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 DALA2025051303688Skin · crackedCRACKS ON FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE. SUMMARY OF NRC 00047: FUSELAGE SKIN ON STA Y=1087 AND LONG 14L AT AFT FUSELAGE WAS REPAIRED PER ERA 626154-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 626154-14 REV 3. SEC II ACCOMPLISSDR BAGA2025061300008Doubler · corrodedFOUND DURRING HEAVY CHECK - REAR BARRELL AT FR 75 WASTED DOUBLER INBD LWR CORNER CORROSION TO BE INVESTIGATED SURROUND, REPAIRED PER REO AND BREEZE EC. TEMP DISPOSITION DVI EVERY 1000 FH. REPAIR VALID FOR 10,000 FHSDR BAGA2025061300006Skin · corrodedFOUND DURRING HEAVY CHECK - FWD PAX DOOR LOWER SKIN UNDERNEATH SCUFFPLATE, REPAIRED PER REO AND BREEZE EC. TEMP DISPOSTION DVI TO BE CARRIED OUT AT EVERY 1000 FH. REPAIR VALID FOR 10000FHSDR ASAA2025051258099Skin · corrodedLOWER FUSELUGE SKIN JUST FWD OF STA 400, FWD SIDE OF DRAIN PLUG SKIN HAS CORROSION MARKED. GROUNDED - YES. REMOVED DAMAGE AND CHECKED LIMITS ORI MAT .080, REMOVED MAT .001, REMAINING .079 FOUND TO BE WITHIN LIMITS IAW B737-MAX9 SRM 53-30-01-01-1, SRM 53-00- 01SDR DALA2025051503758Skin · damaged(LOG 0962148) RH MAIN ACFT POWER RECEPTACLE CUTOUT LOWER FWD SKIN HAS DAMAGED MISSING SKIN. RECEPTACLE CUTOUT LOWER FWD SECTION IAW B737 SRM 53-10-15-2R PROCEDURE 4 ZONE 2.SDR DALA2025051203681Skin · crackedCRACKS ON FUSELAGE SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE. SUMMARY OF NRC 00048: FUSELAGE SKIN AT STA Y=1087 AND LONG 14R ON AFT FUSELAGE WAS REPAIRED PER ERA 626165-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 626165-14 REV 3. ASSOCIATED ER/A SDR CALA2025053005118Skin · corrodedL/H LOWER FUS SKIN FOUND BULGING CORROSSION AT DIAGONAL ATTACHED ANGLE APPROX S-21L STA 540. REF. AAR N/R:9967393ESFR CREATED AND SENT ACCOMPLISHED REPAIR AT WING CENTER SECTION FWD LWR SKIN PANEL REF. AAR ESR-WI #2023385-22-12079 AND EC/RA 5710-02928 REV. ORISDR QXEA2025052100194Doubler · corrodedANTENNA DOUBLER CORRODED AT FR23-24. REMOVED AND REPLACED ANTENNA DOULBER AT FR 23-24 IAW ETD 2025-170-8204301.SDR CALA2025051604725Skin · dentedDENT ON FUSELAGE AT FR66L STR26-27. REPAIRED DENT ON LH FUSELAGE SKIN @ FR66 STR26-27 IAW A320 SRM 5 3-41-11-300-093.SDR YENA2025051300489Skin · dentedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / EXTERNAL SKIN AT THE LAP JOINT @ FR 64-65 & STGR 32L-33L / DENT WITH GOUGE – PERMANENT REPAIR (PENDING DTA); REFERENCES: /1/ DAMAGE REPORT MX-283 AND MAPPING /2/ FERRY FLIGHT CONCURRENCE ECA-304 /3/ AIRBUS DSDR YENA2025051300488Skin · gougedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / EXTERNAL SKIN AT THE LAP JOINT @ FR 64-65 & STGR 32L-33L / DENT WITH GOUGE – TEMPORARY REPAIR; REFERENCES: /1/ DAMAGE REPORT MX-283 AND MAPPING /2/ FERRY FLIGHT CONCURRENCE ECA-304 /3/ AIRBUS DOSSIER 8158766SDR GTIA2025051238916Skin · damagedLIGHTING STRIKE EXTERNAL SKIN