N696QS

Service difficulty reports not matched to an aircraft · 18

They name N696QS, 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 = 'N696QS' 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 DXTA2017042306399Engine · power lossWITH EEC IN MANUAL, TAKEOFF POWER OBTAINED. DURING CLIMB, NOTICED LARGE THROTTLE SPLIT AND NOTICED THAT THE LEFT ENGINE NOT DEVELOPING TAKEOFF THRUST. CONTINUED CHECKING THROUGH CLIMB ONLY GOT 85% N1 101% N2 WITH THROTTLE TO FORWARD STOP.Apr 23, 2017 · N696QS · Cessna 560XL · Engine (Turbine/Turboprop)SDR CWQR20160720022Cable · brokenTHIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLEDJul 20, 2016 · N696QS · Cessna 560XL · Elevator Tab Control SystemSDR CWQR20160720021Cable · frayedTHIS CABLE ASSEMBLY IS REPLACED AT THE AIRCRAFT OPERATOR REQUEST BECAUSE OF RELIABILITY ISSUES. INSPECTED CABLE AFTER REMOVAL, PREFORMED LOOP TEST AND FOUND TO BE UNSERVICEABLE PER AMM CHAPTER 20-10-04. NEW CABLE ASSEMBLY INSTALLED.Jul 20, 2016 · N696QS · Cessna 560XL · Elevator Tab Control SystemSDR CWQR20160701020Hose · blownDURING A SCHEDULED MAINTENANCE GEAR SWING THE RT GEAR UP-LOCK HOOK EXTEND HOSE ASSY, BLEW A HOLE IN IT ABOUT .5 INCH FROM THE SWEDGED FITTING HOSE END. THIS IS THE HOSE END THAT ATTACHES TO THE UP-LOCK ACTUATOR FITTING. NO MAINTENANCE PERSONNEL WERE HURT OR DAJul 1, 2016 · N696QS · Cessna 560XL · Landing Gear Retraction/Extension SystemSDR DXTA2015051906020Coalescer Bag · odorMILDEW SMELL AT FLIGHT LEVEL 410. R & R WATER SEPARATOR CONDENSER SOCK IAW AMM 21-51-00. OPS & LEAK CHECKED GOOD.May 18, 2015 · N696QS · Cessna 560XL · Humidity Control SystemSDR DXTA2014020505639Brake Sys · contaminatedUPON LANDING BRAKES WERE EVENLY APPLIED BUT ASYMMETRICAL BRAKING WAS EXPERIENCED, ACFT PULLED TO THE LT, BRAKES WERE RELEASED & ACFT DIRECTION OF TRAVEL WAS CORRECTED & BRAKES WERE EVENLY APPLIED AGAIN & AGAIN THE ACFT PULLED TO THE LT, WE WERE ABLE TO CLEAR TFeb 4, 2014 · N696QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTA2013100705530Skin · corrodedCORROSION DAMAGE WAS FOUND AT MULTIPLE LOCATIONS BETWEEN WS 117.9 AND 184.9 ON THE LT AND RT UPPER OTBD WING SKINS AND THE LT AND RT T/E SKINS. AFTER BLENDING TO REMOVE ALL CORROSION, THE MINIMUM REMAINING THICKNESSES OF THE AFFECTED SKINS WERE RECORDED FOR ESep 13, 2013 · N696QS · Cessna 560XL · Wing, Plate/SkinSDR DXTA2013050805388Blades · damagedACCOMPLISH BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS. ACCOMPLISHED PREINDUCTION GROUND PERFORMANCE RUN AND TRANSIENT VIBRATION SURVEY. ACCOMPLISHED A BORESCOPE INSPECTION OF THE COMBUSTION LINER NUTS. ACCOMPLISHEApr 1, 2013 · N696QS · Cessna 560XL · Turbine Engine Combustion SectionSDR DXTR20120424002Line · chafedLEFT BRAKE LINE FWD OF COPILOTS RT RUDDER PEDAL IS CHAFED DUE TO RUDDER PEDAL CONTACT. R & R LT BRAKE LINE ASSY FWD OF