Mil-HDBK-516B_Expanded.pdf

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Combat Rescue Helicopter (CRH) Federal contract opportunity
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Text version

MIL-HDBK-516B Expanded Version 26 Sep 2005 Superceding 20 Apr 2005

ASC/EN

Airworthiness Certification Criteria

Expanded Version of

MIL-HDBK-516B

26 Sep 2005

Kathleen Wilson Document POC:

ASC/ENSI

ASC.EN.516B@wpafb.af.mil

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

(Case 88ABW-2010-6398, 6 December 2010)

MIL-HDBK-516B Expanded – 26 Sep 2005 i

FOREWORD

This document is for the use of Air Force programs to aid in the development of Tailored Airworthiness Certification Criteria (TACC) or Modified Airworthiness Certification Criteria (MACC) documents.

It contains all sections (1 – 20 plus Appendices) from the MIL-HDBK-516B, 26 Sep 2005 publication. The criteria and references (sections 4 through 20) contain the addition of recommended standards and methods of compliance for each of the criterion.

The criteria contained herein are qualitative in nature. More specific guidance and background for specific criteria may be found in the appropriate Joint Service Specification Guides (JSSG) and Title 14, Code of Federal Regulations referenced herein. 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.

This document is forms the basis for the USAF Airworthiness Certification Criteria future update to MIL-HDBK-516B currently in writing, and may be updated as the standards and methods of compliance sections for each criterion are further developed.

Note that in electronic versions, the blue highlighted paragraph headings or text in handbook sections 4 through 19 are internal hyperlinks to bookmarks in the appendix Technical Points of Contact table. Clicking the mouse cursor on the blue jumps you to the referenced location in the table. To return from the Technical Points of Contact table to your jump point in the handbook, use the back arrow key on the menu bar (enable View-Toolbars-Web for the back arrow tool). Gray shaded internal cross-references within the document perform similarly.

Any questions regarding this document may be directed to the POC at the MIL-HDBK-516B mailbox:

ASC.EN.516B@wpafb.af.mil

To use this document:

Criteria are either applicable or nonapplicable. Justification must be provided for nonapplicability.

Standards and methods of compliance may be tailored to the needs of the program for the applicable criterion.

References are for guidance in understanding the criterion and tailoring the standards and methods of compliance.

CONTENTS

Paragraph Page ii

1. SCOPE

1.1 Purpose

1.2 Applicability

1.3 Cross references and technical points of contact

1.4 Information sources

2. APPLICABLE DOCUMENTS

2.1 General

3. DEFINITIONS & 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 manuals/technical orders

4.6 Configuration identification

4.7 Configuration status accounting

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 Stability and control

6.2 Vehicle control functions (VCF)

6.3 Aerodynamics and performance

7. PROPULSION AND PROPULSION INSTALLATIONS

7.1 Propulsion safety management

CONTENTS - Continued Paragraph Page iii

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

8.5 Landing gear and deceleration systems

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

8.7 Aerial refueling system

8.8 Deleted - Propulsion installations moved to section 7.2.5

8.9 Mechanisms

8.10 External cargo hook systems (rotary wing)

8.11 External rescue hoist (rotary wing)

8.12 Fast rope insertion/extraction system (FRIES) (rotary wing)

9. CREW SYSTEMS

9.1 Escape and egress system

9.2 Crew stations and aircraft interiors

9.3 Air vehicle lighting

9.4 Human performance

9.5 Life support systems

9.6 Transparency integration

9.7 Crash survivability

9.8 Air transportability and airdrop

9.9 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 Avionics air vehicle installation

