JASC 5310
Service difficulty reports · 38,528
Reports filed under 5310 · Fuselage Main, Structure, 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 = '5310' 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 = '5310' 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 ASAA2023082245085Beam · corrodedRH LAV MOUNT STA 951 HAS CORROSION ON BEAM. GROUNDED - YES. REMOVED AND REPLACED BEAM CAP IAW B737-700 SRM 53-70-51-2R-5 W -1" O-.180" R-.130" L-1" D-050".SDR YENA2023082400986Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON AFT FRAME SEGMENT (2) OF THE EMERG EXIT HATCHES 843 (1) CRACK LENGTH 0.360 INCH (2) SEGMENT CRACK LENGTH 0.375 INCH; REF: AEROMAN W/O 2023-272/1 N/R 2023-424625 REMOVED AND REPLACED FWD FRMAE SEGMENT (1) OF TSDR YENA2023082400985Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FRAME SEGMENT (2) OF THE EMERG EXIT HATCHES 844, CRACK LENGTH (1) L= 0.281 INCH (2) CRACK LENGTH L= 0.400 INCH; REF: AEROMAN W/O 2023-272/1 N/R 2023-424627 AND 2023-424628. REMOVED AND REPLACED FWD AND ASDR YENA2023082400984Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FRAME SEGMENT (2) OF THE EMERG EXIT HATCHES 844, CRACK LENGTH (1) L= 0.281 INCH (2) CRACK LENGTH L= 0.400 INCH; REF: AEROMAN W/O 2023-272/1 N/R 2023-424627 AND 2023-424628. REMOVED AND REPLACED FWD AND ASDR YENA2023082400983Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FRAME SEGMENT (2 EA) OF THE EMERG EXIT HATCHES 834 CRACK (1) L= 0.425 INCH AND (2) L= 0.410 INCH; REF: ARM W/O 2023-272/1 N/R 2023-424625 AND N/R 2023-424626. REMOVED AND REPLACED FWD AND AFT FRAMES IAW SDR YENA2023082400981Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FWD FRAME SEGMENT (2) OF THE EMERG EXIT HATCHES 833 CRACK (1) L=0.350" (2) CRACK L= 0.400 INCH; REF: ARM W/O 2023-272/1 N/R 2023-424631 AND 2023-424632. REMOVED AND REPLACED FWD AND AFT FRAMES ON TASK CARD ASDR YENA2023082400978Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON LOWER FITTING FRONT WINDSHIELD FRAME IN COCKPIT ON INTERNAL SIDE OF THE LOWER ATTACHMENT AREA OF THE WINDSHIELD CENTER POST AROUND UPPER FASTENER HOLE ON UPPER RADIUS, LH SID CHACK LENGTH .100 INCHES; REF: ARM W/O SDR YENA2023082400977Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON LOWER FITTING FRONT WINDSHIELD FRAME IN COCKPIT ON INTERNAL SIDE OF THE LOWER ATTACHMENT AREA OF THE WINDSHIELD CENTER POST AROUND UPPER FASTENER HOLE ON UPPER RADIUS RH SIDE CRACK LENGTH .101 INCHES; REF ARM W/O 2SDR YENA2023082400976Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON LOWER FITTING FRONT WINDSHIELD FRAME IN COCKPIT ON INTERNAL SIDE OF THE LOWER ATTACHMENT AREA OF THE WINDSHIELD CENTER POST ON LOWER RADIUS RH SIDE CRAC LENGTH .150 INCHES; REF: ARM W/O 2023-272/1 N/R 2023-424773. SDR YENA2023082400975Unknown · unknownDURING HEAVY MAINTENANCE: CRACK INDICATION ON CONTINUITY FITTING FRONT WINDSHIELD FRAME IN COCKPIT ON INTERNAL SIDE FOR THE LOWER ATTACHMENT AREA OF THE WINDSHIELD CENTER POST-LH SIDE CRACK LENGTH .160 INCHES; REF: ARM W/O 2023-272/1 N/R 2023-424774. REMOVED ASDR YENA2023082400971Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / NOSE FWD FUSELAGE / WINDSHIELD