# N318QS: 1997 Cessna 560, registration cancelled 2011-05-13 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 13, 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: 560-0418 - Year built: 1997 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 17, 1997 - Certificate issued: January 11, 2011 - Last registry action: May 13, 2011 - Mode S code: A365F8 - 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/N318QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=318QS - Page: https://openairdocs.org/deregistered/N318QS-2011-05-13 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 (17) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2010030504014](https://openairdocs.org/sdr/DXTA2010030504014), Mar 4, 2010: BRAKE. MALFUNCTIONED. ON TAXI OUT THE CO PILOTS RT BRAKE WAS GRABBING AND WAS DIFFICULT TO KEEP THE ACFT STRAIGHT ON TAXIWAY. THE RT BRAKE SEEMED HARDER PRESSURE THAN LT. THE LT BRAK - [SDR DXTA2010012703957](https://openairdocs.org/sdr/DXTA2010012703957), Jan 26, 2010: MASTER CYLINDER. WEAK. COPILOT SIDE, RT BRAKE PEDAL GOES SOFT DURING TAXI. AFTER PEDAL WAS ALMOST TO THE FLOOR, RELEASED PRESSURE, AND BRAKING WAS RESTORED. THIS HAPPENED 5 TIMES ON A - [SDR DXTA2010012503956](https://openairdocs.org/sdr/DXTA2010012503956), Jan 24, 2010: PEDAL. FAILED. WHILE TAXIING FROM RT SEAT, THE RT BRAKE PEDAL WENT ALL THE WAY DOWN TO THE FLOOR. PERFORMED RT BRAKE BLEEDING PROCEDURES 4 TIMES IAW MM CH 32-42-00. - [SDR DXTA2010012203950](https://openairdocs.org/sdr/DXTA2010012203950), Jan 21, 2010: BRAKE ASSY. WEAK. DURING TAXI FO SIDE RT BRAKE PEDAL WENT ALL THE WAY DOWN WITH NO PRESSURE. BLED RT BRAKE IAW MM 32-42-00. PERFORMED TAXI CHECK. OPS CHECK GOOD IAW MM 32-42-01. - [SDR DXTA2009121603898](https://openairdocs.org/sdr/DXTA2009121603898), Dec 6, 2009: ROD. OUT OF ADJUST. WHEN RT THROTTLE WAS RETARDED TO IDLE AFTER SPEED BRAKE CHECK, RT ENGINE FLAMED OUT. N1, N2, AND ITT WENT SMOOTHLY TO ZERO. OPERATED RT ENG AND DUPLICATED DISCR - [SDR DXTA2009090303771](https://openairdocs.org/sdr/DXTA2009090303771), Sep 4, 2009: DISPLAY. INOPERATIVE. DISPLAY FAILED ON TAXI, SEC FLT DISPLAY CIRCUIT BREAKER POPPED, ACRID ODOR IN COCKPIT BREAKER WAS NOT RESET. CONFIRMED FAILURE INSIDE INDICATOR. INSPECTED ALL S - [SDR DXTA200809103272](https://openairdocs.org/sdr/DXTA200809103272), Sep 10, 2008: CONTROL VALVE. INOPERATIVE. DURING TAKEOFF ROLL AT 50 KNOTS W/S AIR O-HEAT ANNUNCIATOR LIGHT ILLUMINATED, PERFORMED ABORT. WHEN POWER WAS REDUCED LIGHT WENT OUT. REMOVED WINDSHIELD BLEED A - [SDR DXTA200803272](https://openairdocs.org/sdr/DXTA200803272), Sep 10, 2008: WARNING