JASC 5330
Service difficulty reports · 79,281
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 JR2R20260511881Doubler · corrodedAFT WET AREA LH SILL O/B DOUBLER CORRODED. REPLACEDSDR VNAA202606300002Skin · damagedFUSELAGE LIGHTNING STRIKE DAMAGE. DAMAGE AROUND FASTENER CSK BY NEXT HEAVY MAINTENANCE VISIT (HMV), PERFORM PERMANENT REPAIR PER SRM 53-00-00-201-003-A03 SECTION 5.C.(4) - PERMANENT DISPOSITION TO FUSELAGE SKIN AROUND THE FASTENER COUNTERSINK FOR DAMAGE DEPTHSDR ASAA2026051065948Bear Strap · damagedAFT CARGO PIT DOOR FRAME AT AFT UPPER CORNER HAS NICK WITH BARE METAL SHOWING. GROUNDED - YES. ACCOMPLISHED CATEGORY "A" MINOR REPAIR TO AFT CARGO DOOR CUT-OUT BEAR STRAP P/N 146A3270-2 AT STA 847 BETWEEN STGR 19R-20R IAW EA M9-53EA-30277 REV 00.SDR DALA2026051102937Skin · dented: RE-EVALUATE DENT FOR BIRD STRIKE EXTERNAL SKIN LOC. BTW FR1 TO FR 2 AT LEVEL OF -Z339 RH SIDE UPPER FUSELAGE (REFERENCE TO LOG PAGE 8221811). PERFORMED PERMANENT REPAIR AS PER A320 SRM 53-11-11-300-041, LOCATED ON EXTERNAL SKIN BTW FR 1 TO FR 3 AT LEVEL OF SDR SWIA2026050977016Skin · scratchedWHILE INVESTIGATING DAMAGE TO FUSELAGE SKIN ASSOCIATED WITH CP 32002666 FOUND 2 OFF SCRATCHES ON EXTERIOR SURFACE OF FUSELAGE SIDE SKIN P/N 601R38327-52 AT FS559.00 +5.00, BETWEEN STR 8R AND STR 10R. (C-CHECK RO 08/28/2026)PERFOMED MAJOR REPAIR TO 2 SCRATCHESDR HNAA2026061700537Skin · gouged00413 FUSELAGE EXTERNAL SKIN AT FR 7, STR 15L, UNDER GPU ACCESS DOOR HAS A GOUGE. PERFORMED CUTOUT AND INSTALLED FABRICATED FILLER AND DOUBLER TO FUSELAGE EXTERNAL SKIN AT FR 7 STR 15L UNDER GPU ACCESS DOOR IAW EMB 145 SRM M53-12-01-RE STEP 2 FIGURE 201 SEE PSDR VNAA202606120003Skin · damagedLIGHTNING STRIKE ON SEVERAL FASTENERS BTW STR 23L AND BS 210 - 265. LIGHTNING STRIKE ON SEVERAL FASTENERS BTW STGR 23L AND BS 210 - 265 WERE REPAIRED IAW SRM 53-00-00-201-003-A01.SDR JJBA20260520023Skin · damagedCREASE ON LH FWD FUSELAGE BETWEEN STGRS 15-16 AND FRAMES 11-12 CLOSE TO FRAME 12. RECOUNTOUR WAS PERFORMED.SDR DALA2026051302989Skin · corrodedCORROSION FOUND AT LAV SERVICE DOOR DURING DVI PER ER/A 612058-14 SECTION 2. COMPLIED WITH ER/A# 634152-14 REV-ORIGINAL ASSOCIATED ER/A 14-634152 ADDED FOR AC 8304. (LP# 1585400; AIRCRAFT WAS GROUNDED)SDR DALA2026051302988Skin · corrodedCORROSION FOUND AT LAV SERVICE AREA DURING DVI PER ER/A 612058-14 SECTION 2. COMPLIED WITH ER/A# 634152-14 REV-ORIGINAL ASSOCIATED ER/A 14-634152 ADDED FOR AC 8304. (LP# 1585396; AIRCRAFT WAS GROUNDED)SDR SIMA20260508002Skin · damagedFUSELAGE SKIN REPAIR (MAJOR REPAIR). COMPLIED WITH ERS-EJ-53MR-5470 FUSELAGE SKIN REPAIRSDR CALA2026052816575Skin · dentedFUSELAGE AT L1 DOOR CUTOUT MIDDLE HINGE PANEL WITH UPPER CORNER DENTED. REMOVED AND REPLACED