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 GTIA2023020136955Seat Track · corrodedCORROSION FOUND ON SEAT TRACK -Y1292 RH BTW FR41- FR7 IN CABIN. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y1292 LOCATED BETWEEN FRAME 41 TO FRAME 47 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IAW EA # 53-0636-22 AND EC NO. EO 5331-2270. REPAIR CSDR GTIA2023020136954Seat Track · corrodedCORROSION FOUND ON SEAT TRACK -Y765 RH BTW FR41- FR47 IN CABIN. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y765 LOCATED BETWEEN FRAME 41 TO FRAME 47 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IAW EA # 53-0636-22 AND EC NO. EO 5331-2270. REPAIR CASDR GTIA2023020136953Seat Track · corrodedCORROSION FOUND ON SEAT TRACK Y765 LH FR41- FR47. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y765 LOCATED BETWEEN FRAME 41 TO FRAME 47 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IAW EA # 53-0636-22 AND EC NO. EO 5331-2270.. REPAIR CATEGORY "A" INSDR GTIA2023020136952Seat Track · corrodedCORROSION FOUND ON SEAT TRACK Y1292 LH FR41-FR47. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y1292 LOCATED BETWEEN FRAME 41 TO FRAME 47 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IAW EA # 53-0636-22 AND EC NO. EO 5331-2270.. REPAIR CATEGORY "A" ISDR GTIA2023020136951Seat Track · corrodedCORROSION FOUND ON SEAT TRACK Y765 LH BTW FR36-41. RAF CREATED-PERFORMED PERMANENT REPAIR ON SEAT TRACK Y765 LOCATED BETWEEN FRAME 36 TO FRAME 41 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IN ACORDANCE WITH EA # 53-0636-22 AND EC. NO EO 5331-2270. REPAIR SDR GTIA2023020136950Seat Track · corrodedCORROSION FOUND ON SEAT TRACK Y1292 LH FR36-41. RAF CREATED-PERFORMED PERMANENT REPAIR ON TO FRAME TRACK Y1292 LOCATED BETWEEN FRAME 36 TO FRAME 41 AND AT LEVEL OF STRINGER 23 IN PASSENGER CABIN IN ACCORDANCE WITH EA #53-0636-22 AND EC. NO. EO 5331-2270. REPAISDR IPXA2023021090850Skin · crackedINSPECTION TYPE:C14*MAJOR REPAIR* CRACK WAS FOUND ON RH SKIN(P/N:148T3121-2)AT STA 1725.5,S-7R.REPAIR I.A.W 767-300F SRM 53-80-01 REPAIR 5,DETAIL III,REV.85.01SDR CALA2023021000393Frame · corrodedCORROSION FOUND AT STA 300 APPROX S-8L ABOVE DOOR SILL DRAIN DIAPHRAM.(UNDER BLANKET411A4901-1349 TO "ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5310-08113 ON OR BEFORE FEBRUARY 6, 2025. PERFORMED PART 1 INTERIM REPAIR PER ECRA 5310-08113. REFERENCE BAM SDR CALA2023021000375Panel · unknownDURING ACOMPLISHMENT OF EC/RA 5350-02474 THE LH STA 955 PRESSURE DECK STIFFENER HAS EXISTING REPAIR INTERFERENCE -INTERIM REPAIR / DEVIATION REQUIRED. CYCLES (TOTAL AIRCRAFT FLIGHT CYCLES 42,251) AND AT A REPETITIVE L INTERNAL (FROM TOP) AND EXTERNAL (FROM WHSDR CALA2023021000403Frame · corrodedR1 DOOR FR16 STGR 22R-STGR 23R CORRODED PER HAECO LCQ N/R 929651 4/40514 GEN BY V061629 "ACCOMPLISH A PERMANENT REPAIR ON THE FRAME AT RH FR16 AFT OF ECRA 5310-08111 ON OR BEFORE JANUARY 27, 2024" WEB FACE AT Z-520 FLOOR LEVEL PER PART 3 OF THE LATEST REVISIONSDR CALA2023021000400Frame · crackedUPPER CABIN INTERIOR FRAME IS CRACKED AT STA 620 STRINGER 