N382QS, cancelled Dec 6, 2024
Service difficulty reports · 39
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 = 'N382QS' AND deregistration_id = 'N382QS-2024-12-06' 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 = 'N382QS' AND deregistration_id = 'N382QS-2024-12-06' 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 DXTA2024090900440Connector · damagedEMERGENCY LIGHTING: MAIN EXIT DOOR EXIT SIGNS NOT ILLUMINATING ALING WITH THE GALLEY WORK LIGHT ALL THE REST OF THE EMERGENCY LIGHTS WORK PROPERLY. CORRECTIVE ACTION: RESEATED PUSHED PIN S AT CANNON PLUG PC045. RESEATED PIN, RECONNECTED CANNON PLUG, OPS CHECK SDR DXTA2024071212336Battery · defectiveEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK #4 REMAIN ILLUMINATED WHEN ALL POWER IS REMOVED FROM THE AIRCRAFT. THE EMER LIGHTS WERE NO LONGER ON. WITH THE MAIN BATTERIES DISCONNECTED, CYCLED ERNER LIGHT SWITCH OFF TO ARM TO ON NOTING THAT ALL EMER LIGHSDR 2023F00306Web · crackedLH WING FWD WEB P/NP/N 6910269-39. CRACKED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING REPAIR OF THE LH WING FWD WEB CRACK SR-680A-ATA57-33170 DATED APRIL 25, 2022 AND 8100-9 DATED APRIL 25, 2022; STANDARD REPAIR - CRACK DAMAGE, CENTER WING FAIRINGS, LH AND RH SDR 2023F00287Spar Cap · corrodedRH LOWER REAR SPAR CAP CORRODED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ41229M1 DATED SEPTEMBER 21, 2023; RH LOWER REAR SPAR CAP CORROSION.SDR 2023F00286Unknown · unknownLH LOWER REAR SPAR CAP CORRODED. ACCOMPLISHED TEXTRON AVIATION ENGINEERING LETTER DQ41230M1 DATED SEPTEMBER 21, 2023; LH LOWER REAR SPAR CAP CORROSION.SDR DXTA2023072491650Condenser · dirtyPNEUMATIC DISTRIBUTION: DURING A LONGER FLIGHT, ONCE THE CABIN BECOMES COLD SOAKED, AND THE SUPPLY DUCT TEMPERATURE WARMS UP WE NOTICED A SLIGHT OIL BURNING ODOR COMING FROM THE VENTS. I CHECKED THE VENT SUPPLY TEMPERATURE AND IT WAS ONLY SHOWING ABOUT 140. //SDR DXTA2023060888160Flag · damagedMAIN CABIN DOOR EXTERIOR FLAG INDICATOR, REMAINS RED WITH THE DOOR HANDLE IN THE STOW DOWN POSITION. NORMAL INDICATION WOULD BE BLACK AND WHITE CROSS MARKS. VERIFIED INDICATOR FAILS IN CLOSED POSITION. REMOVED PAX DOOR SHROUD & ACCESS PANELS & LOCATED THE INTSDR EBVR202305180001Unknown · unknownCORROSION FOUND ON VERTICAL STAB SPAR LH CAP ANGLE BETWEEN VFS 180-184. REPAIRED USING TEXTRON FIELD REPAIR FR-680-0245-11912 AND 8100-9 DATED 17MAY2023. THIS IS A MAJOR REPAIR.SDR DXTA2022120775710Counterbalance · out of adjustDOOR SEEMS TO BE OUT OF RIG. THE BOTTOM STEP APPEARS TO BE 3 TO 4 INCHES HIGHER THAN NORMAL. ALSO THE COUNTERBALANCE IS NOT WORKING WHEN THE DOOR IS CLOSED. IT WILL SLAM SHUT WITH A LOT OF