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 SWIA202266155None · elongatedLH AFT WINDSCREEN INBD AND OTBD CHUTE MOUNT BRACKETS ELONGATED. (C-CHECK RO 7/24/2022) REMOVED AND REPLACED INBD CHUTE MOUNT BRACKET WITH NEW, REF. SRM 51-40-08. COMPLIED WITH ETD2022-170-023496 FOR OTBD WINDSCREEN CHUTE MOUNT BRACKET. APPLIED SURFACE SDR SWIA202266154None · corrodedFWD WET AREA HAS CORROSION ON LH DOUBLER AT FR 19 AS MARKED. (C-CHECK RO 7/23/2022) REMOVED AND REPLACED FWD WET AREA LH DOUBLER AT FR 19, REF SRM 51-40-08.SDR CALA2022070801678Repair · discoveredREF. NR 9816104, "STA 706 FRAME DISCOVERED WITH SECTIONS OF HORIZONTAL FLANGE PREVIOUS REWORKED THAT DOES NOT COMPLY WITH SRM." AIRCRAFT REACHING 50,000 TOTAL AIRFRAME FLIGHT CYCLES". REF. ECRA 5310-08031 PART 1 STEP 14. INITIATE A DTA DIP TO READ AS FOLLOWS:SDR CALA2022070801676Housing · corrodedB757-53-3-0479: BS 333 LH CORROSION AROUND FLIGHT CONTROL CABLE HOUSING. TRANSCRIBED FROM HAECO GSO NRC 9282788 MAT ID 7075.0 .040 PN 141N5170-13 PO 973010.1, FAB''D AND INSTALLED IAW B757 200 SRM 51-40-02 AND BOEING DWG 141M5170 IAW BOEING DWG 14145170 REV SDR GTIA2022070736512Floor Panel · corrodedFLOOR PANEL 262LG FOUND WITH CORROSION, RAF 293443301 OPENED.-VERIFIED NR # 5001164139-0030 NAD TASK CARD 1003765801-0010. HOT BOND REPAIR WAS PERFORMED ON 262LG PANEL AS PER SPIRIT EO 5342-2233 REV. 00.SDR MK1Y20220706008Skin Panel · corrodedCENTER WING SECTION, UPPER CHORD AREA, STA 955, RBL 11.00: DURING CONVERSION WORK AT IAI, A CORROSION WAS FOUND AT DATUM LOCATION ON SKIN PANEL NO.1 OF CENTER WING, PRESSURE DECK WEB, AND UPPER CHORD OF REAR SPAR OF CENTER WING. THE SKIN AND WEB WERE BLENDED ASDR MK1Y20220706006Skin · damagedDURING MAINTENANCE INSPECTION LIGHTNING STRIKES WERE DISCOVERED ON THE EXTERNAL FUSELAGE SKIN BETWEEN STA 368 AND STA 412, STR-28L – STR-30L. THE LIGHTNING STRIKES WERE BLENDED OUT. THE BLEND OUT ARE LOCATED COMMON TO THE EXISTING FASTENERS. AFTSDR 2022FA0000359None · malfunctionedTHE MAGNETIC TIMING HOUSING MAGNETIC SENSOR FAILED DURING FLIGHT CAUSING COMPLETE LOSS OF LEFT ENGINE ELECTRONIC IGNITION. INITIALLY, ENGINE ROUGHNESS WAS NOTED BEFORE COMPLETE FAILURE. ELECTRONIC IGNITION WAS TURNED OFF BUT WOULD NOT COME BACK ON LINE. FLIGHTSDR IXXA2022070502Skin Panel · crackedL/W L/E UPPER FWD SURFACE CRACKED AT #1 SLAT O/B MAIN TRACK CUTOUTSDR DALA2023050903624Unknown · unknownSHIP 3319 LIGHTNING STRIKE ON FASTENER FRAME 73 STRINGER 51L. CORRECTIVE ACTION: FASTENER (TEMPORARY REPAIR) REMOVED IAW A330 SRM 53-41-11. PERFORMED ROTARY PROBE PER NTM 51-10-01. NO DEFECTS NOTED. HOLE WITH NO CRACKS INDICATION = 0.157", COLD EXPAND ACCOMPLISDR DALA2023050903623Unknown · unknownSHIP 3319 LIGHTNING STRIKE 3" AFT OF FR 75 5" DOWN OF STR 51L. CORRECTIVE ACTION: FASTENER (TEMPORARY REPAIR) REMOVED IAW A330 SRM 53-41-11. PERFORMED ROTARY PROBE. NO DEFECTS NOTED. HOLE WITH NO CRACKS INDICATION = 0.159", COLD EXPAND ACCOMPLISHED PER A330 SRSDR CALA2022070601654Fitting · noneLH SIDEWALL KEEL BEAM HOLE L13 HAS ELONGATED HOLE