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 UIEA2024050500331Skin · crackedSECTION 42 FUSELAGE - LH STA 560 BELOW STR 23 2EA FASTENER HOLE EXTERNAL SKIN FOUND CRACK(<P>SKIN FASTENER HOLES (2EA) CRACK AREA REPAIRED AS PER SRM 53-00-01-2R-13 REPAIR B FIG 201. THIS REPAIR IS CAT B, FOLLOW UP ACTION AS PER SRM 53-00-01-2R-13 REPAIR 13 FISDR UIEA2024050500332Skin · crackedSECTION 42 FUSELAGE - LH STA 540 BELOW STR 23 2EA FASTENER HOLE EXTERNAL SKIN FOUND CRACK(<P>SKIN 2EA FASTENER HOLES CRACK AREA REPAIRED AS PER SRM 53-00-01-2R-13 REPAIR 13 FIG 201. THIS REPAIR IS CAT B, FOLLOW UP ACTION AS PER SRM 53-00-01-2R-13 REPAIR 13 FIGSDR UIEA2024051900394Skin · corrodedFUSELAGE EXTERNAL SKIN BS1705 STR 42L FOUND CORROSION.(<P>SKIN CORROSION AREA REPAIRED AS PER SRM 53-00-01-2R-1 REPAIR 1 FIG 201 DETAIL I. NO FURTHER DEFECTS NOTED.</P>)SDR SWIA202409250864Skin · mechanic errorCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA58215-601R-53-21-3299 N986SW MXCODEID51600-PR - FUSELAGE BELOW THE SERVICE DOOR CUTOUT HAS 1EA MIS DRILLED HOLE REQUIRES EVAL CORRECTIVELY REPAIRED MISSED DRILLED HOLE WITH PLATE SUPPORT IAW BOMBARDIER REO 601R-53-SDR SWI202408260771Skin · crackedRH TRU DOOR FUSELAGE SKIN CUT OUT, THE AFT LOWER CORNER POSSIBLY CRACKED IN THE RADIUS (MARKED) (C-CHECK RO 8/24/2024) REMOVED AND REPLACED THE CRACKED RH ADG SKIN ON THE RHS NOSE UNDER TRU BAY WITH NEW REPLACEMENT SKIN (P/N CC670-33109-3) USING ALL NEWSDR SWI202408260770Skin · crackedLH TRU DOOR FUSELAGE SKIN CUT OUT, THE AFT LOWER CORNER POSSIBLY CRACKED IN THE RADIUS (MARKED) (C-CHECK RO 8/24/2024) REMOVED AND REPLACED THE CRACKED HYDRAULIC BAY SKIN ON THE LHS NOSE UNDER TRU BAY WITH NEW REPLACEMENT SKIN (P/N CC670-33106-5S) USINSDR SWIA202408230611Skin · damagedTOOL MARKS ON EXTERNAL TOP SKIN COVERED BY MID AND FWD DORSAL STRAKE FAIRINGS BETWEEN APROX. FS.939.00 TO FS.1000.00 (C-CHECK RO 8/22/2024) REMOVED DAMAGED FROM EXTERNAL TOP SKIN UNDER THE MID AND FWD DORSAL STRAKE FAIRINGS BETWEEN FS939 - 1000 REF REOSDR DALA2024061406089Skin · damaged(LOG 0388439) FOUND SKIN TO BE BLENDED AROUND REMOVED FASTNER AND OVER STR 1 FASTENER AT STA500C. C/W ER/A 618414-14.SDR DALA2024061406088Skin · damaged(LOG 0388434) FOUND TOOLING DAMAGE ON EXTERNAL SKIN AROUND REMOVED FASTNER HOLE AT STA344, LBL5.5.SDR FDEA202406110793Skin · dentedDENT WITH GOUGE ON FUSELAGE SKIN AT STA 390 BTW STR 4/5 RH. FUSELAGE SKIN AT STA 390 BTW STR 4/5 RH WAS REPAIRED IAW SRM 53-00-01-2R REPAIR 14 REV 88 DEC 15, 2023.SDR JGVR20240611001Skin · corrodedBLENDED CORRODED AREAS