FORCE. ADJUSTED DOOR COUNTER BALANCE SYSTEM IAW AMM 52-10-50. NO OTSDR DXTA2022070565260Battery · inoperativeCABIN EMERG LIGHT: DURING POWER ON CHECKLIST ALL EMERERGENCY LIGHTS INOP. WITH BATTERY ON EMERGENCY LIGHTS OPERATIONAL. "CORRECTIVE ACTION" COMPLIED WITH CE-680 EMERGENCY LIGHTING POWER SUPPLY BATTERY EXERCISE PROCEDURE. NO DEFECTS NOTED IAW TC-FLT-33-1001 REVSDR DXTA2022010354690Not Reported · not reportedEMERGENCY LIGHT SWITCH: WHEN YOU TURN THE EMER LIGHTS SWITCH OFF THE FOLLOWING LIGHTS REMAIN ON: AFT OVER WING EMERGENCY LIGHT. EXIT LIGHT IN THE DIVIDER, OVERHEAD LIGHT FORWARD OF THAT EXIT LIGHT, EXIT LIGHT IN LAV, AND OVERHEAD LIGHT ABOVE THE LAV. // SIGNOSDR DXTA2021060743320Structure · bentMAIN DOOR: MAIN CABIN DOOR CORNER BENT OUT APPROXIMATELY 3/4 INCH(JUST TO THE RIGHT OF THE HANDLE). // SIGNOFF // MAIN ENTRANCE DOOR LOWER HALF AFT MID SECTION OF DOOR SKIN EXTENTION.LOC: FS 220 AND WS 105.71. AREA OF TWO INCHES X TWO INCHES. PART OF THE LOWERSDR JGVR20210526003Spar Cap · corrodedMECHANICALLY REMOVED 2 AREAS OF CORROSION LOCATED ON AFT SPAR , LOWER SPAR CAP AT WS 37.00. FOUND INBD BLEND TO BE WITHIN LIMITS. PER NJA GMM 2.2.2 THIS IS LEVEL 1 CORROSION. FOUND 1 AREA AT WS 37.00 TO BE BEYOND LIMITS IAW C680 SRM 51-70-02. PROTECTED BARE MSDR JGVR20210526002Rib · corrodedMECHANICALLY REMOVED AREA OF CORROSION LOCATED IN RH WING GEARWELL BAY 720DR OUTBD RIB LOWER MIDDLE AREA IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND C680 SRM LIMITATIONS. REPAIRED CORROSION BLEND IAW TEXTRON ENGINEERING MEMO REF DQ30071M1 RRL, SSDR JGVR20210526001Rib · corrodedMECHANICALLY REMOVED AREA OF CORROSION LOCATED IN LH WING GEARWELL BAY 730DL OUTBD RIB LOWER MIDDLE AROUND HI-LOK IAW C680 SRM 51-70-02. FOUND CORROSION BLEND TO BE BEYOND C680 SRM LIMITATIONS. REPAIRED CORROSION BLEND IAW TEXTRON ENGINEERING MEMO REF DQ30071MSDR DXTA2021041240650Sensor · defectiveENG FIRE DETECT FAIL R AMBER CAS: IN CRUISE FLIGHT AT FL380 AMBER 'ENG FIRE DETECT FAIL R' CAS MESSAGE DISPLAYED. REMOVED INTERNAL FIRE & OVERHEAT SENSOR, PN:- 30B5702-01 ; SN: 121604. FROM RH ENGINE; DUE TO ENG FIRE DETECT FAIL R AMBER CAS MESSAGE DISPLAYED.SDR JGVR20210219003Door Frame · corrodedREMOVED THE FWD AND AFT CONTOUR RINGS FROM THE EMERGENCY EXIT DOOR AND FOUND SEVERE AREAS OF CORROSION ON THE DOOR STRUCTURE. SENT THE EMERGENCY EXIT DOOR OUT FOR REPAIR.SDR JGVR20210219002Structure · corrodedMECHANICALLY BLENDED AREAS OF BUBBLING PAINT AND CORROSION FROM MAIN CABIN DOOR STRUCTURE, LOCATED UNDER MOVABLE STEP BETWEEN THE TWO CENTER ATTACH POINTS, PERFORMED NDT AN REPORTED FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED BLENDED AREAS IAW