LOC. BTW FR25 TO FR26 AND BTW STR41L TO 42L AT LOWER FUSELAGE RAF-01 3413767-01 GENERATED-PERFORMED PERMANENT REPAIR OF THE FUSELAGE EXTERNAL SKIN AT FR.25 TO FR.26 BETWEEN STR 41L TO STR 43L AT LOWER FUSELAGE DUE TO LIGHTNING STRSDR DALA2025051203670Skin · corroded(LOG 0959151) SECONDARY FINDING CORROSION ON INTERNAL LOWER SKIN LOC BS390 AND STR 28L. COMPLIED WITH ER/A 625651-14 REV ORIGINAL.SDR DALA2025051203675Skin · damagedSHIP 3407 TOOLING DAMAGE AT STR 7 RH. CORRECTIVE ACTION: REPAIRED PER PRI 626125 REV 0, REV 1 AND FINAL ER/A 626125-14 REV ORIG. (0958193)SDR COEA2025073101805Skin · deformedL/H LOWER SKIN PANEL #2 DME MOUNT HOLES ARE DEFORMED. CORRECTIVE ACTION: REPAIR PER SRM 531129-300-802-B01.SDR SWI2025F00892Skin · chafedEXTERIOR SKIN AROUND THE APU EXHAUST, THE AFT EDGE HAS 2EA CHAFFED AREAS (MARKED) (C-CHECK RO 07/11/2025)REPAIRED SKIN AROUND THE APU EXHAUST AFT EDGE AS PER REO 601R-53-61-8341, REV --, DATE: 2025-06-11. ALL STEPS OF REO COMPLIED WITH. COMPLIED WITH M-337 ASDR AALA202506278578Skin Panel · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON UPPER FUSELAGE EXTERNAL SKIN PANEL BETWEEN FR 69 AND FR 70, BETWEEN S1L AND S2L. REPAIRED SKIN PANEL PER EA 365391.SDR SIMA202506139005Service Panel · corrodedSSI 53-23-018 ? WASTE SERVICE DOOR IS CORRODED IN NUMEROUS AREAS. (LEVEL 2 CORROSION). RAR WASTE SERVICING DOOR IAW ERJ 175 AMM 53-03-60SDR DALA2025051503751Skin · not reportedSHIP 3085 PERFORM ER/A 626152-14AD ON EXTERNAL SKIN FROM FR47 TO FR70 BETWEEN STR 23LH AND STR 23RH AT LOWER FUSELAGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 626152-14AD REV ORIGINAL MATCHES WITH ALL STEPS ON PRI 626152-14AD REV 0 IT HAS BEEN VALIDATED. PERFORMSDR YENA2025051300476Lap Joint · dentedDURING HEAVY MAINTENANCE: FUSELAGGE/REAR FUSELAGE/EXTERNAL SKIN NEAR LAP JOINT @ FR65-66 AND STGR 32L-33L DENT WITH GOUGE; PERFORMED JB TASKCARD A25-455-01 WITH NO DEVIATIONS. REF: CAS W/O 703-1410376 N/R 2.SDR DALA2025051203679Skin · crackedCRACKS ON FUSELAGE SKIN ON STA Y=1087 AND LONG 14R AT AFT FUSELAGE. SUMMARY OF NRC 00025: FUSELAGE SKIN ON STA Y=1087 AND LONG 14R AT AFT FUSELAGE WAS REPAIRED PER ER/A 625728-14 REV ORIG SECTION I: PERMANENT REPAIR AND PER PRI 625728-14 REV 3. TIME CONTROLLEDSDR AALA202505124548Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AROUND AFT LAVATORY VENT AT BS 917, BETWEEN S21L AND S22L. REPAIRED SKIN PER SRM 53-70-01-2R-3.SDR DALA2025050903598Skin · gougedSHIP 3357 FORWARD FUSELAGE FOUND GOUGE ON FR35A-FR36, STGR 27L-28L. CORRECTIVE ACTION: COMPLIED WITH A330 SRM 53-21-11. OK TO CONTINUE. (0956968)SDR SWIA202508050002Skin · dentedDENT AT FS295 STGR 26 L/H. DENT BETWEEN FS 280.00-FS295.00 STGR 26 L/H. REPAIR PERFORMED USING FILLER AND DOUBLER MATERIAL # .063 SHEETMETAL 2024T3 LOT# LT20-00865 IAW MHIRJ REO 601R-53-21-3753. TASK CARD 51-900-1003-SKY.SDR AALA202505206242Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN