JASC 5300
Service difficulty reports · 8,206
Reports filed under 5300 · Fuselage Structure (General), 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 = '5300' 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 = '5300' 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 EVCA030123Drive Shaft · crackedCRACK FOUND APPROX. 4.8 INCHES ON FORWARD TAIL ROTOR DRIVESHAFT COWLING ON LH SIDE, FRONT OF HEAT SHIELD.SDR DALA2023042403197Unknown · unknownSHIP 3302 EVIDENCE OF LIGHTNING STRIKE FR 14C STR 39. L/H. CORRECTIVE ACTION: REMOVED DAMAGED FASTENER AT 10A. CONTACTED MCC TO CHANGE LOG TO FR 14A SRT 39LH. PERFORMED BHEC INSP. NO CRACKS FOUND. HOLE AT 14A IS 3/16 DIA, ACCOMPLISHED COLD EXPAND PER A330 SRM SDR DALA2023042403196Unknown · unknownSHIP 3302 EVIDENCE OF LIGHTNING STRIKE FR 14B STR 39. L/H. CORRECTIVE ACTION: REMOVED DAMAGED FASTENER AT 10A REF A330 SRM 51-42-11. CONTACTED MCC TO CHANGE LOG TO FR 14 SRT 39LH. PERFORMED BHEC PER NTM 51-10-01. NO CRACKS FOUND. FR 14 IS 0.1895, ACCOMPLISHED SDR DALA2023042403195Unknown · unknownSHIP 3302 EVIDENCE OF LIGHTNING STRIKE 6" FWD OF L2 BOARDING DOOR. CORRECTIVE ACTION: REMOVED FASTENER. REQUIRES ROTATING PROBE TESTING. COMPLETED BHEC HFEC. NO DEFECTS NOTED. COLD WORKED COMPLETED. INSTALLED FASTERNER PER A330 SRM 53-21-11. (2649308)SDR DALA2023042403194Unknown · unknownSHIP 3302 EVIDENCE OF LIGHTNING STRIKE FR12 STR 31. L/H. CORRECTIVE ACTION: REMOVED DAMAGED FASTENER REF A330 SRM 51-42-11. CONTACTED MCC TO CORRECT LOG TO FR12 STR 39LH. PERFORMED BHEC INSP. NO CRACKS FOUND. ACCOMPLISHED COLD WORK PER A330 SRM 53-11-11. FASTESDR DALA2023042403193Unknown · unknownSHIP 3302 EVIDENCE OF LIGHTNING STRIKE FR 10 @ STR 39. L/H. CORRECTIVE ACTION: REMOVED DAMAGED FASTENER AT 10A. PERFORMED BHEC INSP. NO CRACKS FOUND. HOLE 10A IS 0.1895, ACCOMPLISHED COLD EXPAND PER A330 SRM 53-11-11. FASTENER WAS INSTALLED PER A330 SRM 53-11-SDR SCNA20230404117Unknown · corrodedDEFECT NR00193: L-1 DOOR MOP SILL HAS EVIDENCE OF SUSPECTED CORROSION AT FASTENER HOLE BETWEEN STA 270 AND 344 WL 208.1. (MARKED) - - - RESOLUTION: REPAIRED L-1 DOOR MOP SILL (INNER CORD) PER ATS ER 23-01284 REV 1R AND SCA ENG-53SCA-1114 REV 00. REPAIR IS SDR SWIA20230228Unknown · corroded* SHORT SECTION OF SEAT TRACK AT RBL 9 BETWEEN APPROX 559.00 + 112 AND FS 574.00 CORRODED. (C-CHECK RO 3/23/2023) REMOVED AND REPLACED WITH NEW SEAT TRACK AT RBL 9 