N844QS

Service difficulty reports not matched to an aircraft · 18

They name N844QS, 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 = 'N844QS' 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 DXTA2016032506218Unknown · odorAT FL400 WE TURNED THE DEFOG FAN ON & SMELLED AN ELEC OR PLASTIC BURNING SMELL. TURNED THE DEFOG FAN OFF IMMEDIATELY & THE SMELL DISSIPATED. REMOVED FLOOR PANELS & INSPECTED DEFOG BLOWER & ALL ASSOCIATED DUCT WORK IAW AMM 21-21-01, NO DEFECTS NOTED. PERFORMMar 24, 2016 · N844QS · Cessna 560CESSNA · Air Distribution SystemSDR DXTA2016032506217Unknown · odorAT FL400 WE TURNED THE DEFOG FAN ON & SMELLED AN ELEC OR PLASTIC BURNING SMELL. WE TURNED THE DEFOG FAN OFF IMMEDIATELY & THE SMELL DISSIPATED. REMOVED FLOOR PANELS & INSPECTED DEFOG BLOWER & ALL ASSOCIATED DUCT WORK IAW AMM 21-21-01, NO DEFECTS NOTED. PERFMar 24, 2016 · N844QS · Cessna 560CESSNA · Air Distribution SystemSDR DXTA2015110506116Switch · unserviceableAT FL 380 IN THE CLIMB, TWO LOUD BANGS, EMER PRESS & ACM OVHT LIGHT CAME ON. CABIN WAS -3700 FPM. STARTED EMER DECENT, AFTER 1 MIN CABIN STARTED PRESSURIZING. THEN THE PROCESS REPEATED ITSELF. PLACED BOTH 410° & 450° ACM OVER TEMP SWITCHES ON ORDER FOR SUPNov 5, 2015 · N844QS · Cessna 560CESSNA · Cabin Cooling SystemSDR DXTA2014042105738Switch · faultedAFTER TAKEOFF & CLIMBING THROUGH 400 FT, LEFT THRUST REVERSER ARM LIGHT & HYD PRESSURE ANNUNCIATOR ILLUMINATED. IAW THE CHECKLIST, THE LT EMERGENCY STOW SWITCH WAS PLACED IN EMERGENCY STOW POSITION. BOTH LIGHTS REMAINED ON UNTIL THE LANDING ROLLOUT & BELOW Apr 19, 2014 · N844QS · Cessna 560CESSNA · Engine Thrust ReverserSDR DXTA2012100805137Wheel · unserviceableDURING TAXI, A SHIMMY/VIBRATION IS FELT BETWEEN 15-20KTS. IT FEELS LIKE A "POOR CONDITION" TAXIWAY SURFACE. THERE IS NO NOTICABLE DIRECTIONAL BIAS AND ALL HANDLING CHARACTERISTICS ARE NORMAL. REMOVED NR 1 NOSE WHEEL ASSEMBLY AND NR 2 NOSE WHEEL ASSEMBLY AND Oct 5, 2012 · N844QS · Cessna 560CESSNA · Wheel/Ski/FloatSDR DXTR20120124008Line · chafedFUEL TRANSFER LINE, PN 6526400-61, IS CHAFING THE FUSELAGE UNDER PANEL 161AB.Jan 24, 2012 · N844QS · Cessna 560CESSNA · Aircraft Fuel Distribution SystemSDR DXTA2011092604735Aileron Sys · ratchetingAILERON JERKY IN FLIGHT WITH AUTOPILOT OFF. SMOOTH ON GROUND WITH POWER OFF. RESHIMMED PILOTS CONTROL YOKE DRUM ASSY. ADJUSTED RT AILERON QUADRANT GAP TO ACCEPTABLE TOLERANCE. AILERON REMOVED AND REINSTALLED TO FACILITATE INSP. TENSIONED AND RIGGED AILERSep 25, 2011 · N844QS · Cessna 560CESSNA · Aileron Control SystemSDR CWQR201006Door · stuck(CWQR) DURING A SCHEDULED MX EVENT, THE EMERGENCY EXIT DOOR WAS REMOVED. REMOVAL OF THE EMERGENCY EXIT DOOR WAS FOUND TO BE VERY DIFFICULT. REQUIRED 2 TECHS AND 10 MINUTES TO WORK DOOR LOOSE. THE OPERATOR VERIFIED THAT EMERGENCY DOOR INSP ASL-560-52-04 HAD PDec 14, 2010 · N844QS · Cessna 560CESSNA · Emergency ExitsSDR 2010F00036Warning Light · illuminatedON APPROACH, EXT FLAPS TO 15, HYD PUMP REMAINED ILLUMINATED. REPOSITIONED FLAPS AND THE LIGHT REMAINED ON. IMMEDIATELY EXT GEAR AND FULL FLAPS. THE HYD LIGHT EXTINGUISHED. FLAP POSITION APPEARED