N804QS

Service difficulty reports not matched to an aircraft · 18

They name N804QS, 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 = 'N804QS' 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 DXTA2014021705655Bleed Valve · malfunctionedWHILE LEVELING OFF AT 6000 FEET, LT ENG BEGAN TO VIBRATE, N1 BEGAN TO DECREASE, ITT INCREASED TO APPROXIMATELY 650 DEGREES. ITT DECREASED WITH POWER LEVER RETRACTION & VIBRATION BECAME NOMINAL AT APPROXIMATELY 35% N1. TROUBLE SHOT & REPLACED LT BOV TORQUE MOFeb 15, 2014 · N804QS · Cessna 560CESSNA · Compressor Bleed ValveSDR DXTA2013011805248Strut · leakingAFTER TAKEOFF, GEAR DID NOT RETRACT. THREE GREEN GEAR LIGHTS, ONE RED GEAR UNSAFE LIGHT, ANTI-SKID LIGHT AND THE BRAKE LOW PRESSURE LIGHT, REMAIN ILLUMINATED FOR ABOUT FIVE MINUTES, RAN ABNORMAL CHECKLIST. AFTER THE GEAR HANDLE WAS SELECTED DOWN, EVERYTHING Jan 17, 2013 · N804QS · Cessna 560CESSNA · Main Landing Gear Strut/Axle/TruckSDR CWQR20120914050Drag Angle · crackedDURING A SCHEDULED INSPECTION, FOUND RT WING TO FUSELAGE FAIRING DRAG ANGLE THAT ATTACHES TO THE WING, WAS CRACKED AT THREE FASTENER LOCATIONS.Sep 14, 2012 · N804QS · Cessna 560CESSNA · Fuselage Miscellaneous StructureSDR CWQR20120914049Drag Angle · crackedDURING A SCHEDULED INSPECTION, FOUND THE LT WING TO FUSELAGE FAIRING DRAG ANGLE THAT ATTACHES TO THE WING, WAS CRACKED A 3 FASTENER LOCATIONS.Sep 14, 2012 · N804QS · Cessna 560CESSNA · Fuselage Main, StructureSDR CWQR20120215006Line · chafedWHILE PREFORMING THE INSPECTION FOR SL560-28-09, FOUND FITTING CHAFED ON FUEL LINE. AFTER REMOVAL OF THE FUEL LINE ASSY, FOUND THAT THE FITTING CLAMP ANTI-ROTATION STRAPS HAD CUT INTO THE FITTING BELL MOUTH BEYOND THE ALLOWABLE LIMITS.Feb 15, 2012 · N804QS · Cessna 560CESSNA · Aircraft Fuel Distribution SystemSDR CWQR20120210003Line · chafedWHEN ACCOMPLISHING SL560-28-09, FOUND FUEL LINE CHAFED ON FUEL BAY STRUCTURE IN THE LT WING, IT WAS MORE THAN 60 PERCENT CHAFED THROUGH. THE WING STRUCTURE SHOWS NO DAMAGE.Feb 10, 2012 · N804QS · Cessna 560CESSNA · Aircraft Fuel Distribution SystemSDR DXTA2011120604816Connector · looseON FINAL APPROACH, MLG SELECTED DOWN. DID NOT HEAR SOUNDS ASSOCIATED WITH MLG DOWN. RED MLG UNSAFE LIGHT ILLUMINATED ONLY. AFTER 20 SECONDS, NLG SHOWED DOWN & LOCKED. MISSED APPROACH & RETRACTED MLG HANDLE. RECYCLED MLG WITH NO MLG DOWN INDICATIONS. HYDec 5, 2011 · N804QS · Cessna 560CESSNA · Landing Gear System WiringSDR CWQR20110426001Angle · crackedWHILE ACFT WAS IN A SCHEDULED INSP, DISCOVERED THE FWD Z ANGLE THAT THE UPLOCK IS ATTACHED TO WAS CRACKED. THE CRACKS WERE LOCATED IN THE OTBD ENDS OF THE BEND RADIUS. 1 WAS .50 INCH AND THE OTHER WAS .30 INCH.Apr 26, 2011 · N804QS · Cessna 560CESSNA · Fuselage Miscellaneous StructureSDR DXTA2010050304083Ground Wire · brokenAFTER DEPARTURE, RED GEAR UNLOCKED LIGHT FAILED TO EXTINGUISH AFTER GEAR HANDLE WAS SELECTED IN THE UP POSITION. HYD SYS PRESSURE LIGHT REMAINED ILLUMINATED. 