N140QS

Service difficulty reports not matched to an aircraft · 22

They name N140QS, 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 = 'N140QS' 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 DXTA2013122702608Landing Gear · malfunctionedAFTER TAKEOFF, POSITIVE RATE CALLED FOR LANDING GEAR UP. FIRST OFFICER RAISED GEAR HANDLE UP. LANDING GEAR DID NOT RETRACT & THREE GREEN LIGHT STILL ILLUMINATED. TURNED BACK TO AIRPORT LOWERED THE LANDING GEAR HANDLE IN DOWN POSITION & LANDED. PERFORMED LADec 26, 2013 · N140QS · Raythn 400ARAYTHEON · Landing Gear Retraction/Extension SystemSDR DXTA201312272608Unknown · malfunctionedDURING TAKEOFF POSITIVE RATE CALLED FOR LG UP. FIRST OFFICER RAISED GEAR HANDLE UP. LG DID NOT RETRACT & THREE GREEN LIGHTS STILL ILLUMINATED. TURNED THE AIRPLANE BACK TO THE AIRPORT LOWERED THE LG HANDLE IN DOWN POSITION & LANDED AT AIRPORT.Dec 26, 2013 · N140QS · Raythn 400ARAYTHEON · Landing Gear Retraction/Extension SystemSDR DXTA2012101205140Bulb · inoperativeRT MAIN GEAR INDICATOR LIGHTS DID NOT ILLUMINATE GREEN ON GEAR EXTENSION. LIGHTS TEST WOULD NOT ILLUMINATE RMG LIGHT. FOLLOWED CHECKLIST AND ALL INFORMATION LED TO A NORMAL LANDING AS GEAR APPEARED TO BE DOWN AND LOCKED. REMOVED AND REPLACED ALL FOUR LIGHT BUOct 9, 2012 · N140QS · Beech 400A · Landing Gear Position and WarningSDR DXTA2012012604852Control Box · inoperativeWHILE TAXIING THE BRAKES WOULD ALTERNATELY WORK THEN FAILED. SIMILAR TO ANTISKID TEST. DUPLICATED DISCREPANCY. TROUBLESHOT THROUGH MM CH FAULT ISOLATION 32-40-03. ANTI SKID CONTROL BOX FAILED. REPLACED ANTI-SKID CONTROL BOX IAW MM CH-32-40-00, OPS CHECK GOJan 18, 2012 · N140QS · Raythn 400ARAYTHEON · Brake Anti-Skid SectionSDR DXTA2012011804849Control Box · malfunctionedDURING TAXI TO RAMP, RIGHT BRAKE RELEASED FOR 2 SECONDS. CONTINUED TO SLOW & MADE A SLIGHT RIGHT TURN, APPLYING A LITTLE MORE RIGHT BRAKE THAN LEFT. AGAIN RT BRAKE RELEASED FOR 2 SECONDS. TAXIING STRAIGHT (6 MPH) BOTH BRAKES RELEASED. ROLLED FOWARD ABOUT 1Jan 7, 2012 · N140QS · Beech 400A · Landing Gear Brake SystemSDR DXTA2011121304824Control Box · malfunctionedON TAXI OUT, EXPERIENCED A LOSS OF BRAKING FOR BOTH PILOT & COPILOT. BRAKE PEDALS PULSATED AS IF ANTI-SKID ACTIVATING. R & R ANTI-SKID CONTROL BOX WITH UNIT. OPS CHECKED SATISFACTORY IAW MM 32-40-00.Dec 11, 2011 · N140QS · Beech 400A · Brake Anti-Skid SectionSDR DXTA2011082304706Brake Sys · malfunctionedMOMENTARY BRAKE RELEASE WHEN APPLYING BRAKES PRIOR TO EXITING THE RUNWAY. PERFORMED BRAKE BLEED & TAXI CHECK, UNABLE TO DUPLICATE