# N605CS: 2006 Cessna 680, registration cancelled 2015-07-28

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 28, 2015
- Exported to: Dominican Republic
- Status when cancelled: Valid registration
- Airframe: [Cessna 680](https://openairdocs.org/model/cessna-680) (registry code 2076811)
- Engine: [Pratt & Whitney Canada PW306C](https://openairdocs.org/engine/pratt-whitney-canada-pw306c) (registry code 52169)
- Data sheets: [TCDS T00012WI](https://openairdocs.org/tcds/T00012WI), [TCDS E35NE](https://openairdocs.org/tcds/E35NE) (OpenAirDocs)
- Serial number: 680-0001
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: April 1, 2015
- Certificate issued: May 4, 2012
- Last registry action: April 15, 2015
- Mode S code: A7DA15
- Owner when cancelled: [Cessna Aircraft Co](https://openairdocs.org/faa-owner/CESSNA%20AIRCRAFT%20CO)
- Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- Owner type: Corporation
- Owner's area on the map: 37.6159° N, 97.4350° W: Placed by OpenAirDocs at the center of ZIP code 67215, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N605CS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=605CS
- Page: https://openairdocs.org/deregistered/N605CS-2015-07-28

From the FAA registry file of October 28, 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 680: https://openairdocs.org/model/cessna-680.md

## Service difficulty reports (5)

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

- [SDR Z5FA011911N605CS1](https://openairdocs.org/sdr/Z5FA011911N605CS1), Jan 19, 2011: ENGINE. VIBRATION. ON DESCENDING INTO PBI AT APPROX 37000' CREW REDUCED THE POWER TO APPROX 70 PERCENT N1 AND FELT A SLIGHT VIBRATION AND NOTICED THE CYAN MESSAGE ON THE EICAS "EN
- [SDR Z5FA9032010N605CS](https://openairdocs.org/sdr/Z5FA9032010N605CS), Sep 3, 2010: WINDSHIELD. BROKEN. AT FLIGHT LEVEL 360, AMBER CAS MESSAGE WINDSHIELD ANTI ICE FAIL ILLUMINATED. APPROX 2 MINUTES LATER PILOTS WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED, AND 
- [SDR Z5FA011909N605CS1](https://openairdocs.org/sdr/Z5FA011909N605CS1), Jan 19, 2009: CONTROL WHEEL. BINDS. AFTER A MODERATE CROSS-WIND TAKEOFF FROM MYEF WITH 20 PERCENT LEFT AILERON APPLIED, THE CREW WAS UNABLE TO RETURN THE CONTROL WHEEL BACK TO A NEUTRAL POSITION. 
- [SDR Z5FA02009119001](https://openairdocs.org/sdr/Z5FA02009119001), Jan 19, 2009: CONTROL COLUMN. UNKNOWN. AFTER A MODERATE CROSS-WIND TAKEOFF WITH 20 PERCENT LT AILERON APPLIED, THE CREW WAS UNABLE TO RETURN THE CONTROL WHEEL BACK TO A NEUTRAL POSITION. AFTER 2 TO 3
- [SDR 021407N605CS1](https://openairdocs.org/sdr/021407N605CS1), Feb 14, 2007: LANDING GEAR. MALFUNCTIONED. UPON APPROACH, AFTER SELECTING GEAR EXTEND, THE RT MAIN GEAR DOWN INDICATION FAILED TO ILLUMINATE AND THE GEAR UNLOCK LIGHT REMAINED ILLUMINATED. CREW EXECUTED 

## Other aircraft with N605CS

- [Registered now](https://openairdocs.org/aircraft/N605CS): Bombardier CL-600-2B16, S/N 5801, built 2009

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