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HS 748 Replacement Engine

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    ANNEXURE-ITelephone:+91-512-2451749 to 58Fax: +91-512-2450505Email: [email protected]: DGD/2924/102 DATE: 15*^ Aug2013

    REQUEST FOR INFORMATION (RFI)DUE DATE: 30' Sep'2013 @ 15:00Hrs 1ST.

    SUB: REQUEST FOR INFORMATION (RFI) FOR "ALTERNATE ENGINE FOR HS 748AIRCRAFT" .

    ***

    Hindustan Aeronautics Limited (HAL), a Navratna Public Sector Company is a pioneer inAircraft Industry in South Asia (www.hal-india.com).

    2. Transport Aircraft Division (TAD), is an AS 9100C, IS/ISO 9001:2008, IS/ISO 14001:2004certified division of HAL. HS 748aircraft was manufactured at TAD, Kanpur under licensefrom M/s BAe,UK. HS 748 aircraft is medium sized turbo prop aircraft. It is a 45-48 seat a/cwith takeoff weight 20,180kgs. Currently major overhaul of HS 748 aircraft is carried out atKanpur. HS 748 a/c is currently fitted with Rolls Royce Dart engines 536-2T(2040SHP) and533-2(1990SHP). Transport Aircraft Division, Kanpur is contemplating replacement of RollsRoyce Dart Engine with modern fuel efficient engines on HS 784 aircraft along with otherelectrical, avionics and structural upgradation .

    3. Presently used Roils Royce Dart engine is a gas turbine engine designed to drive apropeller and to give a small amount of jet thrust. Main components of engine are twostage centrifugal compressor, 7 combustion chamber and 3 stage axial flow turbine. Thecompressor is directly coupled through a shaft to turbine and the propeller is driven by theturbine through a separate shaft and compound reduction gear box. This Dart engine hasSpecific fuel consumption of 0.767lbs/hr/shp which is quite high compared to same class ofmodern engines.

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    Further Rolls Royce Dart Engine mechanically drives Accessories Gear Box of Aircraft bydrive shaft assembly. Accessories Gear Box further drives following accessories:

    Cabin super charger(for cabin pressurization). Tachometer. Alternator. Hydraulic pump. Generator.

    Accessories mentioned above needs to be upgraded technically.

    4. Currently there are 59 HS748 aircraft in service with our operators. Due to low utilizationrate (Average 350Hrs/Year) majority of aircraft have technical residual life around80,000Hrs. Owing to the good health of the airframe and considerable residual life,replacement of Rolls Royce Dart Engine with modern fuel efficient engines on these 59 HS784 aircraft is being planned.

    5. Preliminary Technical Requirements of the ALTERNATE ENGINE FOR HS 748 A/C areenclosed as ANNEXURE-II for your perusal and response. In addition to response for theabove requirements, kindly also provide the following details of the suitable alternateengine.

    a) Complete technical specification of Engines.b) Engine installation manual and typical Engine mounting details on any Aircraft.c) Engine deck data to evaluate the performance of engine.d) Engine controls and indications required in the cockpit.e) Details of the propeller used with the Engines along with performance.f) Aircraft Accessories which can be driven by Engines.g) Assistance you can provide in selection of Engine and its integration on aircraft with

    related accessories and controls.h) Any other information considered useful in taking decision on Engine selection and

    its installation.i) Budgetary Proposal.

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    6. Information and Instructions for potential suppliers:i) OEIVl of the engine with proven expertise in design, manufacture and supply ofEngine for Fixed Wing Aircraft programmes are only required to participate in the RFI. Thedetails of the said products designed, manufactured, tested and certified including contactaddresses of the customers should be provided (necessary documentary proof shall beprovided).

    ii) RFI proposal should confirm whether any specific clearances and export licenses arerequired from theGovernment ofseller's country for supply ofsubject item with end use asHAL for Civil & Military applications. If yes, estimated time period for obtaining the exportlicense/ clearance shall beprovided.

    iii) The prospective Supplier shall provide details of Manufacturing facilities, details ofcurrent capabilities (technical expertise) related to design, manufacture, testing,certification, maintenance and supply of same or similar Engine for Fixed Wing Aircraftprogrammes.

    iv) The prospective Supplier shall provide brief on Quality Management System(including process control) being followed at their works present.

    v) Warranty of at least two years is requirecf for the proposed system/its major LRU'sitems.

    vi) The technical details enclosed at Annexure-I are only tentative in nature and aresubject to change and may be considered only as advance information for marketexploration.

    HAL will freeze technical scope based on response to subject RFI and as deemednecessary at the time of issuing RFQ (Request for Quotation) at HAL's discretion.

    Compliance and requisite details against each requirement listed in Annexure-llshould be provided.

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    vii) The potential supplier can propose suitable and proven solution to meet the HAL'srequirement.

    viii) This document is not intended to form the basis of any decision to purchase/finalizecontract and it does not constitute an offer or invitation or solicitation of an offer topurchase.ix) Proposals received from vendor other than OEM will n o t be considered.

    7. Future Process: Based on an evaluation of RFI proposals received, HAL shall finalizetechnical requirement and float Request for Proposal (RFP) at HAL's discretion.

    8. The RFI project proposal (including Technical & Budgetary price proposal) document dulycompleted and signed should be sent to:

    Deputy General Manager (IMM),Transport Aircraft Division (TAD),Hindustan Aeronautics Limited,CHAKERI,KANPUR-208 008, INDIATel: +91-512-2451749to 58, Fax:+91-512-2450505e-mail: p u r c h a s e . k n p @ h a l - i n d i a . c o mo r a l t e r n a t e l y you may a l s o se n d s o f t c o p y by e m a i l p u r c h a se .k n p @ h a l -i n d ia . co m

    9. The due date for submission of RFI proposal is 30*Sep'2013.

    Thanking you.

    For Hindustan Aeronautics Limited,S M (IMM)

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