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.

SDR DALA2016011000453Not Reported · corrodedCORROSION FOUND AT BS 915, RBL 11. C/W REPAIR IAW SRM 53-00-51.Jan 9, 2016 · N171DZ · Boeing 767332SDR DALA2016011000452Not Reported · corrodedCORROSION AT BS 915, LBL 11. C/W REPAIR IAW SRM 53-00-51.Jan 9, 2016 · N171DZ · Boeing 767332SDR CA160114001Cotter Pin · defective(CAN) IT WAS DISCOVERED WHEN SAFETY LOCKING A BOLT THAT A BATCH OF COTTER PINS WERE DEFECTIVE. THE PINS APPEAR TO BE BRITTLE AND WILL BREAK IF SPREAD. THIS COTTER PIN WAS PURCHASED.Jan 7, 2016 · Wsk M18ASDR ASOA2016010214344Floor Support · corrodedCORROSION FOUND ON LBL 9 FLOOR SUPPORT BETWEEN BS 1030-1034. CORROSION DETERMINED TO BE OUT OF LIMITS IAW SRM 53-61-43-101-001-A01. REPAIRED IAW EC/TC EO 700-53-0287 AND GREO 670-53-00-029, REV A.Jan 2, 2016 · N720EV · Cndair CL6002C10SDR SWIA201541745Panel · corrodedPANEL 832FL HAS SIGNS OF CORROSION AROUND MULTIPLE SCREW HOLES. R & R NEW PANEL 832 FL, IAW SRM.Dec 15, 2015 · N794SK · Cndair CL6002C10SDR SCNA20151207175Unknown · crackedCRACKED INBD AND OTBD FLANGE FS 727B, RBL 45.5. CUTOUT DAMAGE, HFECD FLAP PEENED, FABRICATED PARTS AND INSTALLED.Dec 7, 2015 · N710SY · Boeing 73773VSDR DALA2016010700081Structure · crackedDURING ER/A 496764-14, SECT II INSPECTION, A CRACK IS FOUND IN ER/A FIG 3 AREA C, HOLE DURING OPEN HOLE HFEC INSPECTION. CONFIGURED ACFT ON JACKING CONDITION IAW ERA NR 496764-14AD REVISION "E" AND "F" SECTION VII PART "A", AND AMM 07-11-00-581-001A. REPLACEDDec 5, 2015 · N348NW · Airbus A320212SDR DALA2015112807263Fastener · not reportedTWO FASTENERS ON ONE SIDE OF THE CUT LINE OF THE APB LOWER CHORD BETWEEN LONGERONS 26 LT AND 27 LT. FASTENERS WAS ATTENDED WITH ER/A 541554-14, REV ORIGINAL. RII COMPLETED.Nov 27, 2015 · N907DL · Doug MD88SDR DALA2015112807262Structure · damagedTWO FASTENERS ON ONE SIDE OF THE CUT LINE OF THE APB LOWER CHORD BETWEEN LONGERONS 26RT AND 27RT. CUT LINE OF THE APB LOWER CHORD BETWEEN LONGERONS 26RT AND 27RT WAS REPAIRED IAW ER/A 541554-14, REV ORIGINAL. RII COMPLETED.Nov 27, 2015 · N907DL · Doug MD88SDR YENA20151118573Door Sill · corrodedFLT 6415, MAIN CABIN AFT WET AREA L-2 DOOR SILL Y1732 CORRODED AT FRAME 66 TO FRAME 68. R & R L2 DOOR SILL IAW SRM 51-72-11 AND SRM 53-41-14.Nov 18, 2015 · N595JB · Airbus A320232SDR ASOA2015110114090Panel · damagedLIGHTNING STRIKE PANELS UNDER CABIN FLOORBOARD 231CLF REQUIRES REMOVAL TO C/W INSPECTION. REMOVED 3 LIGHTNING STRIKE PANELS UNDER 231CLF FOR INSPECTION IAW AMM 53-01-01-000-806. INSTALLED 3 LIGHTNING PROTECTION PANELS UNDER CABIN FLOORBOARD 