N120QS

Service difficulty reports not matched to an aircraft · 17

They name N120QS, 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 = 'N120QS' 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 DXTA2012112605190Door · out of adjustRED LIGHT IN GEAR HANDLE WOULD NOT EXTINGUISH AFTER GEAR RETRACTION, TOWER NOTICED AND SAID IT APPEARS TO BE THE RT SIDE. GEAR WAS EXTENDED NORMALLY WITH A GEAR SAFE INDICATION, LANDED NORMALLY. JACKED ACFT AND SWUNG LANDING GEAR. CONFORMED INTRANSIT GEAR FANov 23, 2012 · N120QS · Beech 400A · Landing Gear Door Retract SectionSDR DXTA2012111205180Actuator · out of adjustRED GEAR HANDLE LIGHTS FAILED TO EXTINGUISH AFTER GEAR RETRACTION (GEAR DOOR UNSAFE NOT UP AND LOCKED INDICATION). RETURNED TO AIRPORT, LANDING GEAR EXTENTION WAS NORMAL. ADJUSTED NOSE LANDING GEAR RETRACT ACTUATOR IAW AMM 32-20-00-201. PERFORMED NUMEROUS LANov 9, 2012 · N120QS · Raythn 400ARAYTHEON · Landing Gear ActuatorSDR DXTA2012111205179Switch · out of adjustRED GEAR HANDLE LIGHTS FAILED TO EXTINGUISH AFTER GEAR RETRACTION (GEAR DOOR UNSAFE NOT UP AND LOCKED INDICATION). RETURNED TO AIRPORT, LANDING GEAR EXTENTION WAS NORMAL. NOSE GEAR UPLOCK SWITCH CLEANED AND ADJUSTED IAW AMM 32-30-00. GEAR OPERATION AND ANNUNNov 9, 2012 · N120QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA2012102205159Brake Assy · contaminatedAFTER BLOCK-IN, LEFT BRAKE SMOKING. DURING INSPECTION, LEFT TIRE AND WHEEL ASSY WAS EXTREMELY HOT AND A DISTINCT ODOR OF HOT BRAKES. LANDING WAS NORMAL WITH VERY MINIMAL USE OF THE BRAKES. INSPECTED LEFT BRAKE ASSEMBLY, APPEARS TO BE NEW AND NO EVIDENCE OF OOct 20, 2012 · N120QS · Beech 400A · Landing Gear Brake SystemSDR DXTA2012101105142Actuator · failedAFTER TAKEOFF. SELECTED GEAR UP. GREEN LIGHTS WENT OUT, RED GEAR HANDLE LIGHT STAYED ON. ON LANDING, SELECTING GEAR DOWN, 3 GREEN LIGHTS ON AND RED LIGHT WENT OUT. ATTEMPTED NLG OPS CHECK IAW MM 32-20-00-201, NLG WOULD STOP MOVING PRIOR TO UPLOCK ENGAGEMENOct 10, 2012 · N120QS · Beech 400A · Landing Gear ActuatorSDR DXTA2012090405119Spring · failedAFTER TAKEOFF WHEN GEAR HANDLE WAS RAISED, NOTICED RED IN TRANSIT LIGHT REMAINED ILLUMINATED AND ALL GREEN LANDING GEAR LIGHTS WERE OUT. TOWER REPORTED NOSE AND MAIN GEAR APPEARED TO BE RETRACTED BUT BOTH MAIN GEAR DOORS WERE EXTENDED. COMPLIED WITH CHECKLISep 9, 2012 · N120QS · Beech 400A · Landing Gear Position and WarningSDR DXTA2012091005119Landing Gear · malfunctionedAFTER TAKEOFF, WHEN GEAR HANDLE WAS RAISED, NOTICED RED IN TRANSIT LIGHT REMAINED ILLUMINATED AND ALL GREEN LANDING GEAR LIGHTS WERE OUT. TOWER REPORTED NOSE AND MAIN GEAR APPEARED TO BE RETRACTED BUT BOTH MAIN GEAR DOORS WERE EXTENDED. COMPLIED WITH CHECKLISSep 9, 2012 · N120QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA2012040504944Brake Sys · malfunctionedBOTH PILOT AND COPILOT BRAKE PEDALS REQUIRE EXECESSIVE PRESSURE TO ACTUATE THE BRAKES. CHECKED BRAKE WEAR & FLUID LEVELS. NO DEFECTS NOTED. TAXIED ACFT AND PERFORMED BRAKE CHECKS ALL CHECKS NORMAL. PILOT VERIFIED PROPER BRAKE, OPS ON HIGH SPEED TAXI. ALL WApr 4, 2012 · N120QS · Beech 400A · Landing Gear Brake SystemSDR DXTA2010120304344Brake