Dear Sir,

We are pleased to offer you GE F9 Turbine Generators as per the following:

1-      Brand New never used GE F9

2-      These units are scheduled to be delivered to project which has been cancelled

3-      The units come with standard GE warranty & full factory support

4-      These units manufactured in Europe under GE license 

5-      First two units will be delivered out of factory end of Feb of 2008

6-      Another 18 units will be delivered end of June of 2008

7-      The bottom price for the units delivered end of Feb of 2008 is Euro $
34,000,000.00 each (Thirty Four Millions Euro), please be informed that 3-5% should be added if you place order.

8-      After signing the Non disclosure  Application the buyer and the manufacturer  can communicate directly

9-      If an installation and maintenance contract is needed �?please advise and we will provide a full engineering proposal after receipt of deposit

10-  The prices quoted exclude any Federal, State, or local taxes or fees, which may be associated with the purchase of equipment and/or services. No customs or VAT has been included.

11-  These units designed for high ambient temperatures.

12-  For detailed technical specifications please refer to the attached document.

We strongly believe this is an excellent opportunity to buy GE F9 units for the following reasons:

a-      Reduced Price, 15% less than GE price. GE confirmed that the price of New current production GE F9 Turbine Generators is Euro$ 40,000,000.00 each (Forty Million Euro)

b-      Short Delivery Time. GE confirmed that the delivery time for any new contract for GE F9 is 18- 24 month

c-      These units are very desirable and there is huge demand on such units.

Due to reduced price and short delivery time please note that there is very high demand on such units and usually does not last long, please let us know as soon as possible our further steps for completion of this deal.

If you have any questions or require additional information please contact.

Thank you,

Mohammad

COMMERCIAL OFFER

PRICE

The price of the 20 plants, equipment only is Euro 680,000,000.00 (Six Hundred eighty million Euro), 3-5% to be added when place order.

PAYMENT TERMS

• 25% With your appreciated Purchase order

• 75% With Ex works shipment

All payments to be made strictly as per payment schedule.

DELIVERY PERIOD

The Gas Turbine packages will be available end of Feb of 2008. The delivery schedule of the unit will be

formalized after finalization of Contract / Purchase Order and completing all contractual formalities.

TIME SCHEDULE

The schedule for various activities is based on previous experience. However the exact schedule

for each milestone will be provided upon finalization of project. The various activities/milestones

will commence simultaneously.

TITLE TO EQUIPMENT

Upon purchase of equipment from the existing owner, title to the Gas Turbine and associated

equipment will be immediately transferred to end purchaser/ owner. The equipment vendor will

still be responsible for insuring the equipment until delivery to nominated export port, but the end

purchaser/owner will hold secure Title to the units. All units and equipment will be insured during

transit to the site.

VALIDITY

Turbines and equipment are subject to prior sale and price is subject to change without notice.

FORCE MAJEURE

We shall neither be liable for loss, damage, detention or delay nor be deemed to be in default for

failure to perform when prevented from doing so by causes beyond its reasonable control

including but not limited to acts of war (declared or undeclared), Acts of God, fire, strike, labor

difficulties, acts or omissions of any governmental authority or of Purchaser, compliance with

government regulations, insurrection or riot, embargo, delays or shortages in transportation or

inability to obtain necessary labor, materials, or manufacturing facilities from usual sources or

from defects or delays in the performance of its suppliers or subcontractors due to any of the

foregoing enumerated causes. In the event of delay due to any such cause, the date of delivery

will be extended by period equal to the delay plus a reasonable time to resume production, and

the price will be adjusted to compensate PEW for such delay.

TAXES

No sales or use taxes have been included in this proposal. The prices quoted exclude any Federal,

State, or local taxes or fees, which may be associated with the purchase of equipment and/or

services. No customs or VAT has been included.

FIRM PRICE

The final price quoted is not subject to escalation during the quoted build cycle if a commitment is

made during the bid validity period. If the buyer delays payment or delivery, the price shall be

adjusted to reflect the cost of money during delay period until payment has been made current.

