MIL-STD-27733 Base Document:1998

1 SCOPE
1.1 Scope
2 APPLICABLE DOCUMENTS
3 DEFINITIONS
3.1 Modification engineering authority
3.2 Modification number
3.3 Temporary non-standard modification
4 GENERAL REQUIREMENTS
4.1 General
4.2 Modification data
4.2.1 Temporary non-standard modification documentation
4.2.2 Component certificate of airworthiness
4.2.3 Aerospace vehicle certificate of airworthiness
4.2.4 Modification number
4.3 Checks and evaluations
4.3.1 Operational ground checks
4.3.2 Aerodynamic evaluation flight
4.3.3 Inspection prior to first flight
4.3.4 Mass properties
4.3.5 Electrical loads
5 DETAILED REQUIREMENTS
5.1 General
5.2 Modification requirements
5.2.1 Master power switch
5.2.2 Polyvinyl chloride (PVC) wiring
5.2.3 Advisory plate
5.3 Identification and marking
5.3.1 General markings
5.3.2 Control components
5.3.3 Modification components
5.3.4 Specially calibrated instruments or modified components
5.3.5 External components
5.3.5.1 Fuel tanks
5.3.5.2 Non-standard tanks and stores
5.3.6 Electrical wire marking
5.3.6.1 Electrical wire identification
5.3.6.2 Speciality wiring
5.3.7 Tubing
6 NOTES
6.1 Intended use
6.2 Associated data item description (DID)
6.3 Reference information
6.3.1 Wire marking and installation
6.3.2 General engineering manuals
6.3.3 Other manuals
6.3.3.1 Copies of manuals
6.3.4 Quality assurance
6.3.4.1 Responsibility for inspection
6.4 Subject term (key word) listing
6.5 Changes from previous issue
FIGURE
1 Example of typical specific control identification plate
2 Example of typical general control identification plate
3 Component identification label
4 Component identification, limited space
INDEX

Defines marking, safety, and configuration control practices for temporary non-standard modifications on aerospace vehicles owned by Department of Defense, and related support equipment in support of research, development, test and evaluation.