N617QS, cancelled Dec 31, 2024
Service difficulty reports · 33
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 = 'N617QS' AND deregistration_id = 'N617QS-2024-12-31' 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 = 'N617QS' AND deregistration_id = 'N617QS-2024-12-31' 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 DXTA2023092095960Actuator · defectiveWHILE CLIMBING THROUGH FL 390 WE RECEIVED PIT TRIM ANNUCIATION ON BOTH PFDS. THE TRIM WHEEL WAS TRYING TO TRIM BUT WAS BINDING AND NOT MOVING AND HAD AN AUDIBLE BINDING SOUND. NEITHER ELECTRIC OR MANUAL TRIM WERE WORKING. THE TRIM NEVER COULD GO PAST THE WORSDR DXTA2023070690360Motor · damagedPOWER BRAKE CB: BRAKE CB TRIPPED, ANTI SKID AND LOW BRAKE PRESSURE ENNUNCIATED DURING TAXI IN. PNEUMATIC BRAKE APPLIED TO STOP AIRCRAFT AT RAMP PARKING. REMOVED PWR BRAKE MOTOR AND INSTALLED AN OVERHAULED MOTOR IAW CE-560XL AMM 32-44-20 RE-SET CB AND PERFORSDR DXTA2022122676980Pin · lack of lubeMAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE DOOR. CLEANED AND LUBED ALL MAIN CABIN DOOR PINS. ADJUSTED UPPER AFT LATCH PLATE INNER ECCENTRIC IAW MM 52-10-00. OPENED AND CLOSED MAIN CABIN DOOR SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME.SDR DXTA2022012455550Socket · defectiveEMERG LIGHT SWITCH: AMBER LIGHT FOR THE EMERGENCY LIGHT SWITCH IS INOP // SIGNOFF// REMOVED AND RELNSTALLED NEW LAMP P/N 6838. REMOVED AND REPLACED SOCKET P/N MS90308·4, OPERATIONAL CHECK OF LIGHT FOUND SATISFACTORY. REFERENCE: 560XL AMM 33·10·01 AND SPM 20-30SDR DXTA2021071945410Light · shortedCABIN EMERG LIGHT: CIRCUIT BREAKER HT 043 POPPED ON THE AFT CIRCUIT BREAKER PANEL IN THE APU COMPARTMENT. WE EXPERIENCED HEAVY ELECTRICAL SMELL AND SMOKE IN THE CABIN IN FLIGHT . THE SMOKE DISSIPATED AFTER ABOUT 10 MINUTES. FOUND SEVERAL DROP AISLE LIGHTS SDR DXTA2020071503863Strut · out of adjustCABIN ENTRY DOOR SPRING TORQUE COUNTERBALANCE HANDLE BAR EXCESSIVELY LOOSE. BARELY MAKES OVER CENTER LOCK. ADJUSTED CABIN DOOR SUPPORT STRUT ASSEMBLY REF AMM 52-10-01 AND OPS CKD NORMAL FOR POSITIVE OVERCENTER ACTION.SDR DXTA2019082102781Condenser · odorCABIN ODOR OIL SMELL - DISTINCT OIL SMELL IN CABIN AND COCKPIT. STRONGER IN LAV AREA AND CABIN, LESS STRONG ON COCKPIT. NOTICEABLE ON GROUND WITH APU AIR ON AND IN-FLIGHT WITH APU AIR OFF. CLEANED THE WATER SEPARATOR REMOVED AND REPLACED WATER SEPARATOR CONDESDR DXTA2018060501036Unknown · odorCLIMBING THRU 10K, PAX NOTIFIED CREW OF A SMOKE