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Page Title: CARTRIDGES AND CARTRIDGE- ACTUATED DEVICES (CAD)
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SMDC ONE-WAY TRANSFER
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Aviation Structural Mechanic E2 - How airplanes are built and how to maintain them
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EXPIRATION  DATES

The  pilot’s  and  copilot’s  internal  initiator handles transfer a detonation wave signal to the connecting  SMDC  assemblies,  which  are  routed throughout the cockpit area. In turn, the SMDC assemblies   initiate   four   detonating   cord assemblies,  which  are  mounted  on  the  periphery of  the  two  canopies  and  the  two  hatches.  The detonating cord assemblies sever or fracture the stretched  acrylic  canopies  and  hatches.  FLSC assemblies, which are simultaneously initiated, sever the two wing fillet supports and the two upper  wing-to-fuselage  fillets,  which  extend  into the TACCO and SENSO hatch area. Actuation  of  the  TACCO  or  SENSO  internal SMDC  initiator  will  sever  only  the  hatch,  the upper wing-to-fuselage -fillet, and the wing fillet support  at  the  crew  station  in  which  the  initiator was activated. Explosive one-way transfers located forward of the TACCO and SENSO crew stations prevent the detonation wave from severing the pilot and copilot canopies. It is virtually impossible to initiate the system at any point other than an initiator handle. As compared  to  hot-gas  systems,  this  system  maybe considered  immune  to  ordinary  shop  hazards.  The system   is   self-sufficient   and   independent.   It depends   upon   no   other   system   for   aid   or assistance,   and   it   does   not   contribute   aid, assistance,  or  sequence  to  any  other  aircraft system. The S-3A system is much less susceptible to inadvertent actuation than hot-gas systems, and hence more convenient and safe for maintenance personnel. CARTRIDGES AND CARTRIDGE- ACTUATED  DEVICES  (CAD) Learning Objective: Recognize the service life and expiration dates of cartridges and cartridge-activated  devices. The types of explosive devices incorporated in egress systems are varied. The AME working with these devices must know how they function, their characteristics, how to identify them, their service-life  limitations,  and  all  safety  precautions. The AME who understands the importance of all of these factors and who correctly uses the maintenance manuals is better equipped to super- vise  and  train  others.  The  following  manuals  are required   for   the   AME   to   meet   the   above requirements: 1. 2. 3. 4. 5. Description,   Preparation   for   Use,   and Handling   Instructions,   Aircrew   Escape Propulsion System (AEPS) Devices, NAV- AIR   11-85-1 General  Use  Cartridges  and  Cartridge Actuated   Devices   for   Aircraft   and Associated   Equipment   (CADS),   NAV- AIR  11-100-1.1,  NAVAIR  11-100-1.2,  and NAVAIR  11-100-1.3 Specific aircraft MIMs OP 4,  Ammunition  Afloat OP 5, Ammunition  and  Explosives  Ashore SERVICE  LIFE The service life of a CAD is the specific period of time that it is allowed to be used. These periods of  time  are  affected  by  various  environmental conditions, which have resulted in the assignment of  time  limits  or  overage  requirements.  These limits are shelf life and installed life. The establishment of service-life limits is based upon  design  verification  tests,  qualification  tests, and  surveillance  evaluations.  The  established limits  are  approved  by  the  Naval  Air  Systems Command.   Therefore,   the   establishment   of service-life time limits is not arbitrary and must be adhered to as specified. Prior  to  deployment  to  areas  that  do  not permit ready supply and servicing of cartridges or  cartridge-actuated  devices,  an  inspection  must be made of all CAD’s service-life expiration dates. If, during this inspection, it is determined that a CAD will become overage during the period of the deployment, the CAD must be replaced prior to  the  deployment.  Before  installation  of  any CAD, the service-life expiration date of the unit must be checked to ensure that the unit is not overage and will not become overage prior to the next periodic maintenance cycle of the aircraft. During  standard  depot  level  maintenance (SDLM),  the  expiration  dates  of  all  installed CADs must be checked. Those CADs assigned to organizational level for maintenance and that have expiration  dates  prior  to  the  next  scheduled inspection  after  the  aircraft  is  returned  to  its custodian must be replaced. CADs assigned to depot  level  for  maintenance  that  have  expiration dates falling prior to the next scheduled SDLM should also be replaced. The exception is systems replaced exclusively through the use of a field modification  team.  Adherence  to  these  procedures 2-23

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