COURT OF APPEAL (CIVIL DIVISION)
ON APPEAL FROM THE HIGH COURT OF JUSTICE
QUEEN'S BENCH DIVISION COMMERCIAL COURT
Mr Justice Morison
Strand, London, WC2A 2LL |
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B e f o r e :
LORD JUSTICE THOMAS
and
LORD JUSTICE WALL
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Sunrock Aircraft Corporation Limited |
Respondent |
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- and - |
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Scandinavian Airlines System Denmark-Norway-Sweden |
Appellant |
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Smith Bernal Wordwave Limited, 190 Fleet Street
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Akhil Shah (instructed by Messrs Simmons & Simmons) for the Respondent
Hearing dates : 10 and 11 July 2007
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Crown Copyright ©
Lord Justice Thomas:
"In other words, having procured Sunrock to accept re-delivery of the aircraft before these issues were resolved, by entering into the re-delivery agreement, SAS thereafter reneged on the agreement for no good reason other than, I infer, that they calculated they had a better chance of persuading a court to their view of the proper construction of the Lease than persuading an informed expert."
i) What was the obligation under the redelivery clause in respect of the LLPs? The judge decided this issue in favour of Sunrock and concluded that $1.762m was due to them on aircraft 1 and $1.976m on aircraft 2. The issue is one of construction of the terms of the lease.
ii) Were SAS in breach of the redelivery clause of the lease and the dispute resolution agreement in relation to the scab patches on aircraft 1 and, if so, what was the measure of damages recoverable for the breach? Could a greater measure of damages be recovered for breach of the dispute resolution agreement? The judge also decided these issues in favour of Sunrock. He concluded that, as the expert would have awarded the amount of the cost of the repairs in respect of the scab patches, the sum of $139,800 claimed as the cost of repairs should be paid as damages for breach of the dispute resolution agreement. This issue turned on the evidence before the judge and a short point of law.
(1) The issue in relation to LLPs
The factual background
i) LLPs: These are the engine parts on which the engine manufacturer in conjunction with the regulatory authorities imposes a maximum life, as they are critical to the operation of the engine and the effect of failure could be catastrophic. If LLPs are damaged, they must be repaired or replaced. But even if undamaged, they must be replaced at the end of the set life time; the set life time is calculated by reference to the number of cycles of landings and take offs, as it is at these times that the engines are subject to the greatest stresses. Some LLPs for obvious reasons have a life designed to last beyond the life of the engine – 25 years or more. The total value of the LLPs in an engine represents about 40% of the value of that engine when new.
ii) On-condition parts: parts that remain in the aircraft and can be restored and repaired until their condition requires their replacement; they have no finite life measured in hours or cycles.
iii) Consumables: Parts such as replaceable seals and washers.
The nature of the dispute
"b) Components:
(i) each and every life-limited component shall have not less than 4,000 hours remaining to the next scheduled removal under the Lessee's Approved Maintenance Programme
…..
c) Engines:
Each Engine shall be serviceable and no individual engine shall have less than 4,000 operating hours remaining before its next scheduled removal limit or its next shop visit (as measured by its most limiting component).
If the aircraft was not in the condition required by sub-clause 19.2, the lessor was entitled to require the lessee to rectify any defects or deficiencies.
"(a) The Lessor and the Lessee agree that adjustment payments will be made based on the maintenance status of the Aircraft at re-delivery, and:
(i) in the case of the airframe, "half time" (which shall be calculated by reference to the amount of time remaining before the next scheduled "S4C" check, as determined by Boeing's manufacturer's planning document), or
(ii) in the case of the Engines and Landing Gear, the maintenance status of the same at Delivery.
Adjustment payments will be made by the Lessor to the Lessee if the maintenance status of the Airframe, Engines and/or Landing Gear (as the case may be) is better than the applicable status specified in paragraph (i) or (ii) above and adjustment payments will be made by the Lessee to the Lessor if the maintenance status of the Airframe, Engines and/or Landing Gear (as the case may be) is worse than the applicable status specified in paragraphs (i) or (ii) above.
(b) The amount of the adjustment payments referred to in clause 19.9(a) shall be determined by the Lessee choosing three facilities, each of which shall be a third party Federal Aviation Administration approved repair station (at least one of which will be European and two which shall be primarily based in the U.S.A.) from which Lessor will choose one based in the United States (for each of Airframe, Engines and Landing Gear) to provide the scope and work standards for each overhaul. Lessee will then choose two of the three Federal Aviation Administration approved repair stations quotes (one of which must be European) for such applicable work. The average costs of these two facilities shall provide the basis for adjustment payments between Lessor and Lessee."
i) It was common ground that the task under sub-clause 19.9 involved a comparison between the maintenance status on redelivery and, in the case of the engines and landing gear, the maintenance status on delivery.
ii) It was also common ground that the adjustment referred to under sub- clause 19.9 did not require an actual overhaul to take place on or about the time of redelivery.
iii) The parties agreed the amount of the adjustment in respect of the fuselage, the landing gear and the on-condition part of the engine, but not in respect of LLPs.
