Question 8

Refer to: Aviation Maintenance Management, Appendix A, Systems Engineering, pg. 247-254

During the aircraft design phase, a high pressure hydraulic line was properly clamped to the engine and engine nacelle and routed next to the engine and up into the wing. It was determined that the hydraulic line used did not have sufficient heat and abrasion resistance due to high heat and vibration in the area it was routed within the engine area. Which Systems Engineering process term below is best associated with the example provided that would best address this issue before the aircraft is type certificated?

Group of answer choices

System Boundary Control

System Interface Control

System Performance

System Optimization

________________________________________________________

Question 9

Logistics Engineering and Management, 1.7.6 Reliability (R), pgs 33-34

Resilience is an inherent characteristic of design. As such, it is essential that resilience be adequately considered at program inception and that reliability be addressed throughout the system life cycle. This statement is:

Group of answer choices

True

False