LIGHT. ILLUMINATED. DURING TAKEOFF ROLL AT 50 KNOTS W/S AIR O-HEAT ANNUNCIATOR LIGHT ILLUMINATED, PERFORMED ABORT. (K) - [SDR DXTA200803022](https://openairdocs.org/sdr/DXTA200803022), Apr 24, 2008: BRAKE SYS. MALFUNCTIONED. COPILOT'S LT BRAKE PEDAL REQUIRES SIGNIFICANTLY MORE TILT TO ENGAGE BRAKE THAN RT PEDAL, NO VISIBLE FLUID OR LEAKS. BLED BRAKES IAW MM 32-42-00. OPS CHECK GOOD. - [SDR DXTA200702100](https://openairdocs.org/sdr/DXTA200702100), Apr 11, 2007: BRAKE. WEAK. CO-PILOT LT BRAKE IS (SOFT). [SUP 4-19-07] USED BRAKE BLEED PROCEDURE FOR ANTI-SKID SYSTEM FOR CO-PILOTS LT BRAKE IAW. CESSNA 560 MM 32-42-00 CHECKS GOOD. - [SDR DXTA200601757](https://openairdocs.org/sdr/DXTA200601757), Nov 25, 2006: SQUAT SWITCH. OUT OF ADJUST. LEVEL AT 13,000 MSL, RAPID PRESSURIZING OCCURRED. CABIN CLIMBED AT 6000 FPM. RATE OF CLIMB OR SOURCE SELECT KNOB HAS NO EFFECT. CABIN ATITUDE SELECTOR SET AT 40 - [SDR 2006FA0000497](https://openairdocs.org/sdr/2006FA0000497), May 9, 2006: THRESHOLD. CRACKED. CABIN ENTRY THRESHOLD CRACKED AT AFT STEP ATTACH BOLT HOLE. COMBINATION OF BOLT HOLE LOCATED IN RADIUS OF FRAME AND MATERIAL THICKNESS NOT SUFFICIENT TO SUPPORT - [SDR DXTA200601198](https://openairdocs.org/sdr/DXTA200601198), Jan 16, 2006: WIRE. BROKEN. LEFT MAIN LANDING GEAR FAILED TO RETRACT AFTER T/O. RED -UNLOCK- LIGHT REMAINED ILLUMINATED AS WELL AS THE LEFT MAIN -DOWN & LOCKED- LIGHT. AFTER RECYCLING THE - [SDR DXTA200500737](https://openairdocs.org/sdr/DXTA200500737), May 22, 2005: RETRACT CYLINDER. DAMAGED. LEFT MAIN WOULD NOT RETRACT. - PERFORMED GEAR SWINGS AND TROUBLESHOOTING IAW CE560 MM CHAPTER 32-30-00 WITH NO DISCREPANCIES NOTED. SUSPECTED MLG RETRACT ACTUAT - [SDR DXTA200400335](https://openairdocs.org/sdr/DXTA200400335), Jul 12, 2004: MOTOR. BURNED OUT. DURING SHUT DOWN, VERY STRONG BURNING RUBBER ODOR DETECTED COMING FROM OVERHEAD VENTS. AFTER SHUTDOWN INSPECTED AFT EQUIPMENT BAY AND NOTED VERY STRONG BURNING - [SDR DXTA200400263](https://openairdocs.org/sdr/DXTA200400263), Mar 15, 2004: O-RING. FAILED. BRAKES FAILED WHILE TAXIING, POWER BRAKE AND ANTI-SKID INOP, ANNUNCIATOR ILLUMINATED. FOUND BRAKE SYSTEM LEAKING FROM THE ANTI-SKID SYSTEM PUMP. REPLACED O-RING - [SDR 99ZZZX10](https://openairdocs.org/sdr/99ZZZX10), Mar 19, 1998: IGNITER. DAMAGED. REMOVED IGNITER FOR PHASE 4 INSPECTION. DETERMINED CENTER ELECRTRODE MISSING. SUBMITTER STATED THIS IS SUPPOSED TO BE NEW STYLE PLUG, TO PREVENT THIS. REPLACED ## Other aircraft with N318QS - [Registered now](https://openairdocs.org/aircraft/N318QS): Embraer S A EMB-505, S/N 50500162, 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.