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 IXXA202110011601Skin · crackedFUSELAGE SSTA 1654 HAS CRACK IN THE SKIN BETWEEN STR 4L-5LSDR HALA2021110800199None · noneSHIP 393 DENT DAMAGE NEXT TO THE L2 DOOR DUE TO A TOWING IMPACT. THE DENT IS IN THE SKIN AT STR 28L/FR32. STRINGER 28L IS ALSO VISIBLY DISTORTED. IT IS LOCATED 2.2" FWD OF FR31, WHICH IS AT A BUTT SPLICE. THE DAMAGE IS BEYOND ALLOWED LIMITS. CORRECTIVE ACTION:SDR DALA2021110806863None · noneSHIP 3317 BULGE IN SKIN FROM FR21.5 TO FR23 BETWEEN STR 22R AND 23R. CORRECTIVE ACTION: REF AIB R53270227 FOR SKIN PANEL AND HINGE FITTING REPLACEMENT. (2010096)SDR DALA2021110806862None · noneSHIP 3317 WHILE PERFORMING HFEC OF AFT SIDE OF HINGE FITTINGS IN CABIN FOUND THE UPPER REINFORCEMENTS STRAP CRACKED ABOVE NBR 5 HINGE FITTING. CORRECTIVE ACTION: REF AIB REPAIR INSTRUCTION R53270227 FOR STRINGER REPAIR. (2010102)SDR DALA2021110806861None · noneSHIP 3317 SKIN PULLED INWARD AT FRAMES 20A - 24 BETWEEN STR 22R AND 24R. CORRECTIVE ACTION: REF AIB REPAIR INSTRUCTION R53270227 FOR SKIN PANEL AND HINGE FITTINGS REPLACEMENT. (2010083)SDR DALA2021110806860None · noneSHIP 3317 SKIN DAMAGED AT FRAME 23 ABOVE HINGE. APPROX DAMAGE 4.25 X 1.0. CORRECTIVE ACTION: REF AIB REPAIR INSTRUCTION R53270227 FOR SKIN PANEL REPLACEMENT. (2010004)SDR DALA2021110806859None · noneSHIP 3317 SKIN DAMAGED AT FRAME 22A ABOVE HINGE. APPROX DAMAGE 5.5 X 3.0. CORRECTIVE ACTION: REF AIB REPAIR INSTRUCTION R53270227 FOR SKIN PANEL REPLACEMENT. (2009999)SDR DALA2021110806858None · noneSHIP 3317 SKIN DAMAGED AT FRAME 22 ABOVE HINGE. APPROX DAMAGE 6.25 X 3.0. CORRECTIVE ACTION: REF AIB REPAIR INSTRUCTION R53270227 FOR SKIN PANEL REPLACEMENT. (2009997)SDR DALA2021110806857None · noneSHIP 3317 SKIN DAMAGED AT FRAME 21A ABOVE HINGE. APPROX DAMAGE 5.75X3.0. CORRECTIVE ACTION: REF AIB REPAIR INSTRUCTION R53270227 FOR SKIN PANEL REPLACEMENT. (2009986)SDR JR2R20211107184Skin · dentedFWD LH FUSELAGE HAS 2 DENTS NEAR RVSM AREASDR ASAA2021110636652Plate · corrodedAFT CARGO RIGHT HAND TRANSITION PNL HAS CORROSION FROM 727+4 TO 767. GROUNDED - YES. CORR FOUND TO BE OUT OF LIMITS CUTOUT DAMAGED SECTION & REPAIRED TRANSITION PNL IAW B737-800 SRM 53-00-503-2R-5W = 2 O = .040 R = 0 L = 6 D = .040.SDR ASAA2021110636648Plate · corrodedAFT CARGO LH TRANSITION PNL HAS MULIPLE SPOTS OF CORROSION FROM 727G TO 727J. GROUNDED - YES. REPAIRED AFT CARGO LH TRANSITION PNL FROM STA 727G TO 727J IAW B737-800 SRM 53-00-53-2R-5.SDR DALA2021110606828None · noneCORROSION ON EXTERNAL FUSELAGE SKIN BTW STA 626 TO STA 690 AND BTW L-28L TO L-28R. SUMMARY OF NRC 00199: CORROSION LEVEL 2: AFTER BLENDING FOUND DAMGE TO BE OUT OF LIMITS. PERMANENT REPAIR WAS PERFORMED ON EXTERNAL FUSELAGE SKIN BTW STA 626 TO STA 690 AND BTW SDR DALA2021111006922None · noneDTE TRACKING FOR ER/A 595293-14 REVISION ORIGINAL. REPAIR APPROVAL IS LIMITED TO 12 MONTHS SERVICE FROM ER/A 595293 -14 REV ORIGINAL SECTION I ACCOMPLISHMENT. