N679QS
Service difficulty reports not matched to an aircraft · 27
They name N679QS, 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 = 'N679QS' 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 = 'N679QS' 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 JGVR20181220003Axle · corrodedNOSE WHEEL AXLE TUBE AND BUCKETS ARE CORRODED.REMOVED CORRODED WHEEL AXLE TUBE AND BUCKETS. INSTALLED NEW CUSTOMER SUPPLIED WHEEL AXLE TUBE AND BUCKETS (2EA) IAW CESSNA 560XL MM 32-41-01.SDR JGVR20181220002Structure · corrodedL/H HORIZONTAL STABILIZER HAS AREA OF CORROSION UNDER PANEL 340DL NEAR AFT SPAR. BLENDED, PERFORMED NDT, TREATED AND PAINTED AREA OF MINOR CORROSION UNDER PANEL 340DL ON LH HORIZONTAL STAB NEAR AFT SPAR. PER CESSNA MEMO DQ16801M1 DATED DECEMBER 14, 2018. PREPPSDR JGVR20181220001Skin · damagedDURING NOSE LANDING GEAR WELL CORROSION INSPECTION FOUND SKIN PEELED UP BY RH NLG DOOR MIDDLE HINGE AREA AND RH NLG DOOR DAMAGED. REPAIRED CRACKS IN THE RH NOSE SKIN JUST OUTBOARD OF THE CENTER HINGE AND CRACKS ON THE RH NLG DOOR PER AEROSPACE QRD ERO-936348 RSDR DXTA2016102406322Switch · failedDURING FLIGHT AT 25000, THE RIGHT ECC MANUAL LIGHT CYCLED ON AND OFF A FEW TIMES AND THE RIGHT ENGINE N1 FLUCTUATED BETWEEN 80 AND 89 PERCENT.NO CHANGES NOTICED WITH THE ANTI ICE ON/OFF. INSPECTED EEC CONNECTOR & PCBS IN AFT J BOX. NO DEFECTS NOTED. PERFORMESDR DXTA2014042105737Power Unit · malfunctionedSMOKE FILLED CABIN & COCKPIT ON APU STARTUP WITH BLEED AIR ON. REMOVED AND REPLACED AUX POWER UNIT IAW MM 49-10-00. COMPLIED WITH ECU BURN-IN AND COALESOR SOCK CHANGE IAW MM 21-51-00. OPS AND LEAK CHECKS GOOD.SDR DXTA2014030305670Structure · dirtyTHERE IS A STRONG ODOR OF JET FUEL IN AFT ACCESSORY COMPARTMENT. A DRIP IS VISIBLE AT THE BOTTOM OF APU CONTAINER. OPENED PANEL 322AT INSPECTED & CLEANED APU BAY, FOUND NO DEFECTS, CLEANED DRAIN LINES IN MX BAY. RAN ACFT APU FOR SEVERAL MINUTES, INSPECTED &SDR DXTA2013112705582Tube · damagedDURING CLIMB OUT WING O HEAT R CAME ON & STAYED ON FOR ABOUT 10 SECONDS. WE REDUCED POWER TO APPROXIMATELY 70% N1. LIGHT CAME ON AGAIN AT SHORT FINAL FOR ABOUT 3 SECONDS WITH POWER AT ABOUT 50% N1. REPLACED HEAT SHIELD & BLANKET PN 6621281-30, NSN, PN F7802SDR DXTA2013081505476Switch · failedAFTER LANDING, CABIN INTERIOR LIGHTS WERE TURNED ON. WHEN THE AIRSTAIR DOOR WAS OPENED AND LOCKED IN THE FULL DOWN POSITION ALL THE ENTRY AND CABIN INTERIOR LIGHTS WENT OUT. TROUBLESHOT TO FAULTY GALLEY SWITCH PANEL. R & R SWITCH ASSY IAW MM. SYS OPS CHESDR DXTA2013072905458Actuator · failedON DEPARTURE, DURING GEAR RETRACTION, RED GEAR UNSAFE LIGHT WOULD NOT GO OUT. HYD