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2014 CESSNA CARAVAN GRAND 208B EX

Description:

2014 CESSNA CARAVAN GRAND 208B EX

Specification:

Aircraft Serial No.:  5151

Make/Model: 2014 CESSNA CARAVAN GRAND 208BEX

Registration number VN-B466

Date of Mfg:  2014

Date Entered Service:  2014

G1000 AVIONICS SYSTEM

03 BLADES HARTZELL PROPELLER HC-B3TN-3

Maintenance Program : CESCOM (CAMPS) system

Airframe:

  • Total Time: 1805.1 Hrs
  • Landings: 2398

Engine:

  • Engine: Pratt & Whitney
  • Model Number : PT6A 140 876HP
  • Total Time : 1805.1 Hrs
  • Cycles : 2367

Avionics/Radios:

Avionics/Radios

GDUs 1040A Pilot & Co-pilot Primary Flight Display

GDU 1040A Multifunction Display

GDC 74A Dual Air Data Computer (ADC)

GEA 71 Engine/Airframe Unit

GIA 63W Dual Integrated Avionics Unit (Includes Comm, Nav, GPS)

GRS 77 Dual Attitude and Heading Reference System (AHRS)

GMA 1347 Dual Audio System with Integrated Marker Beacon Receiver

GMC 710 Autopilot Mode Controller

GSA 80/81 Servo Actuators with GSM 86 Servo Mounts

GTX 33 Mode S Transponder

Garmin Relative Terrain/Obstacles

Garmin Flight Charts Capable

Garmin Safe Taxi Capable

KN-63 DME

Switch, Avionics Power (Two) (On-Off)

Avionics Cooling, (2) cowl deck fans and (3) display fans

PA System with Aft Cabin Speakers

Additional Equipment

Air Conditioning System

Starter/Generator 200 Amp

Standby Electric System 75 Amp

Dual GTX 33 Mode S Transponder

Dual Audio Panel

KRA 405B Radar Altimeter

FA2100 CVDR

GWX 68 4 – color Digital Weather Radar

KTA 870 Traffic Advisory System (Bendix-King)

TAWS-B Garmin

C 406-N 3 Frequency ELT

FAST system Engine Trend Monitoring

Extended Cord Rudder

Single Point Refueling System

Payload Extender Kit Installed

Gear Advisory System

Exterior:

White with Blue Stripes

Interior:

14-Place Commuter

Inspection Status:

Available On Request.

Disclaimer

The details, photographs and technical information provided are for the purpose of initial review only and will be subject to changes w.r.t. technical parameters, which may include but will not be limited to the Aircraft’s/Helicopter’s /Engine’s/Part’s condition, Airframe & component’s time, etc.
Verification of the Aircraft’s/Helicopter’s/Engine’s/Part’s actual condition shall be the sole responsibility of the Buyer/Lessee.

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