PWS 2.0_jj_MIL-HDBK-516C.pdf

NOT MEASUREMENT

SENSITIVE

MIL-HDBK-516C

12 December 2014

SUPERSEDING

MIL-HDBK-516B

w/CHANGE 1 29 February 2008

DEPARTMENT OF DEFENSE

HANDBOOK

AIRWORTHINESS CERTIFICATION CRITERIA

THIS HANDBOOK IS FOR GUIDANCE ONLY.

DO NOT CITE THIS DOCUMENT AS A REQUIREMENT.

AMSC N/A AREA SESS

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.

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MIL-HDBK-516C

FOREWORD

1. This handbook is approved for use by all Departments and Agencies of the Department of Defense.

2. The criteria contained herein are qualitative in nature. References are provided as background for understanding the criteria, and as a basis for tailoring standards and/or methods of compliance. Also, note that each section contains a list of typical certification source data that may be referenced for evaluating system compliance with that section’s criteria. Terms such as "acceptable" used in the criteria are parameters whose specific definition must be determined and documented by the implementing office in the context of each unique air system.

3. Comments, suggestions, or questions on this document should be addressed to AFLCMC/ENRS, Bldg 28, 2145 Monahan Way, Wright-Patterson AFB OH 45433-7017 or emailed to Engineering.Standards@us.af.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at https://assist.dla.mil.

ii

Check the source to verify that this is the current version before use.

mailto:Engineering.Standards@us.af.mil https://assist.dla.mil/

CONTENTS

PARAGRAPH PAGE

FOREWORD ............................................................................................................ ii

1. SCOPE

1.1 Scope

1.2 Applicability

1.3 Cross reference and technical points of contact

1.3 Information sources

2. APPLICABLE DOCUMENTS

2.1 General

2.2 Government documents

3. DEFINITIONS AND ABBREVIATIONS

3.1 Definitions

3.2 Abbreviations and acronyms

4. SYSTEMS ENGINEERING

4.1 Design criteria

4.2 Tools and databases

4.3 Materials selection

4.4 Manufacturing and quality

4.5 Operator’s and maintenance manual/technical orders

4.6 Configuration management (CM)

5. STRUCTURES

5.1 Loads

5.2 Structural dynamics

5.3 Strength

5.4 Damage tolerance and durability (fatigue)

5.5 Mass properties

5.6 Flight release

6. FLIGHT TECHNOLOGY

6.1 Flying qualities

6.2 Vehicle control functions (VCF)

6.3 Air vehicle aerodynamics and performance

7. PROPULSION AND PROPULSION INSTALLATIONS

7.1 Propulsion risk management

7.2 Gas turbine engine applications

7.3 Alternate propulsion systems

8. AIR VEHICLE SUBSYSTEMS

8.1 Hydraulic and pneumatic systems

8.2 Environmental control system (ECS)

8.3 Fuel system

8.4 Fire and hazard protection

iii

PARAGRAPH PAGE

8.5 Landing gear and deceleration systems

8.6 Auxiliary power system/emergency power system(s) APS/EPS

8.7 Aerial refueling

8.8 Mechanisms

8.9 External cargo hook systems (rotary wing)

8.10 External rescue hoist (rotary wing)

8.11 Fast rope insertion/extraction systems (FRIES) (rotary wing)

9. CREW SYSTEMS

9.1 Escape and egress systems

9.2 Crew stations, control stations and aircraft interiors

9.3 Air system lighting

9.4 Human performance

9.5 Life support systems

9.6 Transparency integration

9.7 Crash survivability

9.8 Lavatories, galleys, and areas not continuously occupied

10. DIAGNOSTICS SYSTEMS

10.1 Failure modes

10.2 Operation

11. AVIONICS

11.1 Avionics architecture

11.2 Avionics subsystems

11.3 Air vehicle avionics

12. ELECTRICAL SYSTEM

12.1 Electric power generation system

12.2 Electrical wiring system, including power distribution

13. ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3)

13.1 Component/subsystem E3 qualification

13.2 System-level E3 qualification

14. SYSTEM SAFETY

14.1 System safety program

14.2 Safety design requirements

14.3 Software safety program

15. COMPUTER SYSTEMS AND SOFTWARE

15.1 System processing architecture (SPA)

15.2 Design and functional integration of SPA elements

15.3 Processing hardware/electronics

15.4 Software development processes

15.5 Software architecture and design

15.6 Software qualification and installation

iv

PARAGRAPH PAGE

16. MAINTENANCE

16.1 Maintenance manuals/checklists

16.2 Inspection requirements

17. ARMAMENTS AND STORES INTEGRATION

17.1 Gun/rocket integration and interface

17.2 Stores integration

17.3 Laser integration

17.4 Safety interlocks

18. PASSENGER SAFETY

18.1 Survivability of passengers

18.2 Fire resistance

18.3 Physiology requirements of occupants

19. MATERIALS

19.1 Properties and processes

19.2 Corrosion

19.3 Non-destructive inspection (NDI)

19.4 Wear and erosion

20. AIR TRANSPORTABILITY, AIRDROP, MISSION/TEST EQUIPMENT AND

CARGO/PAYLOAD SAFETY

20.1 Air transportability and airdrop

20.2 Mission/test equipment operations and installation

21. NOTES

21.1 Intended use

21.2 Subject term (keyword) listing

21.3 Changes from previous issue

APPENDIX A AIRWORTHINESS CERTIFICATION CRITERIA POINTS OF

CONTACT

TABLE

TABLE I Navy first flight release minimum data requirements v

1. SCOPE

Scope. 1.1 This document establishes 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. It is a foundational document to be used by the service airworthiness authority to define an air system’s airworthiness certification basis. This handbook is for guidance only and cannot be cited as a requirement.

Applicability. 1.2 This handbook should be applied at any point throughout the life-cycle of an air system when an airworthiness determination is necessary, especially whenever there is a change to the functional or product baseline.

Each air system configuration, including but not limited to manned, unmanned, fixed or rotary-wing demands unique safety-of-flight (SOF) airworthiness certification requirements. Therefore, unique criteria are included for these types of systems to ensure that minimum levels of design for safe operation and maintenance are established. For unmanned air vehicles (UAVs), SOF risks associated with loss of aircrew may not apply. However, as with manned air vehicles, SOF risk associated with personnel, damage to equipment, property, and/or environment must be considered. UAVs which carry aircrew or passengers are subject to the same airworthiness certification requirements as manned aircraft. Any aircraft which may carry personnel (for example, passengers, patients, special mission personnel) are subject to certification requirements for passenger aircraft.

An Unmanned Aircraft System (UAS) is comprised of individual elements consisting of the UAV, the control station, and any other support elements necessary to enable operation including, but not limited to data links, communications systems/links, and UAS-unique launch and recovery equipment. UAV types vary greatly in size, weight, and complexity. Consideration should be given to the environment in which the UAS will be operated (controlled test range, national airspace, fleet usage, including ship based applications), to the life expectancy of the system for which it is designed, and to the “expendability” of the UAV.

