Couldn’t find any connection to RAF (ETZ, DUW)
http://www.users.waitrose.com/~mbcass/names.htm
but
G-AETY was AX659
http://www.ww2aircraft.net/forum/album/showphoto.php?photo=6857&cat=all&size=big
G-AEUD was AX660
(found no pic)
http://www.imperial-airways.com/Ia_and_the_raf_page.html
The Grace Firefly would probably be WD833? If so, it was being restored to airworthy condition with Amjet at Blaine, but they are now extinct. Nick Grace also seemed to be involved with Fireflies WD899 and VT409.
http://www.warbirdregistry.org/fireflyregistry/firefly-wd833.html
Their last entry is 2002.
Here it’s 2006
http://www.cnapg.org/vw1135.htm#Vintage and Warbird Aircraft.
Fantastic news.. another classic jet back where she belongs. Incidentally are the CAC Sabres Avon powered or US engined.?:cool:
Guess it’s Avon
http://www.aircraftresourcecenter.com/AWA1/401-500/walk483_RAAF-Sabre_Williamson/walk483.htm
Guess you know this pic already …. and maybe this book is helpful:
‘Echoes of war – The story of H2S radar’ by Sir Bernard Lovell
http://www.429sqn.ca/bch2s01.jpg
http://www.429sqn.ca/bch2s.htm
‘The fuel cells and engine oil cells were rubberized fabric self-sealing tanks.
The Mains and Oil tanks were not collapsing.
There were the six main fuel cells….
no 1 and 4 were a single cell…. cap 425 US Gals
The two inbd fuel cells were split to accomadate the landing gear…the inbd tanks were 212 gals and 213 gals..total 425 US Gals.
Tokyo tanks were composed of a set of 5 for the 1 and 4 engines
(again. flexible collapsing rubberized fabric)
and and a set of 4 larger cells for the inbd tanks as the wing was thicker for the inbd….
The set of 5 for the outbd engines capacity was 270 gals
The set of 4 for the inbd engines capacity was 270 gals
Total capacity was 1080
Total fuel capacity with Tokyo tanks was 2780
1700 mains (425 x 4)
Tokyo capacity 1080 1700 + 1080 = 2780
I count a total of 24 tanks…6 mains, 18 tokyo (9 each wing) = 24 tanks
The fuel transfer system was much simplifed…there were two selector valves with 4 positions each …one for left wing, one for right wing…one transfer pump located in bomb bay. A three postion switch controlled the transfer pump..(on off on)….installed so that if the fuel flow was FROM the left wing….the switch was moved in the direction the fuel was to transfer…I.E. toward the Right wing. Transfer rate was 15 gals/minute…to transfer 90 gals.( 90 divided by 15 = 6 minutes).
To transfer from No 1 to No 2, fuel HAD to be transferred first to opposite wing tank, the Selector valves repositioned and then back to No 2.
The Tokyo tanks had a hydraulic valve (normally closed) but when the lever was actuated, the valve was positioned OPEN, and the fuel then was gravity fed into the respective tanks…the tokyo tank for the inbd tanks..sometimes marked AUX fed first into the inbd aux and had a 1″ line coupling it to the inbd main…this required when refueling, to move from the main to the aux and then back to the main as the 1″ line was also feeding fuel to the inbd tank. This process was continued until both tanks (Inbd) were filled.
In ascertaining the partially empty inbd tankage, an average had to be computed due to the arrangement of the tanks…IE 2 Aux dipped level, 130 gals…no 2 main 140 gals…average 135.
The B-17 had as an indicating system, a Liquidometer, which was composed of float and xmttr similar to auto indicating systems…the positions were 1 Main,
2 Aux,2 Main, 3 Aux,3 Main and 4 Main….there was no indication for the tokyo tanks…A note of caution, was that the Mains had to be below 150 before xfrring from the tokyos (to prevent over filling the mains.
The Bomb Bay tank capacity was 410 gals US. (each)
I hope this answers your questions ….’
http://forum.armyairforces.com/tm.aspx?m=79692&high=Tokyo+Tanks
Apparently, the other replica (using some original parts) is to found at Kosice Airport, Slovakia
They mention only an Avia BH-11 :confused:
http://airmuseum.aspdotnet.sk/exponaty_e.html
kev35, do you know this already?
http://upload.wikimedia.org/wikipedia/commons/6/6d/Burtonwood-1945.jpg
Martin
‘Between April 11th and September 30th 1933, the Great Western Railway provided the air service from Plymouth’s Roborough Airport.’
http://www.plymouthdata.info/Air%20Services-GWR.htm
‘Commercial aviation arrived in April 1933 with the opening of an experimental air service between
Cardiff, Haldon (for Torbay) and Plymouth initiated by the Great Western Railway Company. The
service, flown with Westland Wessex aircraft (including G-AAGW) provided by Imperial Airways, was
opened to the public on April 12 and later extended to Birmingham. Although the service only operated
for a single summer season, it served to encourage other operators to use the aerodrome.’
http://www.devonstrut.co.uk/pages/newarticles/NL0506.pdf
‘On 12 April 1933 the GWR Air Service started a twice daily (weekday) service between Cardiff and Plymouth via Haldon. They chartered a Westland Wessex G-AAGW from Imperial Airways, painted cream and brown.’
http://www.exetermemories.co.uk/em/airport.php
http://aviationancestry.com/Aircraft/Westland/Westland-Wessex-1933-1.html
… do you mean this?
‘The trailing edge of each of the main undercarriage trousers can be turned to provide airbraking surface.’
http://www.flightglobal.com/pdfarchive/view/1938/1938%20-%202518.html
edit: guess you meant G-AFEG, De Bruyne-Maas Ladybird, DB3 M1
Martin, PM?
Albert
PM – Private messages, look on top of Forum site
Albert, please look for PM.
Martin
‘Scottish Aviation “Twin Pioneer” (XM-285) Photo taken at Upavon Wiltshire in June 1962.’
http://i17.ebayimg.com/08/i/001/42/b1/a8f3_1.JPG
Martin