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 DALA2024021201959Skin · dentedSHIP 3125 THREE DENTS IN FUSELAGE UNDER FWD CARGO DOOR. CORRECTIVE ACTION: REPAIRED PER ER/A 501814-14. (0194327)SDR DALA2024021101845Skin · handler errorAIRCRAFT 3005, DURING BRIDGE CHECK MSP, A TAIL STAND CONTACTED THE AIRCRAFT RESULTING IN GROUND DAMAGE TO THE AIRCRAFT. THIS ERA COVERS AREAS DAMAGE CONSISTS OF A DENTS TO THE FUSELAGE SKIN. SHEARED FASTENERS BETWEEN STR 34 AND FWD END FITTING REQUIRE REMOVAL.SDR GTIA2024021037898Skin · dentedLEFT SIDE OF FUSELAGE DENT ON UPPER SKIN PANEL FRAME 2 RAF-001 CREATED -ACCOMPLISHED PERMANENT CAT A REPAIR PER AIRBUS RDAF #81347340/005/2024#A. REF HAECO REO #L24856. NO REINSPECTION REQUIREDSDR DALA2024021001841Skin · handler errorAIRCRAFT 3005, WHILE JACKING NOSE FOR SERVICING TAIL SUPPORT STAND WAS LEFT IN PLACE CAUSING DAMAGE. CORRECTIVE ACTION: REMOVED DAMAGED AREA, AND INSTALLED REPAIR PARTS PER ER/A 615438-14. (LP 0194492)SDR SCNA20240309078Skin · corrodedLOWER FUSELAGE, BETWEEN STA 727A AND 727B AND BETWEEN STR 27LH AND 27RH, SKIN WITH CORROSION. PERFORMED PERMANENT REPAIR AT EXTERNAL SKIN SECTION FROM STA 727A AND STA 727B BETWEEN STR 27R AND STR27L DUE TO BLEND OUT AREA NOT PERMITTED IAW COOPESA EO# COOO-ESDR R61A2024022300086Doubler · misinstalledDOUBLER REPAIR INSTALLED AT FR 11-12 STR 23R-25R FOUND IMPROPERLY INSTALLED. MX REPLACED DOUBLER SPLICE IAW ETD 2024-170-003696 REV A. MAJOR REPAIR.SDR DALA2024021001842Skin · handler errorAIRCRAFT 3005, DURING BRIDGE CHECK MSP, A TAIL STAND CONTACTED THE AIRCRAFT RESULTING IN GROUND DAMAGE TO THE AIRCRAFT. THIS ERA COVERS AREAS DAMAGE CONSISTS OF A DENTS TO THE FUSELAGE SKIN. IN AREA OF / FR70-FR71, STR 32L-32R. ACCOMPLISH TRIM OUT OF THE CREASSDR DALA2024021001840Skin · damagedAIRCRAFT 3005, DAMAGE TOLERANCE EVALUATION (DTE) REQUIRED. ERA 615438-14 SECTION ISSUED FOR FUSELAGE SKIN REPAIR AT FR 70 - FR 71, S-41L TO S-40R. CORRECTIVE ACTION: REMOVED DAMAGED AREA, AND INSTALLED REPAIR PARTS PER ER/A 615438-14. DEFERRED TO MONITOR PER ESDR DALA2024020801698Skin · gougedSHIP 3402 GOUGE AT AFT CARGO CUTOUT, FWD LWR CORNER. CORRECTIVE ACTION: COMPLIED WITH A330 SRM 53-41-11-205-045. (5031449)SDR DALA2024020801687Skin · crackedCRACKS (2 EA) ON FUSELAGE SKIN BTW STA Y=1076 AND STA Y=1087 BTW LONG 13R AND LONG 14R AT AFT FUSELAGE. SUMMARY OF NRC 0514: CRACKS (2 EA) ON FUSELAGE SKIN BTW STA Y=1076 AND STA Y=1087 BTW LONG 13R AND LONG 14R AT AFT FUSELAGE. WERE REPAIRED PER PRI 614977-14SDR HNAA2024022700139Skin · damagedE020843 BURN MARK ON FR26 BETWEEN STRINGERS 18R - 19R. REPAIRED BURN MARK AT FR26 BETWEEN STRINGERS 18R - 19R IAW EMB ETD2024-145-003973 REV. A AND EO1-53-24-0127SDR HNAA2024022700138Skin · damagedE020842 BURN MARK ON SKIN AT FR14 BETWEEN STRINGERS 20R - 21R. REPAIRED BURN MARK ON EXTERNAL SKIN AT FR14 BETWEEN STRINGERS 20R-21R IAW EMBRAER ETD2024-145-004117 AND EO1-53-24-0128SDR HNAA2024022700137Skin · damagedE020841 BURN MARK ON FR22 BETWEEN STRINGERS 18R - 19R. PERFORMED THE CUT OUT OF THE DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER ON BURN MARK AT FR 22 BETWEEN STR 18R-19R IAW EMBRAER ETD2024-145-004115 AND EO1-53-24-0138SDR DALA2024020801686Skin · crackedCRACK ON FUSELAGE SKIN ON STA Y=1087 BTW LONG 13L AND LONG 14L AT AFT FUSELAGE. SUMMARY OF NRC 00513: FUSELAGE SKIN ON STA Y=1087 BTW LONG 13L AND LONG 14L AT AFT FUSELAGE WAS REPAIRED PER PRI 614985-14 REV 3 AND ERA 614985-14 REV ORIGINAL SECTION I: PERMANENTSDR IXXA2024020604Skin · crackedCRACK INDICATION FWD DOOR CUTOUT STA332-339 S19LSDR VNAA202402050027Skin · nickedSEVERAL NICKS ON SKIN (ZONE 1) BTW FS501.00 TO FS517.00 AND STGR 21 LH TO STGR 25 LH (ZONA 2) BTW FS 613.00 TO FS 629.00 AND STGR 21 LH TO STGR 25 LH AT FUSELAGE. SKIN (ZONE 1) BTW FS501.00 TO FS517.00 AND STGR 21 LH TO STGR 25 LH (ZONA 2) BTW FS 613.00 TO FSDR VNAA202402050026Skin · damagedLIGHTING STRIKE BTW FS280.00 TO FS295.00 AND BTW STGR 17 TO STGR 16 RH (1EA) LIGHTING STRIKE BTW FS379.00 TO FS394.00 AND BTW STGR 17 TO STGR 18 RH (1EA) AT SELAGE SKIN. LIGHTING STRIKE BTW FS280.00 TO FS295.00 AND BTW STGR 17 TO STGR 16 RH (1EA) LIGHTING STSDR VNAA202402050025Skin · nickedSEVERAL NICKS ON FUSELAGE SKIN BTW STA 1000.00 TO STA 1069.75 AND BTW STGR 21RH TO STGR 27. SEVERAL NICKS ON FUSELAGE SKIN BTW STA 1000.00 TO STA 1069.75 AND BTW STGR 21RH TO STGR 27 WAS REPAIRED PER REO 690-53-61-1331 REV. --SDR VNAA202402050020Skin · dentedGOUGE AND DENT BELOW VENTRAL FIN FARING RH AREA BTW FS 1069.75 - FS 1088.00 AND STGR 21 - 22 RH AT REAR FUSELAGE. BELOW VENTRAL FIN FARING RH AREA BTW FS 1069.75 - FS 1088.00 AND STGR 21 - 22 RH AT REAR FUSELAGE WAS REPAIRED PER REO 690-53-00-548 REV. --SDR EE4Y2023122819076Skin Panel · damagedFORWARD FUSELAGE, AT FR03+215MM, STRINGER 24RH+100MM, LOWER EXTERNAL SKIN WITH LIGHTNING STRIKE. NOTE: THE FUSELAGE SKIN WAS REPAIRED AS PER EMBRAER ETD2023-190-030945 GUIDELINES AS STATED IN ENGINEERING ORDER NO: COO-EO-2023-18945-R00 INSTRUCTIONS ( FOR ADDITSDR DALA2024020601580Skin · bentBENT ON EDGE EXTERNAL SKIN AFT UPPER, AFT LOWER, AND BEAM #4 AT SERVICE DOOR L1. SUMMARY OF NRC 00069: EXTERNAL SKIN ON AFT UPPER EDGE AND EDGE