# N672QS: 2006 Cessna 560XL, registration cancelled 2026-02-18 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 18, 2026 - Status when cancelled: Sale reported - Airframe: [Cessna 560XL](https://openairdocs.org/model/cessna-560xl) (registry code 2076702) - Engine: [Pratt & Whitney Canada PW545B](https://openairdocs.org/engine/pratt-whitney-canada-pw545b) (registry code 52186) - Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE), [TCDS E00059EN](https://openairdocs.org/tcds/E00059EN) (OpenAirDocs) - Serial number: 560-5663 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 12, 2006 - Last registry action: February 18, 2026 - Mode S code: A8E495 - Location: [Bangor, ME](https://openairdocs.org/faa-place/ME/Bangor) - Owner type: Individual - Owner's area on the map: 44.8485° N, 68.8504° W: Placed by OpenAirDocs at the center of ZIP code 04401, within about 6 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N672QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=672QS - Page: https://openairdocs.org/deregistered/N672QS-2026-02-18 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 (32) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2025090404803](https://openairdocs.org/sdr/DXTA2025090404803), Sep 2, 2025: BATTERY. DISCHARGED. EMERGENCY LIGHTING ABOVE MAIN DOOR AND DROP AISLE LIGHTING FORWARD IS OFF WITH MAIN BATTERY CONNECTED AND EMER LTS SWITCH ON CORRECTIVE ACTION: TROUBLE SHOT TO - [SDR DXTA2025080804511](https://openairdocs.org/sdr/DXTA2025080804511), Aug 7, 2025: BELLCRANK. MISINSTALLED. CLIMBING THROUGH 10,000FT, RECEIVED AN AMBER CABIN DOOR ANNUNCIATOR LIGHT. NO PRESSURIZATION CHANGES NOTED, LEVELED OFF AT 12,000 AND RETURNED BACK TO KBTL. TRO - [SDR DXTA2025070804140](https://openairdocs.org/sdr/DXTA2025070804140), Jul 5, 2025: PRESSURE SWITCH. FAULTED. COMING THROUGH 16,000 FEET ON OUR ARRIVAL THE EAGLE WE HAD WHAT APPEARED TO BE AN RAPID DECOMPRESSION. WE HAD A LOUD BANG, FOLLOWED BY CABIN ALTITUDE LIGHT. PAS - [SDR DXTA2025063004068](https://openairdocs.org/sdr/DXTA2025063004068), Jun 27, 2025: NONE. NO DISCREPANCY. JUST BEFORE ROTATION SPEED EXPERIENCED BIRD STRIKE. ON POSTFLIGHT NOTED SMALL BIRD REMAINS AT THE NOSE LANDING GEAR LEFT DOOR FORWARD HINGE. NO OBVIOUS DAMAGE B - [SDR DXTA2025052703608](https://openairdocs.org/sdr/DXTA2025052703608), May 22, 2025: BATTERY PACK. INOPERATIVE. WITH BATTERY POWER ON, ALL EMERGENCY LIGHTS ARE OPERATING NORMAL. WHEN TURNING THE BATTERY SWITCH TO OFF, THE EXIT SIGN UNDER THE LAV IS INOP. THE AIRPLANE HAD - [SDR DXTA2025050303344](https://openairdocs.org/sdr/DXTA2025050303344), May 3, 2025: LIGHT. INOPERATIVE. EMERG EXIT SIGN OVER SEAT 7 DOES NOT ILLUMINATE W/ EMERG LIGHT SWITCH ON CORRECTIVE ACTION: REMOVED LIGHT PN:9919040-6 SN:118004048 IAW 560XL MM 33-20-04 INSTAL - [SDR DXTA2025032602798](https://openairdocs.org/sdr/DXTA2025032602798), Mar 23, 2025: BUSS BAR. CORRODED. WHEN GEAR WAS SELCTED DOWN THE ANTI-SKID ANNUNCIATOR ILLUMINATED AND ABOUT 60 TO 90 SECONDS LATER POWER BRAKE CIRCUIT BREAKER TRIPPED. RESET THE CIRCUIT BREAKER - [SDR DXTA2025020302180](https://openairdocs.org/sdr/DXTA2025020302180), Jan 31, 2025: BRAKE ASSY. FAULTED. LEFT MLG BRAKE: REPEAT WRITEUP. WHEN APPLYING BRAKE PRESSURE AT ANY TAXI SPEED, THE AIRCRAFT PULLS TO THE LEFT. - [SDR