N339QS

Service difficulty reports · 70

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N339QS' AND registry_match = 'registration'
  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 DXTA2021111151650Sensor · defectiveLEED AIR: AT FL430 NORMAL ENGINE ONLY BLEEDS, PAX NOTIFIED US OF SMOKE/HAZE IN CABIN/ INITIATED QRC / UPON ENTERING CABIN I NOTICED A HAZE/ NO PERCEPTIBLE SMOKE/ BUT A SLIGHT ODER, DECLARED EMERGENCY/ DIVERTRED/ FOLLOWED QRC/QRH PROCEEDURES///SIGN-OFF////REMOVNov 10, 2021 · N339QS · Cessna 680CE · Pneumatic Distribution SystemSDR DXTA2020110704319Battery · inoperativeALL AFT INTERIOR EMERGENCY LIGHTS AND ALL EXTERIOR LIGHTS ARE INOPERABLE. PRE-FLIGHT SIGN OFF. SPOKEN WITH PILOTS AS THEY WERE STILL ON THE FIELD AND HAS FOUND THAT AFTER POWER WAS APPLIED TO THE AIRCRAFT FOR AN EXTENDED AMOUNT OF TIME THE EMERGENCY LIGHTINGNov 7, 2020 · N339QS · Cessna 680A · Emergency LightingSDR JGVR20200406002Door · corrodedCONFIRMED CORROSION ON EMERGENCY EXIT IN 20 AREAS, FOUND DURING TASK 52-20-00-2200. REMOVED FWD AND AFT CONTOUR RINGS. MECHANICALLY BLENDED 20 AREA OF INTERGRANULAR CORROSION INNER SIDE OF CONTOUR RINGS ON OUTER FACE OF E-EXIT IAW C680 SRM 51-70-02. CORROSION Apr 6, 2020 · N339QS · Cessna 680A · Emergency ExitsSDR JGVR20200406001Structure · corroded18 SPOTS OF CORROSION FOUND ON LH AND RH FWD DROPPED AISLE. MECHANICALLY BLENDED 18 SPOTS OF CORROSION ON LH AND RH FWD DROPPED AISLE IAW CESSNA 680 SRM 51-70-02. PERFORMED AN EDDY CURRENT AND ULTRASONIC THICKNESS INSPECTION OF THE 18 BLENDED SPOTS ON THE LH AApr 6, 2020 · N339QS · Cessna 680A · Fuselage Miscellaneous StructureSDR DXTA2020021763469Downlock Switch · defectiveLEFT MLG LANDING GEAR RETRACTION DID NOT RETRACT - L MAIN GEAR FAILED TO RETRACT. OVERSPEED TO 250 KNOTS. REMOVED LEFT MLG DOWNLOCK SWITCH PART NO: 6-0373-3 SERIAL NO: N/A AND INSTALLED CUSTOMER SUPPLIED NEW PART NO: 6-0373-3 SERIAL NO: N/A IAW CE680 M/M CHFeb 16, 2020 · N339QS · Cessna 680CE · Landing Gear Position and WarningSDR JGVR20181114004Spar Cap · corrodedFOUND CORROSION IN LH MLG WHEEL WELL AFT SPAR CAP APX W.S. 27.00. FOUND WHILE CLEANING FOD FROM DRAG ANGLE CORROSION REPAIRS.Nov 14, 2018 · N339QS · Cessna 680CE · Wing SparSDR JGVR20181114003Skin · corrodedLEVEL 2 CORROSION FOUND ON R/H WING UPPER INBOARD TRAILING EDGE WING SKIN P/N: 6922681-70 REQUIRED REPLACEMENTNov 14, 2018 · N339QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20181114002Skin · corrodedREMOVED L/H WING UPPER SKIN SECTION P/N 6922680-27 (ABOVE L/H MLG) DUE TO LEVEL 2 CORROSION.Nov 14, 2018 · N339QS · Cessna 680CE · Wing, Plate/SkinSDR JGVR20181114001Drag Angle · corrodedRH AND LH WING @ WING STATION 37 (FWD, MIDDLE, AFT) OVERWING DRAG ANGLES HAVE NUMEROUS AREAS OF CORROSION.Nov 14, 2018 · N339QS · Cessna 680CE · Wing Main, Frame StructureSDR DXTA201802090093Spar Web · corrodedLEFT WING SPAR WEB BULKHEAD FITTING CORRODED.Feb 9, 2018 · N339QS · Cessna 680CE · Wing SparSDR DXTA2017071106428Pump · leakingIMMEDIATELY AFTER LOWERING THE GEAR, AN AMBER HYDRAULIC VOLUME LOW CAS ILLUMINATED. VOLUME INDICATED 110 CU