231CLF IAW AMM 53Nov 1, 2015 · N856AS · Cndair CL6002B19SDR DALA2015102806592Not Reported · crackedU/T INSPECTION INDICATES CRACK RUNNING FWD OUT OF SUBJECT FASTENER HOLE. REPAIRED IAW ERA 540404-14AD.Oct 27, 2015 · N1605 · Boeing 767332SDR IPXA2015092793969Mount · corrodedINSPECTION TYPE:5YR, AFT LOWER EXTERNAL FUSELAGE, AFT RADIO ALTIMETER CAN CORRODED ON MOUNTING FLANGE INNER MATTING SURFACE. R & R CAN IAW SRM 51-40-21.Sep 25, 2015 · N125UP · Airbus A300F4622RSDR HALA2015092300196Unknown · vibrationUNUSUAL VIBRATION & NOISE UNDER MID GALLEY DECREASED WHEN FLAPS EXTENDED. ACFT WAS CLEAN CONFIGURATION WHEN VIB STARTED. INSPECTED ACFT IAW AMM 05-51-38, NO DEFECTS NOTED ALSO INSPECTED AIR CONDITION BATTERY, NO DEFECTS NOTED AND INSPECTED FWD CARGO RECIRCULSep 23, 2015 · N588HA · Boeing 7673CBSDR UHLA201509110738Doubler · damagedFWD CARGO CUTOUT LOWER BEAM AFT DOUBLER DAMAGED. R & R AFT DOUBLER IN FWD CARGO DOOR CUTOUT IAW SRM 51-40-02.Sep 11, 2015 · N858RW · Emb ERJ170100SESDR WVER2015081700011Not Reported · not reportedREPAIR TO FUSELAGE BS 280.00.Aug 17, 2015 · N903FJ · Cndair CL6002D24SDR DALA2015080604856Unknown · crackedCRACK ON AFT FRAME AND BEAM NR 8 L1 DOOR. INTERCOSTAL AND PRODUCTION DOUBLER WERE REPLACED IAW SRM 51-30-2 CRACK LENGTH 0.250.Aug 5, 2015 · N906DL · Doug MD88SDR USAR201507160001Structure · cracked(00163) A CRACK WAS FOUND AT THE UPPER FORWARD CORNER CLOSURE .300" LONG.Jul 14, 2015 · Beech A200CSDR UHLA201507110588Panel · corrodedPANEL 192CR HAS CORROSION AROUND SEVERAL SCREW HOLES. R & R SPACER.Jul 11, 2015 · N855RW · Emb ERJ170100SESDR QXEA2015070100354Seat Track · corrodedCORROSION FOUND IN VARIOUS LOCATION ON SEAT TRACK NR 5 . SEAT TRACK NR 6 FOUND TO BE WITHIN TOLERANCE OF SRM 53-20-49, FIG 201, SHEET 2, MAX DEPTH .005", UPPER CLAW AREA, DEEPEST DEPTH ON LOWER CLAW AREA .025". CHECKED WITH TUC DEPTH GAUGE NR 4745, DUE 2/28/Jun 22, 2015 · N434MK · Bombdr DHC8402SDR IPXA2015061590180Fastener · looseF/O EVAS MOUNTING BRACKET FASTENER NUTPLATES REQUIRE RE-POTTING INTO FLOOR. RESECURED EVAS MOUNTING BRACKET INSERTS IAW EO 2560-45126-G.Jun 15, 2015 · N257UP · Doug MD11FSDR ASOA2015070813292Not Reported · corrodedAFT SIDE BS 295 CORRODED AT STR 25R. REMOVED CORROSION ON FS 295 AT STR 25R IN REF TO SRM 51-21-06-001-001-A01. COMPLIED WITH EC/TC EA 32-2015-255.Jun 14, 2015 · N720EV · Cndair CL6002C10SDR ASOA2015070113215Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 36.20 JUST ABOVE WL 73.50 APPROXIMATELY 1.5 IN LENGTH 100 PERCENT FSH. FAILED NDT INSPECTION. C/W REO 601R-53-61-5498 P1. INSTALLED ALL REPAIR