Register
    2004 CHRISTEN EAGLE II N-NUMBER N921DM2004 CHRISTEN EAGLE II N-NUMBER N921DM
    Photos(5)
    N921DM - 2004 CHRISTEN EAGLE II

    This listing is currently not for sale or available for charter
    See Similar Aircraft For Sale On
    See Similar Aircraft For Charter On
    See Aircraft Operating Costs On
    Aircraft Cost Calculator


    Aircraft Summary

    General
    Year
    2004
    Manufacturer
    CHRISTEN
    Model
    EAGLE II
    Serial Number
    921
    Registration #
    N921DM
    Condition
    Used
    Description
    Great condition Christen Eagle II which was hangared its whole life. No damage history. No hard aerobatics. Engine was overhauled by Zepher Engines in 2004 and a new aerobatic crankshaft was installed at that time. Propeller was overhauled in 2012 by New England Propeller 
    Airframe
    Total Time
    195.2
    Airframe Notes
    TT: 195.2
Empty Weight: 1085 lbs
Gross Weight:  1600 lbs
    Engine
    Engine Notes
    Lycoming AEIO 360 A1D  
Serial Number: L-9152-51A
Engine TT: 2244.2
Engine TSMO: 195.2
Overhaul Date: 2004 Zepher Engines
    Props
    Prop Notes
    Prop TT: 195.2
Prop TSMO: 50.6
Recent Overhaul 6/15/2012 New England Propeller
    Avionics
    Avionics/Radios
    ICOM IC-A210 Radio
Garmin GTX 320A Transponder
TS Engineering TM 1000 Intercom
    Exterior
    Exterior Notes
    9/10 Great condition
    Inspection Status
    Inspection Status
    Current now. To include a fresh Annual with sale

Specifications and Performance
Engine…………………………………………Lycoming AE10-360-A1D, 200 hp
Propeller……………..…………..Hartzell HC-C2YK-4/C7666A-2 constant speed
Empty Weight……….………………...1025 lbs with electrical, radio, and canopy
Gross Weight…………..…...….………………..………………………...1578 lbs.
Competition Weight.………………………………….1290 lbs. (with 190 lb pilot)
Useful Load………….………………………………………..……………553 lbs.
Baggage Allowance…..…………...………………….………………..…….30 lbs.
Fuel Capacity……………………………………………………………..…25 gal.
Length………………………………...….…………………………..…17 ft. 11 in.
Span…………….………………....……..…………..…………………19 ft. 11 in.
Height…………………….……………………………………………….6 ft. 6 in.
Wing Area……………………………....……………..…………………125 sq. ft.
Wing Loading (gross weight).………...…..………………………..12.62 lb./sq. ft.
Power Loading (empty weight)……..………..…………..……………..5.13 lb./hp
Structural Limits (gross weight)..……….…………………….+9g, -6g operational
Top Speed…………………………………………………...…………….184 mph
Cruise Speed…………………………….…………...……………...…….165 mph
Stall Speed………………………………….………………………………58 mph
Never Exceed Speed……………...……………………………………….210 mph
Rate of Climb…………………………..………….…………………..…2100 fpm
Roll Rate……………………………………..………….………….…187 deg/sec.
Vertical Penetration………………………………..…….…………………1250 ft.
Range………………………………………..………….………………..…380 mi.
Inverted Flight Time...…..……………………………………..………...Unlimited


    Click Here to find your Operating Cost


    Aircraft.com does not own the rights to the images displayed on this site. We do not have information regarding the original seller or source of these images unless explicitly stated.