JASC 5330
Service difficulty reports · 79,312
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 VNAA202512020040Skin · corrodedPITTING CORROSION LOCATED ON THE EXTERIOR OF FUSELAGE BETWEEN F.S 501 AND F.S 517 AT STRINGER 27. REQUIRES EVALUATION. SH670-33202 SKINSDR VNAA202512020039Skin · damagedFOUND TWO ELONGATED FASTENER HOLES ON SKIN AT FS 986 STGR 27.SDR VNAA202512020013Skin · crackedRIGHT FUSELAGE SKIN IS CRACKED AROUND THE AFT TRU DOOR LATCH. TRU BAY DOOR LANDINGSDR VNAA202512020007Skin · bulgedAIRCRAFT SKIN SHOWS SIGNS OF DISTORTION & BULGING APPROXIMATELY BS 295 BETWEEN S22-23L.SDR CALA2025120811847Bracket · corrodedRIGHT UPPER WTB, UNDER FAIRINGS, BTWN BS 1080 - 1100, PANEL BRACKET SUPPORT HAS CORROSION. REMOVED AND REPLACED TEE BRACKET ON RT WING UPPER WTB STRUCTURE AT BS 1080 IAW SRM 51-40-02-0G, DWG 149N7552.SDR DALA2025120508878Skin · damagedLIGHTNING STRIKES BETWEEN FS 259 TO 360 ALONG AND BETWEEN STR 26R AND 27R. REMOVED DAMAGE AND COUNTERSUNK PER SRM 53-00. C/W BHEC AT 2 NOTED LOCATIONS W/NTF IAW SRM 53-00-01-2R-41. OVERSIZED 4 HOLES BVETWEEN STR 26 AND 27 TO .250 TO REMOVE DAMAGE AND COUNTERSSDR AALA202512049707Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN AT AFT LAVATORY VENT CUTOUT AT BS 907, S21L. REPAIRED SKIN PER SRM 53-70-01-2R-3-REPAIR 3.SDR DALA2025120408858Skin · damagedLIGHTNING STRIKE DAMAGE TO FASTENER 1 INCH FWD OF STA 312 AND 1.5 INCHES BELOW STR26R. REPAIRED PER ERA 630781-14 REV A.SDR VNAA20260205009Skin · wornWEAR ON EXTERNAL SKIN BTW FS 977.00 TO FS 985.00 STGR 27 AT EXTERNAL FUSELAGE SKIN. REPAIRED PER REO 670-53-00-290 REV F EXTERNAL SKIN BTW FS 977.00 TO FS 985.00 STGR 27 AT EXTERNAL FUSELAGE SKINSDR ASAA2025120262986Skin · gougedRIGHT SIDE LOWER FUSELAGE SKIN ABOVE NLG IS GOUGED. GROUNDED - YES. COMPLIED WITH ASA EA M9-53EA-29695 REV 00.SDR CALA2025121011970Skin · damagedLIGHTNING STRIKE TO FUSELAGE SKIN AT BUTT JOINT BS 360 BELOW S6R. MAJOR REPAIR. ACCOMPLISHED PERMANENT REPAIR IAW ECRA 5310-08732 AND GSO REO-G25672 REV IR. INITIAL INSP THRESHOLD 50,000 TOTAL FLIGHT CYCLES AND INSP INTERVAL TBD.SDR DALA2025120908975Skin · gougedFUSELAGE SKIN FOUND GOUGE ON FR70-FR71 AND S-56LTO S- 56R. COMPLIED WITH A330 SRM 53-41-11-205-002. (1331358)SDR CALA2025120811845Skin · crackedDURING HOLE PROBE INSPECTION FOUND DEFECT IN ONE FASTENER COMMON TO S-27L AT STA 372 AND ONE FASTENER COMMON TO SHEAR TIE AT BS 372 ABOVE S27AS IAW SRM 51-10-02, REAMED HOLE IN SHEAR TIE AREA, SKIN ONLY, TO .233" CRACK INDICATION GONE, REAMED HOLE IN STR 27L,SDR DALA2025120308815Skin · dentedEXTERNAL LOWER FUSELAGE AT 75MM AFT OF FR12, RH AVIONICS COMPARTMENT DOOR CUT OUT, FWD UPPER CORNER SKIN WITH DENT. CORRECTIVE ACTION: COMPLIED WITH ER/A 630214-14. (1332319).SDR JR2R20251202193Skin · dentedFWD FUSELAGE SKIN DENT FR2 TO FR6 BETWEEN STR2R TO STR4R. REPAIRED.SDR DALA2025120808960Skin · crackedCRACK ON