FRAME / CENTER LOWER NODE / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR FDEA202308221473Unknown · unknownEMPENNAGE - AFT ACCESSORY COMPARTMENT DURING DETAILED VISUAL INSPECTION FOUND CRACK AT LOWER TORQUE BOX PANEL WEB AT APPROXIMATE STATION Y = 2122.881.SDR R61A2023082000436Shear Tie · corrodedDURING HEAVY CHECK - CORROSION ON SHEAR CLIP AT FR82 IN AFT CARGO STR.29L TO 29R. REMOVED AND REPLACED SHEAR CLIP AT FR82 AFT CARGO STGR 29L AND 29R AND APPLIED SURFACE PROTECTION TO FASTENERS REFER SRM 51-40-08, 51-23-06, CPM 51-25-00SDR R61A2023082000435Crossbeam · corrodedDURING HEAVY CHECK - "CORROSION ON CROSSBEAM REPAIR AT FRAME 17 BETWEEN LH AND RH CENTER TRACK. REMOVED AND REPLACED CROSSBEAM FRAME 17 REFER SRM 51-40-08 "SDR R61A2023082000434Beam · corrodedDURING HEAVY CHECK - "AFT PASSENGER DOOR CUTOUT LOWER BEAM CORRODED INSIDE AFT GIRT BAR FITTING CUTOUT. REMOVED AND REPLACED AFT PASSENGER
DOOR CUTOUT LOWER BEAM. REF: SRM 51-40-08."SDR R61A2023082000433Crossbeam · corrodedDURING HEAVY CHECK - "FWD WET AREA FLOOR SUPPORT STRUCTURE LH STILL AT FR 16 STGR 17L HAVE CORROSION ON LH CROSSBEAM. REMOVED AND REPLACED FR 16 CROSSBEAM REF: SRM 51-40-08. SEE ATTACHED WIP'S AND TASKS FOR WORK ACCOMPLISHED"SDR R61A2023082000432Beam · corrodedDURING HEAVY CHECK - "FWD SERVICE DOOR CUTOUT STRUCTURE LOWER BEAM, FWD AND AFT SLIDE FITTINGS HAVE MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED FWD SERVICE DOOR CUTOUT STRUCTURE LOWER BEAM REF EMB SRM 51-40-08."SDR R61A2023082000431Beam · corrodedDURING HEAVY CHECK - FWD PASSENGER DOOR CUTOUT STRUCTURE, LOWER BEAM, FWD AND AFT SLIDE FITTING CUTOUT HAVE MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED FWD PASSENGER DOOR CUTOUT STRUCTURE, LOWER BEAM. REF SRM 51-40-08.SDR SWAA2023092191604Pressure Deck · crackedCRACK FOUND AT HORIZONTAL PRESSURE DECK WEB STA 663 LBL 37. CRACK LENGTH 0.343' CRACK FOUND AT HORIZONTAL PRESSURE DECK WEB STA 663 LBL 37. CRACK LENGTH 0.343'<[01] ACCOMPLISHED REPAIR AT HORIZONTAL PRESSURE DECK WEB STA 663 LBL 37 AS PER SRM 53-40-51-2R-2 REPSDR BAGA2023091800008Floor Support · corrodedCORROSION ON ENTRY WAY 9 HOLE FLOOR SUPPORT AROUND FASTENER HOLE AT FR 17 AT Y-13 CORRECTIVE ACTION - REMOVED AND REPLACED 9 HOLE FLOOR SUPPORT PN170-12118-001 AT FRAME 17 Y-13 IAW EMB 190 SRM 51-40-08SDR VNAA202308190015Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM SDR JR2R20230819784Shear Panel · corrodedFLOOR WEBB BETWEEN FR87 THRU FR88 AND LBL11 THRU RBL11SDR VNAA202310100004Striker · wornPAX DOOR SEAL STRIKER WITHIN 1,374.07 FH (BEFORE 20,312.15 FH) . REPLACED PER CRJ900 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND EA 23-C9-53-0145 REV.IRSDR SWAA2023091590415Pressure Deck · crackedCRACK FOUND ON HORIZONTAL PRESSURE DECK WEB R/H STA 663+2 RBL 39+0.7 L: 0.5'<[01] UPDATED STEPS 2-7.;[02] STEP 15 IN PARTIAL.;[03] CRACK FOUND TO BE OUT OF LIMITS ON HORIZONTAL PRESSURE DECK WEB R/H STA 663+2 RBL 39+0.7 NO ALLOWABLE LIMITS IN SRM; REPAIRED ARESDR SWAA2023082491029Pickle Fork · crackedLEFT PICKLE FORK CRACKED AT STA 665 AT STRINGER 18A LT AFT LOWER ABOVE LINK VERIFIED WITH HFEC<[01] PERFORMED HFEC INSPECTION IAW B737 NDT 51-00-00 PART 6 PROC 23 FOR VERIFICATION. PERFORMED HFEC INSPECTION IAW B737 NDT 51-00-00 PART 6 PROC 23 FOR VERIFICATIOSDR VNAA202308180020Frame · wornWEAR ON FRAME 349.00 BTW STGR 1 TO STGR 2 RH. FRAME 349.00 BTW STGR 1 TO STGR 2 RH WAS REPAIRED PER REO 690-53-21-1638 REV.