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The Nimrod Review - Official Documents

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10A.149<br />

Chapter 10A – <strong>Nimrod</strong> Safety Case: <strong>The</strong> Facts (Phases 1 and 2)<br />

Unfortunately, neither QinetiQ nor the <strong>Nimrod</strong> IPT checked to see whether all the risk mitigation evidence<br />

was included in the final safety case reports delivered by BAE Systems. In fact, BAE Systems included none.<br />

Early July 2005: Mech Systems only 20% completed<br />

10A.150 On 5 July 2004, Witness K [BAE Systems] reported to Eric Prince that six out of 20 Functional Pro-Formas and<br />

three out of 33 Zonal Pro-Formas had been completed. He estimated that Mech Systems’ task was only about<br />

20% complete and that a further nine weeks of manpower would be required to complete the remaining 14<br />

Functional Pro-Formas and a further 17 weeks of manpower would be required to complete the remaining<br />

30 Zonal Pro-Formas. In an attempt to address the resource problem, Eric Prince arranged for a further BAE<br />

Systems engineer, Witness R [BAE Systems], to be brought in from Woodford to help Witness K [BAE Systems]<br />

with some of the load in Mech Systems. Witness R [BAE Systems] worked on the Mech Systems Pro-Formas.<br />

It was Witness R [BAE Systems] who was to complete the Mech Systems Pro-Forma for Hazard H73.<br />

10A.151 On 7 July 2004, a Safety Case <strong>Review</strong> Meeting took place. Witness K [BAE Systems] gave his status report on<br />

behalf of Mech Systems. It was reported that, in total, only 41 out of 104 hazards had been returned and 63<br />

still remained to be done. <strong>The</strong> ‘best’ case scenario for completion was the second week of August using 600<br />

hours and the ‘worst’ case scenario was the end of August using 900 hours. A major problem was summer<br />

holidays.<br />

10A.152 On 8 July 2004, a TTRO Engineering Integration Meeting took place. Witness B [BAE Systems] was not present<br />

so the meeting was chaired by Richard Oldfield. <strong>The</strong> NSC does not appear to have featured significantly at<br />

this meeting save for a mention that “Resource reviewed and new estimate to completion issued.”<br />

8 July 2004: MRA4 Generic Data obtained to sentence hazards<br />

10A.153 At an internal BAE Systems NSC meeting on 8 July 2004, Witness R [BAE Systems] inquired whether there were<br />

“standard values” which could be used to sentence hazards. Witness S [BAE Systems] of the Airworthiness<br />

Department and Eric Prince said there were and agreed to try to find them. Later the same day, Witness S<br />

[BAE Systems] circulated an e-mail attaching MRA4 generic probability data which he said had been extracted<br />

from the <strong>Nimrod</strong> MRA4 System Safety Working Practices (Annex K) AWN/NIM/897 Issue 7 (Re 7 Ver 2). He<br />

explained that the significance of this data was that “the Customer has extracted the figures”. <strong>The</strong> e-mail<br />

was copied to Chris Lowe but neither he, nor anyone else, raised any objection to the use of such MRA4 data<br />

(notwithstanding his earlier rejection of the use of any MRA4 data).<br />

10A.154 <strong>The</strong> MRA4 generic data (used to make probability assessments in the MRA4 project) gave a standard failure<br />

probability rating for a number of common failure types. A failure of a “fuel pipe and associated coupling”<br />

was ascribed a failure probability of 1E-6, viz:<br />

Failure Type Failure<br />

Probability<br />

…<br />

Hydraulic pipe and associated coupling 1E-6<br />

Fuel pipe and associated coupling 1 E-6<br />

ECS pipe seal 1.5E-7<br />

10A.155 <strong>The</strong> use of MRA4 generic data to sentence MR2 hazards was inappropriate for the reasons given by Chris<br />

Lowe when the idea was first raised at the Inaugural PSWG Meeting on 18 March 2002, namely because<br />

the two aircraft were “significantly different in roles and systems”. Furthermore, the generic probability given<br />

for a coupling failure was absurdly low: 1E-6 or 10-6 = one-in-million flying hours which equated to one<br />

fuel coupling failure in approximately 66 <strong>Nimrod</strong> years. Any <strong>Nimrod</strong> line engineer would have said this was<br />

absurd, if asked. Failures of fuel couplings were not a rare occurrence.<br />

223

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