2002 AIRBUS ACJ320 E&V ID A AIRBUS ACJ320 (A320) ASKING PRICE: US$ YOM 2002 MSN ISSUE Page 1

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1 AIRBUS ACJ320 (A320) ASKING PRICE: US$ YOM 2002 MSN 1868 Airbus is a leading aircraft manufacturer, which captures approximately half of all orders for airliners with more than 100 seats. Airbus is a division of EADS (European Aeronautic Defence and Space Company) a global leader in aerospace, defense and related services, employing a workforce of about 118,000. The Group includes Airbus, manufacturer of commercial aircraft, Airbus Military covering tanker, transport and mission aircraft, as well as Eurocopter and EADS Astrium, its space division. Airbus corporate jet family is based on the A320 airliner and is comprised of the ACJ318, ACJ319 and ACJ320. The A320 program was launched in March 1982, first flight occurred on February , with certification awarded on February The Airbus A320 is a single-aisle, twin-engine, narrow-body, short- to medium-range aircraft family with a seating capacity for passengers. Based on the A320 airliner, but featuring a customized cabin, extra fuel-tanks for intercontinental range, and a numerous other features, the Airbus ACJ320 has the largest cabin in its class of business jets. Airbus ACJ320 cabins are customized to suit individual owners tastes. With more than 1,030 sq. ft. of floor space, the ACJ320 s cabin is able to carry larger groups than most traditional business jets. The ACJ320 is powered by 2 CFMI CFM56-5B turbofan engines each producing 27,000 pounds of thrust at ISA +29 degrees C. The aircraft is also available with IAEV2527M-5A engines. The overhaul interval is 15,900 hours. The A320 family pioneered the Airbus flight deck, which introduced full fly-by-wire controls, an efficient and uncluttered instrument panel and the side-sticks flight control for pilots. Six interchangeable liquid crystal displays (LCDs) on the main instrument panel replace the dials and gauges on older-generation aircraft, providing easy to assimilate information for the two-member crew. The fly-by-wire controls protect against over speeding, stalling and maintaining operation well within the aircraft s structural limits. Side-stick controllers eliminate the center-mounted control columns on other aircraft, opening an unobstructed view of the instrument panel and providing the best use of fly-by-wire flight controls. The Electronic Flight Instrument System provides flight ISSUE Page 1

2 information including navigation displays, while the Electronic Centralized Aircraft Monitor details engine instrumentation and warnings as well as information about aircraft systems. The Airbus ACJ320 is a large-cabin, medium-range, corporate aircraft configured as a cantilevered, swept low-wing monoplane with swept empennage. The retractable tricycle landing gear has dual wheels on each unit. Like other Airbus products, the ACJ320 is highly automated, and is equipped with fly-by-wire, throttle-by-wire, brake-by-wire and steer-by-wire systems. It has a passenger capacity of 30 and a range of 4,100 nm (7,600 km) with two removable fuel tanks. The Airbus ACJ320 typically accommodates 19 with the widest cross-section and the most headroom of any corporate jet. Business and conference centers, lounge areas, private suites and full-height showers are all possible to meet the demands of charter/vip operations, corporate shuttles and government service. Other features may include a private bath, fully equipped food kitchen as well as DVD players and built in phones. The exceptionally large cabin of the ACJ320 can be configured for a variety of roles, but it is anticipated that most customers will opt to arrange the cabin for passenger seating along with office and conference space, sleeping quarters, lavatories and crew quarters. The cabin is over 90 ft. in length and 12 ft. wide. Even fitted with 2 Additional Center Tanks (ACTs), the remaining volume of 28 cu.m.(1000 cu.ft.) can transport over 200 typical suit cases in bulk configuration. In addition, with its two large opening-outward cargo doors, the ACJ320 can be loaded with large-sized travelling cases. GENERAL CHARACTERISTICS Capacity: passengers Length: ft 3 in (37.57 m) Wingspan: ft 5 in (35.80 m) Height: ft 7 in (11.76 m) Maximum Certified Taxi Gross Weight: Pounds ( Kgs) Maximum Certified Take-Off Weight: Pounds ( Kgs) Maximum Certified Landing Weight: Pounds ( Kgs) Basic Empty Weight: Pounds ( Kgs) Maximum Zero Fuel Weight: Pounds ( Kgs) Operational Empty Weight: Pounds ( Kgs) Powerplant: International Aero Engines 4W5198, 27,000 lbs each ISSUE Page 2

3 AIRFRAME Airframe year of construction: 2002 Interior year of manufacture: 2011 Total time airframe: Hours Total landings: EU-OPS Public Transport certified Certified for 26 passengers Range 4 000Nm Cargo Space 28 Cu. Meter Inspections C / 6 years / 12 years check Landing Gear Overhaul done in 2013 No damage history ENGINES Engine type: IAE V2527-A5 Mfg Part No. International Aero Engines 4W5198 Time since new R/H: L/H: Cycles R/H: L/H: Thrust Rating Nominal Trust Pounds Thrust Rating 5 min Take-Off Static Sea Level Pounds APU APU type: Honeywell 131-9A Time since new Hrs Cycles Ldgs APU Time since Last Shop Visit (TSLSV) Hrs APU Cycles since Last Shop Visit (CSLSV) Hrs ISSUE Page 3

