GENERAL EQUIPMENT INC.

8770 Sunset Drive #191 ● Miami FL 33173 · USA

Tel: +1 305 468 4650 +33 6 68 96 24 99 · Fax: +1 360 937 2965 +33 8 21 46 30 77

Email: info@generalequipment.info ● www.generalequipment.info

TYPE:	Aircraft
DESCRIPTION:	Antonov AN-26 for Sale
PRICE:	Upon Request
PACKING:	Ex-Works

Tactical transport

Powerplants: An-26B -Two 2075kW (2780ehp) ZMKB Progress (formerly Ivchenko) Al-24VT turboprops driving four blade propellers, and one auxiliary 7.85kN (1765lb) Soyuz (formerly Tumansky) RU-19A300 turbojet. An-32 - Two 3760kW (5042ehp) ZMKB Progress Al-20D Series 5 turboprops.

Performance: An-26B - Cruising speed 435km/h (235kt). Max initial rate of climb 1575ft/min. Takeoff run on sealed runway 870m (2855ft). Range with max payload and no reserves 1240km (670nm), range with max fuel and no reserves 2660km (1435nm).

Weights: An-26B - Empty 15,850kg (34,943lb), max takeoff 24,000kg (52,910lb). An-32 - Empty 16,800kg (37,038lb), max takeoff 27,000kg (59,525lb).

Dimensions: An-24B - Wing span 29.20m (95ft 2in), length 23.80m (78ft 1in), height 8.58m (28ft 2in). Wing area 75.0m^2 (807.1sq ft). An-32 - Wing span 23.78m (78ft 0in), length 23.80m (78ft 1in), height 8.75m (28ft 9in). Wing area 75.0m^2 (807.1sq ft).

Accommodation: An-24B - Flight crew of two pilots, flight engineer, navigator and radio operator, plus loadmaster. Seating for up to 40 troops or 24 stretcher patients.

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.

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.

Max Take Off Weight:	24,000kg 52,911lb
Max Landing Weight:	24,000kg 52,911lb
Max Zero Fuel Weight:	20,250kg 44,640lb
Structural Payload:	5,500kg 12,125lb
Main Deck Useable Volume:	50m³ 147ft³ 2in³
Wing Span:	29.2m 95ft 9in
Overall Length:	23.8m 78ft 1in
Overall Height:	8.5m 28ft 1in