MIDDLE GAP COVER SKIN PANEL AT L1 DOOR FWD CUTOUT IAW SRM 51-40-02-0G-0 AND DWG 141A3110.SDR CALA2026052816571Skin · dentedFUSELAGE AT L1 DOOR CUTOUT LOWER HINGE PANEL WITH LOWER CORNER DENTED. REMOVED AND REPLACED LOWER GAP COVER SKIN PANEL AT L1 DOOR FWD CUTOUT REF SRM 51 -40-02-0G-0 AND DWG# 141A3110.SDR IPXA2026051576502Seal Depressor · dentedFAULT-DENT-DEPRESSOR, MAIN DECK CARGO DOOR CUTOUT AFT UPPER SIDE (REPLACE) INSTALLED THE MAIN DECK CARGO DOOR DEPRESSOR SEAL I.A.W AMM 20-11-00-910-802 REV.148, SCREW TORQUE 30 IN-LB.SDR DALA2026051202964Skin · wornUPPER FUSELAGE EXTERIOR SKIN STA 727B TO 727E (RADOME AREA), EVIDENCE OF WEAR DAMAGE ON SKIN AROUND ANTENNA ADAPTER PLATE INTERFACE AT APPROX. 4, 5, 7, 8, AND 11 O'CLOCK POSITIONS. ACCOMPLISHED REPAIR ON UPPER FUSELAGE EXTERIOR SKIN STA 727B-727E (RADOME AREA)SDR SWIA2026050777454Skin · corrodedCORROSION FOUND ON INNER FUSELAGE SKIN BETWEEN FS310 AND FS319 , STR25L TO STR26L. REPAIRED INNER SKIN IAW REO 670-53-21-2887 REV-.SDR SWIA2026050776901Skin · corrodedAIRCRAFT SKIN AT PANEL 195BB HAS CORROSION AT FASTENER HOLES. REPAIRED CORROSION DAMAGE ON AIRCRAFT SKIN AT PANEL 195BB AT FASTENER HOLES IAW REO 601R-53-61-8546, REV--, SEE CONTINUE CARD FOR WORK PERFORMED, COMPLIED WITH 51-900-1003-SKY. LEAK CHKD OK.SDR IPXA2026051070809Skin · dentedRH FUSELAGE HAS A DENT STA#1355 BETWEEN RBL S-13R & S-14R #58-01. DISCOVERED IN LIMIT DENT INFO DEFERRED IAW UPS EO97560-REQ1, IN LEAVE AS IS CONDITION.SDR HNAA2026060400483Rivet · misinstalledEXTERNAL RIVET PLUG IMPROPERLY INSTALLED AT BTW FR2-3 AND ABOVE STR14L NEAR UPPER SKIN EDGE. REPAIRED IAW ETD2026-145-008984 AND EO1-53-26-0258SDR HNAA2026060300480Rivet · looseEXTERNAL SKIN: LOOSE RIVET PLUG BTW FR1A-2, BTW STR14-15L. REPAIRED IAW ETD2026-145-008939.SDR AALA202605224449Skin · wornAIRCRAFT IN BASE MAINTENANCE: WEAR TO AFT CARGO COMPARTMENT FUSELAGE SKIN INTERNAL SIDE, BETWEEN STA 727 AND STA 747, BETWEEN S26R AND S27R. ACCOMPLISHED DOUBLER REPAIR PER SRM 51-20-10 AND EA 374286.SDR IPXA2026051959294Skin Panel · crackedMAJOR REPAIR. CRACKED FWD ENTRY DOOR AFT LOWER CORNER SKIN ACCOMPLISH THE REPAIR I.A.W EO-87307-REQ7 REV2 AND SRM 53-10-01-2R-1 REV.95 AND EGAT WORK SHEET NO.60365 AND UPS EO NO. EO-97461-REQ1 REV1.SDR AALA202605084122Doubler · wornAIRCRAFT IN BASE MAINTENANCE: WEAR TO ELECTRICAL GROUND POWER RECEPTACLE SURROUND DOUBLER AT STA 224.8 BETWEEN S22R AND S23R. REPAIRED DOUBLER PER SRM 53-10-15-2R.SDR DALA2026051403014Doubler · corrodedER/A 634152-14; A220-300 / REAR BARREL FUSELAGE WASTE BOX INTERNAL DOUBLER & SERVICE DOOR CORROSION. SUBJECT REPAIR REQUIRES FOLLOW-ON ACTION. ACCOMPLISH 634152-14, SECTION II REPETITIVE INSPECTION WITHIN EVERY 1,000 FLIGHT HOURS FROM 