THROUGH THE FI TTING AND KEEL BEAM PER NR 9290570/26570 GEN BY V080280 INTERIM REPAIR ACCOMPLISHED IAW ECRA 5330-06955.SEE LOG PAGE 896 0036 FOR REPAIR DETAILS AND DIP LIMITS.SDR CALA2022070601652Fitting · corrodedRH FR68 FWD FACE AND STR23 APROX. HAVE A HOLE WITH CORROSION. FA BRICATE RH FR68 STR23 EXTEND REPAIR FITTING AS REQUIRED PER HAEC O LCQ NON ROUTINES 9291028/27028 AND 9291071/27071 PER HAECO LCQ GENERATED BY V061682/V061742 STR22 RH - 23 RH PER PART 2 OF THE LSDR SWIA202266149None · elongatedL/H AFT WINDSCREEN FRAME 84 OUTBD UPPER MOUNT ELONGATED (C-CHECK RO 7/23/2022) PERFORMED TEMPORARY REPAIR TO L/H AFT WINDSCREEN FRAME 84 OUTBD UPPER MOUNT REF ETD2022-170-023331. THIS TEMPORARY REPAIR IS VALID FOR 7500FC AS OF JUL 13, 2022.SDR CALA2022070401637Floor Support · corrodedSUPPORT TASK: 1602 MAIN CABIN STA 650 RBL25 FLOOR SUPPORT HAS CORROSION. TRANSCRIBED FROM HAECO GSO NRC 9282540SDR YENA2022070500650None · noneDURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION ON SUPPORT PANEL, LOCATED BTW FR88 - FR90 AND +Y=1100 AT PASSENGER FLOOR INTERNAL STRUCTURE (W2); CMOR: REPLACE PER EMB190 SRM 51-41-02, SRM 51-42-01 AND SRM 51-43-01. ACCOMPLISHED ON TECH OPSDR SWIA202266152None · elongatedR/H AFT WINDSCREEN FRAME 84 OTBD UPPER MOUNT ELONGATED (C-CHECK RO 7/23/2022) REMOVED AND REPLACED R/H AFT WINDSCREEN FRAME 84 OTBD UPPER MOUNT REF SRM 51-40-08 AND RESTORED SURFACE PROTECTION REF SRM 51-23-06SDR SWIA202266151None · elongatedR/H AFT WINDSCREEN FRAME 84 INBD UPPER MOUNT ELONGATED (C-CHECK RO 7/23/2022) REMOVED AND REPLACED R/H AFT WINDSCREEN FRAME 84 INBD UPPER MOUNT. REF SRM 51-40-08.SDR SWIA202266150None · elongatedL/H AFT WINDSCREEN FRAME 84 INBD UPPER MOUNT ELONGATED (C-CHECK RO 7/23/2022) REMOVED AND REPLACED L/H AFT WINDSCREEN FRAME 84 INBD UPPER MOUNT, REF SRM 51-40-08.SDR YENA2022070500655None · noneDURING HEAVY MAINTENANCE, SECONDARY NRC IN REF. NRC 00215 AFTER SEALANT REMOVAL, FOUND CORROSION ON SKIN BOTTOM PANEL, FRAME 100; SUMMARY: SKIN BOTTOM PANEL AT FRAME 100 WAS REPAIRED PER EC NO: E22-508-01, ETI-190-22-608 REV: 2 AND EO L01047 REV: IR. WORK ACCOSDR YENA2022070500654None · noneDURING HEAVY MAINTENANCE, CORROSION ON SHEAR CLIP OVER FR-86 BTW STGR 29L / 29R AT AFT CARGO COMP; REF TOMX W/O 1965 NR 00271 - CORROSION ON SHEAR CLIP OVER FR-86 BTW STGR-29L / 29R OUT OF LIMITS. REPLACED PER EMB 190 SRM 51-41-01 & SRM 51-41-02.SDR YENA2022070500651None · noneDURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEAR PANEL, LOCATED BTW -Y=950 AND FR87 - FR88 AT PASSENGER FLOOR INTERNAL STRUCTURE (W2); CMOR: REPLACE PER EMB190 SRM 51-42-01, SRM 51-42-02 AND SRM 51-43-03. WORK ACCOMPLISHED ON TECHOSDR YENA2022070500649None · noneDURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION ON FLOOR BEAM, LOCATED BTW FR84 AND -Y=330 AT PASSENGER FLOOR INTERNAL STRUCTURE (W2); CMOR: REPAIR PER EC NO: E22-494-01, ETI-190-22-599 REV 1, ETD2022-190-02094 REV.: A AND EMB190 SRM 53-23SDR YENA2022070500647None · noneDURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEAR PANEL, LOCATED BTW +Y=600 TO +Y=950 AND FR87 - FR88 AT PASSENGER FLOOR INTERNAL STRUCTURE (W2); CMOR: REPLACE PER EMB190 SRM 51-42-01, SRM 51-42-02 AND SRM 51-43-03. (CONSIDERED AS ASDR YENA2022070500648None · noneDURING HEAVY MAINTENANCE, INITIAL INSPECTION CPCP FINDING: CORROSION ON SHEAR PANEL, LOCATED BTW -Y=150 AND FR87 - FR88 AT PASSENGER FLOOR INTERNAL STRUCTURE (W2); CMOR: REPLACE PER EMB190 SRM 51-42-01 AND SRM 51-43-03. WORK ACCOMPLISHED ON TECH OPS W/O N328JBSDR YENA2022070500646None · noneDURING HEAVY MAINTENANCE, SEVERAL CORROSION POINTS ON SUPPORT, FLOOR-FEWD, FUS, AL OVER FR-16 AND Y-1162; ALL WORK ACCOMPLISHED ON TOMEX NRC 00209, CORROSION ON SUPPORT, FLOOR-FEWD, FUS, AL OVER FR-16 AND Y-1162 WAS REMOVED AND EVALUATED, THEREFORE IT IS OUT SDR CALA2022070401635Intercostal · corrodedSUPPORT TASK: MAIN CABIN STA 324-345 LBL20 INTERCOSTAL HAS CORROSION ON UPPER SURFACE. TRANSCRIBED FROM HAECO GSO NRC 9282558SDR SWIA202266404None · corrodedCORROSION FOUND ON FRAME AT FS 327.763 BETWEEN INTERCOSTALS DD4 AND DD5 (C-CHECK RO 8/31/2022) BLENDED FRAME AT FS 327.763 BETWEEN INTERCOSTALS DD4 AND DD5 REF CRJ 200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 52-00-00. REMOVED AND: INSTSDR JJBA20220721020Skin Panel · corrodedCORROSION FOUND ON INTERNAL SKIN AN ANTENNA DOUBLER BTW STR 21L-21R BTW FR 68-69. AFTER CORROSION INVESTIGATION ON SKIN AT ANTENNA LOCATION BTW FR 68-69 AND STR 21L-21R CRACKS FOUND AROUND RIVET HOLE AND REPAIR IS REQUIRED. SKIN AT FR 68-69 BTW STR 21-21R REPASDR K11A2022070600137Frame · crackedCRACK FOUND ON FUSELAGE FRAME WEB AT SUPPORT BRACKET INBOARD ATTACH RIVET AT STA 727B BETWEEN STRINGERS 8L AND 9LSDR DALA2022070504672None · noneSHIP 664 DENTS ON FRAME BTW STA 1520 AND S- 27L TO S- 25L AT AFT CARGO COMP. CORRECTIVE ACTION: SUMMARY OF NRC 00236: DENT ON FRAME STA 1520 S-27L TO S-25L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2301918)SDR DALA2022070504671None · noneSHIP 664 DENTS ON FRAME BTW STA 1520 AND S- 27L TO S- 25L AT AFT CARGO COMP. CORRECTIVE ACTION: SUMMARY OF NRC 00236: DENT ON FRAME STA 1520 S-27L TO S-25L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2301911)SDR EVCA20220701001Stiffener · crackedRH CONTROL COLUMN SKIN CRACKED AT UPPER RIVET. AFT RH CONTROL COLUMN STIFFENER CRACKED.SDR 2022FA0000327None · noneENGINE WAS REMOVED FROM THE AIRCRAFT AND BROUGHT TO US BECAUSE IT STARTED RUNNING RUFF. UPON DISASSEMBLY WE FOUND A PUSHROD DRIVEN THROUGH THE ROCKER ARM. WE FOUND THREE HYDRAULIC LIFTERS SEVERELY WORN ON THE SURFACE THAT CONTACTS THE CAMSHAFT. THE SNAP RING TSDR FDEA202206301750None · unknownAIRCRAFT REPAIR ASSESSMENT : EXISTING FLOOR BEAM REPAIR FOUND ON AFT CARGO COMPARTMENT AT FR 59, BTW -Y805 ~ -Y1470 POSITION. