N651QX
Service difficulty reports · 38
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 = 'N651QX' 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.
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 = 'N651QX' AND registry_match = 'registration' 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 QXEA2026070700159Fadec · not reportedECMP REPQUEST TO REPLACE THE NR 1 ENGINE FADEC. NR 1 ENGINE FADEC REPLACED ON WORK ORDER 365508.SDR QXEA2026042700096Steering Sys · out of trimFLIGHT 2555. ON TOUCH DOWN AIRCRAFT LEERS HARD TO THE LEFT WITH RUDDERS NEUTRAL. AIRCRAFT ALSO LEERS TO THE LEFT ON TAXI. REMOVED FROM SERVICE. TAXIED AIRCRAFT AND VERIFIED LEFT STEERING PULL. C/W MCN E320065-01. TIRE PRESSURES CHECKD GOOD. LH/RH MLG STRUTSDR QXEA2025032100066Brake Assy · no discrepancyBRAKES FELT LIKE THEY WERE STICKING ON TAXI IN. NEEDED MORE THRUST THAN NORMAL TO TAXI INTO PARK. REMOVED FROM SERVICE. C/W MAIN BRAKE SYSTEM OPS TEST AND MAIN BRAKE PRESSURE TRANSDUCER FUNCTIONAL TEST REF E175 AMM 32-41-00-710-801-A AND 32-41-00-720-802-A. NDSDR QXEA2025011700008Oven · smokeFLIGHT 2080. AT 33,000FT IN CRUISE THE AFT FA REPORTED EXCESSIVE SMOKE FROM THE REAR OVEN. REMOVED FROM SERVICE. DEACTIUVATED OVEN AND PLACED ON NEF 1112642 WITH A 300 HOUR LIMIT. AIRCRAFT RETURNED TO SERVICE.SDR QXEA2024112600281Throttle · malfunctionedFLIGHT 2146. 5 MIN AFTER POWER UP AT FAIL MESSAGE. REMOVED FROM SERVICE AND PLACED ON MEL 22-30-00B. RETURNED TO SERVICE. MEL CLEEARED 11/26/24 BY AT FAULT NOT PRESENT ON STARTUP OR THROUGHOUT TROUBLESHOOTING REF FIM 22-31-00-810-818/860-A AND FAULT CODE AND SDR QXEA2024110800262Fairing · crackedCRACK ON AFT WING TO FUSELAGE FAIRING STRAP AS MARKED IN RH SIDE FR 57-58. PERFORMED CUTOUT REPAIR ON AFT WING TO FUSELAGE FAIRING STRAP AT FR57-58 REF SRM 53-04-02/REPAIR/02P.SDR QXEA2024110800260Strap · corrodedCORROSION IN STRAP AT AFT CARGO DOOR CUTOUT FR 77. REMOVED AND REPLACED STRAP AT AFT CARGO DOOR CUTOUT FR 77. REF SRM 51-40-08.SDR QXEA2024110800261Seat Track · corrodedFWD WET AREA RH SEAT TRACK BETWEEN FR17 AND FR18 HAS CORROSION. REMOVED CORROSION BY BLENDING ON FWD WET AREA RH SEAT TRACK BETWEEN FR17 AND FR18. FOUND MEASUREMENT OF BLENDED AREA TO BE OUT OF LIMITS PER SRM 53-10-10. CUT OUT DAMAGED AREA OF FWD WET AREA SEATSDR QXEA2024110800263Seat Track · corrodedRH IB SEAT TRACK HAS CORROSION BETWEEN FR84 AND FR85. PERFORMED DOUBLER REPAIR AND INSTALLED RH IB SEAT TRACK REPAIR FILLER AND DOUBLER REF SRM 53-23-10 REPAIR 04.SDR QXEA2024110800264Beam · corrodedRH BEAM HAS CORROSION BETWEEN FR86 AND