GENERAL   EQUIPMENT   INC.                    

 

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Miami FL 33173 USA                                  

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AN12

 

 

TYPE:

Aircraft

DESCRIPTION:

Antonov AN-12 for Sale

PRICE:

Upon Request

PACKING:

Ex-Works

 

 

antonov an-12 for sale

 

 

 

 

Tactical transport

Powerplants: An-12BP - Four 2985kW (4000ehp) Ivchenko (now Progress) Al-20K turboprops, driving four blade constant speed propellers.

Performance: An-12BP - Max speed 777km/h (420kt), max cruising speed 670km/h (360kt). Max initial rate of climb 1970ft/min. Service ceiling 33,465ft. Takeoff run at max takeoff weight 700m (2296ft). Range with max fuel 5700km (3075nm), range with max payload 3600km (1940nm).

Weights: An-12BP - Empty 28,000kg (61,728lb), max takeoff 61,000kg (134,480lb).

Dimensions: An-12BP - Wing span 38.00m (124ft 8in), length 33.10m (108ft 7in), height 10.53m (34ft 7in). Wing area 121.7m^2 (131.0sq ft).

Accommodation: Flightcrew of two pilots, flight engineer, navigator (in glazed nose) and radio operator, plus loadmasters. Can carry up to 20 tonnes (44,060lb).

Various special missions variants of the An-12 have been developed, but details on these aircraft are sketchy. Many aircraft have been converted for Elint, festooned with various antennas, and these are covered by the NATO designations 'Cub-A!, and 'Cub-B', while the 'Cub C' and more recent 'Cub-D' are ECM aircraft. Unconfirmed reports have suggested the development of a command post variant, while others have been used for research and development tasks.

 

 

Max Take Off Weight: 61,000kg 141,090lb
Max Landing Weight: 58,000kg 127,870lb
Max Zero Fuel Weight: 48,000kg 105,790lb
Structural Payload: 44,090kg 20,000lb
Fuel Capacity: 21,000kg 46,295lb
Main Deck Useable Volume: 97m3 285ft3 4in3
Cargo Area Width: 3.5m 11ft 5in
Cargo Area Height: 2.6m 8ft 6in
Main Cargo Door Width: 2.95m 9ft 8in
Main Cargo Door Height: 2.6m 8ft 6in
Wing Span: 38m 124ft 8in
Overall Length: 33.1m 108ft 7in
Overall Height: 10.5m 34ft 6in

 

 

 

We are in a position to propose for supply АN-12BK Aircraft ser. No. 7345208, date of manufacture 30.09.1967.

TTL 13500 hrs, 7900 landings, 40 years 07 months;

TBO - 6000 hrs, 3000 landings, 17 years 08 months.

 

Flight hrs / landings of the Aircraft and its components: 

Since new   11026 hrs, 7111 landings, 

After last OH  - 4913 hrs, 2100 landings.

 

AC overhauls: total Qty-3, date of last OH 10.08.1990.

 

Completeness of the aircraft (navigation, avionics and other equipment): 

Aircraft is equipped with standard equipment in accordance with serial plant complete set. Additionally the aircraft is equipped for flights on international routes 

Additionally following equipment is installed:

       - air collision avoidance system TCAS-II version 7.0;

       - satellite navigation system KLN-90B;

       - bank control system БКК-18;

       - command-control units КPP-75С (2 pcs.);

       - radio-stations R-863 are modified for frequency grid  8.33 kHz;

       - КURS-МP-2  system is modified for protection from FM interference and for 40 channels;

       - emergency beacons   АРМ-406P, АРМ-406АС1 of КОSPAS-SARSAT system;

       - Early ground proximity warning system along flight direction EGPWS.

 

Aircraft is positioned in Ukraine at Overhaul Plant. Servicing / maintenance will be fulfilled after signing of the contract. 

Aircraft will be supplied in flying condition with documents certifying one year of Airworthiness. 

Delivery schedule: 04 months after advance payment. 

 

 

Specification and photos are not contractual and are subject to verification upon inspection

 

 

NB: Aircraft offered for sale subject to contract, prior sale, withdrawal from the market and information regarding any aircraft or helicopter and provided verbally or in written documentation and/or contained within this e.mail or associated paper-work should be taken as a guide only in determining the suitability, including that aircraft or helicopters specification and/or performance.  We highly recommend that any buyer or lessee perform their own inspections and due diligence to verify any and all technical, performance and specification information contained therein including OEM claims.

 

PLEASE NOTE: AIRCRAFT SPECIFICATIONS SUBJECT TO VERIFICATION UPON INSPECTION. WE DO NOT ACCEPT ANY LIABILITY FOR AIRCRAFT DEFECTS, HISTORY OR TECHNICAL RECORD ERRORS. IT IS THE BUYERS RESPONSIBILITY TO INDEPENDENTLY VERIFY THE AIRCRAFT AND COMPONENT HISTORY.

 

 

 

 

TAKE NOTICE!

 

PLEASE BE ADVISED THAT INFORMATION INCLUDED IS CONFIDENTIAL IN NATURE AND IS BASED ON PREXISTING BUSINESS RELATIONSHIP WITH THE LEGAL OWNER OF PROPERTY DESCRIBED HEREIN (IF APPLICABLE). AS SUCH, UPON RECEIPT OF SAID INFORMATION THE RECEIVER AKNOWLEDGES THAT ANY UNAUTHORIZED CONTACT WITH SAID LEGAL SELLER WILL BE CHARACTERIZED AS A BREACH OF CONFIDENTIALITY AND SAID AGREEMENT MAY BE ENFORCED UNDER EXISTING LAW OR IN EQUITY.

 

This paper was prepared by General Equipment Corp.
The paper represents an offer of a partner of General Equipment Corp.
All rights are reserved by and for General Equipment Corp..
All content and ideas of this paper are the property of General Equipment Corp.