# N692QS: 2000 Cessna 560XL, registration cancelled 2012-10-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: October 17, 2012 - Exported to: Canada - Status when cancelled: Valid registration - 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: 560-5092 - Year built: 2000 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 17, 2000 - Last registry action: October 17, 2012 - Mode S code: A93393 - Owner when cancelled: [Copter Lease LLC Trustee](https://openairdocs.org/faa-owner/COPTER%20LEASE%20LLC%20TRUSTEE) - Location: [Albuquerque, NM](https://openairdocs.org/faa-place/NM/Albuquerque) - Owner type: Corporation - Owner's area on the map: 35.1517° N, 106.5749° W: Placed by OpenAirDocs at the center of ZIP code 87109, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N692QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=692QS - Page: https://openairdocs.org/deregistered/N692QS-2012-10-17 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 560XL: https://openairdocs.org/model/cessna-560xl.md ## Service difficulty reports (14) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR CWQR20120613041](https://openairdocs.org/sdr/CWQR20120613041), Jun 13, 2012: BRACKET. CRACKED. DURING SCHEDULED MX, FOUND RUDDER/ELEVATOR AUTO-PILOT SERVO CABLE BRACKET CRACKED FROM 1 END TO PASS THE FIRST ATTACH FASTENER. - [SDR CWQR20110424001](https://openairdocs.org/sdr/CWQR20110424001), Apr 27, 2011: ANGLE. CRACKED. THE CRACKED APU CONTAINMENT BOX ANGLES WERE FOUND DURING APU REPLACEMENT. BOTH ANGLES WERE FOUND CRACKED PAST THE LAST RIVET IN THE BEND RADIUS. - [SDR DXTA2010032504052](https://openairdocs.org/sdr/DXTA2010032504052), Mar 24, 2010: BRAKE ASSY. MALFUNCTIONED. ON TAKEOFF FELT A LARGE YAW TO THE RT, RT BRAKE SEEMED TO HAVE GRABBED. TAXIED ACFT FOR 10 MINUTES AND PERFORMED SEVERAL COMPLETE STOPS, RT AND LT TURNS. NO BRA - [SDR DXTA2009121803900](https://openairdocs.org/sdr/DXTA2009121803900), Dec 17, 2009: INDICATOR. OUT OF TOLERANCE. PITCH TRIM INDICATOR OUT OF CALIBERATION . ACFT FEELS TAIL HEAVY DURING TAKEOFF WITH TRIM INDICATOR IN TAKE OFF RANGE. ADJUSTED ELEVATOR TRIM TRAVELS AND INDICA - [SDR DXTA2008122603442](https://openairdocs.org/sdr/DXTA2008122603442), Dec 26, 2008: SWITCH. FAULTY. CABIN DOOR LIGHT CAME ON AFTER TAKEOFF. REMOVED AND REPLACED CABIN DOOR SWITCH. OPS CHECK GOOD IAW MM CH 52-00-00. - [SDR DXTA2008122903442](https://openairdocs.org/sdr/DXTA2008122903442), Dec 26, 2008: WARNING LIGHT. ILLUMINATED. CABIN DOOR LIGHT CAME ON AFTER TAKE OFF. - [SDR DXTA2008120603390](https://openairdocs.org/sdr/DXTA2008120603390), Dec 6, 2008: TRIM SYSTEM. STUCK. THE ELEVATOR TRIM JAMMED AFTER TAKE OFF. RAN ELEVATOR TRIM BY HAND THROUGH COMPLETE TRAVEL NUMEROUS TIMES. TRIM OPERATES SMOOTHLY. PERFORMED TRAVEL CHECKS OF EL - [SDR DXTA2008120803390](https://openairdocs.org/sdr/DXTA2008120803390), Dec 6, 2008: TRIM SYSTEM. STUCK. THE ELEVATOR TRIM JAMMED AFTER TAKE OFF. - [SDR CWQR2006011](https://openairdocs.org/sdr/CWQR2006011), Jun 26, 2006: CONTROL CABLE. FRAYED. DURING A PHASE 1-4 INSPECTION THE ELEVATOR TRIM CABLE ASSEMBLY WAS FOUND TO BE FRAYED WHERE IT PASSES THROUGH THE HORIZONTAL STABILIZER. THE CABLE APPEARS TO HA - [SDR DXTA200501103](https://openairdocs.org/sdr/DXTA200501103), Nov 23, 2005: PCB. MALFUNCTIONED. AFTER TAKEOFF GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH, ALSO HYD PRESS LIGHT STAYED ON. SHORTLY AFTER STAB MIS COMP LIGHT ALSO CAME ON. GEAR AND FLAPS EXTENDED NO - [SDR DXTA200501081](https://openairdocs.org/sdr/DXTA200501081), Nov 12, 2005: COALESCER BAG. DIRTY. AFTER TAKEOFF A STRONG UNDESCRIBABLE ODOR IN COCKPIT, ODOR WAS NOT PRESENT DURING PREFLIGHT WITH APU RUNNING & BLEED AIR ON (APU WAS ON FOR 30 MIN) DID NOT ODOR - [SDR DXTA200500808](https://openairdocs.org/sdr/DXTA200500808), Jun 26, 2005: BRAKE ASSY. LEAKING. LOW BRAKE PRESSURE AND ANTI-SKID INOP LIGHTS CAME ON JUST AFTER TAXI OFF RUNWAY THE BRAKE FLUID IS COMING OUT OF THE OVERFLOW NEAR THE NOSE WHEEL. WOULD NOT CAN - [SDR DXTA200300185](https://openairdocs.org/sdr/DXTA200300185), Nov 23, 2003: CONTROL CABLE. CHAFED. PERFORMED AILERON WING CABLE INSPECTION PER CESSNA ASL560XL-27-12, FOUND CABLES CHAFED/BROKEN BEYOND MANUFACTURER'S LIMITS. REMOVED AND REPLACED LEFT AND RIGHT - [SDR DXTA200300129](https://openairdocs.org/sdr/DXTA200300129), Sep 27, 2003: UPLOCK SWITCH. MALFUNCTIONED. AFTER TAKE-OFF FROM HYA NOSE GEAR WOULD NOT STAY UP AND LOCKED AFTER RETRACTION, DIVERTED INTO SWF. JACKED AIRCRAFT AND PERFORMED GEAR SWINGS, UNABLE TO DUPLICA ## Other aircraft with N692QS - [Registered now](https://openairdocs.org/aircraft/N692QS): Textron 680A, S/N 680A0225, 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.