# Service difficulty reports: N575QS A list on [N575QS](https://openairdocs.org/aircraft/N575QS.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2025011701984](https://openairdocs.org/sdr/DXTA2025011701984.md): Battery · no test · Jan 15, 2025 · N575QS · Cessna 560XL · Emergency Lighting > ALL CABIN EMERGENCY LIGHTS WORK CORRECTLY WITH AIRCRAFT BATTERY SWITCH ON. TURNING AIRCRAFT BATTERY SWITCH TO OFF, ALL FORWARD EMERGENCY LIGHTS ARE INOP. THE REAR EMERGENCY LIGHTS WORK CORRECTLY WITHOUT AIRCRAFT BATTERY SWITCH ON. CORRECTIVE ACTION: REPLACED F - [SDR DXTA2024122401642](https://openairdocs.org/sdr/DXTA2024122401642.md): Display · faulted · Dec 21, 2024 · N575QS · Cessna 560XL · Central Display > AT CRUISE LOST PFD 1 MFD AND FMS. CAMEBACK IN ABOUT 10 MINS. FMS GAVE MSG GPS 1 LOST & NO REQUIRED SENSORS AFTER IT CAME BACK ON. POWERED ACFT & AVIONICS SYSTEMS AND MONITORED FOR 1 HOUR WITH NO DEFECTS. UNABLE TO DUPLICATE DISCREPANCY. PER MCC, PERFORMED IN - [SDR DXTA2023101697990](https://openairdocs.org/sdr/DXTA2023101697990.md): Unknown · unknown · Oct 15, 2023 · N575QS · Cessna 560XL · Passenger/Crew Doors > MAIN DOOR ACOUSTIC SEAL: THE SEAL REMAINS INFLATED WITH THE APU RUNNING MAKING IT VERY DIFFICULT TO OPEN THE DOOR. SEE PHOTOS. //SIGNOFF// ARRIVED AT AC. POWERED ON APU AS REQUIRED. PERFORMED MULTIPLE CYCLES OF THE MAIN ENTRY DOOR. SEAL INFLATED AND DEFLATED A - [SDR 3J7R2023091100001](https://openairdocs.org/sdr/3J7R2023091100001.md): Battery · discharged · Sep 11, 2023 · N575QS · Cessna 560XL · Emergency Lighting > DURING THE MAINTENANCE CHECK, THE FORWARD EMERGENCY LIGHTS WERE FOUND INOPERATIVE ON EMER. BATT POWER. - [SDR DXTA2023091195060](https://openairdocs.org/sdr/DXTA2023091195060.md): Unknown · unknown · Sep 9, 2023 · N575QS · Cessna 560XL · Emergency Lighting > EMERGENCY LIGHTING: ALL INTERIOR AND EXTERIOR EMERGENCY LIGHTS REMAIN ON WITH THE SWITCH IN THE ARM POSITION. APU RUNNING WITH APU GEN OPERATING MAIN DC. AMBER LIGHT NOT ANNUNCIATED. EMG LIGHT SWITCH FUNCTIONS NORMAL IN THE OFF AND ON POSITIONS. //SIGNOFF// - [SDR DXTA2023060287690](https://openairdocs.org/sdr/DXTA2023060287690.md): Unknown · unknown · Jun 2, 2023 · N575QS · Cessna 560XL · Passenger/Crew Doors > MAIN CABIN DOOR CENTER INSPECTION WINDOW GREEN FLAG NEEDS ADJUSTMENT. GREEN FLAG IS MOSTLY VISIBLE WITH THE DOOR IN THE OPEN POSITION, SEE ATTACHED PICTURE FROM OPEN POSITION. THE GREEN FLAG PARTIAL IN THE INSPECTION WINDOW IN THE CLOSED POSITION.//CORRECTIVE - [SDR DXTA2022042560850](https://openairdocs.org/sdr/DXTA2022042560850.md): None · none · Apr 23, 2022 · N575QS · Cessna 560XL · Passenger/Crew Doors > CABIN EXTERNAL HANDLE IS VERY LOOSE. IF ANY WEIGHT IS PLACED ON IT, IT DROPS DOWN ALMOST TO THE DOOR SUPPORTS. ANYONE USING IT AS A HAND RAIL WHILE DEPARTING THE PLANE WILL MOST DEFINITELY FALL. "CORRECTIVE ACTION" INSTALLED CUSTOMER SUPPLIED NEW PIN PN MS3567 - [SDR DXTA2021082647750](https://openairdocs.org/sdr/DXTA2021082647750.md): Battery Pack · defective · Aug 25, 2021 · N575QS · Cessna 560XL · Emergency Lighting > EMERG EXIT SIGN/LIGHT: ON POST FLIGHT FOUND THE FORWARD EMER EXIT LIGHT AND FORWARD DROPPED AISLE LIGHT TO BE INOP WITH AND WITHOUT EMERGENCY POWER SELECTED ON. REMOVED AND REPLACED FORWARD EMERAENCY LIAHTS BATTERY PACK. BATTERY CHARAED AND OPS CHECK IS GOOD. - [SDR DXTA2021021504744](https://openairdocs.org/sdr/DXTA2021021504744.md): Rod · inoperative · Feb 14, 2021 · N575QS · Cessna 560XL · Passenger/Crew Doors > MAIN DOOR TELESCOPING ROD: MAIN CABIN DOOR WILL NOT CLOSE. TELESCOPING ARMS WILL NOT FULLY RETRACT. AIRCRAFT DEPARTED SC IN MODERATE TO HEAVY RAIN. OUTSIDE AIR TEMPERATURE IN MDW IS CURRENTLY -18C. FBO WILL NOT PROVIDE HANGAR SPACE. REMOVED AFT STRUT AND - [SDR 2020F00021](https://openairdocs.org/sdr/2020F00021.md): Skin · chafed · Aug 28, 2019 · N575QS · Cessna 560XL · Wing, Plate/Skin > REPAIR OF LEFT WING LEADING EDGE DAMAGE (CHAFING AGAINST PICCOLO TUBE). REPAIR MEMO DQ22885M1 DATED 8/28/2019. - [SDR 2020F00020](https://openairdocs.org/sdr/2020F00020.md): Tube · chafed · Aug 28, 2019 · N575QS · Cessna 560XL · Pneumatic Distribution System > REPAIR OF LH AND RH LEADING EDGE PICCOLO TUBE DAMAGE (CHAFE). TEXTRON AVIATION REPAIR MEMO DQ22817M1 DATED 8/28/2019. - [SDR DXTA2018123100847](https://openairdocs.org/sdr/DXTA2018123100847.md): Coalescer Bag · dirty · Dec 28, 2018 · N575QS · Cessna 560XL · Humidity Control System > COCKPIT ODOR OIL SMELL - ENROUTE THERE WAS A STRONG OIL SMELL THROUGH THE OVERHEAD VENTS. REMOVED AND REPLACED ACM CONDENSER SOCK WITH A NEW PART IAW MM 21-51-00 OPERATIONAL AND LEAK CHECKS SATISFACTORY - [SDR DXTA2018101601559](https://openairdocs.org/sdr/DXTA2018101601559.md): Motor · failed · Oct 15, 2018 · N575QS · Cessna 560XL · Landing Gear Brake System > BRAKE PRESSURE LIGHT ILLUMINATED - UPON FINAL APPROACH FIX INBOUND ON THE GPS RWY 23 APPROACH, THE LOW BRAKE PRESSURE/ANTI SKID LIGHT ILLUMINATED AND STAYED ILLUMINATED TILL WE INITIATED THE MISSED APPROACH. AT WHICH TIME WE DECLARED AN EMERGENCY RAN THE CHEC - [SDR EBVR20180831001](https://openairdocs.org/sdr/EBVR20180831001.md): Torque Tube · corroded · Aug 31, 2018 · N575QS · Cessna 560CESSNA · Elevator Structure > FOUND DURING VERTICAL STAB INTERNAL INSPECTION. RT ELEVATOR TORQUE TUBE HAS RUST NEAR WELD. REMOVED EXISTING RUSTED TORQUE TUBE ON RT ELEVATOR AND REPLACED WITH NEW TORQUE TUBE P/N 6634002-16 PER SRM 51-40-03, 55-20-01-2(REV 15) AND ERO-928943-6 REV IR DATED 8 - [SDR DXTA2018010400425](https://openairdocs.org/sdr/DXTA2018010400425.md): Seal · leaking · Dec 30, 2017 · N575QS · Cessna 560XL · APU Oil System > OIL ODOR IN THE COCKPIT AND CABIN. ODOR IS STRONGER WHEN THE APU IS RUNNING. INSPECTED THE APU AND FOUND STARTER GEN PAD SEAL LEAKING. REPLACED WATER COALESCER SOCK. RAN BOTH ENGINES AND NO ODOR NOTED. PULLED AND COLLARED APU MASTER C/B. - [SDR DXTA2018010200001](https://openairdocs.org/sdr/DXTA2018010200001.md): Seal · leaking · Dec 30, 2017 · N575QS · Cessna 560XL · Starter-Generator > OILY SMELL IN COCKPIT AND CABIN SMELL IS STRONGER WHEN THE APU IS RUNNING. INSPECTED APU AND FOUND STARTER/GEN PAD SEAL LEAKING. REPLACED WATER COALESCER SOCK. RAN BOTH ENGINES AND NO ODOR NOTED. APU DEFERRED IN ACCORDANCE WITH CE560XLS MEL. COMPLIED WITH MEL - [SDR DXTAT2PL6D005C3ZJ](https://openairdocs.org/sdr/DXTAT2PL6D005C3ZJ.md): Lead · damaged · Aug 28, 2017 · N575QS · Cessna 560XL · Electrical Power System Wiring > IN FLIGHT WITH BOTH ENGINE GENERATORS ONLINE, RIGHT GENERATOR SHOWED 110 AMP LOAD AND LEFT GENERATOR SHOWED 60 AMP LOAD FOR AN ABNORMAL GENERATOR SPLIT. INSTALLED THE WASHERS AND LEADS FOR THE LH AND RH STARTER GENERATOR IAW MM 80-10-00. OPERATIONAL CHECKS - [SDR CWQR20140630004](https://openairdocs.org/sdr/CWQR20140630004.md): Hinge · cracked · Jun 30, 2014 · N575QS · Cessna 560XL · Rudder Structure > DURING A SCHEDULED INSPECTION, TECHNICIAN WAS INSPECTING THE RUDDER HINGES. ON THE UPPER RUDDER ATTACH HINGE, THE LOWER HINGE HALF HE FOUND A 0.21 INCH CRACK FROM THE BRACKET EDGE EXTENDING TOWARDS THE FIRST ATTACHMENT HOLE. RUDDER HINGE HALF WAS REMOVED & A - [SDR DXTA2012080205072](https://openairdocs.org/sdr/DXTA2012080205072.md): Wire · chafed · Aug 1, 2012 · N575QS · Cessna 560XL · Light System Wiring > SHORTLY AFTER TAKEOFF AN ODOR OF SMOKE APPEARED IN THE CABIN. ONE OF THE PASSENGERS ADVISED THAT THE FORWARD ENTRY LIGHT AT THE TOP OF THE STAIRS WAS ARCING. UPON LANDING WE FOUND THAT THE PLASTIC LENS WAS MELTED. FOUND FWD ENTRY LIGHT HAD CHAFED WIRE ARCING - [SDR DXTA2011030704491](https://openairdocs.org/sdr/DXTA2011030704491.md): Warning Light · false indication · Mar 6, 2011 · N575QS · Cessna 560XL · Landing Gear Position and Warning > ON DEPARTURE AFTER LANDING GEAR RETRACTION RED UNLOCK LIGHT REMAINED ILLUMINATED. ALL THREE GREEN LIGHTS WERE EXTINGUISHED. COMPLIED WITH GEAR EXTENSION & RETRACTION TEST IAW MM 32-30-00 R20. OPS CHECKED GOOD AT THIS TIME. INSPECTED UPLOCK SWITCHES. NO DEFE - [SDR DXTA2010121104360](https://openairdocs.org/sdr/DXTA2010121104360.md): Warning Light · illuminated · Dec 9, 2010 · N575QS · Cessna 560XL · Engine Thrust Reverser > DURING TAKEOFF AND CLIMBOUT, THE LT ENGINE THRUST REVERSER UNLOCK LIGHT ILLUMINATED PASSING THROUGH 6000' AND 235 KIAS. EMERGENCY STOW SWITCH WAS PLACED IN EMERGENCY POSITION. EMERGENCY CHECKLIST WAS COMPLETED AND AIRSPEED REDUCED BELOW 200 KIAS. TR "UNLOCK" L - [SDR DXTA200809013259](https://openairdocs.org/sdr/DXTA200809013259.md): Lamp · burned out · Sep 1, 2008 · N575QS · Cessna 560XL · Landing Gear Position and Warning > LT MAIN GEAR DID NOT INDICATE GREEN. PREFORMED CK LIST AND BLEW GEAR DOWN STILL NO INDICATION. REDUCED POWER BELOW 500 FT AND FULL FLAPS TO CK FOR GEAR WARNING DID NOT GET GEAR WARNING, SO LANDED UNEVENTFUL. FOUND BOTH LT INDICATOR BULBS BURNED OUT. REMOVED ## 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 = 'N575QS' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N575QS/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.