# N325QS: 1997 Cessna 560, registration cancelled 2011-06-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 9, 2011 - Exported to: Canada - Status when cancelled: Valid registration - Airframe: [Cessna 560](https://openairdocs.org/model/cessna-560) (registry code 2076750) - Engine: [Pratt & Whitney Canada JT15D 5 series](https://openairdocs.org/engine/pratt-whitney-canada-jt15d-5-series) (registry code 52113) - Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE) (OpenAirDocs) - Serial number: 560-0425 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 11, 1997 - Certificate issued: January 11, 2011 - Last registry action: June 9, 2011 - Mode S code: A38252 - Owner when cancelled: [Wells Fargo Bank Northwest Na Trustee](https://openairdocs.org/faa-owner/WELLS%20FARGO%20BANK%20NORTHWEST%20NA%20TRUSTEE) - Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City) - Owner type: Corporation - Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N325QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=325QS - Page: https://openairdocs.org/deregistered/N325QS-2011-06-09 From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Cessna 560: https://openairdocs.org/model/cessna-560.md ## Service difficulty reports (20) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2010080904188](https://openairdocs.org/sdr/DXTA2010080904188), Aug 6, 2010: BRAKE SYS. WEAK. 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), Jul 18, 2008: STARTER GEN. FAULTY. 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 AMOU - [SDR DXTA200803181](https://openairdocs.org/sdr/DXTA200803181), Jul 17, 2008: FUEL SYS. FLUCTUATES. 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), Jun 24, 2008: CONTROL CABLE. OUT OF RIG. 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 - [SDR DXTA200702324](https://openairdocs.org/sdr/DXTA200702324), Jul 8, 2007: VERTICAL GYRO. FAULTY. AUTOPILOT MALFUNCTION - LEVEL AT 41000 MSL, THE AUTOPILOT AGGRESSIVELY PITCHED UP TO OVER 1000 FPM. THE AUTOPILOT WAS DISCONNECTED. AFTER 1 MINUTE, THE AUTOPILO - [SDR DXTA200702104](https://openairdocs.org/sdr/DXTA200702104), Apr 12, 2007: UNKNOWN. UNKNOWN. DESCENDING THROUGH 11,000 FT, RT ENGINE LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED, TRIGGERING RT FUEL BOOST ANNUNCIATOR TO ILLUMINATE. RAN THE ABNORMAL CHECKLIS - [SDR DXTA200702004](https://openairdocs.org/sdr/DXTA200702004), Mar 7, 2007: MASTER CYLINDER. MALFUNCTIONED. 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 - [SDR DXTA200701848](https://openairdocs.org/sdr/DXTA200701848), Jan 10, 2007: COALESCER BAG. DIRTY. SHARP IRRITATING ODOR/SMELL MAINLY IN COCKPIT, STRONGER RIGHT AFTER TAKE OFF REMAINED THROUGH WHOLE FLIGHT INCREASED AGAIN DURING DESCENT. RAN ENGINES FOR 30 MI - [SDR DXTA200601679](https://openairdocs.org/sdr/DXTA200601679), Oct 20, 2006: BRAKE. MALFUNCTIONED. 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- - [SDR DXTA200601644](https://openairdocs.org/sdr/DXTA200601644), Oct 9, 2006: HOSE. KINKED. 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 - [SDR DXTA200601631](https://openairdocs.org/sdr/DXTA200601631), Oct 4, 2006: BRAKE ASSY. MALFUNCTIONED. 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 - [SDR DXTA200601578](https://openairdocs.org/sdr/DXTA200601578), Aug 27, 2006: BRAKE. LEAKING. 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), Jun 30, 2006: BRAKE. CONTAMINATED. 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 P - [SDR DXTA200501139](https://openairdocs.org/sdr/DXTA200501139), Dec 11, 2005: FCU. FAILED. 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 - [SDR DXTA200501045](https://openairdocs.org/sdr/DXTA200501045), Oct 31, 2005: BRAKE. MALFUNCTIONED. PILOTS LEFT BRAKE ALMOST GOES TO THE FLOOR. ITEM IS UNDER INVESTIGATION. - [SDR DXTA200501041](https://openairdocs.org/sdr/DXTA200501041), Oct 28, 2005: TRANSDUCER. MALFUNCTIONED. 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), Oct 14, 2005: BRAKE ASSY. WEAK. COPILOT'S BRAKE PEDALS ARE SOFT. ITEM IS UNDER INVESTIGATION. - [SDR 20001205SH007](https://openairdocs.org/sdr/20001205SH007), Nov 16, 2000: SKIN. CORRODED. 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 REMOV - [SDR 20001205SH006](https://openairdocs.org/sdr/20001205SH006), Nov 16, 2000: SKIN. CORRODED. 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 REMOV - [SDR 99ZZZX11](https://openairdocs.org/sdr/99ZZZX11), Feb 27, 1998: NUT. MISSING. 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 SWITC ## Other aircraft with N325QS - [Registered now](https://openairdocs.org/aircraft/N325QS): Embraer S A EMB-505, S/N 50500168, built 2013 --- 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.