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: A300/A310 RPR IDENT&SUPPLEMENTAL MX REQ(SMR) TRK, INSPECTION OF EXSDR CALA2022070401631Skin · crackedAD 2019-11-02 EA 5310-06900 REV D - RH UNDERWING LONGERON FUSELAGE SKIN 2EA HOLE FOUND CRACK TRANSFER REF. NON-ROUTINE HX NRC WO.856658 AND ORIGINATED BY EMP NO. V893003 EA 5310-06900 REV D OP 012 RH BS 1035 UNDERWING LONGERON ECRA 5331-02907 REV - PART 2, DIPSDR EE4Y2022063015861Frame · crackedDURING THE STRUCTURAL INSPECTION PER 531135-01-2-001 MPD, IT WAS FOUND LH WINDSHIELD SIDE POST UPPER ATTACHMENT AT FRAME 4 WITH A HOLE WITH CRACK INDICATION AND FITTING WITH A DOUBLE HOLE AND FRAME SECTION WITH TOOL MARK. . DUE TO THIS FACT DETAILS WERE SENT TSDR JR2R8563103Doubler · corrodedRH FWD FLOOR DOUBLER CORRODEDSDR 2022FA0000320None · noneCFM56-5B AFT ENGINE MOUNT WITH UNUSUAL DAMAGES ON BARREL NUT HOLE LOCATION. DAMAGES CAME FROM AN INCORRECT INSTALLATION OF BARREL NUTS. ALL THE INFORMATION ABOUT THE EVENT IS RECORDED IN QA-22055SDR ABXA2022062974None · noneLAV SERVICE DOOR WAS DISCOVERED OPEN DURING PUSH BACK. GROUND PERSONNEL WERE UNABLE TO CLOSE THE DOOR. MAINTENANCE WAS CALLED TO SECURE DOOR PRIOR TO AIRCAFT DEPARTURE.SDR DALA2022070504667None · noneSHIP 664 DENT ON FRAME STA 1460 S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00262: DENT ON FRAME STA 1460 S-26L AT AFT CARGO COMPARTMENT. (C2) WAS REPAIRED PER B757-200 SRM. (2299217)SDR DALA2022070504666None · noneSHIP 664 DENT ON FRAME STA 1460 S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00262: DENT ON FRAME STA 1460 S-26L AT AFT CARGO COMPARTMENT. (C2) WAS REPAIRED PER B757-200 SRM. (2299205)SDR EVCA062922None · crackedTHERE IS A .50 INCH CIRCULAR CRACK ON THE UPPER RH CORNER OF THE HORIZONTAL STABILIZER.SDR SWIA202265973None · crackedREFERENCE CP 25064700-1 FOR ORIGINAL DISCREPANCY. CRACK ON RH COCKPIT WINDSHIELD/WINDOW SIDE POST (P/N 601R33223-2) REQUIRES REPAIR/REPLACEMENT. FORM M-337 HAS BEEN INITIATED.THIS IS CLASSIFIED AS A MAJOR REPAIR. (FILED CLOSED) REMOVED AND REPLACED RHS WISDR YENA2022062900636None · noneFLT#837, JFK-STI. (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO JFK) ' DURING TAKEOFF ROLL AT ROTATION SPEED, AIRCRAFT JERKED HARD LEFT. AFTER LIFT-OFF A SIGNIFICANT VIBRATION WAS FELT. SUSPECTED BLOWN TIRE. DECIDED NOT TO RETRACT LANDING GSDR 2022FA0000315None · noneENGINE MOUNT RECEIVED FOR MAINTENANCE WITH WRONG RETAINERS.SDR SWIA202266131None · crackedCOCKPIT FLOOR STRUCTURE ANGLE BRACKET CRACKED ON L/H FLOOR BEAM AT FRAME 12. (C-CHECK RO 7/13/2022) REMOVED AND REPLACED L/H FLOOR BEAM AT FRAME 12. PER REF SRM 51-40-08SDR SWIA202266130None · crackedCOCKPIT FLOOR STRUCTURE HAS CRACKED ANGLE AT FRAME 12 ON CENTER FLOOR BEAM. (C-CHECK RO 7/13/2022) / REMOVED AND REPLACED COCKPIT FLOOR STRUCTURE ANGLE AT FRAME 12 ON CENTER FLOOR BEAM, REF SRM 51-40-08SDR SWIA202266129None · corrodedFORWARD WET AREA L/H DOUBLER HAS CORROSION AT FRAME 19. (C-CHECK RO 7/13/2022) / REMOVED AND REPLACED FORWARD WET AREA L/H DOUBLER AT FRAME 19, REF SRM 51-40-08.SDR DALA2022063004558None · noneSHIP 664 DENT ON FRAME STA 1380 S-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00260: DENT ON FRAME STA 1380 S-26L AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2296457)
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