OFFER#

SW205

TYPE:	Helicopter
DESCRIPTION:	SW205 HP Helicopter With T53-L-703 Engine
PRICE:	Upon Request
PACKING:	Ex-Works

SW205 HP HELICOPTER WITH T53-L-703 ENGINE

Aircraft Model: SW205

Certification: DR Standard Transport Category Airworthiness Certificate

Production Certificate: HI-101

TCDS: H6SO

Engine Model: T53-L-703

Engine Hours: TBO: 3500 TSO: 0.0

NEW: Soundproofing, Battery (Lead Acid), Seat Covers, Seat Belts, Fire Extinguisher, Windows

MID-TIME: 212 Main Rotor Blades & 212 Tail Rotor Blades

OVERHAULED: Power-train components

ALL current applicable A.D.’s, complied with
Current Annual Inspection	Transponder
Vertical Fin Spar Kit	VHF/NAV Radio
New Single Stage Paint	Dual Flight Controls
Utility Seating Configuration	Wire Strike Kit
Door Struts	KAFLEX Main Driveshaft
Dual Hydraulics	6000 lbs. On-board Cargo Hook Kit
212 Stabilizer Bar Tubes	212 Transmission, 42° Gearbox, Nose
GPS

Standard Aircraft Exterior Dimensions:

Length, fuselage, ft (m)	42.39 (12.92)	Width, fuselage, ft (m)	8.00 (2.44)
Length, T/R turning, ft (m)	42.39 (12.92)	Width, widest point, ft (m)	8.00 (2.44)
Length, both turning, ft (m)	42.39 (12.92)	Width, landing gear, ft (m)	8.00 (2.44)
Height, top, rotor hub, ft (m)	14.39 (4.390)	Gr clearance, fuselage, ft (m)	1.18 (0.36)
Height, top, T/R arc, ft (m)	14.39 (4.390)	Gr clearance, T/R, ft (m)	NA (NA)

Standard Aircraft Interior Dimensions:

Cabin

Length, max, ft (m)	7.67 (2.33)	Width	8.00 (2.44)
Height, max, ft (m)	4.33 (1.32)	Volume, ft³ (m³)	200.00 (6.32)

Standard Aircraft Weights: (Typical)

Max gross, lbs (kg)	11,200 (5080)	Empty, std acft, lbs (kg)	4,840 (2200)
Useful load, lbs (kg)	5,660 (2573)	Useful, with full fuel, lbs (kg)	4,220 (1918)
External load, lbs (kg)	6,000 (2727)	Gross with ext load, lbs (kg)	11,200 (5080)

SW205HP WITH T53-L-703 ENGINE

TAKEOFF AND LANDING GROSS WEIGHT

VERSUS

AMBIENT AIR TEMPERATURE AND PRESSURE ALTITUDE

AMBIENT AIR TEMPERATURE- °C

WEIGHT– ALTITUDE– TEMPERATURE

LIMITATIONS FOR TAKEOFF AND LANDING

See details at:

SWFA SW205 SN 8976 CAMEROON.pdf

SWFA SW205 SN 4374 (1).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 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 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.

GENERAL EQUIPMENT INC.