N624QS

Service difficulty reports not matched to an aircraft · 16

They name N624QS, 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 = 'N624QS' 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 DXTA2019022502072Display · defectiveDISPLAY UNIT - DURING FLIGHT INTERMITTENT HOT ELECTRICAL ODOR IN COCKPIT. AMLCD VERY HOT TO THE TOUCH. FOUND AMLCD VERY HOT TO THE TOUCH . REMOVED AND REPLACED AMLCD IAW CE-560XL M/M 77-40-00. OPS CHECK GOOD. PERFORMED ENG RUNS NO ABNORMAL ELECTRICAL SMELL NOFeb 24, 2019 · N624QS · Cessna 560XL · Central DisplaySDR EBVR20180212001Skin · delaminatedDURING INSPECTION, FOUND THE LT OUTBOARD FLAP IS DELAMINATED. INSTALLED A REPAIR IAW MM 57-50-01, AND 27-51-00.Feb 12, 2018 · N624QS · Cessna 560XL · Trailing Edge FlapsSDR DXTA2018011800487Switch · failedWHILE CLIMBING, THE RT THRUST REVERSER UNLOCK LIGHT CAME ON FOLLOWED BY THE ARM LIGHT. TURNED ON THE EMERGENCY STOW SWITCH PERFORMED MEMORY ITEMS FOLLOWED BY THE CHECKLIST. DECLARED THE EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED TJan 17, 2018 · N624QS · Cessna 560XL · Engine Thrust ReverserSDR DXTA2016060306253Engine · unserviceableDURING CLIMBOUT AT APPROXIMATELY 12,000 FT, THE RT ENGINE OIL PRESSURE WENT TO ZERO. IT WAS IMMEDIATELY FOLLOWED BY A RED MASTER WARNING LIGHT AND A LOW OIL PRESSURE LIGHT. AFTER COMPLETING THE EMERGENCY CHECKLIST, THE GAUGE RETURNED TO NORMAL WITH A REDUCEDJun 9, 2016 · N624QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA201510056100Display · malfunctionedAPU ON & BLEED ON, TEMP WENT RAPIDLY TO 250 DEGREES & THEN AIR DUCT O'HEAT ANNUNCIATOR ILLUMINATED, FOLLOWED BY A VERY STRONG ACRID SMOKY SMELL IN THE CABIN. BLEED AIR WAS TURNED OFF & FULL MANUAL COLD SELECTED, BUT THE SMELL OF SOMETHING BURNING CONTINUED. Oct 4, 2015 · N624QS · Cessna 560XL · Cabin Cooling SystemSDR DXTA2014100605905Engine · malfunctionedRIGHT ENGINE OIL PRESSURE WENT TO 17 PSI INFLIGHT. SHUTDOWN ENGINE. R & R THE ENGINE & OPS & LEAK CHECKED GOOD. PERFORMED A 5 POINT PERFORMANCE CHECK.Oct 3, 2014 · N624QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA2014100605904Display · failedNR 1 DISPLAY UNIT INOPERATIVE, NOTICED SMOKE AS WELL. REMOVED AND REPLACED THE NR 1 DISPLAY UNIT, OPS CHECKED GOOD. NO DEFECTS NOTED, WORK COMPLETED IAW MM 31-50-01.Oct 3, 2014 · N624QS · Cessna 560XL · Flight Management Computing Hardware SystemSDR DXTA2010020203967Trimmer · crackedRIGHT AFTER LIFTOFF, EXCESSIVE FWD PRESSURE REQUIRED (FULL FWD TRIM AND BOTH HANDS ON YOKE APPLYING FWD PRESSURE). AFTER FLAP/STAB RETRACTION AND 200KTS A/S, ACFT WAS ABLE TO BE FLOWN WITH ONE HAND WHILE MAINTAINING FULL FWD TRIM. LEVELING AT 14,000 AND >250 Feb 1, 