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Contact


NORTH TEXAS
Larry Johnson
Phone 972-562-5555
Fax: 214-467-6067
ljohnson@cutteraviation.com

SOUTH TEXAS
John DeLawyer
Phone 210-601-5246
Fax: 210-340-8804
jdelawyer@cutteraviation.com

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Malibu Mirage

Mirage

Now Available

 

The Malibu Mirage keeps getting better.   2005 marks the 21st Anniversary of this revolutionary, one-of-a-kind aircraft.  There is no competitor to the true performance, luxury & joy of flying a Mirage.

Call us today to personalize your new Malibu Mirage!

PERFORMANCE SPECIFICATIONS

 

ENGINE
Manufacturer
Model
Horsepower
Number of Cylinders


Lycoming
TIO-540-AE2A
350 hp
6

PROPELLER
Manufacturer
Number of Blades
Type


Hartzell
3
Constant Speed

WEIGHTS
Maximum Takeoff Weight
Standard Empty Equipped Weight (b and c)
Standard Useful Load (a)


4340 lbs/1969 kg
3120 lbs/1415 kg
1220 lbs/553 kg

DIMENSIONS
Wing Span
Length
Height
Wing Area
Cabin Length
Cabin Width
Cabin Height
HEADROOM (Seat to Ceiling)
Front Seats
Middle Seats
Rear Seats


43 ft/13.1 m
28.9 ft/8.8 m
11.3 ft/3.4 m
175 ft2/16.25 m2
148 in/375.9 cm
49.5 in/125.7 cm
47.0 in/119.4 cm

38 in/96.5 cm
38 in/96.5 cm
37 in/94.0 cm

FUEL and OIL CAPACITY
Usable Fuel
Oil Capacity

BAGGAGE
Forward Compartment Capacity
Aft Compartment Capacity


120 gallons/454 liters
12 quarts/ 11.4 liters

100 lbs/45.4 100 lbs/45.4 kgs

MAXIMUM SPEED
TAS at mid-cruise weight
CRUISING SPEEDS
High Speed Cruise Power (TAS)
(Mid cruise weight, optimum altitude)
CRUISING RANGE
Long Range Cruise Power(IAS)
CCruising range includes 45 minute fuel reserve at long range power plus allowance for fuel used during taxi, take-off, climb at MCP, cruise at stated mixture and descent.


220 knots/408 km/h

213 knots/408 km/h

1345 nm/2491 km




STALL SPEED
Flaps Down Full 36 °
 SERVICE CEILING
100fpm
MAX DIFFERENTIAL PRESSURE
5.5 psid
TAKE-OFF DISTANCEbr> Ground Roll
Over 50 ft Obstacle (Flaps 20° Gross Weight)
LANDING DISTANCE
Ground Roll
TTotal over 50 ft Obstacle


58 knots/107 km/hh

*25,000 ft+/7620 m+


1,090 ft/332 m
2,090 ft/637 m

1,020 ft/311 m
1,960 ft/597 m

a. Standard useful load is maximum takeoff weight minus standard equipped weight.br> b. The standard empty weight and standard equipped weight are the same.
c. Standard equipped aircraft.

*25,000 ft is the maximum approved altitude.