--SDR VNAA202308180016Plate · corrodedCORROSION AT KICKPLATE ON L1 SURROUND STRUCTURE BTW FS 310.00 TO STA 349.00. DUE TO EXCESSIVE CORROSION AT KICKPLATE ON L1 SURROUND STRUCTURE BTW FS 310.00 TO STA 349.00 WAS REPLACED PER CRJ-900 SRM 53-21-23-101-001-A02 AND SRM 51-42-06-001-001-A01SDR VNAA202308180014Seat Track · corrodedCORROSION ON FLOOR SEAT RAIL AT LBL9.00 AND RBL9.00 BTW FS.847.00 AND FS.977.00. FLOOR SEAT RAIL AT LBL9.00 AND RBL9.00 BTW FS.847.00 AND FS.977.00 WERE EVAULATED PER CRJ-900 SRM 53-41-49-101-001-A02; CRJ900 SRM 53-51-49-101-001-A02 AND WERE REPLACED PER CRJSDR CALA2023081802555Beam · unknownYO VERTICAL BEAM AT FR 1 BULKHEAD WAS REPAIRED AT BQN, REPAIR IS AN INTERM (TEMPORARY) SOLUTION. ACCOMPLISH A PERMANENT PER PART 3 OF THE LATEST REVISION OF EC/RA 5311-03051 ON OR BEFORE THE AIRCRAFT REACHES 34,167 TOTAL AIRCRAFT FLIGHT CYCLES(TOTAL AIRCRAFT FSDR VNAA202308170007Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% REAR SPAR DATUM (OML TRACE). FWD DRAG ANGLE LH BTW 55.625% STGR DATUM (TRACE AT BL0.00) TO STGR DATUM TO 67.5% WAS REPAIREDSDR SWAA2023091190375Intercostal · crackedCRACKED INTERCOSTAL BS 380-400; LBL 13; WL 208.<[01] UPDATED STEP 1.;[02] STEP 2 COMPLETE; STEP 3 IN PARTIAL.;[03] COMPLETED MEASUREMENT TABLE.;[04] COMPLETED STEP 1.;[05] TASK CARD COMPLETE.SDR FDEA202308161449None · noneAGING AIRCRAFT - LOWER CENTRE CARGO COMPARTMENT STATION 1841 , X = 15 WEB ASSEMBLY FOUND WITH EXISTING REPAIR DOUBLER. LOWER CENTER CARGO COMPARTMENT STATION 1841 X = 15 WEB ASSEMBLY AT EXISTING REPAIR DOUBLER EVALUATED AND FOUND REPAIRED IN ACCORDANCE SDR ASAA2023081545969Beam · corrodedFWD WET AREA FR18-FR20 CORROSION ON TOP SURFACE OF CENTER RIGHT AXIS Y-254 LONGITUDINAL BEAM GROUNDED - YES. EVALUATED CORROSION ON BEAM, FOUND TO BE OUT OF LIMITS IAW A320 SRM 53-11-14-283-007. REMOVED AND REPLACED LONGITUDINAL BEAM IAW AIRBUS DWG D53111461SDR ASAA2023081545696Beam · corrodedFWD WET AREA FR16-FR20 CORROSION ON TOP SURFACE OF CENTER LEFT AXIS Y254 LONGITUDINAL BEAM GROUNDED - YES. REMOVED CORROSION FROM LONGITUDINAL BEAM (TRACK) BETWEEN FR16-FR20,CENTER LEFT AXIS Y254, ORIGINAL THICKNESS 0.071", REMOVED 0.029", REMAINING MATERIAL SDR SWAA2023081789625Access Panel · broken194BR ACCESS PANEL #5 AFT TRACK BROKEN<[01] REMOVED AND REPLACED PANEL 194BR IAW AMM 53-51-21 AND AMM 20-50-11.SDR DALA2023081606673Unknown · unknownE&E DOOR SURROUND JAMB PAN AND SUPPORT FRAMES DAMAGED DURING LANDING. REMOVED E&E DOOR SURROUND JAMB PAN PER B717 SRM 51-40-02. INSTALLED E&E JAMB PAN AND SUPPORT FRAMES PER B717 SRM 51-40-02 AND DWG 9911550. (LP #2919766)SDR FDEA202308151435Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR68, -Y450 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR68, -Y450 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5SDR FDEA202308151434Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR61 - FR62, Y953 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-510SDR FDEA202308151432Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR27 LH BETWEEN FR77 AND FR78 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR27 LH BETWEEN FR77 AND FR78 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. SDR FDEA202308151431Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR28 LH BETWEEN FR77 AND FR78 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR28 LH BETWEEN FR77 AND FR78 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. SDR FDEA202308151430Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR43 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR43 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. SDR FDEA202308151429Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR42 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR42 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. SDR FDEA202308151428Stringer · unknownEXISTING REPAIR ON FUSELAGE STRINGER AT STGR41 RH BETWEEN FR71 AND FR72 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FUSELAGE STRINGER AT STGR41 RH BETWEEN FR71 AND FR72 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-14 FIG.201. SDR FDEA202308151427Splice · crackedCOMPLY WITH EO 6-5310-7-5023 A PT1 REPLACED THE CRACKED SPLICE AT THE JUNCTION AT STGR18L FR47, TITLE: FUSELAGE - CENTER SECTION - INSPECTION OF STRINGER 18 LH/RH AT FRAME47, AIRBUS SB A300-53-6157 COMPLIED WITH EO 6-5310-7-5023 A PT1 REPLACED THE CRACKED SDR FDEA202308151424Seat Track · unknownEXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR66, Y1456 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MAIN DECK COMPT SEAT TRACK AT FR65 - FR66, Y1456 WAS EVALUATED AND FOUND IN CONFORMITY WITH A300-600 SRM53-10-16 FIG.208. EO: 6-5SDR JR2R20230815780Web · corrodedFLOOR WEB BETWEEN FR87 THRU FR88 AND RBL12 THRU RBL42 CORRODEDSDR ASAA2023081445695Beam · corrodedMAIN CABIN AFT WET AREA R/H LONGITUDINAL BEAM BETWEEN FRAMES 69 ABD 70 AXIS -Y160.5 CORRODED ON UPPER SURFACE. GROUNDED - YES. REMOVED CORROSION FROM MAIN CABIN AFT WET AREA R/H LONGITUDINAL BEAM BETWEEN FRAMES 69 AND 70. AXIS -Y160..5, ORIGINAL THICKNESS 0.1SDR SWAA2023091989579Pressure Web · crackedCRACK FOUND ON HORIZONTAL PRESSURE WEB AT STA 663 AND RBL 42 (CRACK LENGTH .500) CRACK FOUND ON HORIZONTAL PRESSURE WEB AT STA 663 AND RBL 42 (CRACK LENGTH .500)<[01] ACCOMPLISHED PERMANENT REPAIR AT MAIN CABIN HORIZONTAL PRESSURE DECK WEB BETWEEN STA 663.75 ASDR F3LA2023082800137Door Seal · corrodedDISCREPANCY: REFERENCE NR 5001257278-0010. AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX.CORRODED SILL SHAPE ON RH FWD DOOR NO AWOLLABLE DAMAGE FOUND ON SRM REQUIRES REPLACEMENT AS PER A321 SRM 51-72-11 REV.146 CORRECTIVE ACTION: PERFORMED INSTALLSDR FDEA202308131458Panel · crackedWHILE TROUBLESHOOTING FOUND A CRACK IN THE LOWER TORQUE BOX PLANE PANEL AT STA. 2122. REPAIRED CRACK IN THE LOWER TORQUE BOX PLANE PANEL AT STA. 2122 IN REF. EA# 1-5310-T0375777 P1. FUSELAGE - MAINFRAME - CRACK IN LOWER TORQUE BOX WEB, APU COMPARTMENT CEILIN
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