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
Manufacturing and quality
4.4.1
All N/A
4.4.2
All N/A
4.5
Operator's and manintenance manual/technical orders
4.5.1
All
4.5.2
All
4.5.3
All
5.0
STRUCTURES
5.1
Loads
Criteria
#
Platform
Applicability
Aircraft
Connection
Highest Risk
Severity
Verify design criteria, including requirements and rules,
adequately address safety for mission usage, full
permissible flight envelope, duty cycle, interfaces, induced
and natural environment, inspection capability, and
maintenance philosopy.
Power
Data
Mounted
None
Verify design criteria address all components, system and
subsystem interfaces and software.
Power
Data
Verify that the material selection process uses validated
and consitent material properties data, including design
mechanical and physical properties such as material
defects, and corrosion and environmental protection
requirements.
Power
Data
Mounted
None
Verify that the key product characteristics have been
identified.
Verify that all critical process capabilities exist to meet key
product characteristic requirements.
Verify that the processes are in place to dientify and
document all restrictions, warnings, and cautions.
Power
Data
None
Verify that processes are in place to identify and document
the technical data, and that the technical data reflects the
defined functional and product baseline.
Power
Data
Mounted
None
Verify that the procedures are in place establishing and
maintaining flight vehicle integrity.
Power
Data
Mounted
