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The primary structures of the Corporate Jetliner are of composite construction
with aramid fibre (AFRP), glass fibre (GFRP) and carbon fibre (CFRP) reinforced
plastics.
CABIN
The spacious 24m long cabin has a floor area of nearly 80m². The cabin layout
can include executive suites, equipped offices and meeting rooms, a bedroom, a fam-
ily living room or sitting room area and bath or shower room according to the needs
of the individual client or corporate customer.
The cabin can also be designed to allow public transport flights, so that the air-
craft can be operated to allow private or commercial flights. In other words, the inte-
rior can be easily converted to provide seamless commercial passenger service.
The cabin environment gives an exceptionally quiet and comfortable flight.
The air conditioning system provides a constant fresh air flow at low velocity as the
air conditioning manifold is situated in the fuselage recess and maintains the cabin
pressure at 8.33lb/in².
The ACJ is fitted with airstairs to allow self sufficiency at airfields with limited
airport facilities.
FLIGHT DECK
The ACJ 17 hour flight deck has twice the volume of typical business jets and
easily accommodates the pilot and copilot. The aircraft is fitted with Thales/SFENA
fly-by-wire controls. The fly-by-wire system incorporates flight envelope protection,
reduces costs and pilot workload as well as improving the aircraft's performance. The
aircraft has CAT IIIB automatic landing capability.
Each pilot has a side-stick controller allowing single hand control. The fly-by-
wire system incorporates many safety features including a high level of redundancy,
use of dissimilar redundancy with different computers, different microprocessors, dif-
ferent vendors, division and separation of each computer, the segregation of power
supplies and the maximum segregation in signalling lines.
The Thales/VDO electronic flight and information system (EFIS) includes a set
of primary flight and navigation displays for each pilot. The primary flight display
provides speed, altitude and heading data. Two Thales/VDO electronic central air-
craft monitoring (ECAM) displays are mounted in the centre section between the pi-
lot's and co-pilot's instrument panels.
Rockwell Collins supplies the communications and navigations suite including:
ACARS (aircraft communications addressing and reporting system), ADF (automatic
direction finding), VHF omni-directional radio range navigation aid with data from
the distance measuring equipment (VOR/DME), multi-mode receivers (MMRs),
TCAS ll collision avoidance system and weather radar, as well as optional items such
as satellite communications and data-links.
The aircraft is offered with two IAE V2527M-A5 engines or two CFM Interna-
tional CFM 56-5B7 developing 111.9kN. The fuel tanks have a capacity of 6,260 US
gallons (23,860l) giving the aircraft a range of over 6,500km with eight passengers.
The aircraft is approved for 180 minutes ETOPS operations (extended range twin en-
gine operations).
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