N311QS, cancelled Dec 3, 2024
Service difficulty reports · 37
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 = 'N311QS' AND deregistration_id = 'N311QS-2024-12-03' 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 = 'N311QS' AND deregistration_id = 'N311QS-2024-12-03' 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 JGVR20240626003Spar Cap · corrodedREPAIRED SEVERAL CORRODED AREAS ON THE VERTICAL STABILIZER AFT SPAR RH CAP BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS AND SHIMS.SDR JGVR20240626002Spar Cap · corrodedREPAIRED CORRODED AREAS OF THE LOWER FORWARD SPAR CAPS OF THE LH & RH WINGS, LOCATED IN THE MAIN LANDING GEAR WHEEL WELLS, BY REMOVING FASTENERS AS REQUIRED, BLENDING CORRODED AREAS, PERFORMING NDT AND REPORTING FOR REPAIR DISPOSITION, TREATING & PRIMING REPAISDR JGVR202406264001Skin · corrodedREPAIRED CORRODED AREAS OF THE LOWER AFT FUSELAGE TAILCONE SKINS LOCATED UNDER AND ADJACENT TO THE AFT CHIN FAIRING AREAS BY BLENDING CORRODED AREAS, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, FABRICATING AND INSTALLING REPAIR DOUBLERS IN ACCORDANCE WITSDR JGVR20230711001Unknown · unknownBLENDED CORROSION ON THE UPPER SURFACE OF THE UPPER WING SKIN OF THE RH WING, LOCATED ADJACENT TO AND UNDERNEATH THE AFT DRAG ANGLE (WING-TO-FUSELAGE FAIRING AREA), BY REMOVING THE AFT DRAG ANGLE, BLENDING CORRODED AREAS, PERFORMING NDT AND SUBMITTING RESULTS SDR DXTA2022120175180Spring · defectiveMAIN DOOR PRECATCH LEVER: LEVER EXTENDED AND WILL NOT RETRACT. VISUALLY VERIFIED PRECATCH SYSTEM IS NOT WORKING PROPERLY. GAINED INTERNAL ACCESS TO PRECATCH SYSTEM AND NOTED CAM OVERCENTERED AND BEHIND STRIKE PLATE OF PLUNGER. ADJUSTED CAM AS REQUIRED AND INSDR DXTA2022032859060Pump · defectiveFUEL PRESSURE INDICATION: WHILE CROSSFEEDING FROM L TANK, FUEL PRESS LOW L. CASS MESSAGE CAME ON MOMENTAIRLY FOLLOWED BY FUEL BOOST PUMP ON L CASS MESSAGE. FUEL BOOST PUMP ON R CASS MESSAGE THEN CAME ON ALSO.//CORRECTIVE ACTION// REMOVED AND REPLACED LEFT BOSDR DXTA2022031758610None · noneLEFT EMERGENCY LIGHT AFT OF MCD: MULTIPLE EMERGENCY LIGHTS INOP. LEFT EXTERIOR FUSELAGE AFT OF MAIN CABIN DOOR. INTERIOR CEILING LIGHT OVER SEAT 3 AND 5. INTERIOR LIGHT OVER SEAT NONE. // SIGNOFF// REMOVED AND REPLACED PINS IN PL089V DUE TO BEING BURNT AND SHSDR JGVR20210507002Rib · corrodedREMOVED RH EMERGENCY BRAKE BULKHEAD FITTING FROM RH WING, RIB AT RWS 37. BLENDED CORROSION FROM FWD INBOARD WEB ON RIB AT RWS 37. EVALUATED REMAINING THICKNESS AND