N16501

Service difficulty reports · 20

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N16501' AND registry_match = 'registration'
  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 C2XA07RI078Light · malfunctionedFLT 2154 - EWR - CREW REPORTED EMERGENCY EXIT ROW 9A LIGHTS INOPERATIVE. EWR MX RESET ACFT ELECTRIC POWER, AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE.Sep 10, 2007 · N16501 · Emb EMB135BJ · Emergency LightingSDR C2XA06CL080Rmu · smokeCLE FLIGHT NR 2786, CREW REPORTED SMOKE COMING FROM THE CO-PILOTS RMU WHILE TAXIING TO THE GATE. MAINTENANCE INSPECTED SYSTEM AND REMOVED AND REPLACED THE CO-PILOTS RMU. ALL OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE.Oct 1, 2006 · N16501 · Emb EMB135ER · Audio/Video MonitoringSDR C2XA06SH089Stringer · corrodedSHV - DURING C-CHECK STRINGER 20R WAS FOUND TO BE CORRODED AT FRAME 51. MAINTENANCE REMOVED THE DAMAGED AREA AND INSTALLED A DOUBLER REPAIR IAW EC 5310-01393. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 10, 2006 · N16501 · Emb EMB135ER · Fuselage Main, Longeron/StringerSDR C2XA06SH088Floorbeam · corrodedSHV - DURING C-CHECK THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FROM FRAME 20 TO 24. MAINTENANCE REMOVED THE DAMAGED AREA AND SPLICED IN A NEW BEAM SECTION IAW EC5320-01229. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.Sep 6, 2006 · N16501 · Emb EMB135ER · Fuselage Main, Floor BeamSDR CSXA06SH088Floor Support · corrodedDURING C-CHECK LT OMEGA BEAM FROM FR 20 TO 24 HAS CORROSION. MAINTENANCE SPLICED IN NEW LT OMEGA BEAM AT FR 18 TO 24 IAW EC5320-01229.Sep 6, 2006 · N16501 · Emb EMB135ER · Fuselage Miscellaneous StructureSDR C2XA06SH086Skin Panel · corrodedSHV - DURING C-CHECK CENTER FUSELAGE 3 EXTERNAL SKIN HAS AREA OF CORROSION AT STR 19R FR 50 HYDRAULIC LINE PASS THROUGH. MAINTENANCE REPAIRED CENTER 3 EXTERNAL SKIN AT STR R19 FR 50 IAW EC5330-01624. THE AIRCRAFT WAS APPROVED TO RETURN FOR SERVICE.Sep 1, 2006 · N16501 · Emb EMB135ER · Fuselage Main, Plate/SkinSDR C2XA06CL009Pdu · failedCLE FLIGHT 2056 - THE CREW REPORTED A -FLAP FAIL- MESSAGE ON THE EICAS UPON SELECTING FLAPS -22- DEGREES. FLAPS WERE STUCK AT THE -18- DEGREE POSITION. THE CREW DECLARED A EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THEJan 18, 2006 · N16501 · Emb EMB135ER · Trailing Edge Flap Control SystemSDR C2XA05CL017Heater · burnedCLE - FLIGHT 2226 THE CREW REPORTED A HOT BURNING SMELL IN THE CABIN AND COCKPIT. MAINTENANCE REPLACED THE NR 1 WINDSHIELD HEAT CONTROL BOX AND OPERATIONAL CHECKS GOOD.Mar 16, 2005 · N16501 · Emb EMB135ER · Windshield/Door Rain/Ice RemovalSDR C2XA04CL011Light · inoperativeCLE FLIGHT 2683 THE CREW REPORTED THE FIRST EMERGENCY AISLE PATH LIGHT STRIP WAS INOPERATIVE. MAINTENANCE REPLACED THE FIRST FLOOR LIGHT STRIP ASSEMBLY. OPERATIONAL CHECKS WERE GOOD.Feb 9, 2004 · N16501 · Emb EMB135ER · Emergency LightingSDR C2XA04TY006Attach Fitting · gougedDURING A SCHEDULED INSPECTION, GOUGES WERE FOUND ON THE INNER BEARING MATING SURFACES AT THE HORIZONTAL STABILIZER ATTACH POINT. MAINTENANCE ACCOMPLISHED A REAM TO FIRST OVERSIZE REPAIR IAW EC5530-01062, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEJan 10, 2004 · N16501 · Emb EMB135ER · Vertical Stabilizer, Attach FittingsSDR C2XA04TY005Angle · corrodedDURING A SCHEDULED INSPECTION CORROSION WAS FOUND ON THE GALLEY FLOOR RAMP