FUSELAGE SKIN BS 1037, BTW L-14L AND L-13L. FUSELAGE SKIN BS 1037 BTW L-14L AND L-13L WAS REPAIRED IAW PRI 630562-14 REV 5 AND ER/ A 630562-14 REV. (1330895)SDR AALA202512033312Skin · gougedAIRCRAFT IN BASE MAINTENANCE: RIGHT SIDE OF FUSELAGE SKIN IS GOUGED ABOVE THE RIGHT HORIZONTAL STABILIZER, GOUGE LOCATION IS RIGHT HAND SIDE OF FUSELAGE APPROXIMATE 8 FASTENERS FORWARDOF BS 1156 ALONG STR 5R. INSTALLED REPAIRED. PER EA369709.SDR IPXA2025120116797Skin · crackedSECTION 18 LOWER SHELL REPLACEMENT AND INTERNAL STRUCTURE REPAIR. VERIFIED THAT REPAIR FOR SECTION 18 DAMAGE DUE TO TAILSTRIKE WAS REPAIRED ACCOMPLISHED ON AIRBUS WORK CARD 7086382 AND AIRBUS REPAIR DRAWING R53970080 ISSUE B. REPAIR THRESHOLD IS TO BE TRACKESDR VNAA202511290034Skin · corrodedCORROSION ON EXTERNAL FUSELAGE SKIN BTW FS953.00 TO FS 969.00, STGR22R AND BTW FS939.00 TO FS953.00, STGR23R. EXTERNAL FUSELAGE SKIN BTW FS953.00 TO FS 969.00, STGR22R AND BTW FS939.00 TO FS953.00, STGR23R WAS REPAIRED PER REO 670-53-51-361 REV -.SDR VNAA202511290033Skin Panel · wornWEAR ON LH AND RH PANEL SKIN BTW FS 830-847 PROYECTION STRG 24-25RH AND 24-25LH AT EXTERNAL FUSELAGE. WEAR ON LH AND RH PANEL SKIN BTW FS 830-847 PROYECTION STRG 24-25RH AND 24-25LH AT EXTERNAL FUSELAGE WAS REPAIRED PER REO 670-53-42-142 REV: - - AND REO 670SDR VNAA202511290009Web · crackedCRACK ON REPAIR DOUBLER OF WEB BTW BS 195 TO BS 205 AND WL79.50 (RT SIDE) ON INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT. PREVIOUS REPAIR DOUBLER OF WEB BTW BS 195 TO BS 205 AND WL79.50 (RT SIDE) ON INTERNAL STRUCTURE AT FWD EQUIPMENT COMPARTMENT WAS REPLSDR VNAA202511290008Skin · wornWEAR ON EXTERNAL FUSELAGE SKIN AT BS 988 AND STGR27. WEAR ON EXTERNAL FUSELAGE SKIN AT BS 988 AND STGR27 WAS EVALUATED OUT LIMITS PER SRM 53-61-01-101-003-A01 & REPAIRED IAW REO 670-53-00-290 REV - F.SDR VNAA202511290007Skin · wornWEAR ON DOUBLERS OF INTERNAL SKIN FWD AND AFT LOWER SIDE AT FORWARD BAGGAGE-BAY DOOR. DOUBLERS OF INTERNAL SKIN FWD AND AFT LOWER SIDE AT FORWARD BAGGAGE-BAY DOOR WERE REPLACED PER EA 21-C7-52-1250 REV IR SECTION III - PERMANENT REPAIR.SDR VNAA202511290005Skin · temp repairTEMPORARY DISPOSITION FOR BLENDED SCRATCH DAMAGE TO FUSELAGE SKIN AT THE PAX DOOR CUTOUT BETWEEN FS310.00- FS349.00 & STR17L-STR18L THE SUBJECT REWORKED CONDITION IS STRUCTURALLY ACCEPTABLE FOR 1850 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT RESDR VNAA202511290001Skin · dentedDENTS (3 EAS) ON FUSELAGE SKIN BTW FS1031 AND FS1040 AND BTW STGR 22R/21R, NEAR TO GROUND CONNECTION ACCESS DOOR. DENTS (3 EAS) ON FUSELAGE SKIN BTW FS1031 AND FS1040 AND BTW STGR 22R/21R, NEAR TO GROUND CONNECTION ACCESS DOOR WAS REPAIRED PER REO 670-53-61-2SDR N6WA202602190801Skin · dentedAFT FUSELAGE SKIN DENT/GOUGE AT FS 977 STRINGER 27. REPAIRED IN ACCORDANCE WITH GOJET EO C550-53MR-108 O/ AWATS EO 25-CRJ5-53-220SDR DALA2025120108770Skin · damagedEXTERNAL LOWER FUSELAGE AT 188MM FWD OF FR24, 73MM BELOW STGR41R SKIN WITH LIGHTNING STRIKE AND AT 87MM FWD OF FR24, 50MM BELOW STGR42R SKIN WITH NICK. PERFORMED PERMANENT REPAIR ON FUSELAGE SKIN LOCATED AT 188MM FWD OF FR 24 AND 73MM BELOW STGR 41RH DUE TO SDR AALA202512010896Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN ELECTRICAL GROUND POWER RECEPTACLE CUTOUT FUSELAGE SKIN AT BS 230, S21R. REPAIRED SKIN PER SRM 53-10-15-2R-5SDR VNAA202601180019Skin · damagedIN REFERENCE TO: TASKCARD TRFKE00FCUS8, 8000FH PERM-REPAIR FUSELAGE SKIN LIGHTNING STRIKE DAMAGE ON SKIN ONLY (NO FASTENER AT DAMAGE LOCATION) WITHIN 8000FH, ACCOMPLISH PERMANENT REPAIR OF TEMP REPAIR PER 670-53-00-045 SECTION 1 PARAGRAPH B3. SEE ATTACHMENTS FSDR VNAA202601180018Skin · corrodedIN REFERENCE TO: TASKCARD TRFKE00FCUS8, 8000FH PERM-REPAIR FUSELAGE SKIN LIGHTNING STRIKE DAMAGE ON SKIN ONLY (NO FASTENER AT DAMAGE LOCATION) WITHIN 8000FH, ACCOMPLISH PERMANENT REPAIR OF TEMP REPAIR PER 670-53-00-045 SECTION 1 PARAGRAPH B3. SEE ATTACHMENTS FSDR DALA2025120508905Skin · dentedFUSELAGE SKIN TWO DENTS AT STA 654A+88 TO STA 654A+ 110 AND S-23L. DAMAGED AREA REPAIRED PER 767 SRM 53-00-01-2R-1 (1324044)SDR DALA2025120508903Skin · damagedUPPER FUSELAGE SKIN AT STA412-434 BL 0 FOUND EXSITING LIGHTNING STRIKE FASTENER REPAIR, DENT AROUND FASTENER, NO RECORD. DAMAGED AREA REPAIRED PER B767-400 SRM 53-00-01 (1323840)SDR CALA2025120111619Skin · nickedLEFT FWD FUSELAGE RVSM CRITICAL AREA AT 5 INCHES FROM FWD EDGE AND 11 INCHES FROM LOWER EDGE FOUND A NICK. REMOVED NICK AT LT FWD FUSELAGE RVSM CRITICAL AREA AT 5 INCHES FROM FWD EDGE AND 11 INCHES FROM LOWER EDGE REF SRM 51-10-02-0G-0, ORIGINAL THICKNESS: 0.SDR AALA202512012602Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO LOWER FUSELAGE SKIN UNDER LAVATORY SERVICE PAN LOCATED FROM BS 865 TO BS 867, AT S22L. REPAIRED SKIN PER EA 369821.SDR N6WA2025112804Skin · gougedGOUGE FOUND ON SKIN PANEL AT FS977 UNDER AFT FAIRING PANEL 195DL. PERFORMED REPAIR ON SKIN PANEL AT FS977 UNDER AFT FAIRING PANEL 195DL IAW GOJET EO-C550-53MR-110-OSDR DALA2026031101716Skin · corrodedSHIP 3315 CORROSION ON EXTERNAL FUSELAGE SKIN AT FR76-77, STR41L. CORRECTIVE ACTION: CORRECTED PER A330 SRM 53-41-11-205-037. (1320804)SDR DALA2025120308826Skin · crackedCRACK FOUND DURING NDT INSPECTION AT FASTENER HOLE NO 3 (SKIN) AND 4 (SKIN). REPAIR IS REQUIRED BEFORE FURTHER FLIGHT. REPAIRED FWD SERVICE DOOR CUTOUT AFT LOWER CORNER HOLE 3 AND 4 IAW B767-300 SRM 53-10-01 (1322843)SDR DALA2025120308825Bear Strap · crackedCRACK FOUND DURING NDT INSPECTION AT FASTENER HOLE NO 3 (SKIN) AND 4 (SKIN+BEAR STRAP). REPAIRED FWD PAX DOOR CUTOUT AFT LOWER CORNER HOLES 3, 4 IAW B767-300 SRM 53-10-01 (1322829)SDR IPXA2025112536730Skin · crackedSECTION 17 LOWER SKIN SPLICE REPAIR/REPLACEMENT AND INTERNAL STRUCTURE REPAIR. VERIFIED THAT THE DAMAGE TO