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Bombardier Global XRS Limited Edition
INTERIOR CONFIGURATION:
Entry Area:
- Forward lavatory; EVAC vacuum sanitation system, vanity and storage cabinets;
- LH Entrance Enclosure with coat rod, Flight Observer Seat and quick donning oxygen mask for the Flight Observer Seat occupant, various equipment and storage compartments;
- Large forward galley and galley annex (RHS);
- Crew area containing one (1) single marrow executive seat with recliner style footrest, seat pan leveller, electric inflatable lumber, berth able/ recline and swivel capability (LHS);
- Crew area overhead storage bin containing in-flight entertainment equipment and s storage cabinet with fold-down table.
Forward Cabin:
- A single manual sliding LHS pocket door to close off cabin from entry area;
- Four (4) single wide executive seats with recliner style footrest, electric inflatable lumbar, berth able/ recline and swivel capability. Seat pan levellers will be installed for the LHS 2 and RHS 2 seat;
- Two (2) bi-fold pull-out side ledge tables.
Mid Cabin:
- RH side: executive workstation with fax/ printer and single narrow executive seat with electric lumbar and swivel capability. Note: recline capabilities disabled at the workstation due to its proximity to the emergency exit;
- LH side: one (1) manually-operated hi-low conference table with plug in extension;
- LH side: two (2) sets of double seats that feature recline, track & swivel (swivel on inboard chairs only) and electric inflatable lumber;
- Low cabinet under emergency exit;
- A mid-cabin bulkhead with LHS sliding pocket door (removable curtain option to close off mid cabin from aft cabin are for FAR Part 135 or JAR-OPS-1 operation).
The right-hand mid-cabin upper bulkhead is removable (operation requirement when aft cabin divan forward seated position is occupied for taxi, take-off and landing).
Aft Cabin:
- RH side: 3 place berth able 16G divan. Two (2) end cabinets, each featuring: drink holders, storage.
The right-hand mid cabin upper bulkhead must be removed to allow divan forward seated position occupant during taxi, takeoff and landing;
- LH side: one (1) side ledge bi-fold pull-out table and two (2) single wide executive seats with recliner style footrest, seat pin leveller for the forward facing seat, electric inflatable lumbar, berth able/ recline and swivel capability.
Aft Lavatory Zone:
- Aft cabin bulkhead and ringer door;
- EVAC vacuum sanitation system;
- Vanity cabinet with miscellaneous storage;
- Wardrobe and storage cabinet featuring adjustable and fixed shelving.
Baggage Compartment Area:
- Approximately 155 cubic feet;
- Two (2) fold down shelves, one (1) fixed and one (1) fold down coar rod;
- Two (2) hang-up bars (one swings down to stow);
- Storage around ACPC, including removable coat rods with adjustable shelves and restraint net.
EQUIPMENT AND SYSTEMS:
Oxygen system:
- Factory installed EROS MF-10 full face masks are retained for the pilot and co-pilot;
- Puritan Bennet ‘Sweep On’ 2000 half masks on pilot and co-pilot’s bulkheads;
- LH entrance Enclosure MC-20 quick donning oxygen mask with goggles as loose equipment;
- Two (2) therapeutic oxygen outlets in passenger cabin;
- Oxygen drop boxes as required in main cabin as well as galley, lavatories and at Flight Observer Seat.
Environment Control System (ECS):
- Passenger control on two cabin temperature zones (+-2 deg C) around master control setting;
- Entry area heater
- Privacy Latch Activated exhaust fan in each Lavatory.
Portable Water System:
- Re-circulating water system with dual pumps (for redundancy) and UV filter system;
- Heated hose assemblies and component where appropriate for freeze protection;
- Pressurized lines and components are installed within shrouds to protect critical aircraft systems;
- Single exterior servicing port and manual internal fill capability;
- 28.6 US Gallon water tank.
Waste system:
- Single waste tank (16 usable gallons) that services two-vacuum toilet system (forward and aft lavatories);
- The vacuum waste system utilizes the pressure differential when the a/c is above 16,000 feet;
- A vacuum generator is used to generate pressure differential when the aircraft is below 16,000 feet or on the ground.
AVIONICS/ ELECTRICAL SYSTEMS:
Factory installed avionic equipment is listed in ‘Schedule A’.
Service Bulletins:
700-23-004 – Miltope Flight Compartment Printer;
700-34-030 – Honeywell LSZ-860 Lighting Sensor System (LSS);
700-34-004 – Flight Management System – addition of a third FMS (Honeywell). The 3rd FMS replaces the Lasertrak Navigation Display Unit (NDU) installation;
700-11-018 – 75,000 lbs Reduced Maximum Take-off Weight (MTOW);
700-23-005/ 700-23-015 – Airborne Data Link System (ADLS);
700-27-025 – Stick Pusher Cancel Function;
700-31-026 – Quick Access Recorder.
