Paragraph #
MIL-HDBK-516C Criteria Applicability Details
4.0 SYSTEMS ENGINEERING
4.1 Design Criteria
4.1.1 All
4.1.2 All
4.3 Materials Selection
4.3.1 All
4.4
4.4.1 All N/A
4.4.2 All N/A
4.5 Operator's and maintenance manuals/technical orders
4.5.1 All
4.5.2 All
Platform
Applicability
Aircraft
Connection
Verify that the design criteria, including requirements and
ground rules, adequately address airworthiness and safety
for mission usage, full permissible flight envelope, duty
cycle, interfaces, induced and natural environment,
inspection capability, and maintenance philosophy.
Power
Data
Mounted
None
Verify that airworthiness and safety design criteria are
adequately addressed at component, subsystem and
system levels, including interfaces, latencies, software and
information assurance.
Power
Data
For Army and Navy air systems, verify that the material
selection process uses validated and consistent material
properties data, including design mechanical and physical
properties such as material defects, and corrosion and
environmental protection requirements (see also Section
19, Materials; Section 5, Structures; and Section 7,
Propulsion; Section 8, Air Vehicle Subsystems of this
document).
Power
Data
Mounted
None
Verify that key product characteristics (including critical
characteristics) have been identified.
Verify that all critical process capabilities exist to meet key
product characteristic requirements (including critical
characteristics).
Verify that processes are in place to identify and document
normal and emergency procedures, limitations, restrictions,
warnings, cautions and notes.
Power
Data
None
Verify that processes are in place to identify and document
the technical data, and that the technical data are
consistent with the defined functional and product baseline.
Power
Data
Mounted
None
