Current "installation kit" contents
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Comments
May 18, 2019 Revision A.1  Original 
Release
July 4, 2019 Revision A.2   
Clarified language on bleed air mixing system
 
 
May 18, 2019 Revision A.1
An "Installation Kit" contains
  - Inlet from L39 "Y" duct to 731-3 fan inlet casing
 
  - Inlet guide ring or "velocity stack" to guide and align the inlet to the 
  front of the motor
 
  - Stainless front motor mounts with rollers (customer procures installation 
  bolts part number ?????)
 
  - Oil pressure adapter and 0-5V oil pressure sender compatible with current 
  experimental avionics packages (Skyview, G3X)
 
  - Bespoke Rf  fuel flow pickup which replaces the stock fuel flow 
  turbine wheel sensor on Hawker/WestWind style fuel flow sensors (part number 
  ??????)
 
  - Composite fan bypass exit duct with integral jet core hanger.
 
  - Jet core hanger bracket
 
  - Throttle bell crank
 
  - Throttle bell crank to fuel control FCU actuation rod
 
  - Bespoke FCU actuation arm
 
  - Exhaust exit tube
 
  - Exhaust exit tail cone
 
  - Tail cone hanger brackets (exhaust tube side for use with repositioned 
  stock L39 hanger brackets mounted in the tail)
 
  - N1/N2 signal conditioning box for compatibility with modern experimental 
  avionics
 
  - ACM bleed air control valve mounting adapter to attach the stock AI-25 
  bleed air shut off valve to the stock L39 air cleaner
 
  - Stamped Engineering report for the specific L39 serial number being 
  modified to aid in Airworthiness application
 
  - Electronic copy of our current inspection program (has been approved or 
  multiple airframes to date)
 
Under development at this time but NOT currently included in the kit is an 
engine mounted High Pressure - Low Pressure bleed air mixing system.  This 
will be made available when testing is complete.
 
July 4, 2019 Revision A.2
An "Installation Kit" contains
  - Inlet from L39 "Y" duct to 731-3 fan inlet casing
 
  - Inlet guide ring or "velocity stack" to guide and align the inlet to the 
  front of the motor
 
  - Stainless front motor mounts with rollers (customer procures installation 
  bolts part number ?????)
 
  - Oil pressure adapter and 0-5V oil pressure sender compatible with current 
  experimental avionics packages (Skyview, G3X)
 
  - Bespoke Rf  fuel flow pickup which replaces the stock fuel flow 
  turbine wheel sensor on Hawker/WestWind style fuel flow sensors (part number 
  ??????)
 
  - Composite fan bypass exit duct with integral jet core hanger.
 
  - Jet core hanger bracket
 
  - Throttle bell crank
 
  - Throttle bell crank to fuel control FCU actuation rod
 
  - Bespoke FCU actuation arm
 
  - Exhaust exit tube
 
  - Exhaust exit tail cone
 
  - Tail cone hanger brackets (exhaust tube side for use with repositioned 
  stock L39 hanger brackets mounted in the tail)
 
  - N1/N2 signal conditioning box for compatibility with modern experimental 
  avionics
 
  - ACM bleed air control valve mounting adapter to attach the stock AI-25 
  bleed air shut off valve to the stock L39 air cleaner
 
  - Stamped Engineering report for the specific L39 serial number being 
  modified to aid in Airworthiness application
 
  - Electronic copy of our current inspection program (has been approved or 
  multiple airframes to date)
 
Under development at this time but NOT currently included in the kit is an 
engine mounted High Pressure - Low Pressure bleed air mixing system.  This 
will be included in future kits but only after testing is complete. Kits ordered 
prior to this point will not be retrofitted with the bleed air mixing system.