ANGLE AT THE COMPOSITE CROSSBEAM. MAINTENANCE REMOVED AND REPLACED THE GALLEY FLOOR RAMP ANGLE IAW SRM 51-40-02, THE REPAIR WAS SATISFACTORY. THE AIRCRAFT WILL BE RELEASED UPON COMPLJan 10, 2004 · N16501 · Emb EMB120ER · Fuselage Miscellaneous StructureSDR C2XA01CL081Solenoid Valve · failedCLE FLIGHT 3960 AFTER LANDING GEAR RETRACTION CREW REPORTED LOUD AIR NOISE COMING FROM NOSE LANDING GEAR AREA. NOISE INCREASED WITH AIRSPEED. AIRCRAFT RETURNED TO CLEVELAND AND LANDED WITH OUT FURTHER PROBLEMS. MAINTENANCE REMOVED AND REPLACED NOSE LANDINApr 17, 2001 · N16501 · Emb EMB135ER · Landing Gear Door Retract SectionSDR C2XA01CL050Window · leakingCLE FLIGHT 3971 AFTER DEICING OF AIRCRAFT THE CREW REPORTED A HISS AND POP SOUND FOLLOWED BY SMOKE COMING FROM FIRST OFFICER''S SIDE PANEL. THE ENGINES WERE SHUT DOWN AND ALL ELECTRICAL POWER WAS TURN OFF. MAINTENANCE INSPECTED AND FOUND DEICE FLUID HAD LEAKMar 6, 2001 · N16501 · Emb EMB135ER · Flight Compartment WindowsSDR C2XA01CL025Light · inoperativeCLE - FLT 3949 - THE CREW REPORTED THE CABIN EMERGENCY LIGHTS WILL NOT ILLUMINATE AT ROWS 3 THROUGH 6. MAINTENANCE REPLACED THE LIGHT STRIP ASSEMBLY NR 3. THE AIRCRAFT WAS RELEASED FOR SERVICE. (M)Feb 15, 2001 · N16501 · Emb EMB135ER · Emergency LightingSDR C2XA01CL001Charger · inoperativeCLE - FLT 4135 - THE CREW REPORTED THAT THE 2ND AND 3RD SEAT OF AISLE PATH EMERGENCY LIGHTS WERE INOPERATIVE DURING THERE PREFLIGHT CHECK. MAINTENANCE REMOVED AND REPLACED THE NR 2 EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY IAW EMB135 MM 33-50-04. MAINTENANCE Jan 8, 2001 · N16501 · Emb EMB135ER · Emergency LightingSDR C2XAOOCL087Unknown · odorCREW REPORTED A STRONG SMELL OF JET FUMES WHEN THE APU RUNS PACK NR 1. MX RAN APU AND CHECKED FOR LEAKS, NO LEAKS FOUND ALSO RAN PACK AND NO FUMES WERE NOTED. A/C WAS RELEASED FOR SERVICE.Oct 27, 2000 · N16501 · Emb EMB135ER · Air Distribution SystemSDR C2XA00BT085Starter · failedROA - FLT 4009 - EN ROUTE CLE FROM RDU, CREW REPORTED NR 1 ENGINE INFLIGHT SHUTDOWN, OIL PRESSURE ERRATIC, OIL QUANTITY AT TWO QUARTS AIRCRAFT DIVERTED TO ROA AND LANDED UNEVETFULLY. MAINTNANCE DISPATCHED TO TROUBLESHOOT AND FOUND LEAKING NR 1 ENGINE AIR STAROct 2, 2000 · N16501 · Emb EMB135ER · Engine Start Valves/ControlsSDR C2XA00BT070Starter Gen · leakingROA - FLT 4009 - EN ROUTE CLE FROM RDU, CREW REPORTED NR 1 ENGINE IN FLIGHT SHUTDOWN, OIL PRESSURE ERRATIC, OIL QUANTITY AT TWO QUARTS AIRCRAFT DIVERTED TO ROA AND LANDED UNEVENTFULLY. MAINTENANCE DISPATCHED TO T/S AND FOUND LEAKING NR 1 ENGINE AIR STARTER. Oct 2, 2000 · N16501 · Emb EMB135ER · Starter-GeneratorSDR C2XA00CL074Starter · failedRDU-CLE - FLT 4009 - THE CREW REPORTED THE NR 1 ENGINE OIL QUANTITY DROPPED TO 2 QUARTS INDICATED. THE CREW PERFORMED AN INFLIGHT SHUTDOWN AND DIVERTED INTO ROA. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND THE NR 1 ENGINE ASep 30, 2000 · N16501 · Emb EMB135ER · Engine Oil Indicating SystemSDR C2XA99TY002Engine · failedTYS - DURING A SCHEUDLED INSPECTION, THE LEFT ENGINE WAS FOUND TO BE PRODUCING METAL THAT WAS BEYOND MANUFACTURER'S LIMITS. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW EMB-135 MM 71-00-00, OPERATIONAL AND LEAK CHECKS WERE SATISFACTORY. AIRCRAFT RELEOct 26, 1999 · N16501 · Emb EMB135ER · Engine (Turbine/Turboprop)
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