FOUND AREA TO BE OUT OF SRM LIMITS PER CESSNA 680 SRM 51-70-02. SUBMITTED TO TEXTRON ENGINEERINGSDR JGVR20210507001Spar · corrodedREMOVED LH UPPER AND LOWER BRAKE LINES AND BULKHEAD FITTINGS FROM LH WING, MIDDLE SPAR, AFT SIDE. BLENDED CORROSION FROM LH WING, MIDDLE SPAR, AFT SIDE. EVALUATED REMAINING THICKNESS AND FOUND AREA TO BE OUT OF SRM LIMITS PER CESSNA 680 SRM 51-70-02. SUBMITTEDSDR JGVR20210427001Spar Cap · corrodedBLENDED CORRODED AREAS ON THE LEFT AND RIGHT HAND WINGS AFT SPARS LOWER SPAR CAPS, LOCATED IN THE MAIN LANDING GEAR WHEEL WELL AREAS, PERFORMED ULTRASONIC AND EDDY CURRENT INSPECTIONS AND REPORTED FOR REPAIR DISPOSITION. TREATED AND PRIMED REPAIR AREAS IAW TEXSDR JGVR20201123002Skin · corrodedSPOT OF CORROSION ON LT WING INBOARD FWD, JUST BEHIND LEADING EDGE. NOTED DURING 57-00-00-2101-LT FOUND 48 ADDITIONAL CORROSION AREAS AFTER FWD DRAG ANGLE REMOVAL AND CLEAN-UP. 5 HI-LOC'S ON LT WING UPPER WHERE FWD AND MIDDLE DRAG ANGLES WERE REMOVED REQUIRESDR JGVR20201123001Spar · corrodedCORROSION FOUND ON VERTICAL STAB AFT SPAR. FOUND DURING 1 ADDITIONAL AREA OF CORROSION FOUND ON RT SIDE OF VERTICAL STAB SPAR CLIP JUST BELOW RUDDER MIDDLE HINGE. PERFORM TEXTRON ENGINEERING FIELD REPAIR ON VERTICAL STAB SPAR. MECHANICALLY BLENDED 6 TOTAL ASDR JGVR20201120006Structure · corrodedFOUND SEVERAL AREAS OF CONFIRMED CORROSION UNDER SEVERAL NUTPLATES ON THE V-STAB AT THE FOLLOWING LOCATIONS: 341DL 7 NUTPLATES, 341CL 5 NUTPLATES,341BL 5 NUTPLATES, 341DR 3 NUTPLATES,341CR 5 NUTPLATES, 341AL 1 NUTPLATE. REMOVE NUTPLATES AND BLEND CORROSION. SDR JGVR202011110202Spar · corrodedSPOT OF VERIFIED CORROSION IN LT WHEEL WELL ON AFT SPAR, LOWER SPAR CLIP. MECHANICALLY REMOVED 1 SPOT OF VERIFIED CORROSION IN LT WHEEL WELL ON AFT SPAR LOWER SPAR CLIP. FOUND CORROSION BLENDS EXCEEDING C680 SRM 51-70-02 AND SUBMITTED FINDINGS TO TEXTRON ENGSDR JGVR20201111001Spar · corrodedSPOTS OF VERIFIED CORROSION IN RT WHEEL WELL ON AFT SPAR, LOWER SPAR CLIP. MECHANICALLY REMOVED 1 SPOT OF VERIFIED CORROSION IN RT WHEEL WELL ON AFT SPAR LOWER SPAR CLIP. FOUND CORROSION BLENDS EXCEEDING C680 SRM 51-70-02 AND SUBMITTED FINDINGS TO TEXTRON ENSDR JGVR20191023001Door Frame · chafedREPAIRED FIVE CHAFFED AREAS AROUND E-EXIT WEB AND FRAME IN STRINGER 3 SURROUNDING AREAS OF THE INTERIOR FUSELAGE AT FS 409.26 AND FS 426.26 BY INSTALLING REPAIR DOUBLERS AND SHIMS PER ENGINEERING REPAIR ORDER.SDR EBVR20190514001Channel · crackedFOUND DURING PRELIMINARY INSPECTION. LT