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MIL-HDBK-516 Revision C:2014

Current

Current

The latest, up-to-date edition.

AIRWORTHINESS CERTIFICATION CRITERIA

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FOREWORD
1. SCOPE
2. APPLICABLE DOCUMENTS
3. DEFINITIONS AND ABBREVIATIONS
4. SYSTEMS ENGINEERING
5. STRUCTURES
6. FLIGHT TECHNOLOGY
7. PROPULSION AND PROPULSION INSTALLATIONS
8. AIR VEHICLE SUBSYSTEMS
9. CREW SYSTEMS
10. DIAGNOSTICS SYSTEMS
11. AVIONICS
12. ELECTRICAL SYSTEM
13. ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E[3])
14. SYSTEM SAFETY
15. COMPUTER SYSTEMS AND SOFTWARE
16. MAINTENANCE
17. ARMAMENTS AND STORES INTEGRATION
18. PASSENGER SAFETY
19. MATERIALS
20. AIR TRANSPORTABILITY, AIRDROP, MISSION/TEST
    EQUIPMENT AND CARGO/PAYLOAD SAFETY
21. NOTES
APPENDIX A - AIRWORTHINESS CERTIFICATION CRITERIA
             POINTS OF CONTACT

Sets up the airworthiness certification criteria, standards and methods of compliance to be used in the determination of airworthiness of all manned and unmanned, fixed and rotary wing air systems.

Committee
AREA SESS
DocumentType
Standard
Pages
528
PublisherName
US Military Specs/Standards/Handbooks
Status
Current