iv

12. ELECTRICAL SYSTEM

12.1 Electric power generation system

12.2 Electrical wiring system, including power distribution

13. ELECTROMAGNETIC ENVIRONMENTAL EFFECTS (E3 337)

13.1 Component/subsystem E3 337 qualification

13.2 System-level E3 338 qualification

14. SYSTEM SAFETY

14.1 System safety program

14.2 Safety design requirements

14.3 Software safety program

15. COMPUTER RESOURCES

15.1 Air vehicle processing architecture

15.2 Functional design integration of processing elements

15.3 Subsystem/processing element

16. MAINTENANCE

16.1 Maintenance manuals/checklists

16.2 Inspection requirements

17. ARMAMENT/STORES INTEGRATION

17.1 Gun/rocket integration and interface

17.2 Stores integration

17.3 Laser integration and interface

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 Nondestructive inspection

19.4 Wear and erosion

20. OTHER CONSIDERATIONS

v

20.1 Mission/test equipment and cargo/payload safety

21. NOTES

21.1 Changes from previous issue

21.2 Subject term (key word) list

A.1. SCOPE

A.2. TECHNICAL POINTS OF CONTACT

A.3. CROSS-REFERENCE TABLE OF MAJOR SECTION CHANGES

FROM MIL-HDBK-516A TO MIL-HDBK-516B

AIRWORTHINESS

CERTIFICATION CRITERIA

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

1. SCOPE

1.1 Purpose.

This document establishes the airworthiness certification criteria to be used in the determination of airworthiness of all manned and unmanned, fixed and rotary wing air vehicle systems. It is a foundational document to be used by the system program manager, chief engineer, and contractors to define their air system’s airworthiness certification basis.

This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.

1.2 Applicability.

These criteria should be tailored and applied at any point throughout the life of an air vehicle system when an airworthiness determination is necessary, especially whenever there is a change to the functional or product baseline.

Rotary wing air vehicle and unmanned aerial vehicle/remotely operated aircraft (UAV/ROA) features demand unique safety-of-flight (SOF) system 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. The UAV/ROA operating system can be built into the vehicle or be part of the control station for remotely operated aircraft. The UAV/ROA system comprises the control station, data links, flight control system, communications systems/links, etc., as well as the air vehicle. UAV/ROAs vary greatly in size, weight, and complexity.

Because they are unmanned, 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. As such, the airworthiness criteria may be tailored for this unique application, including when a UAV/ROA is designed to be “expendable” or where the UAV/ROA will conduct missions with “minimum life expectancy.”

Consideration should be given to the environment in which the UAV/ROA will be operated (controlled test range, national airspace, fleet usage, including ship based applications), to the airframe life for which the air vehicle is designed, and to the “expendability” of the UAV/ROA in close proximity to the control system, personnel, property, or other equipment.

Similarly, air vehicles intended for use aboard ship 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. 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 contact the FAA Military Certification Office (MCO) in Wichita, KS at the earliest opportunity.

Agreements for reimbursement for military service work performed by the FAA are in place, and in many cases MCO assistance on these alterations may be accomplished without additional cost.

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.

1.2.1 Tailoring to create the certification basis

Not all of the airworthiness criteria apply to every type of air vehicle; 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 either applicable or nonapplicable, considering system or product complexity, type, data, and intended use. Document the rationale for identifying any criteria as nonapplicable.

b. Applicable criteria may not be deleted or modified in any manner. However, if a portion of otherwise applicable criteria does not apply, identify the applicable and nonapplicable portions, and document the rationale.

c. Supplement applicable criteria with specific measurable parameters, where appropriate (i.e., they add value to the definition of airworthiness requirements).

d. Develop additional criteria, as appropriate, for any capabilities or systems not fully addressed by the criteria contained in this handbook.

1.3 Cross references and technical points of contact.

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 assistance in interpreting or applying the criteria, call the appropriate section technical point of contact, or the FAA MCO, provided at appendix A.2.

1.4 Information sources.

Each section in the Airworthiness Certification Criteria is matched with corresponding Title 14, Code of Federal Regulations reference (14CFR reference) and Joint Service Specification Guides (JSSG). In addition, the complete listing of 14CFR reference advisory circulars was consulted for appropriate guidance in airworthiness certification.