ODOR IN THE CABIN. CREW CONFIRMED AND FO WENT BACK TO CHECK WHILE CAPTAIN SHUT DOWN APU. ODOR IMMEDIATELY DISSIPATED. GROUND VISUAL CHECK REVEALED NO EVIDENCE OF A PROBLEM. PERFORMED BOROSCOPE APU INLET INSPECSDR DXTA201711105HQ2TMotor · failedCOMPLETE BRAKE FAILURE DURING TAXI OUT. ANTI-SKID LIGHT AND POWER PRESSURE CIRCUIT BREAKER TRIPPED. THEN LOW BRAKE PRESSURE LIGHTS. HYD FLUID ON NOSE GEAR DURING POST FLIGHT. INSPECTED BRAKE SYSTEM FOR SIGNS OF DAMAGE, NONE FOUND. OPS CHECKED BRAKES, COULD NOTSDR DXTAT2PL6D005BQW8Water Separator · odorODORS IN THE COCKPIT DURING FLIGHT WITH APU RUNNING. SMELLS LIKE BURNED OIL. INSPECTED THE APU INLET AND EXHAUST, APU BLEED AIR DUCT AND HEAT EXCHANGER DUCT, WATER SEPERATOR AND CLEANED WATER SEPARATOR SOCK IAW MM 12-19-02. REINSTALLED WATER SEPERATOR AND SDR DXTA2016012406172Steering Sys · corrodedAFTER DEPARTURE THE LG UNLOCK LIGHT REMAINED ON. DURING CLIMB OUT THE HYD PRESS LIGHT REMAINED ILLUMINATED. COMPLETED THE LG WILL NOT RETRACT CHECKLIST. LG EXTENDED NORMALLY. JACKED ACFT & PERFORMED GEAR OPERATIONAL CHECKS, NO PROBLEMS FOUND. SLIGHTLY TURSDR DXTA2015110706119Selector · malfunctionedDURING TAKEOFF, A LOUD SOUND OF RUSHING AIR & CABIN PRESSURIZING RAPIDLY. ACCOMPANIED BY A STRONG BURNING ODOR. ANNUNCIATOR WITH FLASHING MASTER CAUTION ILLUMINATED BUT WENT OUT. TROUBLESHOT AND VERIFIED ODOR IN COCKPIT & CABIN. PERFORMED ENGINE RUNS & OPSSDR DXTA2015031105992Pressure Switch · failedDURING LANDING, LOWERING THE LANDING GEAR THE LOW BRAKE PRESSURE & ANTI-SKID INOPERATIVE ANNUNCIATOR LIGHTS CAME ON. RAN THE CHECKLIST & USED THE EMERGENCY BRAKE AFTER LANDING. TROUBLESHOT TO A BAD PRESSURE SWITCH. REPLACED THE PRESSURE SWITCH WITH AN OVESDR DXTA2015021705978Unknown · unknownDURING LANDING ROLL OUT AT SPEEDS ABOVE NORMAL TAXI SPEED, THE LT BRAKE GRABS EXCESSIVELY & PULLS THE ACFT TO THE LEFT. THE RT BRAKE APPEARED TO RELEASE & REAPPLY THE BRAKE 5 OR 6 TIMES DURING THE ROLL OUT. NO ANTI-SKID RELEASE MARKERS WERE NOTED AFTER LANDISDR DXTA2013111205563Brake Assy · malfunctionedLT BRAKE GRABS. R & R LT BRAKE ASSY IAW MM 32-42-01. BLED SYS AND PERFORMED OPS CHECKS. OPS CHECKS SATISFACTORY AT THIS TIME. TAXI, OPS, & LEAK CHECKED GOOD.SDR DXTA2013103105553Unknown · odorDURING CRUISE FLIGHT, A LOUD CLICK OR POP WAS HEARD. CREW NOTICED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT THAT QUICKLY WENT AWAY. NO SMOKE WAS NOTED. NO CIRCUIT BREAKERS WERE TRIPPED. PERFORMED COCKPIT LIGHTING CHECK IAW MM 33-10-00, NO DEFECTS NOTSDR DXTA2013070105426Bearing · failedDURING DESCENT AT 35000 FT, ELEVATOR PITCH TRIM FROZE. PITCH TRIM LIGHT ILLUMINATED ON THE PFD. THE ELEVATOR PITCH TRIM WAS IMMOVABLE USING BOTH MANUAL AND ELECTRIC TRIM. PITCH TRIM BEGAN OPERATING NORMALLY AT APPROX. 