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You are here: BAILII >> Databases >> England and Wales High Court (Commercial Court) Decisions >> Lombard North Central Plc & Anor v Airbus Helicopters SAS [2020] EWHC 3819 (Comm) (26 November 2020) URL: http://www.bailii.org/ew/cases/EWHC/Comm/2020/3819.html Cite as: [2020] EWHC 3819 (Comm) |
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BUSINESS AND PROPERTY COURTS
OF ENGLAND AND WALES
COMMERCIAL COURT (QBD)
Fetter Lane London, EC4A 1NL |
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B e f o r e :
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LOMBARD NORTH CENTRAL PLC NATWEST MARKETS PLC |
Claimants |
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- and - |
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AIRBUS HELICOPTERS SAS |
Defendant |
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MR M. REEVE (instructed by Knights plc) appeared on behalf of Defendant.
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Crown Copyright ©
MR JUSTICE BRYAN:
(1) Pursuant to the purchase agreement, Airbus was subject to obligations and/or liabilities under French law in respect of the helicopter, including:
(a) A statutory warranty against hidden defects rendering the helicopter unfit for its intended use. Airbus admits the existence of the statutory warranty, but there is a dispute as to its scope and Airbus contends it was, in any event, excluded by agreement.
(b) An obligation to exercise prudence, monitoring and vigilance as to the safety of the helicopter. Airbus denies that any such obligation arose in relation to this helicopter.
(2) Pursuant to the novation agreement, Airbus assigned those French law obligations and/or liabilities to RBS Aero. Airbus dispute this.
(3) Further or alternatively, it was an implied term of the novation agreement that MSN2707, i.e. the helicopter, would be of satisfactory quality. Airbus denies any such term was implied.
(1) On 1 April 2009, G-REDL, an Airbus AS332 L2 helicopter, crashed with 16 fatalities. The AS332 L2 is a predecessor to the H225, and in particular has an identical "epicyclic module," a component of the main gearbox. An investigation found that the crash was caused by a fatigue fracture in a "second stage planet gear" within the epicyclic module, which caused the main rotor to detach.
(2) In 2012 there were two non-fatal incidents involving H225s (G-REDW and G-CHCN). In each case the main gearbox lost oil pressure and the helicopter had to be ditched in the North Sea and evacuated. There is a disagreement as to whether these incidents are relevant.
(3) On 29 April 2016, LN-OJF, an Airbus H225 helicopter, crashed with 13 fatalities. An investigation found that, like the G-REDL incident, this crash was also caused by a fatigue fracture in a second stage planet gear within the epicyclic module, which caused the main rotor to detach.
(i) The maintenance and airworthiness of the gearbox and monitoring systems of G-REDL prior to 1 April 2009, the accident investigations in respect of that aircraft between 1 April 2009 and 24 November 2011, and the accident report published on 24 November 2011.
(ii) The maintenance and airworthiness of the gearbox and monitoring systems of G-REDW prior to 10 May 2012, the accident investigations in respect of that aircraft between 10 May 2012 and 11 June 2014.
(iii) The maintenance and airworthiness of the gearbox and monitoring systems of LN-OJF prior to 29 April 2016, the accident investigations in respect of that aircraft.
"Were the second stage planet gears of the epicyclic module of the MGB of the H225 type susceptible to fatigue fractures as a result of (a) their design, and/or (b) the serviceable life of second stage planet gears before mandatory replacement being set too high."
In answer to the question, "Is this issue agreed"? the response of the defendant was, "No, as expressed, an expert question", and the defendant suggested a disclosure issue as follows:
"When designing the MGB of the H225 type and setting the serviceable life of the second stage planetary gears, what assessment did the defendant in fact make of the risk of fatigue fractures?"
It will be seen that the focus of that categorisation of the disclosure issue is by reference to the design.
"MSN 2207 and all H225 helicopters were defective in their design so as to render them unfit for their intended use, being the long-range transport of passengers in the offshore oil and gas market. The nature of the defect, as found by the AIBN in its report summarised at paragraph 25 above, was as follows:
PARTICULARS OF THE DEFECT
(1) The second stage planet gears of the epicyclic module of the MGB were susceptible to fatigue fractures, as a result of:
(a) the design of the MGB and second stage planet gears; and(b) the serviceable life of second stage planet gears before mandatory replacement being set too high and at an unsafe level."
So, it will be seen that the plaintiff's formulations very much track that pleaded case at para34(1). Indeed, Mr Reeve's criticism of that is that it is merely a track of the pleaded issue and not what documents may be relevant and the crystallisation of the formulation as a disclosure issue, which he says involves you standing back and looking at what sort of documents there actually are.
"...the Pilot Scheme for Disclosure was not a re-serving of CPR Part 31, exemplified by standard disclosure (equivalent to Model D Extended Disclosure CPR PD 51U), dressed in another garnish. Rather, the Pilot Scheme represents a 'culture change' to the management and disclosure in the Business and Property Courts."
And with the exponential growth of storage, etc., there is a recognition that in many cases a 'leave no stone unturned' approach to disclosure is no longer appropriate.
"Model C in one sense occupies an implicitly preferred position within the choices available amongst the Extended Disclosure models in that the more expansive models of Extended Disclosure, Models D and E, should be selected by the parties and approved by the court where Model C is not appropriate or sufficient (paragraph 6.5 CPR PD 51U). Indeed, the wider Models D and E are not presumed as the appropriate models for Extended Disclosure (paragraph 8.2 of CPR PD 51U)."
Transcribed by Opus 2 International Limited Official Court Reporters and Audio Transcribers 5 New Street Square, London, EC4A 3BF Tel: 020 7831 5627 Fax: 020 7831 7737 [email protected] |