13,074 TOTAL AIRCRAFT FLSDR DALA2026051102946Skin · ground damageAIRCRAFT STRUCK BY BAG LOADER AND KNOCKED OFF COMM 1 ANTENNA. REPAIRED PER ERA 634130-14 (6545520) (AIRCRAFT GROUNDED)SDR SWAA2026050895896Skin · peelingAFT INNER SKIN EDGE COMMON TO L1 DOOR IS BENT INWARD 19.5 INCHES DOWN FROM AFT DOOR FRAME. PEELING SKIN ON L1 DOOR MEASURED 6.00?L BY 0.25?W BY 0.135? D. NO REFERENCE FOUND FOR PEELING BACK SKIN. IF CONSIDERED DENT A/Y IS 1.85 AND IS FOUND OUT OF LIMITS PER SSDR VNAA20260508003Skin · ground damageMANLIFT MADE CONTACT WITH AIRCRAFT BETWEEN FS 1144 - FS 1162. REPAIRED AREA BETWEEN SKIN STGR 5L -7L AND FRAME 55.625% - SPAR 67.50% IAW MHIRJ REO 670-53-71-102 REV -- DATED 2026-04-23.SDR SWIA2026050577158Skin · corrodedFUSELAGE SKIN IS CORRODED AT BS 559.112 CIRCUMFERENTIAL JOINT BETWEEN STRINGERS 27 AND 26R. REPAIRED CORRODED FUSELAGE SKIN IAW REO 601R-53-51-745 REV --.SDR REXA2026070301050Skin · corrodedCORROSION ON SKIN AND STGR 21R BTW FS 349.00 TO 364.00 AND BTW STGR 20R TO 21R AT FUSELAGE INTERNAL STRUCTURE. CORROSION ON SKIN WAS REPAIRED PER EA CRJ953-22252 REV. IR AND STGR 21R BTW FS 349.00 TO 364.00 AND BTW STGR 20R TO 21R WAS CLEANED AND NOT FOUND COSDR AALA202605289820Skin Panel · wornAIRCRAFT IN BASE MAINTENANCE: UPPER REAR FUSELAGE CROWN SKIN PANEL WORN AT THE VIASAT ANTENNA MOUNTING AREA BETWEEN FR 62 AND FR 63, BETWEEN S1R AND S2R. REPAIRED SKIN PANEL PER EA 375293.SDR CALA202602150107Skin · ground damageA}7C HITTED BY LAV TRUCK, NEXT TO LAV SERVICE DOOR. CONDITIONAL INSPECTION FOR HIT WITH GROUND EWUIPPMENT PERFORMED IAW AMM 05-51-59-200-801 BETWEEN BS 867 & 905 AND S-22 LH& S-24 LH // PERMANENT REPAIR PERFORMED IAW ERI-132-2026SDR REXA2026070301045Skin · corrodedCORROSION ON SEATTLEMENT AREA OF AFTER CARGO PROTECTOR PLATE. SEATTLEMENT AREA OF AFTER CARGO PROTECTOR PLATE WAS REPAIRED PER EA CRJ953-22285 REV IRSDR SWAA2026060895300Angle · crackedCRACKED ANGLE, BS 400, S26L, FWD CARGO BAY. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A7545, SHEET 2, REV:B.SDR REXA2026060400902Skin · chafedWEAR ON EXTERNAL FUSELAGE SKIN LOCATED BTW BS 897 - 913 AND STGR 27. EXTERNAL FUSELAGE SKIN LOCATED BTW FS 897.00 TO FS 913.00 AND STGR 27 WAS REPAIRED PER REO 670-53-00-290 REV. -F, PL 670-53-00-29 0 SHEET #5, REV.-E FIGURE 3.SDR SWIA2026050476106Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BSDR SWIA2026050476105Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATESDR SWIA2026050476104Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13L - STRG 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LH FWD FUSLEAGESDR SWIA2026050476103Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN FS 394.00 - FS 409.00 AND STRG 13R - STRG 