8R. CUTOUT AND REPAIRED FUSELAGE FRAME @ STA 620 STRINGER 8R AND 9R AT A/C BRACKET LOCATION PER B757 SRM 53-00-07-2R REPAIR 8.SDR CALA2023021000399Unknown · corrodedUPPER CABIN FLOOR SUPPORT STRUCTURE STA 440 LBL 60 IS CORRODED. UPPER CABIN FLOOR SUPPORT PN-140N0504U3 AT STA 440 LBL 60 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED NEW SUPPORT IAW B757 SRM 51-40-02 PARA 7 AND EC/RA 5300-02911.SDR CALA2023021000398Skin · bulgedTHE EXTERIOR FUSELAGE SKIN IS BULGED AROUND THE RIVETS AT THE FWD I/B CORNER OF THE AFT LAVATORY SERVICE PANEL, COMMON TO STR.29R. REPAIRED AREA IAW AMES DOCUMENT 47539REA02 AND UNITED EC/RA #5330-07040. SEE PARTIAL WORK ACCOMPLISHED FOR WORK COMPLETED AND PASDR CALA2023021000396Unknown · corrodedSHEAR TIE CORRODED AT STA 1440 BETWEEN STR30 & 29R. REMOVED CORRODED SHEAR TIE AND INSTALLED NEW SHEAR TIE PN 146N1101-7UAL IAW B757 SRM 51-40-02 AND AMES DOC 47539FAB02 AND EC/RA #5300-02909. SEE PARTIAL WORK ON BACK AND PWS# 37 PGS 1 0F 1 FOR MORE DETAILS. SDR CALA2023021000395Skin · gougedENTRY FOR SDR: FUSELAGE OUTER SKIN IS GOUGED IN SEVERAL AREAS AT STA 620-640 BETWEEN STR 4L-5L. REPAIRED FUSELAGE OUTER SKIN DAMAGE BETWEEN STA 620-640 IAW SRM 53-00-01-2R DETAIL1. WORK PERFORMED ON AMES ILN NON ROUTINE 154944-0200-0194.SDR V0XD20230209001Support · corrodedL/H SIDE FLOOR SILL AT FR 68- FR 71 HAS SIGNS OF CORROSION IN MULTIPLE SPOTS. CORRECTIVE ACTION: REMOVED AND REPLACED DAMAGED L/H SIDE FLOOR SILL FROM FR 68- FR 71 IAW EMB 135/145 SRM 51-40-02.SDR DALA2023081006519Unknown · unknownSHIP 5637 AMOC, ER/A 605793-14AD - REPAIR IS COMMON TO SSI INSPECTION AREA. CORRECTIVE ACTION: REF ERA 605793-14AD. (2620196)SDR DALA2023042103133Unknown · unknownSHIP 5017 RAMP REPORTS DENT BELOW F/O WINDOW APPROX 2 FT BELOW MAJOR REPAIR. CORRECTIVE ACTION: PERM REPAIR PER A321 NEO SRM 53-00-11 & 53-11-11 WILL BE ACCOMPLISHED. CURRENTLY ON MON. (9908041)SDR IPXA2023021891102Bracket · noneINSPECTION TYPE:C14CRACK ON BRACKET (P/N:148T7312-43) OF L/H HORIZONTAL STABILIZER SEAL FAIRING NEAR STA 1767.25INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 85.01 AND BOEING DWG NO. 148T9220 SH 3 REV ''A'' , BOEING DWG NO. 148T7320 SH 2 REV ''E'' AND BSDR CALA2023021000392Stringer · unknownENTRY FOR SDR: STRINGER CUT AND DISPLACED AT F.S. 590 STR 3L TO FACILITATE SKIN REPAIR. INSTALLED STRINGER AND REPAIR SPLICE IAW SRM 53-00-03-2R-1 AND SRM 51-40-02. WORK PERFORMED AT AMES ILN ON NON ROUTINE 154944-0200-0205.SDR CALA2023021000391Forging · unknownFOR ESFR REPORTING ONLY. EA 5310-04554 ACCOMPLISHED. EA 5310-04554 OP 004 REPAIR FOR CONFIG B APPROVED. RII ITEM PERFORMED AT AARSDR CALA2023021000390Forging · unknownFOR ESFR REPORTING ONLY. EA 5310-04554 ACCOMPLISHED. EA 5310-04554 OP 003 REPAIR ACCOMPLISHED FOR CONFIG B. APPROVED. RII INSPECTION PERFORMED AT AAR MIA BY V891406.SDR YENA2023020900148None · noneDURING HEAVY MAINTENANCE: FUSELAGE / TAIL CONE / FR 83-85 & STGR 3L-6L / IMPACT DAMAGE -PRELIMINARY INSPECTIONS. (SUPPLEMENTAL TO FOLLOW)SDR VNAA202328020006Seat Track · gougedGOUGES AT SEAT RAIL ON LBL9 