praetor 600 DETAILS

AIRCRAFT LISTING DETAILS:

Engines & Airframe

Total Hours:              TBD - 4th Quarter delivery

Total Landings:        TBD - 4th quarter delivery

Engines:  HONEYWELL, hTF7500e 

avionics

Specifications are provided for informational purposes only and do not constitute representations or warranties. These specifications are subject to buyer's independent verification upon inspection. The aircraft is subject to prior sale, lease and/or removal from the market without prior notice.

ELT / NAV

sINGLE adf

e2vs - eMBRAER eNHANCED VISION SYSTEM

SINGLE INERTIAL REFERENCE SYSTEM (irs)

COCKPIT DISPLAY OF TRAFFIC INFORMATION (CDTI)

THIRD VHF

DUAL HF PLUS SELCAL

ACARS DATALINK

ACARS OVER IRIDIUM

Two Honeywell HTF7500E turbofan  engines are pylon mounted on each side of the rear fuselage.  the engine is a twin-spool, medium bypass ratio turbofan.  thrust is generaged by a single stage, wide chord, damper less fan and driven by an uncooled and shrouded three stage low-pressure turbine.  The compressor has four axial blisks with two-stage high pressure turbine with cooled blades.  the compuster is an annular, effusion-cooled through-flow chamber.  

apu:  honeywell

A FULLY-AUTOMATIC HONEYWELL AUXILIARY POWER UNIT (apu) IS INSTALLED IN THE TAIL CONE WITH A CONTANT-SPEED GAS TURBINE ENGINE.  AN ELECTRONIC CONTROL UNIT STARTS THE APU AND COORDINATES ACCELERATION AND OPERATION.  THE APU IS A SOURCE OF SHAFT POWER FOR THE AIRCRAFT'S ELECTRICAL GENERATION SYSTEM, PNEUMATIC POWER FOR THE ENVIRONMENTAL CONTROL SYSTEM (AIR CONDITIONING), AND MAIN ENGINE STARTING SYSTEM ON THE GROUND OR IN FLIGHT.