PYLON AFT CHANNEL ASSEMBLY IS CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER. ATTACHED TO MODIFIED EXISTING CHANNEL ASSEMBLY. ATTACHED TO PYLON TRAILING EDGE. ALL WORK ACCOMPLISHED IAW AQRD ERO-957932 REV IR AND APPROVSDR 2017F00169Trunnion · wornREPAIR OF OVERSIZED DOOR ROD PIN HOLE IN LEFT AND RIGHT MLG TRUNNIONS. REPORT NR S-680-0196/06RD DATED SEPTEMBER 29, 2017 WITH FORM FAA 8100-9.SDR 2017F00170Door · corrodedLEFT AND RIGHT MLG DOOR CORROSION. MEMO DQ9710M1 DATED: OCTOBER 3, 2017.SDR 2018F00007Spar · corrodedLEFT AND RIGHT AFT WING SPAR WEB BULKHEAD FITTING CORRODED.SDR 2017FA0000508Flap · corrodedLEFT INBOARD FLAP CORRODED.SDR DXTA2017041206393Control Handle · malfunctionedLANDING GEAR WOULD NOT RETRACT, GEAR HANDLE STUCK IN UP POSITION. REMOVED FAILED GEAR HANDLE AND INSTALLED NEW. C/W GEAR SWING. OPERATIONAL CHECK GOOD. WORK COMPLIED WITH IAW MM 32-10-00.SDR DXTA2016122906349Uplock Switch · out of adjustABRUPT THUMP FOLLOWED BY RED GEAR UNLOCK LIGHT OCCURRED AT CRUISE AT FL410. TROUBLESHOT TO NOSE LANDING GEAR UPLOCK SWITCH BARLY CONTACTING UPLOCK ROLLER. ADJUSTED NLG UPLOCK SWITCH AND OPS CHECK GOOD IAW MM 32-60-00.SDR DXTA2015100606101Unknown · odorWHEN SELECTING AVIONICS ON, WE HEARD A NOISE LIKE A FAN BLADES HITTING SOMETHING, THEN WE SMELLED THE ODOR OF SOMETHING BURNING.
TURNED AVIONICS BACK OFF AND WHEN TURNING ON AVIONICS BACK ON AGAIN WE RECEIVED "MAU 2 FAIL" CAS MESSAGE. COULD NOT DUPLICATE FASDR DXTA2015082806069Pressure Switch · malfunctionedAT 200 FT AGL THE FUEL BOOST PUMP RT CAS MESSAGE CAME ON. CREW SELECTED RT BOOST PUMP ON. AT 100 FT AGL FUEL PRESS LOW RT CAS MESSAGE CAME ON. ON LANDING ROLL OUT THE RT ENG FAILED & ATTEMPTED TO RELIGHT BUT WOULD NOT RELIGHT. SHUT THE ENG DOWN MANUALLY. SDR DXTA2015061506029Battery · failedRED CAS MESSAGE BATTERY O TEMP LIGHT ILLUMINATED ON TAKEOFF ROLL. TEMP, BATTERY, WENT UP TO +71 C. COMPLIED WITH APPROPRIATE EMERGENCY CHECKLIST. THE CYAN BATTERY OFF LT CAS MESSAGE DID NOT DISPLAY. CFR SAID THEY COULD SMELL ODOR & BURNING FROM LT BATTERY SDR DXTA2014010605615Warning Message · false activationAFTER TAKEOFF, CLIMBING THROUGH 2000 MSL, AMBER ANTI-SKID FAIL CAS ILLUMINATED. COMPLETED ABNORMAL CHECKLIST, CAS DID NOT CLEAR. POWERED ACFT & PERFORMED OPERATIONS CHECK OF THE ANTI-SKID WITH NO DEFECTS NOTED. INTERROGATED CMC & ALL DATA PARAMETERS WHERE SDR DXTA2011012404429Strut · chafedGEAR WOULD NOT RETRACT ON CLIMB-OUT AND THE GEAR HANDLE WOULD NOT MOVE. WHILE CONFIGURING FOR