OF THE FUSELAGE SKIN JUST AFT OF THE MAIN ENTRY DOOR, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, PRIMED AND TOPCOATED AREA PER TEXTRON FILED REPAIR.SDR K11A2024080900276Skin · corrodedSUSPECTED CORROSION ON #2 VHF ANTENNA AROUND MOUNTING AREA JUST OUTSIDE OF SEALANT PERIMETER.SDR CALA2024062601905Skin · dentedDURING WALK AROUND FOUND DENT IN A PREVIOUS REPAIR FWD OF L2 DOOR. ACCOMPLISH PART 3 PERMANENT REPLAIR WITHIN 2 FLIGHT CYCLES PER ECRA 5330-07276. PER ECRA 5330-07276 "ACCOMPLISH PART 3 PERMANENT REPAIR WITHIN 2 TOMC-APPROVAL FROM SC1ELBYC COMMENT FLIGHT CYCLSDR DALA2024061406087Skin · damaged(LOG 0386826) DURING HCK AT ATS-MCI, MULTIPLE LIGHTNING STRIKES SRM 53-00-01 REPAIR 38 CATEGORY C REPAIRS WERE LOCATED. REPAIRS WE ACCOMPLISHED PER ER/A 618414-14.SDR JGVR20240610001Skin · damagedREPAIRED BENDED AREA OF FUSELAGE LH UPPER SKIN AT APPROXIMATELY FS 518.5 AND BL 0.0, TWO AREAS OF FUSELAGE RH UPPER SKIN AT APPROXIMATELY FS 464 AND BL 0.0, AND ONE AREA FS 517 AND BL 0.0 BY BLENDING, PERFORMING NDT, TREATING AND PRIMING AREAS FOUND ACCEPTABLESDR SWI202408260740Skin · wornPAX DOOR SURROUND FWD UPPER PULL IN LEVER RAMP HAS WEAR GROOVE WORN INTO RAMP. (C-CHECK RO 8/24/2024) NO ALLOWABLE DAMAGES ALLOWED ON PAX DOOR FWD UPPER PULL IN LEVER PER REF CRJ 900 SRM 53-00-00-101-001-A01, REMOVED AND REPLACE PART (P/N: SH670-31913-3SDR SWAA2024061399980Panel · crackedPANEL 194FL HAS CRACK EXTENDING FROM APU FUEL FEED DRAIN MAST OPENING<[01] R&R PANEL#194FL REF AMM 53-51-21SDR DALA2024061005960Fastener · abnormalSHIP 684 PREVIOSLY REPAIR (PROTUDING FASTNER) WAS FOUND ON BAD CONDITION BTW STG 2-3 LH AND STA 480-500 ON FUSELAGE SKIN. CORRECTIVE ACTION: SUMMARY OF NRC 00206 PERMANENT REPAIR CATEGORY "B" BTW STA 480- 500 AND STG 2-3LH ON FUSELAGE SKIN WAS PERFORMED PER B7SDR DALA2024061005952Skin · damagedSHIP 3137 EXISTING RE-WORK EXTERNAL SKIN LOCATED BTW FR 58 TO FR 59 AND STR 28L TO STR 29L AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN BTW FR 58 TO FR 59 AND STR 28L TO STR 29L AT LOWER FUSELAGE AS PER A319 SRM 53-41- 11-3SDR DALA2024061005951Skin · nickedSHIP 3137 NICK EXTERNAL SKIN LOCATED AT FR 27 AND STR 40L TO STR 41L AT LOWER FUSELAGE. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON EXTERNAL SKIN LOCATED AT FR 27 AND STR 40L TO STR 41L AT LOWER FUSELAGE AS PER A319 SRM 53-21-11- 300-093. (0385049)SDR SWAA2024071899362Doubler · crackedCRACK ON ELECTRICAL GROUND POWER RECEPTACLE LOWER SURROUND DOUBLER AT LOWER FUSELAGE 2024-376582<[01] ON STEP 5; TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[02] REPAIRED ELECTRICAL GROUND POWER RECEPTACLE LOWER SURROUND DOUBLER AT LOSDR UIEA2024060500477Skin · damagedCREASE ON LH FUSELAGE SKIN AT STA.138.5 AND 21" ABOVE STRG 21.