PRESSURE LIGHT STAYED ON AND THE STAB MISCOMPARE LIGHT CAME ON. PLANE FLEW LIKE GEAR HAD RETRACTED. ON GEAR EXTENSION ALL FUNCTIONED NORMALLY. R & R THE NOSE GEAR UPLOCK ACTSDR DXTA2013061105415Brake Sys · contaminatedTHE RIGHT TOE BRAKE PRESSURE SEEMS TO DIMINISH AS PRESSURE IS APPLIED, LEAVING AN ASYMETRICAL ALIGNMENT OF THE PEDALS THEMSELVES. BRAKES ARE GRABBING, BUT THE RT SIDE FEELS LIKE THERE IS VERY LITTLE PRESSURE IN THE LINE. BLED AIR FROM BRAKES AS REQUIRED IAWSDR DXTR20130417001Attach Bracket · crackedRIGHT ELEVATOR OTBD ATTACH POINT BRACKET CRACKED. R & R RT ELEVATOR OTBD ATTACH POINT BRACKETS IAW SRM 51-40-03, 51-40-06, 51-40-09 & BALANCED IAW SRM 51-60-02.SDR DXTA2009110503847Brake Assy · malfunctionedON LANDING ROLLOUT BRAKES GRABBED MULTIPLE TIMES BEFORE SLOWING TO TAXI SPEED, WHEN BRAKING BECAME NORMAL. VISUALLY INSPECTED BRAKES AND TIRES FOR WEAR AND DEFECTS. NO DEFECTS NOTED. NO DOLLS EYES TRIPPED ON FAULT DISPLAY UNIT IN NOSE COMPARTMENT. PERFORMED ASDR CWQR200809Support Bracket · crackedDURING A PHASE 104 INSPECTION, FOUND THE SUPPORT BRACKET CRACKED. CRACK IS ABOUT 1.5 INCHES LONG AND IS CENTERED AT THE ATTACH POINT FOR THE VALVE. SERVICE CONDITION REPORT HAS BEEN FILED WITH MFG UNDER SCR NR 376160. (K)SDR CWQR200808Support Bracket · crackedDURING A PHASE 1-4 INSP, FOUND THE SUPPORT BRACKET CRACKED, CRACK IS LOCATED IN THE SUPPORT BRACKET FOR THE ECU, THE CRACK INTERSECTS A HOLE FOR THE NUTPLATE THAT ATTACHES ONE OF THE ECU MOUNTING BOLTS. SERVICE CONDITION REPORT HAS BEEN FILED WITH MFG UNDER SCSDR DXTA200803097Brake Sys · malfunctionedLT BRAKE IS EXTREMELY SENSITIVE AIRCRAFT JERKS LT ON EVERY BRAKE APPLICATION. R&R LT BRAKE ASSY IAW MM 32-42-01. INSTALLED LT WHEEL ASSY IAW MM 32-41-02, BLED BRAKES IAW MM 32-42-00, LEAK CHECK AND OPS CHECK GOOD.SDR CWQR200803Control Cable · improper partDURING A ROUTINE CABLE REPLACEMENT OF AILERON CABLE PN 6660002-12, WE FOUND THAT THE CABLE HAD A SWAGED BALL AND A CLEVIS END INSTALLED. THIS CABLE ASSY SHOULD HAVE BEEN MANUFACTURED WITH THE SWAGED BALL WITHOUT THE CLEVIS. THE CABLE ASSY HAS BEEN SENT BACK TOSDR DXTA20082932Pump · inoperativeWHILE TAXING, ANTI SKID INOP LIGHT CAME ON , FOLLOWED BY LOW BRAKE PRESS LIGHT AND SUBSEQUENT LOSS OF NORMAL BRAKING. REPLACED POWER BRAKE HYDRAULIC PUMP WITH NEW CUSTOMER SUPPLIED. REPLACED ANTI-SKID RELAY WITH NEW P/N: MS2416602, REMOVED RELAY P/N: MS241660SDR DXTA20082923Brake · contaminatedUPON SHUTDOWN , SUFFICENT SMOKE FROM RT MAIN GEAR. SMOKE PERSISTED FOR 15 MIN. REMOVED RT MAIN WHEEL AND INSP WHEEL AND BRAKE ASSY FOUND EXCESSIVE GREASE ON INSIDE OF WHEEL, CLEANED GREASE