The first of three test aircraft was delivered to the USAF for operational test and evaluation in December 2008 and the remainder were delivered in February 2009. The second of three C-5M test aircraft made its first flight in November 2006 and the third (a modernised C-5A) in March 2007. In December 2001, Lockheed Martin Aeronautics Company was awarded a system development and demonstration (SDD) contract for the C-5 RERP, to apply the new systems to four C-5 aircraft by 2009.įirst flight of the C-5M, the designation given to aircraft upgraded under RERP and AMP, took place in June 2006. The second phase, the C-5 reliability enhancement and re-engining programme (RERP) is to upgrade the aircraft’s engines and pylons, as well as to improve reliability. The first phase of the upgrade is the avionics modernisation programme (AMP). The US Air Force initiated a comprehensive upgrade programme to ensure the capability of the C-5 fleet to at least 2040. The heavy logistic transport aircraft is of cantilever high-wing monoplane design with a fail-safe semi-monocoque aluminium alloy fuselage. The C-5B is capable of carrying a maximum payload up to 118,387kg to a range of 5,526km,which can be extended by in-flight refuelling.
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