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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR 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 TSDR DXTA2008111403355Rib · crackedWHILE COMPLETING A LUBRICATION SEVERAL CRACKS HAVE BEEN FOUND IN HORZ STAB RIBS, P/N 65320XX-XXX.SDR 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 32-31SDR 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.SDR 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. RESDR 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.SDR 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 BSDR 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 SWITCHSDR 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.SDR 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 SDR 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 HANSDR 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 ARESDR 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 WASDR 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 ANSDR 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 NSDR 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.SDR 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 GOODSDR 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 CHECKESDR 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 SDR 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 SDR 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 SDR 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 SDR 97DXTA091Inverter · failedFLT 72905 - NR 2 INVERTER INOPERATIVE. (X)SDR 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.
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