N425MF - 1977 CESSNA 421C TURBINE
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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