EXCLUSIONS

¨ All Statutory Clearances at client site, however the supporting documents like drawings, will

be provided by us

¨ Soil and Water Analysis Power studies (load flow, short circuit, stability)

¨ Clearance for Grid Paralleling (if the set has to be synchronized with the grid)

¨ Site visits

¨ Foundation piling, if necessary

INPUTS REQUIRED FROM THE CLIENT

¨ Water Analysis

¨ Site Plan (new location)

¨ Norms to be met for Pollution Control

¨ Details of Power Evacuation like Voltage level, Fault level, etc.

¨ Complete set of Drawings for the existing site

¨ Any other details required, to be discussed while post contract review and engineering

discussions.

GE Frame 9 Gas Turbine Packaged Power Plants

SCOPE, LIMITS AND EXCLUSION FROM THE SUPPLY

Scope of Supply

1. Gas turbine generator package

2. Mechanical

• Gas Turbine

• Air Compressor

• Combustors

• Turning and Reduction Gear

• Air Inlet facilities (Filters and Ducts)

• Exhaust facilities (Ducts, Silencer) (less exhaust elbow )

• Starting Motor system

• Dual Fuel Combustors

• Lube and Control Oil System

• Closed Circuit Cooling Water system

• Atomizing and Cleaning system

• Instrument Air system

• Enclosures, including HVAC, Fire-fighting, Electrical Switchboard for:

- Gas turbine unit (external and internal)

- Gas turbine auxiliaries

- Electrical Switchgear

- Control

- Closed Circuit auxiliaries

- Water Injection

• GT Supervision, Control and Protection Systems

• Fire Fighting (detection and protection) system

• Gas Detection system

• Thermal Insulation and Lagging

• Compressor Washing and Cleaning facilities

3. Electrical

• Electrical Generator, auxiliaries and related equipment (Circuit Breaker,

Grounding Switch, Bus duct, Neutral Grounding cubicle, etc.)

• Starting Motor system

• Unit Transformer (11/6 kV) and auxiliary MV/LV Transformers

• Main Switchboards (6 kV, 380 V PC, 380 MCC and emergency MCC) and MV

isolated bus ducts

• Auxiliary Switchboards (Generator Protection, HVAC, Fire-fighting, Lifting

facilities, etc)

• 110 DC Power System

• Uninterruptible Power System (UPS)

• AC/DC Electrical Motors (DC Motor starters included)

• Electrical Protection system

• Lighting and Motive Power system, Heat tracing, Grounding, etc.

• Cables and Cable Trays

4. Instrumentation & Controls

• On board Instrumentation

• Instrument Panels and Junction boxes

• Control, Protection and Monitoring Panels

• MMI (man-machine interface)

5. Miscellaneous

• Special Tools

• Anchor Bolts and Plates

• Stair and Ladders

• Steel Structures

6. Special Tools and Maintenance equipment (for the above mentioned machinery)

7. Operating and Maintenance Manuals

PERFORMANCES: SIMPLE CYCLE

The following Gas Turbine performances:

ISO Conditions

With reference to the following conditions:

Ambient Pressure: 1013 mbar

Ambient Temperature: 15 °C

Relative Humidity: 60 %

Gas Turbine Inlet/Exhaust Pressure drop: 89/127 mm H2O

The Plant Performances at Generator terminals when the plant is operated at GT new and

clean conditions shall be:

Base Load

Output Power: 126 MW

Heat Rate: 10096 BTU/KWh (10650 kJ/kWh) (natural gas)

Gas Turbine and Auxiliaries

Gas Turbine

General description

The PG9171(E) GT package was developed by a GE/ EUROPE authorized licensee with the

frame 9E as basic equipment and within the license agreement with General Electric Co.

(USA).

The PG9171(E) is a single shaft, high efficiency gas turbine for power generation in 50 Hz

grids, suitable for simple cycle and combined cycle application.

