA 1096.75 AND BTW STGR 17LH TO STGR 11LH WERE BLEND OUT PER CRJ900 SRM 51-12-00-001-001-A01 AND WERE EVALUATED IS WITHISDR VNAA202308170002Skin · nickedSEVERAL NICKS ON FUSELAGE SKIN, ON STA 977.00 TO STA 1069.75 AND BTW STGR 21LH TO STGR 22RH.SDR R61A2023090700484Skin · corrodedWHILE REMOVING RIVETS FOUND CORROSION ON SKIN BETWEEN FRAMES 88 - 89 AND STRINGERS 29L - 29R. PERFORMED TEMPORARY REPAIR BY CUTOUT AND DOUBLER REPAIR AT FRAMES 88 - 89 AND STRINGERS 29L - 29R. IN ACCORDANCE WITH, REF ETD2023-170--020249.SDR CALA2023081802565Skin · dentedFLIGHT DECK FLOOR SKIN PANEL HAS A DENT AT STA 259 REF N/R 9205005 AT STA 259 LBL 11 EVALUATED DENT FOUND OUT OF LIMITS PER REF B737 SRM 53-01-51-11-1 ALLOWABLE DAMAGE 1 DETAIL D REMOVED EXISTING REPAIR PER SRM 53-40-02-0G-0 REPAIR FLIGHT DECK FLOOR WBC AT STASDR SIMA20230816001Unknown · unknownDENT IN RVSM AREA BETWEEN FR01 AND FR02, AND STR21R AND STR22R. (MAJOR REPAIR)-C/A-REPAIRED IAW ERS-EJ-53MR-4844.SDR DALA2023081806720Unknown · unknownLH NLG SKIN PANEL 5911400-99 DAMAGED DURING LANDING. REF NR 066: C/W PRI 610190-14 REV 0. C/W PRI 610190-14 REV 1. C/W PRI 610190-14 REV 2. C/W PRI 610190-14 REV 3. C/W ERA 610190-14 REV ORIG. PRI REVS 0-3 MATCH FINAL ERA. (LP #2920961)SDR YENA2023081600949Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR69-71 & STGR 30R-33R / AFT LAV VENT OUTLET / CORROSION. TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR DALA2023081806739Skin · corroded(LOG 2919657) CORROSION FOUND ON EXTERNAL SIDE OF FUSELAGE SKIN BS 679 TO 706 BETWEEN S-1 AND S-2R. C/W ER/A 611032-14 REV ORIGINAL SECTION 1.SDR HNAA2023102300364Unknown · unknownE990366 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 79 BETWEEN STRINGERS 4L-5L. REMOVED CRACKS FROM RIVET HOLE ON FR 79 BETWEEN STGR 4L-5L AND INSTALLED FABRICATED REPAIR BUSHING IAW EMB 145 SRM 53-32-01-RE STEP 9.E, 53-23-01-RE ITEM 9 AND EO1-53-23-030SDR HNAA2023102300363Unknown · unknownE990365 POSSIBLE CRACK ON EXTERNAL FUSELAGE SKIN AT FRAME 78 BETWEEN STRINGERS 4L-5L. : REMOVED CRACKS FROM RIVET HOLE ON FR 78 BETWEEN STGR 4L-5L AND INSTALLED FABRICATED REPAIR BUSHING IAW EMB 145 SRM 53-32-01-RE STEP 9.E, 53-23-01 RE ITEM 9 AND EO1-53-23-SDR SWAA2023083189558Intercostal · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500D TO BS520 AT LEVEL STR28L FWD CARGO COMPARTMENT 2023-508493<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS500D TO BS520 AT LEVEL STR28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-0SDR SWAA2023083195740Fastener · crackedCRACK WEB - INTERCOSTAL LOCATED BETWEEN BS500D TO BS520 AT LEVEL STR28L FWD CARGO COMPARTMENT 2023-508493<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS500D TO BS520 AT LEVEL STR28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-0SDR SWAA2023083189557Angle · crackedCRACK SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R/STR3R AT PASSENGER CABIN 2023-508498<[01] REPLACED SUPPORT ANGLE LOC. BS867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 146A7901 REV. ?.;[02] CORRECTED STEP 1
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