Similarly, air vehicles intended for use aboard ships have unique requirements in areas such as structural integrity, propulsion system dynamic response and tolerance to steam ingestion, control systems response to approach and landings in high turbulence conditions, electromagnetic environmental effects, deck handling, support and servicing, and pilot field of view.

Commercial derivative aircraft (CDA) are initially approved for safety of flight by the Federal Aviation Administration (FAA) and may have an FAA approved Certificate of Airworthiness (that is, Type Certificate). Any non-FAA approved alteration to a CDA may render all FAA certifications invalid. While alterations to CDA are covered by rules unique to each branch of service, the operating service always has the responsibility for the airworthiness certification approval under public aircraft rules. Therefore, when planning any alterations to an FAA certified CDA, the modifier should, at the earliest opportunity, contact the FAA Military Certification Office (MCO) in Wichita, KS.

In all instances, complete and accurate documentation of both applicability and system specific measurable criteria values is critical to ensuring consistent, timely, and accurate airworthiness assessments.

Tailoring to create the certification basis. 1.2.1 Not all of the airworthiness criteria apply to every type of air system; also, platform-unique, previously undefined criteria may need to be added to fully address safety aspects of unique configurations. Therefore, tailor the total set of criteria to identify a complete (necessary and sufficient) subset of applicable airworthiness criteria, creating the system’s certification basis.

This certification basis should be fully documented and maintained under strict configuration control.

Tailoring rules are as follows:

a. Identify each criterion as applicable, partially applicable or non-applicable, considering system or product complexity, type, data, and intended use. Document the rationale for identifying any criterion as non-applicable.

b. Fully applicable criteria may not be deleted or modified in any manner.

c. If a portion of a criterion partially applies, identify the applicable or non-applicable portion.

Document the rationale for identifying any criterion as partially applicable.

d. Supplement applicable or partially applicable criteria where appropriate for any capabilities or systems not fully addressed by the criteria contained in this handbook.

e. Develop additional criteria, as appropriate. Document the rationale for any capabilities or systems not fully addressed by the criteria contained in this handbook. Consider whether such criteria should be submitted for future inclusion in this handbook.

f. Standards and methods of compliance may be tailored, considering system type, capabilities and intended use.

Cross references and technical points of contact. 1.3 The criteria included in this document are written with the intent that an experienced engineer, trained in the specific technical area under consideration, should be able to interpret, tailor, apply, and evaluate a particular system’s compliance with the criteria. To assist in this effort, military and civil references are included with the specific criteria.

For additional information or clarification call the appropriate service point of contact provided in Appendix A.2.

For Commercial Derivative Aircraft (CDA), contact the FAA Military Certification Office (MCO) point of contact, provided in Appendix A.2.

Information sources. 1.4 Where applicable, reference documents are identified for each Airworthiness Certification Criterion. Source reference documents may include, but are not limited to the following:

International Standardization Agreements Federal Specifications Federal Standards

Commercial Item Descriptions Department of Defense (DoD) Specifications Department of Defense Standards Department of Defense Handbooks Other Government documents, drawings and publications.

Non-Government standards and other publications.

The FAA Title 14, Code of Federal Regulations (CFR) Part (for example, 23, 25, 27, 29) referenced is dependent on aircraft type and must be consistent with aircraft size and usage.

The list shown is not all inclusive and the user is cautioned to look at the reference material only as a guide and not for purposes of citing requirements. The user is also advised to use additional FAA Advisory Circulars or other FAA Policy documents, such as Orders and Notices that may be found on the FAA website, to assist in understanding the FAA's implementation of the regulatory requirements.

2. APPLICABLE DOCUMENTS

2.1 General.

The documents listed below are not necessarily all of the documents referenced herein, but are those needed to understand the information provided by this handbook.

2.2 Government documents.

2.2.1 Specifications, standards, and handbooks.

The following specifications, standards, and handbooks form a part of this document to the extent specified herein.

INTERNATIONAL STANDARDIZATION AGREEMENTS

ALLIED ORDNANCE PUBLICATION

AOP-52 Guidance on Software Safety Design and Assessment of Munition- Related Computing Systems

(Copies of these documents are available online at https://assist.dla.mil or http//www.nato.int.)

ALLIED TACTICAL PUBLICATION (ATP)

ATP-3.3.4.2 Air-to-Air Refuelling ATP-56 (STANAG 3971 implements this standard.)

ATP-3.3.4.5 Air-to-Air (Aerial) Refuelling Equipment: Boom-Receptacle System and Interface Requirements (STANAG 7191 implements this standard.)

(Copies of these documents are available online at https://assist.dla.mil or http://nso.nato.int.)

THE INTERNATIONAL ORGANIZATION FOR STANDARDIZATION (ISO)/

THE INTERNATIONAL ELECTROTECHNICAL COMMISSION (IEC)

ISO/IEC

12207:2008(E) IEEE Std 12207

Systems and software engineering – Software life cycle processes

ISO/IEC/IEEE

24765

Systems and software engineering - Vocabulary

(Copies of these documents are available online at http://webstore.iec.ch/.)

NATO STANDARDIZATON OFFICE (NSO)

STANAG 3098 Aircraft Jacking

STANAG 3230 Emergency Markings on Aircraft

STANAG 3278 Aircraft Towing Attachments and Devices

STANAG 3447 Air-to-Air Refuelling Equipment: Probe-Drogue Interface Characteristics

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STANAG 3899 Ground Fit and Compatibility Criteria for Aircraft Stores

STANAG 3971 Air-to-Air Refuelling ATP-56

STANAG 4101 Towing Attachments

STANAG 4591 The 600 BIT/S, 1200 BIT/S and 2400 BIT/S NATO Interoperable Narrow Band Voice Coder

STANAG 4671 Unmanned Aerial Vehicles Systems Airworthiness Requirements

(USAR)

STANAG 7191 Air-to-Air (Aerial) Refuelling Equipment: Boom-Receptacle System and Interface Requirements

(Copies of these documents are available online at https://assist.dla.mil or http//www.nato.int.)

FEDERAL STANDARDS

FED-STD-595 Colors Used in Government Procurement

FED-STD-

595/13538

Yellow, Gloss

FED-STD-

595/37038

Miscellaneous, Flat Lusterless

(Copies of these documents are no longer available from GSA. For further information go to www.gsa.gov/portal/content/142623.)

