N5100X

Service difficulty reports not matched to an aircraft · 20

They name N5100X, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 n_number = 'N5100X' AND registry_match IS NULL
  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 20000501SH001Shutoff Valve · failedTRANSFER SHUTOFF VALVE IS BYPASSING FUEL THROUGH ELECTRICAL CONDUIT. TOP OF SOV BYPASSES FUEL THROUGH ''POTTING'' AND IS FOUND DOWNSTREAM OF ELECTRICAL CONDUIT WITNESS HOLES. SUBMITTER STATED THIS IS THE THIRD LEFT FUEL TRANSFER SOV TO BE REPLACED. FIRST, NFeb 20, 2000 · N5100X · Cndair CL6002B19 · Fuel StorageSDR 99ZZZX826Cowl · chafedRIGHT ENGINE, UPPER CORE COWL IS CHAFING ON OIL TANK LEVEL INDICATOR DUE TO IMPROPER POSITION OF LEVEL INDICATOR. CHAFE DAMAGE WAS CORRECTED BY BLENDING IAW RJ SRM CSP A-008. LANDINGS: 6,453.Jan 6, 1999 · N5100X · Cndair CL6002B19 · Engine Cowling SystemSDR 99ZZZX870Diaphragm · corrodedDURING CUSTOMER ELECTED NOSE LANDING GEAR INSPECTION UPON REMOVAL OF THE AXLE ASSY, FOUND EXCESSIVE CORROSION ON THE OUTER MATING SURFACES OF THE DIAPHRAGM ASSY. REPLACED DIAPHRAGM ASSY WITH A SERVICEABLE ASSY PER MESSIER DOWTY ENGINEERING. TOTAL PART CYCLESDec 14, 1998 · N5100X · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR 99ZZZX869Piston · corrodedDURING CUSTOMER ELECTED NOSE LANDING GEAR INSPECTION UPON REMOVAL OF THE AXLE ASSY, FOUND EXCESSIVE CORROSION ON THE INNER PIN BORE SURFACES WHERE THE AXLE ATTACH PIN ATTTACHES TO PISTON. ASSY WAS REPLACED WITH P/N 16120-1, S/N B15-3 PER MESSIER DOWTY ENGINEEDec 14, 1998 · N5100X · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR 99ZZZX868Axle Assy · corrodedDURING CUSTOMER ELECTED NOSE LANDING GEAR INSPECTION, UPON REMOVAL OF THE AXLE ASSY, FOUND EXCESSIVE CORROSION ON THE INNER PIN (ATTACH) BORE AND THE INNER SURFACE OF THE AXLE ASSY/PISTON MATING SURFACE. AXLE ASSY WAS REPLACED WITH P/N MESSIER DOWTY 16124-101Dec 14, 1998 · N5100X · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR 99ZZZX867Bearing · chafedDURING CUSTOMER ELECTED NOSE LANDING GEAR INTERNAL INSPECTION, FOUND NOSE LANDING GEAR LOWER STRUT BEARING CHAFING INTO THE INNER BORE SURFACE OF THE LANDING GEAR UPPER HOUSING P/N MESSIER DOWTY 16040 (NLG). REPAIRED DAMAGED UPPER HOUSING INNER BORE SURFACE IDec 14, 1998 · N5100X · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR 99ZZZX866Handle · corrodedDURING AIRCRAFT INSPECTION, FOUND THE CREW ESCAPE HATCH EXTERNAL HANDLE INNER ATTACH SURFACE AND HOUSING CORRODED. NO DAMAGE LIMITS LISTED. REPLACED HANDLE/HOUSING ASSY WITH A SERVICEABLE ASSY, P/N 601R33050-1, S/N 0419.Dec 14, 1998 · N5100X · Cndair CL6002B19 · Emergency ExitsSDR 98ZZZX3665Torque Box · crackedLEFT THRUST REVERSER TORQUE BOX IS CRACKED JUST UNDER FORWARD END OF LEFT SIDE, 6 O'CLOCK, SOUND ATTENUATING MATERIAL (SAM) SUPPORT BRACKET. CRACK WAS FOUND DURING ROUTINE ENGINE CHANGE MAINTENANCE PRACTICES.Sep 11, 1998 · N5100X · Cndair CL6002B19 · Engine Thrust ReverserSDR 98ZZZX3664Shaft · damagedDURING REMOVAL/INSTALLATION OF LT AND RT ENGINES, NOTED THAT AFT MOUNT SHAFTS AND AFT MOUNT FITTINGS FOR BOTH LT AND RT SIDES HAD CIRCUMFERENTIAL SCORING FROM COMING IN CONTACT WITH ONE ANOTHER. THE SHAFT AND FITTING ARE NOT TO COME IN CONTACT WITH EACH OTHERSep 11, 1998 · N5100X · Cndair CL6002B19 · Engine Oil Indicating SystemSDR 98ZZZX3663Shaft · damagedDURING REMOVAL/INSTALLATION OF LT AND RT ENGINES, NOTED THAT AFT MOUNT SHAFTS AND AFT MOUNT FITTINGS FOR BOTH LT AND RT SIDES HAD CIRCUMFERENTIAL SCORING FROM COMING IN CONTACT WITH ONE ANOTHER. THE SHAFT AND FITTING ARE NOT TO COME IN CONTACT WITH EACH OTHERSep 11, 1998 · N5100X · Cndair CL6002B19 · Engine Oil Indicating SystemSDR 98ZZZX2949Shaft · scoredDURING ENGINE REMOVAL, NOTED A FOULING CONDITION OCCURRING BETWEEN THE FITTING AND SHAFT ASSEMBLY. THE SHAFT HAS VISIBLE CONTACT IMPRESSIONS OF NO MEASURABLE DEPTH. THIS IS CAUSE FOR REJECTION PER RJ MM CHAPTER 71-22-01 PAGE 403 PARA. 2.A.