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 A6WA202207298242Door Sill · corroded*PAX DOOR LOWER SILL ANGLE CORRODED IN SEVERAL AREAS (MARKED) ***AIRCRAFT REMOVED FROM SERVICE *** REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21, AND DWG 601R31527 REV -AMSDR A6WA202207298241Frame Splice · corrodedFRAME FS605.0 HAS CORROSION STGR24L-23R ***AIRCRAFT REMOVED FROM SERVICE *** REMOVED AND REPLACED FS 605.0 LOWER FRAME SECTOR STGR 21L - 21R REF CRJ 200 SRM 51-42-06 , SRM 51-42-21 , BOMBARDIER DWG 601R36026 REV. AE AND DWG 601R35005 REV AGSDR SWIA202266435None · corrodedCORROSION ON AND AROUND DOME NUTS FOR FWD WI-FI ANTENNA BETWEEN FRAMES 21 AND 22 AND STRINGERS 27R AND 28R INSIDE FORWARD CARGO (C-CHECK RO 9/02/2022) REMOVED AND REPLACED DOUBLER AND 2 EA STIFFENERS BETWEEN FRAMES 21 AND 22 AND STRINGERS 27R AND 28R INSDR JJBA20220808007Skin Panel · corrodedFFI LH EXT SKIN, DENT FOUND AT FR 2 AND BTW STR 15L-17L. DENT ON LH SKIN AT FR FOUND OUT OF LIMITS. FF LH EXT SKIN AT FR 2 AND BTW STR 15L-17L, REPAIR DOUBLER MADE AND INSTALLED.SDR JJBA20220808006Doubler · crackedCORROSION SUSPECTED ON LOWER SKIN UNDER FWD RAD ALT ANTENNA DOUBLER. LOWER SKIN UNDER FWD RAD ALT #2 EXT ANTENNA DOUBLER BLENDED FOR INVESTIGATION (FOUND CORROSION). CUT-OUT C/OUT ON LOWER SKIN UNDER FWD RAD ALT #2. LOWER SKIN BTW FR 64-66 AND BTW STR 20L-20R SDR SWIA202266217None · crackedFOUND CRACK AT THE TOP SCREW HOLE ON THE AIRFRAME STRUCTURE ASSEMBLY BETWEEN RH WINDSHIELD AND SIDE WINDOW. (FILED CLOSED) REMOVED AND REPLACED RH WINDSHIELD/WINDOW SIDEPOST P/N 601R33223-2 IAW SRM 51-42-21 AND DWG# CC670-33055 REV F. WORK PERFORMED BY MHISDR ABXA2023050881Beam · crackedAMES NR 0496 - CABIN, STA 903.5 RBL89, RH INNER CHORD(STUB BEAM) TRANSITION RADIUS CRACKED(END MARKED). STUB BEAM REPAIRED PER ABX-EA-5300-0052-101 (REPAIR - INNER CHORD, STA 903.5, RBL89, B767). VENDOR DID NOT REPORT REPAIR TO ABX AIR. THIS WAS DICOVERED BY ASDR IXXA2022090402None · damagedTAIL COMPARTMENT RIGHT SIDE EWIS SUPPORT BRACKET UNDER CENTER STAB BOX AT STA 1798 DAMAGED REF ST-VAA RN B000205SDR SWIA202266341None · crackedL/H FRAME 52 L-ANGLE IS CRACKED THROUGH THE FASTENERS FWD OF THE L/H MLG WHEEL WELL. (C-CHECK RO 8/18/2022) REMOVED AND REPLACED L/H FRAME 52 L-ANGLE REF SRM 51-40-08SDR SWIA202266322None · corrodedCORROSION, AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 87 WHERE THE BEAM PASSES BETWEEN THE CENTER AND RH SHEAR PANELS. (C-CHECK RO 8/18/2022) / REMOVED AND REPLACED AFT WET AREA, ON RH LONGITUDINAL FLOOR BEAM AT FRAME 86 TO FRAME 89, REF SRM SDR UIEA2022072600782Intercostal · crackedCRACK ON INTERCOSTAL OF AFT CARGO COMPARTMENT FLOOR STRUCTURE AT STA 1590, RBL 27(<P>1) ACCOMPLISHED IAW EI T2022A53M-2058 REV 1 & DWG 65B06061 SH62 REV B & DWG 65B06061 SH 64 REV -. 