N605CS

Cancelled 2015

Deregistered aircraft · 2006 Cessna 680 · Pratt & Whitney Canada PW306C

Cancelled
July 28, 2015
Exported to
Dominican Republic
Status when cancelled
Valid registration
Serial number
680-0001
Year built
2006
Type
Fixed wing multi engine
Engine
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
Location
Wichita, KS
Owner type
Corporation

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.

Service difficulty reports · 5

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

SDR Z5FA011911N605CS1Engine · vibrationON 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 "ENGINE SHUTDOWN - L", INSTANTLY CREW OBSERVED A RELIGHT AND IT RAN PERFECTLY AFTER THAT. THE FLIGHTJan 19, 2011 · N605CS · Cessna 680CE · Engine (Turbine/Turboprop)SDR Z5FA9032010N605CSWindshield · brokenAT FLIGHT LEVEL 360, AMBER CAS MESSAGE WINDSHIELD ANTI ICE FAIL ILLUMINATED. APPROX 2 MINUTES LATER PILOTS WINDSHIELD SHATTERED. AN EMERGENCY WAS DECLARED, AND THE ACFT DIVERTED. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. THE PILOTS WINDSHIELD WAS CHANGED AND THESep 3, 2010 · N605CS · Cessna 680SOV · Flight Compartment WindowsSDR Z5FA011909N605CS1Control Wheel · bindsAFTER 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. AFTER 2 TO 3 FORCEFUL CLOCKWISE MOVEMENT ATTEMPTS, THE CONTROL WHEEL BECAME FREE. WHEN THE AIRCRAFJan 19, 2009 · N605CS · Cessna 680SOV · Aileron Control SystemSDR Z5FA02009119001Control Column · unknownAFTER 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 FORCEFUL CLOCKWISE MOVEMENT ATTEMPTS, THE CONTROL WHEEL BECAME FREE. WHEN THE ACFT WAS AT 5000 FT Jan 19, 2009 · N605CS · Cessna 680SOV · Aileron Control SystemSDR 021407N605CS1Landing Gear · malfunctionedUPON APPROACH, AFTER SELECTING GEAR EXTEND, THE RT MAIN GEAR DOWN INDICATION FAILED TO ILLUMINATE AND THE GEAR UNLOCK LIGHT REMAINED ILLUMINATED. CREW EXECUTED A GO AROUND AND FOLLOWED AFM GEAR EXTEND EMERGENCY PROCEDURES. THE MANUAL MAIN GEAR RELEASE WAS PULLFeb 14, 2007 · N605CS · Cessna 680CE · Landing Gear Retraction/Extension System

Other aircraft with N605CS · 1

The FAA can assign a mark to another aircraft once a registration is cancelled. N605CS is registered now to the first aircraft listed.