# N687QS: 2001 Cessna 560XL, registration cancelled 2015-11-30 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: November 30, 2015 - Exported to: Canada - Status when cancelled: Registration pending - Airframe: [Cessna 560XL](https://openairdocs.org/model/cessna-560xl) (registry code 2076702) - Engine: [Pratt & Whitney Canada PW545 series](https://openairdocs.org/engine/pratt-whitney-canada-pw545-series) (registry code 52154) - Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE), [TCDS E00059EN](https://openairdocs.org/tcds/E00059EN) (OpenAirDocs) - Serial number: 560-5187 - Year built: 2001 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 30, 2001 - Last registry action: October 20, 2015 - Mode S code: A91EA7 - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Individual - Owner's area on the map: 39.7376° N, 75.6671° W: Placed by OpenAirDocs at the center of ZIP code 19808, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N687QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=687QS - Page: https://openairdocs.org/deregistered/N687QS-2015-11-30 From the FAA registry file of November 5, 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 560XL: https://openairdocs.org/model/cessna-560xl.md ## Service difficulty reports (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2014120105939](https://openairdocs.org/sdr/DXTA2014120105939), Nov 26, 2014: MASTER CYLINDER. FAILED. DURING TAXI ONTO RUNWAY WITH LT RUDDER DEFLECTION, HEARD & FELT A POP IN THE RUDDER PEDALS & THEN SMELLED A NOXIOUS ODOR. THE LT BRAKE PEDAL HAD NO EFFECT, HAD - [SDR CWQR20140905005](https://openairdocs.org/sdr/CWQR20140905005), Sep 3, 2014: HOUSING. BROKEN. INSTALLED REPAIRED SERVICEABLE ENG ON THE NR 2 POSITION ON ACFT. DURING THE ENG LEAK & RUN UP CHECKS WE DISCOVERED THAT THE T1 PROBE HOUSING THAT IS IN THE INLE - [SDR DXTA2013100905532](https://openairdocs.org/sdr/DXTA2013100905532), Oct 8, 2013: SEAL. FAILED. AFTER TAKEOFF, RED GEAR UNSAFE LIGHT REMAINED ON, CAUSING THE HYD LIGHT TO REMAIN ON AND THE STAB MISCOMPARE LIGHT TO COME ON. VISUAL INSPECTION OF NLG STRUT FO - [SDR DXTA2013101105534](https://openairdocs.org/sdr/DXTA2013101105534), Oct 8, 2013: WARNING LIGHT. ILLUMINATED. AFTER TAKEOFF, THE RED GEAR UNSAFE LIGHT REMAINED ON, CAUSING THE HYD LIGHT TO REMAIN ON AND THE STAB MISCOMPARE LIGHT THE COME ON. - [SDR DXTA2013032105328](https://openairdocs.org/sdr/DXTA2013032105328), Mar 20, 2013: PUMP. FAILED. DURING TAXI, ANTI-SKID INOPERATIVE ANNUCIATOR ILLUMINATED. RETURNED TO RAMP. WHILE TURNING TO PARK THE BRAKE FAILED AS THE BRAKE LOW PRESSURE LIGHT ILLUMINATED. - [SDR DXTA2012011704847](https://openairdocs.org/sdr/DXTA2012011704847), Jan 16, 2012: ACTUATOR. MALFUNCTIONED. AFTER GEAR WAS EXTENDED, THE RED UNLOCK LIGHT FLICKERED ON/OFF FOR ABOUT 5 MINUTES. 