IN. IAW QRH LANDED USING EMERGENCY BRAKING. AFTER SHUTDOWN VOLUME INDICATES 90-100. FOUND THE LT ENGINE DRIVEN HYDRAULIC PUMP LEAKING EXTERNALLY. CARJul 11, 2017 · N339QS · Cessna 680CE · Hydraulic System, MainSDR DXTA2016092306306Control Handle · defectiveLANDING GEAR DID NOT EXTEND WHEN GEAR LEVER WAS SELECTED. A RED UNSAFE LIGHT SHOWED. THE GEAR LEVER WAS CYCLED AND THE GEAR EXTENDED. SUP: REPLACED LANDING GEAR CONTROL. REMOVED PN: 049801-001, SN: L1946, INSTALLED PN: 049801-001, SN: 0271.Sep 23, 2016 · N339QS · Cessna 680SOV · Landing Gear SelectorSDR DXTA2015122906145Unknown · odorON TAKEOFF, DURING ROTATION WITH APU RUNNING & APU BLEEDS RUNNING, A BURNING ODOR IN THE COCKPIT WAS EXPERIENCED & QUICKLY DISSIPATED WITHIN 30 - 40 SECONDS. ODOR DID NOT REOCCUR REMAINDER OF FLIGHT. GROUND RAN APU SEVERAL TIMES, NO UNUSUAL ODORS NOTED, PERFDec 26, 2015 · N339QS · Cessna 680CE · Air Distribution SystemSDR DXTA2015060906025Unknown · malfunctionedTHE LEFT MAIN GEAR ANNUNCIATION LIGHTS DO NOT ILLUMINATE. UTILIZED THE SECONDARY GEAR BLOW DOWN SYS. GAINED ACCESS TO THE LANDING GEAR SHUTTLE VALVE & RESET. INSPECTED & FOUND THE PNEUMATIC BOTTLE RESET, SERVICED & SAFETIED. REMOVED THE MLG CIRCUIT BREAKEJun 8, 2015 · N339QS · Cessna 680CE · Landing Gear Position and WarningSDR DXTA2014050205760Skin · debondedNOSE SKIN DISBONDS AROUND ACCESS DOOR OPENINGS. REPAIRED IAW S-680-ATA53 04RD.Apr 13, 2014 · N339QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR DXTA2014050205759Skin · damagedBIRD STRIKE TO NOSE OF ACFT. REPAIRED IAW S-680-0191 07RD REV A.Apr 13, 2014 · N339QS · Cessna 680CE · Fuselage Main, Plate/SkinSDR DXTA2013032505339Control Cable · damagedUPPER RUDDER CABLE FRAYED AT SPLITTER SECTOR ASSEMBLY JUST AFT OF WING. REMOVED FRAYED LT UPPER AFT RUDDER CABLE. INSTALLED A NEW PN S3966-4L183.9A LT UPPER AFT RUDDER CABLE. SET AFT RUDDER CABLE TENSIONS TO 200 LBS. RIGGED CABLE TENSION ON BOTH UPPER RUDDMar 8, 2013 · N339QS · Cessna 680CE · Rudder Tab Control SystemSDR DXTA2011071204656Engine · odorDURING TAKEOFF, THROUGH 2000 FT. ENGINE EXHAUST ODOR NOTICED COCKPIT. TURNED RT ENGINE BLEED SWITCH TO OFF, CLEARED EXHAUST ODOR. REMOVED AND REPLACED NR 2 ENGINE. GROUND RAN AND LEAK CHECKED GOOD.Jul 12, 2011 · N339QS · Cessna 680CE · Engine (Turbine/Turboprop)SDR DXTA2011041104544Control Unit · dirtyAFTER TAKEOFF, LANDING GEAR HANDLE COULD NOT BE MOVED FROM THE DOWN POSITION. THIS WAS FOLLOWED BY AN AMBER "WOW MISCOMPARE" CAS MESSAGE. PERFORMED GEAR SWING. NO DEFECTS NOTED. COULD NOT DUPLICATE SQ REMOVED & INSPECTED GEAR HANDLE CONTROL UNIT. FOUND UNIT Apr 11, 2011 · N339QS · Cessna 680CE · Landing Gear Retraction/Extension SystemSDR DXTA2010040504058Strut · dischargedGEAR WOULD NOT RETRACT. WOW MISCOMPARE CAS MESSAGE FOLLOWED SHORTLY AFTER. 2 MINUTES LATER LOUD "THUNK" NOISE FROM BELLY OF ACFT. FOUND NOSE GEAR STRUT PRESSURE LOW WITH 2 O'RINGS ON SCHADER VALVE. REPLACED 1 O-RING AND SERVICED STRUT IAW MM, CH 32-20-00. ALApr 3, 2010 · N339QS · Cessna 680CE · Nose/Tail Landing Gear Strut/Axle
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