N614QS, cancelled Mar 6, 2024
Service difficulty reports · 18
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 = 'N614QS' AND deregistration_id = 'N614QS-2024-03-06' 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 = 'N614QS' AND deregistration_id = 'N614QS-2024-03-06' 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 DXTA2023122910462Unknown · unknownDOOR DOESN`T OPEN AFTER MOVING HANDLE TO OPEN. SEAL REMAINS INFLATED FOR 8-10 SECS. POWER OFF CONFIRMED PRECATCH OPS & DOOR FUNCTIONS NORMAL. STARTED APU & DOOR SEAL SLOW TO DEFLATE. FOUND DOOR ACCOUSTIC SEAL VALVE NOT EXTENDING ALL THE WAY. CLEANED SEVERALSDR DXTA2023122610424Light · damagedAFTER LANDING & CHECKING AC STOCK, FOUND 2 PUNCTURED TOMATO JUICE CANS IN GALLEY DRAWER. PULLED DRAWER OUT TO CLEAN AND CLEANED INSIDE CABINET COMPARTMENT. NOTICED STRONG ELECTRICAL SMOKE BURN SMELL. WHILE CLEANING NOTICED THE LED LIGHT BAR HAD COME DISCSDR DXTA2023100997520Unknown · unknownFORWARD LEFT EMERGENCY AISLE LIGHTS INOPERATIVE. FOUND RECESSED PIN ON LH FORWARD DROP ISLE LIGHT CONNECTOR. RESEATED PIN AND CHECKED VOLTAGE. VOLTAGE CHECKS GOOD. OPERATIONAL CHECKS GOOD IAW MM 33-50-00.SDR DXTA2023071891160Unknown · unknownMAIN DOOR HANDLE: MAIN CABIN DOOR EXTREMELY DIFFICULT TO LATCH CLOSED AND TO UNLATCH. IT TAKES SIGNIFICANT EFFORT TO GET IT LATCHED AND UNLATCHED. EGRESS ISSUE. //SIGNOFF// CLEANED AND LUBED MED DOOR PINS IAW CE·560XL AMM CH. 12·20·52, OPS CHECK GOOD. NO DEFECSDR DXTA2023030281550None · noneMAIN DOOR: MAIN CABIN DOOR INSIDE HANDLE, DOES NOT ACTUATE PINS TO LOCK THE DOOR. *** CORRECTIVE ACTION *** REMOVED MAIN CABIN DOOR STEPS, INSPECTED AND FOUND BROKEN HARDWARE. INSTALLED NEW HARDWARE ON MAIN CABIN DOOR INNER HANDLE IAW CESSNA 560XL MM 52-10-00 SDR DXTA2022042961080Pcb · defectiveANNUNCIATOR WARNING SYSTEM: CABIN DOOR WARNING LIGHT ILLUMINATED AS AIRCRAFT WAS IN A CLIMB AND PASSING THROUGH 33,000'. REPEAT GRIPE. REMOVED CABIN DOOR PCB NZ007 P/N:6618707-26 S/N:0282 INSTALLED CUSTOMER SUPPLIED NEW CABIN DOOR PCB NZ007 P/N:6618707-26 S/NSDR DXTA2022041860360None · noneWHILE IN CRUISE AT 40,000 FEET, WE GOT THE "CABIN DOOR" ANNUNCIATOR. WE FOLLOWED THE QRH AND DIVERTED. UPON ARRIVAL T E DOOR PINS WERE INTACT AND LOCKED. // SIGNOFF// ATTEMPTED TO REPRODUCE PILOT WRITE UP. PERFORMED DOOR WARNING SYSTEM - OPERATIONAL CHECK ISDR DXTA2022033159410None · noneENGINE COMPRESSOR STALL: AT CRUISE ALTITUDE 410 HEARD A LOUD BANG AND FELT A THUMP IN OUR FEET. N1 DROPPED FROM 91.0 TO 85 THEN RETURNED TO 91.0. REST OF FLIGHT WAS NORMAL. 