N375QS, cancelled Jan 22, 2025
Service difficulty reports · 34
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 = 'N375QS' AND deregistration_id = 'N375QS-2025-01-22' 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 = 'N375QS' AND deregistration_id = 'N375QS-2025-01-22' 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 2024FA0000579Skin · corrodedBLENDED CORRODED AREA ON THE LH SKIN ON THE RUDDER NEAR THE REPAIRED LEVEL 2 CORROSION FOUND ON LH SIDE OF RUDDER, JUST AFT OF THE RUDDER TRIM ACTUATOR CUTOUT, BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION, REMOVING EXISTING DOUBLER, FABRICATINSDR DXTA2024030111048Power Supply · failedEMERG EXIT SIGN/LIGHT: EMERGENCY EXIT LIGHTS AT THE CABIN ENTRY DO NOT WORK AS WELL AS THE LEFT EXTERIOR EMERGENCY LIGHT. DID 2-30 MINUTE CHARGES WITH THE GPU WITH NO CHANGE. REMOVED FAULTY POWER SUPPLY PIN CBS28-1 SIN 005715 AND INSTALLED REPAIRED POWER SUPPSDR DXTA2024012510723Battery · faultedSEVERAL INTERIOR EMERGENCY LIGHTS AND THE LEFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. ARRIVED AT AC. POWERED ON EMERGENCY BAIT SWITCH, CONFIRMED DISCREPANCY AND TOOK NOTE OF ALL UNLIT EMER LIGHTS. RESEARCHED AC MM AND WDMS. ARRIVED AT AC. GAINED ACCESS AND PERFSDR DXTA2023091194970Battery · defectiveWHEN EMERGENCY LIGHTS ARE PLACED IN ARMED POSITION EMERGENCY EXIT LIGHTED SIGNS BEHIND SEAT 9, AND ABOVE LAVATORY SEAT DO NOT ILLUMINATE AS WELL AS SEAT LIGHT OVER LAVATORY SEAT. MX SUSPECTS BATTERY PACK FOUR TO BE NOT FUNCTIONING. //SIGNOFF// REMOVED #4 EMESDR EBVR20230623450Unknown · unknownCORROSION FOUND ON THE SKIN AROUND THE EMERGENCY EXIT DOOR ON R/H SIDE OF FUSELAGE. BLENDED SIGNS OF CORROSION FROM 2 SPOTS ON THE E-EXIT OUTER SKIN. REMAINING MATERIAL THICKNESS IN THE BLENDED AREAS ARE WITHIN ALLOWABLE LIMITS SPECIFIED IN SR-680-ATA52-18636 SDR DXTA2023022381040Unknown · unknownNLG LANDING GEAR RETRACTION: REPEAT WRITEUP. AFTER GEAR RETRACTION RED UNLOCK LIGHT REMAINED ILLUMINATED. COMPLIED WITH QRH UNLOCK ON RETRACTION, EXTENSION NORMAL WITH 3 GREEN INDICATIONS. // SIGNOFF// JACKED AIRCRAFT AND MEASURED ALL UPLOCKS. PER AMM - MLG USDR DXTA2022121275960Light · defectiveEMERGENCY LIGHTING: L H EMER LIGHT NOT ILLUMINATED // SIGNOFF // TURNED ON EMERGENCY LIGHTING, FOUND ALL EMERGENCY LIGHTING TO BE OPS ILLUMINATING SATISFACTORY, CONTACTED NJA MCC FOR CLARIFICATION ON CREW SQUAWK, GOT CLARIFICATION THAT THE LIGHT THE CREW SQUASDR DXTA2022101972370Actuator · defectiveAFTER CLIMBING THROUGH 10000 FT AND ACCELERATING TOWARDS 300 KIAS, THE A AUTOPILOT FAILED AND WE EXPERIENCED A NOSE UP PITCH MOTION. THE PF WAS UNABLE TO TRIM NOSE DOWN BECAUSE THE PRIMARY STAB TRIM WAS AT ITS NOSE DOWN LIMIT. HE REDUCED SPEED AND WAS ABLE TSDR DXTA2021082547550Relay · abnormalEMERGENCY LIGHTING: EMERGENCY LIGHTING OFF FUNCTION INOP. UNABLE TO EXTINGUISH INTERIOR OR EXTERIOR EMERGENCY LIGHTING THROUGH NORMAL SWITCH FUNCTIONS. LIGHTS REMAIN ON EVEN WITH BOTH MAIN BATTERIES DISCONNECTED. TROUBLESHOT DISCREPANCY TO A BAD PILOT CONTROSDR JGVR20201120005Skin · corrodedMECHANICALLY