Section 7.5.0. Structural Hardware Tests
The structural hardware tests have two functions: to support
the verification of the complete structural design, and to define those areas
of the structure that need additional attention. These tests are scheduled so
that there is sufficient time to incorporate structural changes into production
aircraft. In fact, production go-ahead
is predicated on completing at least one design lifetime of flight-by-flight
loading in the full-scale durability test (see JSSG-2006 paragraph A.4.11.1.2.2.b). Structural hardware tests include joint
tests, component tests, assembly tests, as well as full-scale structural tests.
Examples of variables that may be considered for the study of
different design concepts, design details and structural materials are:
·
fastener systems
·
type of joints and joint detail
·
forged versus machined or built-up structure
·
production method
·
reinforcement or tear strap shape, size, and spacing
·
multiple or single load path
·
materials or combination of materials
·
effect of design stress level
The testing of one or more of these variables will not be
specifically addressed. Rather, a
discussion of the essential conditions for design development testing for
damage tolerance is presented in general.