2ND WRITEUP. ENGINE SYNC WAS OFF. // SIGNOFF// BEGAN TO TROIBLESHOOTING THE R/H ENGISDR DXTA2022021156540Not Reported · not reportedLEFT FORWARD EMERGENCY LIGHT STRIP ON THE CABIN FLOOR, IS INOP///SIGN-OFF///RESEATED CONNECTORS AT FWD LIGHT ASSY. SYS CK GOOD.. ALL WORK PER CESSNA MODEL 560XL MM 33-20-00.SDR DXTA2021090748180Battery · defectiveEMERGENCY LIGHTING: AFT EMERGENCY DIVIDER LIGHTS VERY DIM DURING PRE-FLIGHT CHECKS. ALL THREE EXTERIOR OVER WING EMERGENCY LIGHTS NOT ILLUMINATING. AFT EMERGENCY BATTERY PACK ISSUE SUSPECTED, NEED INSPECTION. ALL THE EMERGENCY UGHTS ARE WORKING WHILE CHARGINGSDR DXTA2019071002596Transducer · defectiveANTI SKID - DURING TAKEOFF ROLL & PRIOR TO V1, THE ANTI-SKID LIGHT ILLUMINATED. THE F/O CALLED ABORT, APPLIED BRAKING AND T/R'S. APPROXIMATELY, 1500 FEET PRIOR TO THE AIRCRAFT EXITING THE RUNWAY, I STARTED TO LOSE DIRECTIONAL CONTROL. "CORRECTIVE ACTION" REMOVSDR EBVR20192205001Skin · crackedRUDDER TRIM TAB WELL APPEARS TO HAVE A RIVET PULLING OUT. PERFORMED PRELIMINARY INSPECTION OF DAMAGE AND NOTED CRACKED SKIN AT AFT SPAR COMMON TO PULLED FASTENER. PERFORMED REPAIR TO TRAILING EDGE OF RUDDER IN TRIM TAB WELL PER ERO-958235 REV IR DATED 5/20/201SDR DXTA2014090305871Apu · defectiveGRAY SMOKE FILLED COCKPIT AND CABIN ON GROUND. APU WAS RUNNING WITH ACM. IMMEDIATELY SHUT DOWN APU AND ALL ELECTRICAL POWER. ENGINES WERE NOT RUNNING. SMOKE ODOR UNIDENTIFIED. COMPLIED WITH INSPECTION OF THE APU CONTAINMENT BOX AND CLEANED BLEED VALVE DUCSDR DXTA2013100205525Unknown · odorDURING TAXI OUT, SMELLED A STRANGE OIL TYPE ODOR AND NOTICED THE APU HAD SHUTDOWN. STOPPED AND INSPECTED EXTERIOR AND FOUND NOTHING OUT OF THE ORDINARY. ACCOMPLISHED A SUCCESSFUL APU TEST THEN STARTED IT AGAIN. SUPPLY AIR WAS AT AMBIENT TEMP. SHUTDOWN THE SDR DXTA2013080705472Spring · brokenWHEN NORMAL BRAKES ARE APPLIED AFTER LANDING, LEFT BRAKE PEDAL HAS VERY LITTLE RESISTANCE. DEPRESSES MUCH FARTHER THAN RIGHT PEDAL, CAUSING ACFT TO TURN LEFT. THIS OCCURS WITH BOTH CAPT AND F/O BRAKES. BLED BRAKES TWO TIMES EACH SIDE IAW MM 32-44-00. LT SDR DXTA2011091204722Strut · dischargedRAISED LANDING GEAR AFTER TAKEOFF AND RED UNLOCK LIGHT STAYED ON. ALL GREEN INDICATORS WENT OUT. IN ADDITION THE HYD PRESSURE STAYED ON AND STAB MISCOMPARE LIGHT CAME ON. PERFORMED COMPLETE NOSE GEAR STRUT SERVICING IAW MM 12-14-00. GEAR AND STAB OPS CHECKESDR DXTA200802761Downlock Switch · malfunctionedRT GEAR INDICATOR LIGHT SHOWED RT GEAR NOT DOWN AND LOCKED. PEFORMED GEAR SWING MANY TIMES WITH NO FAULTS. APPLIED FREEZE-IT SPRAY TO RT GEAR DOWNLOCK SWITCH GIVING US A FAULTY LIGHT AT GEAR INDICATION. REMOVED RT MAIN ACTUATOR AND INSTALLED REPAIRED ACTUASDR DXTA200601426Warning System · false activationANTI-SKID LIGHT ILLUMINATED ON SHORT FINAL. LOW BRAKE PRESSURE LIGHT FOLLOWED DURING TAXI. EMERGENCY BRAKE SYSTEM WAS UTILIZED. PWR BRK CIRCUIT BREAKER HAS POPED OUT. INSPECTED PWR BRAKE ANTI SKID SYSTEM. FOUND GEAR BRAKE PNEUMATIC BOTTLE PSI TO BE 1950 PSI
Back to N614QS, cancelled Mar 6, 2024