Helicopter capability - Defence Committee Contents


Examination of Witnesses (Questions 20-39)

MR NICK WHITNEY, MR DAVID PITCHFORTH, MR DEREK SHARPLES AND MR ALEX SHARP

19 MAY 2009

  Q20  Mr Hancock: Is there insufficient resources going in then from the MoD to ensure that spare parts are available for this number of aircraft to be regularly in combat?

  Mr Whitney: I think it is difficult to state precisely whether there is insufficient. There are challenges in terms of—

  Q21  Mr Hancock: Where is the problem then? We put these operational aircraft in doing more than they were originally meant to do and far sooner, but we did not supply enough resources to make sure that they were always able to fly—very fast turnaround over maintenance issues. Who is responsible?

  Mr Whitney: It is not just spares; you have to look at all of the lines of development. Your training infrastructure has to be capable of producing pilots; your training infrastructure has to be capable of producing the technicians and maintainers. It is not just about spares supply.

  Q22  Mr Hancock: It is no good having well-trained pilots and crews, if you have not got Merlin gearboxes, is it?

  Mr Whitney: No absolutely. It is no good having aircraft either if you have not got the pilots: the whole lot has to come together to give the effect.

  Q23  Mr Hancock: How do we get over something like the ongoing failures of Merlin gearboxes?

  Mr Whitney: In cases of ongoing failures—and I do not recognise "ongoing failures of Merlin gearboxes", but we have got some specific instances—

  Mr Hancock: When you say you "do not recognise" it, would you say there is not a disproportionate number of gearboxes on the Merlins that fail?

  Q24  Chairman: Let us allow Mr Whitney to answer that question.

  Mr Whitney: I think what I was going to go back to was the method of contracting now in a long-term support arrangement—we call then the IOS; the Integrated Operational Support arrangements—incentivises industry to put these issues right, to buy the correct number of spares. Derek was absolutely right: the challenge is to understand your spares requirements and get the spares on the shelf; clearly not to carry too much inventory—there is a cost and it is driven as a result of that—but to carry enough; to have those spares at the right level of assembly. With the new contracting methods, there is incentivisation on the industry to improve the product through-life. Previously that has not happened, and I think that is where there should be confidence that things are improving and getting better. You will always have instances on helicopters where a certain failure that has not been predicted will cause an issue, and we have to work our way round it. These long-term support contracts equally allow that to happen with much greater urgency and much greater effect.

  Mr Hancock: Why is there then a substantially higher failure of the Merlin gearboxes?

  Q25  Chairman: Would you recognise that there was a substantially higher failure of Merlin gearboxes?

  Mr Whitney: In comparison to what?

  Q26  Mr Hancock: Other aircraft?

  Mr Whitney: I would have to go and examine the figures for that, and I am not in a position to quote.

  Q27  Mr Hancock: We suggest to you there is, but you would not think that? That does not strike you as something you are familiar with?

  Mr Whitney: I am familiar with the fact that the gearbox on the Merlin has had some issues in the past in terms of lifing of components. When you develop an aircraft and you develop new components you start off with the life of a component and you test it and you increase that through-life. That has not taken place in the manner that perhaps we predicted, and that may be a problem to which you refer. Components are being changed—not through failure but through the need to change components on life. In maintaining airworthiness on a helicopter you sometimes give components lives and you change them before those lives expire—that is how you maintain safety. That is something I could recognise, but I would need to come back to you with the exact details of that if you require.[1]


  Q28 Chairman: If you could do that would be helpful. Mr Sharples wants to broaden it.

  Mr Sharples: Chairman, a general comment if I may to try to throw some light on the question. Cannibalisation is more often a problem with new helicopters entering into service than it is with those that have been in service for a number of years. The reason for that is because new aircraft that enter into service lack fleet experience; they lack flying hours; they often are subject to unscheduled maintenance, unpredicted maintenance, which was not considered during the design phase. They often have heavy schedule maintenance programmes which are lightened as the years go by through experience; and they can also be subject to lack of technical expertise—just insufficient time in service for the technical expertise to be built. We often find that cannibalisation is more prevalent on new fleets in service than it is on old ones. I am happy to say that on the Puma fleet in the RAF, cannibalisation is not a major issue for us, because after so many years in service and more than 70 million flying hours, the Puma is a very reliable helicopter and now has had a fully mature service experience.

  Mr Hancock: Can I just ask two quick final questions. One is: I would like to know what any of you would feel can be done to improve the system, speed up the system so that the downtime on aircraft is cut; and my final question goes back to the Apache issue. The real difference here, the crux of the matter, is about this training on one type and then flying another. It is the difference between the theatre entry standard of Apache helicopters and those that are in the depth fleet; and there is a substantial difference, is there not? That must create a problem, either where they are in operational flying or in the training that pilots get to fly those aircraft. If there is a substantial difference between the two, there must be an issue there that ought to be addressed, surely?