DEPARTMENT OF DEFENSE SPECIFICATIONS

JSSG-2000 Air System

JSSG-2001 Air Vehicle

JSSG-2005 Avionic Subsystem Main Body

JSSG-2006 Aircraft Structures

JSSG-2007 Engines, Aircraft, Turbine

JSSG-2008 Vehicle Control and Management System (VCMS)

JSSG-2009 Air Vehicle Subsystems

JSSG-2010 Crew Systems

JSSG-2010-1 Crew Systems Engineering Handbook

JSSG-2010-2 Crew Systems Crew Station Automation, Information and Control/Display Management Handbook

JSSG-2010-3 Crew Systems Cockpit/Crew Station/Cabin Handbook

JSSG-2010-4 Crew Systems Aircrew Alerting Handbook

JSSG-2010-5 Crew Systems Aircraft Lighting Handbook

JSSG-2010-6 Crew Systems Sustenance and Waste Management Handbook

JSSG-2010-7 Crew Systems Crash Protection Handbook

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JSSG-2010-8 Crew Systems Energetics Handbook

JSSG-2010-9 Crew Systems Personal Protective Equipment Handbook

JSSG-2010-10 Crew Systems Handbook

JSSG-2010-11 Crew Systems Emergency Egress Handbook

JSSG-2010-12 Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook

JSSG-2010-13 Crew Systems Survival, Search, and Rescue (SSAR) Handbook

JSSG-2010-14 Crew Systems Aircraft Windshield/Canopy Systems and Transparent Enclosures Handbook

MIL-W-5013 Wheel and Brake Assemblies, Aircraft General Specification for (Inactive for New Design)

MIL-PRF-5041 Tires, Ribbed Tread, Pneumatic, Aircraft

MIL-W-5088 Wiring, Aerospace Vehicle (Inactive for New Design) (Future designs should refer to SAE AS50881)

MIL-PRF-5096 Manuals, Technical - Inspection and Maintenance Requirements;

Acceptance and Functional Check Flight Procedures and Checklists;

Inspection Work Cards; and Checklists; Preparation of

MIL-PRF-5920 Manuals, Technical: Sample Basic Weight Checklists and Loading Data

MIL-T-6053 Tests, Impact, Shock Absorber Landing Gear, Aircraft (Inactive for New Design)

MIL-E-7016 Electric Load and Power Source Capacity, Aircraft, Analysis of MIL-PRF-7032 Inverters, Aircraft, General Specification for

MIL-PRF-7115/4 Converter, Aircraft, 300 Ampere, Type II, Class A, Fan Cooled

MIL-DTL-7700 Flight Manual, Performance Data Appendix, Mission Crew Manual, Supplemental Manual, and Abbreviated Flight Crew Checklist

MIL-L-8552 Landing Gear, Aircraft Shock Absorber (Air-Oil Type)

MIL-PRF-8565 Battery Storage, Aircraft, General Specification for

MIL-B-8584 Brake Systems, Wheel, Aircraft, Design of MIL-S-8812 Steering System: Aircraft, General Requirements for

MIL-A-8863 Airplane Strength and Rigidity Ground Loads for Navy Acquired Airplanes

MIL-A-8865 Airplane Strength and Rigidity Miscellaneous Loads

MIL-A-8870 Airplane Strength and Rigidity Vibration, Flutter, and Divergence

MIL-F-17874 Fuel Systems: Aircraft, Installation and Test of

MIL-A-18717 Arresting Hook Installation, Aircraft

MIL-A-19736 Air Refueling Systems, General Specification for

MIL-PRF-21480 Generator System, Electric Power, 400 Hertz, Alternating Current, Aircraft; General Specification for

MIL-E-22285 Extinguishing System, Fire, Aircraft, High-Rate-Discharge Type, Installation and Test of (Inactive for New Design)

MIL-D-23222 Demonstration Requirements for Helicopters

MIL-DTL-25959 Tie Down, Tensioners, Cargo, Aircraft

MIL-PRF-27260 Tie Down, Cargo, Aircraft, CGU-1/B

MIL-PRF-29595 Batteries and Cells, Lithium, Rechargeable, Aircraft, General Specification for

MIL-PRF-63029 Manuals, Technical: Requirements for Operator's Manuals and Checklists for Manned Aircraft Systems

MIL-T-81259 Tie-Downs, Airframe Design, Requirements for MIL-PRF-81757 Batteries and Cells, Storage, Nickel-Cadmium, Aircraft General

Specification for

MIL-C-83124 Cartridge Actuated Devices/Propellant Actuated Devices General Design Specification for

MIL-C-83125 Cartridge for Cartridge Actuated/Propellant Actuated Devices, General Design Specification for

MIL-C-83126 Propulsion Systems, Aircrew Escape, Design Specification for

MIL-DTL-85025 NATOPS Program Technical Publications and Products; Style, Format and Common Technical Content

MIL-DTL-85110 Bar, Repeatable Release Holdback (RRHB), Aircraft Launching.

General Requirement for

MIL-L-85314 Light Systems, Aircraft, Anti-Collision, Strobe, General Specification for

MIL-E-85583 Electric Power Generating Channel, Variable Input Speed, Alternating Current, 400 Hz, Aircraft; General Specification for

MIL-PRF-85676 Lighting, Emergency Egress, Subassembly

MIL-L-85762 Lighting, Aircraft, Interior, Night Vision Imaging System (NVIS) Compatible

AFGS-87139 Landing Gear Systems

AFGS-87219 Electrical Power Systems, Aircraft

AFGS-87256 Integrated Diagnostics (Inactive for New Design)

MIL-L-85762 Lighting, Aircraft, Interior, Night Vision Imaging System (NVIS) Compatible

DEPARTMENT OF DEFENSE STANDARDS

MIL-STD-188-141 Interoperability and Performance Standards for Medium and High

Frequency Radio Systems

MIL-STD-188-181 Interoperability Standard for Access to 5-kHz and 25-kHz UHF Satellite Communications Channels

MIL-STD-188-182 Interoperability Standard for UHF SATCOM DAMA Orderwire Messages and Protocols

MIL-STD-188-242 Interoperability and Performance Standards for Tactical Single Channel Very High Frequency (VHS) Radio Equipment

MIL-STD-188-243 Tactical Single Channel Ultra High Frequency (UHF) Radio Communications

MIL-STD-331 Fuze and Fuze Components, Environmental and Performance Tests for

MIL-STD-411 Aircrew Station Alerting Systems

MIL-STD-461 Requirements for the Control of Electromagnetic Interference Characteristics of Subsystems and Equipment

MIL-STD-464 Electromagnetic Environmental Effects Requirements for Systems

MIL-STD-704 Aircraft Electric Power Characteristics

MIL-STD-805 Towing Fittings and Provisions for Military Aircraft, Design Requirements for

MIL-STD-810 Environmental Engineering Considerations and Laboratory Tests

MIL-STD-882 System Safety

MIL-STD-889 Dissimilar Metals

MIL-STD-961 Defense and Program-Unique Specifications Format and Content

MIL-STD-1289 Airborne Stores, Ground Fit and Compatibility Requirements

MIL-STD-1290 Light Fixed and Rotary-Wing Aircraft Crash Resistance

MIL-STD-1310 Shipboard Bonding, Grounding, and Other Techniques for Electromagnetic Compatibility, Electromagnetic Pulse (EMP) Mitigation and Safety

