MIL-HDBK-516C DEPARTMENT OF DEFENSE HANDBOOK AIRWORTHINESS CERTIFICATION CRITERIA
MIL-HDBK-516C
CONTENTS
PARAGRAPH PAGE
FOREWORD ............................................................................................................ ii
1. SCOPE .......................................................................................................... 1
1.1 Scope...................................................................................................................... 1
1.2 Applicability ............................................................................................................. 1
1.3 Cross reference and technical points of contact. ..................................................... 2
1.3 Information sources ................................................................................................. 2
2. APPLICABLE DOCUMENTS ......................................................................... 4
2.1 General ................................................................................................................... 4
2.2 Government documents....................................................................................................... 4
3. DEFINITIONS AND ABBREVIATIONS ............................................................ 29
3.1 Definitions ..............................................................................................................29
3.2 Abbreviations and acronyms ..................................................................................40
4. SYSTEMS ENGINEERING ......................................................................... 49
4.1 Design criteria. .......................................................................................................49
4.2 Tools and databases ..............................................................................................53
4.3 Materials selection .................................................................................................54
4.4 Manufacturing and quality ......................................................................................55
4.5 Operator’s and maintenance manual/technical orders ............................................57
4.6 Configuration management (CM) ...........................................................................59
5. STRUCTURES ............................................................................................ 61
5.1 Loads .....................................................................................................................62
5.2 Structural dynamics ................................................................................................75
5.3 Strength .................................................................................................................86
5.4 Damage tolerance and durability (fatigue) ..............................................................93
5.5 Mass properties ................................................................................................... 103
5.6 Flight release ....................................................................................................... 105
6. FLIGHT TECHNOLOGY ............................................................................ 110
6.1 Flying qualities ..................................................................................................... 111
6.2 Vehicle control functions (VCF) ............................................................................ 142
6.3 Air vehicle aerodynamics and performance .......................................................... 178
7. PROPULSION AND PROPULSION INSTALLATIONS ............................. 184
7.1 Propulsion risk management ................................................................................ 185
7.2 Gas turbine engine applications ........................................................................... 187
7.3 Alternate propulsion systems ............................................................................... 216
8. AIR VEHICLE SUBSYSTEMS ................................................................... 235
8.1 Hydraulic and pneumatic systems ........................................................................ 235
8.2 Environmental control system (ECS) .................................................................... 242
8.3 Fuel system.......................................................................................................... 250
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