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LISDR DALA2021111006921None · noneAMOC TRACKING FOR ER/A 595293-14 REV ORIGINAL. REPAIR APPROVAL IS LIMITED TO 3,100 FLIGHT CYCLES OR 6,300 FLIGHT HOURS WHICHEVER OCCURS FIRST FROM SECTION I OF ER/A 595293-14 REV ORIGINAL ACCOMPLISHMENT. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS SDR DALA2021110806877None · noneSHIP 1811 EMEO TASK - HFEC INSPECTION FOUND 01EA CRACK APPROX. 2MM IN LENGTH ON THE LH FUSELAGE SKIN. CORRECTIIVE ACTION: CUT AND REMOVED, MADE THE REPAIR DOUBLER FROM 7075-T6-0.063" CLAD AND INSTALLED PER B767-400 SRM 53-80 (2007479)SDR JR2R20211105264Rib · crackedLH WHEEL WELL FRAME 52 CRACKEDSDR SWAA2021122040689Bracket · crackedFWD CARGO SIDEWALL, BS 500D S19R HAS ONE GUSSET CRACKED. REMOVED GUSSET IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED GUSSET IAW SRM 51-20-01-0G-0. TREATED AND PRIMED GUSSET IAW SRM 51-20-01-0G-0. LOCATED AND DRILLED GUSSET IAW SRM 51-40-05-0G-0. INSTALLED THSDR DALA2021110906917None · noneLIGHTNING STRIKE DAMAGE BETWEEN FR1 + FR2, RT OF CENTER APPROX. 5" REPAIR REF A321 SRM 53-11-11. REMOVED DAMAGE BY DRILLING A 0.159" HOLE. INSTALLED BLIND FASTENER REF A321 SRM 53-11-11. RESTORED FINISH REF PS 900-3-6 NO 3 FWD MONITOR LOG PERMANENT REPAIR REQ SDR DALA2021110506815Web · cracked(LOG 2006296) DURING INSPECTION FOUND CRACK ON WEB BTW STA 663.75 AND RBL 45.57 TO RBL 64. CRACK ON WEB BTW STA 663.75 AND RBL 45.57 TO RBL 64 WAS REPAIRED PER B737-800 SRM 51-70-12-2R REP. 1.SDR MK1Y11042021004Skin · unknownFOUND EXISTING RIVET REPAIR AND BLEND OUTS ON FUSELAGE EXTERNAL SKIN STA 1351 TO STA 1373 STR 28LSDR MK1Y11042021003Skin · unknownFOUND BLEND OUTS ON FUSELAGE EXTERNAL SKIN STA 1417 STR 27L TO STR 33LSDR MK1Y11042021002Skin · unknownFOUND BLEND OUTS ON FUSELAGE EXTERNAL SKIN STA 456 TO STA 500 STR 29R TO STR 34RSDR MK1Y11042021001None · noneFOUND BLEND OUTS ON FUSELAGE EXTERNAL SKIN STA368 TO STA 398 STR TO STR 35LSDR 2021FA0000004Panel · damagedCABIN FLOOR PANEL IS DAMAGED.SDR DALA2021110406798None · noneSHIP 1703 HFEC INSPECTION FOUND 02 EA CRACKS (FWD:0.315" AND AFT0.250") ON THE LH FUSELAGE SKIN BELOW THE NO.8 AND NO.9 STRINGER-ATTACH RIVENTS. CORRECTIVE ACTION: 02 EA CRACKS(FWD: 0.315" AND AFT 0.250") DOUBLER REPAIR AS PER B767-300 SRM 53-80 (2005165)SDR IPXA2021110875760Floor Panel · damagedINSPECTION TYPE:SEGPNL 242XMF DAMAGEDFABBED PNL PER SREO B757-5320-9692-KSDR IPXA2021110875759Floor Panel · damagedINSPECTION TYPE:SEGPNL 242XAF DAMAGEDFABBED PNL PER SREO B757-5320-9692-KSDR IPXA2021110875757Floor Panel · damagedINSPECTION TYPE:SEGPNL 242XBF DAMAGEDFABBED PNL PER SREO B757-5320-9692-KSDR IPXA2021110875755Floor Panel · damagedINSPECTION TYPE:SEGPNL 242XJF DAMAGEDFABBED PNL PER SREO B757-5320-9692-KSDR IPXA2021110875754Floor Panel · damagedINSPECTION TYPE:SEGPNL 242XHF DAMAGEDFABBED PNL PER SREO B757-5320-9692-KSDR DALA2021110606822None · noneSHIP 6823 CORROSION ON INTERNAL DOUBLER OF ANTENNA-VHF COMM R, BETWEEN S29R- AND S30 AND BS 1460-1480, AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00361; INTERNAL DOUBLER OF ANTENNA-VHF COMM R, BETWEEN S29R- AND S30 AND BS 1460-1480, AFT CARGO COMSDR SWAA2021110539300Skin · crackedFUSELAGE SKIN SUBSURFACE CRACK INDICATIONS AT BS 500D+8 TO 500D+11 ABOVE STR4L USING 737 NDT PART 6;53-30-25. CONFIRMED SUBSURFACE CRACK INDICATION USING OPTION 1&4 OF TTG8Q005VW3 ; FSELAGE SKIN SSRFACE CRACK INDICATIONS AT BS 500D+8 TO 500D+11 AOVE STR4L SINGSDR UIEA2021110202327None · noneFUSELAGE SKIN CORROSION AT STA. 1720 AND STRINGER 42 RIGHT(<P ><SPAN>AREA OF CORROSION WAS CUT OUT, NO CORROSION WAS FOUND ON THE STRINGER. HFEC WAS ACCOMPLISHED AROUND CUT OUT AND EXISTING HOLES WITH NO FINDINGS. ORIGINAL SKIN WAS 2024-T3 .080". DOUBLER WASDR 2021F00307Skin · gouged8100-9 SR-680A-ATA53-22175: NDI REQUIRED FOR GOUGE IN BELLY SKIN FROM TRANSFER VALVE.SDR FDEA202111012717Bracket · crackedAPU SUPPORT BRACKET @ BS1787.45 IS CRACKED. REMOVED PNEUMATIC DUCT, REMOVED SUPPORT BRACKET. FABRICATED NEW 212N3047-5 BRACKET, INSTALLED NEW BRACKET, REINSTALLED PNEUMATIC DUCT AND ACCOMPLISHED LEAK CHECK. LEAK CHECK WAS GOOD, PER BAC DWG 212N3047 REV SDR SWAA2021122038665Bear Strap · corrodedTYPICAL CRACK FOUND EMANATING FROM FASTENER OPPOSITE FITTING LATCH AT R1 DOOR BEAR STRAP BETWEEN STA.291.5 AND STA.294.5 BETWEEN S-8R AND S-9R. APPROXIMATE LENGTH OF CRACK : 1.457' ; TYPICAL CRACK FOND EMANATING FROM FASTENER OPPOSITE FITTING LATCH AT R1 DOOR SDR SWAA2021112938706Skin · corrodedCUSTOMER REQUEST CORROSION ON AFT EXTERNAL SKIN BS1016 AND BTW STR 23L TO STR 25L LOWER FUSELAGE ; 2021-496476 / [01] TOOL USED ULTRASONIC EQUIPMENT PN: 25DLPLUS; SN: 071504410; DUE DATE: 20-NOV-21; [02] OPEN FAULT HAS AN ERROR AND IS BEING CORRECTED BY RAISINSDR SWAA2021112938703Doubler · crackedCRACK ON SURROUND DOUBLER LOWER POSITION BTW BS277 TO BS235 ELECTRICAL GROUND POWER RECEPTACLE LOWER FUSELAGE. PERFORMED PERMANENT REPAIR AT SURROUND DOUBLER OF EPGR LOWER POSITION BTW BS277 TO BS235, WL 175 IAW SRM 53-10-15-2R-4 REPAIR 4 FIGURE 204 SHEETS 3SDR REXA2021111600965Seat Track · corrodedAFT CARGO BAY SEAT TRACK AT LBL 27 BEGINNING AT APPROX FS 985.00 CORRODED. - REMOVED FABRICATED AND INSTALLED SEAT TRACK @ LBL27 FS 926-988 IAW CRJ 900 SRM 53-51-49-101-001-A02, 53-00-49-201-002-A01 & AMM 53-00-49-000/400-801-A07.SDR