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 IPXA2023050846500Unknown · unknown*SDR FILED OPEN* FOUR CREW ESCAPE DESCENT DEVICES DROPPEDSDR EE4Y2023050617693Fitting · crackedDURING THE ALLEGIANT TASK 53-210-003_P1-OP-UP-NDT/00 WORK CARD INSTRUCTIONSACCOMPLISHMENT RELATED TO AD 2020-17-03, WAS FOUND THE LH AND RH CONTINUITY FITTING WITH CRACK.AIRBUS WAS CONTACTED TO REQUEST THE KITS P/N FOR REPLACEMENT. AIRBUS PROVIDED THEINFORMATISDR SWIA202306130021Unknown · crackedSTRINGER 3L CRACKED AT FS 280 BULKHEAD (C-CHECK RO 6/9/2023) REPAIRED STRINGER 3L AT F.S 280 REF REO 670-53-21-493 REV-D DATED 2015-07-10. AND SERVICE BULLETIN 670BA-53-040 REVISION C DATED 09-20-2012, FUSELAGE CENTER FUSELAGE PRIMARY STRUCTURE FS280.00SDR A6WA202305058596Seat Track · corrodedCORROSION ON SEAT RAIL AT FS589.00+8 TO FS605.00 & LBL27. P1-L=1.800Ï¿½X W=0.900Ï¿½X D=.050 AIRCRAFT REMOVED FROM SERVICE. CORROSION ON SEAT RAIL BLENDED CORROSION ON SEAT RAIL FS589.00+8 & RBL27.ORIGINAL MATERIAL THICKNESS 0.050Ï¿½ & REMAINING THICKNESS 0.SDR DALA2023050903622Unknown · unknownSHIP 3403 LIGHTENING STRIKE APPROX 30" BELOW 1ST CLASS APPROX FR 21 LEFT AIRCRAFT SIDE. CORRECTIVE ACTION: REPAIRED REF A330 SRM 53-21-11. (2753144)SDR 2A6D20230505001Frame · chafedDAMAGE WAS NOTED TO THE X1790.15 FRAME (PN: 350A21-4099) IN THE FORM OF A CHAFE DAMAGE AREA. THE CHAFE DAMAGE IS LOCATED NEAR THE INBOARD RH CAMLOC AND WAS MEASURED TO BE APPROXIMATELY 0.70” X 0.175SDR CALA2023050501369Panel · corrodedFWD CABIN PANEL BREAK BETWEEN STA 312 AND STA 328 AT RBL 11 WL 208.1 HAS CORROSION AROUND FASTN ER HOLES REF AAR N/R 9672210 REMOVED AND REPLACED THE FWD CABIN BRAKE BETWEEN FS312 AND FS 32 8 RBL11 WL 208.1 IN REF IWTH B737 SRM 51-40-02-0G-0 AND DWG 141A 5400 SDR IPXA2023050826401Lock · crackedDOOR AREA CARGO LOCK #12 AT POS 2R IS CRACKED REMOVED AND REPLACED CARGO LOCK AT POS 2R #12 PER AMM 25-58-01.SDR DALA2023050503506Unknown · unknown(LOG 4742035) DURING INSPECTION FOUND LIGHTNING STRIKE DAMAGES ON RT SIDE FUSELAGE 4 HITS BETWEEN STATIONS 500 TO 500H. C/W SRM REPAIR OF STRIKE AT STA 500E, STR 21R AND 22R PER SRM 53-00-01-1A.SDR GTIA2023050537167Torque Box · corroded"CORROSION FOUND ON LH NLG TORQUE BOX (SWIVEL BEARING) AT FR 19-20 RH HOLE B. RAF01 CREATED. SDR SUBMITTED-REPAIRED LH NLG TQ BOX REF AIRBUS RDAF 80211264/002/2023A HAECO S/O 122166
