Citation Bravo

Primus 1000 Integrated Avionics System
Primus 660 Weather Radar
Honeywell Mark Vii Enhanced Ground Proximity Warning System (EGPWS)
Dual Garmin GTX 3000 (Mode S)
TCAS II With Software Change 7.1
Universal UNS-1L Flight Management System
Garmin GTN625Xi
Avidyne EX 500 Multi-Function Display
Flight Data Recorder
Cockpit Voice Recorder
Artex C406-2 Three Frequency ELT With Navigation Interface
Safe Flight N1 Computer
Pulselight System 2401 With TCAS II Interface
Ground Dispatch Power Switch
Cockpit Speaker Mute Switch
500W/115VAC Inverter located outside pressure vessel

Executive  Passenger Configuration with Leather Seating.

Overall White

EQUIPMENT OPTIONS:

Locking Fuel Caps, Ski Tube, Tail Flood Lights.

Optional Equipment at Purchase:

Permanent Data Transfer Unit – Universal
Mark VII Enhanced Ground Proximity Warning System (EGPWS) – Honeywell KHF – 950 Provisions Only – Honeywell
Cockpit Speaker Mute Switch UNS-1L (Exchange) – Universal
JAA Flight Data Recorder (Provisions Only) – Honeywell and Teledyne Controls
C406-2 three frequency ELT with Navigation Interface (Exchange) – Artex N1 Computer – Safe Flight
Panel Layout Bravo 550-MSPEC-1-02 TCAS II With Software Change 7
Pulselight system 2401 with TCAS II Interface
Provisions only for Garmin GPS-400, coupled and switched with #1 FMS GPS-400 to have primary means Oceanic/Remote Operations capability.
Locate TCAS processor and JAA FDR provisions (with ski tube installed) in the tailcone.
Mode S Diversity Transponders with enhanced surveillance in lieu of optional transponders installed with TCAS II
Light – Tail Flood
Refrigerant Type Supplemental Cooling Locking Fuel Caps (Exchange)
Install Encode ski tube.
500W/115VAC Inverter located outside the pressure vessel Interior/Exterior Aircraft Specification Revision Basic Ground Dispatch Power Switch

MODIFICATIONS:

CAS 67B TCAS II System (Change 7.1) Avidyne EX 500 Multi-Function Display