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When looking at the reconstruction imagery below,
remember that there is heat, fire, submersion, impact and recovery damage.
However some indicators are unique - such as the heat discolouration of
metal. The obvious conclusion is that an accelerator (such as High Pressure
Oxygen Flows) must have been latterly involved. |
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The
MD-11 now flies in Swiss Colours |
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View
to the ceiling in front of cockpit door,
from the forward galley.
Note the
heat and fire
penetration of the air ducts in
the upper right
hand corner.
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View
towards the cockpit door and galley ceiling.
note the wire bundle at the right
and soot in the
ceiling.
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View into the cabin ceiling from the forward
galley, facing to the right rear
side. note the
soot at the air ducts.
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View through the cockpit door
into the scattered cockpit of
HB-IWF. In the foreground:
the
remains of the RH observer
seat.
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Samples
showing the heat discolouration of metal
as a function of
heat and by time of exposure to fire
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IFEN wiring by Hollingsead International in
an SR 111 sister-ship |
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IFEN wiring by Hollingsead International.
view into
the front ceiling
facing towards the cockpit
bulkhead. Note the (green) track
for the forward
right entry door.
Note further the bend-radius
of the
IFEN
wiring (colored) with the OEM wiring turning
90 degree into the PVC tubes and
further into the
cockpit.
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Hollingsead International IFEN
installation behind
the cabin ceiling in the first class
compartment.
note the bend-radius and wire-routing across metal
edges and the tension on the wires
at the lower
right hand corner connector
box.
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Left
hand outside view of the reconstructed
cockpit of HB-IWF
(at the CFB Shearwater hangar)
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The cockpit overhead panel of HB-IWF.
Note the
heat and soot
penetration.
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The
right hand (F/O's side) circuit breaker panel.
Note the heat discolouration of the
metal.
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Arcing can generate heat in
excess of several
thousand degrees Celsius
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HB-IWF in the old
Swissair
colour scheme.
The VAUD
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