N330QS

Service difficulty reports not matched to an aircraft · 44

They name N330QS, 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 = 'N330QS' 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 2008FA0000811Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000810Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000809Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000808Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000807Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000806Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000805Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000804Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000803Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000802Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000801Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000800Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000799Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000798Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000797Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000796Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000795Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000794Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000793Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000792Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR 2008FA0000791Rib · crackedWHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH STABILIZERS, 8 CRACKED RIBS ON THE RT SIDE AND 13 CRACKED RIBS ON THE LT SIDE WERE FOUND. ALL OF TOct 29, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR DXTA2008111403355Rib · crackedWHILE COMPLETING A LUBRICATION SEVERAL CRACKS HAVE BEEN FOUND IN HORZ STAB RIBS, P/N 65320XX-XXX.Oct 24, 2008 · N330QS · Cessna 560CESSNA · Horizontal Stabilizer, Spar/RibSDR DXTA200702675Uplock Switch · out of adjustAFTER RETRACTING THE GEAR, THE HYD PRESS ON LIGHT AS WELL AS THE GEAR UNLOCKED LIGHTS WERE ON. WE RAN THE CHECKLISTS BROUGHT THE GEAR DOWN AND USED THE BLOW DOWN AS A PRECAUTION. INSPECTED AND ADJUSTED UP-LOCK SWITCH. OPS CHECKED GOOD IAW CESSNA 560 MM 32-31Dec 13, 2007 · N330QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200702665Controller · obstructedON TAKE-OFF CABIN CONTROLLER FAILED TO MAINTAIN CABIN PRESSURIZATION. TROUBLESHOT TO VENT BLOCKAGE ON CONTROLLER. CLEARED BLOCKAGE AND PERFORMED OPS CHECK. OPS CHECK GOOD. IAW CE 560 MM CH 21-31-00.Dec 9, 2007 · N330QS · Cessna 560CESSNA · Cabin Pressure ControllerSDR DXTA200702282Landing Gear · inoperativeON DEPARTURE, LANDING GEAR WOULD NOT RETRACT. AUXILLARY GEAR CONTROL WAS ACTIVATED AS A PRECAUTION. [07-12-07] T/S FOUND LEFT GEAR SQUAT SWITCH OUT OF ADJUSTMENT. ADJUSTED SWITCH. IAW CESSNA 560 MM. CH. 32-30-01. OPS. CHECK SATISFACTORY. ALSO BLED MLG. REJun 21, 2007 · N330QS · Cessna 560CESSNA · Landing Gear Retraction/Extension SystemSDR DXTA200702272Display · failedON TAXI OUT PFD NR 2 FAILED. BURNED ELECTRONIC SMELL WAS OBSERVED. [07-10-07] REMOVED AND REPLACED NR 1 PFD IAW CESSNA 560 MM 34-23-02. PFD OPS CHECKS SERVICEABLE.Jun 17, 2006 · N330QS · Cessna 560CESSNA · Central DisplaySDR DXTA200601293Hydraulic System · underservicedCO-PILOTS SIDE RT BRAKE PEDAL IS SOFT. WILL STOP AIRCRAFT HOWEVER WILL TRAVEL APPROX 1.5 INCHES BEFORE PRESSURE IS FULL. WHEN APPLYING BRAKES LEFT SIDE WILL HOLD WHILE RT SIDE WILL TRAVEL FORWARD BEFORE SAME AMOUNT OF PRESSURE IS FELT. PERFORMED ANTI-SKID BMar 13, 2006 · N330QS · Cessna 560CESSNA · Brake Anti-Skid SectionSDR DXTA200601257Proximity Switch · malfunctionedAFTER TAKEOFF, GEAR RETRACTION THE GEAR HORN WARNING SOUNDED. IT LASTED FOR A COUPLE SECONDS, THEN THE GEAR UNSAFE LIGHT WENT OUT AS WELL AS THE HORN STOPPED. ALL GEAR INDICATIONS AFTER LANDING WERE NORMAL. FOUND INOPERATIVE RIGHT THROTTLE 70 PERCENT SWITCHFeb 22, 2006 · N330QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200601230Warning System · malfunctionedAFTER TAKEOFF UPON GEAR RETRACTION, THE GEAR WARNING HORN SOUNDED. IT LASTED FOR A COUPLE SECONDS THEN GEAR UNSAFE LIGHT (RED LIGHT) WENT OUT AS WELL AS THE HORN STOPPPED. ALL GEAR INDICATIONS AFTERWARDS WERE NORMAL INCLUDING THE 150K HORN WARNING CHECK.Feb 2, 2006 · N330QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200500684Bracket · damagedAFTER DEPARTURE GEAR UNSAFE LIGHT REMAINED LIT AND HYD PRESS LIGHT ALSO REMAINED ILLUMINATED. GEAR RETURNED TO DOWN AND LOCKED AFTER PERFORMING CHECK LIST ITEMS. REPLACED ALL PARTS OF BRACKET ASSY PER CE500 SERIES COMPONENT M/M 32-20-01, PERFORMED LANDING Apr 18, 2005 · N330QS · Cessna 560CESSNA · Main Landing Gear Attach SectionSDR DXTA200400361Position Switch · malfunctionedAFTER POSITIVE RATE OF CLIMB DURING TAKEOFF THE GEAR WOULD NOT FULLY RETRACT, WHEN THE GEAR SELECTOR WAS MOVED TO THE UP POSITION THE MAIN GEARS WOULD NOT STOW AND THE RED GEAR UNLOCK LIGHT REMAINED ILLUMINATED. TROUBLESHOT LANDING GEAR SYSTEM, FOUND GEAR HANAug 16, 2004 · N330QS · Cessna 560CESSNA · Landing Gear Position and WarningSDR DXTA200300172Odor · detectedLOUD BANG WAS HEARD AND FELT WHILE CLIMBING THROUGH FL 37 AN ODOR WAS MOMENTARILY ASSOCIATED WITH IT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO LAS. UPON LANDING THE FIRE PERSONNEL REPORTED LARGE QUANTITIES OF SMOKE EMANATING FROM THE ENGINE ARENov 29, 2003 · N330QS · Cessna 560CESSNA · Air Distribution SystemSDR DXTA200300144Relay · failedAFTER SELECTING GEAR DOWN, POWER BRAKE LOW PRESS, ANTI SKID INOP ANNUNICATORS CAME ON, NO BRAKE PRESS EITHER SIDE. GO AROUND, ON SECOND APPROACH BOTH LIGHTS REMAINED ON FOR 5 SECONDS THEN EXTINGUISHED. BOTH PILOTS HAD POSITIVE BRAKE PRESSURE, NORMAL LANDING WAOct 21, 2003 · N330QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200300138Screw · looseAFTER LANDING AT BUY, BRAKES FAILED ON BOTH PILOT’S AND FIRST OFFICER’S SIDES, HAD TO USE EMERGENCY BRAKE TO STOP AIRCRAFT. FOUND LOOSE SCREW ON RT SPEED TRANSDUCER AND PINS LOOSE, ALSO FOUND LT SPEED TRANSDUCER VERY HARD TO TURN AND DRIVE CAP BAD. REMOVED ANOct 15, 2003 · N330QS · Cessna 560CESSNA · BrakeSDR DXTA200300137Brake · malfunctionedON TAXI OUT FIRST 5 BRAKE APPLICATIONS WERE NORMAL, ON THE SIXTH APPLICATION BRAKE PEDALS WENT TO THE FLOOR, CO-PILOTS BRAKES