MIL-STD-1399-

Section 300 Electric Power, Alternating Current

MIL-STD-1399-

Section 390 Electric Power, Direct Current (other than Ship’s Battery) for Submarines (Metric), MIL-STD-1425 Safety Design Requirements for Military Lasers and Associated Support Equipment

MIL-STD-1472 Human Engineering

MIL-STD-1474 Noise Limits

MIL-STD-1530 Aircraft Structural Integrity Program (ASIP)

MIL-STD-1568 Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems

MIL-STD-1683 Connectors and Jacketed Cable, Electric, Selection Standard for Shipboard Use

MIL-STD-1760 Aircraft/Store Electrical Interconnection System

MIL-STD-1787 Aircraft Display Symbology

MIL-STD-1791 Designing for Internal Aerial Delivery in Fixed Wing Aircraft

MIL-STD-1796 Avionics Integrity Program (AVIP)

MIL-STD-1797 Flying Qualities of Piloted Aircraft

MIL-STD-1798 Mechanical Equipment and Subsystems Integrity Program

MIL-STD-2161 Paint Schemes and Exterior Markings for U.S. Navy and Marine Corps Aircraft

MIL-STD-2169 High-Altitude Electromagnetic Pulse (HEMP) Environment (U)

MIL-STD-3009 Lighting, Aircraft, Night Vision Imaging System (NVIS) Compatible

MIL-STD-3013 Glossary of Definitions, Ground Rules, and Mission Profiles to Define Air Vehicle Performance Capability

MIL-STD-3022 Documentation of Verification, Validation, and Accreditation (VV&A) for Models and Simulations

MIL-STD-3024 Propulsion System Integrity Program (PSIP)

MIL-STD-5522 Test Requirements and Methods for Aircraft Hydraulic and Emergency Pneumatic Systems

MIL-STD-7080 Selection and Installation of Aircraft Electric Equipment

MIL-STD-7179 Finishes, Coatings, and Sealants, for the Protection of Aerospace Weapons Systems

MIL-STD-8591 Airborne Stores, Suspension Equipment and Aircraft-Store Interface (Carriage Phase)

MIL-STD-27733 Modification and Marking Requirements for Test Equipment in Aerospace Vehicles and Related Support Equipment

MIL-STD-38784 Standard Practice for Manuals, Technical: General Style and Format Requirements

MIL-STD-46855 Human Engineering Requirements for Military Systems, Equipment, and Facilities

DEPARTMENT OF DEFENSE HANDBOOKS

MIL-HDBK-61 Configuration Management Guidance

MIL-HDBK-217 Reliability Prediction of Electronic Equipment

MIL-HDBK-221 Fire Protection Design Handbook for U.S. Navy Aircraft Powered by Turbine Engines

MIL-HDBK-244 Guide to Aircraft/Stores Compatibility

MIL-HDBK-299 Cable Comparison Handbook Data Pertaining to Electrical Shipboard Cable

MIL-HDBK-310 Global Climatic Data for Developing Military Products

MIL-HDBK-419 Grounding, Bonding and Shielding for Electronic Equipments and Facilities, (Handbook contains both Volume 1 Basic Theory, and Volume II Applications)

MIL-HDBK-470 Designing and Developing Maintainable Products and Systems, Volume I

MIL-HDBK-454 General Guidelines for Electronic Equipment

MIL-HDBK-515 Weapon System Integrity Guide (WSIG)

MIL-HDBK-704-1 Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics (Part 1 of 8 Parts)

MIL-HDBK-704-2 Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics Single Phase, 400 HZ, 115 Volt (Part 2 of 8 Parts)

MIL-HDBK-704-3 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-HDBK-704-4 Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics Single Phase, Variable Frequency, 115 Volt (Part 4 of 8 Parts)

MIL-HDBK-704-5 Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics Three Phase, Variable Frequency, 115 Volt (Part 5 of 8 Parts)

MIL-HDBK-704-6 Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics Single Phase, 60 HZ, 115 Volt (Part 6 of 8 Parts)

MIL-HDBK-704-7 Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics 270 VDC (Part 7 of 8 Parts)

MIL-HDBK-704-8 Guidance for Test Procedures for Demonstration of Utilization Equipment Compliance to Aircraft Electrical Power Characteristics 28 VDC (Part 8 of 8 Parts)

MIL-HDBK-828 Range Laser Safety

MIL-HDBK-1587 Materials and Process Requirements for Air Force Weapon Systems MIL-HDBK-1599 Bearings, Control System Components, and Associated Hardware

Used in the Design and Construction of Aerospace Mechanical Systems and Subsystems

MIL-HDBK-1760 Aircraft/Store Electrical Interconnection System

MIL-HDBK-1763 Aircraft/Stores Compatibility: Systems Engineering Data Requirements and Test Procedures

MIL-HDBK-1783 Engine Structural Integrity Program (ENSIP)

MIL-HDBK-2066 Catapulting and Aresting Gear Forcing Functions for Aircraft Structural Design

MIL-HDBK-2084 General Requirements for Maintainability of Avionic and Electronic Systems and Equipment

MIL-HDBK-2165 Testability Program for Systems and Equipments

MIL-HDBK-5400 Electronic Equipment, Airborne General Guidelines for

MIL-HDBK-6870 Nondestructive Inspection Program Requirements for Aircraft and Missile Materials and Parts

MIL-HDBK-87213 Electronically/Optically Generated Airborne Displays

(Copies of these documents are available online at http://quicksearch.dla.mil. Copies of MIL- STD-2169 are available from the Defense Threat Reduction Agency, 8725 John J. Kingman Road, Stop 6201, Ft. Belvoir, VA 22060 or email michael.rooney@dtra.mil.)

2.2.2 Other Government documents, drawings, and publications.

The following other Government documents, drawings, and publications form a part of this document to the extent specified herein

CODE OF FEDERAL REGULATIONS (CFR)

Title 14 Aeronautics and Space

Part 23 Airworthiness Standards: Normal, Utility, Acrobatic, and Commuter Category Airplanes

Part 25 Airworthiness Standards: Transport Category Airplanes

Part 27 Airworthiness Standards: Normal Category Rotocraft

Part 29 Airworthiness Standards: Transport Category Rotocraft

Part 33 Airworthiness Standards: Aircraft Engines

Part 35 Airworthiness Standards: Propellers

Part 60 Flight Simulation Training Device Initial and Continuing Qualification and Use

Part 121 Operating Requirements: Commuter and On Demand Operations and Rules Governing Persons on Board Such Aircraft

Part 133 Rotocraft External-Load Operations

Title 21 Food and Drugs

Part 1040 Performance Standards for Lighting-Emitting Products

(Copies of these documents can be viewed on line at www.ecfr.gov or purchased from the U.S.

