OFFER#

MI-34C HELICOPTER

TYPE:	Helicopter
DESCRIPTION:	Mi-34C Helicopter
PRICE:	Upon Request
PACKING:	Ex-works

MI-34C HELICOPTER

PRINCIPAL DIMENSIONS

HELICOPTER LENGTH: 11.40m

HELICOPTER HEIGHT ACROSS MAIN ROTOR HUB: 2.75m

HELICOPTER HEIGHT ACROSS STABILIZER: 2.45m

DIAMETER OF MAIN ROTOR: 10,00m

DIAMETER OF TAIL ROTOR: 1.48m

FUSELAGE LOWEST POINT TO THE GROUND: 0.36m

MAXIMUM FUSELAGE WIDTH: 1.42m

TRACK OF SKID LANDING GEAR: 2.22m

HEIGHT OF THE COCKPIT DOORWAY: 1.15m

WIDTH OF COCKPIT DOORWAY: 0.70m

PERFORMANCE

MAXIMUM TAKE-OFF MASS: 1450kg

HELICOPTER EMPTY MASS: 1010kg

CRUISE SPEED ( UP TO 500m ): 170km/h

MAXIMUM SPEED: 225km/h

MAXIMUM RANGE ( STANDARD FUEL TANKS ): 420km

FLIGHT DURATION: 2h 26min

RATE OF CLIMB: 90km/h

TIME TO CLIMB 1000m: 3mintes

RATE OF DESCENT: up to 7m/s

MAXIMUM FLIGHT ALTITUDE: 5000m

Mi-34C are issued with three (3) certificates

Interstate Aviation Committee Aviation Register

Mi-34C Helicopter Type Certificate No 72 – 34C

M-14B26B Engine Type Certificate No 71 –D

APPLICATION

LIGHT , ALL PURPOSE Mi-34C HAS BEEN DESIGNED FOR TRANSORTATION OF PILOT + 3 PASSENGERS OR CARGO.

DUE TO THE Mi-34’s SPECIAL CAPABILITY OF USING NORMAL GASOLINE, MAKES IT IDEAL FOR TERRITORIAL PATROLLING , POLICE, CUSTOMS , OR SPECIAL FORCES ACTIVITIES.

DESIGN

Mi-34C HELICOPTER IS MANUFACTURED TO SINGLE ROTOR AND TAIL ROTOR SPECIFICATIONS. TAIL ROTOR IS DOUBLE – BLADED, AND ALL ROTORS ARE MADE FROM LATEST COMPOSITE MATERIALS. MAIN ROTOR HUB IS EQUIPPED WITH TORSION BARS, HYDRAULIC AND ELASTOMER DAMPERS. SWASH – PLATE IS WITHOUT A SLIDE OR UNIVERSAL JOINT TO THE GEAR BOX CASING. SKID – TYPE LANDING GEAR. THE COCKPIT IS DESIGNED FOR ONE PILOT AND THREE PASSENGERS, AND CAN PERFORM A LANDING IN AUTO-ROTATION MODE. ROBUST THROUGHOUT, THE Mi-34 CAN STAND AN OVERLOAD UP TO 3g ( SI units = 9.806 65m/s ² )

POWER PLANT

Mi-34C IS POWERED BY ONE M-14B26B PISTON ENGINE, FOUR STROKE, PETROL, NINE CYLINDER, AIR COOLED, CARBURETOR MIXING. THE TAKE –OFF ENGINE POWER IN ISA CONDITIONS IS 325/370 hp. THE ENGINE HAS A DOUBLE-CHARGING SYSTEM, PNEUMATIC STARTING, PNEUMATIC LUBRICATION, COMBINED CLUTCH FOR SMOOTH ROTATION OF THE MAIN ROTOR, AND TAIL CLUTCH WITH TRASMISSION GEAR; AUTO ENGINE INTERRUPTION IN CASE OF ENGINE FAILURE.

FUEL AND OIL SYSTEMS

FUEL: AVIATION GASOLINE 91/115, 100LL, 100; AUTOMOBILE GASOLINE SUPER TO USA STANDARDS ASTM-D 4814; GASOLINE GRADE TO EUROPEAN STANDARDS EN228. FUEL TANK CAPACITY IS 132kg OR 176litres. FUEL CONSUMPTION PER HOUR IN HOVERING MODE OVER LANDING AREA –75kg (100L), TAKE OFF MASS IS 1450kg. FUEL CONSUMPTION PER HOUR HORIZONTAL FLIGHT AT ALTITUDE OF 500m –51kg (68L) FUEL CONSUMPTION PER KM OF HORIZONTAL FLIGHT AT AN ALTITUDE OF 500m – 0.32kg/km ( 0.43l/km ) FUEL RESERVE IS 6.5kg (8.7L)

OIL IS AVIATION OIL MC-20, AERO SHELL 100, ESSO AVIATION OIL 100 INSTRUMENT & POWER SUPPLY EQUIPMENT.

Mi-34C IS EQUIPPED WITH ALL STANDARD INSTRUMENTS, RADIO AND NAVIGATION EQUIPMENT: GRYO HORIZON –AGR-29 – SPEED INDICATOR US-350K – ALTIMETER VM-15PV – VERTICAL SPEED INDICATOR VAR-30MK – MAGNETIC COMPASS KI-13K – OVERLOAD INDICATOR ADP-4, TALKS UNIT SPU-9, RADIO-ALTIMETER A-037, AUTO RADIO COMPASS ARK-22, HORIZONTAL SITUATION INDICATOR, HEADING SYSTEM, ULTRA SHORT WAVE RADIO UNIT, FLIGHT INFORMATION REGISTER BUR-4, ETC

GENERATOR = 27v @ 3kwt CAPACITY + 115v @ 400 HERTZ + 3-PHASE @

36v @ 400 HTZ . BATTERY 24vDC @ 17 a/h FOR 15min .

APPLICATION

LIGHT , ALL PURPOSE Mi-34C HAS BEEN DESIGNED FOR TRANSORTATION OF PILOT + 3 PASSENGERS OR CARGO.

DUE TO THE Mi-34’s SPECIAL CAPABILITY OF USING NORMAL GASOLINE, MAKES IT IDEAL FOR TERRITORIAL PATROLLING, POLICE , CUSTOMS, OR SPECIAL FORCES ACTIVITIES.

DESIGN

SERVICE

Can operate anywhere on helipads 20mX20m , with a parking area of 11.5mX11.5m , in temperatures -35°C to +45°C. Inspection every 50hours and scheduled maintenance every 100/200 & 400hours. Calendar service life is 25 years with helicopter life of 5000hours. Engine life is 2500 hours and components 3000hours. Depending on fuel prices, operating costs are under $200/hour.

PORTABILITY

Mi-34C can be assembled from any heavy lift cargo aircraft (AN12-IL76- AN124) ready for flight in 20 minutes .

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 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.
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GENERAL EQUIPMENT INC.