DISCREPANCY, PERFORMED ANTI-SKID RESPONSE CHECK, NO DEFECTS NOTED. ALL WORK DONE IAW MM 32-40-00.Aug 21, 2011 · N140QS · Beech 400A · Landing Gear Brake SystemSDR DXTA2011020104439Switch · malfunctionedON FINAL, EXTENDED LANDING GEAR. SOUNDED NORMAL BUT NO GREEN INDICATION. MISSED APPROACH AND ENTERED CLOSED TRAFFIC. CYCLED GEAR UP AND GOT NORMAL INDICATIONS. ON FINAL AGAIN EXTENDED GEAR AND GOT NORMAL INDICATIONS. LANDED UNEVENTFULLY. TROUBLESHOT LANDJan 28, 2011 · N140QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA2011011204408Unknown · smokeCOCKPIT FILLED WITH SMOKE AFTER MAIN BATTERY SELECTED ON AND AVIONICS TURNED ON. A GPU WAS ALREADY CONNECTED BEFORE POWER-UP. POWERED UP ACFT WITH GROUND POWER CART. NO SIGHT OR SMELL OF SMOKE FOUND. RAN ENGINES, AND CHECKED ALL SYS IN PRE-FLIGHT CHECKLISTJan 11, 2011 · N140QS · Raythn 400ARAYTHEON · Air Distribution SystemSDR DXTA2011011104405Shutoff Valve · leakingAFTER TAKEOFF WITH 4000 LBS FUEL (1200 LBS. IN FUSELAGE) AND CLIMBING THROUGH 10,000 FT, LT WING OVER PRESSURE ANNUNCIATOR ILLUMINATED. FUEL WAS SEEN STREAMING FROM UNDER THE LT WING. THE LT TRANSFER PUMP THEN SHUTOFF AND THE OVER PRESSURE LIGHT EXTINGUISHED.Jan 7, 2011 · N140QS · Raythn 400ARAYTHEON · Fuel Dump SystemSDR DXTA2010122304374Unknown · unknownDURING CLIMBOUT PAST 7000FT, NOTICED EXCESSIVE FUEL VENTING FROM LT WING. APPEARED TO BE NACA VENT BELOW FUEL CAP. YELLOW MASTER CAUTION ILLUMINATED WITH LT WING TANK OVER PRESSURE ANNUNCIATOR. FUEL TRANSFERRING FROM FUSELAGE TO WINGS. FUEL LEAK STOPPED DUDec 22, 2010 · N140QS · Raythn 400ARAYTHEON · Aircraft Fuel Distribution SystemSDR DXTA2010121904368Fuel Cell · leakingDURING CLIMB, FUEL OBSERVED LEAKING FROM UNDER LT WING. FUEL WAS TRANSFERRING FROM FUSELAGE TANKS AND WING FUEL GAUGES, INDICATED FULL LEVELS. DURING DESCENT, FUEL LEAKAGE APPEARED TO STOP, APPROX 15 MINUTES AFTER INITIAL DISCOVERY OF LEAK. INSTALLED NEW PILDec 17, 2010 · N140QS · Raythn 400ARAYTHEON · Fuel StorageSDR DXTA2010112304318Valve · malfunctionedDEPARTED & 4 MINUTES INTO CLIMBOUT, LT WING OVERPRESSURE LIGHT CAME ON. OBSERVED FUEL STREAMING OUT OF LT WING APPROX 2 FT FROM THE TIP NEAR THE OVERPRESSURE VALVE AREA. AFTER A COUPLE OF MINUTES OVERPRESSURE LIGHT WENT OUT & FUEL STOPPED FLOWING OUT OF WINov 22, 2010 · N140QS · Raythn 400ARAYTHEON · Aircraft Fuel Distribution SystemSDR DXTA2010111104304Fuel Sys · unknownDURING CLIMBOUT TROUGH 9500 FT, NOTICED STEADY STREAM OF FUEL LEAK FROM UNDER THE LT WING. ABOUT 2 MIN LATER THE LEAK STOPPED. CONNECTED FUEL HOSE AND TRANSFERED FUEL TO