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The Nimrod Review - Official Documents

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6.100<br />

Chapter 6 – Overflow or Pressure from Air-to-Air Refuelling<br />

6.99.1 <strong>The</strong> conclusion of the Feasibility Study clearly states: “This report describes the incorporation into<br />

a <strong>Nimrod</strong> MR Mk 2 of an AAR capability which will meet the requirements of a full CA Release.”<br />

(emphasis added)<br />

6.99.2 Section 5 of the Feasibility Study expressly considers whether the aircraft’s existing fuel venting system<br />

required any modification and concludes, in this respect, that as regards tank No. 5, “During AAR a<br />

fuel discharge from this valve may cause difficulties due to possible fuel ingress into the port engines.<br />

To alleviate this possibility a differential pressure switch, identical to the Mod 700 installation, will<br />

be fitted”. <strong>The</strong>re would have been no need for BAE Systems to have considered such issues if its<br />

responsibilities in relation to Mod 715 were as limited as it now sought to suggest.<br />

6.99.3 <strong>The</strong> attachments to the Feasibility Study included schematic drawings of the refuel system as a whole.<br />

In my view, therefore, reading Mod 715 and the Feasibility documents together, it is crystal clear that it was<br />

intended that BAE Systems was responsible for ensuring the entire AAR capability, including the internal fuel<br />

system, was Def-Stan 00-970 compliant.<br />

XV230’s experience<br />

6.101<br />

6.102<br />

On return from a sortie in August 2006, the <strong>Nimrod</strong> detachment personnel found a small amount of fuel in<br />

XV230’s bomb bay, and traces of fuel having been discharged from the No. 1 tank blow-off valve during sorties<br />

prior to the aircraft’s loss. <strong>The</strong> <strong>Nimrod</strong> detachment air and ground crew examined the symptoms and made a<br />

logical deduction that the No. 1 tank blow-off had operated and that fuel from the blow-off had penetrated<br />

the bomb bay along the hinge line. A de facto limit of 15,000lbs was subsequently operated by crews when<br />

filling No. 1 tank during AAR and the symptoms disappeared. This limitation was not formally recorded in the<br />

aircraft documentation but I have no doubt that it was put into operation by crews, and it was relayed to FS<br />

Davies when he was briefed prior to his first AAR sortie in theatre and carried out by him. 50 Crew 3 was a highly<br />

experienced, close-knit and capable crew.<br />

In any event, there was no evidence available to the personnel at the time that blow-off might give rise to any<br />

hazard. <strong>The</strong> No. 1 tank blow-off, unlike the No. 5 tank blow-off, had been left functional after the <strong>Nimrod</strong> was<br />

made AAR capable. <strong>The</strong> blow-off was clearly capable of functioning, and indeed was meant to function, either<br />

on the ground or in the air, to prevent over-pressurisation of the tank by fuel. It was, therefore, in my view a<br />

reasonable assumption on the part of all concerned that there was no particular hazard in it functioning in either<br />

environment.<br />

6.103 <strong>The</strong> Air Member for Materiel, Air Marshal Sir Barry Thornton, notes, in his comments on the BOI, “it is unfortunate<br />

that no aircraft incident reports were raised as a result of these events”, 51 while discussing the detachment’s<br />

reaction to the occurrence of blow-off. In my view, however, in the circumstances pertaining at the time in theatre,<br />

it is quite understandable that no incident report was raised. If blow-off had occurred on the ground during refuel,<br />

no similar action would have been taken. <strong>The</strong> aircraft had been refuelled on the ground without incident. <strong>The</strong><br />

symptoms had also disappeared following the application of the 15,000lbs limitation. Thus, there was no reason<br />

for anyone to think that were any significant underlying problems with the No. 1 tank’s refuel system.<br />

6.104<br />

In my view, the air and ground crew have absolutely nothing to reproach themselves for. <strong>The</strong> blow-off valve was<br />

working normally as it was intended to operate. An incident report or call back to RAF Kinloss for instructions<br />

would have been unlikely to have elicited any different solution to the problem. <strong>The</strong> BOI acknowledged that,<br />

even after the accident, it took several months of painstaking investigation to uncover the cause and possible<br />

effects of a blow-off. No one in theatre had any reason to suppose that it was anything other than the correct<br />

operation of the aircraft systems. No one in theatre had any reason to suppose it might be a safety matter. No<br />

one in theatre was, or could reasonably have been, aware of the serious ignition danger lurking in No. 7 Tank<br />

Dry Bay.<br />

50 BOI Report, page 2-34, and Witness Statement 22.<br />

51 BOI Report, Comments of Air Member for Materiel, paragraph 14.<br />

129

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