TEXTROSDR JGVR20210219001Floor Support · corrodedMECHANICALLY BLENDED SEVEN AREAS OF CORROSION IN CABIN DROP AISLE FLOOR CONSISTING OF TWO AREAS ON LT FWD ANGLE APPROXIMATELY 3.5 AND 8 INCHES AFT OF FWD END OF DROP AISLE, RAISED DOUBLER/FLOOR BOARD SUPPORT WITH TWO AREAS ON THE FWD LT SIDE AND THREE ON FWD RSDR JGVR20200605001Rib · corrodedCORROSION AROUND 2 HI-LOKS ON UPPER OUTBOARD RIB ABOVE LT MLG AT APPROXIMATELY MIDLINE. REMOVED 2 HI-LOK FASTENERS AND MECHANICALLY BLENDED CORROSION IN AREA AROUND HOLES ON UPPER OUTBOARD RIB ABOVE LT MLG AT APPROXIMATELY MIDLINE, IAW SRM 51-10-01. PERFORMED SDR 2TJR201910210001Spar Cap · corrodedCORROSION WAS FOUND AT THREE LOCATIONS ON THE 6931012-1 LH AFT SPAR CAP OF THE VERTICAL STABILIZER. ALL CORROSION WAS
REMOVED BY BLENDING IAW CESSNA FIELD REPAIR - CORROSION, VERTICAL STABILIZER, LH REAR SPAR CAP, VFS 115 TO 163 DWG NO. FR-680-0245-7226 DATESDR DXTA2018052100157Skin · corrodedTAILCONE SKIN CORRODED.SDR DXTA2018FA0000156Drag Angle · crackedRT WING DRAG ANGLE CRACKED.SDR DXTA2016020206175Switch · faultyLEFT MAIN GEAR STAYED DOWN AFTER GEAR RETRACTION WITH A LT GEAR DOWN GREEN INDICATION & NO RED INDICATION. OHMED OUT LT GEAR UPLOCK SWITCH SG007 & FOUND WITH THE GEAR DOWN. THE SWITCH IS LIGHTLY TAPPED BETWEEN PINS E & F, RESISTANCE GOES FROM .2 OHMS UP TO 3SDR DXTA2015101206106Brake Assy · lockedEMERGENCY BRAKING WAS USED & RT OTBD TIRE APPEARS TO HAVE LOCKED UP & BLOWN. REMOVED FAULTY RT NR 3 & 4 WHEEL & TIRE ASSEMBLY. INSTALLED OVERHAULED NR 3 & 4 WHEEL & TIRE ASSEMBLY IAW MM 32-41-20. SERVICED RT NR 3 & 4 MAIN TIRES WITH NITROGEN IAW MM CH 12-13SDR DXTA2015100606103Hydraulic Line · faultyIMMEDIATELY AFTER GEAR EXTENSION & 3 GREEN GEAR DOWN & LOCK LIGHTS, RECEIVED AMBER HYD VOLUME LOW CAS MSG. EMER BRAKING WAS USED & RT OTBD TIRE APPEARS TO HAVE LOCKED UP & BLOWN. REMOVED FAULTY NLG ACTUATOR EXTENSION HOSE AND INSTALLED NEW EXTENSION HOSE IAWSDR CWQR20130305013Heat Exchanger · crackedDURING A SCHEDULED INSPECTION WE WERE PREFORMING A PRODUCT IMPROVEMENT (REPLACEMENT OF DUCT ASSY 6914070-67) WE NOTICED THAT THE HEAT EXCHANGER SIDE PLATE HAD 2 CRACKS ABOUT .30" LONG. THE OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN 2 OF THE 4 CORNERS. SDR CWQR20130305014Heat Exchanger · crackedHEAT EXCHANGER SIDE PLATE HAD TWO CRACKS ABOUT .37 INCH LONG. THE OPPOSITE SIDE OF THE HEAT EXCHANGER WAS CRACKED IN THREE OF THE FOUR CORNERS. A NEW HEAT EXCHANGER WAS INSTALLED. PREFORMED A LEAK CHECK ON THE DEFECTIVE UNIT AND FOUND THE CRACKS EXTENDED INSDR CWQR20121221054Tube · crackedACFT CAME IN WITH A REPORTED TREND SHIFT IN ITT. DURING AN ENGINE RUN, FOUND A BLEED AIR