PARTS AT FS 621, BULKHEAD LBL 36 IAW REO 60Jun 3, 2015 · N884AS · Cndair CL6002B19SDR ASOA2015063013197Frame · corrodedCORROSION ON 605 FRAME FROM STR 27 TO STR 24L. FOUND CORROSION ON FS 605, FRAME TO BE OUT OF LIMITS IAW SRM 53-00-00. REMOVED FS 605, FRAME IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW SERVICEABLE FS 605, FRAME SECTOR AND REINFORCEMENT ANGLE IAW SRM 51-42-0Jun 2, 2015 · N884AS · Cndair CL6002B19SDR DALA2015051803417Receptacle · wornDURING CHECK, MAINTENANCE FOUND NUMEROUS ALIGNMENT PIN RECEPTICLES WORN. MAINTENANCE REPLACED THE ALIGNMENT PIN RECEPTICLES. LP 1952193.May 17, 2015 · N907DE · Doug MD88SDR QXEA2015051400238Rivet · corroded8 RIVETS IN STR 24S BETWEEN FRAMES X547 AND X564 HAVE CORRODED SHOP HEADS. COMPLETED FORM M-184. REMOVED 8 EA RIVETS ALONG STR 26S, REF SRM 51-42-05. INSTALLED 8 EA NEW RIVETS REF SRM 51-42-05. RESTORED FINISH TO AFFECTED AREA REF SRM 51-25-25 AND 51-21-10.May 11, 2015 · N419QX · Bombdr DHC8402SDR ASOA2015060312974Rivet · damagedBOTTOM OF LT COCKPIT DOOR POST IS CORRODED AND HAS RIVET HEAD MISSING BLENDED CORROSION ON BOTTOM LT COCKPIT DOOR POST IAW SRM 51-21-06-001-001-A01. REMOVED POST ANGLE BRACKET TO FOM IAW SRM 51-42-13-001-001-A01. INSTALLED NEW ANGLE BRACKET IAW EA 32-2015-2May 10, 2015 · N761ND · Cndair CL6002C10SDR WX0A2015050872568Unknown · vibrationAFTER TAKEOFF, FLIGHT ATTENDANT 2 & 4 REPORTED A RUBBER ODOR, BUT DISSIPATED. APPROX 40 MINUTES INTO FLIGHT, FLIGHT ATTENDANTS REPORTED EXCESSIVE NOISE & VIBRATION FROM ROW 33 & PROGRESSED AFT. ENG PARAMETERS WERE NOTED ON TREND AFTER AUTO-THROTTLES WERE TURApr 30, 2015 · N405NV · Doug DC983SDR DALA2015042903004Structure · corrodedCORROSION ON LOWER SILL LOCATED BETWEEN FRAME 66 TO FRAME 68 AT STR. 23L AT AFT GALLEY AREA, L=1", W=0.500", D=0.003". REPLACED LOWER SILL LEFT SIDE LOCATED BETWEEN FRAME 66 TO FRAME 68 AT LEVEL STR 23L AT AFT GALLEY AREA IAW STEP 51-72-11 AND DWG D53480505.Apr 28, 2015 · N355NW · Airbus A320212SDR DALA2015042902998Structure · corrodedCORROSION ON LOWER SILL BETWEEN FRAME 66 TO FRAME 68 AT STR 23R AT AFT GALLEY AREA L=2", W=1", D=0.002. REPLACED LOWER SILL BETWEEN FRAME 66 TO FRAME 68 AT STR 23R AT AFT GALLEY AREA IAW SRM 51-72-11 AND DWG D53480019. MEASURES OF DAMAGE AREA ARE L=2.886", WApr 28, 2015 · N340NW · Airbus A320212SDR ASOA2015051312807Intercostal · corrodedINTERCOSTAL AT BS 349 - 364, STR 27R HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED DAMAGED INTERCOSTAL. INSTALLED NEW INTERCOSTAL AT STR27R BETWEEN FS 349-364 IAW DWG SH670-32075, REV A AND SRM 51-42-06-001-001-A01, 51-42-21Apr 