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                                                       

 

 

 

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 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

 

 

                                     

 

 

 

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 OWNER 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.