# Service difficulty reports: N325QS, cancelled Jun 9, 2011 A list on [N325QS, cancelled Jun 9, 2011](https://openairdocs.org/deregistered/N325QS-2011-06-09.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2010080904188](https://openairdocs.org/sdr/DXTA2010080904188.md): Brake Sys · weak · Aug 6, 2010 · N325QS · Cessna 560CESSNA · Landing Gear Brake System > BRAKES SPONGY BOTH PEDALS, BOTH SIDES. BLEED LT AND RT BRAKE SYS IAW MM 32-40-00. OPS CHECKED SATISFACTORY. - [SDR DXTA200807183181](https://openairdocs.org/sdr/DXTA200807183181.md): Starter Gen · faulty · Jul 18, 2008 · N325QS · Cessna 560CESSNA · Starter-Generator > LT FUEL FLOW FLUCTUATION DURING CLIMB AND CRUISE FOLLOWED BY LT GEN FAILURE, FOLLOWED BY LT ENGINE VIBRATION SUB: FOUND LT START GEN EXHAUST DUCT HAS LARGE AMOUNT OF SOOT. REMOVED AND REPLACED LT START GEN. C/W SATISFACTORY, OPS CHECK AND PARALLEL IAW MM 24- - [SDR DXTA200803181](https://openairdocs.org/sdr/DXTA200803181.md): Fuel Sys · fluctuates · Jul 17, 2008 · N325QS · Cessna 560CESSNA · Engine Fuel Distribution > LT FUEL FLOW FLUCTUATION DURING CLIMB AND CRUISE FOLLOWED BY LT ENG FAILURE, FOLLOWED BY LT ENGINE VIBRATION. - [SDR DXTA200803141](https://openairdocs.org/sdr/DXTA200803141.md): Control Cable · out of rig · Jun 24, 2008 · N325QS · Cessna 560CESSNA · Aileron Control System > THE AIRCRAFT HAS AN AGGRESSIVE ROLL LEFT WITH THE ASSOCIATED TRIM TAB CENTERED. PLACED A YOKE LEVEL ON THE YOKES AND OPENED THE AFT CABIN FLOOR. INSERTED A RIG PIN IN THE AILERON SECTOR. PLACED THE AILERON TRIM TO NEUTRAL. FOUND THE RT AILERON ABOVE STREAM LI - [SDR DXTA200702324](https://openairdocs.org/sdr/DXTA200702324.md): Vertical Gyro · faulty · Jul 8, 2007 · N325QS · Cessna 560CESSNA · Autopilot System > AUTOPILOT MALFUNCTION - LEVEL AT 41000 MSL, THE AUTOPILOT AGGRESSIVELY PITCHED UP TO OVER 1000 FPM. THE AUTOPILOT WAS DISCONNECTED. AFTER 1 MINUTE, THE AUTOPILOT WAS RECONNECTED AND PROBLEM REOCURRED. REMOVED FAULTY LT SIDE PITOT STATIC PORT HOSE AND NR 1 - [SDR DXTA200702104](https://openairdocs.org/sdr/DXTA200702104.md): Unknown · unknown · Apr 12, 2007 · N325QS · Cessna 560CESSNA · Aircraft Fuel Distribution System > DESCENDING THROUGH 11,000 FT, RT ENGINE LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED, TRIGGERING RT FUEL BOOST ANNUNCIATOR TO ILLUMINATE. RAN THE ABNORMAL CHECKLIST AND LANDED. NO ENGINE FLUCTUATIONS OR OTHER ENGINE INDICATIONS WERE NOTED. [SUP 4-19-07] SUMP - [SDR DXTA200702004](https://openairdocs.org/sdr/DXTA200702004.md): Master Cylinder · malfunctioned · Mar 7, 2007 · N325QS · Cessna 560CESSNA · Master Cylinder/Brake Valve > LT BRAKE ON RT SIDE TRAVELS ALMOST TO FLOOR DURING BRAKE APPLICATIONS. REMOVED CO-PILOTS IB AND OB BRAKE MASTER CYLINDERS AND INSTALLED NEW MASTER CYLINDERS IAW C560 MM 32-42-02. BLED BRAKES AS REQUIRED. - [SDR DXTA200701848](https://openairdocs.org/sdr/DXTA200701848.md): Coalescer Bag · dirty · Jan 10, 2007 · N325QS · Cessna 560CESSNA · Humidity Control System > SHARP IRRITATING ODOR/SMELL MAINLY IN COCKPIT, STRONGER RIGHT AFTER TAKE OFF REMAINED THROUGH WHOLE FLIGHT INCREASED AGAIN DURING DESCENT. RAN ENGINES FOR 30 MINUTES AT 70% FOUND NO ODOR. CHECK OIL LEVELS GOOD. NO SIGN OF EXTERNAL OIL LEAKS. CHECK ACM OIL LEVE - [SDR DXTA200601679](https://openairdocs.org/sdr/DXTA200601679.md): Brake · malfunctioned · Oct 20, 2006 · N325QS · Cessna 560CESSNA · Landing Gear Brake System > RIGHT SEAT LEFT BRAKE REQUIRES MORE PRESSURE FOR RESPONSIVENESS COMPAIRED TO RIGHT SEAT RIGHT BRAKE. SERVICED AND BLED BRAKE SYSTEM IAW CESSNA 560 MM CH. 32-42-00 - [SDR DXTA200601644](https://openairdocs.org/sdr/DXTA200601644.md): Hose · kinked · Oct 9, 2006 · N325QS · Cessna 560CESSNA · Landing Gear Brake System > DURING TAXI WHEN MAKING A SHARP LEFT TURN, FULL DEFLECTION OF RUDDER PEDALS, F/O'S LEFT BRAKE PEDAL WOULD