BTW FS581 TO FS661+32SDR VNAA2023280200005Seat Track · gougedGOUGES AT SEAT RAIL ON RBL9 BTW FS485 TO FS581SDR VNAA202328020004Seat Track · gougedGOUGES AT SEAT RAIL ON LBL27 BTW FS485 TO FS581SDR VNAA202328020003None · noneGOUGES ON SIDE SEAT RAIL BWT FS 485 TO FS 565+8 OF STGR15RSDR VNAA202828020002Seat Track · gougedGOUGES ON SIDE SEAT RAIL BWT FS 485 TO FS 565 +8 IB STGR15LSDR VNAA202328020001Seat Track · gougedGOUGE ON SIDE SEAT RAIL BWT FS421 TO FS437 OF STGR15LSDR IPXA2023021991122None · noneINSPECTION TYPE:C14CRACK ON CLIP(P/N:140T0130-38) OF AFT CARGO COMPARTMENT FLOOR BEAM AT STA 1065, RBL26.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 85.01 AND BOEING DWG NO. 140T0130 SH 10 REV"G"SDR IPXA2023021891101None · noneINSPECTION TYPE:C14CRACK ON CLIP(P/N:140T0130-39) OF AFT CARGO COMPARTMENT FLOOR BEAM AT STA 1065, LBL 26.INSTALL NEW PART I.A.W 767-300F SRM 51-40-02-0G, REV 85.01 AND BOEING DWG NO.140T0130 SH 10 REV ''G''.SDR FDEA202302070233Seat Track · damagedMAIN DECK CARGO SEAT TRACK LOBES DAMAGED AT STA. 1665. 10L. REF. SEQ. #183, W/O 85244 AND WRI 25- 50-3546. 0000237172 : LAFFOND, MARK P - 08-FEB-2023 17:49 REPAIRED MAIN DECK COMPT SEAT TRACK AT STA. 1665 L POSTION 10L. REF MD-11 SRM 53-00-52-2R FIG 2SDR YENA2023020900142None · noneDURING HEAVY MAINTENANCE: AFTER SEAL REST REMOVAL, FOUND CORROSION IN BEAM-LOWER FR, BAGG DOOR AT STRG 27R AND BTW FR 77 / FR 80 IN CF III AFT CARGO DOOR CUTOUT STRUCTURE; REF TOMX NRC00095 WO 2159 CORROSION ON BEAM-LOWER FR, BAGG DOOR AT STRG 27R AND BTW FR 7SDR SCNA20230208077Shield · corrodedDEFECT TC 203750000 NR0004: FWD CARGO BAY, RH AFT AFT SHIELD HAS SEVERAL COORODED FASTENER HOLES RESOLUTION: REMOVED, FABRICATED AND INSTALLED NEW FWD CARGO RH SHIELD AFT CARGO DOOR IAW SRM 51-40-02-0G-0 LOT# 5127013-1 ITEM HFAB53-RP-011.SDR SCNA20230208076Web · corrodedDEFECT TC203750000 NR00120: CORROSION AFT CARGO DOOR SURROUND SUB THRESHOLD WEB. RESOLUTION: REMOVED AND REPLACED AFT CARGO DOOR SURROUND SUB THRESHOLD WEB IAW 51-40-02-0G-0 AND BOEING DWG 146A5120SDR SCNA20230208075Not Reported · corrodedDEFECT TC 203750000 NR 00117: CORROSION AFT CARGO LH ZEE CHANNEL STA 727 TO STA 867 STR 25L RESOLUTION: CORROSION ON ZEE CHANNEL FROM STA 727 TO STA 867, STR 25L AT AFT CARGO FOUND IT TO BE OUT OF LIMITS, REMOVED AND REPLACED AND APPLIED FINAL REFINISHED PESDR SCNA20230208074Not Reported · corrodedDEFECT TC 203350000 NR00005: FWD CARGO BAY, RH Z CHANNEL HAS SEVERAL CORRODED FASTENER HOLES FROM STA 500A-500I. RESOLUITION: REPAIRED FWD CARGO BAY RH ZEE CHANNEL FROM STA 500A-500I IAW B737 SRM 51-40-02-0G, SRM 53-00-53-2R-5 REPAIR 5 AND DWG 143A7500.SDR V0XD20230207004Floor Support · corrodedRH FLOOR SILL FROM FR48 TO FR52 HAS MULTIPLE SIGNS OF CORROSION. CORRECTIVE ACTION IS TO REMOVE AND REPLACE WITH NEW FLOOR SILL IAW EMB 135/145 SRM 51-40-02. AVMAX WO 81031 WC2335.SDR V0XD20230207003Gusset · corrodedFLOOR BEAM GUSSET PLATE AT FR59-FR61 0BL HAS MULTIPLE SIGNS OF CORROSION. CORRECTIVE ACTION IS TO REMOVE AND REPLACE WITH NEW GUSSET PLATE IAW EMB SRM 51-40-02 AND SRM 51-20-03. AVMAX