The FAA Title 14 Code of Federal Regulations Part (i.e., 23, 25, 27, 29) referenced is dependant on airplane type, and must be consistent with airplane size and usage. The list shown is not all inclusive, and the user is cautioned to only look at the reference material 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 necessary to understand the information provided by this handbook. Refer to the current version of these documents, unless otherwise indicated.

2.1.1 Government specifications, standards, and handbooks.

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

Joint Service Specification Guides (JSSG):

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

Click the link below to view the unlimited distribution JSSGs

(http://engineering.wpafb.af.mil/corpusa/specification/jssg)

Military Specifications:

MIL-PRF-5041 Tires, Ribbed Tread, Pneumatic, Aircraft, General Specification for

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-E-7016 Electric Load and Power Source Capacity, Aircraft, Analysis of

MIL-DTL-7700 Flight Manuals, Air Refueling Procedures, and Abbreviated Checklists

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

MIL-B-8584 Brake Systems, Wheel, Aircraft, Design of

MIL-A-8591 Airborne Stores, Suspension Equipment and Aircraft-Store Interface (Carriage Phase); General Design Criteria for

MIL-F-8615 Fuel System Components, General Specification for

MIL-S-8812 Steering System, Aircraft General Requirements for

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MIL-A-18717 Arresting Hook Installation, Aircraft

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

MIL-G-21480 Generator System, 400 Hz Alternating Current, Aircraft, General Specification for

MIL-DTL-25959 Tie Down, Cargo, Aircraft

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

AFGS-87139 Landing Gear Systems

AFGS-87219 Electrical Power Systems, Aircraft

AFGS-87256 Integrated Diagnostics

MIL-F-38363 Fuel System, Aircraft, (for future procurement, see MIL-F-87154) (for future procurement, use AFGS-87154 Fuel Systems General Design Specifications for [inactive but soon to be reactivated])

MIL-A-87166 Aerial Refueling Receiver Subsystem

DEPARTMENT OF DEFENSE STANDARDS

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

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

MIL-STD-188-243 Interoperability and Performance Standards for Tactical Single Channel Ultra High Frequency (UHV) for Radio Communications

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 & Provisions for Military Aircraft, Design Requirements for

MIL-STD-810 Environmental Engineering Considerations and Laboratory Tests

MIL-STD-882 System Safety, Standard Practice for

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

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

MIL-STD-1310 Shipboard Bonding, Grounding, and Other Techniques for Electromagnetic Compatibility and Safety

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MIL-STD-1472 Human Engineering

MIL-STD-1474 Noise Limits

MIL-STD-1530 Aircraft Structural Integrity Program

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-1797 Flying Qualities of Piloted Aircraft

MIL-STD-2169 High-Altitude Electromagnetic Pulse (HEMP) Environment (u) classified SECRET

MIL-STD-3005 Analog-to-Digital Conversion of Voice by 2,400 bit/second Mixed Excitation Linear Prediction (MELP)

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-7080 Selection and Installation of Aircraft Electric Equipment

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

DEPARTMENT OF DEFENSE HANDBOOKS

MIL-HDBK-61 Configuration Management Guidance

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 Electric Shipboard Cable

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

MIL-HDBK-419 Grounding, Bonding, and Shielding for Electronic Equipments and Facilities, Volume 1 & 2

MIL-HDBK-454 General Guidelines for Electronic Equipment

MIL-HDBK-514 Operational Safety, Suitability, and Effectiveness for the Aeronautical Enterprise