LEAK ON THE TOP SIDE OF THE RT ENGINE. REMOVED CLAMP AND FOUND THE TUBE MATING FLANGE CRACKED.SDR DXTA2012092405133Door Frame · corrodedMINOR CORROSION FOUND ADJACENT TO AFT SHEAR TIE ON CABIN DOOR FRAME. .023 DEEP, OUT OF LIMITS, DOOR FRAME WILL BE CHANGED.SDR DXTA2011092004733Brake · leakingMAIN WHEEL LEAKING HYD FLUID. BRAKES VERY RIGID ON BOTH RUDDER PEDALS WHEN BRAKES APPLIED ON TAXI/TAKEOFF/LANDING ROLLOUT. BOTH PILOT BRAKE APPLICATIONS REQUIRED MORE BRAKE APPLICATION THEN NORMAL TO STOP. R & R THE LT OTBD WHEEL & BRAKE ASSY AND INSTALLED SDR DXTA2010092804253Landing Gear · malfunctionedRED MLG UNLOCK INDICATION REMAIND ILLUMINATED AFTER MLG HANDLE WAS PLACED IN THE UP POSITION. 3 GREEN MLG INDICATORS EXTINGUISHED. MLG DEPLOYED NORMALLY. JACKED ACFT AND DUPLICATED PROBLEM AFTER 3 GEAR SWINGS. REPOSITIONED HYD SYS & FOUND NOSE GEAR ABOUT TO SDR DXTA2010032304049Strut · malfunctionedON DEPARTURE, LANDING GEAR HANDLE COULD NOT BE MOVED TO THE UP POSITION, LANDING GEAR REMAINED DOWN AND LOCKED. APPROX 1-2 MINS LATER THE "WOW MISCOMPARE" CAS MSG ILLUMINATED FOR 30 SECONDS THEN EXTINGUISHED. REMOVED LOWER STRUT, CLEANED AND REPACKED WITH NEWSDR DXTA2009111003856Landing Gear · malfunctionedWHILE ENROUTE AT FL400, APPROX 25 MINUTES INTO FLIGHT, NOSE GEAR EXTENDED UNCOMMANDED, NOSE DOORS OPENED, THEN NOSE GEAR RETRACTED VERY ABRUPTLY. INDICATIONS ON GEAR DISPLAY WERE ONE RED, NO GREEN. RED LIGHT STAYED ON TILL GEAR HANDLE WAS SELECTED DOWN FOR LSDR DXTA2009111003852Landing Gear · malfunctionedWHILE EN ROUTE AT FL400, APPROX 25 MINUTES INTO FLIGHT, NOSE GEAR EXTENDED UNCOMMANDED, NOSE DOORS OPENED, THEN NOSE GEAR RETRACTED VERY ABRUPTLY. INDICATIONS ON GEAR DISPLAY WERE ONE RED, NO GREEN. RED LIGHT STAYED ON TILL GEAR HANDLE WAS SELECTED DOWN FOR LASDR DXTA2008122703444Switch · shortedAT APPROX 13,000 FT ON APPROACH, GOT AN "AMC O' HEAT" TEMP CAS MESSAGE FOLLOWED BY AN EMER PRESS ACTIVATION. SHORTLY AFTER EMER PRESS CAME ON CABIN STARTED TO AQUIRE SMOKE. IT GOT TO A "HAZY CLOUD" THICKNESS AND THEN STABILIZED. SMOKE SMELL ASSOCIATED. VERISDR DXTA2008122903444Unknown · smokeSMOKE IN COCKIT DURING APPROACHSDR DXTA20082935Uplock Sensor · malfunctionedUPON GEAR RETRACTION, OUT OF DEPARTURE, RT GEAR WOULD NOT RETRACT. REMOVED AND REPLACED RT UPLOCK SWITCH WITH NEW. C/W FULL GEAR FUNCTIONAL CHECK. ALL OPS CHECK GOOD AT THIS TIME. IAW MM 32-61-00.SDR DXTA20082880Landing Gear · malfunctionedMANUAL GEAR EXTENSION WITH BLOW DOWN DUE TO NOSE GEAR NOT EXTENDED DURING LANDING. RESET BLOWDOWN BOTTLE AND SERVICED SWING GEAR MULTIPLE TIMES. UNABLE TO DUPLICATE PROBLEM. REF: MM SEC 32-30-00
Back to N382QS, cancelled Dec 6, 2024