N425MF - 1977 CESSNA 421C TURBINE


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    Aircraft Summary


    General

    Year
    1977
    Manufacturer
    CESSNA
    Model
    421C TURBINE
    Serial Number
    0270
    Condition
    Used
    Registration #
    N425MF
    FlightRules
    IFR
    Description
    PRISTNE CORPORATE CESSNA 421-C CONQUEST I CONVERSION. ALL THE SPEED, PERFORMANCE, SAFETY, COMFORT AND ECONOMICS. 260 +kts @ 65 gph=1200nm. 4578 TT w/ 618 / 618 SMOH, 3500TBO. 100% Unscheduled Maintenance Protection Plan. Garmin GNS530 & GNS430, weather data Link. TAWS, WX 1000. Fresh Annual 2/2008 Eagle Aviation. Call for Details Available $ 895,000.00. 421C Turbine Eagle Conquest I, Pratt Engines 260 kts@65gph. Speed, Comfort, Safety

    Airframe

    Total Time
    4578.0
    Airframe Notes
    * 4,578 Hours Total Time Since New * No Known Damage History * Corporately Owned & Operated. * Excellent Condition Annual 2/20067, Eagle Aviation. * Engines Boroscope 12/2005 excellent condition.

    Engine Program

    Engine Program Notes
    Engine Specs: ENGINES: Pratt & Whitney PT6A-112 Engines with 3,500 Hr TB0's: * Only 618 Hours SMOH by Standard Aero (October 2000) * Left Engine s/n: PCE-12061 * Right Engine s/n: PCE-12063

    Engine 1

    Engine 1 Time
    618
    Engine 1 Time Since
    SMOH

    Engine 2

    Engine 2 Time
    618
    Engine 2 Time Since
    SMOH

    Props

    Prop Notes
    Hartzell Three-Blade, Fully Feathering: * 178 Hours SPOH w/New Hubs (no recurring inspection) 2/16/2006.

    Avionics

    Avionics/Radios
    Garmin Avionics Package: w/Garmin 530/330, Garmin GNS 430! * Audio Panel: King KMA-24 w/3-Light Marker Beacon * Comm #1: Garmin GNS530 * Comm #2: Garmin GNS430 * Nav #1: Garmin GNS530 * Nav #2: King KNS-80 w/King KI-209 (2nd GS) * Autopilot: Cessna/Sperry 800 IFCS w/Altitude Alerter & Preselect (overhauled by Autopilots Central July 2003) * L/Range Nav #1: Garmin GNS530 GPS/MFD * L/Range Nav #2: Garmin GNS430 * L/Range Nav #2: King KNS-80 RNAV/VOR/DME * DME #1: Garmin GNS530 * DME #2: King KNS-80 * Radar Alt: Cessna * RMI: King KI-229 Dual Needlew/rem. switching, * WX Radar: Bendix RDR-160 Color Radar * Xpdr #1: Garmin GTX-330 w/TIS * Xpdr #2: KT-76C * WX Avoidance: BFGoodrich WX1000 Stormscope * TAWS: Garmin GNS530 "Class B" * Altimeter: EA-801A Encoding Altimeter * Marker Beacons: KR-21 Marker Beacon * Davtron Dig. Clock and Timer * Instrument Panel Nu Lite

    Additional Equipment

    Additional Equipment
    Lots of Extras! * WSI Datalink Weather * Oregon Aero Pilot & Copilot Seats * K-Ice Certified w/Glass Pilot's Windshield * Propeller Synch * Micro Aerodynamics VG's * Aft Flushing Lav Seat w/Seatbelt * Shadin Digiflo-L Fuel Computer * 11.0 Cubic Foot Supplemental Oxygen * Foxboro Fuel Totalizer * Complete Copilot Instruments * 5.0 PSI Cabin w/Variable Rate Controller * Lead Acid Battery * JB Electric Air Conditioning * LH & RH Executive Writing Tables * 347-Gallon Long Range Fuel * Electroluminescent Cockpit * Nu Lite System for Panel Lighting

    Exterior

    Year Painted
    2003
    Exterior Notes
    The Exterior looks nearly new and is completed in a RAM scheme in overall Matterhorn White over Navy Blue with Gold Laser Stripe. Completed in 1999 by Cheyenne Air motive - Looks Like New!

    Interior

    Year Interior
    2003
    Number of Seats
    7
    Interior Notes
    The Six-Passenger Interior features four (4) Champagne Leather Seats in club Configuration, one (1) aft fwd-facing seat completed in Champagne Leather and one (1) aft/belted flushing toilet. Medium blue carpeting and cockpit compliments the patterned wool sidepanels and Oyster headliner. The Refreshment Center includes an ice storage drawer, a large dry storage locker and overhead storage compartment. Completed in 1999 by Cheyenne Airmotive it is in Very Good Condition! Refurbished 2/2006.

    Modifications/Conversions

    Modifications/Conversions
    Riley International "Turbine Eagle" Conversion utilizing Pratt & Whitney Canada PT6A-112 Engines: Performance Data: * Maximum Gross Weight: 7,629 lb. * Empty Weight: 5,216 lb. * Maximum Fuel: 2,298 lb. (343 US gallons/4.9-hours with 30-min. reserve, range 1,298 nm w/ reserves) * Fuel Burn @ Max Cruise: 210-220 lb./hour/engine (62-66 US gallons total/hour) * Fuel Burn @ L/Range Cruise: 150-155 lb./hour/engine (45-46 US gallons total/hour) Normal Cruise Speed: 255-278 KTAS @ FL190-FL270 Takeoff Distance(s) over 50’ Obstacle: * (Sea Level, ISA/59F, Max Gross Wt.) 2,277’ * (4,000’, ISA+20/65F, Max Gross Wt.) 2,958’ * (6,000’, ISA+20/58F, Max Gross Wt.) 3,295’ Landing Distance: * (Sea Level, ISA/59F, 7,200 lb.) 2,286’ * (4,000’, ISA+20/65F, 7,200 lb.) 2,618’ * (6,000’, ISA+20/58F, 7,200 lb.) 2,760’ Miscellaneous: * Date of Conversion: December 1982

    Inspection Status

    Inspection Status
    * Annual Inspection was completed May 2008 at Eagle Aviation, Columbia, S.C. * Props Overhauled 5 year item January 2006 “ 178 “ time with new style hubs. * New Co-Pilot's Windshield and Pilot's Storm Window were Installed in November 2003 and the remaining Cabin Windows were polished to remove all scratches. * The Pitot-Static & Transponder Certifications were completed 3/ 2006. * Missing Original Airframe log book from 1977-1981. Conversion done in 1982. Believe Log books were left at the conversion center


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