FR87. REMOVED AND REPLACED RH BEAM IN AFT WET AREA FR 86-89 REF SRM 51-40-08.SDR QXEA2024101000235Lever · malfunctioned#1 ENGINE THRUST LEVER DOES NOT RETURN TO MIN REV POSITION AFTER MAX REV WAS USED WITHOUT MANUALLY MOVING THE #1 LEVER TO MIN REV. REMOVED FROM SERVICE. INTERROGATED CMC, NO FAULTS FOUND. REMOVED AND REPLACED THRUST CONTROL QUADRANT IAW AMM 76-11-01-000-801-A SDR QXEA2024071900174Light · migratedEMERGENCY FLOOR PATH LIGHTING PHOTO LUMINESCENT STRIP BETWEEN SEATS 2A & 3A HAS MIGRATED FWD. REMOVED LIGHT STRIP IAW E175 TASK 33-50-21-000-801-A & ADJUSTED STRIP. CLEANED & APPLIED NEW TAPE. INSTALLED IAW TASK 33-50-21-400-801-A.SDR QXEA2024070500168Light · brokenDURING INSPECTION FOUND PHOTOLUMINESCENT STRIP FWD OF ROW 1 R/H SIDE CRACKED BEYOND LIMITS. REMOVED AND REPLACED PHOTOLUMINESCENT STRIP ON R/H SIDE FWD OF ROW 1 IAW E175 AMM 33-50-21-000/400-801-A. NO FURTHER DEFECTS NOTED.SDR QXEA2024030800051Sign · faultedAFT GALLEY OVERHEAD EMERGENCY LIGHT INOP. REPLACED THE #3 EMERGENCY LIGHT POWER UNIT IAW AMM 33-50-01-000/400-801-A AND REPLACED THE EXIT SIGH IAW AMM 33-50-19-000/400-801-A.SDR QXEA2023062800097Unknown · unknownDURING FLIGHT CONTROL TEST, VIBRATION FELT WHEN RELEASING BACK PRESSURE ON CONTROL COLUMN. REMOVED FROM SERVICE. C/W MCN #E270006, ISS #01. CNTRL-COLUMNS MOVE SMOOTHLY WITHOUT BINDING. C/W FCS-RTS TEST REF E175 AMM 27-00-00-070-801-A. NO ABNORMAL NOISE OR VIBRSDR QXEA2023062700096Unknown · unknownDURING FLIGHT CONTROL TEST, NOTICED A VIBRATION IN CONTROL COLUMN AFTER RELEASING BACK PRESSURE. REMOVED FROM SERVICE. PERFORMED GVI OF CONTROL-COLUMN DAMPER FLUID LEVEL IAW E175 AMM 27-31-02-210-801-A. SERVICED RH CONTROL COLUMN DAMPER IAW E175 AMM 12-21-16-6SDR QXEA2023062100090Unknown · unknownLOST V SPEED INDICATION AT ABOUT 45 KTS ON T/O ROLL. REJECTED T/O @ APPROX 60KTS. REMOVED FROM SERVICE. PERFORMED AIR DATA SYSTEM TEST IAW E175 AMM TASK 34-15-00-710-801-A. OPS TEST GOOD NO FURTHER DEFECTS NOTED. RETURNED TO SERVICE.SDR QXEA2023011300005Latch · dirtyFLIGHTDECK DOOR VERY DIFFICULT TO OPEN FEELS LOCKED BUT ISNT. REMOVED FROM SERVICE. CLEANED FLIGHTDECK LATCH DOOR, OPERATES NORMALLY, NO FURTHER DEFECT NOTED RETURNED TO SERVICE.SDR QXEA2022121200337Button · malfunctionedAUTOMATIC DOOR LOCKING AND UNLOCKING PUSH BUTTON WOULD NOT UNLOCK FLIGHT DECK DOOR. HAD TO USE EMERGENCY DOOR OPENING MANUAL LATCH. PLACED ON MEL 52-51-00A.SDR QXEA2022100400303Door · noneAFTER UNLOCKING COCKPIT DOOR IS HARD TO IOPEN . REMOVED FROM SERVICE. INSPECTED FLIGHT DECK DOOR AND LOCK MECHANISM WITH NO DAMAGE FOUND