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Page Title: CHAPTER 5 NAVY AIRCREW COMMON EJECTION SEAT (NACES)
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Forward ejection seat

CHAPTER 5 NAVY AIRCREW COMMON EJECTION SEAT (NACES) Chapter Objective:  Upon completion of this chapter, you will have a working knowledge  of  the  Navy  Aircrew  Common  Ejection  Seat  (NACES),  including functional   description,   physical   description,   component   identification,   and maintenance   concepts. The incorporation of the Navy Aircrew Com- mon Ejection Seat (NACES) in Navy aircraft re- presents a significant improvement in ejection-seat design that takes advantage of the latest escape system technology. The NACES system gives the aircrew  improved  chances  for  escape  in  all  ejection situations, reduced potential for injury, extended preventive maintenance intervals, and a significant reduction  in  life-cycle  costs.  This  Martin-Baker ejection seat will be fitted to the new Grumman F-14D  Tomcat,  the   McDonnel   Douglas/British Aerospace T-45A Goshawk two-seat trainer, and the  McDonnel  Douglas  F/A-18C  and  D  aircraft. The  purpose  of  the  common  ejection  seat  is to  ease  the  logistics  and  maintenance  problems  on the  Navy’s  inventory  of  aircraft.  The  new  seat  will increase  the  standardization  and  reliability  of aircraft  emergency  escape  and  aircrew  and  ground crew   training.   The   electronically   controlled NACES represents the state-of-the-art in escape system  technology,  and  it  has  been  selected  as  the future  standard  of  the  U.S.  Navy.  The  NACES series was engineered from the outset for future growth  potential.  The  ejection  seat  is  designed  for simple reprogramming or modification to ensure that  it  maintains  current  technology. As a senior AME, you already have the prere- quisite knowledge and experience to understand ejection   seat   theory.   New   ideas   have   been incorporated  into  the  NACES.  Now  all  that  is required  is  your  willingness  to  learn  these  new ideas  so  that  NACES  characteristics  become  as familiar as previous Martin-Baker ejection seats. SYSTEM  DESCRIPTION  AND COMPONENTS Learning  Objective:  Recognize  the  func- tional and physical description of the NA- CES and the components within the system. The   NACES   system   uses   a   flexible configuration to meet the exact requirements of the  crew  station  designer.  Although  this  is  a common ejection seat, the designator number for the  seat  versus  aircraft  types  are  different,  as shown  below. SEAT TYPE    AIRCRAFT-LOCATION 1. SJU-17(V)1/A F/A-18C, F/A-18D, rear cockpit 2.  SJU-17(V)2/A  F/A-18D,  front  cockpit 3.  SJU-17(V)3/A  F-14D,  rear  cockpit 4.  SJU-17(V)4/A  F-14D,  front  cockpit 5.  SJU-17(V)5/A  T-45,  rear  cockpit 6.  SJU-17(V)6/A  T-45,  front  cockpit Although the physical description may differ between  the  seats  used  in  the  F-14D  as  compared to  the  F/A-18  and  T-45  (fig.  5-1),  the  functions of all the seats are the same. In this chapter we will  use  the  F/A-18  ejection  seat  to  discuss  system description,  operation,  function,  and  component identification. FUNCTIONAL  DESCRIPTION WARNING The  emergency  escape  system  incorporates several explosive cartridges and rockets containing  propellant  charges.  Inadvertent firing of any of these may result in serious or fatal injury to personnel on, or in the vicinity of, the aircraft. 5-1

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