Government Online Bookstore at http://bookstore.gpo.gov.)

Check the source to verify that this is the current version before use.

http://quicksearch.dla.mil/ mailto:michael.rooney@dtra.mil http://www.ecfr.gov/ http://bookstore.gpo.gov/

DEPARTMENT OF DEFENSE

DoDM 4140.01, Volume 11

DoD Supply Chain Materiel Management Procedures: Management of Critical Safety Items, Controlled Inventory Items Including Nuclear Weapons-Related Materiel

DoDI 4650.1 Policy and Procedures for Management and Use of the Electromagnetic Spectrum

DoDI 5000.02 Interim

Operation of the Defense Acquisition System

DoDI 5000.36 System Safety Engineering and Management

DoDI 6055.11 Protecting Personnel from Electromagnetic Fields

DoDD 3150.02 DoD Nuclear Weapon Surety Program

DoD 6055.9-M DoD Ammunition and Explosives Safety Standards, Vols 1 thru 8

DoDM 4140.01 DoD Supply Chain Materiel Management Procedures, Vols 1 thru 11

(Copies of the DoD documents are available online at www.dtic.mil/whs/directives.)

DoD AIMS 03-

Technical Standard For The ATCRBS/IFF/Mark XIIA Electronic Identification and Military Implementation of Mode S and Classified Addenda 1-4

DoD AIMS 97-

Technical Standard for the ATCRBS/IFF/MarkXII Electronic Identification and Military Mode S

(Copies of the DoD AIMS documents are available online at www.dod-aims.com.)

DD Form 250 Material Inspection and Receiving Report

DD Form 365-1 Weight Checklist Record, Chart A - Basic

DD Form 1494 Application for Equipment Frequency Allocation

(Copies of the DD Forms are available online at www.e-publishing.af.mil.)

JOINT/INTERSERVICE DOCUMENTS

TB 700-2/

NAVSEAINST 8020.8/

TO 11A-1-47

Department of Defense Ammunition and Explosives Hazard Classification Procedures

(Copies of the Joint Technical Bulletin are available online at https://www.ddesb.pentagon.mil/docs/TB200-2.)

SECNAVINST 4140.2/

AFI 20-106/

DA Pam 95-9/

DLAI 3200.4/

DCMA INST CSI (AV)

Management of Aviation Critical Safety Items

Check the source to verify that this is the current version before use.

http://www.dtic.mil/whs/directives http://www.dod-aims.com/ http://www.e-publishing.af.mil/ https://www.ddesb.pentagon.mil/docs/TB200-2

AFMAN 24-204 (Interservice)/

TM 38-250/

NAVSUP PUB 505/

MCO P4030.19J/

DLAI 4145.3

Preparing Hazardous Materials for Military Air Shipments

AR 702-7/

AFR 74-6/

SECNAVINST 4855.5/

DLAR 4155.24

Product Quality Deficiency Report Program

NAVAIR 01-1B-50

TO 1-1B-50

TM 55-1500-342-23

Army Aviation Maintenance Engineering Manual for Weight and Balance

NAVAIR 01-1A-505-1

TO 1-1A-14

TM 1-1500-323-24-1

Installation and Repair Practices, Volume 1 – Aircraft Electric and Electronic Wiring

(Copies of this document are available online at http://armypubs.army.mil/epubs or http://doni.daps.dla.mil.)

JOINT AERONAUTICAL COMMANDERS’ GROUP (JACG)

JACG Aviation Critical Safety Item Management Handbook

(Copies of this document are available online at https://acc.dau.mil/CommunityBrowser.aspx?id=444472.)

JACG Aviation Source Approval and Management Handbook

(Copies of this document are available online at https://acc.dau.mil/CommunityBrowser.aspx?id=394562&lang=en-US.)

JOINT SOFTWARE SYSTEM SAFETY ENGINERING WORKGROUP

DoD Joint Software Systems Safety Engineering Handbook (JSSSEH)

(Copies of the JSSSEH are available online at http://www.acq.osd.mil/se/pg/guidance.html.)

RANGE COMMANDERS COUNCIL

RCC 319 Flight Termination Systems Commonality Standard RCC 323 Range Safety Criteria for Unmanned Air Vehicles

(Copies of RCC documents are available online at www.wsmr.army.mil/RCCSITE.)

CHAIRMAN OF THE JOINT CHIEFS OF STAFF INSTRUCTION

CJCSI 6212.01 Net Ready Key Performance Parameter (NR KPP)

(Copies of this document are available online at http://www.dtic.mil/cjcs_directives/.)

Source: https://assist.dla.mil -- Downloaded: 2014-12-17T14:14Z Check the source to verify that this is the current version before use.

http://armypubs.army.mil/epubs http://doni.daps.dla.mil/ https://acc.dau.mil/CommunityBrowser.aspx?id=444472 https://acc.dau.mil/CommunityBrowser.aspx?id=394562&lang=en-US http://www.acq.osd.mil/se/pg/guidance.html http://www.wsmr.army.mil/RCCSITE.)

http://www.dtic.mil/cjcs_directives/.)

ARMY PUBLICATIONS

ARMY REGULATIONS

AR 11-9 The Army Radiation Safety Program AR 40-10 Health Hazard Assessment Program in Support of the Army

Acquisition Process

AR 70-62 Airworthiness Qualification of Aircraft Systems

AR 385-10 The Army Safety Program

ARMY PAMPHLETS

DA PAM 5-11 Verification, Validation and Accreditation of Army Models and Simulations

DA PAM 385-16 System Safety Management Guide

DA PAM 385-24 The Army Radiation Safety Program

(Copies of Army Regulations and Pamphlets are available online at http://armypubs.army.mil/epubs.)

ARMY MATERIEL COMMAND PHAMPLET

AMCP 706-201 Helicopter Engineering, Part One - Preliminary Design (AD A002007)

AMCP 706-203 Engineering Design Handbook, Helicopter Engineering, Part Three, Qualification Assurance

(Copies of these documents are available online at www.dtic.mil.)

ARMY AVIATION AND MISSILE COMMAND (AMCOM)

AMCOMR 385-

AMCOM Software System Safety Policy

AMCOMR 702-7 Flight Safety Parts/New Source Testing Program Management

(Copies of these documents are available online at https://amcom.aep.army.mil/PandP/Regulations.)

ARMY AVIATION SYSTEMS COMMAND (USAAVSCOM)

USAAVSCOM

TR-89-D-22B

Aircraft Crash Survival Design Guide, Volume II – Aircraft Design Crash Impact Cnoditions and Human Tolerance (AD-A218 435)

USAAVSCOM

TR 89-D-22E

Aircraft Crash Survival Design Guide, Volume V – Aircraft Postcrash Survival (AD-A218 438)

(Copies of these documents are available online at www.dtic.mil.)

