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Page Title: EJECTION SEAT CARTRIDGES AND CARTRIDGE-ACTUATED DEVICES (CAD)
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SAFETY  PRECAUTIONS  FOR EJECTION  SEATS  AND  EXPLOSIVE DEVICES
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Aviation Structural Mechanic E1&C - How airplanes are built and how to maintain them
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Derivation of Lot Number

result in severe injury or death to personnel and damage  to  or  destruction  of  aircraft.  Therefore, due   to   the   inherent   dangers   associated   with ejection seats and canopy systems, a seat/canopy check-out   procedure   is   required.   The   Egress/ Environmental  Work  Center  (AME  shop)  is  re- sponsible for indoctrinating all personnel in the hazards  and  safety  precautions  associated  with these systems. A thorough seat check-out will be given,  by  a  qualified  Aviation  Structural  Mechanic (Safety  Equipmentman)  (AME),  to  all  newly assigned  maintenance  personnel  prior  to  their performing any aircraft maintenance work on the aircraft,  and  every  6  months  thereafter.  In addition,  any  personnel  removed  from  aircraft maintenance responsibilities for over 90 days must receive  a  seat  check-out  before  performing  any aircraft maintenance. The AME work center and the  other  maintenance  work  centers  will  maintain records of seat check-outs, including date given, date   due,   and   the   signature   of   the   AME performing  the  check-out. The seat check-out program will be established by a squadron MI. All personnel due seat check- out requalification will be listed in the monthly maintenance plan. EJECTION  SEAT  CARTRIDGES AND    CARTRIDGE-ACTUATED DEVICES  (CAD) 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   these   factors   and   who   correctly   uses   the maintenance  manuals  is  better  equipped  to supervise  and  train  others.  The  following  manuals are  required  for  the  AME  to  meet  the  above requirements: 1. Description, Preparation   for   use,   and Handling   Instructions,   Aircrew   Escape Propulsion   System   (AEPS)   Devices,   NAVAIR 11-85-1 2.  General   Use   Cartridges   and   Cartridge Actuated  Devices  for  Aircraft  and  Associated Equipment  (CADS),   NAVAIR    11-100-1.1, NAVAIR   11-100-1.2,   NAVAIR   11-100-1.3 3.  Specific  aircraft  MIMs 4.  OP  4,  Ammunition   Afloat 5.  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. Before  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 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  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 will  prevent  loss  of  aircraft  mission  capability  due to  CAD  service-life  expiration. Expiration Dates To  determine  service-life  expiration  dates, both  the  shelf  life  and  installed  life  must  be computed.  First,  compute  the  shelf  life  of  the CAD  by  using  its  lot  number  to  determine  the month  and  year  of  manufacture.  Refer  to  table 1-1  to  ensure  correct  interpretation  of  the  lot number  since  there  are  currently  two  methods used to derive lot numbers. Obtain the established shelf  life  (number  of  months  and  years)  for  the individual  CAD  from  the  NAVAIR  11-100-1 series manual. Add this figure (shelf life) to the 1-8

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