(<P>CREASE ON LH FUSELAGE SKIN AT STA.138.5 AND 21" ABOVE STRG 21 WAS REPAIRED PER SRM 53-00-01-2R-14. NO FURTHER DEFECT NOTED.</P>)SDR DALA2025051903827Skin · puncturedPUNCTURE ON FUSELAGE SKIN BETWEEN FR 32 AND 33 AND AT STR 26L. PUNCTURE ON FUSELAGE SKIN BETWEEN FR 32 AND 33 AND AT STR 26L. DAMAGE REPAIRED PER SECTION I: TIME-LIMITED REPAIR PER ER/A 618530-14 REV ORIGINAL. PERMANENT REPAIR IS REQUIRED WITHIN 200 FLIGHT CYCSDR DALA2024061106027Skin · damagedGROUND CREW NOTED DAMAGE FWD OF L2 DOOR. COMPLIED ERA 618530-14 REV. ORIG SECTION 1 TIME LIMITED REPAIR ON N/R 2. PERMANENT REPAIR IS TO BE ACCOMPLISHED IN 200 FLIGHT CYCLES. (LP# 5875264)SDR AALA202406117553Skin Panel · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK FOUND AT THE NOSE FORWARD FUSELAGE LEFT HAND LATERAL FORWARD SKIN PANEL EXTERNAL SURFACE RADIATING FROM FASTENER HOLE BETWEEN FR 13 AND FR 14, BETWEEN AT Z+780 AND Z+950. REPAIRED SKIN PANEL PER EA 355027.SDR DALA2024061005968Skin · noneSHIP 3309 A330 / FUSELAGE SKIN AT FR67-FR68, STGR45RH-48RH / DOUBLER REPAIR NEAR BULK CARGO DOOR CUTOUT. CORRECTIVE ACTION: COMPLIED WITH ERA 613921-14 REV A. (0381607)SDR DALA2024061005967Skin · noneSHIP 3309 A330 / FUSELAGE SKIN AT FR67-FR68, STGR45RH-48RH / DOUBLER. CORRECTIVE ACTION: COMPLIED WITH ERA 613921-14 REV A. (0381600)SDR 29GA2024060700001Skin · puncturedDURING POST FLIGHT WALK AROUND PUNCTURE FOUND IN AIRCRAFT BEHIND CAPTAINS' SEAT ON OUTSIDE OF AIRCRAFT. CORRECTIVE ACTION-LH FUSELAGE SKIN REPAIR AT AFT SIDE OF FRAME 10, 7 INCHES ABOVE STRINGER 14 HAS BEEN ACCOMPLISHED IAW SRM, POST REPAIR PRESSURE AND FUNCTISDR AALA202406075534Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: DURING THIS VISIT, PRODUCTION DISCOVERED SIGNIFICANT CORROSION DAMAGE TO THE FUSELAGE SKIN ON THE INTERNAL SURFACE IN THE AFT CARGO COMPARTMENT BETWEEN BS 727I TO 927. ACCOMPLISHED TIME LIMITED REPAIR. PER EA 352428.SDR YENA2024061100856Skin · damagedDURING HEAVY MAINTENANCE: DURING CURRENT CHECK ON N203JB (MSN: 023) @ MCN, EAMS REPORTED THREE (3) BLEND-OUT SPOTS ON THE CENTER FUSELAGE I EXTERNAL SKIN @ FR30-32 & STGR 25L-26L. SEE REF /1/, ETD REV A, FOR COMPLETE INFORMATION. EMBRAER PROVIDED ENGINEERING SDR YENA2024061100855Skin · crackedDURING HEAVY MAINTENANCE: DURING CURRENT LEASE RETURN CHECK ON N203JB (MSN 023) AT MCN DATED 05/2024, A DENT WAS FOUND ON THE