DESIGN AND DEVELOPMENT OF FUEL BOOSTER PUMP OF DO-228 AIRCRAFT

Firm Qty Requirement of DO228-10129 after successful development

Qty required for Calender Year 2026-27

Total Value M = L x G

NRC FOR D & D OF FUEL BOOSTER PUMP

Part No.

Firm Qty Requirement of DO228-10129 after successful development

Qty required for Calender Year 2026-27

Total Value M = L x G

NRC FOR D & D OF FUEL BOOSTER PUMP

Requirements

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The approved Technical Requirement for the Unit is enclosed at Annexure-B. Development Agency shall carry out Requirement Review with an external domain expert in co-ordination with the airworthiness agencies / HAL to ensure the adequacy of technical specification document

To address all TBD (To Be Defined) points of Technical Specification Document (TSD) prior to Requirement Review.

Submission of Type Certification Basis (TCB), Airworthiness Certification Plan (ACP) and Quality Assurance Plan (QAP) documents in co-ordination with HAL to airworthiness agencies for approval. QAP shall be submitted post PDR and prior to fabrication of prototype(s) of indigenous Unit.

Carrying out the Technical Requirement Review (TRR), Preliminary Design Review (PDR), Critical Design Review (CDR) & Test Adequacy Review (TAR) with prior intimation (min. 15 working days) to HAL and Airworthiness Agencies. Development Agency shall extend the necessary technical support required after TRR, PDR & CDR for updating of TSD. Development Agency shall implement all the necessary modifications in the indigenous Unit emerged out after TRR and PDR & CDR.

Development of all necessary Design Documents, Process Documents & Test Documents required for airworthiness certification and will get the approval by airworthiness agency through HAL.

Procurement of raw materials required for fabrication of prototype(s), along with test reports and Certificate of Conformity (CoC) traceable to OEM as per approved Bill of Material (BoM). Development Agency has to offer the kit for inspection in-line with AQA directive 06/2018 dated 15.10.2018, guideline for "Kit Inspection of Electrical, Mechanical components and Consumables for airborne modules/LRUs"

Initially 02 set - 01 Successful QT unit and 01 for SOFT prototype unit set for Ground testing and Flight testing/ performance evaluation will be required After successful trial testing and approval and production accecptance, bulk quantity order will be processed. Installation kit containing required mating connectors/ fastners on aircraft side should be considered as part of supply.

Development of the Test Equipment/ Rig, generating all the required documents, fabrication of Test Equipment / Rig as per approved BOM and carrying out necessary QT (Qualification Test) as per QAP & ATP (Acceptance Test Procedure) document approved by Airworthiness agencies. The Test Equipment /Rig is required to carry out the standalone functional test for acceptance of indigenous Unit

Carrying out functional tests as per approved Acceptance Test Procedure (ATP) document to meet the requirement mentioned in the approved TSD.

Fabrication of special fixtures for' qualification tests, if required and get it approved from airworthiness agencies

Carrying out Qualification Tests as per approved Qualification Test Procedure (QTP) to meet the requirement of approved TSD. Qualification Tests are to be done in two stages i.e. first stage is Limited Qualification Test (LQT) on pbtotype Unit-1 to obtain the clearance for aircraft level test and second stage is for Ground testing / Aircraft testing on prototype Unit-2.

After completion of all development activities, Development Agency to provide all support to HAL for applying for Letter of Technical Approval (LoTA) /Production Clearance (PC) for certification of indigenous Unit from CEMILAC/RCMA.

The complete development process of subject system/Unit will be done in co-ordination with CEMILAC and DGAQA/DGCA/ TARDC. The qualification requirements suggested by regulatory authority at any stage of development shall be binding to the vendor and shall be demonstrated to CEMILAC/DGAQA/DGCA/ TARDC.

Documentation: The details of documents/ publications that should be provided by Development Agency at the time of QT/flight trials must include and not restricted to the following: a. Approved drawings. b. Qualification test reports. c. Acceptance Test Procedure (ATP) for approval during development phase. d. Certificate of Conformity (COC)/Form-1 e. Component Maintenance Manual (CMM) f. Installation Manual

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Providing Technical Requirement of Unit/Systems.

Conducting ground testing/flight testing.

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INFORMATORY

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PART-III

RFQ Clauses

i) All the bidders/ Bidders should ensure that they are GST compliant and their quoted tax structure/ rates as per GST Act/ Rules. Bidder should be registered under GST and furnish GSTIN number and GST Registration Certificate in their offer unless they are specifically exempted from registration under specific notification/ circular/ section/ rule issued by statutory authorities.

ii) GST Registration Number (15-digit GSTIN): If the bidder has multiple business verticals in a state and has separate registration for each vertical, the GSTIN of each vertical is concerned with the supply and service involved, as per the scope of Schedule of Requirements and Price Schedule quoted. If the supply/ service provided is from multiple states, the bidder should mention GST registration numbers for each state separately.

iii) Composition scheme: If the Bidder has opted for a composition levy under Section 10 of CGST, he should declare the fact while bidding along with GSTIN and GST registration certificate.

(iv) Exemption from Registration: If a bidder is not liable to take GST registration, i.e., having turnover below threshold, he shall submit undertaking/indemnification against tax liability. Bidder claiming exemption in this respect shall submit a valid certificate from practising Chartered Accountant (CA)/ Cost Accountant with Unique Document Identification Number (DIN) to the effect that Bidder fulfils all conditions prescribed in notification exempting him from registration. Such bidder/ dealer shall not charge any GST and/ or GST Cess in the bill/ invoice. In such case, applicable GST shall be deposited under Reverse Charge Mechanism (RCM) or otherwise as per GST Act by the Procuring Entity directly to concerned authorities. Bidder should note that his offer would be loaded with the payable GST under the RCM. Further, Bidder should notify and submit to the Procuring Entity within 15 days from the date of becoming liable to registration under GST.