  Q29  Chairman: Would you like to deal with that second question first and then come back at the end to what can be done to improve things?

  Mr Whitney: I will take the Apache aircraft question. I do not think the difference is substantial. Yes, there are differences in terms of some of the modifications associated around defensive aids kit and fuel tanks etc., but I do not think this is a huge burden in terms of that to which you allude. Perhaps industry is not the best judge of that; I think the military would be a much better point at which to make that question.

  Mr Sharp: Certainly I do not have the experience that you all do with the British military and how many types. I was just listening to the number of types involved and I think if you are looking for ways to increase efficiency we come back to the same point that was made before, which is: in a multi-role helicopter, if you have something that can do more than one thing, and you have many more of them, then the supply chain that will support those is going to support across a broader array. If you have one that can be used for utility, but can also be used for Medevac, but can also be used for lifting a 105 mm Howitzer and ammo then there are more of that same type, then you are driving towards having a logistics footprint that supports that one multi-role asset versus many separate types that may, through long lines of logistics, be difficult to support. I used the MRCA example previously; the US Navy followed your example and replaced some time ago all the F-4s, A-7s and A-6s with an F-18. Now on our carrier deck an F-18 is a fighter; it is an attack jet; it is an electronic warfare airplane; it is now used as a tanker and you have one basic airplane. Yes, there are some different types but the MFDs, the multifunction displays, are the same; the stick and throttles are all in the same place; the engines are the same. So you have, again, a multi-role attack at this logistics problem; and now we have downsized the logistical footprint on the aircraft carrier to support really one basic type.

  Chairman: I think we would all like many, many more in the American way, Mr Sharp!

  Q30  Mr Jenkin: On this question of supply of spare parts, how do OEMs give confidence to the MoD that battle-critical parts get priority over any other demands from any other of your civilian customers who may be more commercially valuable to you?

  Mr Pitchforth: From a Boeing perspective the UK Chinook fleet of spare parts is purely the UK Chinook fleet of spare parts. There is no cross-fertilisation with any other fleet, military or civilian. It is completely bespoke through TLCS, for the UK Chinook aircraft.

  Q31  Mr Jenkin: But that would not be true for the Merlin, would it?

  Mr Whitney: Absolutely, yes, they are military bespoke aircraft. In fact, it goes one step further in terms of the long-term support contracts because we have a joint team. The team is sat together, either at Yeovil or Sherborne, and that is a joint industry/MoD team.

  Q32  Mr Jenkin: Supposing there is a shortage of widgets on rotors, whatever it may be, and that part is sourced from some other part of the world, or another part of your Finmeccanica operation: how do you give confidence to the MoD that, when that part is needed for a helicopter—

  Mr Whitney: They are party to the dialogue that goes on. They actually see the requests being made. We have joint sessions with the companies concerned where we sit just like this; we have a meeting where the MoD are actually sat alongside us. It is not like we can hide behind anything.

  Q33  Mr Jenkin: The military get the priority?

  Mr Whitney: Absolutely. In terms of war fighting, I do not think there is any question that, when it comes to UORs or support to the front line, industry absolutely understand the urgency and need that is upon us and we stand up to deliver.

  Q34  Mr Hamilton: Could I just take that one stage further and that is about the upgrades that continually take place. I come from a background where I worked in heavy industry for 20-odd years, in the coalmine industry, and it was quite regular to upgrade as we went through heavy machinery. One of the things that comes through is, when we started to put heavy engines into machines which could not take it, we began to see the splits taking place in the casts, and the splits taking place in a number of other ways. My question is: what are the risks associated with putting a powerful engine into an old frame?

  Mr Sharp: Certainly in the US we have experienced a number of issues, and then there are workarounds to try to address those issues—the latest of which was the E-2 Hawkeye put advanced triple broad engines with new propellers on the front of them; and we had a lot of excessive vibration in the back and fretting in the back end of the airplane. Those tend to be unintended consequences of improvements to the system. My experience in the military, part of which was looking at the overhaul of fighters coming in over 55-60 months in San Diego, we had a contract with the military where we did a standard statement of work to overhaul that, ship it out, take the wings off, engines out, and get it back to the fleet all bright and shiny. Although that is a neat idea, each and every single airplane that comes through, although on the outside they look the same, when you take the turtlebacks off and you get on the inside, what has happened to each one of the airplanes or helicopters, wherever it was, is different; so the statement of work automatically mushrooms into: does this keel beam need to be replaced; does the engine need to be replaced? The cost savings of doing everything the same way off an assembly line and upgrading it is very, very difficult to quantify upfront until you actually get into the project; and once you are into the project you need a lot more money to finish it.