3 GREEN WERE CONTINUOUSLY ILLUMINATED. EVENTUALLY FLICKERING STOPPED. OPTED - [SDR DXTA2011111104782](https://openairdocs.org/sdr/DXTA2011111104782), Nov 10, 2011: WARNING LIGHT. INTERMITTENT. DURING GEAR EXTENSION A FLICKERING GEAR UNLOCK INDICATION WAS NOTICED. ALL 3 GREEN LIGHTS WERE ON. APPROPRIATE CHECKLIST WAS COMPLIED WITH. AFTER PROCEDURE THE - [SDR DXTA2009032703568](https://openairdocs.org/sdr/DXTA2009032703568), Mar 26, 2009: SWITCH. LOOSE. UPON APPLYING T/O POWER THE LT ENGINE TR HAD AN UNCOMMANDED DEPLOYMENT, THIS HAPPEN MULTIPLE TIMES. EACH TIME WE USED EMER STOW. DID NOT BEGIN TAKEOFF ROLL. TRO - [SDR DXTA200803140](https://openairdocs.org/sdr/DXTA200803140), Jun 23, 2008: CONTROL VALVE. MALFUNCTIONED. ENCOUNTERED SEVERE TURBULENCE AT FL350. GEAR HANDLE PLACED IN THE DOWN POSITION ON FINAL APPROACH AND NOTHING HAPPENED FOR 3-5 SECONDS TEHN THE GEAR EXTENDED NO - [SDR DXTA200702257](https://openairdocs.org/sdr/DXTA200702257), Jun 11, 2007: SERVO. INOPERATIVE. RT ENGINE WILL NOT MAKE TAKEOFF POWER 88.1 N1 WAS NEEDED AND IT WOULD ONLY GO TO 80 PERCENT. R&R BOV TORQUE MOTOR IAW PRATT & WHITNEY 545A MAINT. MANUAL 75-30-0 - [SDR DXTA200601673](https://openairdocs.org/sdr/DXTA200601673), Oct 20, 2006: ACTUATOR. FAILED. LANDING GEAR " UNLOCK" LIGHT WOULD NOT EXTINGUISH ON GEAR RETRACTION, GEAR SOUNDED LIKE IT STOWED. HOWEVER, LIGHT REMAINED ILLUMINATED. REMOVED AND REPLACED LT - [SDR CWQR200617](https://openairdocs.org/sdr/CWQR200617), Jul 31, 2006: CONTROL CABLE. FRAYED. DURING PHASE B INSPECTION, IAW OPERATOR REQUEST, INSPECTED THE AFT ELEVATOR TRIM CABLES. UPON INSPECTION WE FOUND 3 BROKEN WIRES. REMOVED CABLE AND PREFORMED LO - [SDR DXTA200501147](https://openairdocs.org/sdr/DXTA200501147), Dec 16, 2005: SEAL. LEAKING. WITH APU ON FOR 15 MIN, CAB IN FILLED WITH SMOKE. OIL SMELL TO IT. BLEED AIR ON, TEMPS NORMAL ON APU. CABIN SEEMED TO NOT BE COOLING EFFECTIVELY. - FOUND APU ST - [SDR DXTA200500845](https://openairdocs.org/sdr/DXTA200500845), Jul 17, 2005: APU. OVERSERVICED. AIRCRAFT APU RUNNING ON GROUND / CABIN FILLED UP WITH BLUE SMOKE, CUT APU BLEED AIR OFF, AND SMOKE SLOWED BUT DID NOT STOP, AIRCRAFT HAD BEEN SITTING IN HEAVY R - [SDR DXTA200500819](https://openairdocs.org/sdr/DXTA200500819), Jul 7, 2005: ODOR. DETECTED. UPON DESCENT THROUGH 14000 FT, MFD SCREEN WENT BLANK ABRUPTLY. STRONG ODOR OF BURNED PLASTIC FILLED COCKPIT, BUT NO SMOKE DETECTED. PERFORMED USER INITIATED SEL - [SDR 2003FA0001292](https://openairdocs.org/sdr/2003FA0001292), Dec 22, 2003: CUSHION. MISSING. NR 6 AND NR 8 CABIN SEATS WERE AT MAINTENANCE FACILITY FOR ROUTINE REFURBISHMENT. DURING DISASSEMBLY IT WAS FOUND THAT THE SEAT PAN CUSHIONS WERE MISSING. IT AP - [SDR DXTA200300141](https://openairdocs.org/sdr/DXTA200300141), Oct 17, 2003: PROXIMITY SWITCH. OUT OF ADJUST. RT T/R ARM LIGHT ILLUMINATED IN FLIGHT ACCOMPANIED BY A CONSTANT HYDRAULIC PRESSURE ANNUNCIATOR, FOLLOWED BY INTERMITTENT UNLOCK LIGHT OF LANDING GEAR CAUSING S - [SDR CWQ2002F00006](https://openairdocs.org/sdr/CWQ2002F00006), Aug 16, 2002: LENS. CRACKED. FOUND LT WING TIP LIGHT ASSEMBLY LENS CRACKED AROUND FORWARD AND AFT FLANGE. POSSIBLE CAUSE: OVER-TORQUE OF ATTACHING HARDWARE. REPLACED WING TIP LIGHT ASSEMBLY ## Other aircraft with N687QS - [Registered now](https://openairdocs.org/aircraft/N687QS): Textron 680A, S/N 680A0216, built 2019 --- 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.