# N371QS: 1998 Cessna 560, registration cancelled 2011-06-02 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: June 2, 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: 560-0471 - Year built: 1998 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 30, 1998 - Certificate issued: January 11, 2011 - Last registry action: June 2, 2011 - Mode S code: A438F1 - 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/N371QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=371QS - Page: https://openairdocs.org/deregistered/N371QS-2011-06-02 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 (28) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2010071204148](https://openairdocs.org/sdr/DXTA2010071204148), Jul 9, 2010: TRIM SYSTEM. LOOSE. ON TAKEOFF WITH PITCH TRIM IN TAKEOFF RANGE REQUIRED EXCESSIVE AFT YOKE FORCE TO GET NOSE OFF GROUND. AFTER AIRBORNE FULL NOSE UP TRIM APPLIED & REQUIRES EXCESS - [SDR DXTA200902020348A](https://openairdocs.org/sdr/DXTA200902020348A), Jan 31, 2009: BRAKE. UNSERVICEABLE. DURING TAXI, AIRPLANE PULLS LT WHILE BRAKING FROM THE PILOTS SIDE. R&R RT BRAKE ASSY IAW MM 32-42-00. - [SDR 2008FA0000790](https://openairdocs.org/sdr/2008FA0000790), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000789](https://openairdocs.org/sdr/2008FA0000789), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000788](https://openairdocs.org/sdr/2008FA0000788), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000787](https://openairdocs.org/sdr/2008FA0000787), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000786](https://openairdocs.org/sdr/2008FA0000786), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000785](https://openairdocs.org/sdr/2008FA0000785), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000784](https://openairdocs.org/sdr/2008FA0000784), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000783](https://openairdocs.org/sdr/2008FA0000783), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000782](https://openairdocs.org/sdr/2008FA0000782), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000781](https://openairdocs.org/sdr/2008FA0000781), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000780](https://openairdocs.org/sdr/2008FA0000780), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000779](https://openairdocs.org/sdr/2008FA0000779), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR 2008FA0000778](https://openairdocs.org/sdr/2008FA0000778), Oct 29, 2008: RIB. CRACKED. WHILE PERFORMING THE PHASE 1-5 INSP, CRACKS WERE NOTICED IN SEVERAL RIBS LOCATED INSIDE THE LT AND RT HORIZ STABILIZERS. AFTER REMOVAL OF THE TOP SKINS ON BOTH - [SDR DXTA200803065](https://openairdocs.org/sdr/DXTA200803065), May 17, 2008: ACTUATOR. MALFUNCTIONED. UPON LOWERING LANDING GEAR, BOTH MAIN GEAR LIGHTS WERE GREEN, BUT THE NOSE GEAR LIGHT DID NOT ILLUMINATE. REPLACED NLG ACTUATOR WITH REPAIRED UNIT PERFORMED PRO - [SDR DXTA200702648](https://openairdocs.org/sdr/DXTA200702648), Dec 4, 2007: ARM. OUT OF RIG. AFTER TAKEOFF GEAR WOULDN'T RETRACT. SECURED GEAR AND FOUND BLOW DOWN BOTTLE ARM AND HANDLE/CABLE OUT OF PROPER