gun pods, and bombs. The maximum external payload is 1,000 kg. The prototype aircraft was initially powered by a SNECMA Turbomeca Larzac 04-H-20 non-afterburning turbofan developing 14.12 kN of thrust. All production models will use the more powerful NPO Saturn AL-55I engine with about 16.9 kN of thrust, as stipulated by the 2005 air staff requirements from the Air Force. Development 2000s The first and second prototypes of the HJT-36, labeled PT-1 and PT-2, flew on 7 March 2003 and in March 2004, respectively. The program was then delayed with the Air Force assessing the SNECMA Turbomeca Larzac engine, with 14.1 kN of thrust, as under-powered. In response, in August 2005, HAL reached a deal to replace the SNECMA engine with the NPO Saturn AL-55I with 16.9 kN of thrust. The deal also provided for license-production of the engine in India by HAL. Further delays were caused by delays in delivery of the NPO Saturn engine by 2 years, as well as due to two accidents in February 2007 and in February 2009 involving each of the prototypes, which grounded the aircraft for repairs and investigations. The first AL-55I engine was received from Russia on 28 December 2008, 2 years later than committed, and was installed on PT-1. Following ground taxiing trials, flight tests with the new engine started on 9 May 2009. 2010 After further development and extensive testing, the Indian Air Force placed an order for 73 aircraft. After over 280 test flights, the aircraft entered limited series production in 2009 for the first 12 aircraft to be delivered to the Air Force. The first flight test for the limited series aircraft occurred in January 2010, and initial operational capability was expected by July 2011. The Air Force order was expected to grow to over 200 aircraft. 2012 On 27 July 2012, first Engine Ground Run was performed on third prototype. 2013 In December 2013, HAL declared that Sitara was 'weeks' from certification. 2014 On 19 February 2014, the Indian MOD submitted a statement that the development of IJT was in the advanced stages of certification, with more than 800 test flights completed so far. The activities were progressing well with completion of sea level trials, night flying trials, high altitude trials as well as weapon and drop tank trials. The activities left for obtaining Final Operational Clearance (FOC) are the refinement of stall characteristics, and spin testing