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In early December 2004 it
was found that there was some corrosion in the right hand sliding door as
well as in parts of the airframe around the doorway. Removing the door
for treatment was difficult because corrosion, around the sliding
locking rod at the top of the door (above right), prevented it's
withdrawal. It was eased out with some gentle hammering and application
of rust-removing fluid |
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| Serious work has
started on preparing the cabin interior for cleaning and repainting. As
usual the difficult decision has to be made as to whether the original
paint is to be completely stripped off, in the knowledge that corrosion
can often lurk beneath apparently sound paint. This was well illustrated
on 4th December 2004 when paint on a channel frame below the right side cabin window, which seemed to be in fairly sound condition (above
left), flaked off when disturbed and exposed patches of corrosion (above
right). It appeared that the original primer had not adhered to the
bare metal in that area. |
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| In early January
2005, while removing heavy corrosion from the cabin roof, it was
realised that one of the metal deck panels, below and slightly to the rear of the
gearbox, was perforated in several places (above). To allow
replacement, or even patching, of the panel it was decided that the main
rotor head and gearbox would have to be lifted from the deck. |
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| Throughout
much of January 2005 work continued to disconnect the maze of control
rods, oil pipes and hydraulic lines (above left) which surround
the transmission and main rotor head. The drive shaft from the engine and the
drive shaft to the tail rotor were disconnected. On 12th February
2005 the securing bolts were removed one by one and the entire assembly
was lifted from the deck (above right) and lowered slowly onto a
waiting trolley. |
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