NORMAL. ON SHORT FINAL, TOO LOW FLAPS, TOO LOW TERRAIN SOUNDEFeb 11, 2010 · N844QS · Cessna 560CESSNA · Central WarningSDR DXTA2009063003710Throttle Cable · frayedWHEN ATTEMPTING TO ADJUST POWER AFTER TURNING ANTI-ICE ON AT FL450, THE RT PWR LEVER WAS STUCK AND WOULD NOT MOVE FWD OR BACKWARD. ON DESCENT AND UPON REACHING +7 DEGREES CELSIUS THE LEVER WOULD MOVE AGAIN. REMOVED AND REPLACED STIFF LT & RT FORWARD FUSELAGE Jun 28, 2009 · N844QS · Cessna 560CESSNA · Power LeverSDR DXTA2009020403487Wire Harness · malfunctionedANTI SKID INOP LIGHT CAME ON DURING TAXI. WHILE TRYING TO STOP PLANE IT VEERED OFF TO THE LT LIKE 1 BRAKE WAS NOT WORKING. T/S ANTI-SKID SYS IAW AMM 32-42-00 AWDM 32-40-01. REMOVED NR 2 (RT) MAIN GEAR-WELL ANTI SKIED WIRE BUNDLE (PN 6528030-30) IAW AMM 32-4Feb 4, 2009 · N844QS · Cessna 560CESSNA · Brake Anti-Skid SectionSDR DXTA2009020303487Brake Assy · malfunctionedANTI SKID INOP LIGHT CAME ON DURING TAXI. WHILE TRYING TO STOP PLANE IT VEERED OFF TO THE LT LIKE 1 BRAKE WAS NOT WORKING.Feb 4, 2009 · N844QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200808183234O-Ring · leakingLOSS OF BRAKES ON TAXI INTO PARKING WITH LOW BRAKE PRESSURE AND ANTI-SKID INOP LIGHTS. REQUIRED USE OF EMERGENCY BRAKES. UPON INSPECTION FLUID WAS LEAKING FROM NOSE. FOUND O-RING ON PWR BRAKES LEAKING FILTER BOWL AND O-RING VERIFIED. REPLACED IAW AMM 32-4Aug 18, 2008 · N844QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200803234Brake · inoperativeLOSS OF BRAKES ON TAXI INTO PARKING. REQUIRED USE OF EMERGENCY BRAKES. (S)Aug 18, 2008 · N844QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200702495Warning Light · illuminatedEMER PRESS CAME ON DURING TAKEOFF AND WAS WITHOUT AN ANNUNCIATOR. COULD HEAR THE "RUSHING AIR" SOUND WHEN THE THROTTLES WERE POWERED UP. RAN A/C FOR 30 MINUTES AT VARIOUS POWER SETTINGS WITH PRESSURIZATION SELECTED NORMAL - SELECTED EMERGENCY SEVERAL TIMES. Sep 23, 2007 · N844QS · Cessna 560CESSNA · Central WarningSDR DXTA200702332Indicator · malfunctionedLT MAIN LANDING GEAR INDICATOR WOULD NOT EXTINGUISH AFTER GEAR WAS BROUGHT UP. CYCLED GEAR 3 TIMES, INDICATOR STAYED ON EACH TIME. [07-23-07] JACKED A/C IAW CESSNA AIRCRAFT TO MODEL 560 MAINTENANCE MANUAL 7-10-11. SWING LANDING GEAR THROUGH 5 CYCLES, COULJul 12, 2007 · N844QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200702123Fcu · malfunctionedLT ENGINE WOULD NOT DEVELOP FULL POWER FOR TAKEOFF. MAX POWER DEVELOPED WAS APPROXIMATELY 2 PERCENT N1 LOW, RIGHT ENGINE DEVELOPED FULL POWER. [SUP 05-02-07] VERIFIED DISCREPANCY. REMOVED AND REPLACED FCU WITH SERVICEABLE UNIT, CANNIBALIZED FROM OTHER AIRCRAApr 20, 2007 · N844QS · Cessna 560CESSNA · Fuel Control/Turbine EnginesSDR DXTA200501110Fuel Filter · bypassingPRIOR TO 70 KTS DURING TAKEOFF ROLL THE LEFT FUEL FILTER BYPASS ANNUNCIATOR ILLUMINATED & THE TAKEOFF WAS ABORTED. INSPECTED BOTH LEFT AND RIGHT WING TANKS. REMOVED AND REPLACED BOTH ENGINE FUEL FILTERS. PERFORMED LEAK CHECK OF ACCESS PANELS AND ENGINES CHENov 23, 2005 · N844QS · Cessna 560CESSNA · Aircraft Fuel Filter/Strainer
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