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The Nimrod Review - Official Documents

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<strong>The</strong> <strong>Nimrod</strong> <strong>Review</strong><br />

6.44<br />

6.45<br />

118<br />

<strong>The</strong> dyed water trials from the APU bay and the forward drain of an MRA4 (discussed above) show the manner<br />

in which fuel tracking down the aircraft fuselage will enter compartments, despite the fact that the panels are<br />

flush with the aircraft fuselage and that, in the case of these trials, the aircraft is recently manufactured and<br />

built to modern tolerances. Even 30 minutes after landing, dyed fluid was found “dripping from the tail-cone<br />

bay door”; and when the door was opened it was noted that the fluid had “coated an area in the bay within<br />

approximately one foot all around the door” (see the pink dye in the photographs below).<br />

Pink dye found inside door<br />

Figure 6.7: MRA4 Dyed Fluid Inside Tail Cone Bay Door<br />

Rubber seal<br />

around the<br />

door<br />

<strong>The</strong> report notes that there was no evidence of fluid pooling in the bay. <strong>The</strong> amount of fluid released into the<br />

airflow, however, was very small, only 0.4 litres in total, and the distance it had to travel large, namely several<br />

metres from the MRA4 APU bay (in the rear of the wing) to the tail cone bay. By way of contrast, when blowoff<br />

occurs during AAR, the flow rate is very large. It has been calculated to be approximately 120 litres every 10<br />

seconds. 26 Further, as illustrated above, blown-off fuel would only have to track 2.1 metres along the fuselage<br />

skin to reach the SCP fairing. It should be noted that, although the MRA4 is indeed a different aircraft to the<br />

MR2, its fuselage is the original MR2 shape.<br />

Further considerations<br />

6.46<br />

<strong>The</strong>re is clear evidence from the incident in 2006 involving a <strong>Nimrod</strong> being refulled by an VC10 of fuel flowing<br />

down the outside of the airframe and entering several chambers on the MR2 external to the pressure hull: the<br />

bomb bay, the rear hinged fairing, the dinghy bay, aerial mounts, the self defensive flares chamber and the tail<br />

cone, to name only some. 27 Although the starboard No. 7 Tank Dry Bay was never identified as containing fuel<br />

following this incident, or other similar event, this may well be because this bay is not an area that was examined<br />

regularly prior to the loss of XV230 and, in any event, if fuel had entered the starboard No. 7 Tank Dry Bay lower<br />

26 Approximately 12 household buckets every 10 seconds.<br />

27 Air Incident Report KIN 066/06.

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