OF EXTERNAL SKIN AT BEAM #4 WAS CONFORMED PER B717 SRM-51-20-09-0G. AFT LOWER EDGE OF EXTERNAL SKIN AT SERVICE DOOR SDR VNAA202404150003Skin · dentedSEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT/RIGHT VENTRAL FIN FAIRING BTW FS 1069.75 TO REAR SPAR DATUM STABILIZER 67.5%, BTW STGR 22LH/RH TO STGR 21LH/RH. SEVERAL DENTS ON FUSELAGE SKIN, SETTLEMNT AREA OF LEFT/RIGHT VENTRAL FIN FAIRING BTW FS 10SDR VNAA202403230016Skin · dentedSEVERAL DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING. DENTS ON EXTERNAL FUSELAGE SKIN IN AREA COVERED BY RH VENTRAL FIN FAIRING WERE REPAIRED PER REO 690-53-61-1349 REV --SDR SWAA2024031248861Doubler · crackedGROUND POWER DOOR INTERNAL DOUBLER TORN;CRACK FWD LOWER CORNER<[01] ACCOMPLISHED PERMANENT REPAIR CATEGORY B AT EXTERNAL POWER RECEPTACLE CUTOUT AS PER B737-700 SRM 53-10-15-2R-5 REPAIR 5. REF TO STEP 13 FOR FURTHER INSPECTION REQUIREMENTS.;[02] VERIFIED FINALSDR SWAA2024030748929Doubler · crackedEXTERNAL POWER DOOR CUTOUT SKIN DOUBLER IS CRACK AT AFT CENTER EDGE<[01] ACCOMPLISHED TRIMOUT REPAIR AT ELECTRICAL GROUND POWER RECEPTACLE AFT CENTER EDGE IN REF B737-700 SRM 53-10-15-2R-4 FIG 203.;[02] VERIFIED STEP 1SDR DALA2024020901757Doubler · damagedSHIP 1604 FWD CARGO COMPARTMENT FOUND 01EA FUSELAGE REPAIRED DOUBLE FASTENER IN POOR CONDITION AT STA434 TO STA456. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 615309-14 (0187820)SDR UIEA2024012800051Skin · corrodedFUSELAGE SKIN AT LOWER LOBE CIRCUMFERENTIAL SPLICE LOCATION STA 1715 S45R FOUND CORROSION APPROX 1" X 1"(<P>SKIN REPAIRED AS PER SRM 53-00-01-2R-1 REPAIR 1 FIG 201 DETAIL I. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024020100060Skin · corrodedFX R/H AIRCON BAY STA 1000-1003 CENTER SECTION LOWER SURFACE CORR. AT RBL 15" - RBL 29"(<P>SKIN CORROSION AREA REPAIRED AS PER RI-57-10-16703 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100062Skin · crackedFX - FUSELAGE SKIN STA 1680 STR 41R FOUND CORR CRACK(<P>SKIN REPAIRED AS PER RI-53-61-16685 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020100066Skin · chafedFX SKIN STA 724 STR 0-1R FOUND CHAFING.(<P>CHAFING AREA REPAIRED AS PER RI NO. RI-53-20-16706 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024020200068Skin · corrodedFX - AIRCON BAY L/H STA 1240 CENTER WING LWR SURFACE CORR AT LBL 91" - LBL 102" AND LBL 105" - LBL 113".(<P>SKIN CORROSION AREA REPAIRED AS PER RI NO. RI-57-10-16704 REV.A. NO FURTHER DEFECTS NOTED.