Thanks Peter. In which case, what is it that is pictured near the top in the two photos and which you have coloured red in your picture? I had assumed this was a stiffener (like the piece found) – I am obviously missing something!!!
Mike,
Many thanks for your explanation of the rivet positions. So we seem to have a situation where there is an ‘upper’ stiffener as shown by the two photos, but without any reference to it on the Avro drawing? I am confused!!
I have been having a closer look at MikeHoulder’s Avro drawing. Peter, you have suggested that the piece we have been discussing is the stiffener shown in your picture of the rear bulkhead. Mike’s detailed drawing shows the lower fitting by the steps down into the rear of the aircraft, which can be seen in the lower of the two pictures at the top left below. This fitting appears to have an attachment for the steps. The main Avro drawing shows what I assume to be the rivet positions for the upper of the two fittings (but not the stiffener itself). I had thought that these two items would be similarly configured, but on further inspection, it seems that this may not be so.
At the bottom below (in orange) is shown the detailed Avro drawing of the piece which is nine-and-a-half inches long and with the angled indented ends. According to the drawing, the rivet positions at the point where the upper stiffener is fitted are as shown in the upper of the two diagrams below (depicted in yellow). It is difficult to read some of the measurements on the drawing, but the rivets on the two flanges of the stiffener appear to be asymmetric, with the distance between the outermost rivets in the top flange being eight-and-seven-eighths inches and that for the bottom flange being eight-and-a-half inches. This is all very curious – and the length of the fitting itself may be less than nine-and-a-half inches – but perhaps I have misinterpreted the drawing!
I have not yet heard from Laurent, who is probably having difficulty in locating our piece amongst all those in the collection. If we have identified its location correctly as being from the rear bulkhead, it seems more likely to be the upper of the two fittings, but without any measurements our potential identification may be inconclusive, particularly if the piece is fractured.
Mike – the drawing is the icing on the cake. Very many thanks for your help on this one. The chewed end of our piece may make it difficult to be certain, but everything looks right.
That’s brilliant, Peter. It looks spot on. Any chance of an unmarked higher resolution copy of the picture by e-mail, please?
And thanks again to MikeHoulder for putting us on the right track.
Many thanks for the picture, Peter. It is very helpful as it confirms that the piece we have, although identically shaped, is almost certainly too small to be one of the forward bulkhead stiffeners.
However I think MikeHoulder may have put us on the right track with his comments on Hennie’s thread. The Lancaster Manual says that the forward bulkhead is at former E. There is an armoured bulkhead at former 7, and another bulkhead at the end of the bomb compartment at former 22, presumably like the one in your photo, Peter, but with observation windows into the bomb bay? Could this mean that the bulkhead stiffeners here would be shorter? Aft of this the fuselage tapers in plan and elevation. The Manual does not refer to further bulkheads, but says that the rear fuselage is constructed in a similar manner to the rear end of the rear centre portion.
I am now wondering whether what we have is a smaller bulkhead stiffener from one of the bulkheads further aft. It would be logical for its design to be the same as that for the larger forward bulkhead stiffener – why change it – why not just alter its size to strengthen a smaller area?
So, does anybody have any drawings, diagrams, parts lists, photographs or first-hand knowledge which would confirm the existence and/or size of any such stiffeners on the other bulkheads (or elsewhere), and which they would be happy to share, please? Any help to solve the mystery would be much appreciated.
Peter,
I have been having a closer look at the indented stiffener. I do not yet have the measurements from Laurent, but I think our piece is identical to that pictured on Hennie’s thread. It seems to have seven rivets on each side, but one end appears to have fractured, making it difficult to be certain. If this is so, then, as MikeHoulder has commented on Hennie’s thread, the piece is too small to be a forward bulkhead stiffener – it seems to be about 8 inches long which is roughly one third of the size of the stiffeners illustrated in the diagram in my last post, although similar in design.
So it seems that my original question remains. Where else on the aircraft might a stiffener like this be used? Presumably on a smaller flat surface somewhere within the main fuselage? Can anyone help, please?
Bulkhead stiffener?
A long time ago in post #35 I attached some pictures of items laid out on a table at the time of our visit to France in 2012. Some recent exchanges on Hennie’s thread ‘New Member With A Lancaster Story To Tell …..’ (see my post #885 above) have sparked my interest. There is an item at the top centre of picture T4 in my earlier post which can be seen from a different angle in picture T.
I attach a close-up view of the piece in question – the picture quality leaves a bit to be desired because it is an enlarged detail from the complete photo. On the right is an Avro diagram posted by MikeHoulder on Hennie’s thread. If you are reading this Mike, first my thanks – I hope you don’t mind me copying it here, and secondly I wonder whether you, or anybody else, could help with a little more information, please. The similar item which Hennie found was thought possibly to be one of the stiffener angles from the front lower bulkhead at the back of the bomb aimer’s compartment.
The item from ED908, found where the main fuselage came to rest, appears to be a similar, but fractured, bulkhead stiffener – it seems to have the angled end at about 60 degrees to the vertical as shown in the diagram. However, I fear the measurements and rivet count may not be a great deal of assistance as the piece appears to be broken and very rusty. It may not be worth trying to clean it, even if Laurent could still find it amongst the large number of small fragments in his possession!! Nevertheless I will ask if he has any time available to have a look.
My question is this. Mike’s diagram shows ‘Item 9’ with a reference to ‘Item 11 Similar’. My assumption is that these two similar items are the shorter and longer stiffeners on the forward bulkhead respectively. Is this correct, or are there similar angled stiffeners to be found elsewhere on the aircraft? The only diagram I have been able to locate is that included in the picture below where the four stiffeners are highlighted.
