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2005 Bell 407 [复制链接]

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1#
发表于 2010-11-22 15:58:27 |只看该作者 |倒序浏览
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Rank: 9Rank: 9Rank: 9

2#
发表于 2010-11-22 15:59:18 |只看该作者
2005 Bell 407 SN – 53648 – N9133D OVERVIEW AFTT: 330 Hours High Skid Gear w/ Flight Steps Sliding Passenger Windows Particle Separator Dual Controls Rotor Brake Aux Fuel Equipment & Provisions 28 AMP Battery Engine Fire Detection Wire Strike Protection System Attitude & Turn & Slip Indicators Markings for High Visibility Main Rotor Blades AVIONICS Avionics Console Avionics Master Switch PMA 7000 Audio Panel w/ 5 Station Aft ICS/Cabin ICS call Garmin GNS-430 GPS/COM/NAV/GS Interfaced to KI-525A Garmin GTX-327 Transponder w/ Trans-Call SSD-120 Blind Encoder Honeywell KY-196A Comm Honeywell KCS-55A Compass System w/ KI-525 HSI Honeywell KR-87 ADF w/ KI-227 Indicator Pointer 4000-10 ELT w/ Remote Switch ACCESSORIES Air Comm Air Conditioner with Dual Forward Evaporators, Heater & Chin Bubble Defroster 5 Door Automatic Door Opener Preflight Kit (Includes 4 step handles Left and Right and Folding Maintenance Step) Baggage Spacemaker Cabin Floor Protector Alpine TDM-758 Cassette/CD Control w/ Alpine CHM-S630 – 6-Disc Changer Speakers Mounted in Hat Bin & Vertical Tunnel 7x David Clarke H10-13H Headsets Aircraft Offered Subject to Prior Sale or Withdrawal from Market. Specifications Subject to Verification by Buyer. AIRFRAME - Cabin: Bonded aluminum honeycomb, and semi-monocoque structure with composite side panels and aft fuselage skins - Doors (5): One hinged double door & copilot door on left side, pilot and passengers on right side, aft doors are composite material - Landing Gear: Tubular skid type with replaceable skid shoes - Locks for Cabin doors and luggage compartment - Luggage compartment (16 cu ft, 250lbs capacity) with composite door - Provisions for mooring, jacking and single point lifting - Tail boom: Monocoque structure with vertical fin and fixed stabilizer - Tail Skid (tail rotor guard) - Windows (except windshield): gray tinted plexi-glass INTERIOR - Interior with soundproofing, carpeting, and data case - Shoulder harnesses, dual straps in cockpit, single strap in cabin - Fire Extinguisher - First Aid Kit - Parcel Shelf (behind aft seat) - Ram air ventilation system - Storage area behind pilot & copilot seats POWERPLANT - Rolls-Royce Model 250-C47B gas turboshaft engine with FADEC and Direct Reversion to Manual Governor - Fuel Pump, engine driven - Fuel Pumps (4 canister type) w/ 2 boost pumps submerged in main tank, and 2 transfer pumps in forward fuel tanks - Fuel System: 127.8 gal usable capacity - Oil System: 1.5 gal capacity with sight glass - Compressor wash provisions - Engine mounted 10-micron oil filter - Airframe Fuel Filter (eliminates requirement for PRIST) ROTORS and CONTROLS - Main Rotor: soft in plane flex beam hub with four fiberglass blades - Tail Rotor: two fiberglass blades, semi-rigid - Hydraulic boost system for Main and Tail Rotor (separate pump and reservoir) - Mechanical flight control linkages throughout - Airspeed Activated Pedal Stop (AAPS) with built in test function, electrical override release switch and manual override release Aircraft Offered Subject to Prior Sale or Withdrawal from Market. Specifications Subject to Verification by Buyer. TRANSMISSION DRIVE SYSTEM - Soft mounted pylon isolation system - Freewheeling unit (between engine and main transmission) - Kaflex input drive shaft - Gearbox, tail rotor, 90° reduction - Main Transmission - Oil cooler - Oil filter with replaceable type cartridge - Oil pump, constant pressure ELECTRICAL - 28 volt DC system - Battery, 17 amp-hr nickel cadmium - External power and grounding receptacle - Starter-generator (180 ampere) - Solid state voltage regulator - 28 volt outlet in cabin - Heated pitot tube & static ports LIGHTS - Anticollision Strobe - Cockpit/map - Instrument - Aft cabin - Landing (two 250 watt) - Position MISCELLANEOUS - Engine inlet and exhaust stack covers - Pitot tube covers - Flight bag - Ground handling wheels with lift tube - Tiedown assemblies, main rotor and tail rotor Aircraft Offered Subject to Prior Sale or Withdrawal from Market. Specifications Subject to Verification by Buyer. Aircraft Offered Subject to Prior Sale or Withdrawal from Market. Specifications Subject to Verification by Buyer. Aircraft Offered Subject to Prior Sale or Withdrawal from Market. Specifications Subject to Verification by Buyer.

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3#
发表于 2010-11-26 15:25:45 |只看该作者
看看的哦 谢谢楼主

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