R1 DOOR SURROUND FUSELAGE SKIN AT BS 295 FROM S6R TO S10R. REPAIRED SKIN PER SRM 53-10-01-2R-6 AND EA 364150.SDR DALA2025051603785Skin · nickedSHIP 3087 NICK EXTERNAL SKIN LOC. BTW FR 21 TO FR 23 AND BTW STR 41 RH TO -Y175 AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS EXTERNAL SKIN LOC. BTW FR 21 TO FR 23 AND BTW STR 41 RH TO -Y175 AT LOWER FUSELAGE AS PER A321 SRM53-11-11 (0956SDR JJBA20250515069Skin · dentedEXTERNAL FWD FUSE, DENT FOUND 3 INCH AFT FRAME 1A AND 3 INCHES BELOW STR 15R. DENT ON SKIN 3 INCH AFT OF FR 1A AND 3 INCH BELOW STR 15R REPAIRED WITH DOUBLER. ALSO NOTICED 7 PREVIOUS REPAIRS FOUND ON SKIN BTW FR 1A-2 BTW STR 13R-17R. 2 REPAIRS FOUND WITH ELONGSDR SWIA202505140008Skin · gougedGOUGE/DENT AT FRAME 84 & BETWEEN STRG 19R & STRG 20R. DAMAGE NEEDS TO BE CUT OUT. (FILED CLOSED)PERMANENT REPARREPAIR OF GOUGE/DENT AT FRAME 84 & BETWEEN STRG 19R & STRG 20R DONE IN REFERENCE TO REO ETD2025-170-920649 REV.: CRE INSPECT INSTRUCTIONS FROM TIME SDR DALA2025051403746Skin · damagedDTE, ERA 603429-14 REV A. DAMAGE TOLERANCE EVALUATION REQUIRED. ERA 603429-14 SECTION I IS TIME LIMITED TO 12 MONTHS FROM 1XFEB2 025. FUSELAGE SKIN ON THE SKIN NEAR FR24 AND REPORTED TO BE 1.9" . SECTION III IS DTE LIMITED TO 1 YEAR FROM 16FEB25. ADDITIONAL ENSDR JJBA20250513057Skin · crackedEXTERNAL REAR FUSE I, CRACK FOUND FRAME 75 BTW STR 2L-3L. REPAIR DOUBLER ON LH REAR FUSE I SKIN, AT FR 75 AT STR 2LSDR JJBA20250513056Skin · crackedEXTERNAL REAR FUSE 1, CRACK (X2) FOUND FRAME 77 BTW STR 9R-8R AND BTW STR 5R-7R. 2 BUSHING REPAIRS ON RH REAR FUSE II SKIN, AT FR77 BTW STR 6R-7R AND STR 8R-9RSDR JJBA20250513055Skin · crackedEXTERNAL RF II, CRACK FOUND FRAME 78 BTW STR 5L-6L. BUSHING REPAIR ON LH REAR FUSE II SKIN, AT FR 78 BTW STR 5L-6LSDR JJBA20250513054Skin · crackedEXTERNAL RF II, CRACK FOUND FRAME 77 BTW STR 8L-9L. BUSHING REPAIR ON LH REAR FUSE II SKIN, AT FR 77 BTW STR 8L-9LSDR NACA2025050800001Skin · crackedWHILE PERFORMING EO 737-53-0087-01, FOUND EVIDENCE OF A SUBSURFACE CRACK 3/8 INCH LONG, STR 10R 727A + 111/4"SDR CALA2025051204610Skin · damagedACCOMPLISH PERMANENT REPAIR OF FWD LOWER FUSELAGE BY RADOME AT STA 178 BL 0 PER ECRA 5310-08583 PART 3, ON OR BEFORE 24 MONTHS ...REF L/P# 4699788 FOR ALL WORK ACCOMPLISHED. UPGRADED TO MAJOR REPAIR REF EC/RA#:5310-08583 REV A. ADDED ESFR INFORMATION. REF ECSDR AALA202505091689Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN BELOW AFT LAVATORY VENT AT BS 917 BETWEEN S21L AND S22L. ACCOMPLISHED REPAIR PER SRM 53-70-01-2R-3.SDR AALA202505091932Skin · bulgedAIRCRAFT IN BASE MAINTENANCE: BULGE / WRINKLE IN FUSELAGE CROWN SKIN FROM BS 500C TO BS 500D, FROM S1R TO S2R. ACCOMPLISHED DOUBLER REPAIR PER EA 364391.SDR VNAA2025050800034Skin · crackedHN00195027 DISCREPANCY: AFT FUSELAGE SKIN DOUBLER AT LAV SERVICING LOCATION IS CHAFED AND MULTIPLE FASTENERS ARE CHAFED. CORRECTIVE