JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 04FDEA02878Ventilator Panel · crackedNUMBER 3 PYLON PRECOOLER PANEL CRACKED AT WELD CORNER. WELD REPAIRED IN NEW PIECE OF MATERIAL IAW FEDEX EA 8-5480-81477 NACELLE/PYLONS NR 3 ENGINE VENTILATOR PANELS REPAIR. REFERENCE NON-ROUTINE NR N00798.SDR 04FDEA02855Ventilator Panel · crackedNR 3 PYLON TOP PANEL 487DR HAS THREE AREAS OF CRACKS. REPAIRED VENTILATOR ASSY P/N AUB7054-501 IAW FEDEX EA 8-5480-77611. LOCATED AND DRILLED VENTILATOR ASSY IAW DC10 SRM 51-31-01 VOL II. VENTILATOR ASSEMBLY TO BE INSTALLED UNDER FEDEX OPS 43R-FIT. REFERESDR UPS04443312Web · crackedINSPECTION TYPE: C, NR 2 PYLON - DURING ACCOMPLISHMENT EO ON AFT LOWER SPAR WEB, 1EA NON STANDARD REPAIR PATCH FOUND INSTALLED ON LOWER SPAR WEB JUST AFT OF REAR END MOUNT BULKHEAD. DEFECTIVE AREA AFT LOWER SPAR WEB REPAIR CARRIED OUT AS PER SRM 54-10-03 FIG SDR A6WA200460045Fairing · corrodedNR 1 ENGINE PYLON NOSE FAIRING NR 451 AT FORWARD EDGE HAS FRETTING DAMAGE. REPAIR IN PROGRESS. (M)SDR A6WA200460044Fairing · damagedFOUND NR 4 ENGINE PYLON NOSE FAIRING NR 484B FORWARD EDGE HAS FRETTING DAMAGE, REPAIR IN PROGRESS. (M)SDR UIEA200400162Pylon · crackedDURING SCHEDULED MAINTENANCE, NR 1 PYLON CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT STATION 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODSDR UIEA200400165Pylon · crackedDURING SCHEDULED MAINTENANCE, NR 4 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT FS 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-FS 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODISDR UIEA200400163Pylon · crackedDURING SCHEDULED MAINTENANCE, NR 2 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT FS 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-FS 254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODISDR UIEA200400164Pylon · crackedDURING SCHEDULED MAINTENANCE, NR 3 PYLON, CRACK DAMAGE WAS FOUND AT PRE-COOLER EXHAUST CUTOUT LOWER AFT CORNER AT FS 248. THE NR 3 STIFFENER WAS REINFORCED WITH A NEW LOWER REPAIR ANGLE FROM FS 235-254. THE RIB INSTALLATION AT NACELLE STATION 248 WAS MODIFIESDR 04FDEA02772Fitting · nickedLEFT HAND WING PYLON AFT ATTACH CLEVIS FITTING FORWARD LOBE HAS NICK. BLENDED AREA IAW DC10 SRM 57-00-01 VOL I, FOUND TO BE WITH IN LIMITS IAW DC10 SRM 57-00-01 VOL I, AND EA 8-5742-81464, PRIMED IAW DC10 SRM 51-21-01 VOL II. REMOVED APPROXIMATELY 0.060 INCHSDR 04FDEA02771Ventilator Panel · crackedNR 3 PYLON VENT PANEL 487 DR HAS SEVERAL CRACKS. ROUTED OUT CRACKS IN WELDED AREA, FABRICATED FILLER AND WELDED IAW FEDEX EA 8-5480-31457. REMOVED AND REPLACED CRACKED BRACKET, FABRICATED BRACKET IAW