WERE SPONGY BUT AFTER PUMPING BRAKES WAS ABLE TO STOP AIRCRAFT, TAXI AIRCRAFT AND APPLIED BRAKES 30-40 TIMES FOUND BRAKES TO OPERATE NOct 14, 2003 · N330QS · Cessna 560CESSNA · BrakeSDR DXTA200300091Brake · failedCOPILOT'S BRAKE FAILED ON TAXI, PILOT'S BRAKES PULSATING DURING SLOW TAXI. - PERFORMED BRAKE BLEED PROCEDURE IAW CE560 MM CHAPTER 32-42-01 LEAK CHECK GOOD. FUNCTIONAL TEST GOOD.Aug 15, 2003 · N330QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200300047Wire Harness · defectiveON LANDING, BRAKE PRESSURE AVAILABLE BUT SLOW TO APPLY. DURING TAXI IN, ABOUT 10 MPH, BRAKES RELEASE AND ENGAGE INTERMITTENTLY. TROUBLESHOT AND FOUND RT ANTI-SKID WIRING HARNESS DEFECTIVE. REMOVED & REPLACED HARNESS IAW 560 M/M CH 32-42-07, OPS CHECKED GOODJun 14, 2003 · N330QS · Cessna 560CESSNA · Landing Gear System WiringSDR DXTA200300046Brake · failedON TAXI IN DEPRESSED BRAKE AND AIRCRAFT WOULD NOT STOP FOR 2-3 SECOND . WITH BRAKE PEDALS DEPRESSED AIRCRAFT CONTINUED TO ROLL FOR SHORT DISTANCE. ITEM IS UNDER INVESTIGATION. INSPECTED BRAKE RESEVIOR, ACUMULATOR, MASTER CYLINDERS AND BREAK ASSY'S ALL CHECKEJun 11, 2003 · N330QS · Cessna 560CESSNA · Landing Gear Brake SystemSDR DXTA200300007Wire · chafedDURING INSPECTION, AN 8 GAGE DC POWER DISTRIBUTION CABLE WAS FOUND TO HAVE CHAFED AND ARCING AGAINST A RELAY. THIS CABLE IS ENCLOSED BEHIND A PANEL AND DIRECTLY ADJACENT TO A SHROUDED FUEL CROSSFEED LINE, AND CABIN OUTFLOW VALVES. SHOULD A FIRE START, IT IS Feb 10, 2003 · N330QS · Cessna 560CESSNA · Electrical Power System WiringSDR DXTA20030007Wire · chafedDURING INSPECTION, AN 8 GAGE DC POWER DISTRIBUTION CABLE WAS FOUND TO HAVE CHAFED AND ARCING AGAINST A RELAY. THIS CABLE IS ENCLOSED BEHIND A PANEL AND DIRECTLY ADJACENT TO A SHROUDED FUEL CROSSFEED LINE, AND CABIN OUTFLOW VALVES. SHOULD A FIRE START, IT IS Feb 10, 2003 · N330QS · Cessna 560CESSNA · Electrical Power System WiringSDR DDXTA20030007Wire · chafedDURING INSPECTION, AN 8 GAGE DC POWER DISTRIBUTION CABLE WAS FOUND TO HAVE CHAFED AND ARCING AGAINST A RELAY. THIS CABLE IS ENCLOSED BEHIND A PANEL AND DIRECTLY ADJACENT TO A SHROUDED FUEL CROSSFEED LINE, AND CABIN OUTFLOW VALVES. SHOULD A FIRE START, IT IS Feb 10, 2003 · N330QS · Cessna 560CESSNA · Electrical Power System WiringSDR 98ZZZX4821Wire · failedSMOKE OBSERVED COMING FROM THE AFT LAVATORY AREA. BATTERY SWITCH WAS TURNED OFF, AND GROUND POWER UNIT DISCONNECTED FROM ACFT. A CHECK OF CIRCUIT BREAKERS IN THE COCKPIT AND AFT POWER JUNCTION BOXES SHOWED ALL CB' S WERE ENGAGED. FOUND WIRE GOING FROM K55 Oct 19, 1998 · N330QS · Cessna 560CESSNA · Electrical Power System WiringSDR 97DXTA091Inverter · failedFLT 72905 - NR 2 INVERTER INOPERATIVE. (X)Nov 8, 1996 · N330QS · Cessna 560CESSNA · AC InverterSDR 96ZZZX6171Rudder Skin · crackedLT RUDDER SKIN HAS 2 INCH CRACK APPROX 3 INCHES BELOW TRIM TAB FWD OF HINGE LINE. THIS IS THE SECOND DISCOVERED VERTICAL CRACK, AND THE SIXTH RUDDER SKIN CRACK OVERALL. CESSNA WAS NOTIFIED BY SERVICE CONDITION REPORT.Oct 30, 1996 · N330QS · Cessna 560CESSNA · Rudder, Plate/Skin
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