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all-chap-4-WEB
95 pages
Published by
Antoine Daoust
FUSELAGE STRUCTURE
radio frequency signals thereby protecting the crew from radiation.
The radome is hinged at the top to
perr.
liteasy access to the antenna
area.
In the open position, the radome is supported by two jury struts,
which...
[More]
FUSELAGE STRUCTURE
radio frequency signals thereby protecting the crew from radiation.
The radome is hinged at the top to
perr.
liteasy access to the antenna
area.
In the open position, the radome is supported by two jury struts,
which are attached to the bulkhead
at Station 24.
In the closed position, the radome is secured by four
flush fitting toggle fasteners.
The exterior surface of the radome
is painted to match the exterior
a.
ir-cr-af tfinish.
3.
The cockpit hood assembly consists of an internally braced dome
attacr.
ed to the hood ring, which
extends around the aperture in the
fuselage.
The dome is covered by
an u~pressurized fairing, thus obtaining a smooth junction at the
upper fuselage.
Five window frames
are fitted into the frames between.
the fuselage hood ring and cockpit
dcme , These five window frarnes are
fitted trith three f orwar-d facing
windshields.
The two frames, one
on each side of the cockpit, are
each fit.
t.
edwith a fixed window and
a sliding wind
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Tags
bulkhead,
canada,
chapter,
date,
floor,
frame,
fuselage,
located,
maintenance,
manual,
nose,
position,
pressure,
section,
side,
viscount,
window