N/R 24053 CAT A REPAIR "SDR DALA2023050403464Unknown · unknownSHIP 3356 CORROSION FLOOR BEAM Y380 BTW FR75/FR78 AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: REPLACED FLOOR BEAM Y380 LOC. BTW FR75/FR78 AT AFT GALLEY AREA. RII INSPECTION COMPLETE. (2750601)SDR SWIA20230613020Unknown · corrodedINTERCOSTAL CORRODED - STR 20R FS 319.0 - FS 333.0 (C-CHECK RO 6/9/2023) REMOVED AND REPLACED INTERCOSTAL FS319-FS349 STGR 20R REF. DWG SH670-31950 REV. Y, CRJ 700 SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01. COMPLIED WITHI TASK CARD 51-900-1002SDR SWAA2023060544494Scuff Plate · crackedCRACK ON FORWARD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-299328<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189515;DUE DATE:19-DEC-23.;[02] RADIOMETER TOOL USED PN: XRP-3000; SN: 1753759; DUE DATE: 14-OCT-23;[03] REPAIRED FORWARD CORNER SCUFFSDR MK1Y20230503023Unknown · unknownSTA 139 - ATA 180.5, BELOW WINDOWS R1 AND R1: DURING MAINTANACE INSPECTION AT IAI, SHOP FOUND TWO (2) DOCUMENTED REPAIRS AT THE NOTED LOCATION. FWD REPAIR: LIGHTNING STRIKE REPAIR AT STA 139, BELOW WINDOW R1. AFT REPAIR: A DOUBLER REPAIR ON THE EXTERNAL FUS SKSDR SWIA2023052503Unknown · corrodedCORROSION FOUND AT COCKPIT FLOOR DOUBLER FROM FR 7-8 STRG 16L AS MARKED (C-CHECK RO 5/21/2023) SPLICED IN NEW LH COCKPIT FLOOR DOUBLER REF ETD2023-170-011500 REV.:/. REPAIR DOUBLER PARTS WEIGHED 89.5 GRAMS (LESS THAN 2.5 LBS), NO CHANGE TO WEIGHT AND BSDR MK1Y20230503021Unknown · unknownEXTERNAL FUSELAGE SKIN, STA 661, STR-30R-STR-31R: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE BULGE ON FUSELAGE SKIN LOCATED AT STA 661, 2-INCH BELOW THE STR 30R. INITIAL DIMENSION OF BULGE IS A=0.57”, Y=0.0278” (A/Y=20). BULGE IS OUT OF LIMITS PER SRSDR MK1Y20230503020Unknown · unknownSEC 46 FUSELAGE SKIN, STA 1564.3, 5” ABOVE STR 16L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 1264.3, 5” ABOVE STR 16L. INITIAL DIMENSION OF DENTED AREA A=0.720”, Y=0.032” (A/Y=22). DENT IS OUT OF LIMITS PER SRM SDR MK1Y20230503019Unknown · unknownSECTION 41 – FUSELAGE SKIN – STA 422 BETWEEN STR 31L AND STR 32L: A BULGE OUT OF LIMITS ON THE FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8SDR MK1Y20230503018Unknown · unknownSECTION 43 FUSELAGE SKIN STA 669.3 BETWEEN STR 35L AND STR 36L: AN EXISTING BULGE OUT OF LIMITS ON FUSELAGE SKIN WAS REPAIRED PER SRM 53-00-01 REPAIR 8.SDR MK1Y20230503017Unknown · unknownSEC 43 FUSELAGE SKIN, STA 600.8 BTWN STR 32L-33L: DURING MAINTENANCE INSPECTION, MAINTENANCE FOUND ONE DENT ON FUSELAGE SKIN LOCATED AT STA 600.8 BETWEEN STR 32L AND STR 33L. INITIAL DIMENSION OF DENTED AREA A=0.680”, Y=0.027” (A/Y=25). DENT IS OUT OF LIMITS PSDR MK1Y202305173013Unknown · unknownBT STA 1518-1562, STR 38L-37R: DURING DAMAGED SHEAR TIE P/N 140T2102U585 REMOVAL IN ORDER TO INSTALL NEW SHEAR