MIL-HDBK-515 Weapon System Integrity Guide http://www.assistdocs.com/search/document_details.cfm?ident_number=36826&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D1399%2D390&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=36858&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D1425&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=36903&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D1472&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=36905&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D1474&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=36952&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D1530&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=37091&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D1683&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=37120&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D1760&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=37143&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D1787&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=70037&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D1797&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=208937&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D3005&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=209352&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D3009&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=212831&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D3013&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=113799&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D7080&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=204149&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D27733&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=116799&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DSTD%2D38784&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=202239&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DHDBK%2D61&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=53942&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DHDBK%2D221&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=53945&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DHDBK%2D224&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=68094&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DHDBK%2D299&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=202658&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DHDBK%2D310&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=54042&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DHDBK%2D419&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=115984&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DHDBK%2D454&search%5Fmethod=BASIC� hhttp://www.assistdocs.com/search/document_details.cfm?ident_number=213028&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DHDBK%2D514&search%5Fmethod=BASIC� http://www.assistdocs.com/search/document_details.cfm?ident_number=212249&StartRow=1&PaginatorPageNumber=1&doc%5Fid=MIL%2DHDBK%2D515&search%5Fmethod=BASIC�

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

MIL-HDBK-828 Laser Safety on Ranges and in Other Outdoor Areas

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

MIL-HDBK-1587 Materials and Process Requirements for Air Force Weapon Systems

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-1791 Designing for Internal Aerial Delivery in Fixed Wing Aircraft

MIL-HDBK-1798 Mechanical Equipment and Subsystems Integrity Program

MIL-HDBK-2165 Testability Program for Systems and Equipments

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

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

MIL-HDBK-46855 Human Engineering Program Process and Procedures

MIL-HDBK-87213 Electronically/Optically Generated Airborne Displays

MIL-HDBK-87244 Avionics/Electronics Integrity

(Copies of these documents are available from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094 or http://dodssp.daps.dla.mil. or http://assist.daps.dla.mil/quicksearch/. Copies of documents indicating a distribution limitation (for example, statement D) may be ordered from ASC/ENOI, 2530 Loop Rd West, Bldg. 560, Wright-Patterson AFB, OH 45433-7101 or online at https://www.en.wpafb.af.mil/engstds/engstds.asp).

2.1.2 Other Government publications.

The following other Government publications form a part of this document to the extent specified herein.

AIR FORCE INSTRUCTIONS

AFI 11-202 General Flight Rules (Volume 3)

AFI 11-2C-130 C-130 Operating Procedures

AFI 21-101 Aerospace Equipment Maintenance Management

AFI 63-14 Aircraft Information Programs

AFI 63-501 Air Force Acquisition Quality Program

AFI 63-1201 Assurance of Operational Safety, Suitability, and Effectiveness

(OSS&E)

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AFI 63-1301 Assurance of Communications Navigation Surveillance/Air Traffic Management Performance

AIR FORCE POLICY DIRECTIVES

AFPD 62-4 Standards of Airworthiness for Passenger Carrying Commercial

Derivative Transport Aircraft

AFPD 62-5 Standards of Airworthiness for Commercial Derivative Hybrid Aircraft

AFPD 62-6 USAF Aircraft Airworthiness Certification

AFPD 63-12 Assurance of Operational Safety, Suitability, and Effectiveness

(OSS&E)

AFPD 63-13 Communications Navigation Surveillance/Air Traffic Management and Navigation Safety Performance for USAF Aircraft

(Copies of Air Force Policy Directives and Instructions can be viewed online at the AFDPO web site at http://afpubs.hq.af.mil.

AFOSH 48-139 Laser Radiation Protection Program

AIR FORCE OCCUPATIONAL SAFETY AND HEALTH

T.O. 00-5-1 AF Technical Order System

AIR FORCE TECHNICAL ORDER

T.O. 31Z-10-0 Electromagnetic Radiation Hazard (Copies of Air Force technical orders may be obtained via https://www.toindex-s.wpafb.af.mil/.)

ASC/EN Manufacturing Development Guide

AERONAUTICAL SYSTEMS CENTER ENGINEERING GUIDE

(Copies of this ASC/EN Guide may be obtained by mail ASC/ENSM, 2530 Loop Rd W., Wright- Patterson AFB, OH 45433-7101, Commercial (937) 255-1656, DSN 785-1656; or may be viewed online at the EN website: https://www.en.wpafb.af.mil/mdg/mdg.pdf.)

