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exmpa

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  • in reply to: The (even more) merged Vulcan thread once again. #1266522
    exmpa
    Participant

    I posted the reply below on a previous Vulcan thread. It seems to me as apposite now as it did then.

    “I am not surprised by this latest turn of events. I have always been highly sceptical about the viability of the project and nothing would ever induce me to make any commitment to it, financial or other. I always wondered about the nature of the support that the ‘558 project attracted until I attended the V-Force reunion at Newark a couple of years ago. What struck me was that those most enthusiastic for it had little or no significant commercial aviation experience. The more exposure people had had to the harsh realities of aviation business, the less likely they were to see the project as viable. Why were voices not raised? Quite simply the “enthusiasts” did not want to hear what you said. If you disagreed with them, then you were disloyal. So, most just kept quiet and let them get on with it. Just to establish my credentials to hold an opinion, I did fly the Vulcan; I last flew it in 1972; and I did display it. I left the RAF after 20 years service and am still flying large aircraft professionally.”

    exmpa

    in reply to: Compensation #558289
    exmpa
    Participant

    Vrede,

    Start by following this link Air Transport Users Council

    exmpa

    in reply to: Esperia Air at MME & Manston #559015
    exmpa
    Participant

    If anyone believes that this is “real” then just try and crew the schedules. It can’t be done.

    exmpa

    in reply to: Small long-haul mess @ bmi! #566358
    exmpa
    Participant

    And it gets worse!!

    http://www.belfasttelegraph.co.uk/n…sp?story=699279

    and everything published in the newspapers is totally accurate and entirely without embellishment…..

    exmpa

    in reply to: Risk Assessment #1295831
    exmpa
    Participant

    The Fauld Explosion

    If you are ever in the Burton-on-Trent area a diversion to visit the Fauld Crater is worthwhile. Over 60 years on there is quite a lot of vegetation encroaching now so the crater is not as dramatic as it once must have been. However you can still make your way to the edge (signposted from the village) and stand there observing a hole of “nuclear” proportions. Sobering thought is that it appeared all of a sudden one November morning!. The pub in the village has a good display of contemporary photos as well as a fine pint.

    exmpa

    in reply to: Risk Assessment #1296395
    exmpa
    Participant

    This may be of interest

    The Fauld Explosion

    exmpa

    in reply to: Jet Provost 'wheels up' 7/7/06. #1304506
    exmpa
    Participant

    Check the Manual for details. Chapter 4, para 15.

    I regret that I no longer have an aircrew manual for the JP (or pilots notes as it was called when I first flew it) so I shall take your word for what it says. I do however know what I used to be able to do to show the inadequacy of the warning system.

    exmpa

    in reply to: Jet Provost 'wheels up' 7/7/06. #1304511
    exmpa
    Participant

    The flag has absolutely nothing to do with the button position.

    As you wish. I wonder how I managed to demo it all those times on E of C 2 then? Reduce speed until the flag appears, press the button partially and it disappears. No other gear indications.

    I should add that it worked on the 3,3A,4,5 and 5A and having just checked my log book I see that I was given E of C 2 as the primary exercise on my my A2 ride, so I guess that the trapper thought it was OK as well.

    exmpa

    in reply to: Jet Provost 'wheels up' 7/7/06. #1304670
    exmpa
    Participant

    Despite their relative age, the JP does have a gear warning system, which consists of a white U/C flag in the airspeed indicator when the speed drops to below around 120 knots without the gear being extended

    Not quite true Trinny. The first movement of the down button isolates the warning flag not the gear actually being down. It’s really not worth having, the absence of the flag is no substitute for 3 green lights.

    exmpa

    in reply to: Uni Project Idea #589260
    exmpa
    Participant

    I need something that I can effectively research-analyse-design-test-analyse-conclude based on an aeronautical engineering subject.