V1 sites in the Forêt d’Eawy
I have been in touch with Laurent and he agrees with my analysis of the aerial photographs in post #882, namely that the most fruitful areas for locating any remaining fragments are likely to be amongst the undisturbed trees on the lower slopes of the forest along the northern and eastern edges, as has proved to be the case thus far. At present, he is continuing to have difficulty in finding sufficient spare time to concentrate on further searches, but he has not given up!!
I have added another aerial view to the photo-gallery. This attempts to put the Forêt du Croc site in the context of the other V1 sites in the northern part of the Forêt d’Eawy to the south of Dieppe.
The Germans started to build V1 storage sites in 1943. The Allies named them ‘ski-sites’ because of the distinctive shape of the storage buildings. Two such sites constructed in the Forêt d’Eawy were at Les Pet!ts Moraux and Ardouval. They are marked in white on the photograph. Some of the buildings still survive at Les Pet!ts Moraux, including one with false chimneys added in an attempt to disguise it as a farm building. The site at Ardouval is largely preserved with most of its buildings still intact – some showing wartime damage. Neither of these sites became functional following Allied bombing in 1943, and after the site at Ardouval was abandoned, it was decided instead to build smaller sites, hidden in the forest around les Grandes-Ventes.
Typically these smaller sites built in the spring of 1944 (marked in yellow on the picture) comprised:
• the launch ramp (supported on metal struts with concrete bases or sometimes with earth mounds);
• the firing blockhouse (with slit windows for observation and control of the launch);
• an assembly workshop (a rectangular building where the wings were attached to the flying-bomb);
• an amagnetic building (an arched building from the ceiling of which the missile would be suspended to set its compass);
• small water reservoirs (for washing the ramp and fire emergencies); and
• underground shelters (for detonator storage or personnel).
All these features can be found amongst the remains of the site at the Forêt du Croc.
There might also be a reception building for delivery and temporary storage – no longer the easily identifiable ski-shaped buildings with their anti-blast curvature.
The British War Ministry prepared a listing of ‘Constructional Sites’ known as “Noball” targets, showing the geographical co-ordinates and map references of their locations. The reference numbers of the sites are shown on the picture – Les Pet!ts Moraux and Ardouval being amongst the early targets identified. The discovery of the smaller sites, built later, was often helped by reports from the local Resistance. The names on the picture (which are also listed below) show first the nomenclature in the “Noball” list, followed in brackets by the names by which they were known locally. There were three other sites hidden in the forest near les Grandes-Ventes to the south of le Hoquet which seem not to have been identified by the Allies, as they do not appear on the list of targets. These were at le Chemin Coursier, Route de la Loge, and la Route Charlemagne. These are marked on the picture in italics together with another planned site at Muchedent (Pubel) to the west, which did not become functional. To complete the scenario, there was another site further to the south at Maucomble (Carrefour 118), known by the Allies as Forêt de St. Saens, XI/A/238. The identified sites shown in the area pictured were:
La Briqueterie – Forêt des Nappes, XI/A/220: (la Laie Madame);
Ardouval II – Forêt d’Eawy, XI/A/221: (le Châtelet);
Val des Joncs, XI/A/234: (le Fond du Six Frères);
Forêt du Croc, XI/A/235: (Freulleville – le Croc); and
Le Hoquet, XI/A/257: (la Mare du Four).
Ardouval II – Forêt d’Eawy had been the target of a 109 Sqn night-time marking sortie by the Mosquito of Jim Foulsham and John Swarbrick on 27/28 June 1944. This was followed on 9 July by Ben Weightman and his 582 Sqn crew acting as Master Bomber on a daylight sortie to the same site using target indicator flares. The two crews came together for the fateful Oboe-Lancaster leader attack by ED908 (60-Z) on the Forêt du Croc on 20 July.
As can be seen from the numbering, there were over 250 ‘Constructional sites’ identified in northern France and Belgium. When the V-weapon storage dumps are included, there was an astonishing total of approximately 300 potential targets overall. A map displayed at the preserved Ardouval site at Val Ygot shows the locations of a total of 117 V1 sites in the Seine Maritime region alone.
To view in the photo gallery, click the link below. Click on an image to obtain a caption and start a slide-show.
Peter, The lugs aren’t big enough to support anything so I don’t think it’s a bracket, more like some sort of back plate filling a hole in a component…
Hennie, I think you are getting your Peters and Bobs muddled up!!!!
My best guess is along the lines of what you say in your last post. Maybe the real Peter has some more ideas??
Hennie, Yes it would include the fire extinguishers, but the number is not the same in the parts list. However, part numbers do vary as changes are made. I have looked at a couple of pictures of fire extinguishers, but nothing looks the same as your piece. Hence my suggestion that it could be a bracket or perhaps a back-plate of some sort.
No trouble, Peter – our different time zones gave me a head start!.
Hennie, 27N is the code for fire-fighting equipment – having said which I cannot work out what your piece is – maybe a bracket of some sort? Perhaps someone else can add something?
Bulkhead union
Hennie, just to complete the picture a revised diagram of the bulkhead unions is attached. Your part is number 39 on the diagram, and there were two fittings on the bulkhead as shown. The manual says that the cabin was heated by hot air from two radiators mounted on the front spar between the inboard engine nacelles and the fuselage, and connected with the inboard engine cooling systems by flow and return pipes which were lagged with asbestos cord. The parts list indicates that different fittings seem to have been used for the port (LH) and starboard (RH) wings.
Hennie, item 1SS 3523 is a similar union to the oil vent union, but for the cabin heating system, positioned a little below the item in my diagram on the engine bulkhead. I can’t help with the other reference you mentioned.
Oil vent on bulkhead
Thanks, Peter – I hoped you would be able to confirm. The piece in the diagram shows four bolts, so it looks right.
Hennie, can you see a number?