# Service difficulty reports: N614QS, cancelled Mar 6, 2024 A list on [N614QS, cancelled Mar 6, 2024](https://openairdocs.org/deregistered/N614QS-2024-03-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2023122910462](https://openairdocs.org/sdr/DXTA2023122910462.md): Unknown · unknown · Dec 28, 2023 · N614QS · Cessna 560XL · Passenger/Crew Doors > DOOR 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 SEVERAL - [SDR DXTA2023122610424](https://openairdocs.org/sdr/DXTA2023122610424.md): Light · damaged · Dec 24, 2023 · N614QS · Cessna 560XL · Passenger Compartment Lighting > AFTER 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 DISC - [SDR DXTA2023100997520](https://openairdocs.org/sdr/DXTA2023100997520.md): Unknown · unknown · Oct 8, 2023 · N614QS · Cessna 560XL · Emergency Lighting > FORWARD 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 DXTA2023071891160](https://openairdocs.org/sdr/DXTA2023071891160.md): Unknown · unknown · Jul 17, 2023 · N614QS · Cessna 560XL · Passenger/Crew Doors > MAIN 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 DEFEC - [SDR DXTA2023030281550](https://openairdocs.org/sdr/DXTA2023030281550.md): None · none · Mar 1, 2023 · N614QS · Cessna 560XL · Passenger/Crew Doors > MAIN 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 DXTA2022042961080](https://openairdocs.org/sdr/DXTA2022042961080.md): Pcb · defective · Apr 28, 2022 · N614QS · Cessna 560XL · Central Warning > ANNUNCIATOR 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/N - [SDR DXTA2022041860360](https://openairdocs.org/sdr/DXTA2022041860360.md): None · none · Apr 15, 2022 · N614QS · Cessna 560XL · Door Warning System > WHILE 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 I - [SDR DXTA2022033159410](https://openairdocs.org/sdr/DXTA2022033159410.md): None · none · Mar 30, 2022 · N614QS · Gulstm 560 · Engine (Turbine/Turboprop) > ENGINE 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 ENGI - [SDR DXTA2022021156540](https://openairdocs.org/sdr/DXTA2022021156540.md): Not Reported · not reported · Feb 10, 2022 · N614QS · Cessna 560XL · Emergency Lighting > LEFT 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 DXTA2021090748180](https://openairdocs.org/sdr/DXTA2021090748180.md): Battery · defective · Sep 3, 2021 · N614QS · Cessna 560XL · Emergency Lighting > EMERGENCY 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 CHARGING - [SDR DXTA2019071002596](https://openairdocs.org/sdr/DXTA2019071002596.md): Transducer · defective · Jul 9, 2019 · N614QS · Cessna 560XL · Brake Anti-Skid Section > ANTI 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" REMOV - [SDR EBVR20192205001](https://openairdocs.org/sdr/EBVR20192205001.md): Skin · cracked · May 22, 2019 · N614QS · Cessna 560XL · Rudder, Tab Structure > RUDDER 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 5/20/201 - [SDR DXTA2014090305871](https://openairdocs.org/sdr/DXTA2014090305871.md): Apu · defective · Sep 2, 2014 · N614QS · Cessna 560XL · APU Core Engine > GRAY 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 DUC - [SDR DXTA2013100205525](https://openairdocs.org/sdr/DXTA2013100205525.md): Unknown · odor · Oct 1, 2013 · N614QS · Cessna 560XL · Air Distribution System > DURING 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 DXTA2013080705472](https://openairdocs.org/sdr/DXTA2013080705472.md): Spring · broken · Aug 6, 2013 · N614QS · Cessna 560XL · Landing Gear Brake System > WHEN 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 DXTA2011091204722](https://openairdocs.org/sdr/DXTA2011091204722.md): Strut · discharged · Sep 11, 2011 · N614QS · Cessna 560XL · Nose/Tail Landing Gear Strut/Axle > RAISED 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 CHECKE - [SDR DXTA200802761](https://openairdocs.org/sdr/DXTA200802761.md): Downlock Switch · malfunctioned · Jan 10, 2008 · N614QS · Cessna 560XL · Landing Gear Position and Warning > RT 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 ACTUA - [SDR DXTA200601426](https://openairdocs.org/sdr/DXTA200601426.md): Warning System · false activation · Jun 5, 2006 · N614QS · Cessna 560XL · Landing Gear Brake System > ANTI-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 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N614QS-2024-03-06/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.