TIE SHOP MISTAKENLY DOUBLE DRILLED THE TEAR STRAP AND SKIN AT 4EA HOLES. THE ORIGINAL HOLE DIA 0.186”. THE HOLES WERE DRILLED UNTIL THE WHOLE DAMAGE SDR IPXA2023050884762Unknown · unknown*SDR FILED OPEN* FAULT - FOUND AFT CARGO TRAY-LOCK CRACK AT STA 1336 LBL 43. (REPLACE) 3.DRILLING NEW HOLDS FOR TRAY-LOCK IAW SRM51-40-05-0G REV.86.00SDR IPXA2023050884890Unknown · unknown*SDR FILED OPEN* FAULT - FOUND AFT CARGO TRAY-LOCK CRACK AT STA 1336 LBL 20. (REPLACE) DRILLING NEW HOLE FOR TRAY-LOCK I.A.W SRM 51-40-05-0G REV.86.00.SDR CALA2023050501354Skin · unknownOPEN AMES WORK PACK N664UA-1 FOR C-4 MAINTAINENCE CHECK.SDR DALA2023050503504Unknown · unknown(LOG 2749886) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER EM 5300-01157, MAINTENANCE FOUND A CRACK ON THE FAILSAFE STRAP (P/N: 225A3523-3) COMMON TO THE LH FS663 PICKLE FORK FITTING. MAINTENANCE REPAIRED DAMAGE PER ERA 607842-14AD.SDR DALA2023050503503Unknown · unknown(LOG 2749844) DURING INSPECTIONS FOR CRACKING OF THE FS663 PICKLE FORK FITTINGS PER EM 5300-01157, MAINTENANCE FOUND A CRACK ON THE FAILSAFE STRAP (P/N: 144A2412-3) COMMON TO THE LH FS663 PICKLE FORK FITTING. MAINTENANCE REPAIRED CRACK PER ERA 607711-14AD.SDR YENA2023005020487Unknown · unknownDURING HEAVY MAINTENANCE: [CPCP FINDING] CORROSION ON FLOOR BEAM BTW FR 87 AND Y= 300 LH AT FLOOR STRUCTURE W2; (RESOLVED ON W/O: 1216530 TASKCARD: NR-00001 ) ALL WORK ACCOMPLISHED ON TOMEX NRC # 00094: CORROSION ON FLOOR BEAM BTW FR 87 AND Y= 300 LH WAS REMOVSDR YENA2023005020486Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION IN FLOOR BEAM LOCATED BTW FR15 AND FR19 PLUS Y= -270.0 ON PASSENGER FLOOR STRUCTURE W1; (RESOLVED ON W/O: 1216530 TASKCARD: NR-00002 ) ALL WORK ACCOMPLISHED ON TOMEX NRC 00149, FLOOR BEAM LOCATED BTW FR15 AND FR19 PLUS Y= -2SDR YENA2023005020482Unknown · unknownDURING HEAVY MAINTENANCE: CORROSION IN FLOOR BEAM LOCATED BTW FR15 AND FR19 PLUS Y= -270.0 ON PASSENGER FLOOR STRUCTURE W1; ALL WORK ACCOMPLISHED ON TOMEX NRC 00149, FLOOR BEAM LOCATED BTW FR15 AND FR19 PLUS Y= -270.0 ON PASSENGER FLOOR STRUCTURE W1, IT IS CLASDR YENA2023005020481Unknown · unknownDURING HEAVY MAINTENANCE: [CPCP FINDING] CORROSION ON FLOOR BEAM BTW FR 87 AND Y= 300 LH AT FLOOR STRUCTURE W2; ALL WORK ACCOMPLISHED ON TOMEX NRC # 00094: CORROSION ON FLOOR BEAM BTW FR 87 AND Y= 300 LH WAS REMOVED AND EVALUATED, THEREFORE IS OUT LIMITS. THE SDR YENA2023005020480Unknown · unknownDURING HEAVY MAINTENANCE: FUSELAGE / CENTER FUSELAGE III / FRAME 80 / BTW STGR 28R - 27R / CORROSION -TEMPORARY REPAIR. (CONSIDERED AS A MAJOR REPAIR)SDR