18, 2015 · N751EV · Cndair CL6002C10SDR SIMA20150328001Unknown · vibrationCLIMBING THROUGH FL300 AT APPROX .68M WITH AUTOPILOT ON, A SIGNIFICANT VIBRATION BEGAN IN BOTH CONTROL COLUMNS. AUTOPILOT WAS DISCONNECTED & THE VIBRATION CONTINUED. WE LEVELED OFF & SLOWED & THERE WAS NO CHANGE. WE BEGAN A DESCENT & THE VIBRATION SUBSIDED Mar 28, 2015 · N645AE · Emb EMB145LRSDR DALA2015032802491Static Port · damagedDURING INSPECTION, FOUND SCRATCH ON STATIC PORT LOCATED BETWEEN FR 3 TO FR 4 LT SIDE PANEL ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR PRINCIPLE 1 ON STATIC PORT LOCATED BETWEEN FR 3 TO FR 4 LT SIDE SKIN FUSELAGE IAW SRM 53-11-11, PARA 5A, FIG 203, PAGES 21Mar 27, 2015 · N345NW · Airbus A320212SDR DALA2015032802490Static Port · damagedDURING INSPECTION, FOUND SCRATCH ON STATIC PORT LOCATION BETWEEN FR 23 TO FR 24 RT SIDE ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR PRINCIPLE 1 ON STATIC PART LOCATED BETWEEN FR 23 TO FR 24 RT SIDE SKIN FUSELAGE IAW SRM 53-11-11, PARA 5A, FIG 203, PAGES 215Mar 27, 2015 · N345NW · Airbus A320212SDR DALA2015031602219Structure · crackedFORWARD OUTER CHORD RT HAS CRACK INDICATION USING HFEC AND LFEC INSPECTION AT THE BOTTOM FORWARD FASTENER OF THE SPLICE ANGLE. REPLACED RT SPLICE IAW ERA 533808-14AD.Mar 15, 2015 · N128DL · Boeing 767332SDR DALA2015090205392Structure · crackedDURING M-CHECK AND INSPECTION IAW AA 5716-01015, CRACKS WERE FOUND AT HOLE 'A' ON THE RT SIDE OF THE FUSELAGE AND HOLE 'B' AT THE LT INSPECTION AREA. STEPPED REAM HOLES TO REMOVED DAMAGE, AND INSTALLED REPAIR BUSHING IAW ER/A 531922-14.Mar 5, 2015 · N803NW · Airbus A330323SDR DALA2015022101534Beam · crackedCRACKS ON FWD AND AFT EDGE BEAM NR 1 AT FWD ENTRY DOOR. CRACKS ON FWD AND AFT EDGE BEAM 1 WERE REPAIRED IAW SRM 52-05, FIG 97 AND 98 SHEET 3.Feb 17, 2015 · N980DL · Doug MD88SDR DALA2015010600080Unknown · corrodedDURING INSPECTION, FOUND CORROSION ON SECTION-CONNECTING IN AFT CARGO FUSELAGE UNDERFLOOR LOCATED AT FR 67 AND STR 28L MEASURES L=3", W=0.100", D=0.002" APPROXIMATELY SSI 534144.Jan 5, 2015 · N328NW · Airbus A320211SDR CA141218021Fastener · sheared(CAN) DURING ABC STRUCTURAL INSPECTION CHECK MAINTENANCE NOTICED A SHEARED FASTENER AT LH FRAME STA 288 FWD SPAR BOX SECTION. RECTIFICATION: REPAIRED IAW FR-CO-103576. REMAINDER OF SHEARED FASTENER REMOVED. NDT (EDDY CURRENT) CARRIED OUT TO ENSURE NO FURTHEDec 16, 2014 · Beech 1900DSDR CA141203003Fastener · sheared(CAN) DURING A SCHEDULED STRUCTURAL INSPECTION OF FUSELAGE BS 288, A CHECK WAS CARRIED OUT FOR STRESSED AND MISSING FASTENERS ON THE LOWER FUSELAGE