FWD FUSELAGE SKIN BETWEEN FR 1-2 & STRR 22L-24L. SEE REF /1/ ETD FOR DETAILS. THE DENT IS MEASURED TO BE 0.70” L X 0.50” W AND 0.008”SDR YENA2024061100854Skin · damagedDURING HEAVY MAINTENANCE CHECK ON N203JB (MSN: 023) @ MCN, EAMS REMOVED THE EXISTING DOUBLER REPAIR IAW ETD2019-190-137093 REV A. THE DENT IS LOCATED OVER 3 BAYS AND THE REPAIR CROSSES OVER A ROW OF RIVETS BETWEEN FR98-99 AND STGR 25R-29R. AN HFEC INSPECTION WSDR SWAA2024062798895Doubler · crackedEGPR SURROUND DOUBLER IS CRACKED BS233 WL175 8' ABOVE S-24R MARKED<[01] UPON FURTHER INVESTIGATION IT WAS FOUND TO BE A PREVIOUS REPAIR FILLER THAT WAS CRACKED. PREVIOUS REPAIR WAS ACCOMPLISHED OF FAULT TTG8Q00TSS0N.;[02] CORRECTION TO CORRECTION STEP 1 SHOULDSDR CALA2024061301794Skin · crackedEA 5310-06900 REV E OP 016 1EA CRACK FOUND ON R/H FUS SKIN APPRO X 0.500" IN LENGTH REF HX NR WO.3271543, INSPECTIONS PER THE LATEST REVISION OF ECRA 5330-07272 PART 2 ON REPEAT THE INSPECTION AT INTERVALS NOT TO EXCEED 4,000 TOTAL OR BEFORE THE AIRCRAFT REACHSDR YENA2024061100859Skin · dentedDURING HEAVY MAINTENANCE: PER CUSTOMER REQUEST: CENTER FUSELAGE I EXTERNAL SKIN BTW FR30 AND FR32 STGR 25L AND STGR 26L WITH DENTS (3EA) RE-EVALUATE EMBRAER NR-00097 W/O H9417; REPAIRED 3EA AREAS ON FUSELAGE I EXTERNAL SKIN BTW FR30 AND FR32, STGR25L AND STGRSDR YENA2024061100858Skin · dentedDURING HEAVY MAINTENANCE: RE-EVALUATE DENT AT FR98-FR99 & STR25R-STR29R, THE DENT IS LOCATED OVER 3 BAYS AND REPAIR CROSSES OVER 1 RIVET ROW REF. EMBRAER NR-00179 W/O: H9417; REMOVED EXISTING REPAIR DOUBLER AND INSTALLED NEW REPAIR DOUBLER AND FILLER AT FR98-SDR YENA2024061100857Skin · dentedDURING HEAVY MAINTENANCE: COMPLY WITH E24-606-01 (REV 6-5-24 ) FUSELAGE / FWD FUSELAGE / EXTERNAL SKIN BETWEEN FR1-2 & STG 22L-24L / DENT & CRACK PERMANENT REPAIR REF. EMBRAER NR-00210 WO: H9417; COMPLIED WITH E24-606-01 REV 6-5-24.SDR DALA2024060705877Skin · damagedFUSELAGE SKIN DAMAGED BETWEEN STA 954 AND 974 LONGERON 20L AND 21L. COMPLIED WITH STEPS 1-3 PER RI 618607-14. PERFORMED HFEC PER RI 618607-14 STEP 4 W/ NO DEFECTS NOTED. COMPLIED WITH STEPS 5 & 6 PER RI 618607-14. ADDITIONAL INFORMATION: STEPS 1-3, 5-6 PERFORMSDR VNAA20250716016Doubler · corrodedCORROSION ON DOUBLER FS1000-1015 STGR 26R-25R AT AFT CARGO COMPARTMENT CORRECTIVE ACTION: EVALUATED, DUE TO EXCESIVE CORROSION ON DOUBLER, STIFFENER (2EAS), BRACKET AND STRINGER CLIP (4EAS) ON FS1000-1015 STGR 26R-25R AT AFT CARGO COMPARTMENT PER CRJ900 SRM 53SDR FDEA202406050914Skin · dentedNOSE FUSELAGE LOWER SKIN PANEL GOT A DENT BETWEEN