iv) It was common ground that LLPs are the subject of maintenance, but the parties disputed what was meant by "maintenance status" in sub-clause 19.9.
v) It was also common ground that none of the LLPs actually required replacement at the next overhaul of the engine by reason of the expiry of their life limit. The LLPs on the aircraft had been properly maintained under clause 13 and had a significant proportion of their life still available.
vi) Sunrock, however, contended that an adjustment was required for the LLPs under the terms of sub-clause 19.9 in respect of that proportion of the life of the LLPs used during the lease. SAS disputed this. On this issue of construction the contentions of the parties were:
a) The essence of Sunrock's contention was that as the clause required the adjustment in respect of the engines to be made on the basis of maintenance status at redelivery and delivery, this meant that SAS was required to bear the cost of putting the maintenance status of the engines into the same status as that status was on delivery. In respect of LLPs this entailed an adjustment calculated by reference to the proportion of the lifetime of the LLPs used during the period of the lease; as a proportion of the life had been used since delivery, the maintenance status of the LLPs at redelivery could only be compared with the status on delivery by reference to the cycles used and an adjustment being made on that basis. Sunrock did not shy away from accepting that this was in fact an additional payment for use calculated by reference to the life of the LLPs.b) SAS contended that they were not obliged to make any such payment; their obligation was limited to making an adjustment by reference to what would ordinarily be described as the maintenance of the aircraft and the work that would actually have to be done on an overhaul of the engine as provided for in sub-clause 19(b).vii) The terms of the redelivery agreement dated 4 November 2003 did not affect the issue of construction, only the process for its resolution. As I have said, SAS refused to abide by the terms of the agreement and hence Sunrock had to bring these proceedings.
The approach to the issue: the so called "commercial background"
My conclusion on construction
i) SAS was required by sub-clause 13.1(c) to ensure that the aircraft was maintained, serviced, repaired and overhauled in accordance with the manufacturer's Approved Maintenance Programme so that the aircraft was kept in as good an operation condition as on delivery, "fair wear and tear excepted".
ii) SAS was obliged by sub-clause 13.1(d) in respect of the aircraft, the engine and its parts at its own expense to replace any part which might from time to time be worn out, lost, stolen, destroyed, damaged or rendered unfit for use.
iii) SAS was entitled under the same sub-clause to remove any engine or part provided it replaced it as promptly as possible; the sub-clause provided:
"Each Replacement Engine or Part shall be free and clear of all Encumbrances other than Permitted Liens and shall be in as good operating condition as, and shall have a value substantially equal to or greater than, the Engine or Part replaced assuming such replaced Engine or Part was then of the value and in the condition and repair required to be maintained by the terms hereof."iv) SAS were entitled by sub-clause 13.3 to pool parts and engines.
i) The phrase "maintenance status" must be interpreted by reference to the obligations under the other provisions of the lease. As set out above, SAS was under an obligation by sub-clause 13.1(c) to comply with the Approved Maintenance Programme. This was defined by clause 1 to mean the maintenance programme for aircraft with engines of the type fitted which had been approved by the regulatory authorities of the state of the aircraft's registration. It encompassed:
"scheduled maintenance (including block maintenance), condition monitored maintenance and on-condition maintenance of Airframe, Engines and Parts of the Aircraft including, but not limited to, servicing, testing, preventive maintenance, repairs, structural inspections, system checks, overhauls, approved modifications, service bulletins, engineering order, airworthiness directives, corrosion control, inspections and treatment. "ii) As set out at paragraph 11, maintenance programmes required aircraft to undergo overhauls for such work at given intervals. The obligation to maintain applied to the engine as a whole and to its parts; the maintenance status in paragraph 19.9 also plainly referred to both the engine as a whole and its parts. As is also set out at paragraph 11, LLPs are serviced and it is plain that such servicing was maintenance of the LLPs.
iii) The Aircraft Transfer Receipt on delivery set out as "the time since overhaul", the number of cycles and hours since the last overhaul; it would have been known what was done on that overhaul. The time of the last overhaul before redelivery was known as was the time when the next overhaul after redelivery would be required and what was to be done then in accordance with the Approved Maintenance Programme.
iv) Redelivery could well occur at any point of time between such overhauls. If it was redelivered just after an overhaul, Sunrock would, absent adjustment, have the benefit of a longer period before the next overhaul; if it was redelivered as close to the next overhaul as was permitted by the obligation under clause 19.2(b) (i), Sunrock would have a disadvantage of having to see to the overhaul in the immediate future.
v) It made obvious commercial sense to provide for an adjustment to take place by reference to a comparison as at delivery and at redelivery in the timing and work required for maintenance at such an overhaul.
vi) Looked at in this way, the phrase maintenance status plainly refers to the position of the aircraft in relation to the time between overhauls and what needed to be done at that overhaul.