LANDING THE "WOW MISCOMPARE" CAS MESSAGE ILLUMINATED. R & R NLG UPPER AND LOWER BARREL ASSEMBLIES IAW CMM CHAP 32-20-01 R 1. OPS CHECKED GOOD. UPPER BARREL ASSY PSDR DXTA2010121104359Pressure Switch · malfunctionedFUEL FILTER BYPASS L CAS ILLUMINATED IN FLIGHT, EMERGENCY DECLARED. REMOVED & INSPECTED LT FUEL FILTER ELEMENT. NO DEBRIS OR FOREIGN MATERIAL FOUND IN ELEMENT OR IN BOWL. PERFORMED LT ENGINE START & IMMEDIATELY RECEIVED A FUEL FILTER BYPASS "L" CAS MESSAGE WSDR DXTA2009082103764Module · failedTHE ENG CONTROL FAULT R FAILED AT FL430. DID NOT FLY THROUGH ANY WEATHER. DASHES ON EVERYTHING RT SIDE. ON POWERING DOWN THE AMBER MAU 2 FAIL CAME ON. REMOVED AND REPLACED CUSTOM I/O MODULE OPS CHECKS GOOD IAW MM 34-17-00.SDR DXTA2009030903538Latch · unsecureUPPER FWD LATCH OF REAR BAGGAGE DOOR POPPED OPEN IN FLIGHT. INSPECTED DOOR LATCH, PINS, AND LOCKS. FOUND DOOR TO OPERATE AS REQUIRED WITH NO DEFECTS NOTED.SDR DXTA2009010303463Control Unit · inoperativeDURING CRUISE AP A FAIL CAS MESSAGE POSTED FOLLOWED 30 SECONDS LATER BY AP B FAIL CAS MESSAGE. BOTH MESSAGE REMAINED ON THE RESET OF THE FLIGHT REVIEWED CDMS FAULTS, FOUND PITCH TRIM FAULT ON LAST FLIGHT. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNISDR DXTA200901033462Control Unit · inoperativeDURING CRUISE, AP A FAIL CAS MESSAGE POSTED FOLLOWED 30 SECONDS LATER BY AP B FAIL CAS MESSAGE. BOTH MESSAGES REMAINED ON THE RESET OF THE FLIGHT REPEAT WRITE-UP. REVIEWED CDMS FAULTS, FOUND PITCH TRIM FAULT ON LAST FLIGHT. REMOVED AND REPLACED HORIZ STAB SDR DXTA2009010503462Autopilot Sys · malfunctionedDURING CRUISE AP A FAIL CAS MSG POSTED FOLLOWED 30 SECONDS LATER BY AP B FAIL CAS MSG.SDR DXTA200808083220Steering Sys · out of limitsAFTER TAKEOFF, POSITIONED GEAR HANDLE UP. MAIN CAME UP BUT NOSE DID NOT RETRACT AND THE RED UNLOCK LIGHT STAYED ILLUMINATED. RECYCLED GEAR AND SAME THING HAPPENED. AFTER ABOUT 10 MIN THE NOSE GEAR RETRACTED. JACKED ACFT, 3 GREEN, CYCLED GEAR SEVERAL TIMES. NLGSDR DXTA200803220Indication Sys · malfunctionedAFTER TAKEOFF, POSITIONED GEAR HANDLE UP. THE MAINS CAME UP BUT THE NOSE DID NOT RETRACT AND THE RED UNLOCK LIGHT STAYED ILLUMINATED. (S)SDR DXTA200803158Strut · lowGEAR WILL NOT RETRACT AFTER TAKEOFF. "WOW MISCOMPARE" AMBER MESSAGE IN FLIGHT INTERMITTENTLY. WENT OUT BEFORE LANDING. ONLY ON FOR ABOUT 15 SECONDS. NOSE STRUT NOT EXTENDING COMPLETELY. NITROGEN SERVICE LOW AT UPPER AND LOWER SERVICE PORT. RESERVICED NOSE
Back to N311QS, cancelled Dec 3, 2024