2010 · N624QS · Cessna 560XL · Elevator Control SystemSDR DXTA200803105Actuator · malfunctionedTHE NOSE WHEEL GREEN LIGHT WOULDN’T GO OUT AFTER THE GEAR WAS SELECTED UP. REMOVED & REPLACED ACTUATOR, COMPLIED WITH GEAR ANGLE, RETRACTION, LEAK & BLOWDOWN CHECKS IAW MM 32-30-03, 32-20-00 & 32-01-00. SERVICED PNEUMATIC RESERVOIR IAW MM 12-13-01. OPS CHECKSJun 8, 2008 · N624QS · Cessna 560XL · Landing Gear Position and WarningSDR DXTA200803099Servo Valve · malfunctionedLT EEC FAILED DURING TO ROLL. REMOVED AND REPLACED NR 1 ENGINE SERVO VALVE. PERFORMED OPERATIONAL CHECK AND NO DEFECTS NOTED AT THIS TIME REF MM 75-30-01 & 71-00-00.Jun 6, 2008 · N624QS · Cessna 560XL · Fuel Controlling SystemSDR DXTA200702155Rudder Pedal · damagedAFTER ROTATION, THE YAW DAMPER WOULD NOT ENGAGE AND WHEN WE TURNED LT, THE LT RUDDER PEDAL WOULD NOT MOVE. AFTER ENGAGING AND DISENGAGING THE YAW DAMPER THE RUDDER OPERATED NORMALLY. ON THE GROUND WE COULD FEEL AND HEAR GRINDING SOUND IN THE RUDDER PEDALS WHApr 27, 2007 · N624QS · Cessna 560XL · Rudder Control SystemSDR DXTA200701953Windshield · failedCAPT`S WINDSHIELD SHATTERED.Feb 17, 2007 · N624QS · Cessna 560XL · Flight Compartment WindowsSDR DXTA200601710Thrust Reverser · vibrationACCELERATING THROUGH 250KTS, FELT EXCESSIVE VIBRATION. UPON LANDING, FOUND THAT THE RT TR BUCKET NOT FLUSH WITH ENGINE COWLING. M2B- REACTIVATED RT TR UPON APPLYING HYDRAULIC PRESS. RT BUCKET CLOSED FLUSH WITH ENGINE COWL. INSPECTED TR FOR DAMAGE AND CYCLED RNov 4, 2006 · N624QS · Cessna 560XL · Engine Thrust ReverserSDR DXTA200500999Actuator · inoperativeAFTER SETTING T/O POWER ON DEPARTURE ROLL RUDDER PEDALS BECOME VERY STIFF (FEELS LIKE YAW-DAMP IS ON). ABORTED TAKEOFF AT STP AFTER REACHING 60 KIAS. A/C TAXI'S NORMAL AND RUDDER BIAS TEST WAS NORMAL. REMOVED AND INSTALLED A NEW RUDDER BIAS ACTUATOR, OPS CHOct 4, 2005 · N624QS · Cessna 560XL · Rudder Control SystemSDR DXTA200500792Engine · malfunctionedON TAKEOFF WITH THROTTLE IN THE T/O DETENT, THE LT ENGINE ITT EXCEEDED 720 DEG CELSIUS WITHIN 10 SECS. THE LT ITT INDICTED 724 DEG CELSIUS AND WAS STILL SLOWLY INCREASING. LT THROTTLE REDUCED TO CLIMB. DETENT AND ITT INDICATION IMMEDIATLY DECREASED BELOW 720Jun 20, 2005 · N624QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR DXTA200500514Limit Switch · failedNO TAKEOFF LIGHT WILL NOT GO OUT ON GROUND, HORN SOUNDS WHEN POWER IS ADVANCED ALL ASSOCIATED SYSTEMS CHECKED / NO PROBLEMS INDICATED. FOUND STAB POSITION SWITCHES OUT OF ADJUSTMENT AND CORROSION ON SPEED BRAKE SWITCH CONNECTORS. ADJUSTED HORIZONTAL STAB POSIJan 4, 2005 · N624QS · Cessna 560XL · Central Computers
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