DALA2023050403466Unknown · unknownSHIP 3319 LIGHTNING STRIKE 6 FASTENERS AFT OF FRAME 87 ON STRINGER 51L. CORRECTIVE ACTION: FASTENER(TEMPORERY REPAIR) REMOVED PER A330 SRM 53-51-11 ROTATING PROBE REQUEST. FASTENER LOCATION IS NOT IDENTIFIED CORRECTLY IN ORIGINAL WRITE UP, THERE IS NO STRINGERSDR V0XD20230503002Gusset · corrodedRH GUSSETT PLATE AT Y = 479.0 AND FRM 60 HAS SIGNS OF CORROSION. EVAL CORRECTIVE ACTION: REMOVE AND REPLACED R/H GUSSETT PLATE P/N 145-26437-001 @ Y = 479.0 FR 60 IAW EMB 145 SRM 51-20-03 AND SRM 51-40-02 SEE AVMAX WO 81054 WC 1200SDR MK1Y20230503011Unknown · unknownSTA 236.5, LBL 69.25: DURING MAINTENANCE INSPECTION SHOP FOUND FLOOR BEAM AND SHEAR WEB WITH MISSING MATERIAL.SDR MK1Y20230503010Unknown · unknownFUS. SKIN, SEC 48, BT STA 1809.5 – STA 1824, ABOVE STR 22L: DURING MAINTENANCE INSPECTION SHOP FOUND UNDOCUMENTED REPAIR ON THE EXTERNAL FUS SKIN, P/N 148T3181-7. A REVIEW OF THE PREVIOUS OPERATOR’S RECORDS (DAL) WAS PERFORMED AND NO DOCUMENTATION WAS FOUND. TSDR MK1Y20230503009Unknown · unknownSEC 46, STA 1197 – 1197=22, STR 38L -38R: UNDOCUMENTED DOUBLER REPAIR FOUND NEXT TO DOCUMENTED DOUBLER BETWEEN STA 1189 – 1197=14, STR35L – 38L, DOCUMENTED ON ERA 518660-14AD.SDR MK1Y20230503008Unknown · unknownDURING MAINTENANCE INSPECTION, SHOP FOUND A LIGHTNING ST88IKE DAMAGE ON SKIN, AT A BUTT JOINT AT THE NOTED AREA. SHOP PERFORMED 0.4"X1.0" SIZE BLEND OUT ON THE DAMAGED AREA. AFTER NDT INSPECTIONS, IT WAS FOUND THAT THE MINIMUM THICKNESS IS 0.54", AND THE NOMINSDR MK1Y20230503007Unknown · unknownTAILCONE OUTER SKIN BTWN STA 1943.5-1952: DURING CONVERSION AT IAI IN TLV, MTX FOUND SEVERAL DAMAGES AND UNDICUMENTED REPAIRS ON OUTER TAILCONE SKIN. THE FOUNDS WERE: -BLEND OUTS; - WELDING REPAIRS; - LIGHTNING STRIKES; - FASTENER REPAIRS. SOME OF THESE FOUNDISDR MK1Y20230503005Unknown · unknownDURING AIRCRAFT CARGO CONVERSION, A 0.186" DIAMETER INITIAL FASTENER HOLE WAS MISTAKENLY DAMAGED IN THE STA 1065 BULKHEAD WEB AND NO. 6 STIFFENER. THE BULKHEAD STRUCTURE IS CLASSIFIED AS PRIMARY STRUCTURE, A PSE, AND FCBS (NOTE 1) PER REF 767-300 SRM 51-00-04,SDR MK1Y20230503002Unknown · unknownFUSELAGE SKIN REPAIR, BETWEEN STA 157 AND STA 162, ABOVE STR-21L: DURING MAINTENANCE CHECK, IAI SHOP DISCOVERED AN EXISTING REPAIR IN FUSELAGE SKIN LOCATED AT THE NOTED AREA. THE FLUSH REPAIR IS LOCATED IN THE EXTRA CRITICAL AREA, FWD TO THE PITOT STATIC PROBESDR V0XD2023050300001Gusset · corrodedR/H AISLE GUSSET UNDER SEAT TRACK AT FRM 35 TO FRM 39 SHOWS SIGNS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED R/H GUSSET IAW EMB 145 SRM 51-40-09, 