Transcription of F-15 AIRFRAME MOUNTED
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F-15 AIRFRAME MOUNTED
F-15 AIRFRAME MOUNTED ACCESSORY DRIVE SYSTEM I moved back into the Journal Building in early 1970 and joined the F-15 Project, whichwas just setting up manpower requirements. At this time, Tom Williams was the ProgramManager and Pete Engel was the Senor Project Engineer. Wade Brock, John Irwin and I came onas Project Engineers. The system consisted of a Jet Fuel Starter (Model JFS190-1), a Left HandAirframe MOUNTED Accessory Drive (LH AMAD), a Central Gear Box (CGB), a Right HandAirframe MOUNTED Accessory Drive (RH AMAD), and two Power Takeoff Shafts (PTO). Because it was a very large system, the work load was assigned as follows: Wade wasresponsible for the JFS, John was responsible for the three gear boxes, and I was responsible forPTO shafts and all reports and data.
A conceptual mockup of the system is presented in Figure 2 and Figure 3 Figure 2 Figure3 The boiler plate accessory drive gearbox, which is the heart of this system, is presented in
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