REMOVED 12 AREAS OF CORROSION LOCATED AT LT UPPER WING FWD, MIDDLE AND AFT DRAG ANGLES. REPAIRED CORROSION BLENDS, IAW TEXTRON ENGINEERING STANDARD REPAIR SR-680-ATA57-27245 REV-. TITLED "STANDARD REPAIR-CORROSION, WING UPPER SKINS, WS 37" DATEDSDR JGVR20201120004Drag Angle · damagedREPAIRED BLENDED AREAS ON LT AND RT WING INBOARD SKINS NEXT TO FORWARD DRAG ANGLES, PER TEXTRON FIELD REPAIR, FR-680-0230-8540 REV-. TITLED: FIELD REPAIR-CORROSION, WING, UPPER SKINS, LT/RT WS 37, DATED: 10/29/2020, SUPPORTED BY FAA FORM 8100-9 DATED: 10/29/2SDR JGVR20201120003Skin · corrodedFOUND 17 AREAS OF VERIFIED CORROSION ALONG FUSELAGE AFT CHIN FAIRING. FOUND ADDITIONAL 120 AREAS OF CORROSION UNDER AFT CHIN FAIRING. REPAIRED BLENDED AREAS OF LEVEL 2 CORROSION ON LOWER FUSELAGE SKIN UNDER AFT CHIN FAIRING BY INSTALLING REPAIR DOUBLERS. ALSDR JGVR20201120002Skin · corrodedRT LOWER WING SKIN IN GEAR WELL HAS VERIFIED CORROSION UNDER 7 FASTENERS. PERFORM TEXTRON MINOR REPAIR MEMO DQ27295M1 DATED: OCT 9, 2020 FOR RT LOWER CENTER WING SKIN. REMOVED 7 FASTENERS AND BLENDED 7 AREAS OF CORROSION ON RT LOWER WING SKIN IN GEAR WELL, ISDR JGVR20201120001Skin · corrodedFOUND 11 AREAS OF VERIFIED CORROSION ON E-EXIT OUTER SKIN. FOUND DURING TASK 52-20-00-2202 FOUND 4 ADDITIONAL SPOTS OF VERIFIED CORROSION UNDERNEATH CONTOUR RINGS OF THE E-EXIT.SDR JGVR20201113002Door Frame · chafedREPAIRED CHAFED E-EXIT SURROUND WEB AND FRAME AT APPROXIMATELY FS 400 PER AEROSPACE QRD ERO-967189 REV IR, TITLED "E-EXIT SURROUND WEB AND FRAME REPAIR" DATED OCT 30 2020 AND SUPPORTED BY FAA FORM 8110-3 DATED 10/30/2020.SDR JGVR20201113001Structure · corrodedREPAIRED SEVERAL AREAS OF CORROSION ON FUSELAGE DROP AISLE STRUCTURE BETWEEN FS 165 AND FS 426 PER AEROSPACE QRD ERO-967178 REV IR DATED NOVEMBER 09, 2020 AND SUPPORTED BY FAA FORM 8110-3 DATED NOVEMBER 09, 2020.SDR JGVR202001112001Spar · corrodedVERTICAL STAB AFT SPAR LT UPPER ANGLE HAS 2 AREAS OF VERIFIED INTERGRANULAR CORROSION. MECHANICALLY BLENDED CORROSION ON VERTICAL STAB AFT SPAR RT UPPER ANGLE, ABOVE RUDDER LOWER HINGE, IAW CESSNA 680 SRM 51-70-02. FOUND BLENDED AREA TO BE OUT OF LIMITS, PERSDR DXTA2019093002907Downlock Switch · malfunctionedRIGHT MLG LANDING GEAR EXTENSION DID NOT EXTEND - UPON GEAR DOWN SELECTION 6 MILE FINAL 28R SFO RIGHT MAIN GEAR DID NOT LOCK (NO GREEN). ADVISED TOWER TO EXECUTE MISSED APPROACH UPON GOING AROUND THE RIGHT MAIN GEAR LIGHT TURNED GREEN. RAN THE QRC CHECKLIST SDR DXTR2017121800648Tee Fitting · corrodedMAIN CABIN DOOR SPADE DOOR HINGE ATTACH NUTPLATES CORRODED. MEMO 10436M2 DATED DECEMBER 14, 2017.SDR 2018F00053None · noneREPAIR OF OVERSIZED DOOR ROD PIN HOLE IN RIGHT MAIN LANDING GEAR TRUNNION. REPORT NO. S-680-0230/02RD DATED DECEMBER 6, 2017 WITH FAA FORM 8100-9 DATED DECEMBER 8, 2017.SDR 2018F00052None · noneREPAIR OF DRILL STARTS IN RIGHT WING LEADING EDGE SKIN. REPORT NO. S-680-0230/03RD DATED DECEMBER 6, 2017 WITH FAA FORM 8100-9 DATED DECEMBER 7, 2017.SDR 2018F00051None · noneMAIN CABIN DOOR SPADE DOOR HINGE ATTACH NUT-PLATES. MEMO 10436M1 DATED