# N613QS: 2005 Cessna 560XL, registration cancelled 2025-08-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 18, 2025
- 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: 560-5599
- Year built: 2005
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 8, 2005
- Last registry action: August 18, 2025
- Mode S code: A7FB52
- 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/N613QS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=613QS
- Page: https://openairdocs.org/deregistered/N613QS-2025-08-18

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 (26)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DXTA2024041911545](https://openairdocs.org/sdr/DXTA2024041911545), Apr 19, 2024: BRAKE SYS. MALFUNCTIONED. UPON TAXI OUT APPLYING LIGHT BRAKING, THE LEFT BRAKE MAKES A CHATTERING SOUND AND VIBRATES. GOING SLIGHTLY FASTER THAN NORMAL TAXI SPEED AND APPLYING HEAVIER BR
- [SDR DXTA2024012910748](https://openairdocs.org/sdr/DXTA2024012910748), Jan 28, 2024: SPRING. DEFECTIVE. LEFT MLG BRAKE: LEFT MLG GEAR BRAKE IS GRABBING AND CHATTERING AT LOW TAXI SPEEDS. INTERMITTENT. REPEAT WRITEUP. LEFT MLG BRAKE: LEFT MLG GEAR BRAKE IS GRABBING
- [SDR DXTA2024012310706](https://openairdocs.org/sdr/DXTA2024012310706), Jan 22, 2024: BRAKE ASSY. ABNORMAL. DURING TAXI AFTER LANDING THE LT BRAKE WAS GRABBING HARD ENOUGH TO LOCK UP THE TIRE. REMOVED AND REPLACED L/H BRAKE ASSY IAW CE560XLAMM 32·42·01, PERFORMED BRAK
- [SDR DXTA2023100296940](https://openairdocs.org/sdr/DXTA2023100296940), Oct 2, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO CLOSE OR OPEN DOOR. PROGRESSIVELY GETTING WORSE //SIGNOFF// LUBED ALL DOOR PINS AND ADJUSTED DOOR 
- [SDR DXTA2023090594510](https://openairdocs.org/sdr/DXTA2023090594510), Sep 3, 2023: CONTROL VALVE. DEFECTIVE. ON TAKE OFF COULD NOT RETRACT LANDING GEAR UNTIL THIRD ATTEMPT. CYCLED GEAR IN FLIGHT WITH NORMAL FUNCTION. REMOVED LANDING GEAR CONTROL PN: 9912550-1 SN: M8807
- [SDR DXTA2023030181520](https://openairdocs.org/sdr/DXTA2023030181520), Feb 28, 2023: UPLOCK SWITCH. OPEN. MLG: MLG- UPLOCK RED-GEAR UNLOCK LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. RAN QRH, CYCLED THE GEAR AND GEAR UNLOCK LIGHT WOULD NOT EXTINGUISH. JACKED U
- [SDR DXTA2023021380350](https://openairdocs.org/sdr/DXTA2023021380350), Feb 11, 2023: ACTUATOR. DEFECTIVE. NOSE GEAR: AFTER TAKEOFF, RETRACTION OF GEAR FOLLOWED BY FLAP RETRACT , THE HYD PRESS AND STAB MISCOMPARE ANNUNCIATORS ILLUMINATED AND THE UNLOCK LIGHT WITH THE
- [SDR DXTA2023011078270](https://openairdocs.org/sdr/DXTA2023011078270), Jan 10, 2023: COUNTERBALANCE. OUT OF ADJUST. WHEN OPENING DOOR WITH INTEGRATED DOOR HANDLE NOTICED EXCESSIVE FORCE NEEDED TO UNSEAT DOOR. ADJUSTED COUNTER-BALANCE SPRINGS AS NEEDED IAW CES60XL AMM CHAPTER 
