Submitted by admin on Fri, 03/23/2018 - 15:51

The FAA Compliance:

  • Created to meet FAA Guidance Letter dated Sept 18, 2002 Systems.
  • Provides the crew a means of removing power (115 VAC) from all PAX Cabin Systems.
  • Provides maintenance with the ability to Test power removal functions.
  • Creates “auto-shed” capability where none exist. (A320 family)
     
EPS front
EPS back

System Features:

  • Removes all power (at source) from all “Cabin Systems” by a single switch operation.
    (Ref.: FAA Guidance Letter Dated Sept 18, 2002).
  • Provides load-shedding function when not available from existing aircraft electrical system (ex. A320 & CRJ).
  • Provides power down function upon cabin decompression when not available from existing installed system’s installation (IFE, LAPTOP power etc.).
  • Latched and guarded “Master Reset Switch” only accessible to maintenance personnel.
  • Allows for individual system’s power down for maintenance purposes.
  • Used to create and control an “Independent Cabin System’s Power Bus” when not available from existing aircraft electrical system (ex. A320 & CRJ).

Technical Information:

  • P/N: FC-0901-001/002/003/004/005/006/007
  • Dimensions: 3” H, 8.1” W, 4” D
  • Weight: 1.8 lb
  • Power Requirements: 28VDC, 12W

Documentation:

ESP