DECEMBER 7, 2017.SDR DXTA2017041606397Sensor · malfunctionedLEFT ENGINE OIL TEMP IN RED IN THE CLIMB PASSING 14,000 FT. HIGHEST NOTED TEMP WAS 144 DEGREES. UPON POWER REDUCTION, OIL TEMP RETURNED TO GREEN AND REDUCED SETTING WAS MAINTAINED UNTIL LANDING TO KEEP THE TEMP IN THE GREEN. SUB REMOVED THE INOP SENSOR, REPLSDR 2016F00206Spar Cap · corrodedCORROSION ON VERTICAL STABILIZER AFT SPAR CAP.SDR DXTA2016010406152Monitor · failedTV MONITOR AT SEAT 7 BEGAN SMOKING & HAS A SPOT WHERE PLASTIC ON BACK OF MONITOR STARTED TO MELT. FOUND BURN HOLE IN BACK OF MONITOR HOUSING. REMOVED MONITOR. INSPECTED WIRING & CABLE, NO DEFECTS NOTED. DAMAGE IS ONLY ON MONITOR ASSY ITSELF. INSTALLED REPAIRESDR DXTA2015092206088Condenser · failedBLUE SMOKE & OIL ODOR FROM OVERHEAD WEMAC VENTS. COMPLIED WITH TASK CARD ECS DUCT BURN OUT, FORM TC-680-21-120905M. REMOVED CONDENSER FROM WATER SEPARATOR. REMOVED OLD COALESCE SOCK FROM CONDENSER. INSTALLED A NEW COALESCE SOCK ONTO CONDENSER. RE-INSTALLESDR DXTA2014090905877Drain Line · obstructedIN CRUISE CREW NOTICED ENVIRONMENTAL SYS ODOR & SMOKE IN CABIN. ACCOMPLISHED ABNORMAL PROCEDURE, SMOKE APPEARED TO DECREASE WHEN PRESS SOURCE SELECTOR WAS IN RIGHT POSITION. INSPECTED & TROUBLE SHOT SYS. WHEN REMOVING WATER SEPARATOR FOUND EXCESS WATER & CASDR DXTA2011021704469Strut · dischargedAFTER TAKEOFF "WOW MISCOMPARE" ILLUMINATED AND GEAR WOULD NOT RETRACT. FOUND NLG STRUT UPPER CHAMBER 10PSI LOW AND LOWER CAMBER AT OPSI. PERFORMED NLG STRUT SERVICE IAW MM 32-20-00. PERFORMED GEAR SWINGS AND LEAK CHECKS. OPS AND LEAK CHECKS GOOD.SDR DXTA2010070204138Duct · leakingSUPPLY BLEED LEAK R, CASS MESSAGE. RAN ABNORMAL CHECKLIST AND CASS MESSAGE CAME BACK ON AFTER SYSTEM RESET. R & R RT PRECOOLER UPPER DUCT ASSY AND LOWER DUCT SEAL IAW MM CHAP 36-10-00 LEAK CHECK GOOD.SDR DXTA2008122903449Unknown · odorDESCENDING THROUGH 18000 FT, ACM O' TEMP AND EMER PRESS ANNUNCIATORS ILLUMINATED. AFTER 15 SECONDS, BOTH CLEARED. CABIN HAD SMALL AMOUNT OF SMOKE AND CLEARED AS WELL. OPERATED CABIN AND COCKPIT ENVIRONMENTAL SYS IN AUTO AND MANUAL 1 HOT AND COLD USING APU ANSDR DXTA2008122803448Unknown · odorDESCENDING THROUGH 18000 FT, ACM OVERTEMP AND EMER PRESS ANNUNCIATORS ILLUMINATED. AFTER 15 SECONDS, BOTH CLEARED. CABIN HAD SMALL AMOUNT OF SMOKE AND CLEARED AS WELL. OPERATED CABIN AND COCKPIT ENVIRONMENTAL SYS IN AUTO AND MANUAL 1 HOT AND COLD USING APU ASDR DXTA2008122903448Warning Light · illuminatedACM OVERTEMP AND EMERGENCY PRESSURE ANNUNCIATORS ILLUMINATED. SMALL AMOUNT OF SMOKE IN CABIN.SDR DXTA20082870Landing Gear · malfunctionedUPON RETRACTION OF LANDING GEAR, GEAR UNSAFE LIGHT ILLUMINATED. JACKED AND SWUNG GEAR TEN TIMES WITH NO FAULTS. LUBED ALL UP LOCK ROLLERS AND GEAR. OPS CHECKED GOOD IAW MM CH32-01-00.SDR DXTA200802810Hose · leakingDURING TOUCHDOWN AT PDK, COPILOT'S LT BRAKE PEDAL WENT COMPLETELY TO THE FLOOR. REMOVED AND REPLACED BOTH CO-PILOTS UPPER MASTER CYLINDER HOSES. IAW MM CHAP 32-42-02. ALSO COMPLETED APPROVED BLEEDING PROCEDURES CHAP 32-42-00.
Back to N375QS, cancelled Jan 22, 2025