BULKHEAD, PN 114-430094-13 OR -15. DURING THIS INSPECTION OF THE FUSELAGE, MAINTENANCE NOTICED A SHEARED HI-LOKDec 3, 2014 · Beech 1900DSDR DALA2014120506418Structure · corrodedCORROSION IN AFT CARGO BILGE AREA, BS 1231 L29R-28R, FWD AND AFT OF FORMER. REMOVED THE CORROSION AND EVALUATED MAT AT STA 1231, FROM L-29R-28R ON FORMER. ORIG MATERIAL .080, REMAINING MATERIAL .050, MAT LOSS .030 AND FOUND TO BE OUT OF LIMIT IAW SRM 53-01, Dec 3, 2014 · N905DL · Doug MD88SDR DALA2014120406416Unknown · crackedLT AFT FUSELAGE BS 1380 IS CRACKED AT FASTENER APPROXIMATELY 12" ABOVE PYLON. ACCOMPLISHED WORK STEPS OF PRI 531053-14, REV 0 AND COMPLIED WITH ER/A 531053-14, REV ENTERED AND DEFERED FOR SDR REPORTING.Dec 3, 2014 · N991DL · Doug MD88SDR QXEA2014120200977Structure · corrodedANGLES CENTER FUSELAGE PN 85329542-116, COMMON TO MACHINED WEB AT X26.70 AND ACFT SKIN BETWEEN STR 23P AND STR 25P AND PN 85329542-115 COMMON TO MACHINED WEB AT X6.700 AND ACFT SKIN BETWEEN STR 23P AND STR 25P SHOWS EVIDENCE OF HEAVY PITTING CORROSION. EVALUATNov 25, 2014 · N416QX · Bombdr DHC8402SDR QXEA2014120200974Structure · corrodedCORROSION UNDER FINISH OF RT STRAKE LOWER MOUNTING AREAS. CORROSION UNDER FINISH OF RT STRAKE LOWER MOUNTING AREAS BLENDED/REMOVED REF SRM 51-21-00. C/W ET INSP ON REWORKED AREAS AS MARKED REF NDTM PT1 51-00-06. NO DEFECTS NOTED. FINISH REWORED TO REWORK ARNov 25, 2014 · N416QX · Bombdr DHC8402SDR SWIA201440286Visor · failedVISOR PANEL 326AR FAILED GAP CHECK, C-CHECK, RECOUNTERED VISOR PANEL 326AR REF REO. GAP CHECKS GOOD.Nov 23, 2014 · N427SW · Cndair CL6002B19SDR QXEA2014120200975Structure · corrodedLEFT STRAKE AREA ON FUSELAGE AT AFT ATTACH LUGS UPPER AND LOWER HAVE CORROSION AROUND SCREW HOLE. CORROSION UNDER LT STRAKE AT 2 AFT ATTACH LUG UPPER & LOWER LOCATIONS REMOVED/BLENDED REF SRM 51-21-00. C/W ET INSP & UT THICK TEST ON REWORKED AREAS REF NDTM PNov 23, 2014 · N416QX · Bombdr DHC8402SDR QXEA2014112200922Structure · damagedFOUND MAIN CABIN DOOR HEAD BUMPER CRACKED AND BROKEN.Nov 22, 2014 · N448QX · Bombdr DHC8402SDR SWIA201439995Panel · damagedPANEL 174DZ HAS AN OVERSIZED HOLE. C-CHECK, PANEL 174DZ WAS REPAIRED IAW EA.Nov 13, 2014 · N611SK · Cndair CL6002C10SDR SWIA201440041Panel · crackedPANEL 222CLC, HAS CRACKS AROUND SCREW HOLE. REPAIRED PANEL IAW EA.Nov 7, 2014 · N984CA · Cndair CL6002B19SDR SWIA201439896Panel · chafedSTUB FAIRING PANEL 172DR IS CHAFED IN MULTIPLE PLACES. BLENDED STUB FAIRING 172DR IN MULTIPLE PLACES IAW SRM AND EA.Oct 27, 2014 · N751SK · Cndair CL6002C10
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