20,000 FT AND OPERATED NORMALLY THEREAFSDR DXTA2013050605373Apu · fodAFTER STARTING APU, A BURNING ODOR CAME FROM APU. WENT OUTSIDE AND FOUND FLAMES COMING FROM EXHAUST ALONG WITH DEBRIS FROM A BIRDS NEST. SOME OF THE STICKS AND GRASS WENT INTO THE INTAKE. SHUTDOWN APU AND DISCHARGED A PORTABLE FIRE EXTINGUISHER. CLEANED OSDR 2013F00002Bolt · wornON PERFORMING AN INSPECTION-B, FOUND LT ENGINE FORWARD COWLING STRUT UPPER ATTACH BOLT SEVERELY WORN. SUSPECT VIBRATION CAUSING EXCESSIVE WEAR. THIS CONDITION HAS BEEN FOUND ON SEVERAL OF THIS MODEL ACFT.SDR DXTA2011091504727Motor · failedACFT WAS TAXIING TO THE RUNWAY, WHEN THE POWER BRAKES AND ANTI SKID SYSTEMS FAILED. THE CREW STOPPED THE ACFT ON THE TAXIWAY. REMOVED FAULTY MOTOR PN MP50B-1, SN 2728. FOUND COUPLER BETWEEN PUMP AND MOTOR WORN EXCESSIVELY. REPLACED COUPLER WITH NEW PN 6517SDR DXTA2010100604257Brake Assy · malfunctionedBRAKES NOT FUNCTIONING PROPERLY. GRINDING AND GRABBING. TAXIED ACFT & VERIFIED PROBLEM, BUT WENT AWAY DURING TAXI. LET BRAKES COOL DOWN & RETAXIED & BRAKE FUNCTIONED NORMALLY. BLED LT & RT BRAKES IAW MM 32-44-00 & NEW BLEEDING PROCEDURE. TAXI CHECKED ACFT SDR DXTA2009111003857Nose Cone · damagedPOSSIBLE BIRD STRIKE ON RT ENGINE AT 7 O`CLOCK POSITION. DENT FOUND ON ENGINE LIP AND BLOOD WITH FEATHERS AROUND INTAKE. PERFORMED A BIRD STRIKE INSP ON RT ENG AND BOROSCOPRED AND FOUND NO RESIDUE OF BIRD FID INGESTION. REMOVED AND REPLACED NOSE CONE LIP WITSDR DXTA2009111103853Structure · dentedPOSSIBLE BIRD STRIKE ON RT ENGINE AT 7 OCLOCK POSITION. DENT FOUND ON ENGINE LIP AND BLOOD WITH FEATHERS AROUND INTAKE.SDR DXTA2009071703731Seal · leakingDURING TAKEOFF APPROX 500FT, CREW GOT A RT 'LO OIL PRESS' INDICATION LIGHT. CREW FOLLOWED CHECKLIST AND LANDED THE ACFT SAFELY. OIL PRESSURE WAS AT APPROX 30 PSI. ALL OTHER INDICATIONS WERE NORMAL. RAN ACFT AT TAKEOFF PWR AND FOUND GARLOCK SEAL ON FCU LEAKINSDR DXTA200702508Actuator · inoperativeRT EEC INOP ON TAKEOFF ROLL AND COULD NOT REACH TAKEOFF POWER SETTING IN MANUAL POSITION. REMOVED & REPLACED R/H BLEED TORQUE MOTOR. RAN A/C FOR LEAK & OPS CHECKS. SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ENG