- [SDR DXTA2022032158730](https://openairdocs.org/sdr/DXTA2022032158730), Mar 21, 2022: TIRE. DEFECTIVE. LEFT MLG TIRE: LEFT MAIN TIRE BLEW ON ROLL OUT AFTER LANDING RUNWAY 22 LEXINGTON. (AIRPORT HAS A/C OUT OF THE WAY NOW.)//CORRECTIVE ACTION// REMOVE AND REPLACE 
- [SDR DXTA2020090904076](https://openairdocs.org/sdr/DXTA2020090904076), Oct 9, 2020: TRIM SYSTEM. MALFUNCTIONED. CLIMBING THROUGH 27,500 FT, THE PITCH TRIM ANNUNCIATOR ILLUMINATED ON BOTH PFDS. THE AUTOMATION WAS DISENGAGED. WE LEVELED AT FL 280. WE ATTEMPTED TO MOVE THE T
- [SDR DXTA2020091094076](https://openairdocs.org/sdr/DXTA2020091094076), Sep 9, 2020: FLAP SYSTEM. FROZEN. CLIMBING THROUGH 27,500 FT, THE PITCH TRIM ANNUNCIATOR ILLUMINATED ON BOTH PFDS. THE AUTOMATION WAS DISENGAGED. WE LEVELED AT FL 280. WE ATTEMPTED TO MOVE THE T
- [SDR DXTA2020030903545](https://openairdocs.org/sdr/DXTA2020030903545), Mar 4, 2020: CONTROLLER. DEFECTIVE. CABIN PRESSURIZATION CONTROL NOT PRESSURIZING - PRESSURIZATION QUIT WORKING AS WE CLIMBED TO A HIGHER ALTITUDE. GOING THROUGH 31,500 FEET I FELT THAT THE CABIN 
- [SDR DXTA202003050354](https://openairdocs.org/sdr/DXTA202003050354), Mar 4, 2020: UNKNOWN. MALFUNCTIONED. CABIN PRESSURIZATION CONTROL NOT PRESSURIZING - PRESSURIZATION QUIT WORKING AS WE CLIMBED TO A HIGHER ALTITUDE. GOING THROUGH 31,500 FEET I FELT THAT THE CABIN 
- [SDR DXTA2019121303196](https://openairdocs.org/sdr/DXTA2019121303196), Dec 13, 2019: ACTUATOR. FAILED. RIGHT MLG LANDING GEAR UNLOCK LIGHT ILLUMINATED, AFTER GEAR SELECTED DOWN, THE RIGHT MLG LIGHTS DID NOT ILLUMINATE AND THE GEAR UNSAFE LIGHT REMAINED ON. AFTER 
- [SDR DXTA2019030402106](https://openairdocs.org/sdr/DXTA2019030402106), Mar 4, 2019: UNKNOWN. VIBRATION. AIRFRAME VIBRATION - IN CRUISE FLIGHT AT FL410 WE EXPERIENCED AN AIRFRAME VIBRATION. IT SOUNDED LIKE A PUMP RUNNING ON AND OFF AND SOUNDED LIKE A DEEPER BASS TY
- [SDR DXTA2018102901608](https://openairdocs.org/sdr/DXTA2018102901608), Oct 29, 2018: DISPLAY. OVERHEATED. ON ARRIVAL AT GXY, DESCENDING THRU 27000 THE RIGHT PFD WENT BLANK AND CAME BACK ON ABOUT 2 SECONDS LATER. THERE WAS A HOT ELECTRICAL ODOR BRIEFLY, NO SMOKE WAS 
- [SDR DXTA2016121506340](https://openairdocs.org/sdr/DXTA2016121506340), Dec 15, 2016: BRAKE SYS. MALFUNCTIONED. DURING LANDING ROLLOUT, ANTI-SKID ANNUNCIATOR ILLUMINATED. AFTER EXITING THE RUNWAY, LOW BREAK PRESSURE ILLUMINATED. PWR BRAKES CIRCUIT BREAKER TRIPPED. RESET T
- [SDR DXTA2016010806158](https://openairdocs.org/sdr/DXTA2016010806158), Jan 7, 2016: LIGHT. INOPERATIVE. BURNING SMELL COMING FROM INSIDE PAX DOOR. STRONG ENOUGH TO BE SMELLED IN THE COCKPIT. SUSPECT BURNING SMELL IN PASSENGER DOOR WAS LOWER AFT STEP LIGHT HAVING B