ARMY AERONAUTICAL DESIGN STANDARDS

ADS-10C-SP Air Vehicle Technical Description

ADS-13F-HDBK Air Vehicle Materials and Processes

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

ADS-29 Structural Design Criteria for Rotary Wing Aircraft

ADS-33E-PRF Performance Specification Handling Qualities Requirements for Military Rotorcraft

ADS-36 Rotary Wing Aircraft Crash Resistance

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

ADS-40A-SP Air Vehicle Flight Performance Description

ADS-43A-HDBK Qualification Requirement and Identification of Critical Characteristics for Aircraft and Engine Components http://www.e-publishing.af.mil/pubfiles/af/63/afi63-1301/afi63-1301.pdf� http://www.e-publishing.af.mil/pubfiles/af/62/afpd62-4/afpd62-4.pdf� http://www.e-publishing.af.mil/pubfiles/af/62/afpd62-5/afpd62-5.pdf� http://www.e-publishing.af.mil/pubfiles/af/62/afpd62-6/afpd62-6.pdf� http://www.e-publishing.af.mil/pubfiles/af/63/afpd63-12/afpd63-12.pdf� http://www.e-publishing.af.mil/pubfiles/af/63/afpd63-13/afpd63-13.pdf� http://afpubs.hq.af.mil/� https://www.toindex-s.wpafb.af.mil/� https://www.en.wpafb.af.mil/mdg/mdg.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ADS10CSP.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ADS13FHDBK.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ads33front.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ADS37APRF.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ADS40ASPR.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ADS43AHDBK.pdf�

ADS-44-HDBK Aeronautical Design Standard Handbook Armament Airworthiness Qualification

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

ADS-51-HDBK Rotorcraft and Aircraft Qualification (RAQ) Handbook (http://www.redstone.army.mil/aed/eng/raqh/raqh.html)

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-65-HDBK Airworthiness Qualification and Verification Requirements for Electro- Optics and Infrared Sensor Systems

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

(Copies of Army Aeronautical Design Standards may be obtained via http://www.redstone.army.mil/amrdec/sepd/tdmd/StandardAero.htm)

ARMY REGULATIONS

AR 11-9 The Army Radiation Safety Program

(Copies of Army Regulations may be obtained via http://www.army.mil/usapa/epubs/11_series_collection_1.html.

ARMY TECHNICAL BULLETINS (TB)

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

Radiation and Ultrasound

(Official Department of Army (DA) administrative publications and forms are managed by the Army Publishing Directorate (APD) under the direction of the Administrative Assistant to the Secretary of the Army (AASA). APD uses the latest publishing technologies to produce high-quality, enhanced, electronic publications and forms. This is the Army's latest collection of electronic DA administrative publications and DA forms. Copies of Army Technical Bulletins may be obtained via http://www.army.mil/usapa/med/index.html)

AR-56 Structural Design Requirements (Helicopters)

NAVY AERONAUTICAL REQUIREMENTS

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.)

NAVAIRINST 4200.25D Management of Critical Application Items including Critical Safety Items.

NAVAL AIR SYSTEMS COMMAND INSTRUCTIONS

http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ADS50R5.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ADS51HDBK.pdf� http://www.redstone.army.mil/aed/eng/raqh/raqh.html� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ads-62-sp.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ads-63-sp_final.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ads-65HDBK.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/Documents/ADS-66-HDBK.pdf� http://www.redstone.army.mil/amrdec/sepd/tdmd/StandardAero.htm� http://www.army.mil/usapa/epubs/pdf/r11_9.pdf� http://www.army.mil/usapa/epubs/11_series_collection_1.html� http://www.army.mil/usapa/med/DR_pubs/dr_a/pdf/tbmed523.pdf� http://www.apd.army.mil/� http://www.army.mil/usapa/med/index.html�

NAVAIRINST 13034.1C Flight Clearance Policy for Air Vehicles and Aircraft Systems

NAVAIR 00-80T-110 NATOPS Air Refueling Manual (USN/USMC)

(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 via http://airworthiness.navair.navy.mil/.)

