A productive day then… Sorry I couldn’t get up there! Busy dismantling Jet Provosts, but by the looks of things, your Tempest is in better condition……..
Bill Gunston’s Classic Aircraft ‘Fighters’. It was on my Grandma’s bookshelf and was compulsive reading EVERY sunday… It now graces my sheves….
That DC8 is the only thing which has flown over my house in years that I hadn’t been able to positively identify! THANKS!!!!
Hello,
From the MoD I see that the UK forces are to get the A330.
Should we not worry a little ?
Folowing the Nimrod with all its costly changes and problems.
We now are about to take on the A330.
One of which in service in Civil colours has been tragically lost and cause(s) for the loss is/are as yet still unproven.
Again it seems that the Duty of care to our troops and other servicemen is to be put on the back burner.
Alex
Can you name a large aircraft type which has never had a hull loss of any type? (Except A380 – its brand new..)
Any OTU scheme – preferably like the AR213 Hawarden scheme with the slightly mental stripes on the nose….
HP Jetstream 200 G-BBYM at Newcastle Aviation Academy
(Not public, but preserved nonetheless…..)
Shorts 330 G-OGIL at NEAM, Sunderland
On SAR, we once scrambled a heli to find an aircrew wrist-watch beacon which had been set off. The Aircrew chap was quite upset to find a Sea King following him down the M1……
Agreed, Mr. Boyle.
I have spent 4 weeks dismantling a Jetstream 200, and the last year trying to re-build the thing! And thats a tiny airliner. At some point, a certain 737 is going to be replaced, and although I would like to preserve it, there is no economical way to take it apart and transpoirt it. For that particular one, it will be, at best, a cockpit section or forward fuselage.
Airliners are not designed to be taken apart easily……….
Prototype UO-1 (or Piper Aztec for the US Navy) is alive and well at Newcastle Aviation Academy as N73LW.. (alongside first service delivery JP T3 XM355)
The plane could have a structural defect, that could have happened years and years ago, constantly weakening througth flight cycles. When the storm placed an increase in the amount of stress acting upon the fuselarge, it could have ruptured causing the decompression. Something similar happened in Japan Air 123 and that China Airways 747 that broke up suddenly en route from Taipai to HK
refer to page 2 of this thread, post no. 53. Airbus statement: 2500 cycles, 4 years old.
Condolences.
September 1979 Reno Air race final lap……. flown by Steve Hinton
try here.. http://forum.keypublishing.co.uk/showthread.php?t=73217
The same photo is in the original ‘Aces & Wingmen’ captioned as being YF-L of the 358th Fighter Sqn (355th FG), crashed at Manston on 3rd Jan 1945. However 44-14564 was bellied in by Capt. Grant A Seeley near Steeple Modern on that date. According to the database on Littlefriends site it was coded YF-E but what can be seen of the letter doesn’t look like an ‘F’.
The officer is identified as Lt Col Moody of the 355th, which would make more sense for him to have been photographed close to their base rather than Manston.
It looks feasible that this side of the aircraft is coded L * YF. The lower portion of the Y is between the pilot’s knees, next to his hand….. His body would mask the top of the Y perfectly.
given that a similar scene unfolded a few years ago and culminated in the loss of a Valetta and the destruction of the Canberra nose glazing, I would normally vote for razor wire too. HOWEVER, the main thing which stops people volunteering is that fact that at most museums, NEAM included, you have to pay. I know the yearly outgoings in membership is very little, but imagine how you would feel when told this:
We want you to set aside as much time as you can spare to help us, oh and by the way, you owe us £15 for the privilege….., oh and you’re not going to be working on planes – would you mind cutting the grass, picking litter and do a bit of painting…
The best solution all round is a bigger fence and a thick hedge…… and a doberman….
The recommendation has always been that it should be stop drilled. If you were to move the aircraft (as we were looking to do), then that drag brace should be replaced. There is significant internal corrosion, but the crack did not elongate over the last 2 years in the severe wind conditions (I thought the whole thing was going to flip over at one point), and shouldn’t pose a serious risk to H+S in the immediate future. I would suggest a 3mm stop drill at either end will suffice until a collar can be fitted which should be firmly rivetted to the brace.
A serious case of Deja Vous….