</P>)SDR VNAA202402050009Skin · corrodedAFTER REMOVAL OF THE AFT DRAIN MAST, PITTING CORROSION AND WEAR ON THE SKIN WERE FOUND. CORRECTIVE ACTION: SKIN OF SETTLEMENT AREA OF DRAIN MAST WAS REPAIRED PER REO 690-53-61-1338 REV. --SDR VNAA202402050007Skin · dentedDENTS ON FUSELAGE SKIN, SETTLEMENT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1162.00 TO REAR SPAR DATUM STABILIZER 55% BTW STGR 20LH TO STGR 21 LH. CORRECTIVE ACTION: FUSELAGE SKIN, SETTLEMENT AREA OF LEFT VENTRAL FIN FAIRING BTW FS 1162.00 TO REAR SPAR DATUM SSDR GTIA2024020637833Skin · dentedREF LOG PAGE 2993502-01 FWD L/H SIDE FUSELAGE GOT HIT BY A BAGGAGE CART. MEASURES 8.0"L X 8.0" W X .280" D. RAF 01 CREATED-ACCOMPLISHED REPAIR OF LH FWD SIDE LOWER FUSE SKIN FR 13-14 STR 36L LOWER STRG LH PER REO L24851 AND EA 5311-2410 AND RDAF 81338012/019/2SDR SWAA2024030748232Doubler · corrodedFUSELAGE LWR SKIN DOUBLER HAS SURFACE CORROSION @ STA 685 + 10; BETWEEN STR-1 AND STR-2R; MARKED; PICS ATTACHED.<[01] NO ALLOWABLE DAMAGE LIMITS ENTRIES FOUND IN SRM FOR THIS ITEM. COVER PLATE ITEM 7340372 REPAIRED BY REPLACEMENT. PER SRM 51-10-02 PARAGRAPH 9.SDR CALA2024020500320Skin · corrodedAFT FUSELAGE TOILET WASTE DISPOSAL VENT/EXHAUST IS CORRODED 204- 05. () REPAIRED AFT TOILET WASTE VENT AREA BY DOUBLER IAW SRM 53-41-11- 300-004 MAJOR REPAIR CAT A 44-0008 ATTACHED. WORK A CCOMPLISHED AT ST ENGINEERING OF MOBILE AT BFM ON NR#: 85591SDR DALA2024020401514Skin · handler errorAIRCRAFT 3082, DURING LAYOVER IN MSP, A CATERING TRUCK HAD CONTACTED THE AIRCRAFT AFT OF THE L4 DOOR. THE FUSELAGE SKIN SUSTAINED A LARGE PUNCTURE DAMAGE BETWEEN FR 71-72 AND STR 26L 28L AND INCLUDED SOME ADDITIONAL DENTING IN THE LOCAL AREA. THE FUSELAGE SKSDR R61A2024020300067Doubler · corrodedWHILE IN HEAVY CHECK - CORROSION ON INTERNAL DOUBLER FOR AFT HEATED DRAIN MAST AT FR 86-87 STGR 27R-28R. REMOVED AND REPLACED INTERNAL DOUBLER FOR AFT HEATED DRAIN MAST BETWEEN FR 86-87 STGR 27R-28R.SDR R61A2024020300058Doubler · corrodedWHILE IN HEAVY CHECK - "WASTE BOX INTERNAL DOUBLER CORRODED. REMOVED AND REPLACED WASTE BOX INTERNAL DOUBLER BETWEEN FR 88-89 STGR 26R-28R. REF EMB SRM 51-40-08."SDR NACA2024020200002Skin · crackedACCORDING TO AD 2019-08-03 INTERNAL OPEN HOLE HFEC INSPECTION , 2 EA FASTENERS HOLE SKIN CRACKED(UP L: 0.4" LOWER L:0.35") AT BS380 IB CHORD BETWEEN S20L AND S21L. REPAIRED DAMAGED CHORD AT BS 380L BETWEEN STRANGER S21 & S22 AS PER NAC EO 737-53-3507 REV. IRSDR SWAA2024030747945Doubler · crackedEXTERNAL POWER DOOR CUTOUT SKIN DOUBLER IS CRACK AT AFT. LOWER EDGE.