2) JOB COMPLETED</P>)SDR UIEA2022072600783Intercostal · crackedCRACK ON INTERCOSTAL OF AFT CARGO COMPARTMENT FLOOR STRUCTURE AT STA 1590, LBL 27(1) ACCOMPLISHED IAW EI T2022A53M-2059 REV 1 & DWG 65B06061 SH 60 REV - & DWG 65B06061 SH 58 REV B. 2) JOB COMPLETED</P>)SDR 2A6D20220726001Floor Support · corrodedTHE UPPER T-CAP ON FRAME 3 AT (X FS 3150) (Z WL 1365) (Y BL 0) WAS FOUND TO HAVE CORROSION UNDER A NUTPLATE ON THE BOTTOM OF THE MAIN CABIN FLOOR. ALSO, THE FRAME 3 WEB AT (X FS 3150) (Z WL 1150) (Y BL 0) WAS FOUND TO HAVE DENT DAMAGE NEAR A STIFFENERSDR SWIA202266429None · dentedDENT MEASURING 1.625" W AND .025" D LOCATED 3.5" ABOVE STGR 18L AND .5" AFT OF FR 10. EVALUATE AND REPAIR OR ELIMINATE EVIDENCE USING STANDARD PRACTICES. SEE ADM# N607CZ-6931 (C-CHECK RO 9/02/2022) PERFROMED A PERMANENT REPAIR BY REMOVING AND REPLACING SDR JJBA20220824025None · noneCF2, L/H OMEGA BEAM #2 FOUND CRACKED AT 3 LOCATIONS ON INBD FLANGE. AFTER INVESTIGATION, 5 CRACKS FOUND. BEAM REPAIRED WITH 5 DOUBLERS.SDR CALA2022072501875Tat Probe · dentedDENT LOCATION OF IS APPROXIMATELY 4" AFT OF TAT PROBE AND 13" ABOVE. ACP''D 737 NDT EDDY CURRENT PART 6 51-00-00 PRECEDURE 23 FOUND NO CRACK EXTERIOR SKIN SURFACE. INSPECTED MEASUREMENTS OF 3" X 2 1/2" X 1/16.DENT IS WITHIN LIMITS.SDR R61A2022081200513Tie Clip · corrodedCORROSION - SHEAR CLIP AT FR88 STR27R/28R. REMOVED AND REPLACED SHEAR CLIP FR88 STRINGER 27-28R REF: EMB SRM 51-40-08,51-40-02.SDR R61A2022081200512Tie Clip · corrodedCORROSION - SHEAR CLIP AT FR88 STR27R/28R. : REMOVED AND REPLACED SHEAR CLIP FR 88 STRINGER 27-28R REF: EMB SRM 51-40-08,51-40-02.SDR CALA2022072501881Fitting · corrodedMAIN CABIN L2 DOOR AFT LOWER CORNER FITTING HAS CORROSION IN FWD AND AFT AREA. GENERATED AT HAECO LCQ PER NR 9296507 (42507) BY V935513 {A3NB-05-3-6059} REPLACED MAIN CABIN L2 DOOR AFT LOWER CORNER FITTING IAW A319 SR M 51-72-11-91-001. PERFORMED BY V937663 INSDR CALA2022072501879None · faultyTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/25/22.FILTER BYPASS LIGHT ON ENGINE 1 NORMAL ENG INDICATIONS #1 ENGINE FUEL FILTER DIFFERENTIAL PRESSURE WARNING SYSTEM. REPLACED #1 ENGINE FUEL FILTER BYPASS SWITCH (S241). EEC TEST CHECSDR GTIA2022072636555Doubler · dentedDENT ON FUSELAGE FRAME 71+6" STR 10L. RAF-01 2915008-02 GENERATED-FOUND DENT TO BE OUT OF LIMITS IAW A320 SRM 53-51-11-283-013. REPAIRED WITH DOUBLER AND FILLER IAW A320 SRM 53-51-11-300-036 FIG 001. REPAIR IS CAT B PERMANENT REPAIR. REQUIRES REINSPECTION AT 6SDR 2022FA0000397Filter Housing · leaking#2 ENGINE FILTER BOWL CRACKED. FOUND DURING AIRCRAFT SHUTDOWN. OIL LEAKING FROM FACE OF OIL FILTER BOWL. AIRCRAFT CYCLES, FILTER HOUSING TT, TC, TS_ AND ENGINE TC AND TS_ ARE ALL UNK. FORM WOULD NOT LET ME PUT UNK.SDR JJBA20220801038Floorbeam · crackedCF 1 LH OMEGA BEAM FOUND CRACKED AT FR 22 & 23. 2 REPAIR DOUBLERS ON LH CENTER FUSE 1 OMEGA BEAM, ON INBD FLANGE AT FR 22 & 23SDR JJBA20220801037Bear Strap · crackedCFII, CRACK FOUND ON LH OMEGA BEAM AT FR 24 AND FR 25. 2 REPAIR DOUBLERS ON LH CENTER FUSE 2 OMEGA BEAM, ON INBD FLANGE AT FR 24 & 25SDR IXXA2022072210Tie Clip · corrodedLWW SUPPORT ANGLE CORRODEDSDR 2022FA0000366None · failedDURING EXTERNAL LOAD OPERATIONS, THE AIRCRAFT TAIL ROTOR PEDALS MALFUNCTIONED. PILOT WAS ABLE TO PERFORM A RUN-ON LANDING WITH NO INJURIES OR DAMAGE TO THE AIRCRAFT.
