AgustaWestland helicopter deal: In first reaction, govt gives itself clean chit
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The govt, in its first reaction to a story broken by The Indian Express, says news reports could not have formed 'basis for preliminary determination' of wrongdoing.
It adds, authorities moved into action as soon as CEO Giuseppe Orsi was arrested.
According to the notification released by govt, contract specifically bans bribery, 'undue influence' and even boasts of an 'integrity contract' that shows its desire to retain transparency in deal.
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Acquisition of AW-101 Choppers for IAF: The Facts
1. In August 1999, the IAF which is responsible for carrying out VVIP communication task, proposed the replacement of Mi-8 VIP helicopters due to severe operational constraints, such as, inability of Mi-8 to operate at night and in adverse weather, inability to operate safely at places in elevation beyond 2000 meters etc. IAF felt the need for the replacement of Mi-8 helicopters as they were completing their total technical life.
2. A global RFP was issued in March 2002 to which 4 vendors responded. The Technical Evaluation Committee shortlisted 3 helicopters and accordingly flight evaluations were conducted. Since, EH-101 of M/s. AgustaWestland was not certified for an altitude of 6000 meters, it did not participate in the flight evaluation. The Russian helicopter Mi-172 could not comply with 7 mandatory Operational Requirements (ORs). After flight evaluation, EC-225 of M/s. Eurocopter, France was found suitable for acquisition.
3. On November 19, 2003 a meeting was taken by Principal Secretary to PM on this subject. In the meeting, Principal Secretary observed that his main concern was that the framing of the mandatory requirements has led us effectively into a single vendor situation. It was also noted that PM and President have rarely made visits to places involving flying at an altitude beyond 4500 meters. In the meeting it was decided to make the mandatory requirement for operational altitude 4500 meters. The higher flying ceiling of 6000 meters, and a cabinet height of 1.8 meters could be made desirable operational requirements. It was observed that with these revisions, several helicopters which otherwise met all requirements but had been rejected due to the altitude restriction, would now come into the reckoning.
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