DXTA20240110775](https://openairdocs.org/sdr/DXTA20240110775), Dec 30, 2024: PRESSURE SWITCH. DEFECTIVE. AT 13,000¿ ON APPROACH TO HIGH ALTITUDE A/P (KTEX), HEARD LOUD POP, FOLLOWED BY RUSHING AIR AND CAB ALT RED ANNUNCIATOR (HOWEVER CABIN ALTITUDE SHOWED 9000 FEE - [SDR DXTA2024121701558](https://openairdocs.org/sdr/DXTA2024121701558), Dec 16, 2024: G SWITCH. MALFUNCTIONED. DURING PREFLIGHT CHECKS, FOUND THE AFT EMERGENCY LIGHTS AND THE EXTERIOR ENERGENCY LIGHTS TO BE ILLUMINATED WITH THE EMERGENCY LIGHTS SWITCH ARMED AND THE SEATB - [SDR DXTA2024092300610](https://openairdocs.org/sdr/DXTA2024092300610), Sep 20, 2024: POWERPACK. FAILED. DURING TAXI TO RAMP, NORMAL AC BRAKES FAILED AND AC STRUCK THE BUILDING. REMOVED ANTI-SKID MOTOR AND REPLACED WITH A OVERHAULED UNIT IAW CESSNA 560XL/XLS MM 32- - [SDR DXTA2023060587770](https://openairdocs.org/sdr/DXTA2023060587770), Jun 5, 2023: BATTERY. DEFECTIVE. FLOOR EMERGENCY LIGHTING, FROM SEAT 3 TO SEAT 5 IS INOP. HOWEVER, THE EMERGENCY FLOOR LIGHTING FOR THE MAIN CABIN DOOR (SAME SIDE) WORKS. REMOVED AND REPLACED F - [SDR DXTA2023022080770](https://openairdocs.org/sdr/DXTA2023022080770), Feb 19, 2023: NONE. NONE. MAIN DOOR: THE MAIN DOOR WILL NOT CLOSE FROM THE INSIDE. APU BLEED AIR IS OFF. WE CAN NOT MOVE THE INTERIOR HANDLE PAST THE ONE O'CLOCK POSITION. /// SIGN OFF / - [SDR DXTA2022072866880](https://openairdocs.org/sdr/DXTA2022072866880), Jul 27, 2022: BATTERY. DEFECTIVE. EMERG EXIT SIGN/LIGHT: THE FORWARD INTERIOR EMERGENCY LIGHTS DO NOT WORK WHEN SLECTED ON WITH THE EMERGENCY LIGHT SWITCH AND THE MAIN BATTERY OFF AS PER THE MEL - [SDR DXTA2021123154500](https://openairdocs.org/sdr/DXTA2021123154500), Dec 30, 2021: APU. LEAKING. APU BLEED AIR: THE APU WAS RUNNING WITH THE GENERATOR ON. AN OILY SMOKE AND SMELL WAS COMING OUT OF THE AIR VENTS. WHEN THE APU BLEED AIR WAS SELECTED ON THE AP - [SDR JGVR20210611001](https://openairdocs.org/sdr/JGVR20210611001), Jun 11, 2021: STRAKE. CORRODED. REPAIRED CORROSION AT 3 UPPER SURFACE LOCATIONS (AT UPPER AND LOWER CARBON CAPS) ON RH STRAKE (TAILCONE RH LOWER FIN) BY INSTALLING REPAIR DOUBLERS IAW NETJETS - [SDR DXTA2018051700968](https://openairdocs.org/sdr/DXTA2018051700968), May 17, 2018: CONTROL VALVE. FAULTY. ALL LANDING GEAR EXTENSION DELAY, GEAR WAS SELECTED DOWN AT 200 KTS. FOR AT LEAST 30 SECONDS THERE WAS ONLY THE RED GEAR UNSAFE LIGHT ILLUMINATED, NO HYDRAULIC - [SDR DXTA2018010400435](https://openairdocs.org/sdr/DXTA2018010400435), Jan 3, 2018: BRAKE SYS. CONTAMINATED. AFTER LANDING, AND DURING TAXI RECEIVED A LOW BRAKE PRESSURE AND ANTI-SKID INOPERATIVE ANNUNCIATORS WITH A MASTER CAUTION. ABLE TO STOP WITH NORMAL BRAKES, BUT - [SDR DXTA201712200635](https://openairdocs.org/sdr/DXTA201712200635), Dec 20, 2017: WARNING LIGHT. ILLUMINATED. WHEN LANDING GEAR WAS BROUGHT DOWN FOR LANDING, LOW BRAKE PRESSURE AND ANTISKD LIGHTS NEVER EXTINGUISHED. BRINGING THE MASTER CAUTION ON FLASHING. DEPARTED THE - [SDR EBVR20170406001](https://openairdocs.org/sdr/EBVR20170406001), Apr 6, 2017: RIB. CORRODED. CORROSION FOUND ON LOWER RIB OF THE RUDDER AT THE BONDING POINT. REPAIRED EXISTING LOWER RUDDER TORQUE TUBE RIB PER AQRD ERO-891028 REV IR. ATTACHED NEW REPAIR - [SDR DXTA2016113006333](https://openairdocs.org/sdr/DXTA2016113006333), Nov 30, 2016: ENGINE. FAILED. AFTER TAKEOFF, A BANG WAS HEARD