The engine is designed for 3000 rpm nominal speed, to be directly coupled to a two-pole

synchronous electric generator. This gas turbine unit includes all features and design solution

coming from the operating experience of the MS9000 family, whose evolution has brought to

the PG9161(E) one of its highest reliability value. The PG9161(E) unit consists of three

compartments, one housing the auxiliaries, one the gas turbine itself, and the last one housing

the exhaust plenum. Each compartment is equipped with access doors for easy site inspection

and maintenance. The rotor is a single shaft assembly consisting of one compressor rotor

joined to one turbine rotor by a flanged joint, and lays on three journal bearings (two elliptical

and one tilting pad type). Two thrust bearings; one Kingsbury type (loaded) and one tilting pad

type (unloaded) are also provided.

Compressor

The compressor rotor consists of 17 stages with 12.3/1 overall compression ratio. The

compressor rotor consists of 15 wheels, shrunk onto a forged shaft (rotor stages 2nd to 16th), two

stub shafts (1st and 17th rotor stages), 16 tie bolts and stator/rotor blades. The stationary blades

are assembled into two half rings (diaphragms) for each stage; the diaphragms are fitted into the

compressor casing. The rotating blades are fitted on the discs by dove-tail roots and fixed by

means of pins. The compressor external casing is totally made of grey cast iron. The compressor

front portion contains the Inlet Guide Vanes (IGV) device that allows modulating the inlet flow

during start up and optimize performance at part load operation. Air bleed ports provide cooling

air for 1st and 2nd turbine stages (stationary and rotating buckets). The compressor end portion

that discharges the air mass flow into the combustion chamber contains the compressor diffuser,

devoted to eliminate flow swirl and then improve diffuser efficiency.

Combustion Section

The PG9161(E) combustion system has been designed in order to ensure reliability, durability

and flexibility, even in case of using different fuels. The combustion system is contained in a

carbon steel casing which is part of the compressor-combustor shell and provides housing for

combustor wrapper, combustions chamber assemblies, fuel nozzles, spark plug ignitors, UV

flame detectors, cross flame tubes, transition piece. The combustion takes place in 14

combustion chambers, circumferentially arranged around the machine axis. The hot gas flows

from the combustion chambers toward the turbine section via 14 "S" shaped transition pieces.

This special arrangement ensures a good mix between the film cooling air and the combustion

gases, thereby optimizing the gas temperature pattern at the first turbine stage inlet. The

combustion section consists of Hastelloy cylinders joined together with corrugated rings, which

lead the cooling air film along the wall, thus improving cooling.

The combustion chambers are installed and removed without lifting the combustor casing

cover, in order to facilitate inspection and to reduce the inspection time. The transition pieces

connecting the combustors to the turbine inlet are manufactured with NIMONIC 263 alloy,

which yields good anti-corrosion properties together with high cracking resistance, and is

furthermore easily weld able for maintenance at site, without needing heat treatment. Spark

plug igniters, located in the 10th and 11th combustion chambers, are used t ignite the fuel/air

mixture; the remaining chambers are ignited through cross flame tubes that provide connection

between every two adjacent combustors. Two ultraviolet (UV) flame scanners, located in the 4th

and 5th combustion chamber are provided to detect ignition during start up. The fuel is injected

into the combustion chambers through fuel injectors, one per each combustion chamber, which

are provided for single fuel operation.

Turbine

The 3-stage turbine rotor is constituted by 3 discs, forged in alloy steel and coupled each other

by bolted connections.