  Q35  Chairman: Mr Whitney, I think the Apache helicopter, which had a Rolls-Royce engine put into it for the British buy, seems to have worked pretty well with that Rolls-Royce engine?

  Mr Whitney: Indeed it has. The Rolls-Royce RTM engine is performing extremely well. It is higher powered than the American engine that was fitted, and is demonstrating that capability in theatre. However, I think the Apache was designed from day one as a crashworthy aircraft. I think the issues that you raise in terms of putting more powerful engines into older aircraft can work. You can get greater performance from an aircraft, but you have to then go back to the basic structure air crashworthiness. Certainly if we are looking at a modern aircraft, it is designed to different standards to an old aircraft, and that is where you suffer the potential downsides of just increasing the power,

  Q36  Mr Hamilton: Are you saying that modern aircraft are different in the sense they are sleeker than what the old aircraft were?

  Mr Whitney: No, the other way around. What I am saying is that a modern aircraft will be designed around the concept of having a crashworthy undercarriage that can take descent velocities much greater than older aircraft; they will have attenuating seats that take impact and allow much greater survival rates. I would not want to guess but if I looked at a 40% crash case—and when you design for a crash case there are some distinct criteria that you have to take into account; there are lots of analyses done of lots of previous crashes—the data that we design around an old aircraft would typically be a 40% survival rate against that crash case; a more modern aircraft would be circa 80%; and if I look at the future Lynx today, and the future Lynx is a good point, the old Lynx is probably a 50% aircraft; and the new future Lynx, which is a new structure, much greater descent velocity, it would be a 95% aircraft. It just gives you some analysis in terms of where you can get with modern design.

  Mr Hancock: The judgment for when an aircraft can be upgraded is a pretty fine one, is it not? Those judgments have to be pretty well analysed, do they not? You cannot just say, "We're going to upgrade a Puma", for example, without knowing the real consequences of that. Where are those judgments made? Are they made by industry or are they made by the MoD relating to the cost of either developing a new aircraft or taking a chance on upgrading?

  Chairman: I think we ought to move on because we are running out of time and I want to cover a lot more ground.

  Q37  Mr Jenkin: We are using our helicopters very much more intensively than we expected in battlefield conditions and very harsh environments. What effect do you think this has on their lifespan?

  Mr Pitchforth: Some of that depends upon whether the airframe is lifed. In the case of the Chinook if it is not we can continue to repair and maintain that aircraft throughout its life. There is an advantage also of being a member of a very large fleet. The learning on the Chinook fleet is quite extensive through the thousands of aircraft in service; so therefore many of the issues that we may see with the extra usage we can predict and/or inspect for, understanding when those issues are going to arise. The Chinook fleet is a well understood fleet with a large sample and statistically therefore we understand what is going to happen to the airframe, because these are not pressurised aircraft; they do not have the high stress issues that a pressurised fuselage does, so therefore their life is considerably greater than a pressurised aircraft.

  Mr Sharples: Just a word on the Puma fleet, if I may. I think it is fair to say that in comparison to the civilian Puma fleet, the military Puma rate of flying is not as intensive as some of the fleet leaders on the Puma fleet. Offshore, for example in the very extreme conditions in which Puma fleets are operating in the civilian world also, either in Alaska, in the Middle East, in parts of South-East Asia or, indeed, in the North Sea, to give an example, fleet leader in the civilian Puma fleet currently has more than 38,000 flying hours on the airframe. Although I cannot tell you what the fleet leader in the RAF Puma fleet is, I am quite sure it is only a fraction of that. That is to say, despite the intense use to which we put our machines in military theatre—and again I have personal experience of doing that—nevertheless these machines are built for very intensive operations; and I do not think today we are in danger of running out of the lifetime of these machines.

  Q38  Mr Jenkin: Of course, some modern airframes are lifed. Is this just the equivalent of food manufacturers putting early sell-by dates on their processed foods, so the housewife has to throw them away?

  Mr Whitney: In terms of the products that AgustaWestland support, I do not think it is. The impact on operating in an extremely harsh environment may be that some components require replacement sooner than anticipated; and in a long-term support arrangement, like IMOS, that is costing us, industry, money. The aircraft are designed to work within a flight envelope, within an environment; and, indeed, the theatre they are in is a challenging environment but it is one that they are tested and designed to operate in.

  Q39  Mr Jenkin: What is the airframe life of a Merlin?

  Mr Whitney: 10,000 hours.


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