BECOME STIFF AND ROLL FORWARD, UPON STRAIGHTENING NOSE GEAR BRAKES RETURNED TO NORMAL, ONLY ON F/O SIDE, ONLY DURING LEFT TURN. M2B - T/S TO LOWER HOSE O - [SDR DXTA200601631](https://openairdocs.org/sdr/DXTA200601631.md): Brake Assy · malfunctioned · Oct 4, 2006 · N325QS · Cessna 560CESSNA · Landing Gear Brake System > WHEN LEFT RUDDER PEDAL IS PUSHED TO THE FLOOR AND THEN LT BRAKE IS APPLIED THERE IS NO PRESSURE AND TRAVELED TO THE FLOOR WITH NO BRAKING ACTION. BLED BRAKES AS PER CE560 AMM 32-42-00. BRAKE SYSTEM OPERATED NORMALLY DURING NORMAL BRAKING, AND WITH FULL RUDDER - [SDR DXTA200601578](https://openairdocs.org/sdr/DXTA200601578.md): Brake · leaking · Aug 27, 2006 · N325QS · Cessna 560CESSNA · Brake > DURING TAXI AIRCRAFT PULLS HARD TO RIGHT WHEN BRAKES ARE APPLIED; POST FLIGHT INSPECTION SHOWS SMALL FLUID LEAK ON FRONT SIDE OF LEFT BRAKE. - [SDR DXTA200601471](https://openairdocs.org/sdr/DXTA200601471.md): Brake · contaminated · Jun 30, 2006 · N325QS · Cessna 560CESSNA · Brake Anti-Skid Section > BRAKES VERY SOFT, YOU HAVE TO PUSH BRAKE PEDALS A LOT FURTHER THAN NORMAL TO MAKE BRAKES WORK IAW CESSNA 560 MM 32-42-00, PERFORMED BRAKE BLEEDING MAINTENANCE PROCEDURE. FOUND LARGE AMOUNTS OF AIR IN SYSTEM ALONG W/ LOW BRAKE FLUID LEVEL. REMOVED AIR AND REP - [SDR DXTA200501139](https://openairdocs.org/sdr/DXTA200501139.md): Fcu · failed · Dec 11, 2005 · N325QS · Cessna 560CESSNA · Fuel Control/Turbine Engines > DID NOT GET FULL PWR ON RIGHT HAND ENGINE DURING STATIC TAKEOFF, N1 75.9 ITT 450, N2 83 WITH THROTTLES FULL FWD. REMOVED AND REPLACED RIGHT ENGINE FCU AND FUEL PUMP. ENGINE OPERATES NORMAL AT THIS TIME IAW PWA M/M 71-00-00. - [SDR DXTA200501045](https://openairdocs.org/sdr/DXTA200501045.md): Brake · malfunctioned · Oct 31, 2005 · N325QS · Cessna 560CESSNA · Landing Gear Brake System > PILOTS LEFT BRAKE ALMOST GOES TO THE FLOOR. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200501041](https://openairdocs.org/sdr/DXTA200501041.md): Transducer · malfunctioned · Oct 28, 2005 · N325QS · Cessna 560CESSNA · Brake Anti-Skid Section > CAPT LEFT BRAKE PEDAL INTERMITTENTLY LOSES PRESSURE IN TURNS. REMOVED AND REPLACED LT ANTI SKID TRANSDUCER IAW CE 560 MM 32-42-07. - [SDR DXTA200501021](https://openairdocs.org/sdr/DXTA200501021.md): Brake Assy · weak · Oct 14, 2005 · N325QS · Cessna 560CESSNA · Landing Gear Brake System > COPILOT'S BRAKE PEDALS ARE SOFT. ITEM IS UNDER INVESTIGATION. - [SDR 20001205SH007](https://openairdocs.org/sdr/20001205SH007.md): Skin · corroded · Nov 16, 2000 · N325QS · Cessna 560CESSNA · Wing, Plate/Skin > UPON INSPECTION OF WING DEICE BOOTS, THE AERODYNAMIC FILLER WAS DETERMINED TO BE SEPARATING FROM SKIN CAUSING THE DEICE BOOT TO DEBOND. THE DEICE BOOT WAS REMOVED AND SKIN CLEANED OF DEFECTION FILLER. AT THIS TIME, THE SKIN WAS FOUND TO BE CORRODED AT THE LO - [SDR 20001205SH006](https://openairdocs.org/sdr/20001205SH006.md): Skin · corroded · Nov 16, 2000 · N325QS · Cessna 560CESSNA · Wing, Plate/Skin > UPON INSPECTION OF WING DEICE BOOTS, THE AERODYNAMIC FILLER WAS DETERMINED TO BE SEPARATING FROM SKIN CAUSING THE DEICE BOOT TO DEBOND. THE DEICE BOOT WAS REMOVED AND SKIN CLEANED OF DEFECTION FILLER. AT THIS TIME, THE SKIN WAS FOUND TO BE CORRODED AT THE LO - [SDR 99ZZZX11](https://openairdocs.org/sdr/99ZZZX11.md): Nut · missing · Feb 27, 1998 · N325QS · Cessna 560CESSNA · Landing Gear Position and Warning > WHILE INSPECTING LANDING GEAR ASSY DETERMINED BOTH MAIN LANDING GEAR SQUAT SWITCHES MISSING JAM NUT THAT SECURES THE ROD END TO THE TORQUE LINK. THE SQUAT SWITCH ASSY COULD BE TURNED AND MOVED. ## 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 = 'N325QS' AND deregistration_id = 'N325QS-2011-06-09' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N325QS-2011-06-09/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.