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MIL-STD-1474 Revision E:2015 NOISE LIMITS
FAA AC 25.1309-1 : 0 SYSTEM DESIGN AND ANALYSIS
MIL-HDBK-310 Base Document:1997 DEPARTMENT OF DEFENSE HANDBOOK - GLOBAL CLIMATIC DATA FOR DEVELOPING MILITARY PRODUCTS
RTCA DO 331 : 2011 MODEL-BASED DEVELOPMENT AND VERIFICATION SUPPLEMENT TO DO-178C AND DO-278A
STANAG 3899 : 0 GROUND FIT AND COMPATIBILITY CRITERIA FOR AIRCRAFT STORES
MIL-HDBK-1599 Revision A:1997 BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS
MIL-STD-805 Revision B:1987 TOWING FITTING AND PROVISIONS FOR FIXED WING AIRCRAFT, DESIGN, REQUIREMENTS FOR
FAA AC 33.76-1 : 2009 BIRD INGESTION CERTIFICATION STANDARDS
FAA AC 20-138 : 2014 AIRWORTHINESS APPROVAL OF POSITIONING AND NAVIGATION SYSTEMS
FAA AC 25-9 : 0 SMOKE DETECTION, PENETRATION AND EVACUATION TESTS AND RELATED FLIGHT MANUAL EMERGENCY PROCEDURES
MIL-HDBK-470 Revision A:1997 DESIGNING AND DEVELOPING MAINTAINABLE PRODUCTS AND SYSTEMS - VOLUME 1
EIA 632 : 1999 PROCESSES FOR ENGINEERING A SYSTEM
ADS-63-SP : 2001 AERONAUTICAL DESIGN STANDARD - STANDARD PRACTICE - RADAR SYSTEM AIRWORTHINESS QUALIFICATION AND VERIFICATION REQUIREMENTS
SAE AS 8584 : 2013 BRAKE SYSTEMS, WHEEL, MILITARY AIRCRAFT
MIL-HDBK-1587 Base Document:1996 MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEM
FAA AC 20-115 : 2017 AIRBORNE SOFTWARE DEVELOPMENT ASSURANCE USING EUROCAE ED-12( ) AND RTCA DO-178( )
FAA AC 25.981-1 : 2008 FUEL TANK IGNITION SOURCE PREVENTION GUIDELINES
FAA AC 33-5 : 0 TURBINE ENGINE ROTOR BLADE CONTAINMENT/DURABILITY
MIL PRF 5096 : F MANUALS, TECHNICAL - INSPECTION AND MAINTENANCE REQUIREMENTS - ACCEPTANCE AND FUNCTIONAL CHECK FLIGHT PROCEDURES AND CHECKLISTS - INSPECTION WORK CARDS, AND CHECKLISTS, PREPARATION OF
MIL-PRF-85676 Revision A:2006 LIGHTING, EMERGENCY EGRESS, SUBASSEMBLY
SAE ARP 1070 : 2014 DESIGN AND TESTING OF ANTISKID BRAKE CONTROL SYSTEMS FOR TOTAL AIRCRAFT COMPATIBILITY
MIL-HDBK-6870 Revision B:2012 NONDESTRUCTIVE INSPECTION PROGRAM REQUIREMENTS FOR AIRCRAFT AND MISSILE MATERIALS AND PARTS
FAA AC 120-42 : 2008 EXTENDED OPERATIONS (ETOPS AND POLAR OPERATIONS)
MIL-STD-331 Revision D:2017 FUZES, IGNITION SAFETY DEVICES AND OTHER RELATED COMPONENTS, ENVIRONMENTAL AND PERFORMANCE TESTS FOR
MIL-STD-2161 Revision C:2014 Paint Schemes and Exterior Markings for U.S. Navy and Marine Corps Aircraft
FAA AC 43.13-1 : 0 ACCEPTABLE METHODS, TECHNIQUES, AND PRACTICES - AIRCRAFT INSPECTION AND REPAIR
FAA AC 20-41 : A SUBSTITUTE TECHNICAL STANDARD ORDER (TSO) AIRCRAFT EQUIPMENT
FAA AC 25.853-1 : 0
EIA SEB6 : A1990 SYSTEM SAFETY ENGINEERING IN SOFTWARE DEVELOPMENT
GEIA EIA649B:2011 CONFIGURATION MANAGEMENT STANDARD
MIL-STD-1798 Revision C:2013 MECHANICAL EQUIPMENT AND SUBSYSTEMS INTEGRITY PROGRAM
MIL-HDBK-704-7 Base Document:2004 Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics 270 VDC (Part 7 of 8 Parts)
SAE ARP 5412 : 2013 AIRCRAFT LIGHTNING ENVIRONMENT AND RELATED TEST WAVEFORMS
MIL-W-5088 Revision L:1991 Wiring, Aerospace Vehicle (Future Design Should Refer to SAE-AS50881)
JSSG-2006 Base Document:1998 JOINT SERVICE SPECIFICATION GUIDE - AIRCRAFT STRUCTURES
FED-STD-595 Revision C:2008 COLORS USED IN GOVERNMENT PROCUREMENT
NASA STD 8739.8 : 2004 SOFTWARE ASSURANCE STANDARD
RTCA DO 236 : C2013 CHG 1 2014 MINIMUM AVIATION SYSTEM PERFORMANCE STANDARDS: REQUIRED NAVIGATION PERFORMANCE FOR AREA NAVIGATION
MIL-STD-1289 Revision D:2003 AIRBORNE STORES GROUND FIT AND COMPATIBILITY, REQUIREMENTS
MIL-PRF-7115-4 Revision A:2014 CONVERTER, AIRCRAFT 300 AMPERE, TYPE 2, CLASS A, FAN COOLED
RTCA DO 255 : 2000 Requirements Specification for Avionics Computer Resource (ACR)
FAA AC 25-17 : 2009 TRANSPORT AIRPLANE CABIN INTERIORS CRASHWORTHINESS HANDBOOK
MIL-A-19736 Revision A:1960 AIR REFUELLING SYSTEMS, GENERAL SPECIFICATION FOR
FAA AC 20-128 : 0 DESIGN CONSIDERATIONS FOR MINIMIZING HAZARDS CAUSED BY UNCONTAINED TURBINE ENGINE AND AUXILIARY POWER UNIT ROTOR FAILURE
MIL STD 188/182 : B CHANGE 3 INTEROPERABILITY STANDARD FOR UHF SATCOM DAMA ORDERWIRE MESSAGES AND PROTOCOLS
MIL-HDBK-221 Base Document:1965 FIRE PROTECTION DESIGN HANDBOOK FOR U.S. NAVY AIRCRAFT POWERED BY TURBINE ENGINES
RTCA DO 297 : 2005 Integrated Modular Avionics (IMA) Development Guidance and Certification Considerations<br>
JSSG-2010-5 Base Document:1998 Crew Systems Aircraft Lighting Handbook
FAA AC 25.869-1 : 2007 FIRE PROTECTION: SYSTEMS
MIL-HDBK-419 Revision A:1987 GROUNDING, BONDING, AND SHIELDING FOR ELECTRONIC EQUIPMENTS AND FACILITIES - VOLUME 1: BASIC THEORY & VOLUME 2: APPLICATIONS
FAA AC 20-148 : 2004 REUSABLE SOFTWARE COMPONENTS
FAA AC 20-29 : 0 USE OF AIRCRAFT FUEL ANTI-ICING ADDITIVES
MIL-HDBK-2084 Base Document:1995 General Requirements for Maintainability of Avionic and electronic Systems and Equipment
RTCA DO 332 : 2011 OBJECT-ORIENTED TECHNOLOGY AND RELATED TECHNIQUES SUPPLEMENT TO DO-178C AND DO-278A
SAE AIR 4845 : 1993 THE FMECA PROCESS IN THE CONCURRENT ENGINEERING (CE) ENVIRONMENT
SAE ARP 5794 : 2014 CENTRIFUGAL AIRCRAFT FUEL PUMP REQUIREMENTS, DESIGN AND TESTING, AEROSPACE STANDARD
MIL-HDBK-1760 Revision A:2004 AIRCRAFT/STORE ELECTRICAL INTERCONNECTION SYSTEM
ARINC 609 : 1987 DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS
MIL-STD-1425 Revision A:1991 SAFETY DESIGN REQUIREMENTS FOR MILITARY LASERS AND ASSOCIATED SUPPORT EQUIPMENT
MIL-HDBK-704-3 Base Document:2004 Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics Three Phase, 400 HZ, 115 Volt (Part 3 of 8 Parts)
MIL-STD-961 Revision E:2003 DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT
FAA AC 33.28-1 : 0 COMPLIANCE CRITERIA FOR 14 CFR SECTION 33.28, AIRCRAFT ENGINES, ELECTRICAL AND ELECTRONIC ENGINE CONTROL SYSTEMS

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