AND FOUND SMALL SUPERFICIAL BURN MARKS. REINSTALLED RT MAIN WHEEL IAW SDR DXTA200702693Check Valve · bypassing(LO HYD FLOW RT) ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL AT 40 KNOTS. NO SECONDARY INDICATIONS. ABORTED TAKEOFF. REMOVED AND REPLACED R/H LO HYD. FLOW CHECK VALVE WITH A NEW UNIT. PERFORMED OPS TEST. CHECKED SATISFACTORY NO LEAKS NOTED. I.AW. CE-560XL M.M. CSDR DXTA200702633Limit Switch · out of adjustHORIZONTAL STAB MOVED NORMALLY UPON FLAP RETRACTION AFTER TAKEOFF. AT 16000 FT AND LEVEL FLIGHT 280 KNOTS, "STAB MISCOMPARE" AND "HYD PRESS" ANNUNCIATORS CAME ON. ADJUSTED UP AND DOWN LIMIT SWITCHES IAW 560XL MM CHP. 27-40-00. PERFORMED T/O WARNING SYS AND HOSDR DXTA200702200Unknown · unknownIN CRUISE, AT FL300 "STAB MIS COMP" AND "HYD PRESS" ANNUNCIATORS ILLUMINATED. CONNECTED AIR DATA TEST SET AND PERFORMED FULL "TWO POSITION HORIZONTAL STAB OPERATIONAL CHECK" AND "AIRSPEED SWITCH AND HORIZONTAL STAB OPS CHECK" IAW CH 27-40-00 OF THE CE-560XL MMSDR DXTA200601603Actuator · defectiveAFTER TAKEOFF WHEN GEAR WAS SELECTED UP ALL GREEN LIGHTS EXTINGUISHED THEN RED LIGHT EXTINGUISHED FOLLOWED BY NOSE GEAR GREEN LIGHT COMING ON WITH NOISE OF NOSE GEAR DOWN RECYCLED GEAR WITH SAME RESULT. REPLACE NLG ACTUATOR AND NLG UPLOCK ACTUATOR OPERATIONALSDR DXTA200601562Warning Light · false activationWHEN THE GEAR WAS SELECTED UP AFTER TAKEOFF THE GEAR LIGHTS SEQUENCED OUT AS NORMAL THEN NOSE GEAR GREEN LIGHT CAME BACK ON AND STAYED ON . AIR NOISE FROM GEAR CONFIRMED THAT NOSE GEAR SELECTED DOWN AND OBTAINED 3 GREENS. INSPECTED NOSE GEAR UPLOCK IAW M/M TSDR DXTA200501157Wheel · out of positionAFTER LIFT OFF EXCESSIVE AMOUNT OF FWD CONTROL PRESSURE REQUIRED FOR NORMAL CLIMB. AIRCRAFT ALMOST WANTED TO ROTATE BY ITSELF. THROUGHOUT FLIGHT, TRIM INDICATOR AT OR ABOVE FWD END OF WHOLE RANGE MARKINGS. UPON INSPECTION OF TRIM WHEEL FOUND TRIM POINTER IN SDR DXTA200500968Elevator · malfunctionedTHROUGH 110 KTS ON TAKEOFF ROLL FULL AFT ELEVATOR DID NOT INITIATE ROTATION TAKEOFF ABORTED. ITEM IS UNDER INVESTIGATION.SDR DXTA200500618Rudder · malfunctionedAIRCRAFT REQUIRES EXCESSIVE EFFORT FOR RUDDER CONTROL IN HIGH POWER SETTINGS ON GROUND AND INFLIGHT "AIRSPEED IS NOT AN ISSUE". FEELS AS IF YAW DAMPER IS ON, SUSPECT RUDDER BIAS SYSTEM. ITEM IS UNDER INVESTIGATION.SDR DXTA200400264Warning Light · illuminatedAFTER LANDING, DURING TAXI ANTISKID INOP AND LO BRAKE PRESS ANNUNCIATOR ILLUMINATED. BRAKES FELT HARD AND INEFFECTIVE BUT DID NOT GO TO THE FLOOR, USED EMERGENCY BRAKE TO STOP AIRCRAFT ON TAXIWAY. ITEM IS UNDER INVESTIGATION.
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