NAV SEA OP 3565 Electromagnetic Radiation Hazard

NAVAL SEA SYSTEMS COMMAND INSTRUCTIONS

NAV SEA TM-59310-AQ-SAF-010 Technical Manual for Batteries, Navy Lithium Safety Program, Air Vehicle Subsystems

NAV SEA TM-59310-AQ-SAF-010 Technical Manual for Batteries, Navy Lithium Safety Program, Air Vehicle Subsystems

(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. Additional information is available online through the NAV SEA specs and standards website: http://www.navsea.navy.mil/specsAndstandards/. Copies of NAVSEA technical manuals can be ordered from the Naval Inventory Control Point (NAVICP), Mechanicsburg, PA.

They can be ordered using 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.)

Joint Software System Safety Committee, Software System Safety Handbook: A Technical & Managerial Team Approach, Dec 1999. (For copies, call (301) 342-2350.)

JOINT SERVICE DOCUMENTS

Range Commander’s Council (RCC) 316-98, Laser Range Safety

(Copies of DoD instructions and documents may be obtained via Secretariat, Range Commanders Council, ATTN CSTE-DTC-WS-RCC, Building 100 Room 138, White Sands Missile Range NM 88002-5110, Commercial (505) 678-1107/1108, DSN 258-1107. The Secretariat may be contacted via email: Secretariat (rcc@wsmr.army.mil, or online:

http://jcs.mil/RCC/

DoDD 3150.2 DoD Nuclear Weapon System Safety Program Manual

DEPARTMENT OF DEFENSE DOCUMENTS

DoDD 4650.1 Management and Use of Radio Frequency Spectrum

DoD 6055.9-STD DoD Ammunition and Explosives Safety Standards

DD Form 1494 Application for Equipment Frequency Allocation

DEPARTMENT OF DEFENSE FORMS

DoDI 5000.2 Operation of the Defense Acquisition System

DEPARTMENT OF DEFENSE INSTRUCTIONS

DoDI 6055.11 Protection of DoD Personnel from Exposure to Radiofrequency Radiation and Military Exempt Lasers http://airworthiness.navair.navy.mil/reference_library/documents/NAVAIRINST%2013034.1C.pdf� http://airworthiness.navair.navy.mil/� http://www.navsea.navy.mil/specsAndstandards/� http://www.nll.navsup.navy.mil/� mailto:rcc@wsmr.army.mil� mailto:rcc@wsmr.army.mil� http://jcs.mil/RCC/�

T. O. 11A-1-47 DoD Ammunition and Explosives Hazard Classifications

DEPARTMENT OF DEFENSE TECHNICAL ORDER

ATP-56 Air To Air Refueling, NORTH ATLANTIC TREATY ORGANIZATION (NATO)

STANAG 3098 Aircraft Jacking

STANAG 3278 Aircraft Towing Attachments and Devices

STANAG 3447 Aerial Refueling Equipment Dimensional and Functional Characteristics

STANAG 4101 Towing Attachments

(Copies of NATO STANAGs may be obtained via SAF/AQRE, 1060 Air Force Pentagon, Washington D. C., DSN 223-3221.

TITLE 14 Aeronautics and Space

FEDERAL AVIATION ADMINISTRATION CODE OF FEDERAL REGULATIONS (CFR)

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

Part 25, Airworthiness Standards, Transport Category: Airplanes

Part 27, Airworthiness Standards, Normal Category Rotorcraft

Part 29, Airworthiness Standards, Transport Category: Rotorcraft

Part 33, Airworthiness Standards, Aircraft Engines

Part 133, Rotorcraft External-Load Operation

SFAR 88, Special Federal Aviation Regulation, Fuel Tank System Fault Tolerance Evaluation Requirements

