OFFER#

MD 500

TYPE:	Helicopter
DESCRIPTION:	MD 500 Helicopter, From New Production
PRICE:	Upon Request
PACKING:	Upon Request

MD 500 HELICOPTER FROM NEW PRODUCTION

STANDARD AIRCRAFT SPECIFICATIONS

Type:	MD500 (Hughes 369D) Helicopter
Type Engine:	Allison 250-C20B turbo shaft 420 Horsepower
Crew:	1 pilot and up to 3 Scientists/Technicians
Service Ceiling:	12,500 feet (without supplemental oxygen) 16,000 feet (with supplemental oxygen)
Airspeed:	Hover to 156 knots
Max. Gross weight:	3,000 pounds (1361 kilograms)
Empty Weight:	1550 pounds (703 kilograms)
Useful Load:	1450 pounds (658 kilograms) (fuel, personnel, and cargo)
Fuel Load:	400 pounds (60 gallons) - standard fuel load 160 pounds (25 gallons) - additional capability with the addition of one auxiliary fuel tank
Type Fuel:	Jet A, Jet B, JP4, JP8
Fuel Burn Rate:	180 pounds/hour (~28 gallons/hour)
Range (normal):	225 Nautical miles ~2.2 hours @110 knots
Range (w/aux. fuel):	300 Nautical miles ~2.8 hours @110 knots
Dimensions (external):	Main rotor span - 26.41 feet Total length - 30.84 feet Tail height - 8.9 feet
Dimensions (internal):	42" Long x 42" Wide x 36" High
Useable Volumes:	Cabin - 30 cubic feet
Navigation:	GPS receiver Radar Altimeter VOR with DME Automatic Direction Finder (ADF)
Communication:	Two VHF Radios (117-135 Megahertz) Marine Band FM/VHF Radio (150-174 Megahertz) Transponder with Mode C Intercom System

Additional Equipment/Capabilities:

Cargo Hook for external loads up to 1000 pounds
Emergency Pop-out Floats for over-water operations
High skid gear for underslung equipment
belly to ground clearance- 2.4 feet
Helicopter is transportable on cargo airplane
Passenger compartment work station (table) with:
12volt DC laptop computer power supply
Digital Radar Altimeter readout and RS232 computer drop
Magnetic compass
Digital Timer
GPS aircraft position readout and RS232 computer drop (Latitude/Longitude)
Crew and Cabin Doors removable

Drawing of MD500 (Hughes 369D) Helicopter

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 email 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 PRE-EXISTING BUSINESS RELATIONSHIP WITH THE LEGAL OWNER OF PROPERTY DESCRIBED HEREIN (IF APPLICABLE). AS SUCH, UPON RECEIPT OF SAID INFORMATION THE RECEIVER ACKNOWLEDGES 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.

GENERAL EQUIPMENT INC.