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The Nimrod Review - Official Documents

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

7.10<br />

136<br />

Following BAe’s May 1982 report, the RAF provided further information regarding the <strong>Nimrod</strong>’s operational<br />

procedures to BAe in October 1982. In light of this further information, BAe re-calculated the fatigue lives<br />

for the Cross-Feed bleed-air ducting and set out its calculations in a further report dated January 198413 . As<br />

before, a copy of this report was provided to the MOD’s RTO. <strong>The</strong> report highlighted the potential damage that<br />

could be caused by a fracture of an element of the hot air system, recognising that there “could be potential<br />

damaging to structure (spar), aircraft control systems and bomb bay loads”. 14 It concluded that, from theoretical<br />

calculations, the fatigue lives for the Cross-Feed ducting had either been exceeded (for the ducting mounted on<br />

the outboard side of rib 2) or were low (for the ducting between the two Cross-Feed air valves up to the fiveway<br />

duct) compared to the required life of the aircraft. It was nonetheless acknowledged that a “safe factor of<br />

5” 15 had been applied and that “only one serious leak has occurred”. 16<br />

7.11 In light of its findings in its January 1984 report, BAe recommended that “a programme of inspection and<br />

replacement should be initiated immediately”. 17 Subsequent documents (see below) make clear the fact that<br />

the policy of ‘replacement’ now simply referred to replacing ducts as they failed, not undertaking a structured<br />

replacement programme. It recommended that inspections for leaks should be carried out at the earliest<br />

opportunity and at every Minor maintenance thereafter, with defective ducting being replaced. <strong>The</strong> report also<br />

recommended that “a programme is initiated to provision adequate spares to support the replacement of all the<br />

hot air ducts in runs 1 and 2b18 at least once in the life of the aircraft”.<br />

7.12<br />

7.13<br />

On 12 January 1984, the <strong>Nimrod</strong> Structural Integrity Working Party (NSIWP) was informed that the January 1984<br />

BAe report “showed that many of the ducts on the aircraft had already survived for nearly twice the calculated<br />

(factor 5) life”, thus the “previous philosophy of changing at 2nd major was therefore no longer relevant.” 19<br />

To make it perfectly clear “BAe reiterated that pipes were no longer lifed but changed on condition.” 20 At a<br />

subsequent meeting of the NSIWP, the Headquarters Strike Command (HQ STC) representative stated that,<br />

while the short-term policy was to leak check, “in the longer term the policy would be to change the complete<br />

system once in the aircraft lifetime”. 21<br />

Following these reports and meetings, the MPs discussed above were introduced. <strong>The</strong>se MPs appear to have<br />

been successful, in that there have been no catastrophic failures of ducts in the areas which they addressed;<br />

however, as was discovered after the XV227 incident, the only pressure test of the SCP system aft of the<br />

PRSOV was conducted after Major maintenance. It would further appear that, in accordance with the BAe<br />

recommendation on spares provision, in February 1984, HQ STC initiated urgent provisioning action for 20<br />

aircraft sets of spare ducts.<br />

7.14 <strong>The</strong> long-term aspiration to replace the ducts was still being advertised by HQ STC in October 1984: “the EA’s<br />

long term policy is to replace all the ducts concerned at least once during the remaining in-Service life of the<br />

<strong>Nimrod</strong>”. 22 However, whilst the ensuing years saw continued discussion of a proposed replacement programme<br />

for the ducts, 23 it never in fact materialised. This may well have been at least in part due to the low number of<br />

leaks detected during testing. For example, a report of the <strong>Nimrod</strong> Aircraft Engineering Defect Investigation<br />

Team (NAEDIT) in 1989 noted that “It appears that the resources expended on applying [the leak checks of the<br />

high pressure duct system] have yet to find faults consistent with the concern expressed by the DA [BAE] over<br />

the fatigue life of the ducting.” 24 Given that this report was produced almost seven years after the initial BAe<br />

report highlighting that many of the ducts had passed their fatigue lives, the MOD’s questioning approach to the<br />

initial BAe recommendations is perhaps understandable, if not wholly justifiable. However, despite its apparent<br />

13 BAe report 801/MAN/DES/277, dated January 1984.<br />

14 Ibid, paragraph 3.2.<br />

15 Ibid, paragraph 4.2.<br />

16 Ibid, paragraph 4.3.<br />

17 Ibid, paragraph 5.1.<br />

18 <strong>The</strong> Cross-Feed system, from the engines to the 5-way duct.<br />

19 Minutes of the NSIWP held on 12 January 1984 (DD <strong>Nimrod</strong> 16/19, dated 18 Jan 1984).<br />

20 Ibid.<br />

21 Minutes of the NSIWP held on 30 October 1984 (DD <strong>Nimrod</strong> 16/19, date indecipherable).<br />

22 STC/13004/7/1/ Strike Eng 21a, dated 9 October 1984.<br />

23 For example, in April 1988, the MOD was still stating that “a programme to replace [25 hot air ducts] will be implemented at Major servicing”:<br />

STC/13004/7/1/Srt Eng 21a, dated 7 April 1988.<br />

24 NAEDIT/1505/88/21/Task (Ao1124), dated 22 Mar 1989.

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