MAKES POD IN BOTH MANUAL & AUTO. ALL WORK DONSDR DXTA200601474Adc · fluctuatesEXPERIENCED PITCH OSCILLATIONS IN CLIMB WITH KP/FD COUPLED TO AUTO PILOT. VIS FLUCTUATED FROM 500FPM TO +5000 FPM. GOT RED X ON VSI AND ALT AND A/S YELLOW FLAGS. APPEARS TO BE NR 1 ADC. REPLACED NR 1 ADC WITH REPAIR UNIT CERTIFIED TO AN ALTITUED OF 59,500 SDR DXTA200601437Windshield · crackedRIGHT FRONT WINDSHIELD HAS MULTIPLE CRACKS BROKE AT FLIGHT LEVEL 390 AND APPEARS TO BE THE OUTER LAYER ONLY. VERIFIED CO-PILOTS WINDSHIELD SHATTERED. REMOVED & REPLACED RT WINDSHIELD. C/W EDGE SEAL. C/W FUNCTIONAL TEST, CHECK GOOD. C/W RETAINER SCREW TORQSDR DXTA200601367Position Switch · out of adjustAFTER TAKEOFF, GEAR RAISED WITH NORMAL INDICATIONS. AT 400FT WHEN FLAPS RAISED TO (0) DEGREE, GOT A STEADY HYD PRESS AND STAB MISCOMPARE LIGHT. AFTER RUNNING CHECKLIST, FLAPS WERE LOWERED TO 15 DEGREES RESULTING IN HYD PRESS AND STAB MISCOMPARE LIGHTS. ADJUSSDR DXTA200601359Position Switch · contaminatedSHORTLY AFTER TAKEOFF POWER APPLIED NO TAKE OFF LIGHT ILLUMINATES AND AUARAL WARNING. AFTER CLEARING RUNWAY LIGHT GOES OUT. TROUBLESHOT SYSTEM. CLEANED LT AND RT SPEED BRAKE SWITCHES AND CONNECTORS, CHECKED OPERATION OF FLAP POS SWITCH, RT STAB SWITCH, ELEVSDR DXTA200500740Wire Harness · faultyDURING TAKEOFF ROLL LEFT ENGINE PRODUCED 80% N1. SCHEDULED TAKEOFF POWER WAS 90.1% - REMOVED AND REPLACED ENGINE WIRING HARNESS PER P&WC M/M CH 76-20-02 OPERATIONAL CHECKS SATISFACTORY. BOTH AUTO AND MANUAL MODES.SDR DXTA200500626Uplock Cable · out of adjustWHILE IN CRUISE AT FL410, CREW HEARD CLUNK SOUND FROM GEAR AREA, RED GEAR UNSAFE LIGHT ILLUMINATED AND HYD PRESS LIGHT ILLUMINATED STEADY. PULLED HYD CONTROL CB, HYD PRESS EXTINGUISHED, GEAR UNSAFE REMAINED ILLUMINATED. FOUND NOSE GEAR FREEFALL CABLE TO BE TSDR DXTA200500603Landing Gear · malfunctionedAFTER ROTATION, GEAR SELECTED UP, AFTER 3-4 SEC GEAR MADE A CYCLING THUMPING NOISE FOR APPROX 3 SECONDS. RECEIVED A HYD FLOW & A HYD LOW CAUTION LIGHT. CYCLING STOPPED, GEAR LOCKED UP & HYD FLOW LIGHT WENT OUT. KEPT FLAPS AT 15 DEG AND RE-EXTENDED GEAR. HYSDR DXTA200400500Switch · malfunctionedAFTER GEAR UP/FLAPS UP HAD HYD PRESS, STAB MISCOMPARE ANNUNCIATORS AND UNLOCK GEAR LIGHT. PULL HYD C/B, AND LOUD THUMP HEARD AND FELT IN NOSE GEAR AREA. PUSH HYD C/B IN GET SAME NOISE. ALL LIGHTS OUT AND SYSTEMS WORKED FINE WITH GEAR DOWN AND FLAPS FULL AT
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