Sys · malfunctionedON LANDING, WHEN APPLYING BRAKES, BOTH PEDALS WERE HARD AND THERE WAS NO BRAKING ACTION UNTIL AFTER THE ACFT SLOWED BELOW 60KNTS. BRAKES WORKED NORMAL WITH THE ANTI-SKID OFF DURING TAXI. COULD NOT DUPLICATED DISCREPANCY. ALL WORK PERFORMED IAW MM 32-40-03 ANDec 2, 2010 · N120QS · Raythn 400ARAYTHEON · Landing Gear Brake SystemSDR DXTA2010081804197Adc · inoperativeCO-PILOT AIR DATA INOP. REMOVED ADC AND INSTALLED AN OVERHAULED UNIT. OPS CHECK OF SYSTEM SHOWS NORMAL OPERATION. PERFORMED PITOT-STATIC. LEAK CHECKED - COMPLIED WITH RVSM TEST IAW AMM 34-10 CHART 201. ALL WORK PERFORMED IAW AVIONICS SYSTEM MANUAL SECTION 5.Aug 17, 2010 · N120QS · Raythn 400ARAYTHEON · Air Data ComputerSDR DXTA2009061503688Control Box · malfunctionedON TAXI IN, DISCOVERED WHEEL BRAKES WERE NOT RESPONDING PROPERLY. FIRST 1 TO 2 INCHES OF BRAKE APPLICATION THERE IS NO RESPONSE, THEN BRAKES WERE STIFF & GRABBY; VERY HARD TO APPLY BRAKES SMOOTHLY. SELECTED ANTI-SKID SWITCH TO OFF AND BRAKES RESPONDED NORMAL. Jun 13, 2009 · N120QS · Raythn 400ARAYTHEON · Brake Anti-Skid SectionSDR DXTA200702700Bulb · burned outLT MAIN GEAR DOWN AND LOCK INDICATION INOPERATIVE. REPLACED LT MAIN LANDING GEAR DOWN INDICATION BULB. OPS CHECK GOOD IAW HAWKER 400XP MM CH 32-60-00.Dec 20, 2007 · N120QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200702261Unknown · unknownWHILE IN A 3000FPM DESCENT, WE EXTENDED THE SPEEDBRAKES. AIRCRAFT ABRUPTLY ROLLED RT 12-15 DEGREES AND THEN JUST AS ABRUPTLY ROLLED LT AFTER APPROX 2 SECONDS. PERFORMED SPEED BRAKE OPERATIONAL CHECK IAW 400XP MM 27-60-00. OPS CHECKED GOODJun 13, 2007 · N120QS · Beech 400A · Drag Control SystemSDR DXTA200701922Indicator · no indicationWHEN GEAR WAS PLACED IN DOWN POSITION. THE RT GREEN R DID NOT ILLUMINATE. OHMED OUT GEAR INDICATOR HARNESS NO DEFECTS WERE NOTED. ACCESSED CONNECTOR P272 IN R/H WHEEL WELL OHMED OUT DOWN LOCK SWITCH FOUND HIGH RESISTANCE THROUGH CLOSED CONTACTS ON SWITCH. NOTFeb 8, 2007 · N120QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200601242Flt Controls · out of positionON TAKEOFF WARNING HORN CAME ON ABORTED TAKEOFF AT 50 KNOTS FLIGHT CONTROLS APPEARED TO BE IN CORRECT POSITION. COMPLIED WITH TAKEOFF WARNING HORN CHECK IAW RAYTHEON 400/400A M/M 27-40-00 OPS CHECKS SATISFACTORY NO DEFECTS NOTED AT THIS TIME.Feb 15, 2006 · N120QS · Beech 400A · Flight Control SystemSDR DXTA200601183Position Switch · malfunctionedON TAKEOFF KTEB GEAR WOULD NOT RETRACT, USED OVER RIDE. GEAR RETRACTED NORMAL. JACKED A/C, RETRACTED GEAR SEVERAL TIMES, NO DEFECTS NOTED. CHECKED LT LANDING GEAR SAFETY SWITCH. SWITCH AT LIMIT. ADJUSTED SWITCH, OPS CHECK GOOD IAW HAWKER 400XP MM.Jan 5, 2006 · N120QS · Beech 400A · Landing Gear Position and WarningSDR DXTA200500952Position Switch · inoperativeDURING CRUISE FLIGHT AT FL,360/.78 MACH THE LT DEPLOY LIGHT ILLUMINATED (THE DEPLOY ONLY-NO ARM OR UNLOCK.) DESCENDED AND PUSHED EMERGENCY STOW. THE BOTTOM PORTION OF THE EMERGENCY STOW THRUST REVERSER. ARM AND DEPLOY WERE NOW ILLUMINATED. THE DEPLOY LIGHT Sep 5, 2005 · N120QS · Beech 400A · Engine Thrust Reverser
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