(5). INSTALLED A NJul 2, 1998 · N5100X · Cndair CL6002B19 · Engine Mount SectionSDR 98ZZZX2948Shaft · scoredDURING ENGINE REMOVAL, NOTED A FOULING CONDITION OCCURRING BETWEEN THE FITTING AND SHAFT ASSY. THE SHAFT IS SCORED .0005 INCH TO .001 INCH IN DEPTH. THIS IS CAUSE FOR REJECTION PER RJ MM CHAPTER 71-22-01 PAGE 403 PARA 2.1.(5). INSTALLED A NEW SHAFT.Jul 2, 1998 · N5100X · Cndair CL6002B19 · Engine Mount SectionSDR 98ZZZX2947Fitting · chafedDURING ENGINE REMOVAL, NOTED A FOULING CONDITION OCCURRING BETWEEN THE FITTING AND SHAFT ASSY. THE SHAFT IS SCORED .0005 INCH TO .001 INCH IN DEPTH. THIS IS CAUSE FOR REJECTION PER RJ MM CHAPTER 71-22-01 PAGE 403 PARA 2.A.(5). INSTALLED A NEW FITTINGS.Jul 2, 1998 · N5100X · Cndair CL6002B19 · Engine Mount SectionSDR 98ZZZX2946Bearing · corrodedAT ENGINE REMOVAL, NOTED THE LARGE BEARINGS WERE CORRODED. INSTALLED NEW BEARINGS.Jul 2, 1998 · N5100X · Cndair CL6002B19 · Engine Mount SectionSDR 98ZZZX2945Bearing · corrodedAT ENGINE REMOVAL, NOTED THE SMALL BEARINGS WERE CORRODED. INSTALLED NEW BEARINGS.Jul 2, 1998 · N5100X · Cndair CL6002B19 · Engine Mount SectionSDR 98ZZZX2950Fitting · chafedDURING ENGINE REMOVAL, NOTED A FOULING (CONTACT) CONDITION OCCURRING BETWEEN THE FITTING AND SHAFT ASSEMBLY. THE SHAFT HAS VISIBLE CONTACT IMPRESSIONS OF NO MEASURABLE DEPTH. THIS IS CAUSE FOR REJECTION PER RJ MM CHAPTER 71-22-01 PAGE 403 PARA. 2.A.(5). INSJul 1, 1998 · N5100X · Cndair CL6002B19 · Engine Mount SectionSDR 96ZZZX3818Pcu Link · defectiveCREW REPORTED A HIGH PITCH NOISE COMING FROM THE RIGHT AILERON. INVESTIGATION PROVED THE AILERON PCU TO AILERON LINK WAS CHATTERING ON THE AILERON BOLT BUSHING. SPECIFICALLY, THE ANTI-ROTATION TABS OF THE LINK. THE BUSHINGS WERE REPLACED AS WELL AS THE LINKJul 3, 1996 · N5100X · Cndair CL6002B19 · Aileron Control SystemSDR 96ZZZX3723Sensor · brokenDURING ROUTINE BRAKE CHANGE, NOTICED THE BRAKE TEMPERATURE SENSOR WAS UNSERVICEABLE DUE TO A CRACK GOING ALL THE WAY AROUND THE BASE OF THE PROBE. THE SENSOR WS REPLACED AND THE BRAKE CHANGE WAS COMPLETED. AIRCRAFT WAS RETURNED TO SERVICE. SUBMITTER RECOMMEJun 24, 1996 · N5100X · Cndair CL6002B19 · Landing Gear Brake SystemSDR 96ZZZX757Thrust Reverser · crackedWHILE PERFORMING A BLOCKER DOOR REPAIR, NOTICED THE INNER BARREL AT THE 6 O'CLOCK POSITION HAD A 6-INCH LONG CRACK IN THE SHAPE OF THE LETTER 'L'. CONSIDERING THE PRELOADING PROBLEM ON THE BLOCKER DOOR AND APPARENT MISALIGNMENT OF THE BLOCKER DOOR MOUNTS AT PDec 3, 1995 · N5100X · Cndair CL6002B19 · Engine Thrust ReverserSDR 95ZZZX5652Light Assy · wires burnedTWELVE TO FIFTEEN MINUTES FROM HOME BASE, THE FLIGHT ATTENDANT SMELLED AN ELECTRICAL BURNING ODOR FROM THE REAR LAV AREA OF THE AIRCRAFT. UPON INVESTIGATING, SHE FOUND NO VISIBLE INDICATIONS. ON LANDING, MAINTENANCE WAS INFORMED AND THEN FOUND THE 4 FLUORESCSep 12, 1995 · N5100X · Cndair CL6002B19 · Passenger Compartment Lighting
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