2017 BOMBARDIER GLOBAL 7000

2017

BOMBARDIER

GLOBAL 7000

New

The new Bombardier Global 7000 business jet completely defines freedom, flexibility and comfort. The unique, true 4-zone cabin offers infinitely greater configuration possibilities to optimize productivity or allow for leisure pastimes without compromise. Equally impressive, the Global 7000 aircraft flies 7,300 nm at Mach 0.85 with 10 passengers, connecting key city-pairs such as New York-Dubai, London-Singapore, and Beijing-Washington. Next-generation GE engines developed specifically for this aircraft set the new standard on efficiency, with their industry-leading low fuel burn and low emissions An unparalleled 4-zone living space Designed for 7,300 NM range with 10 passengers at Mach 0.85 with an unsurpassed Mach 0.90 high-speed cruise capability Next-generation GE engines deliver more efficiency with low fuel burn and low emissions The aircraft shall be certified to the transport category airplane / large airplane airworthiness requirements of TC, FAA and EASA. The Aircraft shall be certified for operations in day and night, under known icing, VFR and IFR conditions, RVSM / DRVSM operations and Category II operations. The pressurization system shall be certified for operations to a maximum pressure altitude of 51,00 ft (15.545 m). The aircraft and its installed equipment (excluding cabin systems) shall be certified to operate at sea level ambient temperatures from -40°C (-40°F) to +50°C (+122°F). Unless otherwise agreed to between Seller and Buyer, Seller will provide Buyer with a Transport Canada or FAA Standard Airworthiness Certificate, compliant with Private category operations per TC CAR 604 or FAA FAR Part 91. S/N: 13, Delivery date: Second Quarter 2017, Designed for 7,300 NM range with 10 passengers at Mach 0.85 with an unsurpassed Mach 0.90 high-speed cruise capability

Crew (minimum) 2 Passengers (typical / maximum) 10/19 FUEL SYSTEM : Tank Configuration - 3 Wing Tanks, 1 Aft Tank ELECTRICAL SYSTEM : Number of Engine AC Generators - 2 (1 per engine) RANGE PERFORMANCE (M0.85 Cruise) : Range 7,300 NM + 2% 13.520 km + 2% FLIGHT CHARACTERISTICS : High speed cruise M 0.90 516 kts Typical cruise M 0.85 488 kts Maximum operating altitude 51,000 ft 15,545 m Initial cruise altitude after MTOW departure 43,000 ft + 1,000 ft 13.106 m + 305 m TAKE-OFF (SL, ISA, MTOW) : Take-off field length 5,950 ft + 8% 1.814 m + 8% LANDING (SL, MLW) : Actual landing distance 2,810 ft + 8% 856 m + 8% Approach speed – Vref 133 kts + 3%

Number 2 Make General Electric Thrust 16,500 lb (73.4 kN) Maintenance Program On Condition

Avionics Suite - Highly Integrated Advanced Flight Deck The navigation system includes the following: Integrated Flight Information System (IFIS) Paperless operation Electronic Flight Bag (EFB) Head-Up Flight Display System (HUD) Enhanced Vision System (EVS) Synthetic Vision System (SVS) Integrated Electronic Standby Instrument Air Data System (ADS) Weather Radar Inertial Reference System (IRS) Navigation and surveillance sensors – include GPS, VHF, ADF, DME, TCAS II (featuring ADS-B and TIS-B) Transporder and Radio Altimeter systems. AUTOFLIGHT : Automatic Flight Control Systems (AFCS) provides an interface with the flight control system. The AFCS includes computations for flight guidance, autopilot and auto throttle. The flight director modes are selected on the Flight Control Panel (FCP) or via the take-off go-around switches on the throttles. Each automatic flight control system includes an automatic throttle subsystem, consisting of thrust and speed commutations that drive and integrated Throttle Quadrant Assembly (TQA). COMMUNICATIONS : The Aircraft communication system includes a triple VHF Communication system, an HF Communication system, a dual SELCAL system, a Datalink system (including Modes A and 2, as well as FANS and CPDLC functionalities), and a triple digital audio system. INDICATIONS / RECORDING SYSTEMS : The Indicating / Recording system includes the Electronic Flight Instrument System (EFIS), a Cockpit Voice Recorder (CVR) system (supporting the recording of Datalink communications) with a Recorder Independent Power Supply (RIPS), a Flight Data Recorder (FDR) with an Underwater Location Device (ULD), an Emergency Locator Transmitter (ELT), and dual GPS synchronized clocks. Automatic display reversion reduces workload and ensures that the primary information is always available to the crew in all display configurations.