Other Avionics/ Electrical Systems:
- Satellite Communication System (SATCOM)
- Satellite Communication System and High Speed Link (SAT-6100);
- Three (3) channels Aero H+ (2 voice channels and 1 data channel). Data channel supports ACARS/ maintenance functions;
- One (1) single channel Iridium based airborne telephone system;
- PBX (Aerocom 3000B) integrates cabin voice communication allowing common access from handsets;
- Four (4) passenger cabin handsets (cockpit, crew area, RHS 2 and LHS 6);
- Dual channel high speed data system. Two (2) HST-2100 provides data transfer up to 128 kbps total (64 Kbps of data transfer rate per channel);
- Cabin power bus disconnect;
- Illuminated approach chart holders for pilot and co-pilot;
- Flight Observer Seat Audio Panel located on the cockpit pedestal;
- One (1) power converter (3500 VA/ 115V/ 60Hz);
- Cockpit analogue telephone jack and loose equipment telephone handset (back-up phone);
- EICAS small service door ‘OPEN’ annunciation (production and/ or completion);
- Power Distribution of aircraft AS and DC power;
- 115 VAC GFI electrical outlets located as follows:
- A dual outlet in each lavatory and at the Galley, workstation, LH entrance enclosure;
- A single outlet at each single seat and outboard double seats;
- A single outlet located adjacent to each cockpit seat.
Cabin Electronic System (CES) – Rockwell Collins
- Global Office:
- 10/100 Base T Ethernet Local Area Network (LAN) with connections for laptops and other portable devices;
- Plain paper Fax/ Printer/ Scanner;
- RJ-45 LAN interface located at the following locations: two (2) in the cockpit, one (1) in the crew area, one (1) at each single seat grouping, one (1) at the workstation and one (1) at the double seats, one (1) at each divan and cabinet;
- Wireless Local Area Network (LAN).
- Cabin Utilities/ Control and Display:
- One (1) 10.4’’ (in) galley touch screen control monitor;
- One (1) 8.4’’ (in) cockpit Touch Screen Equipment (co-pilot side);
- Wireless Passenger control units (PCU), entertainment switch panel and local switch panels.
- Power Distribution of aircraft AC and DC power;
- Entertainment:
- Three (3) multi-region CD/ DVD players combined unit;
- Two (2) bulkhead-mounted 21.3’’ (in) LCD video monitors in passenger cabin;
- High quality cabin speakers/ subwoofer arrangement;
- Eight (8) receptacles for plug-in monitors installed in the passenger area and one (1) in the Crew rest area;
- Three (3) plug-in 10.4’’ (in) touch screen LCD monitors provided as loose equipment;
- Passenger headphone distribution system;
- Airshow ASXi interactive In-Flight information system (moving map).
- Cabin services:
- Cabin/ Lavatory Call System;
- Passenger Address System;
- Passenger briefing system;
- ICG ICS-100 Iridium Telephone system.
- Maintenance and Diagnostics:
- Central maintenance function for applicable integrated cabin systems;
- Diagnostic reports viewable on the galley touch screen and other connected devices. A security access protocol prevents unauthorized access.
Lighting:
- Light Emitting Diode (LED) interior lighting;
- Wing tip taxi lights;
- Wheel well maintenance lights;
- Pulse landing light system;
- Illuminated ordinance signs;
- Exterior ground service panel lights (pylon lights);
- External Service Panel lighting;
- Service Lights timer override;
- Logo Lights.
Aircraft Miscellaneous installations:
- Aircraft miscellaneous installations:
- Addition of Reduce/ De-fuel Control Panel in the Entrance Enclosure;
- Common keyed locks (external door panels);
- Airstair forward handrail extension;
- External baggage door lock override;
- Catwalk battery access;
- Aft equipment bay storage box with a maximum weight capacity of 60lbs;
- Tow bar assembly and tow bar storage provisions (tow bar is loose equipment);
- Multipurpose aft equipment bay access ladder;
- Two (2) 7-inch gear pin storage boxes in the Airstair;
- Semi0reccessed Jeppesen manual storage box at cockpit entrance.
- Cockpit miscellaneous equipment:
- Two (2) engraved Maglite rechargeable flashlights;
- Two (2) roller screens;
- Two (2) writing pad holders;
- Two (2) Storage pouches on each side console;
- Cockpit footrest storage bin (former Lasertrak location);
- Protective smoke goggles in pouch.
- Galley Equipment:
- One (1) 0.7 cu.ft. microwave oven (TIA);
- One (1) AEROLUX NESPRESSO manual fill coffee maker;
- One (1) TIA (1545-3) high temperature oven behind a nesting door with digital oven controller;
- One (1) air chiller unit used to cool the selected galley areas;
- One divided ice drawer with overboard drain.
Note: The china, crystal and flatware are customer supplied.
- Passenger cabin miscellaneous equipment:
- Entry area heater;
- Accordion-type electric window shades.
- Loose Equipment (in addition to standard items):
- Three (3) plug-in 10.4’’ (in) touch screen LCD monitors in leather pouches;
- Single and Double Seats armrest covers;
- Eight (8) through pillows;
- Lasertrak unit (replaced by 3rd FMS);
- Standby analog handset.
- Selected Spares (in addition to standard items):
- One (1) spare carpet (FS 250 to FS 799).
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