ACTION: REMOVED AND REPLACED DOUBLER IAW CRJ-700 SRM 51-42-06-001-001-A01.SDR REXA2025050800569Skin · corrodedF.S. 533-581 BAGGAGE DOOR SURROUND CORRODED, FWD AND CENTER TOP PLATES CORRODED IN MULTIPLE PLACES. REPAIRED FORWARD BAGGAGE BAY INNER CLOSING SKIN IAW ENDEAVOR AIR EA CRJ753-18690 REV IR DATED 3/17/2025SDR SWI2025F01470Skin · out of limitsCOMPLY WITH SCHEDULED MAINTENANCE CODE: WIFI PCS/TIMING ANTENNA SDI 900 - 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 - SDR REXA2025052900616Access Panel · corrodedCORROSION / CHAFE DAMAGE AT ALL SETTLEMENT AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB SETTLEMENT (STRAP) AREA OF HYDRAULIC LOWER ACCESS PANEL 195AB WAS REPAIRED PER EA CRJ953-19313 REV IR AND WAS REPLACED PER CRJ900 SRM 51-42-10-001-001-A01SDR R61A2025052700250Skin · dentedBIRD STRIKE ON FWD FUSELAGE FROM FRA 1 TO FRA 3 AND FROM STR 2R TO 8R INCLUDING THE FWD PRESSURE BULKHEAD. REPAIRED FWD PRESSURE BULKHEAD AND REPLACED FWD UPPERSKIN IAW EMB ETD2025-170-920760,ALSO REF VP-019402-2025 FOR WORK PERFORMED.SDR DALA2025051203662Skin · dented(LOG 0953506) UPON ARRIVAL INTO AMES (TPA), MTC REPORTED A DENT BY BIRD STRIKE LOCATED IN STA 178.4 AND ABOVE STR 21R. ADDITIONALLY, THAT THERE IS A PREVIOUS REPAIR WITH DISTANCE OF 12.8 INCHES BETWEEN DENT LAND UPPER EDGE OF THE PREVIOUS REPAIR. REPAIRED PERSDR DALA2025050903635Skin · dented(LOG 0953755) DENT FROM A BIRD STRIKE AT STA 178 4 INCHES ABOVE STR 21. MEASURING 1INCH WIDE BY 4INCHES LONG WITH A MAX DEPTH OF 0.090 INCHES. REPAIRED PER ERA 626141-14.SDR DALA2025050903617Doubler · corroded(LOG 0954293) CORROSION DOUBLER LOCATED INTERNAL STRUCTURE BETWEEN BS747 TO BS767 AND FROM STR27R TO STR27L AT AFT CARGO COMPARTMENT. REPLACED FITTING ASSY AND FASTENERS LOCATED INTERNAL STRUCTURE BETWEEN BS747 TO BS767 AND FROM STR27R TO STR27L AT AFT CARGO CSDR GTIA2025050938909Skin · damagedGOUGE DAMAGE FOUND ON CROWN SKIN AT FRAME 52 STRINGERS 2R-3R. RAF-01 3292829-01.-ACCOMPLISHED REPAIR OF GOUGE ON WO 346167 RAF 01-3292829-01SDR CALA2025050904581Skin · corrodedEXTERNAL FUSELAGE (SECTION 46) WASTE SERVICE DOOR PAN DOUBLER SURFACE BULGING AND BOTTOM EDGE SIGNS OF CORROSION. (REF AAR N/R 9968388)(FOR ESFR PURPOSES) ESFR COMPLETED PERFORMED A REPAIR TO THE DAMAGED LOWER SKIN IN ACCOREDANCE WITH EC/RA # 5331-03161. THIS SDR WRXR20250507002Skin · corrodedPOTENTIAL PITTING CORROSION FOUND ON OUTSIDE OF FUSELAGE SKIN LOCATED BETWEEN FS 942-927 AND STRG 9L-8L. NEAR TOP FWD CORNER OF PAX WINDOW. COMPLIED WITH REO 690-53-51-466 REV --.SDR AALA202508067074Skin Panel · deformedAIRCRAFT IN BASE MAINTENANCE: FUESELAGE LOWER SKIN PANEL HAS EVIDENCE OF SKIN DEFORMATION BETWEEN FR 72 AND FR 75, BETWEEN S30L AND S31R. REPAIRED SKIN PANEL PER SRM 53-51-29-300-002,SDR 2025FA0000494Stiffener · crackedFUSELAGE AFT LWR SKIN, STIFFENER CRACKED.
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