RIG. RE-RIGGED AND SERVICED BOTTLE. COMPLETED SE - [SDR DXTA200702403](https://openairdocs.org/sdr/DXTA200702403), Aug 14, 2007: BRAKE ASSY. UNKNOWN. COPILOT BRAKE PEDALS NEED TO BE PUSHED ALMOST FULL DOWN BEFORE ANY BRAKE APPLICATION IS FELT. ONCE YOU REACH THAT POINT, THE BRAKE PEDAL "FEEL" IS NORMAL. BLED - [SDR DXTA200702398](https://openairdocs.org/sdr/DXTA200702398), Aug 12, 2007: MASTER CYLINDER. BYPASSING. DURING TAXI BRAKE CHECK, FOUND COPILOT BRAKE PEDALS WERE VERY SPONGY AND THE PEDAL TRAVEL IS 3 TIMES MORE THAN THE CAPTAINS SIDE. THE RIGHT COPILOT PEDAL IS WOR - [SDR DXTA200702395](https://openairdocs.org/sdr/DXTA200702395), Aug 9, 2007: BRAKE ASSY. WEAK. RT SEAT BRAKES VERY MUSHY WHEN BRAKE PRESSURE APPLIED. M2B- BLED BRAKE SYSTEM PER CHAPTER 32-42-00 OF THE CITATION 560 MM OPERATIONAL AND LEAK CHECK GOOD. - [SDR CWQR200708](https://openairdocs.org/sdr/CWQR200708), Jul 31, 2007: SUPPORT CHANNEL. CRACKED. DURING MAINTENANCE FOUND THE RUDDER UPPER SUPPORT CHANNEL CRACKED WHERE IT ATTACHES TO THE INSTRUMENT PANEL. THIS AIRCRAFT HAD SL560-27-13 COMPLIED WITH 826.6 H - [SDR DXTA200702327](https://openairdocs.org/sdr/DXTA200702327), Jul 10, 2007: BRAKE ASSY. WEAK. BRAKES ARE VERY SPONGY USING BOTH SETS OF RUDDER PEDALS. INSPECTED AND BLEED BOTH LT AND RT BRAKE ASSY. NO DEFECTS FOUND, OPS CK GOOD IAW MM CH 32-42-00. - [SDR DXTA200702258](https://openairdocs.org/sdr/DXTA200702258), Jun 12, 2007: BRAKE. MALFUNCTIONED. ANTI SKID SEEMS TO ACTIVATE AROUND 40 KNOTS. BRAKES SEEM TO GRAB AND RELEASE SERVERAL TIMES. TAXIED AIRCRAFT WITH ANTI-SKID ON. WHEN TAXI WAY WET AND DRY. SYSTE - [SDR DXTA200702223](https://openairdocs.org/sdr/DXTA200702223), May 29, 2007: CONTROLLER. INOPERATIVE. WITH THE W/S BLEED ANTI ICE ON LOW (APPROX 3-5 MINUTES AFTER BEING SWITCHED ON) THE W/S O'HEAT ILLUMINATED WITH SMOKE/HAZE IN THE COCKPIT AND CABIN ALONG WITH S - [SDR DXTA200601189](https://openairdocs.org/sdr/DXTA200601189), Jan 10, 2006: PUMP. MALFUNCTIONED. LEFT FUEL BOOST PUMP CAME ON DURING TAKEOFF ROLL, ABORTED. PERFORMED RUN UP AFTER RESETTING PUMP, CAME ON AGAIN. PERFORMED 3RD RUN UP ON RAMP, DID NOT COME ON. - [SDR DXTA200500752](https://openairdocs.org/sdr/DXTA200500752), Jun 2, 2005: TRANSDUCER. INOPERATIVE. DURING TAXI BOTH PEDALS ON RT SEAT BECAME SOFT, ANTI-SKID LIGHTS CAME ON. AFTER PUMPING THE PEDALS THE LIGHT WENT OUT, AND THE BRAKES FELT NORMAL. THIS HAPPENED - [SDR DXTA200500748](https://openairdocs.org/sdr/DXTA200500748), Jun 1, 2005: O-RING. LEAKING. LOST BRAKE PRESSURE ON TAXI. BRAKE FLUID LEAKING OUT OF RIGHT BRAKE ASSEMBLY. REMOVED AND REPLACED LEAKING O-RING ON BRAKE LINE FITTING. OPS AND LEAK CHECK GOOD - [SDR DXTA200300029](https://openairdocs.org/sdr/DXTA200300029), May 6, 2003: INDICATOR. MALFUNCTIONED. DURING TAKEOFF ROLL CAPTAIN'S ATTITUDE INDICATOR INDICATED 5 DEGREES NOSE DOWN WITH 3 DEGREES RIGHT BANK. REJECTED TAKEOFF. FOUND NR 1 VERTICAL GYRO DEFECTIVE. ## Other aircraft with N371QS - [Registered now](https://openairdocs.org/aircraft/N371QS): Embraer Executive EMB-505, S/N 50500279, built 2015 --- 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.