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 CALA2026080918408Skin · corrodedEXTERNAL FUSELAGE, APU INLET CUTOUT EXTERNAL, HAS EVIDENCE OS CORROSION AT BS 1825, S6R AND BY BS 1787, S3R. PERFORMED REPAIR AT APU INLET CUTOUT STA 1825 IAW SRM 5 3-80-15-2R-1, REPLACED FWD STRAP AT BS 1787 BTW S3-6R, 2 EA SUPPORT ANGLES BTW BS 1825 - 1787SDR BAGA2026081300006Doubler · corrodedACFT IN HEAVY CHECK. CORROSION ON WASTE DOUBLER. REAR BARREL FR 75 WASTE DOUBLER INBOARD CORNER FOUND CORROSION. WASTE DOUBLER REPLACED C/O IAW REO-500-53-61-2718, & EC CATC-53-EA-02917.SDR AALA202608102472Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACKED FUSELAGE SKIN PANEL AT FR 14 BETWEEN Z780 AND Z950 - REPAIRED SKIN PANEL PER EA 377882SDR DALA2026080904592Skin · corrodedDURING CCK IN MSP, MAINTENANCE WAS ACCOMPLISHING ROUTINE CARD 2021-2025 AND FOUND CORROSION COMMON TO THE AFT WASTE SERVICE DOOR AREA. CORROSION IS COMMON TO THE DOOR AT HINGE ARM ATTACHMENT AND ON THE DOUBLER INBOARD FORWARD AND AFT CORNERS. THE FUSELAGE SKINSDR SWIA2026080776758Skin · demodificationPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN BS 100000 - 101500 AND STR 25R - 26R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM DETERMINED TO BE A MAJOR REPAIR. PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKISDR DALA2026082504824Skin · corrodedER/A 618056-14 REV A ISSUED FOR CORROSION REPAIR TO THE LOWER AF T FUSELAGE SKIN AND WASTE BOX AREA. FOLLOW ON ACTION IS REQUIRED. ERA 618056-14 REV A SECT. IV ACCOMPLISHED IN MSP 07AUG26. SECTION II REPEAT INSPECTIONS ARE REQUIRED @ EVERY 1000FH AFTER SECT.I SDR CALA2026082518898Skin · damagedAFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FASTENER BTW STA 400 AND 2" BELOW OF S-20R. (REF AAR NR 1000084255).PERFORMED REPAIR LIGHTNING STRIKE ON FASTENER BTW STA 400 AND 2" BELOW OF S-20R, IAW B737-900ER SRM 53-00-01-2R-41 THIS REPAIR I S A CATEGORSDR CALA2026081718644Fastener · damagedAFTER PHASE II INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER AT BS 293, S18R. PERFORMED REPAIR OF THE LIGHTNING STRIKE ON FASTENER IAW SRM 53-00-01-2R-40, THIS REPAIR IS A CATEGORY A REPAIR STEP 2.A.SDR CALA2026081118492Skin · damagedAFTER PHASE II INSPECTION, FOUND A LIGHTNING STRIKE ON FUSELAGE SKIN BTWN BS 221 & 7.7 INCHES BELOW S17R. PERFORMED A REPAIR ON FUSELAGE SKIN IAW SRM 53-00-01-2R-38, THIS REPAIR IS A CATEGORY A REPAIR.SDR CALA2026081118490Skin · damagedAFTER PHASE II INSPECTION, FOUND A LIGHTNING STRIKE ON FUSELAGE SKIN BTWN BS 199 AND 7.5 INCHES BELOW OF S-17R. PERFORMED A REPAIR ON FUSELAGE SKIN IAW SRM 53-00-01-2R-38, THIS REPAIR IS A CATEGORY A REPAIR.SDR CALA2026081118488Skin · damagedAFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN BTW BS 213.8 AND 8 INCHES BELOW OF S17R. PERFORMED REPAIR LIGHTNING STRIKE ON SKIN BTW BS 213.8 AND 8 INCHES BELOW S17R, IAW SRM 53-00-01-2R-38 THIS REPAIR IS A CATEGORY A REPAIR.SDR CALA2026081118486Plate · corrodedLOWER TCAS ANTENNA MOUNTING SURFACE SKIN HAD GOUGES AND CORROSION. REMOVED AND REPLACED ADAPTER PLATE IAW DWG 141A3501, REV- AND SRM 51-40-02. RESTORED