Flight Control System Fully Powered Landing Gear Tricycle Configuration Hydraulics 3 Independent Systems

EXTERIOR DIMENSIONS : Lenght (minimum) 110.6 ft 33,71 m Height 26.7 ft 8,14 m Wingspan 104.3 ft 31,79 m Maximum Fuselage Diameter 8.84 ft 2,69 m

The Global 7000 aircraft is configured with an entrance/working area with lavatory, four distinct seating zones in the passenger cabin, a large aft lavatory and a baggage compartment. ENTRANCE AREA The entrance area comprises a mixed working space for cabin crew as well as features for use by passengers. LHS wardrobe with storage space, includes jump seat and emergency oxygen. RHS galley with storage including chilled insulated storage, amenities for food preparation, sink and faucet as well as a work surface. RHS lavatory with sink and faucet, vanity cabinet with storage, and vacuum-toilet system. LHS crew rest area with single seat (16G qualified) with recline and berthing capability. Crew rest also includes side ledge stowable table, cup holders and cabin amenities. PSU overhead amenities including lighting and emergency oxygen. PASSENGER CABIN – ZONE 1 Four single seats (16G qualified) with recline and berthing capability LHS and RHS sideledge with tables (one between each seat pair). Sidelage also includes cup holders, storage space and cabin amenities. PSU overhead amenities including lighting and emergency oxygen. PASSENGER CABIN – ZONE 2 Two RHS single seats (16G qualified) with recline and berthing capability. RHS sideledge with pull-out table (one between seat pair), cup holders and cabin amenities. LHS 4-place conference seating (16G qualified) One LHS Hi-Lo conference table. PSU overhead amenities including lighting and emergency oxygen. PASSENGER CABIN – ZONE 3 RHS low storage cabinet inboard of emergency exit. RHS credenza with storage and entertainment monitor One LHS 3-place divan (16G qualified) including end cabinets with storage, cup holders and cabin amenities. PSU overhead amenities including lighting and emergency oxygen. PASSENGER CABIN – ZONE 4 One LHS single seat (16G qualified) with recline berthing capability. Sidelage with pull-out table, cup holders and cabin amenities LHS angled entertainment cabinet, with monitor, entertainment equipment and storage. One RHS 3-place divan (16G qualified) including end cabinets with storage, cup holders and cabin amenities. PSU overhead amenities including lighting and emergency oxygen. AFT LAVATORY Vacuum toilet system Sink and faucet with mirror and lighting Vanity with storage space LHS wardrobe for additional storage. BAGGAGE 195 cu ft useable baggage compartment. ENVIRONMENTAL CONTROL SYSTEM : Equivalent Cabin Altitude at 51,000 ft 5,674 ft (1.729 m) Number of independent temperature zones 4 INTERIOR DIMENSIONS : Height (maximum) 6.25 ft 1,91 m Width (maximum) 8.17 ft 2,49 m Lenght (between cockpit and aft pressure bulkhead) 59.6 ft 18,17 m Passenger door height 6.17 ft 1,88 m Passenger door width 3.0 ft 0,91 m Aft baggage useable volume 195 cu ft 5,52 cu m First zone can be blocked-off from the main living area to accommodate personnel (e.g. 2nd flight attendant, security) and still provides a 3-zone private cabin Available FAR Part 135 compliant Crew Rest for flight over 12 hours. Fully enclosed crew rest provides calm and privacy