DOUGLAS DWG AUB 7054, REINSTALLED SKIN IAW DC10-30 SRM 51SDR 04FDEA02717Fitting · migratedNR 3 ENGINE PYLON AFT SPHERICAL BEARING MIGRATES. REMOVED SPHERICAL BEARING IAW DC10-30MM FEDEX 54-40-02 HONED HOLE IAW DC 10-30 FEDX AMM 54-40-02-2, REMOVED DRAIN LINE IAW FEDEX DC10-30 MM 54-10-00, REMOVED NUT STRIPS IAW DC10-30 FEDEX SRM 51-31-01, INST NSDR 04FDEA02680Fairing · dentedNR 1 ENGINE PYLON FAIRING DENTED, FORWARD PYLON TO NACELLE FAIRING. REPAIRED FAIRING BY REFORMING TO ORIGINAL CONTOUR AND INSPECTING USING HFEC PER AIRBUS NTM FOR CRACKS, NO CRACKS WERE NOTED. ALL WORK DONE PER EA 6-5480-73051A PART 3 AND A310 SRM 54-50-00 FSDR QXEA200400678Support Angle · crackedLEFT HAND LOWER COWL CONE SUPPORT ANGLE CRACKED. LEFT HAND SIDE AT ATTACH POINT TO TOP DECK. REMOVED CRACKED SUPPORT ANGLE. REPAIRED IAW RD 8/4-71-016.SDR USAA040586Pylon · crackedFOUND NACELLE WITH .5 INCH CRACK, LT ENGINE PYLON, NR 1527L ACCESS, OUTBOARD EDGE LIP. DOUBLER INSTALLED PER TYPICAL REPAIR 54-30-07. (M)SDR 04FDEA02643Pan · gougedNR 2 ENGINE RIGHT HAND FAN COWL INTERIOR HAS RUBBING APPROXIMATELY 8 INCHES ABOVE CENTER "U" BOLT. REMOVED CENTER "U" BOLT FITTING TO FOM. REMOVED DAMAGED SECTION OF PAN IAW DC10 SRM 51-35-01 VOL II. WELD REPAIRED IAW FEDEX EA 8-5410-81450. INSTALLED PAN ISDR USAA040541Pylon · corrodedCLT - FOUND PYLON CORRODED THREE .5 INCHE HOLES, RIGHT ENGINE PYLON. INSTALLED FILLER PER EA 95777. (M)SDR P5CA0401170Frame · crackedFRETTING & CRACKS IN FRAME AFT EDGE OF HYD COMPT. CUT OUT DAMAGE AREA PER SRM 53-10-04, FABRICATED ANGLE & PLATE INSTALLED PER SRM 53-10-02.SDR QXEA200400624Clip · crackedPDX - OUTBOARD SPLINE COWL CLIP IS CRACKED ALONG EDGE OF WELD IN RADIUS ON NR 1 NACELLE. REMOVED CRACKED CLEAT AT NR 1 OUTBOARD FORWARD POSITION. LOCALLY FABRICATED REPLACEMENT CLEAT FROM .025 INCH TITANIUM MATERIAL IAW RD 8/4-71-032. COMPLETED INSTALLATIONSDR QXEA200400623Pan · crackedRT PYLON PRESSURE PAN CRACKED AT AFT HYDRO, FITTING. REMOVED RT PYLON PRESSURE PAN. DRILLED UP AND INSTALLED INTERNAL DOUBLER IN NEW PAN. INSTALLED NEW PAN AND COMPLETED INSTALLATION AT FASTENERS THROUGH NEW PAN IAW SRM 51-42-06.SDR 04FDEA02259Strip · damagedCOMPY WITH EA 7-7110-80586 POWERPLANT - COWL NR 3 ENG COWL RUB STRIP REPAIR P/N 259-0175-135. COMPLIED WITH EA 7-7110-80586.SDR 2004UALA00686Fitting · gougedNR 1 PYLON AT NAC WL 160, AFT UPR DRAG FITTING IS GOUGED INSIDE BORE. OVERSIZED BORE AND INSTALLED OVERSIZE BUSHING.SDR C2XA04SH462Stiffener · chafedSHV - DURING C-CHECK THE NR 1 ENGINE UPPER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA04SH461Stiffener · chafedSHV - DURING C-CHECK THE NR 1 ENGINE LOWER COWLING AFT STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 04FDEA02030Truss Fitting · corrodedCOMPLY WITH EA 8-5420-7-79546B NACELLE/PYLON NR 1 ENGINE FWD TRUSS FITTING CORROSION REPAIR P/N AUB7000-501. COMPLIED WITH EA 8-5420-7-79546B.SDR 04FDEA01916Fitting · corrodedCOMPLY WITH EA8 -5420-79546 NR 1 PYLON FWD TRUSS FITTING CORROSION. COMPLIED WITH EA 8-5410-79546.SDR QXEA200400472Stiffener · crackedPDX - CRACK IN WEB STIFFENER FOR AFT CONE. STIFFENER IS AT 12 O'CLOCK POSITION ON CONE NR 1 LOWER ENGINE COWL. COMPLETED INSTALLATION OF FASTENER AS PER Q400 SRM 51-42-03.SDR 04FDEA01847Shackle · corrodedNR 2 ENGINE NR 1 SHACKLE HAS TWO AREAS OF PITTING CORROSION NEAR BUSHES. OFF AIRCRAFT PART. PROCURED NEW SHACKLE FOR NR 2 PYLON WING ATTACH POINTS. INSTALLED ON WC 64S0506, STA 485/RIB 7.SDR 04FDEA01846Shackle · corrodedNR 2 ENGINE O/B NR 4 SHACKLE HAS PITTING CORROSION NEAR BOTH UPPER AND LOWER BUSHES AT THREE PLACES. (OFF AIRCRAFT PART) PROCURED NEW FOR NR 2 PYLON OUTBOARD SHACKLE PYLON WING ATTACH POINTS, STA 539/RIB 8.SDR DL757040592Pin · crackedCRACKS WERE NOTED IN THE FUSE PINS ON THE NR 1 PYLON DIAGONAL BRACE. COMPLIED WITH ERA 091408-14AD.SDR QXEA200400426Fitting · crackedPDX - FORWARD LEFT CLEAT FOR NR 1 ENGINE SPLINE COWL CRACKED. REPAIRED IAE RD 8/4-71-032.SDR SWIA200413522Structure · crackedLEFT HYDRAULIC BAY SHEET METAL CRACKED AT BULKHEAD. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CRACKED BULKHEAD IAW 120 SRM 51-10-02 PAGE 2, PAR 2B.SDR QXEA200400380Support · chafedPDX - LEFT HAND NACELLE LOWER INBOARD ENGINE SUPPORT STRUT IS CHAFED ON INBOARD SIDE OF STRUT. APPLIED PROTECTIVE COATING PER RD 8-54-036.SDR UIEA200400096Fitting · crackedD-CHECK. REWORK OF STRUT NR 1 DIAGONAL BRACE LOWER SPAR FITTING, SP 747-54A2196 REV 1. DURING ACCOMPLISHMENT OF THE TERMINATING ACTION, DAMAGE WAS FOUND AT THE UPPER MOST FASTENER HOLE ON THE RIGHT SIDE OF THE FITTING AFT VERTICAL FLANGE. THE DEFECT WAS COMSDR QXEA200400344Rod · chafedPDX - NR 2 ENGINE RIGHT HAND LOWER STRUT IS CHAFED FROM HOLD OPEN ROD ON PANEL 424AR. REPAIRED IAW RD 8-54-038.SDR QXEA200400345Truss · chafedPDX - NR 1 ENGINE INBOARD LOWER TRUSS CHAFED 6 X .001 INCH ADJACENT TO FUEL FLOW TRANSMITTER. REPAIRED IAW RD 8-54-036.SDR QXEA200400343Strut · wornPDX- UPPER OB STRUT PROTECTIVE COATING IS WORN OFF 14 INCHES FORWARD OF FIREWALL ON IB SIDE. APPLIED EPOXY PRIMER IAW RD 8-54-036.SDR QXEA200400342Strut · scratchedPDX- UPPER IB STRUT PROTECTIVE COATING IS SCRATCHED 24 INCHES FORWARD OF FIREWALL. APPLIED EPOXY PRIMER IAW RD 8-54-036.SDR AUS20040391Door · missing(AUS) NR 2 ENGINE NACELLE/STRUT OB ACCESS DOOR MISSING.SDR