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The Nimrod Review - Official Documents

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Fuel Seal Replacement Programme<br />

15.16<br />

Chapter 15 – BOI Recommendations and Post-XV230 Events and Measures<br />

18 As a result of a key BOI recommendation, a Fuel Seal Replacement Programme (FSRP) was instituted. This<br />

targeted for replacement 42 fuel seals in areas where an independent study19 had shown that a fuel leak would<br />

be particularly undesirable. This programme is being undertaken by a specially trained team who ensure that<br />

their work does not disturb the alignment of the fuel system pipes. Contrary to some prognostications by those<br />

who believed that fuel seals were best left undisturbed, the FSRP has so far produced encouraging results.<br />

Hot Air Duct Replacement Programme<br />

15.17<br />

20 As a result of a further key BOI recommendation, a Hot Air Duct Replacement Programme (HADRP) was<br />

instituted. <strong>The</strong> BOI recommendation was made in the light of the disintegration of part of the SCP duct at the<br />

‘elbow’ on XV227 in November 2004, following which BAE Systems was commissioned to complete a survey<br />

of the ducting within the system and, if necessary, recommend the ‘lifing’ of the components. <strong>The</strong> initial BAE<br />

Systems report21 recommended setting lives for the ducts which were significantly lower than those that the<br />

RAF had experienced in actual use. As a result, BAE Systems was tasked to reconsider its proposals in the light<br />

of practical experience and fatigue tests of actual ducts. BAE Systems produced a further series of papers and<br />

letters in 2007 and 2008; the result of this activity was a decision, agreed with the <strong>Nimrod</strong> IPT, that a life of<br />

2,500 hours for the aircraft’s hot air ducts would be appropriate. This in turn triggered the HADRP. <strong>The</strong> residual<br />

risk inherent in continuing to use the system was mitigated by the fact that the prohibition on SCP use would<br />

continue, the Cross-Feed ducts would only be used on the ground for engine start and all high-temperature<br />

ducting in use in the air is contained within a fire zone.<br />

15.18 As explained in Chapter 7, as a result of BAE Systems’ work and the BOI’s recommendation, in June 2008, the<br />

<strong>Nimrod</strong> IPT issued a Special Technical Instruction (STI 926) regarding a fleet-wide duct replacement programme,<br />

requiring the replacement of the high pressure hot air ducts between the ECU and the Cross-Feed valves, and<br />

also those that formed the Cross-Feed system. <strong>The</strong> <strong>Nimrod</strong> IPT determined that, for the risk to the aircraft to<br />

remain ALARP, the replacement programme should be completed by 31 March 2009 and that aircraft that<br />

had not had their hot air ducts replaced by this time would not be flown until the work had been completed.<br />

Although it had originally been planned that the programme would be completed by 31 March 2009, delays in<br />

the provision of replacement parts made this unachievable. As at the date of writing, eight <strong>Nimrod</strong> MR2s and<br />

two R1s have been through the HADRP. <strong>The</strong> only aircraft that have not been through the HADRP are those in<br />

scheduled maintenance; these aircraft will have their ducts replaced before returning to service.<br />

Teardown by QinetiQ commenced August 2008<br />

15.19<br />

While scoping the work necessary to complete the AASyA, the IPT concluded that the most effective means of<br />

achieving the BOI’s intent would be physically to dismantle a <strong>Nimrod</strong> to identify areas of concern; indeed, this<br />

would enable an examination of the condition of the entire aircraft, not just its systems. <strong>The</strong> Chief of Defence<br />

Materiel authorised a forensic ‘teardown’ of a <strong>Nimrod</strong> to be carried out. I understand that this may be the first<br />

full-scale forensic teardown of an aircraft to examine systems that has ever been conducted anywhere in the<br />

world. On 1 August 2008, QinetiQ was contracted to undertake this major task. <strong>The</strong> task was completed in<br />

July 2009 and the total cost is estimated to be £2.6 million. <strong>The</strong> aircraft chosen (XV236) was one which would<br />

have been due a Major maintenance procedure; by virtue of the time since it had last undergone an extensive<br />

maintenance procedure, this aircraft would exhibit the greatest range of defects and degradation. This approach<br />

proved fruitful. A large number of issues were found and raised by QinetiQ. <strong>The</strong> majority of arisings were of a<br />

relatively minor nature and would have been identified and corrected during the previously planned Major. 22<br />

18 Following the decision not to life fuel system seals (BOI Recommendations 5 and 6 at paragraphs 65a (1) and (2)), other means were sought to<br />

address the issue of fuel leaks; the Fuel Seal Replacement Programme was one of these measures.<br />

19 “<strong>Nimrod</strong> Fuel System Zonal Hazard Assessment”, QINETIQ/EMEA/IX/SA0701788, Issue 1.<br />

20 BOI Recommendation 11 at paragraph 65 c of the BOI Report recommended measures to prevent the hot air system acting as a source of ignition,<br />

including that “the study into corrosion....undertaken following the hot air leak on XV227 is completed and its recommendations acted upon”. <strong>The</strong><br />

decision to replace the hot air ducts was a direct result of this study.<br />

21 MBU-DEB-R-NIM-FF0786, dated 1 June 2005.<br />

22 Comment by QinetiQ personnel to <strong>Review</strong> member during <strong>Review</strong> inspection of XV236 at Boscombe Down.<br />

419

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