WO 81031 WC 1197.SDR V0XD20230207002Floorbeam · corrodedFLOOR BEAM AT BL0 AND FR59 HAS SIGNS OF CORROSION AT NUTPLATE AND GUSSET. CORRECTIVE ACTION IS TO CUTOUT DAMAGE AREA 1 INCH BY 1 INCH AND CUTOUT NEW FILLER FORM DOUBLER AND REPAIR IAW EMB 135/145 SRM 53-24-10 AND ETD 2023-145-001-702. AVMAX WO 81031 WC 1232.SDR V0XD20230207001Floor Support · corrodedRH FLOOR SILL FR35 TO FR41 HAS MULTIPLE SIGNS OF CORROSION. CORRECTIVE ACTION IS TO REMOVE AND REPLACE WITH NEW FLOOR SILL IAW EMB 1356/145 53-23-10. AVMAX WO 81031 WC2333.SDR SWAA2023031399795Angle · corrodedFWD CARGO FLOOR R/H TRANSITION ANGLE BETWEEN STA 500B TO 500D HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES.<[01] FWD CARGO R/H TRANSITION ANGLE IS OUT OF LIMITS BETWEEN STA 500B AND 500I PER SRM 53-00-53-1A-2.;[02] CORRECTION OF CORRECTIVE ACTION #1: FWD CASDR QXEA2023020700015Not Reported · not reportedFWD SERVICE DOOR FWD GIRT BAR FLOOR FITTING SPRING IS BROKEN. REMOVED AND REPLACED SPRING ON FWD SERVICE DOOR FWD GIRT BAR FLOOR FITTING REF AMM 53-10-25.SDR QXEA2023020700014Not Reported · corrodedFWD CARGO DOOR FUSELAGE CUTOUT CENTER LOWER SEAT REST CORRODED AS MARKED AT FR25. REMOVED AND REPLACED FWD CARGO DOOR FUSELAGE CUTOUT CENTER LOWER SEAT REST REF SRM 51-40-08 AND RESTORED SURFACE PROTECTION REF SRM 51-23-06.SDR CALA2023020600344Not Reported · crackedR/H W/W VAPOR BARRIER LOWER CHORD CRACKED BETWEEN RBL6.01 AND RBL15.04 STA693. REF BY AIRBORNE/PEMCO NR.13088.0811. REPAIRED R/H W/W VAPOR BARRIER LOWER CHORD BETWEEN RBL15.04 STA 693 AS PER REF B737 SRM 57-10-10-2R-5 FIG 202 SHEET 4. COMPLETED BY V095648, INSSDR DALA2023020600897Not Reported · not reportedSHIP 689 CORROSION ON RH SIDE PLATE AND SPLICES (2 EAS) BTW STA 1380 AND STA 1440AT AFT CARGO C2. CORRECTIVE ACTION: SUMMARY OF NRC 165: RH SIDE PLATE AND SPLICES (2 EAS) BTW STA 1380 AND STA 1440AT AFT CARGO C2 WERE REPLACED PER B757-200 SRM. (2616094)SDR SWAA2023031398649Shield · corrodedAFT CARGO RIGHT TRANSITION ANGLE767-787 HAS CORROSION AROUND MULTIPLE FASTNER HOLES. MARKED.<[01] REMOVED CORROSION RIGHT TRANSITION ANGLE STA 767-787. REMAINING THICKNESS 0.030?. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] VERIFIED C/A #1.;[03] REMOVSDR SWAA2023031398650Angle · corrodedAFT CARGO LEFT TRANSITION ANGLE HAS AREAS OF CORROSION AROUND FASTNER HOLES STA 727I-747.<[01] REMOVED CORROSION AROUND FASTENER HOLES LEFT TRANSITION ANGLE STA 727I - 747. REMAINING THICKNESS IS 0.030. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2;[02] VERISDR QXEA2023020700013Seat Track · corrodedFWD WET AREA HAS CORROSION ON RH SEAT TRACK AT FR 13 AS MARKED. REMOVED AND REPLACED NEW RH SEAT TRACK AT FRAME 13 REF SRM 51-40-08. COMPLIED WITH SURFACE PROTECTION REF SRM 51-23-06. APPLIED CIC PROTECTION ON REF CPM 51-25-00.SDR V0XD20230204001Seat Track · corrodedLH SIDE SEAT TRACK HAS MULITPLE SIGNS OF CORROSION AT FR 36- FR 47. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT TRACK FROM FR 36- FR 47 L/H SIDE IAW EMB 135/145 AMM 53-01-06.
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