ARMY AERONAUTICAL DESIGN STANDARDS

ADS-1-PRF Rotorcraft Propulsion System Airworthiness Qualification Requirements Ground and Flight Test Surveys and Demonstrations

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http://armypubs.army.mil/epubs http://www.dtic.mil/ https://amcom.aep.army.mil/PandP/Regulations http://www.dtic.mil/

ADS-10-SP Air Vehicle Technical Description

ADS-13-HDBK Air Vehicle Materials and Processes

ADS-24 Structural Demonstration (Cancelled)

ADS-27-SP Requirements for Rotorcraft Vibration Specifications, Modeling and Testing

ADS-29 Structural Design Criteria for Rotary Wing Aircraft (Cancelled)

ADS-33-PRF Handling Qualities Requirements for Military Rotorcraft

ADS-36 Rotary Wing Aircraft Crash Resistance (Inactive)

ADS-37-PRF Electromagnetic Environmental Effects (E3) Performance and Verification Requirements

ADS-40-SP Air Vehicle Flight Performance Description

ADS-43-HDBK Qualification Requirements and Identification of Critical Characteristics for Aircraft Engine Components

ADS-44-HDBK Armament Airworthiness Qualification for U.S. Army Aircraft

ADS-45-HDBK Data and Test Procedures for Airworthiness Release for U.S. Army Helicopter Armament Testing (Guns, Rockets, Missiles)

ADS-50-PRF Rotorcraft Propulsion Performance and Qualification Requirements and Guidelines

ADS-51-HDBK Rotorcraft and Aircraft Qualification (RAQ) Handbook ADS-62-SP Data and Test Requirements for Airworthiness Release for Helicopter

Sensor Data and Testing Requirements in Development Stage ADS-63-SP Radar System Airworthiness Qualification and Verification

Requirements

ADS-64-SP Airworthiness Reqirements for Military Rotorcraft (Inactive)

ADS-65-HDBK Data and Test Guidance for Qualification of Sensor Systems on Aircraft

ADS-66-HDBK Guidance for Data for Safety of Flight Airworthiness Release for Helicopter Aircraft Survivability Equipment (ASE)

ADS-79-HDBK Condition Based Maintenance System for US Army AircraftVibration, Specifications, Modeling and Testing

(Copies of these documents are available online at http://www.amrdec.army.mil/amrdec/rdmr-se/tdmd/StandardAero.htm.)

ARMY MEDICAL PUBLICATIONS

TB MED 523 Control of Hazards to Health from Microwave and Radio Frequency Radiation and Ultrasound

(Copies of this document are vailable online at http://armypubs.army.mil/med/index.html or http://phc.amedd.army.mil.)

Source: https://assist.dla.mil -- Downloaded: 2014-12-17T14:14Z Check the source to verify that this is the current version before use.

http://www.amrdec.army.mil/amrdec/rdmr-se/tdmd/StandardAero.htm http://www.amrdec.army.mil/amrdec/rdmr-se/tdmd/StandardAero.htm http://armypubs.army.mil/med/index.html http://phc.amedd.army.mil/

ARMY TEST AND EVALUATION CENTER

Personnel Airdrop Optimizatiopn (PAO) Models for New Personnel Airdrop Platforms; (C-141 Cumulative Distribution Function (CDF) Curve)

(Copies of this document are available from the US Army Test and Evaluation Command, Aberdeen Proving Ground Maryland by emailing usarmy.APG.atec.mbx.atec-hq-pao@mail.mil.)

NAVY PUBLICATIONS

NAVY INSTRUCTIONS

NAVAIRINST

4200.56

Critical Item Management

COMNAVAIRFO

RINST 4790.2

The Naval Aviation Maintenance Program (NAMP)

OPNAVINST

4790.2

The Naval Aviation Maintenance Program (NAMP)

NAVAIRINST

5000.21

NAVAL SYSCOM Risk Management Policy

NAVAIRINST

5100.3

Naval Aviation System Safety Program

NAVAIRINST

13034.1

Flight Clearance Policy for Air Vehicles and Aircraft Systems

(Copies of these documents are available online at http://www.navair.navy.mil/lakehurst/hro-lakehurst/inst.html. Copies of the NAMP are available online at www.navair.navy.mil/logistics/4790/.)

NAVY AERONAUTICAL REQUIREMENTS

AR-56 Structural Design Requirements (Helicopters)

AR-89 Structural Ground Test Requirements (Helicopters)

(Copies of Navy Aeronautical Requirements documents may be obtained via U. S. Mail from the following address: Structures Division, ATTN: Bldg. 2187, Suite 2340A, NAVAIRSYSCOM, 48110 Shaw Road, Unit 5, Patuxent River, MD 20670-1906. For inquiries, phone (301) 342- 9381.)

NAVAL AIR SYSTEMS COMMAND

SD-24L, Vol II General Specification for Design and Construction of Aircraft Weapon Systems – Rotary Wing Aircraft

NAVAIR 01-1B-

Technical Manual, USN/USMC Aircraft Weight and Balance Control

(Copies of these documents are available from Naval Air Systems Command, Standardization Section (AIR-4.1C), 1421 Jefferson Davis Highway, Arlington VA 22243.)

Source: https://assist.dla.mil -- Downloaded: 2014-12-17T14:14Z Check the source to verify that this is the current version before use.

mailto:usarmy.APG.atec.mbx.atec-hq-pao@mail.mil http://www.navair.navy.mil/lakehurst/hro-lakehurst/inst.html http://www.navair.navy.mil/lakehurst/hro-lakehurst/inst.html http://www.navair.navy.mil/logistics/4790/

NAVAL AIR ENGINEERING CENTER

NAEC-MISC-

06900

Aircraft Carrier Reference Manual

(Copies of Naval Air System Command documents may be obtained via Commander, Naval Air System Command, 47123 Buse Rd, B2272 Unit IPT, Patuxent River MD 20670-1547. Copies of NAVAIR Flight Clearance instructions may be obtained online at https://mynavair.navair.navy.mil.)

NAVAL SEA SYSTEMS COMMAND INSTRUCTIONS

NAV SEA OP

Electromagnetic Radiation Hazard

NAVAL SEA SYSTEMS COMMAND TECHNICAL MANUALS

NAVSEA TM-

S9310-AQ-SAF-

Technical Manual for Navy Lithium Battery Safety Program Responsibilities and Procedures

(Copies of Naval Sea System Command documents may be obtained via Naval Air System Command, 1333 Isaac Hull Ave S. E., Washington Navy Yard, D. C. 20376, phone (202) 781- 0000. Copies of NAVSEA technical manuals can be ordered from the NAVSUP Weapon Systems Support (NAVSUP WSS), Mechanicsburg, PA or from the Naval Logistic Library (NLL) at http://www.nll.navsup.navy.mil. Tech Manuals can also be acquired at Defense Automatic Addressing System Center Automatic Message Exchange System (DAMES), Standard Automated Logistic Tool Set (SALTS) or Naval Message.)