OPEN ANC CLOSED DOOR AND OPERATED LOCK MULTIPLE TIMES WITH NO DEFECT NOTED. COULD NOT DUPLICATE. RETURNED TO SERVICE.SDR QXEA2022051700198Galley · inoperativeFLIGHT ATTENDANT B REPORTS SMELL OF BURNING IN AFT INBD COFFEE POT. REMOVED FROM SERVICE. R/R AFT INBOARD COFFEEMAKER IAW E175 AMM 25-37-03-000-801-A/400-801-A OPS CK GOOD IAW E175 AMM 25-37-03-710-801-A PLACARDS ARE REMOVED C/B RESET THIS CLEARS DEFECT 959SDR QXEA2022033100134Battery · inoperativeDURING EMERGENCY LIGHT POWER UNIT FUNCTIONAL TEST, FOUND CENTER EMERGENCY LIGHT IN AFT GALLEY WOULD NOT ILLUMINATE. REMOVED AND REPLACED CENTER EMERGENCY EXIT LIGHT ASSY IN AFT GALLEY DUE TO BURNT CIRCUITRY PER E175 AMM 33-50-19-000-801-A, 33-50-19-400-801-A, SDR QXEA2022010600016Connector · damagedFLIGHT ATTENDANT HEADSETS 'EMER PILOT' RED LIGHT ILUMINATING INTERMITTENTLY AND ALSO DIMLY - BOTH FORWARD AND AFT HANDSETS. REMOVED FROM SERVICE. DURING T/S REMOVED AFT CEILING PANEL, NOTED PLUG POS 40 WARM. REMOVED CANNON PLUG NOTED SOCKETS T & S EVIDENCE OF SDR QXEA2021093000457Spring · damagedR1 DOOR FWD EVAC SLIDE-FITTING SPRING APPEARS BROKEN. REMOVED AND REPLACED R1 DOOR FWD EVAC SLIDE-FITTING SPRING REF 175 AMM 53-10-25-000-804A AND 53-10-25-400-804A. NO ADJUSTMENTS MADE.SDR QXEA2021080200383Floor Panel · looseFA REPORTS THE AFT LAV FLOORING MAT HAS BECOMING DETACHED FROM THE FLOOR AND IS A BAD TRIPPING HAZARD. PLACED ON NEF. RETURNED TO SERVICE.SDR QXEA2021070600350Wire Harness · misroutedDURING FQIS HARNESS INSPECTION FOUND INCORRECT ROUTING UNDER PANEL 195AL. REROUTED GROUND SPOILER CONTROL MODULE HARNESS SO THAT IT RUNS SEPARATE FROM FQIS HARNESS TO COMPLY WITH INSPECTION CRITERIA IN E175 AMM 28-41-00-210-801-A.SDR QXEA2021060800283Smoke Detector · false activationLAV SMOKE MASTER WARNING ILLUMINATED DURING PRE FLIGHT. REMOVED FROM SERVICE. NO ACTIVE SMOKE MASTER CURRENTLY ON EICAS. CW TEST OF FWD LAV SMOKE SYSTEM IAW E175 AMM TASK 26-14-01-700-801-A. SYSTEM TEST GOOD. NO FURTHER DEFECTS NOTED. SMOKE MASTER CAUTION REMASDR QXEA2021030200095Module · inoperativeON LANDING, ENG 1 REV TLA FAIL, ENG 1 REV IND & PRIOR TO ANNUNCIATION. REMOVED FROM SERVICE. T/S IAW E175 FIM 76-11-00-810-803-A. R&R SPDA1 SLOT 3 IAW E175 AMM 24-61-13-000/400-801-A. MESSAGE EXTINGUISHED. AIRCRAFT RETURNED TO SERVICE.SDR QXEA2020113000330Smoke Detector · false activationLAV SMOKE MASTER WARNING IN CRUISE. F/A VERIFIED THAT PASSENGER BUMPED HIS HEAD ON AFT LAV CEILING NO SMOKE FOUND IN LAV. MASTER WARNING/MESSAGE DURATION ABOUT 30 SECONDS. REMOVED FROM SERVICE. PERFORMED GVI OF LAV SMOKE