All rotating blades are precision cast, and are attached to the wheels by straight, axial-entry,

multiple-tang dovetails that fit into matching cut-outs in the rims of the wheel. The turbine

stationary blades (nozzles) are precision cast according to the following table:

- first stationary row 18 segments x 2 vanes Cooled

- second stationary row 16 segments x 3 vanes Cooled

- third stationary row 16 segments x 4 vanes Uncooled

The cooling flow for the cooled profiles is bled from suitable compressor stages (see

compressor section). The space between 2nd and 3rd rotor wheels is also cooled by compressor

bleed air. Nozzle diaphragms are attached to the inside of both 2nd and 3rd stage nozzle

segments. These diaphragms prevent air leakage past the inner sidewall of the nozzles and the

turbine rotor. A turbine shroud is included, whose main function is to provide a cylindrical

surface for minimizing bucket tip clearance leakage (a secondary function is to provide a high

thermal resistance between the hot gases and the comparatively cool shell). This reduces the

shell-cooling load and allows controlling the shell diameter and roundness and turbine

clearances. The shroud segments are maintained in the circumferential position by radial pins

from the shell. Joints between shroud segments are sealed by interconnecting tongues and

grooves.

Exhaust Frame and Exhaust Plenum

The flanged end of gas turbine shell is bolted to exhaust frame. On the structural point of view,

the frame consists both of an outer and an inner cylinder, interconnected by radial struts. The

GT end journal bearing is supported from the inner cylinder. The exhaust frame, fabricated in

ASTM A435 carbon steel, receives gas flow from the GT diffuser, and is connected to the

exhaust plenum by flexplate expansion joint.

The exhaust plenum consists of a box, open at one side and welded to its own base. It is

fabricated in carbon steel, lined with 409 SS chromium steel sheet. Thermocouples for

measurement of exhaust gas temperature and for transmitting the values to the GT control

system are located in the final part of the exhaust plenum.

Gas Turbine Control System (SUMIVAC)

Gas Turbine Auxiliaries

The Gas Turbine includes the following auxiliaries:

• Oil Systems (Lubricating Oil system, Control Oil system)

• Inlet Air system (Filtration system, Inlet Air duct, etc.)

• Exhaust Gas facilities (silencer, vertical stack)

• Fuel system (dual fuel: natural gas, diesel oil)

• Compressor Washing system

• Enclosures including HVAC, Fire-fighting, etc.

• Lube Oil closed circuit Cooling Water system

• Instrument Air system

• Fire Fighting system (CO2 and dry chemical type)

• Gas Detection system

• Electrical equipment (Generator Neutral Grounding Cubicles, Generator Protection)

• Board, Low Voltage Distribution Board, Power Control Centre, Motor Control Centers,

DC Power system, Uninterruptable power supply, Cables, Induction Motors, Grounding

system, Vibration monitoring and protection system, Indoor Lighting system).

Electrical Generator

The electrical Generator is a synchronous machine, ventilated in open air-circuit, with airexchanger

shell & tube cooler provided. Characteristics of generator as follows:

NOTE: Closed Cooling Cooler not included. Special Design for climate conditions

Rated Output: 163 MVA**

Rated Terminal Voltage (± 5%): 11.000 V

Rated Phase Current: 7400 A

Rated Power Factor: 0.85

Frequency: 50 Hz

Speed in RPM: 3000

Design Temperature: As per IEC 34

Insulation: Class F

Maximum Air Inlet Temperature: 40°C

Generator Excitation System: Static type

Response Ration: >1.9 s-1

Power Consumption at rated load: _290 kW

** The Generator is oversized to allow upgrade to PG-1971-E at first overhaul.

Electrical Systems

GAS TURBINE Generator

The GT generator, endowed with related auxiliary systems and devices, shall be rated to

operate continuously at full load.

The excitation system shall be static type with automatic and manual Automatic Voltage

Regulator (AVR) system.

The main functional generator characteristics shall be as listed below:

Rated Capacity 139 MW (ambient air at 40°C)

Power factor 0.85

Voltage 11 kV

Frequency 50 Hz

Rotation speed 3000 RPM

Phases 3

Class of insulation F

Standard IEC at 835 m.

Step-up Transformer (NOT INCLUDED)

Unit Transformers (included)

 to be continuted.