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 CALA2025112411433Skin · corrodedAFT CARGO COMPARTMENT BS 1660 - 1680, S25R- S26R INTERNAL SKIN AROUND WATER DRAIN MAST ATTACHMENT HAS EXFOLI ATION CORROSION. REMOVED CORROSION ON INTERNAL SKIN IAW SRM 51-10-02-0G- 0 .004 MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 53-00-01-1A-1 FIG 101 DSDR SWIA2026022574317Skin · dentedFOUND DENT ON FUSALAGE SKIN NEXT TO BS 565, STRINGER 21R. DENT IS 1 INCH IN LENGTH, .25 INCH WIDE, & .018 INCH DEEP. COMPIED WITH REO 670-53-31-1123 REV-. REPAIR TO RT FUSELAGE SKIN PANEL, LOWER, FWD BARREL AT BS 565, S21R - 22R. COMPLIED WITH TASK CARD 5SDR FDEA202511212197Skin · dentedDENT AT RT LOWER LATERAL SKIN BELOW UPPER LAP SEAM BETWEEN BS 1620 & 1650. DENT AT RT LOWER LATERAL SKIN BELOW UPPER LAP SEAM WAS REPAIRED IAW EA. H-5330-T0369691 REV NOV 19,2025. RELEASE DATE: JUL 23,2022.SDR SWIA2025112400021Skin · dentedFOUND DENT ON FUSALAGE SKIN NEXT TO FS565 STRINGER 21R. DENT IS 1" IN LENGTH .25" WIDE AND .018" DEEP. REF SRM 53-31-01. (FILED OPEN)SDR IPXA2025112068723Skin · damagedFUSELAGE SKIN DAMAGE AT FR80/82 BETWEEN STR44LH AND STR 44RH VERIFIED THAT THE DAMAGE DUE TO THE TAIL STRIKE WAS REPAIRED IN ACCORDANCE WITH UPS EO-95523-REQ1, AIRBUS WORK CARD 7086636 AND AIRBUS REPAIR DRAWING R53970081 ISSUE B. REPAIR THRESHOLD IS TO BE TRACSDR JR2R20251120283Skin · corrodedFWD CARGO DOOR ENTRY LOWER SURFACE HAS MULTIPLE AREAS OF CORROSION ON SKIN. REPAIRED PER ETD.SDR SWIA2025111975726Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA84579-REO 601R-53-11-3871. COMPLY WITH PERMANENT REPAIR ON RA ID: 845792+ CM DENT RIGHT SIDE NOSE, ADJACENT TO N/W DOOR. PERMANENT REPAIR IS DUE WITHIN 5650 FLIGHT HOURS FOR THE DENT DAMAGE TO FUSELAGE SKIN BETWEEN FSSDR SWAA2025123036983Skin · corrodedCORROSION ON FUSELAGE LOWER INTERNAL BLIGE SKIN COMMON TO EXTERNAL DOUBLER INSTALLED AS PER REPAIR-53EO-00182 BS747 TO BS767 BL-0 WL149. REPAIRED IAW EA 25-153-03257 WITH AN INSPECTION THRESHOLD DEFINED IN 25-153-03257-DTI.SDR SWI2025F01826Skin · damagedLIGHTNING STRIKE DAMAGE UPPER FUSELAGE ON SKIN BETWEEN FRAMES 20-21 AND STRINGERS 1 - 2L. DAMAGE IS 0.067, NOMINAL=0.040, DAMAGE IS 0.375" FROM FRAME 20, DRILLED A # 40 HOLE AND INSTALLED FASTENER REF ETD 2025-170-932740.SDR GTIA2025112039186Skin · puncturedPENETRATION DAMAGE FOUND ON CROWN SKIN AT FRAME 49-50 STRINGERS 5L-5R. RAF-01 3072220-01 CREATED. -REF W/O 346076 ON LOGPAGE 3072221-2 FOR PERMANENT REPAIR.SDR JGVR20251119002Skin · corrodedREPAIRED THE CORRODED AREA ON THE RT SKIN/PANEL OF THE NOSE LANDING GEAR TUNNEL BY BLENDING CORRODED AREA, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLER IN ACCORDANCE WITH ENGINEERING REPAIR ORDER.SDR JGVR20251119001Skin · corrodedREPAIRED CORRODED AREAS OF THE LOWER AFT TAILCONE SKINS, LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING JOINT, BY BLENDING AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS PER ENGINEERING