As Authorized Marketing Agents for SAS, Bombardier Presents for ...
As Authorized Marketing Agents for SAS, Bombardier Presents for ...
As Authorized Marketing Agents for SAS, Bombardier Presents for ...
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<strong>As</strong> <strong>Authorized</strong> <strong>Marketing</strong> <strong>Agents</strong> <strong>for</strong> <strong>SAS</strong>,<strong>Bombardier</strong> <strong>Presents</strong> <strong>for</strong> SaleQ400 Aircraft - 4013Rev. 6B
Aircraft Summary:The Q400 is an extraordinary modern technology turboprop, offering airlines exceptionaleconomics with jet speed and com<strong>for</strong>t in the 70-seat market. Designed to meet therequirements of regional airlines <strong>for</strong> more seats, superior economics and greater speed inthe high-density regional arena, the Q400 is also replacing and supplementing jets on manyregional and mainline routes worldwide.With a maximum cruise speed of 360 kts, outstanding per<strong>for</strong>mance and seating of up to 78passengers, the Q400 provides airlines with greater revenue-generating opportunities inregional and low cost markets and extends an airline's reach well beyond traditionalturboprop markets.The Q400 is easily as fast as most jets on airline routes under 500 miles (800 km) and it’sextraordinary economics, best of any regional aircraft today, are enabling it to competeeffectively against established low cost carriers.While the Q400 is larger and faster than the other Q Series models, the same pool of pilotscan fly this aircraft, resulting in reduced crew costs <strong>for</strong> airlines with a mixed Q Series fleet.Aircraft History:<strong>SAS</strong> was the launch customer of the Q400. The <strong>SAS</strong> fleet Q400 was delivered as newaircraft directly from <strong>Bombardier</strong> between February 2000 and February 2002. In lateOctober 2007, <strong>SAS</strong> elected to voluntarily withdraw the Q400 from active service andsubsequently offer 24 Q400 aircraft <strong>for</strong> sale.Rev 6, Page 2 of 10B
Aircraft Specification:Technical Data PDFDelivery Conditions:The <strong>SAS</strong> Q400 aircraft will be delivered in the following condition:• Valid C of A and if required a C of A <strong>for</strong> Export• Fresh next due C-Check to MRB Standard (Note aircraft 4012 and 4036 will be soldon the basis of C-checks already done to <strong>SAS</strong> Maintenance Program)• All Airworthiness Directives due 90 days after delivery• Engines, props and landing gear times and cycles largely in accordance with theattached spec sheets.• 600 hours, 600 cycles and 6 months on all other components• Landing Gear Mods complied with per schedule driven by Customer Support.• <strong>SAS</strong> Logos painted over.• Otherwise delivery will be “AS-IS”Not IncludedManuals, Spares, GSERev 6, Page 3 of 10B
Specifications:Please visit www.q400.com <strong>for</strong> product overview and general detailsStandard Avionics:• Avionicso Automatic Flight Control Systemo Autopilot with Dual Flight Directoro Dual Attitude and Heading Reference System (APIRS)o Dual Air Data Computerso EFIS (Electronic Flight Instrument System) (Thales V810 incorporated)o Cat II capabilityo Engine and Systems Integrated Display (ESID)• Navigationo Dual VHF (VOR, Glideslope and Marker)o Dual ADF, DME and ATC Mode S (EHS capable)o Single Flight Management System with GPS (UNS-1E)• Communicationo Dual VHF System (8.33 kHz frequency spacing)o Service Interphone and Passenger Address System• Other Systemso Integrated Standby Flight Instrument System (Thales)o Dual Radio Altimeter (Honeywell KRA-405B)o Colour Weather Radar (Honeywell Primus P660)o Enhanced Ground Proximity Warning System (EGPWS) (Honeywell Mk V)• with terrain clearance floor display on MFD• Steep approach switch on 4010, 4022, 4033, 4034, 4054o TCAS II/ACAS (change 7) (Honeywell CAS 67A)o Audio Integrating Systemo Solid State Cockpit Voice Recorder (2 hr) (Honeywell 6022)o Emergency Locator Transmitter (3 frequency) (Kannad 406AF)o Solid State Flight Data Recorder (Honeywell 4700)o Centralized Maintenance and Diagnostic Systemo ACARS with ½ size printer & 3 rd VHF Comm (8.33 kHz) (Unilink 700)o EQAR (Extended Quick Access Recorder) (Thales)o Passenger boarding and music system (Team)<strong>SAS</strong> Incorporated STC’s:• Installation of Crew Oxygen Servicing System• Installation of Saftglo Emergency Photoluminescent Floorpath Marking• Installation of No-Slip Floor in front of Airstair Door• Installation of Rein<strong>for</strong>ced Cockpit Door• Modification of Switch <strong>for</strong> Internal baggage door, to improve reliability• Modification of Aft Baggage Compartment door restraint netRev 6, Page 4 of 10B