PROTECTIVE TREATMENT IAW AMM 51-21-99.SDR FDEA202608071109Skin · corrodedAVIONICS COMPARTMENT FR 18 - 19, STRINGERS 50L - 51L INNER SKIN CORRODED. REPAIRED THE CORRODED SKIN AT AVIONICS COMPARTMENT FR18 - FR19, S50L - S51L. THIS IS CATEGORY B REPAIR DUE TO AWAITING FURTHER DAMAGE TOLERANCE ASSESSMENT(DT) APPROVAL. SOLUTION LIFE ORSDR CALA2026081118446Skin · damagedAFTER PHASE II INSPECTION, FOUND POSSIBLE LIGHTNING STRIKE ON FUSELAGE SKIN BTWN BS 500C - 500D, STRINGER 18R. PERFORMED A REPAIR TO THE SKIN IAW SRM 53-00-01-2R-41 THIS REPAIR IS A CATEGORY A REPAIR AND NOT REQUIRE REPETITIVE INSPECTIONS STEP 2.A.SDR CALA2026081118444Skin · damagedAFTER PHASE II INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER BTWN BS 360 AND 2 INCHES ABOVE OF STRINGER 14R. PERFORMED A REPAIR ON SKIN, PERFORMED NDT, NO CRACKS FOUND, THIS REPAIR IS CATEGORY A AND NOT REQUIRE REPETITIVE INSPECTIONS, ALL WORK PERFORMED IAWSDR CALA2026081118442Skin · damagedAFTER PHASE II INSP, FOUND LIGHTNING STRIKE ON SKIN BTWN BS 187 AND 8.5 INCHES BELOW OF STRINGER 17R. .REMOVED PAINT FROM SKIN IAW AMM 51-21-11-150-810. PERFORMED VISUAL INSP OF THE DAMAGE LOCATION, DAMAGE IS NO MORE THAN 0.5 INCH OF LEGHT AND BLEND OUT IAW SSDR CALA2026081118440Skin · damagedAFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FASTENER BTW STA 197 AND 8.3 INCHES BELOW OF STRINGER 17R. PERFORMED REPAIR IAW SRM 53-00-01-2R-41 THIS REPAIR IS A CATEGORY A REPAIR AND NOT REQUIRE REPETITIVE INSPECTIONS STEP 2.A.SDR CALA2026081118438Skin · damagedAFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FASTENER BTWN BS 236 AND 10" ABOVE OF EXTERNAL POWER. PERFORMED REPAIR IAW SRM 53-00-01-2R-40 THIS REPAIR IS A CATEGORY A REPAIR STEP 2.A.SDR CALA2026081118436Skin · damagedAFTER PHASE II INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER BTWN BS 294 & STRINGER 19R. PERFORMED REPAIR OF THE DAMAGE ON FASTENER. THIS REPAIR IS A CATEGORY A REPAIR AND NOT REQUIRE REPETITIVE INSPECTIONS IAW STEP 2.A.SDR CALA2026081118434Skin · damagedAFTER PHASE II INSPECTION, FOUND LIGHTNING STRIKE ON FASTENER BTW BS 328 & STRINGER 19R. PERFORMED REPAIR OF THE LIGHTNING STRIKE ON FASTENER IAW SRM 53-00-01-2R-40 THIS REPAIR IS A CATEGORY A REPAIR.SDR CALA2026081118432Skin · damagedAFTER PHASE II INSPECTION FOUND LIGHTNING STRIKE ON FUSELAGE SKIN BTW STA 322 AND 1 INCH ABOVE OF STRINGER 18R. PERFORMED A REPAIR OF LIGHTNING STRIKE ON FASTENER BTW BTW BS 322 AND 1 INCH ABOVE OF S18R, IAW SRM 53-00-01-2R-38. THIS REPAIR IS A CATEGORY A RESDR SWIA2026080776757Skin · abnormalPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13L - 14L DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO LT FWD FUSLESDR SWIA2026080776756Skin · abnormalPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO RH FWD FUSLEAGE SKIN LOCATED BETWEEN BS 394 - 409, STR 13R - 14R DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO RT FWD FUSLESDR SWIA2026080776755Skin · abnormalPERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN BS 830.40 - 847, STR 1L - 0 DUE TO THE DEMODIFICATION OF ATG 4 WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR). PERFORMED PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEASDR WX0A2026081032917Skin · dented(MAJOR REPAIR) (AIRCRAFT NOT GROUNDED) DURING BIRD STRIKE INSP FOUND DENT BELOW FO'S WINDOWS ON FUSELAGE (INITIAL DEFECT: 2174315) / ACCOMPLISHED SECTION 1 - INTERIM REPAIR IAW STS EA 79-2026-173 REV. IR. PERFORMED PERMANENT REPAIR PER STS EA 79-2026-188 REV ISDR CALA2026080918398Skin · damagedAFTER PHASE II INSPECTION FOUND POSSIBLE LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 727E - 727F, STR 24R - 25R. PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN BS 727E & 727F, STR 24R - STR 25R, ORIGINAL THICNESS: 0.090" MATERIAL LOSS: 0.005" REMAINING THICKNESSSDR CALA2026080918396Skin · damagedAFTER PHASE II INSPECTION, FOUND POSSIBLE LIGHTNING STRIKE ON FUSELAGE SKIN BETWEEN BS 500A TO 500B, STR 19R. PERFORMED REPAIR ON FUSELAGE SKIN BETWEEN BS 500A - 500B, STR 19R, IAW SRM 53-00-01-2R-41.SDR CALA2026080918386Skin · corrodedCENTER UPPER SKIN NR 1 PANEL AT BS 95.5 & RBL 74.81, RBL 97.42 WAS REPAIRED AT GIG. THIS REPAIR IS A CATEGORY C REPAIR AND MUST BE REPLACED. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF THE LATEST REVISION OF EC/RA 5710-02887 ON OR BEFORE 15,128 TOTAL FLIGHT CYSDR YENA2026080700663Doubler · corrodedDURING HEAVY MAINTENANCE, EA AC26-609-01, FUSELAGE / REAR FUSELAGE / WASTE ACCESS DOUBLER FR 75-76 & STGR 32L-35L. CORROSION - TEMPORARY REPAIR (CONSIDERED MAJOR REPAIR)SDR IXXA20260806001Skin · corrodedCORROSION ON SKIN AT BS 955 WHERE THE PICKLE FORK COMES IN CONTACT BELOW THE FLOOR.SDR DALA2026080604543Skin · crackedCRACK ON EXTERNAL FUSELAGE SKIN BS 1087 BTW LONG 13L & 14L, COMPLIED WITH ER/A 635909-14. (1741062) (AIRCRAFT GROUNDED).SDR SWIA2026080577073Skin · damagedLIGHTNING STRIKE FR 1-2 STR 28R-26R (C-CHECK RO 08/30/2026)PERFORMED PERMANENT DOUBLER TRIPLER REPAIR ON FWD LOWER FUSELAGE SKIN FR 01-02 STGR 28R-26R REF. ETD2026-170-013578 REV. C. REPAIR WEIGHT MEASURED 531.7 GRAMS REF. GMM CH. 3, SEC. 12, ITEM 1.1.3. CALSDR FDEA202608051111Skin Panel · crackedFUSELAGE FRAME, FR 54 LATERAL PANEL THREE HOLES CRACKED AT STRINGER 36L, 44L - 44R. COMPLIED WITH EA 6-5330-T0388383 P1 REPAIRED THE FUSELAGE FRAME FR54 LATERAL PANEL 3EA CRACKED HOLES AT S36L S44L S44R. EA TITLE: FUSELAGE - PLATES & SKINS - CRACK HOLES OSDR SWIA2026080576738Skin · damagedAIRCRAFT FUSELAGE SUSTAINED DAMAGE DURING MAINTENANCE BETWEEN BS 265 AND BS 280 AND BETWEEN STR 27L AND STR 26L. PERFORMED PERMANENT REPAIR TO FUSELAGE SKIN BTWN BS 265 & BS 280, STR 26 - 27L IAW REO 670-53-11-2354. ALSO COMPLETED CARD ST 51-900-1002-SKY.SDR DALA2026080604536Skin · damagedIMPACT DAMAGE BETWEEN FR63-64 FROM S-39L TO S-42R. THE DAMAGE CONSISTS OF DENTS AND GOUGES TO THE SKIN PANEL. COMPLIED WITH ER/A 635883-14 PRI REV 0, ER/A 635883-14 PRI REV 1, ER/A 635883-14 PRI REV 2, ER/A 635883-14 PRI REV 3, ER/A 635883-14 PRI REV 4, ER/ASDR KCSA202608051123Skin · crackedDURING HFEC SURFACE INSPECTION OF OUTER SKIN, CRACK INDICATION AROUND FASTENER FOUND AT STA 1456 STR 23LSDR SWIA2026080477108Antenna · demodificationCOMPLY WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44) COMPLIED WITH LH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). WEIGHT OF REPAIR PARSDR SWIA2026080477105Antenna · demodificationCOMPLY WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44) COMPLIED WITH RH SIDE ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). WEIGHT OF REPAIR PASDR SWIA2026080477104Antenna · demodificationCOMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44) COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93. REPAIR PARTS WEIGH 330.1 GRAMS NO CHANGE TO WEIGHT AND BALASDR SWIA2026080477102Antenna · demodificationCOMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR IAW DWG 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-03 (EA ERJ4111-44). WEIGHT OF REPAIR PARTS LESS THAN SDR SWAA2026090142229Stringer · crackedSTRINGER18AL BS 727 UPPER FASTENER HOLE COMMON TO INNER CHORD INDICATES A CRACK DEFECT IN STR.18A PER BOEING NDT MANUAL PART6, 51-00-00 PROC.16. L/H STR.18A STA.727 UPPER FASTENER HOLE COMMON TO INNER CHORD INDICATES A CRACK DEFECT IN STR.18A PER BOEING NDT MASDR IPXA2026081903745Skin · crackedMAJOR REPAIR, SKIN , DURING PERFORM T/C : EO-24301-JIC001 FOUND SKIN CRACK AT BS 1725.5 , S-7R. ACCOMPLISH THE REPAIR I.A.W EO-24301-JIC3 REV7 AND SRM 53-80-01-2R-5 REV.95 AND EGAT WORK SHEET NO.60614 AND EO-98363-REQ1 REV1.SDR COEA2026092809807Skin Panel · dentedWO 275319 NR 3 HEAVY CHECK COE/MAJOR REPAIR: EXTERNAL FUSELAGE SKIN BETWEEN FRAMES 5-6 STRINGERS 11R-12R DENTED. CORRECTIVE ACTION: REPAIRED PER SRAS-00054254-01 ISSUE A, DATED 8/18/2026.SDR DALA2026080604532Skin · scratchedSCRATCH EXTERNAL SKIN LOCATED BTW FR 56 TO FR 57 AND STR 25L TO STR 26L AT LOWER FUSELAGE. PERFORMED REPAIR INSTRUCTIONS ON EXTERNAL SKIN LOCATED BTW FR 56 - 57, S25L - 26L AT LOWER FUSELAGE IAW SRM 53-41-11-300-109, RECHK IS REQUIRED DUE TO THIS REPAIR IS COSDR CALA2026080518272Skin · crackedEA 5330-07074 REV C OP 002, RT FUSELAGE SKIN COMMON TO UNDERWING LONGERON BTWN BS 1014 & 1035, S37R CRACKED. SKIN REPLACED IAW EA 5310-07557, OP 008.SDR DALA2026080404488Skin · crackedCRACKS FUSELAGE SKIN STA Y=1087, L-13L TO L-14L. REPAIRED PER ERA 635909-14. (1735466) AIRCRAFT WAS GROUNDED.SDR FDEA202608031080Skin · corrodedLWR FUSELAGE AFT POTABLE WATER DRAIN DOOR CUT OUT POSSIBLE CORROSION COMPLIED WITH EA F-5330-T0388116P1 AFT LAV PAN CUTOUT SKIN CORROSION REPAIR BTW BS 1681-1701 S26R - 29L.SDR REXA2026091001782Skin · corrodedCORROSION ON INTERNAL FUSELAGE SKIN ON SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR INTERNAL FUSELAGE SKIN ON SETTLEMENT AREA OF MAIN AVIONICS COMPARTMENT DOOR WAS REPAIRED PER REO 690-53-21-032 REV. - -SDR DALA2026080604547Skin · dentedDENT FOUND ON THE FUSELAGE BTWN BS 218 - 229, COMPLIED WITH ER/A 636117-14. (1734913) (AIRCRAFT GROUNDED).SDR DALA2026080504502Doubler · corrodedWASTE BOX DOUBLER CORROSION AT CUTOUT ON FWD RH CORNER AND AFT EDGE. COMPLIED WITH ER/A 613288-14 REV A PRI REV 0, ER/A 613288-14 REV A PRI REV 1, AND FINAL ER/A 613288-14 REV A. (LP# 1734788: AIRCRAFT WAS GROUNDED)
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