3 GREEN POSITION LIGHT INDICATORS EXTINGUISHED. UPON SELECTION OF THE GEAR HANDLE TO THE DOWN POSITIONApr 30, 2010 · N804QS · Cessna 560CESSNA · Landing Gear System WiringSDR 2009FA0000953Display · inoperativeLT SEAT PILOTS PFD - BLANKED OUT AT APPROX 50 KTS ON TAKEOFF ROLL - (ABORTED TAKE OFF). PFD CAME BACK ON DURING ROLLOUT OF ABORT AND WORKED AGAIN UNTIL SHUTDOWN.Nov 6, 2009 · N804QS · Cessna 560CESSNA · Central DisplaySDR DXTA2009051803658Lamp · inoperativeWHEN MLG SELECTED DOWN FOR LANDING , LT MLG INDICATOR LIGHT DID NOT ILLUMINATE. NO MLG UNSAFE INDICATION NOTED. PERFORMED MLG WILL NOT EXTEND CHECKLIST. LT & RT LOW HYD FLOW LIGHTS BLINKED INTERMITTENTLY AFTER MLG BLOWN DOWN. MLG LIGHT REMAINED OFF. PERFORMEDMay 15, 2009 · N804QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200702561Outflow Valve · inoperativePRESSURIZATION WORKED NORMALLY UP TO FL 310 BETWEEN FL 310 AND FL 320 THE CABIN STARTED TO RAPIDLY CLIMB AT A RATE OF 5500 FPM. THE CABIN BEFORE THE CLIMB WAS AROUND 4000 FT BEFORE THE RAPID CLIMB. THE 10000 FT ALTITUDE ANNUNCIATOR AND MASTER WARNING CAME ONOct 22, 2007 · N804QS · Cessna 560CESSNA · Pressure Regulator/Outflow ValveSDR CWQR200712Intake Duct · crackedDURING A PHASE INSPECTION FOUND RT ENGINE INLET DUCT ASSY CRACKED. CRACKS WERE FOUND ON THE AFT PORTION OF THE INLET DUCT ASSY THROAT. THIS UNIT HAD TO BE RETURNED TO THE MFG FOR REPAIR. AN SCR WAS SUBMITTED TO MFG UNDER NR 308873.Aug 13, 2007 · N804QS · Cessna 560CESSNA · Engine Air Intake SystemSDR CWQR200711Intake Duct · crackedDURING A PHASE INSPECTION FOUND LT ENGINE INLET DUCT ASSY CRACKED. CRACKS WERE FOUND ON THE AFT PORTION OF THE INLET DUCT ASSY THROAT. THIS UNIT HAD TO BE RETURNED TO THE MFG FOR REPAIR. AN SCR WAS SUBMITTED TO MFG UNDER NR 308858.Aug 13, 2007 · N804QS · Cessna 560CESSNA · Engine Air Intake SystemSDR CWQR200710Fork · looseDURING A MAINTENANCE TAXI CHECK NOTICED SHIMMY FROM NOSE GEAR. UPON DISASSEMBLY FOUND FORK LOOSE ON NOSE GEAR PISTON, THIS SHOULD BE A PRESS FIT FROM THE FACTORY. SENT UNIT RELIABILITY GROUP FOR EVALUATION. A SCR HAS BEEN SUBMITTED TO MFG UNDER NR 308107.Aug 8, 2007 · N804QS · Cessna 560CESSNA · Nose/Tail Landing GearSDR DXTA200601684Fuel Control · failedLEFT ENGINE FAILURE ON DESCENT THROUGH 17,000 FT. ENGINE POWER 40% N1 NOTICED ENGINE ROLLBACK WITH NO ABNORMAL INDICATIONS. NO FUEL OR OIL BYPASS LIGHTS ON, TRANSFERRED FUEL FROM LEFT TO RIGHT THEN NOTICED BOTH FUEL PUMP LIGHTS ON. BOTH FUEL PUMP SWITCHES IOct 25, 2006 · N804QS · Cessna 560CESSNA · Fuel Control/Turbine EnginesSDR DXTA200400232Engine · flamed outWHILE DESCENDING THROUGH FL 310 WITH THE RIGHT POWER LEVER AT FLIGHT IDLE, THE BOOST PUMP CAME ON AND OIL PRESSURE DROPPED TO ZERO, GENERATOR WENT OFF-LINE. THE RIGHT ENGINE FLAMED OUT, IT THEN AUTO RELIT AT FL 290. REMOVED AND REPLACED THE RT ENGINE IAW CESSJan 28, 2004 · N804QS · Cessna 560CESSNA · Engine (Turbine/Turboprop)SDR DXTA200300208Fuel Control · failedRIGHT ENGINE FLAMED OUT DURING DESCENT (THROUGH 22000) PERFORMED RESTART WITHOUT EVENT. ENGINE OPERATION WAS NORMAL THROUGH THE REST OF FLIGHT, AIRCRAFT CONTINUED TO DESTINATION. SUMPTED RT FUEL TANK TO CHECK FOR WATER OR CONTAMINATION, SYSTEM CHECKED GOOD, IDec 22, 2003 · N804QS · Cessna 560CESSNA · Fuel Control/Turbine Engines
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