AIRCRAFT IS OPERATED FROM THE LEFT HAND CREW SEAT DURING EXTERNAL LOAD OPERATION USING PARAVISDR 2022FA0000525Exhaust Valve · brokenDURING CRUISE FLIGHT ENGINE BEGAN TO RUN ROUGH AND MANIFOLD PRESSURE INCREASED. PILOT WAS ABLE TO RETURN TO THE HELIPAD AND MAKE A NORMAL LANDING. EXHAUST VALVE STEM WAS FOUND TO BE BROKEN AT THE BELL CURVE AND THE VALVE WAS IN THE CYLINDER BORE. SEVERE CYLINDSDR YENA2022072200673None · noneFLT#276, SJU-BDL. (AIRCRAFT PERFORMED AN AIR TURN BACK TO SJU) ' PASSING 9'000 FEET FAS REPORTED BURNING RUBBER SMELL THEY REPORTED THE SMELL STARTED AFTER T/O FUMES CHECKLIST COMPLETED SMELL D15 REDUCED SMELL NOTICED FROM ROW 3 FWD; PERFORMED FIM 05-50-00-81SDR GTIA2022072136551None · noneFUME EVENT IN FLIGHT. ISOLATED PACK #2 AND ALTERNATY PACK#1 AND SMELL DID NOT GO AWAY OR DISIPATED-PERFORMED IDLE RUN ON ENG #1 & ENG #2 WITH PACK #1 ON IAW AMM 7100-00. NO SMELL NOTED AT THIS TIME.SDR YENA2022072200702None · noneDURING HEAVY MAINTENANCE: CRACK: CROSSBEAM FOM HOLE H25 FR20 RH AFT AVIONICS COMPARTMENT L= 0.042" 1 O'CLOCK DIRECTION LOOKING AFT; REF AEROMAN NR 2022-317690 W/O: 2022 68/1: ACCOMPLISHED AD 2018-14-09-FAA-01 AND SB A320-53-1286.SDR YENA2022072200701None · noneDURING HEAVY MAINTENANCE: CRACK: CROSSBEAM FROM HOLE H26 AT FR20 RH AFT AVIONICS COMPARTMENT L= 0.063" 12 O'CLOCK DIRECTION LOOKING AFT; REF AEROMAN NR 2022-317692 W/O: 2022 68/1: ACCOMPLISHED FAA AD 2018-14-09 AND SB A320-53-1286.SDR YENA2022072200700None · noneDURING HEAVY MAINTENANCE: CRACK: FR20LH HOLE 26 AFT AVIONICS COMPARTMENT L=0.048" 6 O'CLOCK DIRECTION LOOKING FORWARD; REF AEROMAN NR 2022-317693 W/O: 2022 68/1: ACCOMPLISHED FAA AD 2018-14-09 AND SB A320-53-1286.SDR YENA2022072200699None · noneDURING HEAVY MAINTENANCE: CRACK: FR 16LH HOLE 1 LATERAL AVIONICS COMPARTMENT LH L=0.035" 1 O'CLOCK DIRECTION LOOKING FORWARD; REF AEROMAN NR 2022-317694 W/O: 2022 68/1: ACCOMPLISHED FAA AD 2018-14-09 AND SB A320-53-1286.SDR YENA2022072200698None · noneDURING HEAVY MAINTENANCE: CRACK: CROSSBEAM FROM HOLE H6 FR16LH AT LATERAL AVIONICS COMPARTMENT LH L=0.039" 1 O'CLOCK DIRECTION LOOKING FWD; REF AEROMAN NR 2022-317695 W/O: 2022 68/1: ACCOMPLISHED FAA AD 2018-14-09 AND SB A320-53-1286.SDR YENA2022072200690None · noneDURING HEAVY MAINTENANCE: CORROSION: STR43L FR64-65 AFT CARGO; REF AEROMAN NR 2022-317689 W/O: 2022 68/1: REPAIRED IAW SRM 53-41-13-300-004. CAT A REPAIR, NO FURTHER ACTION REQUIRED.SDR YENA2022072200688None · noneDURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE OF THE DOOR STOP N7 FR16LH AT LOWER INBOARD HOLE; REF AEROMAN NR 2022-317799 W/O:2022 68/1: REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS AT FR16LH LOWER INBOARD HOLE LEVEL OF DOOR STOP #7 IAW SRM 51-42-SDR YENA2022072200687None · noneDURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE OF THE DOOR STOP N7 FR16RH AT UPPER INBOARD HOLE; REF AEROMAN NR 2022-317801 W/O:2022 68/1: REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS AT FR16LHUPPER INBOARD HOLE LEVEL OF DOOR STOP #7 IAW SRM 51-42-1SDR YENA2022072200686None · noneDURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE OF THE DOOR STOP FR16RH AT LOWER INBOARD HOLE; REF AEROMAN NR 2022-317802 W/O:2022 68/1: REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS AT FR16RH LOWER INBOARD HOLE LEVEL OF DOOR STOP #7 IAW SRM 51-42-11,SDR YENA2022072200685None · noneDURING HEAVY MAINTENANCE: CRACK: FASTENER HOLE OF THE DOOR STOP FR16RH AT LOWER INBOARD HOLE; REF AEROMAN NR 2022-317798 W/O:2022 68/1: REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS AT FR16LH UPPER INBOARD HOLE LEVEL OF DOOR STOP #7 IAW SRM 51-42-11,SDR YENA2022072200670None · noneFLT#123, JFK-LAX. 'FUME EVENT DIRTY SOCK SMELL ON DESCENT FORM COMPLETED; REF INFO NOTICE 2017-T015 TSM 05-50-00-810-831-A TYPE 10 EVENT TRANSIENT/MISCELLANEOUS. THE ODOR DISSIPATED IN 10 MINUTES, WITH NO HISTORY OVER 25 FLIGHTS. EVENT ONLY OCCUR IN DESCENT. ASDR TAMF20220721023Door · crackedDURING AIRCRAFT LOADING PROCEDURE, THE AFT CARGO DOOR ANGLE PN/ F5347534721000 IN THE FUSELAGE WAS HIT.
ACTION TAKEN: PERFORMED TEMPORARY REPAIR IN ACCORDANCE WITH AIRBUS SRM 53-41-29-300-001SDR R61A2022080800486Shear Panel · corrodedDURING HEAVY CHECK FOUND REAR INTERNAL FUSELAGE, FOUND MID SHEAR PANEL CORRODED. REMOVED AND REPLACED MID SHEAR PANEL IAW EMB 170/175 SRM 51-42-01.SDR R61A2022080800485Shear Panel · corrodedDURING HEAVY CHECK FOUND REAR INTERNAL FUSELAGE, RH SHEAR PANEL BETWEEN FR87-FR88 CORRODED. REMOVED AND REPLACED SHEAR PANEL IAW EMB 170/175 SRM 51-42-01 AND 51-43-01.SDR R61A2022080800484Crossbeam · corrodedDURING HEAVY CHECK FOUND REAR INTERNAL FUSELAGE, BEAM AT FR90 CORRODED. REMOVED AND REPLACED BEAM IAW EMB 170/175 SRM 51-41-01 AND 51-43-01.SDR R61A2022080800483Gusset · corrodedDURING HEAVY CHECK FOUND REAR INTERNAL FUSELAGE, FOUND RH GUSSET AT FR90 AND RBL 18 CORRODED. REMOVED AND REPLACED GUSSET IAW EMB 170/175 SRM 51-41-02.SDR R61A2022080800482Gusset · corrodedDURING HEAVY CHECK FOUND REAR INTERNAL FUSELAGE, RH GUSSET AT FR90 CORRODED. REMOVED AND REPLACED RH GUSSET AT FR90 IAW EMB 170/175 SRM 51-41-02.SDR AALA202207256352Bulkhead · crackedAIRCRAFT IN BASE MAINTENANCE: 12 IN DIAGONAL CRACK LOWER SURFACE RIGHT MAIN LANDING GEAR BULKHEAD STA. 663 RIGHT BUT LINE 55. DOT 88-020. REPAIRED WITH BONDED REPAIR SRM 51-70-04.SDR YENA2022072200684None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 LH UPPER O/B SIDE POSITION OPEN FAS TENER HOLE DOOR STOP FITTING Ñ7; REF AEROMAN N/R 2022-355590, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP 7SDR YENA2022072200683None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 LH LOWER O/B SIDE POSITION OPEN FAS TENER HOLE DOOR STOP FITTING Ñ7; REF AEROMAN N/R 2022-355591, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP #SDR YENA2022072200682None · noneDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FRAME 16 L/H UPPER I/B SIDE POSITION OPEN FASTENER HOLE DOOR STOP FITTING Ñ7; REF AEROMAN N/R 2022-355592, REMOVED AND REPLACED INTERCOSTAL FITTING AND FASTENERS LOC BTW FR 15 TO FR 16 AT LEVEL OF DOOR STOP #
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