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1993
Antonov
AN-74d vip
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Registration No:
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Location: Ukraine
Price:
6200000
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Listing No: AI0169013784
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Pictures:
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Listing #:
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AI0169013784 |
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Make:
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Antonov |
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Model:
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Code or name:
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AN-74d vip |
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Year:
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1993 |
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Aircraft Total Time:
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2996 |
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Engine Time:
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3020 |
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Price:
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6200000 |
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Location:
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Ukraine |
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Registration:
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Airframe Description and
Additional Equipment:
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General characteristics
Crew:2-3
Capacity: 17 passengers
Length: 26.58 m (87 ft 2 in)
Wingspan: 25.83 m (84 ft 9 in)
Height: 8.24 m (27 ft 0 in)
Wing area: 98.62 m |
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Engine:
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Engines have the certificate of type "On noise on locality" on accordance to the requirements of Convention about international civil aviation.
On an airplane the undercarriage of high ability travel to cross-country, executed on a three-point chart, is applied (base of a 8,677 meter, track of a 4,094 meter). The radius of turn of airplane is 12 meters. |
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Avionics:
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The modern complex of pilotage-navigation and radio electronic equipment allows to work with the domestic and foreign second radio-locators of the systems of DME and TAKAN. The apparatus of navigation and landing can adopt the signals of the ground radio beacons of the system of VOR, landing radio beacons of the international system of ILS and systems as SP. |
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Interior:
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White natural skin and mahogany.
Two salons have for the VIP passengers with a sofa and by folding tables and one salon on 8 accompanying. Door- ladder, is closed from gidrosistem of airplane. Two rest rooms for VIP
passengers and accompanying., 2 kitchens, cloak-rooms, audyo- videoequipment, oxygen equipment, are AKB-17 UM.
Equipped and sufferet to international flights (CAS- 67A, RLN-90B, ARM-406p, ARM-406ac). |
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Exterior:
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White and blue or any by order |
Maintenance
Inspections
Certifications:
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After repair 2007 with the complete TBO resource
a resource 10000 hours or 12 years to the nearest repair of airplane.
Engines are 6000 hours or 7 years |
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Contact Information:
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Message from Seller:
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An unusual design feature of the An-72 and An-74 is the use of the Coanda effect to improve STOL performance, utilizing engine exhaust gases blown over the wing's upper surface to boost lift.
It was designed as a STOL .Min distance 350 m. |
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Posted:
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2007-02-28 |
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