GENERAL   EQUIPMENT   INC.                    

 

8724 Sunset Drive #191Miami FL 33173 · USA                                  

                                                  
Email:
info@generalequipment.infowww.generalequipment.info                                                       


 

 

UH60A BLACKHAWK

 

 

TYPE:

Helicopter

DESCRIPTION:

UH60A Blackhawk

PRICE:

Upon Request

PACKING:

Ex Depot

 

 


S70A blackhawk

 

Subject Unsold or Market Withdrawal

 

 

Crew: 2 pilots (flight crew) with 2

crew chiefs/gunners

2,640 lb (1,200 kg) of cargo internally, including 11 troops or 6 stretchers, or 9,000 lb (4,100 kg) (UH-60L) of cargo externally

Capacity:

Length: 64 ft 10 in (19.76 m) Fuselage length: 50 ft 1 in (15.27 m)

Disc area: 2,260 ft² (210 m²)

Empty weight: 10,624 lb (4,819 kg) Max. takeoff weight: 23,500 lb (10,660 kg)

Rotational speed:

Engine 20,900 RPM, main rotor 258 RPM (gear ratio 81:1)[166]

Powerplant: 2 General Electric T700-

GE-701C turboshaft, 1,890 hp (1,410 kW) each

Fuselage width: 7 ft 9 in (2.36 m)

Rotor diameter: 53 ft 8 in (16.36 m) Height: 16 ft 10 in (5.1

 

See details at:



Sikorsky_Black_Hawk_S-70A KBM.pdf

 

 


 

1982 Sikorsky UH-60A Blackhawk

 

 

The Blackhawks are "N" Registered and in FAA Restricted Category.

 

Sale of the Blackhawks are subject to the US State Department approval.

 

See details at:

1982 Sikorsky UH-60A Blackhawk.pdf

N563DJ Component Report.pdf

N563DJ.pdf

N563DJ_AMS_Audit_.pdf

 

 

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 PRE-EXISTING 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 Inc.
The paper represents an offer of a partner of General Equipment Inc.
All rights are reserved by and for General Equipment Inc.
All content and ideas of this paper are the property of General Equipment Inc.

 

 


 

This transmission may include information on International Traffic in Arms Regulation (ITAR) (22 CFR-120-130) controlled items.  These controlled items may not be resold, diverted, transferred or transshipped outside of the United States or to any other country without U.S. State Department approval.

 

US State Department Arms License: K-5943

 

 

Defense items are subject to final destination approval and granting of an

export license issued by exporting country's authorities