AIR FORCE PUBLICATIONS

AF POLICY DIRECTIVES

AFPD 62-6 USAF Airworthiness

AFPD 63-1;

AFPD 20-1

Integrated Life Cycle Management

AF INSTRUCTIONS

AFI 11-202V3 General Flight Rules

AFI 11-2C-

130V3

C-130 Operations Procedures

AFI 21-101 Aircraft and Equipment Maintenance Management

AFI 48-139 Laser and Optical Radiation Protection Program

AFI 63-133 Aircraft Information Programs

AFI 63-137 Assurance of Communications, Navigation, Surveillance/Air Traffic Management (CNS/ATM), Navigation Safety, and Next Generation Air Transportation System (NEXTGEN) Performance

AFI 63-501 Air Force Acquisition Quality Program

Source: https://assist.dla.mil -- Downloaded: 2014-12-17T14:14Z Check the source to verify that this is the current version before use.

https://mynavair.navair.navy.mil/ http://www.nll.navsup.navy.mil/

AFI 63-101/20-

Integrated Life Cycle Management

AF PAMPHLET

AFPAM 63-113 Program Protection Planning for Life Cycle Management

AF OCCUPATIONAL SAFETY AND HEALTH (AFOSH)

AFOSH

AFOSHSTD48-

Occupational Noise and Hearing Conservation Program

(Copies of these documents are available online at http://www.e-publishing.af.mil/.)

AIR FORCE TECHNICAL ORDER (AFTO)

TO 00-5-1 AF Technical Order System (ATOS)

TO 00-5-3 AF Technical Order Life Cycle Management

TO 1-1B-50 Basic Technical Order for USAF Aircraft – Weight and Balance

TO 31Z-10-0 Electromagnetic Radiation Hazard

TO 31Z-10-4 Joint Services Command, Control, Communication, and Computer Systems Electromagnetic Radiation Hazards

(Copies of these documents are available online at www.tinker.af.mil/technicalorders/.)

AIR FORCE TECHNICAL REPORTS

AFFTC-TR-95-

Evaluation of the C-17A Aircraft Personnel and Equipment Bundles Airdrop Capabilities; (C-17 High Altitude Entanglement Test Procedures)

AFRL-HE-WP-

TR-2002-0118

(ADA405598)

Body Size Accommodation in USAF Aircraft

(Copies of these documents are available online at www.dtic.mil.)

OTHER AIR FORCE DOCUMENTS

ASC-TM-ENE-

77-1

Criteria for Nonstandard Airdrop Loads

BP-99-06D AFLCMC/LP USAF Propulsion Center of Excellence Best Practice, Risk Management Process

AWB-013 USAF Airworthiness Bulletin, Risk Identification and Acceptance for Airworthiness Determinations

ENFS-SB-05-

Joint USAF/USN Aircraft Loads Flight Release Methodology to Establish Aircraft Operating Limits Utilizing Demonstrated Strength Capability

Check the source to verify that this is the current version before use.

http://www.e-publishing.af.mil/ http://www.e-publishing.af.mil/ http://www.tinker.af.mil/technicalorders/

EN-SB-08-001 Revised Damage Tolerance Requirements and Determination of Fail- Safety Life Limits for Fail-Safe Metallic Structures

EN-SB-12-002 USAF Structures Bulletin: Methodology to Establish Bird Strike Design Criteria

ENFC-CSB-08-

USAF Crew Systems Bulletin Aircrew Accommodation Requirements/Verification

(Copies of these documents are available by contacting Engineering.Standards@us.af.mil;

copies of SBs are available online at https://cs4.eis.afmc.af.mil/sites/1636/ASIP/ASIPDistroA/Forms/AllItems.aspx.)

PROPULSION CENTER OF EXCELLENCE

PCoE BP 99-06 Aircraft Gas Turbine Engine Flight Safety Risk Management Process

(Copies of this document are available online at https://cs.eis.afmc.af.mil/sites/Propulsion/PCOE/default.aspx.)

AFLCMC/ENSM Manufacturing Development Guide

(Copies of the Manufacturing Guide may be obtained by mail ASC/ENSM, 2145 Monahan Way, Bldg 28, Wright-Patterson AFB, OH 45433-7017, Commercial (937) 656-5973, DSN 986-5973;

or may be viewed online at the EN website:

http://www.wpafb.af.mil/shared/media/document/AFD-100630-068.pdf.)

ASC/EN Systems Engineering Guide

(Copies of this document are available by contacting Engineering.Standards@us.af.mil.)

Flying Qualities Development Process (FQDP)

(Copies of this document are available from AFLCMC/EZFT, Mr. William Thomas, Wright- Patterson AFB OH 45433-7101; DSN 785-8579 or at 937-255-8579.)

USAF Weapon Systems Software Management Guidebook

(Copies of the WSSM are available online at https://acc.dau.mil/CommunityBrowser.aspx?id=280695&lang=en-US.)

Unmanned Systems Safety Guide for DOD Acquisition

(Copies of this document are available online at https://acc.dau.mil.)

DEPARTMENT OF TRANSPORTATION – FEDERAL AVIATION ADMINISTRATION (FAA)

FEDERAL AVIATION REGULATIONS (FAR)

Title 14 Aeronautics and Space

Part 23 Airworthiness Standards: Normal, Unility, Acrobatic, and Commuter Category Airplanes

Source: https://assist.dla.mil -- Downloaded: 2014-12-17T14:14Z Check the source to verify that this is the current version before use.

mailto:Engineering.Standards@us.af.mil https://cs4.eis.afmc.af.mil/sites/1636/ASIP/ASIPDistroA/Forms/AllItems.aspx https://cs.eis.afmc.af.mil/sites/Propulsion/PCOE/default.aspx http://www.wpafb.af.mil/shared/media/document/AFD-100630-068.pdf mailto:Engineering.Standards@us.af.mil https://acc.dau.mil/CommunityBrowser.aspx?id=280695&lang=en-US https://acc.dau.mil/

Part 25 Airworthiness Standards: Transport Category Airplanes

Part 27 Airworthiness Standares: Normal Category Rotocraft

Part 29 Airworthiness Standards: Transport Category Rotocraft

Part 33 Airworthiness Standards: Aircraft Engines

Part 35 Airworthiness Standards: Propellers

Part 60 Flight Simulation Training Device Initial and Continuing Qualification and Use

Part 121 Operating Requirements: Domestic, Flag, and Supplemental Operations

Part 133 Rotorcraft External-Load Operations

Title 21 Food and Drugs

Part 1040 Performance Standards for Light-Emitting Products

(Copies of the FARs can be viewed on line at www.ecfr.gov or purchased from the U.S.