    OK how about this one:

    On modern airliners the use of autobrake systems is encouraged because of reduction in break wear and improved passenger comfort. Current systems operate by providing a number of predetermined decelleration rates. With ever rising levels of air traffic there is pressure to increase flow rates and achieving minimum runway occupancy times after landing is an integral element of this strategy. Unfortunately the runway exits are not always in the optimum positions or of the best configuration to achieve this objective (e.g. 90degree turn off must be taken slower than a 40degree exit). An autobrake system which could be programmed to provide a constant decelleration rate to the required exit speed for a specific exit could be a valuable tool in the quest for improved runway usage.

    In short what I am suggesting is a “dial a landing distance” autobrake system which takes into account the type of turn off to negotiated. Now I am not suggesting that it is really a gap in the market which airlines will beat a path to your door to buy! But it is the kind of thing which might make a good project.

    exmpa

    in reply to: Uni Project Idea #589489
    exmpa
    Participant

    The Tail Brake Chute (TBC) was a product of its time. In the 1960’s military aircraft in particular were operating with total energy values which were close to the limits of the braking systems available. The addition of the TBC increased the safety margins for takeoff and landing but routine operation was never based upon the serviceability of the TBC in the same way that current philosophy does not assume any reverse thrust on a rejected takeoff or normal landing. So, the TBC would always be a “bolt on goody” and could not be used to provide ehanced takeoff or landing performance.

    To go back to your original proposal, its use solely as an emergency stopping device. Landing performance is calculated with a number of safety margins included, reported headwind component is factored down and tailwinds are factored up, landings are presumed to be made in a “touchdown zone” and not at specific point, allowance is made for some speed deviation over the runway threshold. So there is a good deal of margin already built in, but as we have seen this does not cater for the gross excedeance cases. When deciding the worth of fitting a TBC you would have to assess rate of gross excedeance incidents and show that the your system would be of positive benefit. Problems you would have (in no particular order):

    A. Weight penalty, not just of the installation itself but the additional structure to cope with the deployment forces.

    B. Cost, not only purchase and provision but in service maintainance.

    C. Operational factors, reduction in allowable crosswind component if use of TBC is predicated.

    D. Aerodynamics, the TBC is a Zero Lift Drag (ZLD) device. Its effectiveness is greater at high speed (varies as Vsq)[Think of the Drag equation] so to get best effect is must be deployed as early as possible.

    E. When and how are you going to decide to use it? For a TBC to be effective in an unpremeditated situation (viz, AF A340) you would require some kind of assessment of current decelleration/runway length remaining/remaining brake energy capacity. If a TBC was fitted and used late it is really of no greater benefit than not having one in the first place.

    F. The brake energy capacity of modern aircraft is enormous. Modern carbon or ceramic brakes are incredibly efficient, so much so that is very unusual to find that Brake Energy is the limiting factor in a performance calculation.

    Where does that leave things? Probably with the conclusion that fitting TBCs to modern airliners would only be of benefit in an extremely small number of cases. It is therefore probably more beneficial that any investment be made in systems which would ehnace safety in event of more frequent occurrences.

    exmpa

    in reply to: Shackleton Mystery (Long-lived thread) #1253947
    exmpa
    Participant

    Crisp Monster

    I cannot claim any specific knowledge of the incident you refer to, my maritime days were long after that, but the loss of the two 42 Sqn aircraft was always cited as prime example of the importance of rigidly adhering to “boundary procedures” to avoid confliction between aircraft operating in adjoining areas. So, let’s look at the circumstances in general terms:

    Two large, modern (at the time) aircraft with eighteen highly trained crewmen vanished without a trace.

    Yes modern but with pretty basic navigation equipment by current standards. Not difficult to be 10 or more miles away from where you meant to be (cf the 8 Sqn AEW Shack which flew into one of the Scottish islands 30 years later). The rapid fixing aid of the time was GEE, not much use at low level, and LORAN had limited coverage in the Southwest Approaches (SWAPPS).