TITLE 21 Food and Drugs, Part 1040, Subchapter J - Radiological Health, Performance Standards for Light-Emitting Products

FEDERAL AVIATION ADMINISTRATION ADVISORY CIRCULARS (AC)

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

AC 20-30 Aircraft Position Light and Anti-Collision 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 Due to Lightning

AC 20-60 Accessibility to Excess Emergency Exits

AC 20-115 Radio Technical Commission for Aeronautic, Inc. Document

RTCA/DO-178B

AC 20-119 Fuel Drain Valves

AC 20-129 Airworthiness Approval of Vertical Navigation (VNSV) Systems for use in the U.S. National Airspace System (NAS) and Alaska http://ecfr.gpoaccess.gov/cgi/t/text/text-idx?c=ecfr&sid=52ec69e506164f6e5523096e76aea276&tpl=/ecfrbrowse/Title14/14cfr23_main_02.tpl� http://ecfr.gpoaccess.gov/cgi/t/text/text-idx?c=ecfr&sid=52ec69e506164f6e5523096e76aea276&tpl=/ecfrbrowse/Title14/14cfr25_main_02.tpl� http://ecfr.gpoaccess.gov/cgi/t/text/text-idx?c=ecfr&sid=52ec69e506164f6e5523096e76aea276&tpl=/ecfrbrowse/Title14/14cfr27_main_02.tpl� http://ecfr.gpoaccess.gov/cgi/t/text/text-idx?c=ecfr&sid=52ec69e506164f6e5523096e76aea276&tpl=/ecfrbrowse/Title14/14cfr29_main_02.tpl� http://ecfr.gpoaccess.gov/cgi/t/text/text-idx?c=ecfr&sid=52ec69e506164f6e5523096e76aea276&tpl=/ecfrbrowse/Title14/14cfr33_main_02.tpl� http://ecfr.gpoaccess.gov/cgi/t/text/text-idx?c=ecfr&sid=4ef43d75b77865305af255bc30c4cf11&tpl=/ecfrbrowse/Title14/14cfr133_main_02.tpl� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgFAR.nsf/CurrentSFARPart/EEFB3F94451DC06286256C93004F5E07?OpenDocument� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/31CB1A4B2CFC33FB862569A5006217E2?OpenDocument� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/94D4758B3F48035186256BF40064457D?OpenDocument� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/CEBA7446F88ECFA1862569C3004BA827?OpenDocument� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/CF2F4F1406354490862569AD00777471?OpenDocument� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/C5ADB0DB1C12BE8D862569AE006D2F17?OpenDocument� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/AB1A49F0F72C9605862569AE006D3BBA?OpenDocument� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/DCDB1D2031B19791862569AE007833E7?OpenDocument� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/FC8BD2EC0D5C0BE886256BF40064431A?OpenDocument� http://www.airweb.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/44D02208237AF050862569AF006AB0EA?OpenDocument�

AC 20-130 Airworthiness Approval of Navigation or Flight Management Systems Integrating Multiple Navigation Sensors

AC 20-136 Protection of Aircraft Electrical/Electronic Systems against the Indirect Effects of Lightning

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

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 [Large AC] Transport Airplane Cabin Interiors Crashworthiness Handbook

AC 25.853-1 Flammability Requirements for Aircraft Seat Cushions

AC 25.869-1 Electrical System Fire and Smoke Protection

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 Minimization

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

AC 27-1 [Large AC] Certification of Normal Category Rotorcraft

AC 29-2 [Large AC] Certification of Transport Category Rotorcraft

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

AC 33-2 Aircraft Engine Type Certification Handbook

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 33-5 Turbine Engine Rotor Blade Containment/Durability

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

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

AC 43.13-1 [Large AC. This includes Change 1.] Acceptable Methods, Techniques, and Practices- Aircraft Inspection

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) and Precision Area Navigation (P-RNAV), AC 90-97 Use of Barometric Vertical Navigation (VNAV) for Instrument Approach Operations Using Decision Altitude

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