DALA2021110106702None · none(LOG 1999629) DURING INSPECTION FOUND CORROSION ON INTERNAL DOUBLES BTW STA 727G TO 727H AND BTW S-2L TO S-2R. CONNECTOR BTW STA 727G TO 727H AND BTW S-2L TO S-2R (3 EA) WERE FABRICATED AND REPLACED PER DWG. AR230-0134-00 REV ORIGINAL AND DWG. AR230-0136-00 RESDR SWAA2021112338119None · crackedCRACK BILGE AREA SUPPORT ZEE LOCATED BTW BS 500 TO BS 500A AND S-26L AT FWD CARGO COMPARTMENT ; 2021-461085 / [01] TOOL USED:DIGITAL CALIPER P/N:500-197-30;S/N:A18135101;DUE DATE:06/AUG/22.; [02] REPLACED SUPPORT ZEE LOCATED BTW BS 480+10 INCH TO BS 500D S-26LSDR DALA2021110206754None · noneA220-100 / FUSELAGE / NOSE FWD FUSELAGE / BL5.76R FWD OF FR10 / DENT. REPAIR APPROVAL IS LIMITED TO 30,000FC/52,500FH, (WHICHEVER OCCURS FIRST) FROM SECTION I REPAIR. ADDITIONAL ENGINEERING AUTHORIZATION IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. NOTSDR DALA2021110106722None · noneAFTER GEAR SWING, FOUND DENTS AROUND TAIL JACK PAD BETWEEN FR73 AND AND FR74. REPAIRED FUSELAGE SKIN DAMAGE PER ERA 595061-14 REV ORIG ASSOCIATED ER/A 14-595061 ADDED FOR AC 3030. (LP# 1999523)SDR FDEA202110282650Skin · corrodedEMPENNAGE INTERIOR BILGE AREA BOTTOM SKINUPPER SURFACE HAS CORROSION BETWEEN BS1848 AND LBL10 TO LBL16 REPAIRED PER EA # F-5330-T0364985-P1SDR DALA2021102906693Unknown · unknownSHIP 3311 EVIDENCE OF LIGHTNING STRIKE STR 39R APPROX. 11.5 INCHES AFT OF FR 31. CORRECTIVE ACTION: REMOVED DAMAGED FASTENER. ENLARGED HOLE SIZE UP TO NEXT RIVET SIZE REF A330 SRM 53-00. BHEC INSPECTED WITH NO ITEMS NOTED. INSTALLED TEMP REPAIR FASTENER PER A3SDR SWAA2021110137656Doubler · corrodedBS 1042, 311AL ACCESS DOOR CUTOUT DOUBLER CORRODED, 2 INCHES BELOW STR 20L. CORROSION REMOVED IAW SRM 51-10-02. NO CRACKS NOTED UT MEASURED MATERIAL IAW NDT P4 51-00-00 P2 IAW EA #21-153-03210 WIP 1, REV A. LOCATED AND DRILLED IAW EA 21-153-03210 WIP 1,SDR SWAA2021110137658Skin · corrodedFUSELAGE LOWER SKIN INTERGRANULAR CORROSION NOTED AT STA. 1042 AND 2' BELOW STR 20L AT FWD UPPER CORNER OF 311AL ACCESS DOOR CUTOUT. ALL WORK FOR THIS REPAIR ACCOMPLISHED ON TTG8Q00712D9 REF EA 21-153-3210 INSPECTION VERIFIED. AUDIT CWSDR FDEA202110272644None · noneFOUND LIGHTING STRIKE DAMAGE TO SKIN 1.5" AFT OF STA 520 2.75" IB OF STR S29L WRITTEN ON WRI 53-00-6918 WORKED ON SEQ 5 UNDER W/O 81650 CARD WRITTEN FOR RDR/SDR. REPAIRED LIGHTING STRIKE DAMAGE TO SKIN 1.5" AFT OF STA 520 2.75" I/B OF STR S29L REF 757 SRM 5SDR FDEA202110272643None · noneFOUND LIGHTING STRIKE DAMAGE ON SECTION 43, ON STA 580, 4.5" IB OF STR 29R DAMAGE WRITTEN UP ON WRI 53-00-6925 REPAIR WORKED ON SEQ 6 W/O 81650. CARD WRITTEN FOR RDR/SRD REPAIRED LIGHTING STRIKE DAMAGE ON SECTION 43 ON STA 580 4.5" I/B OF STR 29R REF 757 SRM
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