FUSELAGE TANKS. FILLED LT WING. LET PUMP RUN TO CHECK FOR FUEL BYPASS INTO SURGE TANK. Nov 10, 2010 · N140QS · Raythn 400ARAYTHEON · Fuel StorageSDR DXTA2010111004303Fuel Cell · overservicedDURING CLIMBOUT THROUGH 8000 FT, NOTICED A STEADY STREAM OF FUEL COMING FROM UNDER THE LT WING. DURING RETURN TO AIRPORT, NOTICED THE STREAM STOPPED AS ACFT LEVELED OFF AT 5000 FT. FOUND FUEL CELL OVERSERVICED.Nov 9, 2010 · N140QS · Raythn 400ARAYTHEON · Fuel StorageSDR DXTA200702407Unknown · unknownDURING DESCENT WHEN SPEED BRAKES WERE EXTENDED, THE AIRPLANE ROLLED TO THE RT. WHEN THE SPEED BRAKES WERE EXTENDED IN LEVEL FLIGHT, NO ROLL CHANGES WERE NOTED. C/W SPEED BRAKE SYSTEMS, OPS CHECKS. CHECKED RIGGING & CABLE TENSIONS ALL CHECKS GOOD. IAW 400XP Aug 15, 2007 · N140QS · Beech 400A · Drag Control SystemSDR DXTA200601436Landing Gear · inoperativeGEAR WOULD NOT RETRACT AFTER TAKEOFF. ITEM IS UNDER INVESTIGATION.Jun 13, 2006 · N140QS · Beech 400A · Landing Gear Retraction/Extension SystemSDR DXTA200601383Connector · dirtyON TAXI, LOST ALL BRAKES. THE ANTISKID WAS ARMED BUT BEGAN TO FLICKER A FAIL MESSAGE BUT NEVER STEADY. TURNING THE ANTISKID OFF, HAD FULL BRAKES. TROUBLESHOT BRAKE SYSTEM. INSPECTED AND CLEANED TRANSDUCERS. ACCESSED ANTI SKID CONTROL BOX AND CLEANED CONNEMay 7, 2006 · N140QS · Beech 400A · Brake Anti-Skid SectionSDR DXTA200601380Controller · noneDURING CLIMBOUT AN UNUSUAL ODOR WAS PRESENT IN THE COCKPIT. ODOR BECAME STRONG ENOUGH THAT AN IMMEDIATE LANDING WAS MADE. NO SMELL ON GROUND OR DURING RUNUP. POWER SETTINGS MADE NO DIFFERENCE IN INTENSITY. UPON INSPECTION, FOUND CABIN VIP SEAT TEMP CONTROLMay 3, 2006 · N140QS · Beech 400A · Cabin Temperature ControllerSDR DXTA200601276Pcb · malfunctionedNORMAL BRAKES FAILED TO ENGAGE TO STOP AIRCRAFT ON TAXI-IN,AIRCRAFT SKIDDED ABRUPTLY WHILE APPLYING NORMAL BRAKE BRESSURE,THEN CONTINUED TO ROLL FOR APPROX 3 TO 4 FT UNTILL EMERGENCY BRAKE APPLIED. - TROUBLESHOT BRAKES AND ANTI-SKID SYSTEM, BLED BRAKES AND REPMar 2, 2006 · N140QS · Beech 400A · Landing Gear Brake SystemSDR DXTA200500977Odor · detectedWHEN ENGINE, WING, AND TAIL ANTI ICE ON STRONG ODOR WAS PRESENT IN CABIN. ITEM IS UNDER INVESTIGATION.Sep 20, 2005 · N140QS · Beech 400A · Air Distribution SystemSDR DXTA200500911Warning Light · illuminatedAFTER TAKEOFF RED AP PITCH TRIM FAIL LIGHT CAME ON AND AP KICKED OFF. AIRCRAFT CHECKLIST COMPLETED AND LANDED AS SOON AS PRACTICAL. ITEM IS UNDER INVESTIGATION.Aug 21, 2005 · N140QS · Beech 400A · Autopilot System
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