51-40-02.SDR SWI2023F00047Unknown · galledLEFT HAND SIDE SEAT RAIL IS GALLED BTW STA 364 AND 379 (C-CHECK RO 6/9/2023) BLENDED LH SIDE SEAT RAIL BTW STA 364 AND 379, REF CRJ 700 SRM 53-21-49-101-001-A01DAMAGE IS OUT OF LIMITS DUE TO NO DAMAGE REMOVAL ALLOWABLE IN BLENDED AREA REF CJ700 SRM 53-2SDR SWIA2023052502Unknown · corrodedNOTED CORROSION ON SHEAR CLIP, FORWARD INBOARD CORNER, OF LAVATORY SERVICE CUTOUT, AT FR 88 AND STGR 27R. (C-CHECK RO 5/21/2023) REMOVED AND REPLACED SHEER CLIP ON FORWARD INBOARD CORNER OF LAVATORY SERVICE CUTOUT REF EMB SRM 51-40-08. RESTORED SURFACESDR CALA2023050301321Fitting · unknownINSPECT THE REPAIRED AREAS AT FUSELAGE STA 808 & S13R PER THE LATEST REVISION OF ECRA 5350-02481 PART 2 ON OR BEFORE 29-APR-2024 GENERATED A DTA/DIP PER ECRA 5350-02481 PART 1 ITEM 2. REF EC 5350-02481, INSPECT THE REPAIRED AREAS AT FUSELAGE STA808 TOMC-APPROVSDR CALA2023050301320Unknown · unknownINSPECT THE FUSELAGE SKIN AND CHORD STRAP REPAIR INSTALLED AT STA 1725.5 AND S-7R, PER LATEST REVISION OF ECRA 5380-01359 PART 2 BEFORE THE AIRCRAFT REACHES 37,500 TOTAL FLIGHT CYCLES. REPEAT THE INSPECTIONS AT INTERVALS NOT TO EXCEED 6,000 FLIGHT CYCLES THERESDR V0XD20230502003Floor Support · corrodedR/H AISLE GUSSET SHOWS SIGNS OF CORROSION FROM FRM 39 TO FRM 45. CORRECTIVE ACTION: REMOVED AND REPLACED FLOOR SILL FROM FRM 39- FRM 45 R/H SIDE IAW EMB 145 SRM 51-40-02. SEE AVMAX WO: 81054 WC: 1201SDR SWIA2023060900501Unknown · scratchedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA73636-SRM 53-10-01/AD01 N144SY,MXCODEID59214-PR - ON PUSH GROUND CREW NOTICED A SCRATCH ON LEFT SIDE OF AIRCRAFT BELOW THE SKYWEST LOGO. FOUND DAMAGE TO FWD FUSELAGE SKIN TO BE LESS THEN 20 PERCENT OF THICKNESS IN REF SDR CALA2023050301317Intercostal · brokenFLOOR STRUCTURE INTERCOSTAL BROKEN BTW STA 328 TO STA 360 BL11 (REF: AAR NR 99967560 REMOVED INTERCOSTAL BROKEN BTW STA 328 TO 360 BL11, LOCATED & DRILLED NEW INTERCOSTAL P/N 141A5410U148, INSTALLED NEW INTERCOS TAL IAW B737-900,SRM 51-40-02-0G-0, SRM 51-40-05SDR CALA2023050301316Intercostal · brokenFLOOR STRUCTURE INTERCOSTAL BROKEN BTW STA 328 TO 360 BLO (REF: AAR NR 99967559) REMOVED INTERCOSTAL BROKEN BTW STA 328 TO 360, LOCATED & DRILLED NEW INTERCOSTAL P/N: 141A5410U147, INSTALLED NEW INTERCOSTAL, I AW B737-900, SRM 51-40-02-0G-0, SRM 51-40-05-0G-0.SDR QMLA2023050120035Unknown · damagedWHILE MOVING THE AIRCRAFT INTO THE HANGER, THE PILOT ACCIDENTALLY PUNCHED A HOLE IN THE BELLY BEHIND THE AFT CROSS TUBE ON THE #2 SIDE FROM THE HELIPORTER.
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