CALA0400476Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 1 PYLON ANGLE JUST AFT OF I/B MIDSPAR ATTACH BOLT. A NEW ANGLE WAS INSTALLED IAW SRM 51-40-00.SDR UPS04842393Fitting · crackedINSPECTION TYPE: C1, NR 1 PYLON UPPER AFT END HAS PN 57567901 CRACKED AT YN 384.942. REMOVED CRACK FROM FITTING BY REMOVING INTEGRAL STIFFNER IAW UPS. ENGINEERING FILE NR DC8-54-20038 AND SAA SK 730-344.SDR CA040428001Access Door · cracked(CAN) DURING THE DAILY INSPECTION THE COWL INSPECTION DOOR HINGE WAS FOUND LOOSE ALLOWING THE DOOR TO HANG DOWN. UPON REMOVAL OF THE COWLING IT WAS FOUND THAT THE ATTACH FLANGE FOR THE COWL ACCESS DOOR HINGE WAS CRACKED ACROSS 75 PERCENT OF THE FLANGE LENGTH. SDR SWIA200413327Bracket · crackedRT HYDRAULIC PACK VERTICAL MOUNT BRACKET IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD HALF OF VERTICAL MOUNT BRACKET ASSY PER SRM 51-40-02.SDR 04FDEA001104Support · brokenON TAKEOFF AT 1200 FT AGL THE EGT ON NR 1 ENG WENT TO 960 DEGREES INDICATED VERY RAPIDLY. TOOK 4 THROTTLE WIDTHS TO BRING THE EGT BACK INTO PARAMETERS AND ENG RUNNING SMOOTLY. DUMPED APPROX 20K LBS OF FUEL. INITIAL VISUAL INSPECTION REVEALED SEVERAL BROKENSDR C2XA04SH235Stiffener · chafedSHV- DURING C-CHECK THE LEFT HAND ENGINE LOWER COWLING AFT EDGE STIFFENER WAS FOUND TO BE CHAFED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED STIFFENER IAW EMB 145 SRM 51-40-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 04FDEA00986Support · crackedNR 2 RIGHT AFT COWL ENGINE DRAIN LINE SUPPORT CRACKED. FABRICATED DRAIN LINE SUPPORT FROM 2024-T3 .032C BATCH 715298 AND INSTALLED IAW SRM 51-30-2 AT MAE.SDR 04FDEA00984Strip · tornPANEL 5531 CHAFE STRIP IS TORN. REMOVED AND REPLACED STRIP IAW SRM 51-30-2 AT MAE. FABBED FROM 301-25 .012SS BATCH 000705488.SDR 04FDEA00968Panel · missingON ARRIVAL WALKAROUND CHECK FOUND NR 2 ENGINE LEFT FWD LOWER PICKLE BARREL PANEL MISSING. RECEIVED PANEL AJC7077-1, PRE-DRILLED HOLES DO NOT LINE UP WITH STRUCTURES HOLES. COMPLIED WITH EA 8-5410-76625 PART 1. FLEW A/C TO IND FOR PERMANENT REPAIR. COMPLIEDSDR SWIA200413334Support Channel · crackedRIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL CRACKED AT INBOARD END. DISCOVERED DURING C-CHECK INSPECTION. REPLACED RIGHT HYDRAULIC RESERVOIR LOWER SUPPORT CHANNEL AT INBOARD IAW EMB120 SRM 51-10-02 SEC 2 ITEM C.SDR 04FDEA00892Nut Plate · damagedON LANDING ROLLOUT NR 3 WOULD NOT GO INTO REVERSE. DID NOT GET ANY LIGHTS FOR INDICATION OF REVERSE PRESS OR UNLOCK. BY DIRECTION OF MAINT TRIED TO CYCLE REVERSER ON TAXI IN, NO JOY. MEL 09APR04. RELEASED FOR SERVICE PER MEL/CDL: 78-01-01-A CATEGORY: A EXP
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