
                 ************************************
                 *    Raytheon Beech B1900D         *
                 *        UNITED EXPRESS            * 
                 *      Great Lakes Aviation)       *
                 *           Ver 6 Model            *
                 *           Reg# N220GL            *
                 ************************************
        
        
        NOTAM: This aircraft is in FS2002 PRO Format

        FS2002 PRO Raytheon / Beechcraft B1900D
        United Express
        Operated by:
        Great Lakes Aviation Ltd
        Cheyenne, Wyoming
        http://www.greatlakesav.com
   
        File name B19UEX22 for FS2002 Only
      
        AF99/AA Design FD, MP and original artwork by: Barry Blaisdell
        email: barrywb@snet.net

        United Express livery and night effects by Bob May 
        email: bob@wem162.worldonline.co.uk
        ----------------------------------------------------------------

        This aircraft was created by Barry Blaisdell using AF99 Aircraft Factory
         and Aircraft Animator by Abacus Software.

        It consists of many 3D parts, Full animated control surfaces,
        and landing gear, Steerable Nosewheel and Retracted Wheels showing in their wells.

        Ver 6 FOR FS2002 now adds a new 16 point fuselage, new engines, new motion                 sequences,
        Textured Props, special night effects.. plus lots more stuff...
   
        =====================================================================

        Spec's from Jane's "All the Worlds Aircraft"

        Beech B1900D Specifications:
 
        Aircraft Data:

        The Beech 1900D is powered by 2 P&W Canada PT6A-67D
        Turbo Shaft Engines rated at 1,279 shp each driving
        9 ft-1 in dia Hartzell 4 blade constant speed,
        fully feathering, pitch reverseible metal propellers.
        
        Crew of 2
        Passengers : 19

        Wing span....................57 ft-11 in
        Length overall...............57 ft-10 in
        Overall Height...............15 ft- 6 in
        Max cruise speed.............288 kts TAS @ 16,000 ft
        Normal Cruise speed..........276 kts TAS @ 8,000 ft
        Service Ceiling..............25,000 ft.
        Maximum Ceiling..............31,000 ft.
        Empty Weight.................10,615 lbs.
        Max. Take Off Wt (MTOW)......16,950 lbs.
        Max. Rate of Climb @ MTOW....2300 fpm @ SL
        Clean stall..................101 kts.
        Dirty stall (flaps & gear)...84 kts.
        Flap Notches - (3)  0 - 17 - 35
        Max. Range(Full Load)..................1475 nm
        Total Usable Fuel............668 US Gallons       
        Take Off Speed...............105-111 Kts @ MTOW(14,930 lb)
        Approach Speed...............117 Kts @ MLW (15,000 lb)

  
        Barry Blaisdell, Stratford, Connecticut,  USA
        4nm DME 5 deg Radial from BDR ILS

        Internet: barrywb@snet.net
        Web Site: http://www.flightsimnetwork.com/premaircraft/

       **********************************
                           
                          LEGAL NOTICE

1. These files are for free use and enjoyment of individual hobby flightsimmers but
   the copyright remains with me and any other persons who have contributed to the work.

2. The files should not be altered and cannot be incorporated into other 
   programs, including freeware and shareware,  or published on any electronic or mechanical
   media anywhere in the world without my written permission. This includes
   CD's or other media offered free, whether as part of a commercial or non-commercial transaction.

3. REPAINTING. You may repaint this aircraft FOR YOUR OWN EXCLUSIVE use
   without seeking permission, but if you intend to upload the repainted aircraft to any
   web site or bulletin board, including a Virtual Airline site, then contact me first for
   permission. I reserve the right to check the files and documentation before publication.

Barry Blaisdell  
Contact me by email at: barrywb@snet.net

ALL FILES ARE Copyright 2002  by the author(s). 