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Airframe: BRAND NEW
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, Crew Name Plaque (11-30-4202) various
equipment and storage compartments.Large forward galley and galley annex (RHS).
Crew area containing one (1) single narrow executive seat with recliner style footrest, seat
pan leveler, and electric inflatable lumbar, berthable/recline and swivel capability (LHS).Crew area overhead storage bin containing in-flight entertainment equipment and a 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 footrests, electric inflatable lumbar,
berthable/recline, and swivel capability. Seat pan levelers 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 lumbar.Low cabinet under emergency exit.
A mid-cabin bulkhead with a LHS sliding pocket door (removable curtain option to close off
mid cabin from aft cabin area for 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 berthable 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 occupation 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 footrests, seat pan leveler for the forward facing seat, electric inflatable lumbar, berthable/recline, and swivel capability..
Aft Lavatory Zone:Aft cabin bulkheads and hinged door.
EVAC vacuum sanitation system.
Vanity cabinet with miscellaneous storage.
Wardrobe and storage cabinet featuring adjustable and fixed shelving.
Baggage Compartment Area:Approximately 155 cu. ft.
Two (2) fold-down shelves, one (1) fixed and one (1) fold-down coat 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 Bennett “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.
Environmental Control System (ECS):Passenger control of two cabin temperature zones (+/- 2 deg. C) around master control
setting.
Entry area heater.
Privacy Latch Activated exhaust fan in each Lavatory.
Potable 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:Honeywell LSZ-860 Lightning Sensor System (LSS)
Flight Management System - Addition of a third FMS (Honeywell). The 3rd FMS replaces the
Lasertrak™ Navigation Display Unit (NDU) installation.75,000lbs Reduced Maximum Take off Weight (MTOW).
Airborne Data Link System (ADLS)
Stick Pusher Cancel Function Disabled
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).
EICAS small service door “OPEN” annunciation (production and/or completion).
Power Distribution of aircraft AC 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.Electronic Security System Integrated with Camera system (44-50-4003)
Electronic Flight Bag
Cabin Electronic System (CES) – Rockwell Collins
Global Office10/100 Base T Ethernet Local Area Network (LAN) with connections for lap tops 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, and one (1) at each divan end cabinet.Wireless Local Area Network (LAN).
Cabin Utilities / Control and Display
One (1) 10.4” (in.) galley touch screen control monitor.
Two (2) 8.4” (in.) cockpit Touch Screen Equipment.
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-inch LCD video monitors in passenger cabin. High quality cabin speaker/subwoofer arrangement. Eight (8) receptacles for plug-in monitors installed in the passenger area and one (1) in the Crew rest area. Six (6) plug-in 10.4” touch screen LCD monitors provided as loose equipment Passenger headphone distribution system. Airshow ASXi interactive In-Flight information system (moving map). Portable Multimedia input Port (44-22-4006)Cabin Services
Cabin/Lavatory Call System Passenger Address System Passenger briefing system ICG ICS-100 Iridium Telephone systemMaintenance and Diagnostics
Central maintenance function for applicable integrated cabin systems Diagnostic reports viewable on the galley touch screen monitor or 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.
Miscellaneous Equipment and Installations:Aircraft miscellaneous installations
Addition of Refuel/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 60 lbs. Towbar assembly and towbar storage provisions (towbar is loose equipment). Multi purpose aft equipment bay access ladder. Two (2) 7-inch gear pin storage boxes in the Airstair. Semi-recessed Jeppesen manual storage box at cockpit entrance. Aircraft identification plate (11-30-4001)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 (retained from factory). One (1) side console storage bin (former Lasertrak location) Protective smoke goggle in pouch.Galley Equipment:
One (1) 0.7 cu. ft. microwave oven (TIA). One (1) AEROLUX NESPRESSO manual fills 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 An allowance of $25,000 US for china, crystal and flatware has been included.
Passenger cabin miscellaneous equipment: Entry area heater Accordion-type electric window shadesLoose Equipment (in addition to standard items):
Six (6) plug-in 10.4” touch screen LCD monitors in leather pouches. Single and Double Seats armrest covers. Eight (8) through pillows. Lasertrak™ unit (replaced by 3rd FMS). One (1) portable defibrillator
Emergency Equipment:Smoke detector in each lavatory, in aft wardrobe and in baggage (factory-installed)
JAR OPS 1 Life rafts, life vests, PBEs, fire extinguishers, and first aid kit as required.
Engraved Maglite flashlight (in addition to (2) cockpit flashlights)
Exterior Paint:The Aircraft detailed paint is done in accordance with the Customer-approved drawing.
The aircraft exterior will be painted at Savannah Air Center.