BETWEEN APPROX 559.00 + 112 AND FS 574.00 REF CRJ200 AMM 53-01-11-400-802. SEE CONTINUATSDR V0XD20230320002Beam · corrodedCORROSION ON UPPER SURFACE OF HAT BEAM AT Y + 479 BETWEEN FR 59- FR 61. CORRECTIVE ACTION: CUT OUT DAMAGE ON HAT BEAM AROUND NUTPLATE ON R/H SIDE BTWN. FR 59-61 ( 2 LOCATIONS ) . FABRICATED 2 REPAIR DOUBLERS P/N: 2024-T3 .040. LOCATED DRILLED AND INSTALLED 2 NSDR R61A2023031500188Seat Track · corrodedLEVEL 2 CORROSION WAS FOUND ON LH INBD CABIN SEAT TRACK BETWEEN FR 23 AND FR 34. TRACK WAS REPLACED IAW SRM 51-41-02.SDR A6WA202302288490Floorbeam · corrodedOUTBOARD PORTION OF SEAT RAIL SUPPORT BEAM IS CORRODED AT BL 27 BETWEEN FS559+80 - FS621 **********AIRCRAFT REMOVED FROM SERVICE********* REMOVED CORROSION FROM O/B SEAT RAIL SUPPORT BEAM LBL27 BETWEEN FS559.00+80 TO FS621.00 PER CRJ 200 SRM 51-21-06. FOUND RESDR 21GA20230228005Skin · crackedDURING MAINTENANCE FOUND CRACK ON SKIN AT RH FUSELAGE FWD UPPER FASTENER AT STA. 1809 AT STR 12A.SDR UIEA2023022100156None · noneAPU COMPT TAIL CONE INTERNAL LH FS 2753 WL 359 SUPPORT FRAME CRACK.(<P>FRAME CRACK AREA REPAIRED AS PER RI NO. RI-53-80-16075 REV.A</P>)SDR UIEA2023022100155None · noneAPU FIREWALL STA 2658 FWD FACE #2 STIFFENER (COUNT FROM BOTTOM) FOUND L/H O/B END CRACKED.(<P>CRACK AREA REPAIRED AS PER RI NO. RI-53-83-16077 REV.A</P>)SDR UIEA2023022100152None · noneAPU FIREWALL AT STA 2658 FWD FACE #2 STIFFENER (COUNT FROM BOTTOM) FOUND END CRACKED.(<P>CRACK AREA REPAIRED AS PER RI NO. RI-53-83-16077 REV.A</P>)SDR UIEA2023022000141None · noneFX SECTION 48 FROM STA 2747 TO 2753 AND BETWEEN WL 357 AND WL 361 FOUND SKIN CRACK.(<P>SKIN CRACK AREA REPAIRED AS PER <SPAN>RI NO. RI-53-80-16075 REV.A</SPAN></P>)SDR UIEA2023022000140None · noneFX FUSELAGE LOWER SKIN STA 2120-2140 STR 44R-45R FOUND 1EA LIGHTNING STRIKE.(<P>SKIN LIGHTNING STRIKE AREA REPAIRED AS PER SRM 53-00-01-2R-9 REPAIR 9.</P>)SDR UIEA2023022000139None · noneLH BS720 1EA CRACK WAS FOUND ON THE FWD CHANNEL OF THE UPPER DECK TENSION TIE APPROX 1/2" IN LENGTH AT RADIUS AREA.(<P>CHANNEL REPAIRED AS PER SRM 53-20-30-2R-1 REPAIR 1. THIS REPAIR WAS CATEGORY B.</P>)SDR UIEA2023021700132None · noneEMP - APU COMPT RH FRAME AT STA 2664 WL 305 FOUND CRACKED.(<P>CRACK AREA REPAIRED AS PER SRM 53-80-07-2R-1 REPAIR 1.</P>)SDR UIEA2023021600125None · noneFX LH BODY FAIRING #191KL INTERCOSTAL AT STA 1240 UPPER AND LOWER FLANGE FOUND CRACK.