FR4~5, 7 O'CLOCK POSITION. ACCOMPLISHED THE DOUBLER REPAIR AT NOSE FUSELAGE LOWER SKIN PANEL BETWEEN FR4~5, 7 O'CLOCK I.A.W A300-600 SRM 53-11-12-201, PARA 5A , PAGE 203-210 FIG 201, SRI 53-11-12-201, IIR 5SDR IPXA2024061514092Skin · mechanic errorR/H FUSELAGE FWD SIDE FROM WING TO BODY AT STA 751 AND STRINGER 21RH HAS A MISDRILL TO SKIN. ATA 53. ACCOMPLISHED EO-90721-REQ1 AND EA 757-5330-01-B0209 IR.SDR JJBA20240612032Skin · corrodedREAR FUSELAGE 1, FRAME 61 BTW STR 19L-18L, CORROSION SUSPECTED ON INNER SKIN SURFACE. CORROSION DAMAGE ON INNER SKIN SURFACE AT FR61 BTW STR 19L-18L REPAIRED.SDR JJBA20240611028Skin · damagedCENTER FUSELAGE 2, EXTERNAL SKIN, SEVERAL LIGHTNING STRIKE FOUND BTW FRAME 25-31 AND STR 21L-19L. PERFORMED REPAIRS ON CENTER FUSELAGE 2, EXTERNAL SKIN BTW FR 25 - FR 31 AND STR 21L-19LSDR AALA202406108635Skin · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT INTERNAL FUSELAGE SKIN FROM STA 927 TO STA 947, FROM S27L TO S27R. REPAIRED SKIN PER EA 352646.SDR DALA2024060705848Skin · corrodedAIRCRAFT 6814, DURING H CHECK MAINTENANCE VISIT, WHILE ACCOMPLISHING JOB CARD 2020-2443, THE STRINGER S-28L P/N 146N3110 179 BETWEEN STA 1555 AND STA 1565 WAS FOUND WITH TWO (2 EA) CORROSION SPOTS. THE LOCATION OF THE CORROSION SPOTS WAS IN THE DATUM OF AN EXTSDR KCSA202406051068Skin · damagedLOWER HALF OF FUSELAGE EXTERNAL SKIN HAS EVIDENCE OF LIGHTNING STRIKE RIGHT SIDE APPROX STA 160 AND S-42ASDR SIMA20240604008Skin · corrodedNRTC # E041386- FUSELAGE INTERNAL SKIN UNDER POTABLE WATER TANK SUPPORT STRUCTURE CORRODED BETWEEN FR 86/87 STGRS 29L/29R. (MAJOR REPAIR). PERFORMED PERMANENT REPAIR TO FUSELAGE INTERNAL SKIN UNDER POTABLE WATER TANK SUPPORT STRUCTURE BETWEEN FR 86/87 STGRS 2SDR CALA2024061701824Skin · damagedPERFORM A PERMANENT REPAIR AT LH FUS EXTERNAL SKIN AT STA 390, STRG 19L PER LP#4324692.(REF: AAR NR 100008644) SFR #1036381 1036524). PERFORMED A PERMANENT REPAIR AT L/H FUSELAGE EXTERNAL SKIN STA 390, STR 19L & INSTALLED IAW SRM 53-00-01-2R-1, IS A CATEGORY BSDR JJBA20240611029Skin · dentedFWD FUSELAGE, DENT FOUND 4.000 INCHES FWD FRAME 7 AND 14.000 INCHES STR 15L. REPAIR DOUBLER PERFORMED ON FWD FUSELAGE BTW FR 6-7 AND BELOW GPU ACCESS PANELSDR DALA2024060705847Skin · crackedAIRCRAFT 659, DURING HCK AT QRO, WHILE PERFORMING A HFEC INSPECTIONS AT 1L DOOR CUTOUT PER WC 5331-01232-02A, CRACKS WERE FOUND AFFECTING THE FUSELAGE SKIN & BEAR STRAP, BETWEEN STA 333.45 350.0, AND BETWEEN STRINGERS 6L AND 8L. CORRECTIVE ACTION: ELIMINATED
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