<[01] ACCOMPLISHED TRIMOUT REPAIR AT ELECTRICAL GROUND POWER RECEPTACLE AFT LOWER EDGE IN REF B737-700 SRM 53-10-15-1A-4 FIG 104 DETAIL A.;[02] VERIFIED STEP 1SDR CALA2024020500322Skin · crackedEA 5300-01986 REV A OP.001 ( AD 2008- 16-12 ) FX SKIN STA 2195.75 STR 6L-7L 1EA CRACK FOUND NOT MORE THAN 1 INCH CREATE OP.007 FOR REPAIR , TASK TRANSFER TO WO.2724398. FUSELAGE SKIN REPAIRED AS PER EA5300-01986 REV A OP007 AND ECRA 5385-01016 REV - JUST AT SDR NACA2024020100004Skin · dentedDENT (3.2" X 2.0" IN AREA, MAX. DEPTH= 0.080") AT BS STA 1148, RBL+4". PERFORM PERMANENT REPAIR AT BS STA 1148 RBL+4" PER NAC EO737-53-0336SDR IPXA2024031445752Skin · corroded*** SUPPLEMENTAL SDR *** FAULT - CORROSION - SKIN , AFT FACE OF R/H WING GEAR W/W FWD BULKHEAD CENTER TANK FUEL PUMP CUTOUT , STA 1241. (REPAIR) REMOVED CORROSION AREA I.A.W SRM 51-10-02-0G-0 REV.99. I.A.W AMM 28-31-01-404-011-002 REV.109 INSTALL CENTER WING TSDR SWAA2024030147681Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AL BELLY FAIRING FWD EDGE APPROXIMATELY 16 INCHES FROM TOP EDGE AT LOWER FUSELAGE 2024-77386<[01] TOOL USED:CALIPER PN: 500-197-30 SN: A21141912; DUE DATE: 24-DEC-24.;[02] TOOL USED: SCALE P/N:CR5200 S/N:8342514597 DUE DATE:21-FEB-2SDR ASAA2024020147713Skin · damagedDAMAGE ON AIRCRAFT SIDE SKIN, APU DOOR FWD AND AFT HINGE AREAS. GROUNDED - YES. ACCOMPLISHED DAMAGED SKIN REMOVAL AND CUTOUT REF SRM 53-80-01-2R-1. PERFORMED HFEC ON SKIN ARIUND CUT, NO DEFECT NOTED REF 737 UDT PART 6 51-00-00 ASA60530 02/02/2024. FABRICATED DSDR DALA2024020301508Skin · corrodedCORROSION ON INNER SKIN BTW STA Y=655/663 AND BTW LONGERONS 29L/29R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00166: CORROSION LEVEL 2. INTERNAL SKIN DOUBLER BTW STA Y=655/663 AND BTW LONGERONS 29L/29R AT FWD CARGO COMPARTMENT WAS REPAIRED PER ERA 614961-1SDR DALA2024020201502Skin · puncturedSHIP 665 PUNCTURE NOTED FWD OF L1 DOOR LINE UPON TOW-IN AT GATE. CORRECTIVE ACTION: (REF BUFF NR 001) CUT OUT DAMAGE PER B757-200 SRM. C/W HFEC AND BHEC INSP, NO CRACKS. C/W INSURANCE CUT PER SRM. FABRICATED REPAIRS AND INSTALLED.SDR DALA2024020201489Paint · missingSHIP 3271 DISC: AAI FINDING: DURING INSPECTION OF EXISTING REPAIR DOUBLER LOCATED ON T HE FUSELAGE EXTERIOR, LOCATED ON THE RIGHTHAND SIDE FR69-FR 70 BETWEEN STR 31R AND STR 32R (LAV VENT EXHAUST) REF ER/A 589202-14AD REV A: NU MEROUS FASTERS THROUGHOUT THE RESDR DALA2024020201488Sealant · missingSHIP 3271 DISC: AI FINDING: DURING INSPECTION OF EXISTING REPAIR DOUBLER LOCATED ON T HE FUSELAGE EXTERIOR, LOCATED ON THE RIGHTHAND SIDE FR69- FR70 BETWEEN STR 31R AND 32R (LAV VENT EXHAUST) REF ER/A 589202-14AD REV A: ARE A BOVE STR 31R IS MISSING FAYING SEA
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