AND THE LEFT HAND ENGINE ITT SHOWED 800 DEGREES. THERE WAS VIBRATION FELT FOR ABOUT 30 SECONDS. AT THAT POINT THE LEFT OIL PRESS - [SDR DXTR2013091801](https://openairdocs.org/sdr/DXTR2013091801), Sep 18, 2013: WINDSHIELD. CRACKED. LEFT WINDSHIELD CRACKED DURING FLIGHT, CLIMBING THROUGH FL220. R & R WINDSHIELD IAW MM 56-12-00. - [SDR DXTA2013091705507](https://openairdocs.org/sdr/DXTA2013091705507), Sep 16, 2013: WINDOW. DAMAGED. SIDE WINDSHIELD CRACKED DURING FLIGHT, CLIMBING THROUGH FL220. REMOVED AND REPLACED THE LEFT COCKPIT WINDSHIELD IAW MM 56-12-00. PRESSURIZIATION, LEAK CHECK AND - [SDR DXTA2013010705230](https://openairdocs.org/sdr/DXTA2013010705230), Jan 4, 2013: RING. DAMAGED. ON TAKEOFF, RETRACTED GEAR AND RECEIVED A RED GEAR UNSAFE LIGHT AND A FLASHING HYD LIGHT. THERE WAS A RUMBLE FROM THE NOSE SECTION. THE NOSE STRUT LOOKS TO BE L - [SDR DXTA2013010205224](https://openairdocs.org/sdr/DXTA2013010205224), Dec 31, 2012: CONTROL VALVE. FAILED. AFTER TAKEOFF, GEAR RAISED AND RED UNLOCK LIGHT STAYED ILLUMINATED AND WOULD NOT EXTINGUISH. R & R LANDING GEAR CONTROL VALVE IAW MM 32-30-02. LEAK AND OPS CHEC - [SDR CWQR2012040326](https://openairdocs.org/sdr/CWQR2012040326), Apr 3, 2012: HUB. CRACKED. DURING A SCHEDULED INSPECTION OF THE CABIN DOOR, FOUND THE FORWARD CABIN DOOR COUNTERBALANCE SPRING REEL HUB TO BE CRACKED WHERE THE ROLL PIN GOES THROUGH THE H - [SDR CWQR2012040225](https://openairdocs.org/sdr/CWQR2012040225), Apr 2, 2012: SUPPORT CHANNEL. CRACKED. DURING A SCHEDULED INSPECTION OF THE TAIL BAGGAGE DOOR HINGE, FOUND THE LOWER FORWARD HINGE SUPPORT CHANNELS CRACKED, SB560XL-52-13 HAD BEEN COMPLIED WITH AT TH - [SDR CWQR2012040224](https://openairdocs.org/sdr/CWQR2012040224), Apr 2, 2012: CONTROL CABLE. FRAYED. DURING A SCHEDULED INSPECTION THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTIC - [SDR DXTA200803017](https://openairdocs.org/sdr/DXTA200803017), Apr 24, 2008: OIL SYSTEM. LOW PRESSURE. ABORTED T/O, WITH MASTER WARNING LIGHT AND L OIL PRESSURE LOW ILLUMINATED. PRIOR TO T/O ROLL OIL PRESSURE WAS IN THE GREEN. NO OIL SHOWING IN SIGHT GAGE ON POST - [SDR DXTA200702264](https://openairdocs.org/sdr/DXTA200702264), Jun 14, 2007: TIRE. FAILED. RT MAIN TIRE BLEW UP UPON LANDING. [07-09-07] INSPECTED RIGHT MLG DOOR, LINKAGES, WIRING, STRUCTURE, AND HYDRAULIC LINES FOR DAMAGE. NO DAMAGE NOTED. REMOVED AN - [SDR DXTA200702274](https://openairdocs.org/sdr/DXTA200702274), Jun 8, 2007: CIRCUIT BOARD. INOPERATIVE. HYDRAULIC PUMP WOULD NOT BRING THE LANDING GEAR UP, WITH GEAR HANDLE UP, GEAR STAYED DOWN AND LOCKED. REMOVED PCB P/N 6618723-5 S/N 0267. INSTALLED NEW PCB 6618 - [SDR DXTA200702182](https://openairdocs.org/sdr/DXTA200702182), May 9, 2007: SQUAT SWITCH. INOPERATIVE. AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT HANDLE LOCKED IN DOWN POSITION. REMOVED AND REPLACED LEFT SQUAT SWITCH WITH NEW. OPS CHECK GOOD. REF CESSNA 560XL M ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20240804008589I](https://openairdocs.org/incident/20240804008589I), Aug 4, 2024: Cessna 560XL (N672QS), Bridgeport, CT, Minor damage. Bird strike on takeoff resulting in broken plexiglass housing for left landing and left recognition lights. Left landing light and left recognition light… --- 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.