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Page Title: THERMAL RADIATION PROTECTION UTILITY SYSTEMS
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Aviation Structural Mechanic E2 - How airplanes are built and how to maintain them
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THERMAL RADIATION PROTECTION  UTILITY  SYSTEMS-Cont.

plug is called a safety plug. The relief valve relieves the excess pressure in the container instead of completely emptying the container. Some larger aircraft use more than one fire extinguishing  agent  container  to  direct  the  agent to several points within an area. With cockpit switches set at various positions, the agent can be released through specific discharge outlets; and if the fire persists, the switch positions can be changed to release agent from a second container to different discharge outlets within the same area. The fire extinguishing system of the P-3 air- craft is an example of this type of system. The containers   used   in   the   P-3   system   are   also equipped  with  two-valve  (bonnet)  assemblies  for discharging  the  container;  however,  only  one assembly is fired at any one time to discharge the container.  This  dual  arrangement  provides  a secondary means of discharging a cylinder in the event a cartridge fails for any reason to fire and discharge the container. MAINTENANCE Maintenance  of  the  CF3Br  fire  extinguishing system at the organizational level of maintenance consists  of  replacement  of  faulty  components and  discharged  or  below  pressure  containers, maintenance  of  associated  plumbing,  and  per- forming operational checks. Containers   should   be   replaced   when   the pressure   falls   below   that   indicated   on   the container  or  in  the  applicable  MIM.  Each container   has   a   pressure   indicating   gage. Suspected leakage in system plumbing requires disconnection  of  the  container(s)  and  pressure leakage  testing  of  all  lines  by  using  nitrogen pressure  and  a  leakage  tester.  The  leakage  tester measures pressure drop over a specified period of time, as outlined in the MIM. The  operational  checkout  of  the  fire  ex- tinguishing   system,   primarily   a   checkout   of electrical  circuitry  such  as  wiring  continuity checks,  proper  switch  operation,  etc.,  is  per- formed by personnel of the AE rating. THERMAL RADIATION PROTECTION  UTILITY  SYSTEMS Learning  Objective:  Recognize  the  purpose of the thermal radiation protection system. Naval   aircraft   used   for   special   weapons delivery have means of protecting the pilot and crew members from the effects of heat and light that  such  weapons  emit.  Several  of  the  Navy attack   aircraft   are   equipped   with   a   thermal radiation protection system and flak protection curtains. The A-6, for example, can be equipped with radiation   enclosures   for   the   windshield   and canopy.  These  enclosures  shield  off  the  see- through  portions  of  the  cockpit,  which  gives  the flight crew protection from the extreme heat and light created by a special weapons delivery. The  radiation  shields  consist  of  fixed  and sliding fiber glass panels mounted on each side of the canopy. The sliding panels are equipped with rollers and suspended on a system of tracks between  the  fixed  side  panels  and  the  canopy center overhead spline structure. The   sliding   panels   for   each   side   of   the canopy move independently of each other and are  manually  positioned  by  the  pilot  or  bombar- dier/navigator. The shield is closed by pulling the forward sliding panel towards the canopy forward arch. The forward panel is equipped with a lip, which engages on the lip of the aft sliding panel, drawing it forward at the same time. The  sliding  panels  will  automatically  lock  in one of three positions; open, closed, or half open, as desired. A latch handle on each forward sliding panel  releases  the  detent  pins,  unlocking  the panels. If the panels are closed and ejection becomes necessary,  it  may  be  initiated  through  the  closed shields. The windshield curtain is a fiber glass cloth assembly with an aluminized coating. It is fastened between the instrument panel glare shield and the windshield bow structure to close off the entire windshield  area.  Springs  pull  the  windshield curtain down flat on the glare shield for stowage when the curtain is unzipped. Flak curtains, similar to the canopy curtain, are  mounted  beside  the  pilot  and  bombardier/ navigator  foot  area,  cockpit  side  area,  and  along the lower portion of the canopy. They provide a limited measure of protection from flak and small arms fire when making low-level attacks on enemy positions. The canopy-mounted curtain is a sandwich- type  pad  constructed  on  vinyl-coated  glass  cloth with a nylon center. The cockpit area side panels are basically of the same construction with the outboard vinyl coating deleted. The foot guard panel is constructed of a metal plate with a nylon curtain riveted to the outboard side. Installation 1-34

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