(<P>INTERCOSTAL UPPER AND LOWER FLANGE REPAIRED AS PER RI NO. RI-53-40-16059 REV.A</P>)SDR UIEA2023021600124None · noneFX RH BODY FAIRING #192KR INTERCOSTAL AT STA 1240 UPPER AND LOWER FLANGE FOUND CRACK.(<P>UPPER & LOWER FLANGE REPAIRED AS PER RI NO. RI-53-40-16060 REV.A</P>)SDR CALA2023030100588None · corrodedBULK CGO COMPT BILGE STA 1540 S38L -S39L SHEAR TIE FOUND CORROSION TRANSFER REF. NON-ROUTINE HX NRC WO.1469539 AND ORIGINATED BY EMP NO. V896810 BULK CARGO COMPT BILGE STA 1540 BETWEEN STR 38L AND STR 39 SHEAR TIE REPLACED AS PER SRM 51-10-02. ATTACHED FORM 44SDR CALA2023030100578Tray · noneAFT CABIN WET AREA RH FR68-FR69 O/B TRAY FASTENER HOLES ELONGATE D PER HAECO LCQ N/R 9290816/22816 GENERATED BY V061629. FABRICATED TRAY AT AFT CABIN WET AREA R/H FR68-69 O/B IAW A319 D RAWING 18D53480019 & REMOVED & REPLACED OLD TRAY IAW A319 SRM 51 -72-11-91SDR CALA2023030100574Window · crackedTHIS NR GENERATED FOR ESFR REPORTING ONLY L/H NO 1 WINDOW FRAME HAS CRACK EA 5310-04554 REV B.SDR IPXA2023032392188Skin · gougedINSPECTION TYPE:3CTAIL CONE INSIDE COMP. R/H UPPER FWD EDGE SKIN HAS A GOUGED,REPAIRED R/H UPPER FWD EDGE SKIN AT THE TAIL CONE STA 2165 IAW UPS EO MD11-5350-66790-B (MINOR)SDR IPXA2023032192101Beam · dentedINSPECTION TYPE:3CTAIL CONE COMP UPPER FWD SRTUCTRE BEAM HAS A DENT AT BOTTOM SIDE.REPLACED BEAM AT THE UPPER FWD SIDE ON TAIL CONE COMP. IAW SRM 51-31-01.(MINOR)SDR IPXA2023032192099Shear Tie · crackedINSPECTION TYPE:3C*MAJOR REPAIR* MAIN CABIN CEILING AREA HAS A SHEAR TIE THAT IS CRACKED AT LONGERON 4R AND STA 1902REPAIRED CRACKED SHEAR CHIP AT THE MAIN CABIN CEILING AREA AT LONGERON 4R AND STA 1902 IAW 53-00-06 REPAIR 1 FIG 202 REV 69.01 (MAJOR)SDR IPXA2023031491838Longeron Splice · crackedINSPECTION TYPE:3CMAIN CABIN CEILING HAS A SPLICE THAT IS CRACKED BETWEEEN STA 1521 AND 5-11 AT LONGERON 4L .REPLACED CRACKED SPLICE AT MAIN CABIN CEINLING BEWTEEN STA 1521 AND 5-11 AT LONGERON 4L IAW SRM 53-00-05 (MINOR)SDR JJBA20230306008None · noneCF3, LH OMEGA BEAM #5 CRACKS SUSPECTED FOUND BTW FRAME 41 AND 42 ON FLOOR STRUCTURE. CF3, LH OMEGA BEAM #5 HAS CRACKS SUSPECTED FOUND AT FRAME 41 AND 42 ON FLOOR STRUCTURE. 