REPAIR ORDER.SDR SWIA2025111876640Skin · dentedCOMPLY WITH PERMANENT REPAIR ON RA 78977, FOUND DENT ON EXTERIOR OF FUSELAGE AT INTERSECTION OF BS 501 AND STR 21R. COMPLIED WITH TEMPORARY REPAIR PER REO670-53-31-627 REV A. PERMANENT REPAIR DUE WITHIN 8000 FLT HRS BY 47667.7 TAT, PERFORMED DRESSBACK AND SDR SWIA2025111876632Skin · dentedFOUND DENT ON EXTERIOR OF FUSELAGE 2 INCHES FWD OF BS2 80 AND 1 INCH ABOVE STGR 26R. COMPLIED WITH TEMPORARY REPAIR PER REO 670-53-11-1678 REV A DATED 2022-06-01. PERMANENT REPAIR DUE WITHIN 8000 FLT HRS BY 47667.7 TAT, PERFORMED PERMANET REPAIR BY EVALUATINSDR SWIA2025112400018Skin · dentedREF AML 1751235: UPON INSPECTION FOUND: 3-OFF AREAS OF DENT DAMAGE TO LHS FUSELAGE SKIN PANEL (DWG: MM670-35146, 0.080€? ±0.005€? NOMINAL PAD UP THK, 0.050€? ±0.005€? & 0.060€? ±0.005€? CHEM-MILLED POCKET THICKNESS, REF) BETWEEN FS1015.00 -FS1047.00 ASDR SWIA2025111900008Skin · dentedREF AML# 1751235: UPON INSPECTION FOUND: 3-OFF AREAS OF DENT DAMAGE TO LT FUSELAGE SKIN PANEL (DWG: MM670-35146, 0.080€? ±0.005€? NOMINAL PAD UP THK, 0.050€? ±0.005€? & 0.060€? ±0.005€? CHEM-MILLED POCKET THICKNESS, REF) BETWEEN FS1015.00 -FS1047.00 ASDR DALA2025111908444Skin · gougedFOUND 3 GOUGES BELOW AFT CARGO DOOR ON STRINGER 46R, FRAMES 60A, 61, 61A. REWORKED DAMAGED AREAS PER A330 NEO SRM 53-42-11-283-022. (7971596)SDR IXXA20262026001Skin · corrodedFUSELAGE EXTERNAL SKIN IS CORRODED AT LAP SEAM S-20L BS 1718.SDR CALA2025120511793Skin · damagedDAMAGE ON THE FWD CARGO DOOR SILL, DAMAGE TO THE OUTER & INNER SKIN OF THE LAP SPLICE BS 490, S24R. DAMAGE OUT OF LIMITS IAW SRM 53-00-01-1A-6. IAW AVO 16027 STEP 1. PERFORMED INSPECTION OF DAMAGED AREA, USING A 20" RADIUS. NO FURTHER DAMAGE NOTED. IAW AVO SDR DALA2025111908452Skin · corrodedWASTE WATER ACCESS PANEL FWD EDGE EXTERNAL SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# 1308921SDR DALA2025111908451Skin · corrodedWASTE BOX- FWD DOUBLER R/H CORNER HAS CORROSION INTERNAL AND EXTERNAL COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# SDR DALA2025111908450Skin · corrodedWASTE BOX- AFT CUTOUT FLANGE SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# 1308846)SDR DALA2025111908449Skin · corrodedWASTE BOX- INSIDE THE BOX FWD RT CORNER SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# 1308845)SDR DALA2025111908448Skin · corrodedWASTE BOX CUT-OUT FWD RT CORNER SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". ORIGINAL THICKNESS 0.125". REMAINING THICKNESS 0.066". (LP# 1308843)SDR DALA2025111908447Access Panel · corrodedWASTE WATER ACCESS PANEL FWD EDGE INTERNAL SKIN HAS CORROSION. COMPLIED WITH PRI 629290-14 REV 0, 1, 2, AND SECTION I TIME-LIMITED REPAIR OF ERA 629290-14 REV 0. MAX MATERIAL REMOVED 0.059". (LP# 1308838)SDR N6WA2025111901Skin · damagedDAMAGE LOWER SKIN FWD OF FS977.00 AT STRINGER 27. COMPLETED REPAIR OF DAMAGED LOWER SKIN FWD OF FS 977.00 AT S27 IAW GOJET EO-C550-53MR-108-OSDR DALA2025111808420Skin · crackedFOUND ONE CRACK BELOW THE NR 7 FASTENER HOLE, COUNTING FROM FRONT TO THE BACK, BETWEEN FRAMES 1654 - 1678, STRINGER 13AL. REPAIED IAW SRM 53-80 -01-2R-7 (1308025).SDR JGVR20251117002Skin · corrodedREPAIRED CORRODED AREAS OF THE INNER SURFACES OF THE BAGGAGE COMPARTMENT SKINS, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. FABRICATED AND INSTALLED REPAIR DOUBLERS PER REQUEST FOR TECHNICAL SERVICES REPORT.SDR IPXA2025121295448Skin · damagedFOUND SCRATCH 3FT AFT OF LH AOA PROVIDING CORRECTED SRM REF UPDATE FOR ASSOCIATED MAINTENIX BARCODE [T3F18E007SYGS] BLENDED GOUGE AT LOCATION 328 BS BETWEEN S22 AND S23 BLENDED DAMAGED AREA PER SRM 51-10-02-0G-0. EVALUATION FOUND HORIZONTAL SCRATCH THAT IS APPSDR IPXA2025112401030Skin · pilot errorTAIL STRIKE EVENT - FUSELAGE AFT INTERMEDIATE SECTION SKIN/STRUCTURE REPLACEMENT/REPAIRSSDR AALA202511176812Skin · corrodedAIRCRAFT WAS GROUNDED: CORROSION ON FUSELAGE SKIN AROUND LAVATORY VENT LOCATED AT BS 917, FROM S21L TO S22L. REPAIRED SKIN PER SRM 53-70-01-2R-3.SDR SWAA2025121935354Access Panel · delaminatedDELAMINATED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR IAW SRM 51-70-05-2R-2, REPAIR 2.SDR DALA2025111708376Skin · puncturedHOLE IN FUSELAGE, AFT OF DOOR 1L. ACCESSED TO DAMAGE IS FWD BB, SUBMITTED DIMENSIONS OF DAMAGE TO ENGINEERING. ALL REPAIR WORK COMPLETED IAW ER/A 630504-14 REV. A. RII'S COMPLIED WITH. FWD CARGO SIDEWALL PANEL INSTALLED IAW AMP 50-11. ASSOCIATED ER/A 14-63SDR EE4Y2025111423461Skin · nickedDURING STRUCTURAL INSPECTION, SKIN WITH NICKS WERE FOUND AT FWD FUSELAGE FROM FR18+85MM / FR19+150MM, BTWN STR26L / 27L+80MM. THE NICKS REPORTED EXCEED THE LIMITS FOR NON-SIGNIFICANT DAMAGE AND THE ALLOWABLE DAMAGE PER SRM53-10-01 AD51, DUE TO THEIR LOCATION WSDR EE4Y2025111423448Skin · damagedDURING STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGES (LSD) WERE FOUND ON THE FUSELAGESKIN. THE LSDS WERE REMOVED BY BLENDING THE AFFECTED AREAS IN ACCORDANCE WITH SRM 51-10-03(BLEND-OUT TYPES A AND D). THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-9307SDR EE4Y2025111423446Skin · damagedDURING STRUCTURAL INSPECTION, SMALL NICKS AND LIGHTNING STRIKE DAMAGES WERE FOUND ONTHE FUSELAGE SKIN. MOST NICKS WERE REMOVED VIA BLEND-OUTS. 3 LSDS WERE REMOVED BY DRILLING THE SKIN. THE CONDITION REPORTED WAS REPAIRED IAW ETD2025-190-930784 AND DOCUMENTED PSDR SWIA2026020975223Skin · gougedLOWER SKIN GOUGED AT APPROXIMATELY BS 969, STGR 27. REPAIRED LOWER SKIN GOUGE AT APPROX BS 969, STGR 27 IAW REO 670-53-00-290 REV F.SDR SWAA2025122235042Skin · corrodedCORROSION ON EXTERNAL SKIN BTW BS 967 AND BS 986.5 AND BTW STR 26L AND STR 27L LOWER FUSELAGE. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q018UWBN.SDR ASAA2025111363113Transition Panel · corrodedUPON REMOVAL OF AFT PIT SIDEWALL PANEL FOUND L/H TRANSITION TO HAVE CORROSION AT BS 727-767. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO L/H TRANSITION PANEL FROM STA727 TO STA 767 IAW SRM 51-40-02-OG-OW= 1/2" O= .040 R= 0 L= 1/4" D= .040.SDR SWIA2025120300113Doubler · corrodedWASTE SERVICE PANEL CUTOUT FLANGE HAS CORROSION ON FWD SIDE. REMOVED AND REPLACED WASTE SERVICE BOX DOUBLER IAW SRM 51-40-08. REPLACED WITH FACTORY PART.SDR CALA2025111711284Skin · damagedFOUND LARGE CREASE IN SKIN ABOVE TOILET SERVICE PANEL.DAMAGE MEASURES APPROXIMATELY 39" LONG X 5" WIDE LOCATED BETWEEN FUSALAGE BS 848 & 887, AND STRINGERS 21L & 22L. INITIAL DEPTH MEASURES 5 TO 7 MM. PER THE REF SRM 53-00-01-1A-5 FIG. 102 SHEET 6 DAMAGE EXCSDR CALA2025111711241Skin · gougedRAMP REPORTING DAMAGE TO ACFT, FERRY FROM EWR, CUT AND REMOVED DAMAGE IAW SRM 53-00-01-2R-3. PERFORMED HFEC ROTOSCAN IAW NDTM PART 6, 51-00-00 PROCEDURE 16, HFEC ON HOLES THAT WERE CLEANED ON REPAIR PER NDT PART 6 51-00-00 PROC 16, NO ADDITIONAL DEFECTS SDR DALA2025111408357Skin · damagedFR 61 FOUND TOOLING MARKS ON INTERNAL SKIN SURFACE AT FR 61 BETWEEN STGR 2L-3L. REPAIRED PER A330 SRM 53-11. (1303016)SDR DALA2025111408356Skin · damagedFOUND TOOLING MARKS ON INTERNAL SKIN SURFACE AT FR 61 BETWEEN STGR 1L-2L. REPAIRED PER A330 SRM 53-11. (1303014)SDR EE4Y2025111323455Skin · dentedDURING A STRUCTURAL INSPECTION, A DENT WAS IDENTIFIED ON THE CENTER FUSELAGE LOWER SKIN AT FRAME 27 AND BETWEEN STRINGERS 27LH-28RH. ACCORDING TO DOCUMENTATION FROM THE PREVIOUS OPERATOR, THE DENT WAS ASSESSED UNDER REFERENCE ETD2017-190-094601. THE AREA IS CSDR EE4Y2025111323457Skin · damagedDURING A STRUCTURAL INSPECTION, NICKS WERE FOUND ON THE FUSELAGE SKIN AT FR 26 AND STRINGER 27L. THE DAMAGE WAS REMOVED VIA BLEND-OUT IN ACCORDANCE WITH SRM 51-10-03. THE RESULTING BLENDED AREA WAS EVALUATED PER SRM 53-21-01 AD51 AND DETERMINED TO BE OUT OF LISDR EE4Y2025111323456Skin · nickedDURING A STRUCTURAL INSPECTION, NICKS WERE IDENTIFIED ON THE FUSELAGE SKIN FROM FR 32 TO FR 32 + 175 MM, BETWEEN STRINGERS 27R AND 28R. THE DAMAGE WAS REMOVED VIA BLEND-OUT IN ACCORDANCE WITH SRM 51-10-03. WHILE MOST OF THE BLENDED AREA WAS CLASSIFIED AS NON-SSDR EE4Y2025111323454Skin · dentedDURING A STRUCTURAL INSPECTION, A CRACK WAS FOUND IN FWD FUSELAGE SKIN DENTED, BTWN FR18/19, BTWN STR-18R/19R. THE AFFECTED AREA WAS REPAIRED IAW ETD2014-190-051915 AND DOCUMENTED PER COOPESA EO COO-EO-2025-23345. UNDER JOB A1Q219 NRI 21-81.SDR EE4Y2025111323453Skin · damagedDURING STRUCTURAL INSPECTION, A DENT WITH OIL CANNING AND SEVERAL NICKS LOCATED BETWEEN FR17 AND FR19 WERE FOUND, AND BETWEEN STRINGERS 26R AND 26L. MOST NICKS WERE REMOVED BY BLENDING AND CLASSIFIED AS NON-SIGNIFICANT DAMAGES PER SRM 51-75-16. HOWEVER, THREE SDR EE4Y2025111323449Skin · damagedDURING A STRUCTURAL INSPECTION, LIGHTNING STRIKE DAMAGE (LSD) WAS FOUND ON THE FUSELAGE SKIN AT FR 97 + 25 MM, STR-27LH, DUE TO ITS PROXIMITY TO THE STRINGER 27L FASTENER ROW, THREE FASTENERS WERE REMOVED. AFTER DAMAGE REMOVAL VIA BLEND-OUT IN ACCORDANCE WITH
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