vii) That this is so is clear from the terms of sub-clause 19.9(b) which contemplated obtaining quotations for the cost of the "applicable work". Thus although no actual overhaul was to take place on redelivery, the costs were to be calculated by reference to what would be done on the overhaul of the engine; it was for this reason quotes were to be obtained from the facilities. Apart from servicing the LLPs in the way described in paragraph 11 above, none would be replaced, unless they needed replacing (either because of damage or the expiry of their life) on that overhaul. It is self evident that the calculation of usage of an LLP for the purpose of calculating the cost of its usage is not what would happen on an overhaul and it is not "applicable work" in any sense of the term; the only work would be servicing and that as I have said is the maintenance of the LLPs. The term cannot extend to their notional replacement.
viii) The ordinary definition of maintenance is keeping in good condition or repairing regularly and thus the phrase "maintenance status" as ordinarily understood accords entirely with the meaning which I consider it bears under the contract.
ix) Although sub-clause 13.3 of the lease gave SAS the right to pool parts and to change the engines, the position of Sunrock was protected by the provisions of clause 13 which, as I have set out at paragraph 21.iii) above, required SAS to replace what was removed with what was at least as good.
i) It gives the word maintenance a construction that its ordinary meaning and its meaning under the lease plainly does not bear. Nothing was to be done to the LLPs by reference to the ordinary meaning of the word or the meaning used in the definition clause in the contract.
ii) Although I accept as self evident that the purpose of maintenance is to ensure safety and serviceability and that replacement of LLPs on the expiry of their life will be part of that maintenance, it is also self evident that the maintenance of LLPs does not include their replacement until their life expires or they are damaged; their maintenance is their servicing as described in paragraph 11. I reject as an artificial construct the argument that a maintenance cycle has two elements – the time for regular overhauls for on-condition parts and the fixed time for the replacement of LLPs; the artificiality of the construct is exemplified by the fact that LLPs need maintenance, such as cleaning and being given protective coatings, on the regular overhauls at which the whole engine, including the on-condition parts, is maintained.
iii) Although as I have said it was common ground that there was to be no actual overhaul on redelivery, it is clear that the costs were by the terms of sub-clause 19(b) to be calculated by reference to the applicable work for the next overhaul. A notional cost of replacement based on the percentage of time used during the lease could not be part of the applicable work at that overhaul, as no LLP was to be replaced and hence no work was to be done.
iv) I also reject the argument that the overhaul referred to in sub-clause 19.9(b) was not the next scheduled overhaul, but was, as respects LLPs the replacement of the LLPs as and when their life expired. It was accepted that the replacement of LLPs would be over a period of years stretching into the future. The clause contemplated quotations being obtained for the applicable work at the overhaul of the engine. That plainly provides for a single overhaul and not a series of notional overhauls as and when the life of the LLPs expired.
v) The interpretation contended for by Sunrock deprives the meaning of "fair wear and tear" of all content. It was suggested that the phrase applied to on-condition parts and not to LLPs; there is no reason for such an approach. It seems to me that fair wear and tear is naturally applicable to the gradual expiry of the life cycle of LLPs.
vi) The argument, in short, had nothing to do with adjustments for maintenance status which was the subject of sub-clause 19.9; it was simply a clever attempt to obtain more money for the use of the aircraft.
(2) The scab patches
The measure of damages for breach of the lease
"Damages are designed to compensate for an established loss and not to provide a gratuitous benefit to the aggrieved party from which it follows that the reasonableness of an award of damages is to be linked directly to the loss sustained. If it is unreasonable in a particular case to award the cost of reinstatement it must be because the loss sustained does not extend to the need to reinstate."
Second, a passage in the speech of Lord Lloyd of Berwick at page 366; he referred to the judgment of Cardozo J in the Court of Appeals of New York in Jacob & Youngs v. Kent, 129 N.E. 889 and then continued:
"Cardozo J's judgment is important, because it establishes two principles, which I believe to be correct, and which are directly relevant to the present case; first, the cost of reinstatement is not the appropriate measure of damages if the expenditure would be out of all proportion to the benefit to be obtained, and, secondly, the appropriate measure of damages in such a case is the difference in value, even though it would result in a nominal award."
The measure of damages for breach of the agreement to refer the dispute for expert determination
"In my judgment, there is every good reason to consider that had SAS not reneged on clause 19.7 of the Lease [and an equivalent provision in the Redelivery Agreement] an expert third party would have approached the matter as did Mr Seymour; that is, they would have adopted a repair value since it is difficult to say whether the scab patches had or would have any impact on the marketability of the aircraft. The clauses were aimed at providing a quick and easy monetary value on items in dispute on redelivery. In my judgment, it was in the contemplation of the parties that an expert determination would adopt a cost of repair methodology and that it was intended that financial adjustments should be made on that basis. That approach would obviate the need for research into market values and is a simple approach within the spirit of the mediation provisions.
In my judgment, to put the parties into the position they would have been in had SAS complied with their obligations under clause 19.7 and the Redelivery Agreement, an award of compensation on the basis of the cost of flush repairs would be appropriate. … It follows, I think, that Sunrock are entitled to judgment for the sum of US$139,800 as damages for breach of their obligation to participate in the mediation processes which they had agreed to.
Conclusion
Lord Justice Wall
Lord Justice Ward