SECTION 17 DUE TO THE TAIL STRIKE WAS REPAIRED IN ACCORDANCE WITH AIRBUS WORK CARD 7086383 AND AIRBUS REPAIR DRAWINGS R53970076 ISSUE B AND R53970056 ISDR AALA202511252221Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO FUSELAGE SKIN ADJACENT TO AFT LAVATORY SERVICE PANEL, LOCATED AT BS 847, S25L. REPAIRED SKIN PER EA 369756.SDR SWIA2025112475489Skin · gougedFUSELAGE EXTERIOR LEFT SIDE BS 969 - 985, ABOVE STRINGER 27. SKIN GOUGED. REPAIRED DAMAGE TO FUSELAGE EXTERIOR BETWEEN BS 969 AND BS 985 STGR 27L IAW REO 670-53-00-290, REV-F AND REO 670-53-00-807, REV-A.SDR SWIA2025120124Skin · dentedEVALUATE DENT MARKED WITH YELLOW DOT ON LH FUSELAGE SKIN ABOVE FWD CARGO DOOR. (C-CHECK RO 11/30/2025)AFTER REMOVAL OF PAINT 3EA DENTS WERE IDENTIFIED WHERE YELLOW DOT WAS LOCATED. 2EA DENTS WERE WITHIN LIMITS OF CRJ 700 SRM 53-00-01-101-001-A01. THE THIRD DSDR DALA2025112508623Skin · damagedTOOLING DAMAGE ON SKIN AND J CHANNEL ON FORWARD SIDE OF FRAME 60 AT P'1. REPAIRED PER ERA 628248-14. (1320004)SDR 2A6R1124202574604Skin · damagedOVERSIZED FASTENER HOLE DAMAGE WAS FOUND ON THE L/H FUSELAGE SKIN (P/N: 350A210053.BW), FWD FRAME ANGLE (P/N: 350A211036.28), AFT FRAME (P/N: 350A211240.00), LOWER FRAME (P/N: 350A211245.22), AND MAINTENANCE STEP (P/N: 350A21137.20) DURING REMOVAL AND REPLACEMSDR CALA2025112511469Skin · damagedENGINEERING WAS NOTIFIED BY THE FAA THAT THE RVSM ALTITUDE KEEPI NG IS NOT WITHIN LIMITS. ENGINEERING REQUESTS TO PERFORM THE FO LLOWING CHECKS: AMM TASK 51-10-00-206-025 STATIC PORT SKIN WAVINESS, AMM TASK 34-12-00-735-013 SYSTEM TEST - AIR DATA COMPUTING SYSDR AALA202511240406Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION TO FUSELAGE SKIN AT AFT LAVATORY VACUUM WASTE VENT AT STA 917 FROM S21L TO S22L. REPAIRED SKIN PER SRM 53-70-01-2R-3 REPAIR 3.SDR SWIA2025112376498Skin · chafedBS 913 - 927, STRINGER 27, THE AFT BODY FAIRING HAS CHAFED THE FUSELAGE EXTERIOR SKIN. REPAIRED FUSELAGE EXTERIOR SKIN AT BS 913 - 927 STRINGER 27 IAW REO 690-53-51-533 REV-. COMPLIED WITH ALL STEPS OF REO 690-53-51-533 REV-- AND REO 670-53-00-290 REV F. COMPSDR SWI2025F01851Skin · corrodedWASTE SERVICE PANEL INNER UPPER SURFACE HAS AREAS WITH POSSIBLE CORROSION AT SEAMS AROUND FIBERGLASS PROTECTIVE COVER. (C-CHECK RO 12/19/2025)REMOVED AND REPLACED INNER DOUBLER AT WASTE SERVICE BOX FR 88-89 STRG 26R-28R REF EMB 175 SRM 51-40-08.THIS REPAIR DOSDR HNAA2026012100038Skin · crackedPOSSIBLE SKIN CRACK AT FR 77 BTWN STGRS 3L-4L. REPAIRED SKIN CRACK AT FR 77 BTWN STGRS 3L-4L WITH INSTALLATION OF SKIN BUSHING IAW EMB145 SRM 53-32-01RE, ITEM 9, FIG. 213 AND EO1-53-26-0005.SDR AALA202511248424Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN ELECTRICAL GROUND POWER RECEPTACLE CUTOUT FUSELAGE SKIN FROM BS 224.8 TO BS 235.8, FROM S20R TO S21R. REPAIRED SKIN PER SRM 53-10-15-2R-5.
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