1 CRACK FOUND AT FR41. BEAM REPAIRED WITH A DOUBLERSDR JJBA20230306007None · noneCF3, LH OMEGA BEAM #6 CRACK SUSPECTED FOUND AT FRAME 51 ON FLOOR STRUCTURE. CF3, LH OMEGA BEAM #6 CRACK FOUND AT FRAME 51 ON FLOOR STRUCTURE. BEAM REPAIRED WITH A DOUBLER.SDR JJBA20230306005None · noneCF2, CORROSION AND (3X) SUSPECTED CRACKS FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BETWEEN FR 24-30. CF2, CORROSION (LEVEL 1) AND 3 CRACKS FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 24-30. BEAM IS REPAIRED WITH 3 DOUBLERSSDR CALA2023030100573Support · crackedLH E&E COMPARTMENT FR 11 WEB SUPPORT CRACKED PER HAECO LCQ N/R 9 290215/22215 GENERATED BY V798788 REMOVED/REPLACED WEB @ FR11 L/H IAW A-319 SRM TASK 51-42-11/001. SRM TASK 51-44-11/001 AND SRM 51-21-11/001 PER MECH V929087 INS P V061757.SDR 2A6R2023022766002Frame · chafedDURING 1000 HOUR INSPECTION FOUND A CHAFE ON FRAME 4 INNER SKIN. PERFORMING A REPAIR PER AIRBUS RDAS-EC135-53-2023-0534ASDR 2A6R2023022766001None · corrodedDURING 1000 HOUR INSPECTION, FOUND THE RIGHT COCKPIT FLOOR CORRODED AROUND THE FWD GROUNDING POINT. PERFORMING A REPAIR AS PER AIRBUS HELICOPTERS RDAS-EC135-53-2023-0540ASDR V0XD20230227001Seat Track · corrodedLH FLOOR SEAT TRACK HAS MULTIPLE SIGNS OF CORROSION AT FR 18 TO FR 24. CORRECTIVE ACTION: REMOVED AND REPLACED LH FLOOR SEAT TRACK AT FR 18 TO FR 24 IAW EMB 135/145AMM 53-01-06.SDR JJBA20230309013None · noneCORROSION ON REAR FUSE 2 LOWER SKIN, BTW FR 80-81 AND BTW STR 19L-21L. CORROSION ON REAR FUSE 2 LOWER SKIN BTW FR 80-81 AND BTW STR 19L-21L. SKIN IS REPAIRED WITH A DOUBLER.SDR JJBA20230309011None · noneAT REAR FUSE 1 EXT, RADIO ALT ANTENNA NO 2 AFT LOWER DOUBLER CORRODED ON BELLY SKIN BTW FR 68-69. AT REAR FUSE 1 EXT, RADIO ALT ANTENNA NO 2 AFT LOWER DOUBLER CORRODED ON BELLY SKIN BTW FR 68-69, SKIN REPAIRED WITH A DOUBLERSDR JJBA20230309009None · noneCORROSION FOUND ON L GUSSET IN TOILET AREA BTW FR 59-61. CF4, CORROSION FOUND ON LH GUSSET IN TOILET AREA BTW FR 59-61. AFTER INVESTIGATION, CORROSION FOUND ON OMEGA BEAM AT FR 59 & 61. BEAM REPAIRED WITH 2 DOUBLERSSDR JJBA20230306006None · noneCF2, CORROSION AND (3X) SUSPECTED CRACKS FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BETWEEN FR 29-36. CF2, CORROSION (LEVEL 1) AND 3 CRACKS FOUND ON LH OMEGA BEAM #2 FLOOR STRUCTURE BTW FR 29-36. BEAM IS REPAIRED WITH 3 DOUBLERSSDR EE4Y2023022417277Fitting · crackedDURING THE ACCOMPLISHMENT OF ALLEGIANT EO E5316-002 RELATED TO AD 2022-02-11 PARAGRAPH G AND SB53-1330, IT WAS FOUND THE FWD SERVICE DOOR AND FWD ENTRY DOOR WITH CRACK INDICATION AT FR16 R/H DOOR STOP FITTING #7 WITH CRACK INDICATION.