Note: Bombardier does not recommend the painting of large surfaces in metallic paint. This
is due to the natural properties of the paint, which preclude color matching, and color blending across large surfaces and panel joints, and which significantly increases the risk of paint cracking due to normal aircraft flexion. All metallic paint applications are heavier than non-metallic applications. Per Schedule A, Revision 4, dated June 2005, paragraph 15.3. Notwithstanding Article 15.2, the Warranty for the Completion Work shall be for 2,000 flight hours or 24 months from Delivery Time, whichever first occurs except for the Warranty for the metallic exterior paint, which shall be limited to 90 days from Delivery Time.The following provisions are provided:
One (1) color, silver metallic paint with one (1) Seminole red straight stripes shown on the fuselage and nacelles. Landing gear is retained as received from the factory (painted white). The main entry door and baggage door edges and frames are painted. The main entrance airstair is painted the same color as the bottom fuselage color. Paint inside of engine cowlings. An erosion protective film is installed on the radome.The following original bright work on the aircraft exterior will be highly polished:
Cabin window surround polished The leading edges of: wings and winglets, vertical stabilizer, engine cowl and pylon, and horizontal stabilizer. Baggage door handle polished. APU exhaust surrounding area polished. Radome, avionics and service doors hinges polished. APU access cowling latches polished.
Aesthetic Trim Allowance (Material content only):Up to two species (types) of hi-gloss veneer on cabinetry shipset (galley, vanity, enclosures,
furniture, magazine racks, tables, cabin ledges, handrails, bulkheads and doors).Combination fabric -veneer or mirror- veneer as optional selections on bulkheads and doors.
Simple hardwood molding complementing veneer where applicable. Choice of up to ten
routered moldings (bullnose) where applicable.Flat beveled (no etching) Lexan glassware closeout in upper galley area (no curves or
radius).Plated (24K polished gold, satin antique brass or equivalent) appointments in the main
passenger area only.Up to two inlays in tables, bulkheads, galley, vanity and longitudinal cabin area (dado or
sidewall), (plated metal, cross grain veneer, or marquetry to compliment veneer in cabinetry components), (plated metal in dado or sidewall overlay).100% wool, 3/8” pile (approximately 95 oz face-weight) machine quality custom carpet in
main cabin area (up to three colors, cut, loop, or multi-pattern design).100% wool, 5/16” pile (approximately 52 oz face-weight) machine quality custom carpet on
seat bases, dado trim and cockpit floor (up to three colors, cut, loop, or multi-pattern design).Common stitched fabric, leather or combination fabric/leather passenger seating dress
covering in a choice of ten standard design styles.Common stitched fabric or leather divan dress covering in a choice of four standard design
styles.Up to two types of common stitched fabric, leather, or fabric/leather combination on lower
dado (no box pleating or decorative stitching).Fabric finished periphery (headliner, PSU, valance, and sidewall overlays).
Fabric interior curtains where applicable complete with fabric/leather acoustic entry curtain.
Durable grospoint fabric lining in utilitarian area (wardrobes).
Solid surface (Corian, Surell, Avonite, etc.), Aeroquest, or Polystone galley and lavatory
countertops complete with stainless steel sink galley sink and plated or integrally molded vanity sink as applicable (no granite tile).Choice of two (2) galley tapsets.
Choice of eight (8) elegant lavatory tapset and towel bar design options.
Choice of four (4) SAM latch design styles (plated).
Combination of paint and plastic laminate drawer linings in the galley and lavatory.
Fabric lined divan armrest drawers.
Painted sidewall window rings.
Standard factory grey cockpit with headliner and cockpit carpet to match interior aesthetics.
Standard factory baggage finishes.
Certification:Quality Assurance and Control
A TC approved Quality Assurance and Quality Control system will be maintained by the
CompletionCenter and applied to the work performed on the aircraft. Quality Control (QC)
department personnel including Transport Canada (TC) authorized inspectors will be responsible for: All inspection activities on the aircraft from the initial receiving inspection to final Customer inspection and delivery. In this capacity, QC will verify that all measures to preserve the aircraft, fabricate and install the interior to an approved design, workmanship and safety standards are maintained during the completion program.Assurances that the systems, processes and procedures utilized by all personnel
working on aircraft are in accordance with the TC regulations.Certification.
This Specification meets the airworthiness requirements of JAR 25 and the equipment
requirements necessary for JAR OPS 1 operations.
The Completion Center will be responsible for obtaining approval for the interior
completion modifications and any required negotiations with the regulatory authorities.The following configurations will be approved: Fourteen (14) passenger configuration
features a frangible mid cabin door.The aircraft may not be operated for hire or common carriage.
Note: The mid cabin RHS removable upper bulkhead must be removed if the forward
seating position of the 16G divan is to be occupied for taxi, take-off and landing. If the removable mid cabin bulkhead is installed, then the passenger capacity of the aircraft is reduced to thirteen (13).This specification includes complete provisions to support a future interior modification
enabling the aft cabin to be used as a flight crew sleeping quarter as required under FAA rules for FAR Part 135 operations for flights between 10 to 12 hours of duration; as well as a means to disable the frangible mid cabin door and a privacy curtain. The device used to disable the mid cabin door and the privacy curtain will be provided as loose equipment.Note: Service Bulletin 700-31-020 Crew Force Measuring System (FDR upgrade),
which is required for FAR Part 135 operation, has not been included.This specification includes life rafts that meet the airworthiness requirements for certification of the aircraft for ditching.
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