Government Online Bookstore at http://bookstore.gpo.gov.)

ADVISORY CIRCULARS (AC)

AC 20-29 Use of Aircraft Fuel Anti-Icing Additives

AC 20-30 Aircraft Position Light and Anticollision Light Installations

AC 20-41 Substitute Technical Standard Order (TSO) Aircraft Equipment

AC 20-42 Hand Fire Extinguishers for Use in Aircraft

AC 20-53 Protection of Aircraft Fuel Systems Against Fuel Vapor Ignition Caused by Lightning

AC 20-60 Accessibility to Excess Emergency Exits

AC 20-115 Airborne Software Assurance

AC 20-119 Fuel Drain Valves AC 20-128 Design Considerations for Minimizing Hazards Caused By

Uncontained Turbine Engine and Auxiliary Power Unit Rotor Failure

AC 20-131 Airworthiness Approval of Traffic Alert and Collision Avoidance Systems (TCAS II) and Associated Mode S Transponders

AC 20-136 Aircraft Electrical and Electronic System Lightning Protection

AC 20-138 Airworthiness Approval of Positioning and Navigation Systems

AC 20-140 Guidelines for Design Approval of Aircraft Data Link Communication Systems Supporting Air Traffic Services (ATS)

AC 20-145 Guidance for Integrated Modular Avionics (IMA) that Implement TSO- C153 Authorized Hardware Elements

AC 20-148 Reusable Software Components

Check the source to verify that this is the current version before use.

http://www.ecfr.gov/ http://bookstore.gpo.gov/

AC 20-152 RTCA, Inc., Document RTCA/DO-254, Design Assurance Guidance for Airborne Electronic Hardware

AC 20-156 Aviation Databus Assurance

AC 20-170 Integrated Modular Avionics Development, Verification, Integration and Approval using RTCA/DO-297 and Technical Standard Order- C153

AC 23-1309-1 System Safety Analysis and Assessment for Part 23 Airplanes

AC 23-1311-1 Installation of Electronic Display in Part 23 Airplanes

AC 25-9 Smoke Detection, Penetration, and Evacuation Tests and Related Flight Manual Emergency Procedures

AC 25-16 Electrical Fault and Fire Prevention and Protection

AC 25-17 Transport Airplane Cabin Interiors Crashworthiness Handbook

AC 25.853-1 Flammability Requirements for Aircraft Seat Cushions

AC 25.869-1 Fire Protection: Systems

AC 25.963-1 Fuel Tank Access Covers

AC 25.981-1 Fuel Tank Ignition Source Prevention Guidelines

AC 25.981-2 Fuel Tank Flammability Reduction Means

AC 25.994-1 Design Considerations to Protect Fuel Systems During a Wheels-Up Landing

AC 25-1309-1 System Design and Analysis

AC 27-1 Certification of Normal Category Rotorcraft

AC 29-2 Certification of Transport Category Rotorcraft

AC 33-1 Turbine Engine Foreign Object Ingestion and Rotor Blade Containment Type Certification Procedures

AC 33-2 General Type Certification Guidelines for Turbine Engines

AC 33-3 Turbine and Compressor Rotors Type Certification Substantiation Procedures

AC 33-4 Design Considerations Concerning the Use of Titanium in Aircraft Turbine Engines

AC 33.4-2 Instructions for Continued Airworthiness: In-Service Inspection of Safety Critical Turbine Engine Parts at Piece-Part Opportunity

AC 33-5 Turbine Engine Rotor Blade Containment/Durability

AC 33.28-1 Compliance Criteria for 14 CFR §33.28, Aircraft Engines, Electrical and Electronic Engine Control Systems

AC 33-76-1 Bird Ingestion Certification Standards

AC 43.13-1 Acceptable Methods, Techniques, and Practices - Aircraft Inspection and Repair

AC 90-96 Approval of U.S. Operators and Aircraft To Operate Under Instrument Flight Rules (IFR) in European Airspace Designated For Basic Area Navigation (B-RNAV)/RNAV 5 and Precision Area Navigation (P-

RNAV)

AC 91-85 Authorization of Aircraft and Operators for Flight in Reduced Vertical Separation Minimum Airspace

AC 120-40 Airplane Simulator Qualification

AC 120-42 Extended Operations (ETOPS and Polar Operations)

AC 120-63 Helicopter Simulator Qualification

FAA TECHNICAL STANDARD ORDERS (TSO)

TSO-C70 Liferafts (Reversible and Nonreversible)

TSO-C77 Gas Turbine Auxiliary Power Units

TSO-C112 Air Traffic Control Radar Beacon System/Mode Select (ATCRBS/MODE S) Airborne Equipment

TSO-C151 Terrain Awareness and Warning System (TAWS)

TSO-C153 Integrated Modular Avionics Hardware Elements

FAA TECHNICAL REPORTS

DOT/FAA/AR-

07/48

Handbook for Real-Time Operating Systems Integration and Component Integration Considerations in Integrated Modular Avionics Systems

DOT/FAA/AR-

99/58

Partitioning in Avionics Architecture: Requirements, Mechanisms, and Assurance

FAA GUIDES

Guide to Reusable Launch and Reentry Vehicle Software and Computing System Safety

(Copies of these documents are available online at https://www.faa.gov/about/office_org/headquarters_offices/ast/regulations/.

FAA CERTIFICATION AUTHORITIES SOFTWARE TEAM (CAST) POSITION PAPERS

CAST-24 Reliance on Development Assurance Alone When Performing a Complex and Full-Time Critical Function

SPECIAL FEDERAL AVIATION REGULATION (SFAR)

SFAR 88 Fuel Tank System Fault Tolerance Evaluation Requirements

(Copies of these documents are available online at www.faa.gov.)

NATIONAL AERONAUTICS AND SPACE ADMINISTRATION (NASA)

NASA-STD-7009 Standard for Models and Simulations

Source: https://assist.dla.mil -- Downloaded: 2014-12-17T14:14Z Check the source to verify that this is the current version before use.

https://www.faa.gov/about/office_org/headquarters_offices/ast/regulations/ http://www.faa.gov/

NASA-STD-

8719.13

Software Safety Standard

NASA-STD-

8739.8

Software Assurance Standard

NASA-GB-

8719.13

NASA Software Safety Guidebook

NASA PROCEDURAL REQUIREMENTS

NASA-NPR

7150.2

NASA Software Engineering Requirements

(Copies of these document are available online at https://standards.nasa.gov..)

2.3 Non-Government publications.

The following documents form a part of this document to the extent specified herein.

AERIAL REFELING SYSTEMS ADVISORY GROUP (ARSAG) INTERNATIONAL

ARSAG 03-00-

03R

Aerial Refueling Pressures: Definitions and Terms, Design and Verification Guidance

(Copies of this document are available online at http://arsaginc.com or from ARSAG International, P.O.