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGESDR SWIA2026050476102Skin · damagedPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN FS 830.40 - FS 847.00 AND STRG 1L - STRG 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (FILED CLOSED)PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKINSDR SWIA2026050476100Skin · damagedCOMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 05/24/2026)COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). SEE CSDR SWIA2026050476099Skin · damagedCOMPLY WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 05/24/2026)COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44SDR SWIA2026050476098Skin · damagedCOMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 05/24/2026)COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). SEE CSDR SWIA2026050476097Skin · damagedCOMPLY WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 05/24/2026)COMPLIED WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-4SDR HNAA2026052000422Skin · damagedCOCKPIT UNDERFLOOR HATCH 123BL HAS TOOLING MARK ON EXTERNAL SKIN CLOSE TO THE BLACK RUBBER SEAL. REPAIRED COCKPIT UNDERFLOOR HATCH 123BL TOOLING MARK ON EXTERNAL SKIN CLOSE TO THE BLACK RUBBER SEAL IAW PIEDMONT EO1-52-26-0223 AND ETD2026-145-007987.SDR IPXA2026050716996Skin · damaged*** MAJOR REPAIR *** TO LINK AND ACCOMPLISH EO-97088-REQ1 (N122UP: FUSELAGE SKIN LEFT AND RIGHT SIDE EXTERNAL DOUBLER REPAIRS AT FR7 AND FR8) REVIEWEDSDR SWAA2026052695211Skin · crackedFOUR CRACKS FOUND BETWEEN BS 727A - 727D APPROX. 3IN ABOVE STR14. FUSELAGE CRACK AT BS727A REF TTG8Q01BZCXU; FUSELAGE CRACKED AT BS727D REF TTG8Q01BZCYB; FUSELAGE CRACK AT BS 727B REF FOUR CRACKS FOUND BTWN BS727A-BS727-D APPROX. 3IN ABVE STR14. REPAIRED FUSESDR DALA2026050602886Skin · damagedACCOMPLISH A REPAIR AT FUSELAGE SKIN INTERNAL DOUBLER, NLG WHEEL WELL CUTOUT LHS FR 12. COMPLIED WITH ER/A 601201-14AD REV-B (AMOC) ASSOCIATED ER/A 14-601201. (LP# 1575634; AIRCRAFT WAS GROUNDED)SDR SWAA2026052694951Skin · crackedFUSELAGE HAS A .45 VERTICAL CRACK AT BS 727A; APPROX. 3 ABOVE STR 14R; VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. .26-153-01210SDR SWAA2026052694952Skin · crackedFUSELAGE HAS A .95 VERTICAL CRACK AT BS 727B; APPROX. 3 ABOVE STR 14R. VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02. REFER TO FAULT TTG8Q01BZXU WHERE EA 26-153-01210 WAS ADDED AS A SUBTASK. SDR SWAA2026052694953Skin · crackedFUSELAGE HAS A .50 VERTICAL CRACK AT BS 727D APPROX. 3 ABOVE STR 14R; VERIFIED WITH HFEC PER NDT PART 6; 51-00-00 PROCEDURE 23 AND FLUORESCENT PENETRANT INSPECTION PER SOPM 20-20-02<[01] REFER TO FAULT TTG8Q01BZCYK WHERE EA 26-153-01211 WAS ADDED AS A SUBTAS
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