- [SDR DXTA2016010406151](https://openairdocs.org/sdr/DXTA2016010406151), Jan 3, 2016: PROBE. FAULTY. DURING CLIMB AROUND 8,000 FT, THE MASTER WARNING LIGHT ILLUMINATED WITH NO INDICATION WHY. IT WAS RESET & IT ILLUMINATED AGAIN WITH A BATTERY OVER TEMP ABOVE 16
- [SDR DXTR2015100101](https://openairdocs.org/sdr/DXTR2015100101), Oct 1, 2015: HINGE FITTING. CORRODED. AFT HINGE FITTING FOR CABIN ENTRY DOOR, FUSELAGE SIDE, IS CORRODED. R & R AFT HINGE IAW SRM 51-40-03.
- [SDR DXTA2012010304835](https://openairdocs.org/sdr/DXTA2012010304835), Dec 30, 2011: CONTROL CABLE. OUT OF ADJUST. AFTER DEPARTURE AND DURING CLIMBOUT, NOTICED SIGNIFICANT RT AILERON HAD TO BE APPLIED TO KEEP PLANE LEVEL. ACFT ACCELERATED TO 200 KTS AND MORE RT AILERON CONTR
- [SDR DXTA2009111103855](https://openairdocs.org/sdr/DXTA2009111103855), Nov 10, 2009: ENGINE. POWER LOSS. AT CLIMB OUT RT LOW OIL PRESSURE ANNUNCIATOR ILLUMINATED, REDUCED POWER ON RIGHT ENGINE, PERFORMED CHECKLIST AND SHUT DOWN RT ENGINE. MOTORED ENGINE. OIL PRESS 
- [SDR DXTA200803000](https://openairdocs.org/sdr/DXTA200803000), Apr 15, 2008: UNKNOWN. UNKNOWN. GEAR RETRACTED DURING LANDING ROLLOUT. MALFUNCTION UNDER INVESTIGATION.
- [SDR DXTA200802842](https://openairdocs.org/sdr/DXTA200802842), Feb 5, 2008: CONTROL UNIT. INOPERATIVE. AT HIGH POWER SETTING, LT ENGINE FIRE WARNING LIGHT FLICKERED ON AND OFF (VERY DIM) NEVER CAME ON FULL BRIGHT. FOUND FIRE DETECTOR CONTROL UNIT BAD. INSTALLED N
- [SDR DXTA200802806](https://openairdocs.org/sdr/DXTA200802806), Jan 28, 2008: FIRE LOOP. OUT OF POSITION. AT 34.0 FT IB TO MSP LT ENGINE, ENGINE FIRE LIGHT BLINKED ON AND OFF ABOUT 10 TIMES A MIN FOR 10 MIN INSPECTED LT ENGINE FIRE LOOP CONNECTIONS. INSPECTED FIRE L
- [SDR DXTA200802739](https://openairdocs.org/sdr/DXTA200802739), Jan 2, 2008: BRAKE ASSY. FAILED. WHILE TAXIING, WE LOST OUR BRAKES AND USED EMERGENCY BRAKES TO STOP. FOUND PWR BRAKE CB PULLED. BLED BRAKES COMPLETED OPERATIONAL CHECK OF ANTI-SKID SYSTEM AND 

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB NYC08LA162](https://openairdocs.org/ntsb/NYC08LA162), Apr 15, 2008: Cessna 560XL (N613QS), White Plains, NY, substantial damage. Probable cause: An uncommanded landing gear retraction after touchdown for undetermined reasons.

## 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.

- [Accident 20080415837749A](https://openairdocs.org/incident/20080415837749A), Apr 15, 2008: Cessna 560XL (N613QS), White Plains, NY, Substantial damage. (-23) After a normal approach and touchdown to runway 34, [privacy data omitted] (co-pilot) extended the speed brakes and [privacy data omitted]…

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