Additional Installed Options:• Servicing - Cold weather maintenance – External AC powered heating – Wash watersystem (T1) and wet galley (G1)• Servicing – Engine oil level indication system in cockpit• Servicing – Pressure water filling system <strong>for</strong> G1 galley• Air conditioning – Installation of ground air conditioning connector• Electrical power – Relocation of AC ground power connection to RHS fwd fuse• Baby change table in lavatory• Additional manual stowage in flight compartment• Forward RHS galley unit (G6) with stowage provisions <strong>for</strong> two aisle trolleys and twoSU’s• 51 ft3 baggage compartment – removable upper shelf• Overhead bin – handrails• G1 Galley with stowage locations <strong>for</strong> two aisle trolleys and four SU’S – Installation of50L watertank (approx) & AC powered water boiler• G3 Galley with stowage locations <strong>for</strong> four aisle trolleys and 1 SU and & 2 ACpowered KSSU size ovens• Crew seats - AMI model 1414 Pilot seats• Moveable class divider curtains above passenger seats only, no aisle curtain• Lavatory – Wash water system• Baggage divider nets and posts (aft compartment)• Passenger window blinds• Fuel indication – Introduction of metric quantity and flow indication• Tail logo lights• VHF COMM – Provisions <strong>for</strong> 3rd VHF radio• Installation of second radio altimeter• TCAS II (SOFTWARE CHANGE 7.0) / ACAS• Full face oxygen and smoke masks <strong>for</strong> flight crew and observer – Puritan Bennet• 3 PBE‘S installed in passenger compartment – Puritan Bennett• Emergency equipment – Additional F/A portable oxygen• Altimeter digital barometric read-out on PFD in millibars in lieu of standard inches ofmercury• APU – Louvered inlet cover• Auxiliary Power Unit (APU) – including DC generation and titanium tailcone• Airstair door compatible with jetway – folding handrails• Cockpit centre console extension• Passenger Seat ReclineRev 6, Page 5 of 10B
Rev 6, Page 6 of 10B
Galley Configurations:G6 Galley– Fwd RHS- 2 carts- 2 SU’s- Emergency Equipment- Misc. stowageG5 Galley– Rear RHS, Aft FacingComposed of G1 + extension- 2 carts- 50L water tank and boiler- 4 SU’s- Work counter- Trash bin- Misc stowageG3 Galley*– Rear RHS, Fwd Facing- 4 carts- 1 SU- 2 Ovens- Work counter- Trash bin- Misc. stowage*Galleys may not be exactly as shown in line drawings.Rev 6, Page 7 of 10B
Aircraft Photos:Flight deckCabin with moveable class dividers installedRev 6, Page 8 of 10B
Aircraft Photos: continuedPassenger handrailCabin window blindsPassenger service unit detailsRear galley curtain1 st Row in-arm meal traysRev 6, Page 9 of 10B
DisclaimerIn<strong>for</strong>mation contained in this document is proprietary to <strong>Bombardier</strong> Inc.,<strong>Bombardier</strong> Aerospace, Regional Aircraft (“<strong>Bombardier</strong>”). This document mustnot be reproduced or shared with, or distributed to, any third party in whole orin part without <strong>Bombardier</strong>’s prior written consent.This document is submitted <strong>for</strong> in<strong>for</strong>mational purposes only, is not part of anyproposal, and creates no contractual commitment. <strong>Bombardier</strong> provides thein<strong>for</strong>mation contained in this document on an ‘as is, where is’ basis, andmakes no representation or warranty of any kind regarding the applicability orreliability of any of such in<strong>for</strong>mation with respect to any use whatsoever to bemade of it by the recipient.Any in<strong>for</strong>mation of a technical nature contained in this document may containinaccuracies, is subject to change and should never be relied upon <strong>for</strong>operational use.Rev 6, Page 10 of 10B