4 INTERIOR ISSUE Page 4

5 FORWARD GALLEY AREA HALLWAY G1 (wet galley) Sink and water tap Ice drawer Two cooled compartments with capacity for 12 ATLAS standard containers Air chiller Two Induction Heating Units Nespresso Microwave Drawers and Storage Compartments G2 (dry galley) Several drawers and storage compartments Working table between G1 and G2 Full Hallway length credenza below the windows with storage cabinets and height adaptable shelves Noise suppression curtain between hallway and entrance PRIVATE BEDROOM Two persons bed with two nightstands and surround providing additional storage space One 19 inch LCD screen Wireless telephone Dressing table with mirror installed above it Full height hanging/storage wardrobe Remote control for IFE VIP BATHROOM Round shower cabin Large washbasin with vanity, mirror and storage space Side by side installed toilet and bidet PRIVATE OFFICE 3-seat divan with surround providing additional storage space and bed convertible RH side club seating arrangement with pull-out table and two single VIP seats Two 19 inch LCD screens Wireless handset telephone ISSUE Page 5

6 CONFERENCE AND DINING AREA Six single VIP seats A large oval shaped table with foldable leaves Wireless handset telephone Partitions equipped with one 19 inch, one 42 inch LCD screens and book shelves Credenza with various storage cabinets fitted on the LH side. Cabinets located on both LH and RH aft corners LOUNGE AREA 3-seat divan and two single VIP seats with Hi-Lo position table Side stands with drawers on each side of divan Club-2 seating arrangement with 2 VIP seats and a pull-out table Bar/refreshment equipped with 42 inch LCD screen and stowage flaps. AFT partition with etched semi-transparent screens is equipped with 19 inch LCD screen Wireless handset telephone FIRST CLASS AREA Two club-4 seating arrangements, each with four single VIP seats and a fixed height table 10 inch LCD screen in the seats armrest Literature stowage on AFT partitions Wireless handset telephone AFT VIP LAVATORY Large washstand/vanity cabinet with sink and storage space Large mirror above washstand Toilet with decorative cover and provided with handspray Lavatory amenity storage COMMUNICATION CENTER & AFT STORAGE AREA COMMUNICATION CENTER 1 VIP seat Desk assembly consisting of a working top, a shelf, a drawer and a fax/copier/printer 10 inch LCD at seat armrest Cordered telephone handset AFTER STORAGE AREA Full height storage/wardrobe located aft of the first class area, opposite and beside the VIP lavatory ISSUE Page 6

7 AFT GALLEY AREA Sink and water tap Ice drawer Air Chiller Nespresso Beverage maker Cold Jug Two Induction Heating Units Four ATLAS containers Two FS trolleys, 1 waste trolley and one foldable trolley Several stowage compartments Day configuration Night configuration Lie flat Partial recline Fix sofa ISSUE Page 7

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9 AVIONICS Automatic Flight Control 2 Thales Avionics C13042BA01 Flight Management Guidance Computer 2 Thales Avionics B397BAM0513 Flight Augmentation Computer 1 Thales Avionics C12850AB02 Flight Control Unit 2 Honeywell Multipurpose Control Display Unit Communications 1 Honeywell HF Transceiver 3 Honeywell VHF Transceiver 1 Honeywell Cockpit Voice Recorder 1 Team BC2065C SELCAL Decoder 1 ELTA ELT 406MHz Flight Controls 2 Thales Avionics ELAC Elevador /Aileron Computer 2 Litef «Litton Technische» FCDC Flight Control Data Concentrator 2 Thales Avionics B397BAM0513 FAC Flight Augmentation Computer 2 Liebherr Aerospace-Actuation Divisio SFCC Slat/Flat Control Computer 3 Thales Avionics B372BAM0509 SEC- Spoiler/Elevator Computer Independant Instruments 1 Thales Avionics C12860AA02 CFDIU Central Fault Display Interface 1 Honeywell DFDR Digital Flight Data Interface Recorder 1 SFIM FDIMU ED48A100 DFDIU Digital Flight Data Interface Unit 3 Thales Avionics DMC Display Management Computer 1 Allied Signal Multifunction Printer 2 Airbus 350E SDAC Systems Data Acquisition Concentrator 6 Thales Avionics Primary Flight Display / Navigation Display 2 Airbus 350E FWC Flight Warning Computer ISSUE Page 9

10 Navigation 3 Honeywell HG2030AD11 ADIRU Air Data Inertial Reference Unit 2 Honeywell ATC Air Traffic Control Mode S with ELS/EHS Capability 2 Honeywell DME Distance Measuring Equipment Interrogators 1 Honeywell EGPWS Enhanced Ground Proximity Warning System 2 Honeywell Radio Altimeter 2 Honeywell VHF VOR Receiver 1 Honeywell TCAS II Traffic Collision Avoidance System 1 Honeywell Weather Radar Transceiver 2 Rockwell MMR Multi Mode Receiver (GPS included) 1 Rockwell ADF Receivers CONTACT ENGEL&VÖLKERS AVIATION Eric PAUWELS eric.pauwels@engelvoelkers.com ISSUE Page 10

11 DISCLAIMER This offering is subject, but not limited to, errors, omissions, price fluctuation, and prior sale or withdrawal without notice. All details disclosed are without guarantee and solely based on the information received by Engel & Völkers Aviation. Engel & Völkers Aviation cannot be held liable for any lack of completeness, inaccuracy, or ambiguities and/or errors contained in the information disclosed. It is the buyer s responsibility to disclose the details of any concern(s) to the seller, by the request of an independent survey, pre-purchase inspection and/or enquiry. The buyer must ensure that the purchase contract properly reflects his concern(s) and that it sets out any representations and/or details on upon which he may rely. We are at your disposal for any further information about the aircraft. Upon receipt of notice, the aircraft is available for viewing at timing to be agreed upon, accompanied by an Engel & Völkers Aviation representative. ISSUE Page 11