DETECTORS, NO DAMAGE NOTED. COMPLISDR QXEA2020111600321Smoke Detector · false activationLAV SMOKE WARNING MESSAGE APPEARED DURING PASSENGER BOARDING. NO SMOKE WAS EVIDENT. REMOVED FROM SERVICE. PERFORMED OPERATIONS TEST OF FWD LAV SMOKE DETECTOR, IAW E-175 AMM TASK 26-14-01-700-801-A. OPERATIONS TEST PASSED, NO FURTHER DEFECTS. CREW STATED FSDR QXEA2020083000268Door · bindingFLIGHT DECK DOOR DIFFICULT TO OPEN FROM THE INSIDE THE FLIGHT DECK. REMOVED FROM SERVICE, FOUND DOOR TO OPEN/CLOSE PROPERLY. COULD NOT DUPLICATE. DURING OP'S CHECK FOUND AUTOMATIC LOCKING SYSTEM INOPERABLE, PLACED THAT ON MEL. REF E175 AMM 52-51-03 PARA 10 FSDR QXEA2020081300240Smoke Detector · false activationLAVATORY SMOKE ILLUMINATED BRIEFLY DURING CRUISE. THEN WENT OUT. NO REPORT OF SMOKE FROM F/A OF AFT LAVATORY. REMOVED FROM SERVICE.PERFORMED GVI OF AFT LAV NO DEFECTS NOTED. PERFORMED OPS TEST OF AFT LAVATORY SMOKE DETECTOR IAW AMM TASK 26-14-01-700-801-A OPS SDR QXEA2020012100036Autothrottle Sys · malfunctionedUPON ROTATION TAKEOFF GUIDANCE CHANGED TO FLIGHT DIRECTOR, ATTCS COMMANDED CLB-2. AUTO THROTTLES RETARDED AND AIRCRAFT ATTEMPTED TO LEVEL OFF BELOW ACCELERATIONS HIGHT. DIVERTED. REMOVED FROM SERVICE. NO FAULTS FOUND OR RECORDED ON CMC. OPS CHECK OF FMS PERFOSDR QXEA2020012180033Receptacle · fireFIRE AT GROUND POWER RECEPTACLE. FERRIED FOR REPAIRS.SDR QXEA2019122300474Panel · stuckEMERGENCY GEAR EXTENSION SWITCH PANEL IS JAMMED SHUT, UNABLE TO ACCESS THE GEAR EXTENSION HANDLE. REMOVED FROM SERVICE. OPENED DOOR AND CLEANED HINGE AND LATCH AREA AS REQUIRED. OPS CHECK GOOD. A/C FOR SERVICE. NO PARTS REPLACED.SDR QXEA2019121600462Visor · damagedDURING CLIMB AFTER THE AFTER THE TAKE OFF FLOW.THE FIRST OFFICER PLACED HIS SUNVISOR UP TO HELP THE CAPT REMOVE THE SUN FROM HIS EYES.SHORTLY AFTER THE T-O SUNVISOR FELL MOVING THE FLAPS TO POSITION 1 AND @ 250KTS RECEIVED A HIGH SPEED ORAL WARNING FOR LESS THSDR QXEA2019112700432Elevator · bindingAFTER ENGINE START, DURING CONTROL CHECK WHEN PERFORMING AFT ELEVATOR CHECK THERE IS A BINDING VIBRATION UNTIL BACK TO NEUTRAL. CHECKED MULTIPLE TIMES. THE VIBRATION WAS CONSISTENT. BOTH CA AND FO SIDES HAD SAME ISSUE. AIRCRAFT REMOVED FROM SERVICE. INTERROGATSDR QXEA2019112500429Control Column · unknownDURING FLIGHT CONTROL CHECK CAPTAIN AND F/O SIDE CONTROL COLUMN HAS BINDING AND FRICTION FEEL WHEN GOING FROM FULL AFT TO NEUTRAL POSITION. REMOVED FROM SERVICE. C/W E175 FIM TASK 27-33-00-810-801-A STEPS 1-6L(1)(A-E). NO BINDING NOTED. CONTROL COLUMN MOVES
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