DUE TO THERE IS NOT SRSDR EE4Y2023022417278Fitting · crackedDURING THE ACCOMPLISHMENT OF ALLEGIANT EO E5316-002 RELATED TO AD 2022-02-11 PARAGRAPH G AND SB53-1330, IT WAS FOUND THE FWD SERVICE DOOR AND FWD ENTRY DOOR WITH CRACK INDICATION AT FR20 R/H DOOR STOP FITTING #1 AND WEB AREA WITH CRACK INDICATION.
DUE TO THSDR EE4Y2023022417279Frame · crackedDURING THE ACCOMPLISHMENT OF ALLEGIANT EO E5316-002 RELATED TO AD 2022-02-11 PARAGRAPH G AND SB53-1330, IT WAS FOUND THE FWD SERVICE DOOR AND FWD ENTRY DOOR WITH CRACK INDICATION AT FR20 L/H DOOR STOP FITTING #1 AREA WITH CRACK INDICATION.
DUE TO THERE IS NSDR IPXA2023032392186Longeron · corrodedINSPECTION TYPE:3C*MAJOR REPAIR* CENTER CARGO BILGE AREA STA 1821 HAS CORROSION LONGERON 46R.REPARIED CORRODED LONGERON 46R AT THE CTR CARGO BILGE AREA STA 1821 IAW VTSAA 011-5310-01-A9839 I/R, UPS EO MD11-5310-86260-A DATED 03/20/23 AND FAA FORM 8100-9 SIGNEDSDR R61A2023031500192Seat Track · corrodedCF3 CORROSION FOUND ON LH IB SEAT TRACK BTWN FR 74-84. RERPLACED SEAT TRACK IAW SRM 51-43-03, 51-43-04SDR R61A2023031500187Seat Track · corrodedCENTER FUSELAGE III, CORROSIONS FOUND ON R/H I/B SEAT TRACK BETWEEN FR 74 - 84. CENTER FUSELAGE III, R/H I/B SEAT TRACK BETWEEN FR 74 - FR 84 REPLACED WITH NEW AND INSTALLED IAW SRM 51-41-01, SRM 51-43-03, AND SRM 51-43-04.SDR A6WA202302258487Intercostal · crackedATTACHING CLIP CRACKED ON 3RD INTERCOSTAL ON R/H AFT SIDE OF AFT PRESSURE BULKHEAD. *********AIRCRAFT REMOVED FROM SERVICE********* INSTALLED NEW ATTACH CLIP (PN: 601-35012-54) IAW CRJ200 SRM 51-42-21SDR A6WA202302258491Coaming · dentedAFT CARGO DOOR SURROUND COAMING IS DENTED/MISSING MATERIAL IN MULTIPLE LOCATIONS *******AIRCRAFT REMOVED FROM SERVICE********* REMOVED AND REPLACED AFT CARGO DOOR SURROUND COAMING REF CRJ200 SRM 51-41-02 AND SRM 51-42-10.SDR JJBA20230315021Unknown · unknownRF1, LH FR68 REINFORCEMENT BRACKET CARGO DOOR HOLDER FOUND CRACKED. AFTER INVESTIGATION, A CRACK IS FOUND ON Z FRAME. Z FRAME SPLICEDSDR SWAA2023031309687Angle · corrodedREJECT: FAULT TTG8Q00HGSR7 (AFT CARGO DOOR SILL PLATE HAS SEVERAL AREAS OF CORROSION) REQUIRES INSPECTION BUYBACK.<[01] FAULT TTG8Q00HGSR7 HAD NO INSPECTION BUY BACK. NEW FAULT RAISED ON TTG8Q00HJ4X0 FOR INSPECTION AND MEASUREMENTS ARE FROM THAT FAULT.;[02] LISDR JJBA20230309010None · noneCRACKS SUSPECTED (14X) ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. CRACKS SUSPECTED ON LH SKIN AROUND FASTENERS BTW FR 77-80 BTW STR 3L-9L. AFTER NDT INSPECTION, 4 CRACKS FOUND. INSTALLED REPAIR DOUBLER AT FR 78 AND BTW STR 5L-7L.
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