COPILOTS RT RUDDER PEDAL IAW MM 20-10-06.Apr 24, 2012 · N696QS · Cessna 560XL · Landing Gear Brake SystemSDR DXTR20120424001Bracket · crackedRUDDER AUTOPILOT CABLE BRACKET AT AFT CANTED BULKHEAD IS CRACKED ON INBD RIVET LINE. R & R RUDDER AUTOPILOT CABLE BRACKET IAW SRM 51-40-03 AND MM 22-11-01.Apr 24, 2012 · N696QS · Cessna 560XL · Fuselage Miscellaneous StructureSDR DXTA2011022104472Pitot Tube · obstructedBOTH PILOTS PFD'S DISPLAYED AN AMBER IAS MESSAGE AFTER PASSING THROUGH 160 KTS. AT MINIMUM LT PILOTS IAS INDICATING 160, RT PILOTS INDICATING 166 & STANDBY INDICATING 167. ACCELERATED TO 200 KTS, SPLIT INCREASED TO ABOUT 9 KTS BETWEEN PRIMARY IAS INDICATORS Feb 20, 2011 · N696QS · Cessna 560XL · Pitot/Static SystemSDR DXTA2009013103481Water Separator · dirtyBOROSCOPE COMBUSTION SECTION FOUND IT TO BE GOOD. INSPECTED INTAKE COLD EXHAUST ALSO FOUND THEM TO BE GOOD. REMOVED OLD WATER SEPARATOR. INSTALLED NEW WATER SEPARATOR. IAW MM CH 21-51-00. RAN APEX ELS SYS IAW MM CH 21-11-00 WITH NO DEFECTS NOTED.Jan 31, 2009 · N696QS · Cessna 560XL · APU Bleed Air SystemSDR DXTA2009020203481Unknown · smokeSMOKE IN THE COCKPIT CAME THROUGH THE GASPER FANS WITH THE APU RUNNING ON THE GROUND.Jan 31, 2009 · N696QS · Cessna 560XL · Air Distribution SystemSDR DXTA2009020203480Unknown · smokeSMOKE IN THE COCKPIT CAME THROUGH THE GASPER FANS WITH THE APU RUNNING ON THE GROUND.Jan 31, 2009 · N696QS · Cessna 560XL · Air Distribution SystemSDR DXTA200702197Actuator · defectiveON DEPARTURE AFTER RAISING THE GEAR, THE GEAR UNLOCK LIGHT ON AND THE GREEN NOSE GEAR LIGHT ILLUMINATED. RECYCLED THE GEAR AND HAD THE SAME INDICATION. EXTENDED GEAR AND GOT THREE GREEN. LT GEAR DOWN AND LANDED. REMOVED DEFECTIVE NOSE GEAR ACTUATOR AND INSMay 15, 2007 · N696QS · Cessna 560XL · Landing Gear ActuatorSDR DXTA200702088Windshield · failedLT WINDSHIELD SHATTERED. RECEIVED LT FAULT, SELECTED OFF, LT O'HEAT WINDSHIELD, ARCED AND SHATTERED, DIVERTED. [SUP 4-19-07] REPLACED WINDOW IAW MM 56-11-00Apr 7, 2007 · N696QS · Cessna 560XL · Flight Compartment WindowsSDR DXTA200702017Transmitter · malfunctionedDURING POWER REDUCTION TO IDLE AT 10.000 FT, LT ENGINE OIL PRESSURE DROPPED TO BELOW 20 PSI AND JUMPED BACK AND FORTH TO 40 PSI. ON POWER INCREASE, PRESSURE STAYED AROUND 30 PSI. ENGINE WAS LEFT AT IDLE UNTIL COMPLETION OF FLIGHT. LOWERED NR 1 ENGINE COWLING.Mar 13, 2007 · N696QS · Cessna 560XL · Engine Oil PressureSDR DXTA200500857Transducer · inoperativeON TAKEOFF ROLL, APPROACHING 60K MASTER CAUTION LIGHT ILLUMINATED WITH ANTI-SKID ANNUNCIATOR LIGHT SWITCHES PROPER POSITION, TAKEOFF ABORTED. T/S TO BAD RT WHEEL TRANSDUCER. INSTALLED NEW TRANSDUCER OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CJul 24, 2005 · N696QS · Cessna 560XL · Brake Anti-Skid Section
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