Cessna 525

Service difficulty reports · 260

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = '525'
  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 96ZZZX1367Circuit Board · burnedCUSTOMER REPORTED NO COCKPIT FLOOD LIGHTS. INVESTIGATION REVEALED THE THRUST ATTENTUATOR CIRCUIT BOARD WAS BURNED. THE FLOOD LIGHT RESISTOR HAD BURNED THROUGH. INSTALLED NEW BOARD AND RETURNED TO SERVICE.Nov 21, 1995 · N26CB · Cessna 525 · Flight Compartment LightingSDR CA951206008Diode · open circuit(CAN)PILOT REPORTED RIGHT WING "HOT" ON GROUND WITH WING ANTI-ICE SELECTED OFF. DIODE FOUND OPEN WHICH ALLOWS ENGINE BLEED AIR TO PASS THROUGH THE WING ANTI-ICE VALVE, HEATING THE LEADING EDGE.Nov 20, 1995 · Cessna 525 · Airfoil Anti/De-ice SystemSDR 95ZZZX6466Rate Gyro · failedRATE GYRO FAILED CAUSING THE YAW DAMPER TO DISENGAGE. TEN MINUTES LATER, THE EFIS A.C. CIRCUIT BREAKER TRIPPED (1 AMP) WHICH RESULTED IN THE LOSS OF THE EADI AND EHSI. FLIGHT WAS UNDER VFR CONDITIONS. THIS PROBLEM LED TO THE LOSS OF THE PILOT'S FLIGHT INSTROct 19, 1995 · N800HS · Cessna 525 · AC Indicating SystemSDR 95ZZZX3609Filter · warn lightLEFT FUEL FILTER BYPASS INDICATOR LIGHT ILLUMINATED (ANNUNCIATING PENDING FILTER BYPASS) DURING 'GO-AROUND'. AIRCRAFT LANDED WITHOUT PROBLEMS. LEFT ENGINE FUEL FILTER ELEMENT WAS REPLACED. NO OBVIOUS FAULTS NOTED. RIGHT ENGINE FILTER ELEMENT WAS ALSO REPLAJun 29, 1995 · N94MZ · Cessna 525 · Engine Fuel DistributionSDR 95ZZZX2844Frame · damagedWHILE PERFORMING REMOVAL OF COCKPIT SIDE WINDOW (RIGHT), THE WINDSHIELD RETAINER MUST BE REMOVED. UPON REMOVAL OF SAID RETAINER, TWO HOLES WERE FOUND DRILLED IN THE FRAME STRUCTURE. THIS IS A CONDITION THAT IS CONSIDERED TO BE AN ISOLATED INCIDENT. REPAIRS May 15, 1995 · N800HS · Cessna 525 · Fuselage Miscellaneous StructureSDR 95ZZZX1584Igniter · brokenWHILE PERFORMING A CHECK-1 IAW WILLIAMS INTERNATIONAL FJ44-1A INSPECTION GUIDE, DISCOVERED THE ELECTRODE INSULATOR ON THE RT ENGINE INBOARD IGNITER HAD BROKEN OFF. A BORESCOPE INSPECTION WAS PERFORMED WHICH REVEALED DAMAGE TO THE TURBINE SECTION. THE ENGINE Mar 21, 1995 · N12PA · Cessna 525 · Ignition SwitchingSDR 95ZZZX1039Circuit Breaker · shortedPILOT REPORTED LANDING GEAR AND FLAP SYSTEM CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. LANDING GEAR WAS BLOWN DOWN WITH EMERGENCY SYSTEM. TROUBLESHOT SYSTEM AND FOUND P.C. BOARD HAD BURNED TRACKS. FOUND CIRCUIT BREAKER FOR LANDING GEAR CONTROL DIODE ON LAFeb 6, 1995 · N444RH · Cessna 525 · Landing Gear Retraction/Extension SystemSDR 95ZZZX1038Pc Board · defectivePILOT REPORTED LANDING GEAR AND FLAP SYSTEM CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. LANDING GEAR WAS BLOWN DOWN WITH EMERGENCY SYSTEM. TROUBLESHOT SYSTEM AND FOUND P.C. BOARD HAD BURNED TRACKS. FOUND CIRCUIT BREAKER FOR LANDING GEAR CONTROL DIODE ON LAFeb 6, 1995 · N444RH · Cessna 525 · Landing Gear Retraction/Extension SystemSDR 95ZZZX973Coupling · failedPILOTS REPORTED ANTI-SKID AND POWER BRAKES FAILED. FOUND POWER BRAKE MOTOR TO PUMP COUPLING HAD FAILED. REASON UNKNOWN. REPLACED COUPLING WITH NEW UNIT. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. AIRCRAFT TOTAL TIME 175.4. AIRCRAFT TOTAL LANDINGS 293Feb 2, 1995 · N20FL · Cessna 525 · Landing Gear Brake SystemSDR 95ZZZX1317Gearbox · seal failedLEFT ENGINE LOSS OF OIL PRESSURE, 135 OPERATOR - IMJA. OIL SEAL INSTALLED DURING COURSE OF SB71-05 9-18-94. TIME IN SERVICE, 22.0 HOURS, 12 CYCLES.Feb 1, 1995 · N800HS · Cessna 525 · Turbine Engine Accessory Drive
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