    What seems peculiar about the collision explaination is this; why would maritime patrol aircraft be flying in formation in the middle of the sea and in the middle of the night? It would seem to serve no purpose. Surely this sort of aircraft operates alone in order to cover the maximum amount of ocean. If they were not in formation but happened to “bump” into one another, this would seem extremely unfortunate considering the size of the Irish Sea and the fact that both aircraft were equipped with radar.

    They wouldn’t be in formation; but consider this; if there is a potential target within the detection range of two aircraft, then it is quite probable that both will detect it at a similar time. Why can we say this? Because both aircraft will have optimised their tactics against the same type of target. So one can imagine the situation where both aircraft have a significant nav error, neither believes they are close to the buffer zone between their area and that of the other aircraft. They are both operating the same radar policy, say intermittent all round scan and a possible target is detected. Both aircraft independently turn on and commence a radar homing. the radar they are equipped with is the ASV21, a pretty basic set and optimised against small surface targets, not airborne targets. The aircraft nav lights are also pretty basic, no anti-collision lights and fairly dim nav lights. But who’s looking for nav lights anyway? There’s a possible target out there! ESM I hear you say? Again, if fitted, optimised against target emitters, not friendly sets and much more labour intensive than today’s kit or even the ARAR/ARAX of the Nimrod. So the scene is set for disaster over the target datum when the 2 aircarft arrive at abot the same time and collide. That I believe was the opinion of the Board of Inquiry (BoI)

    why was no wreckage ever found? A searching aircraft apparently sighted orange wreckage floating on the sea around this time, but as this was not recovered due to the weather it could not be proven to come from the aircraft. Presumably a mid air collision would scatter wreckage over a wide area, and one imagines at least some of it would float.

    The Shackleton operated at low level and low speed, any wreckage area following a collision would be small. As to why none was found, who knows, weather and sea state, the fact that the aircraft quite possible hit the sea largely intact but sank very quickly. Believe me, there was precious little on the surface when the Air India 747 went in West of Ireland. Were the search aircraft looking in the correct area?

    One assumes these aircraft would have been visible on radar at some point, unless of course they were flying at very low level. None of the sources I have looked at in researching this have mentioned whether they were tracked at any point, but if they were not then this again suggests a collision at low level.

    Not a lot of radar coverage in the SwAPPS in those days, the threat axis was from the East. Highly unlikely that they were seen by any agency.

    It was noted in this article that an engine from one of the aircraft was trawled up in 1966, 11 years after the disappearence and some 100 miles NNW of the area the Shackletons were supposed to be operating in. This would indicate that either the current in this area is strong enough to move an engine several tons in weight many miles, or that at least one of the aircraft was way off course.

    Well, the current would certainly not move an engine that distance! Nav error? Possible that a gross error could be made, confusion over the assigned area, it’s happened before, plus a plotting error it could add up. But 100 miles is the best part of 30 minutes flying in a Shackleton at low level, so who knows? Any way, by 1966 did anyone look particularly closely at the find and its position? Did the fisherman know where he was anyway? I did enough SAR missions to find fishing boats to have a healthy scepticism about their navigation (this was in the pre Omega/GPS days).

    So in summary, by modern standards it seems incredible that two aircraft should collide over the ocean. By the standards of the time, 10 years after WW2 and still using the equipment of that period it becomes more understandable. All in all a tragic accident in a time when such events were relatively common.

    exmpa

    in reply to: Vulcan Display Pilot #1260124
    exmpa
    Participant

    Come on Moggy when are you going to merge this one?????

    I am sorry Denis, but I cannot see the connection between your post and the question posed by Black Knight. Could you please explain.

    Thank you
    exmpa

    in reply to: Vulcan Display Pilot #1262061
    exmpa
    Participant

    He got an OBE as well.

    Maybe so; although I am not certain of its relevance; but I am not entirely sure that he has a licence.

    exmpa

    in reply to: Vulcan Display Pilot #1262460
    exmpa
    Participant

    Paul is already “North” of 60 and would he want it anyway?

    exmpa

Viewing 15 posts - 256 through 270 (of 299 total)