Sorry Phil, but the rotors were not turning or rotating at the time of impact, so it was not misreported.
From the AAIB:
Examination at the accident site and further more detailed examinations at the AAIB facility in Farnborough have shown no evidence that the transmission system, main rotor, Fenestron tail rotor and associated drive shafts were rotating when the aircraft struck the roof of the building.
If the pilot mishandles the emergency, or there is some other force, then the rotors will stop, and quickly. That is why a pilot must enter autorotation to maintain rotor speed. There was no post impact fire from the aircraft, as can be seen from the photos.
It also appears that while the main tank had 76 kg of fuel, the supply tanks were almost empty (0.4kg) and empty. The supply tanks do supply fuel to the engines, not the main tank (the main tank supplies fuel to the supply tank via transfer pumps). All pumps were deemed to be operational at the time of the accident (operational, not necessarily operating).
Here is what the AAIB said about the fuel switches:
The fuel pump switches were examined at the accident site and it was found that the No 1 and No 2 prime pump switches (pRIMe I and II) were set to the on position and the fore and aft transfer pump (XFeR F and A) switches were set to the oFF position.
Here is a link to the AAIB report:
http://www.aaib.gov.uk/cms_resources.cfm?file=/AAIB%20S2-2014%20G-SPAO.pdfFrom a quick look, and my experience with a similar helicopter type, it may be as simple as incorrect switch selection. Normally, after starting the engines, the prime switches are turned off and the transfer pumps turned on.