SAE INTERNATIONAL

SAE INTERNATIONAL AEROSPACE

STANDARDS

HAI AIRWORTHINESS, CBM AND HUMS

SPECIALISTS' MEETING

9th February, 2015, Huntsville, AL, USA

Dr. Richard Greaves FSAE

2015 SAE President

SAE INTERNATIONAL

AGENDA 1. ABOUT SAE INTERNATIONAL

2. SAE AEROSPACE STANDARDS PROGRAM

& STRUCTURE

3. SAE STANDARDS SUPPORTING

REGULATION

4. SAE STANDARDS FOR HUMS, IVHM AND

CBM

SAE INTERNATIONAL

Mission StatementSAE International is a global

body of scientists, engineers, and practitioners

that advances self-propelled vehicle and system

knowledge in a neutral forum for the benefit of

society.

VisionSAE International is the leader in

connecting and educating engineers while

promoting, developing and advancing aerospace,

commercial vehicle and automotive engineering.

SAE INTERNATIONAL

• Maintains more than 11,000 ground vehicle, aerospace and aerospace

material specifications standards. All standards are industry consensus

standards with the participation of all stakeholders

• Offers more than 200 professional development classroom courses and

90 e-learning products

• Publishes or co-publishes hundreds of technical and historical books, CD-

ROMs and Web-based products

SAE INTERNATIONAL

Aerospace Automotive Commercial

Vehicles

SAE International is a global association committed to being the ultimate knowledge source for the engineering profession. By uniting over 148,000 engineers and technical experts, we drive knowledge and expertise across a broad spectrum of industries. We act on two priorities: encouraging a lifetime of learning for mobility engineering professionals and setting the standards for industry engineering. We strive for a better world through the work of our philanthropic SAE Foundation, including programs like A World in Motion® and the Collegiate Design Series™.

SAE INTERNATIONAL

World Headquarters – Warrendale PA, USA Automotive Headquarters – Troy MI, USA Aerospace Standards – Washington DC Aerospace Standards Europe – London SAE China - Shanghai

SAE INTERNATIONAL

SAE AEROSPACE STANDARDS HISTORY – FROM 1916

“The work covered by the SAE is of such

value that everybody identified with the

industry should take out membership.”

Orville Wright, 1918

The Wright Brothers

SAE INTERNATIONAL 8

SAE MEMBERS: AVIATION PIONEERS

Orville Wright Glenn Curtiss Glenn Martin Elmer Sperry Chance Vought

Jimmy Doolittle Charles Lindbergh Amelia Earhart Kelly Johnson Igor Sikorsky

SAE INTERNATIONAL 9

SAE AEROSPACE STANDARDS HISTORY – FROM 1916

SAE INTERNATIONAL

GOVERNMENT, MILITARY, RESEARCH AND ASSOCIATIONS RELY ON

SAE STANDARDS

Regulatory Bodies Associations

Research Organisations

Military Agencies

SAE INTERNATIONAL

• SAE International attendance at HeliExpo 2014, 2015

• HAI expertise and participation in SAE Technical Standards Committees:

• G-10EVS Human Factors for Enhanced & Synthetic Vision Systems

• HM-1 for IVHM & HUMS

• Opportunities for greater partnership to serve the global rotorcraft community

11

SAE AND HAI

SAE INTERNATIONAL 12

SAE STANDARDS PORTFOLIO

Active

Aerospace: 8,279

Ground Vehicle: 2,215

TOTAL: 10,494

Historical

Aerospace: 17,532

Ground Vehicle: 2,669

TOTAL: 20,201

30,695 Standards in Circulation

SAE INTERNATIONAL

SAE ORGANIZATIONAL STRUCTURE

13

Technical

Standards

Board

SAE Board of Directors

Engineering

Meetings

Board

Sections

Board

Aerospace

Council

Engineering

Education

Board

Foundation

Board of

Trustees

Membership

Services

Board

Publications

Board

Staff

Performance

Review

Institute

SAE INTERNATIONAL

TYPES OF SAE STANDARDS

AS Aerospace Standards – specific performance requirements used for design

standards, parts standards, minimum performance standards, quality and other areas

conforming to broadly accepted engineering practices or specs for a material, product,

process, procedure or test method

AMS Aerospace Material Specifications – specific performance requirements for

material and process specifications

ARP Aerospace Recommended Practices – documentations of practice, procedures,

and technology that are intended as guides to standard engineering practices. May be

of a more general nature or propound data that have not yet gained broad acceptance.

AIR Aerospace Information Reports – compilations of engineering reference

data, historical information, or educational material useful to the technical

community

SAE INTERNATIONAL

Industry technical standards play a very important role in aviation regulation

The regulatory agencies use technical standards such as SAE standards as a basis

or a support for:

• Federal Aviation Regulation (FAR) / Certification Specifications (CS),

• Technical Standards Orders (TSO) / European Technical Standards Orders (ETSO)

• Advisory Circulars (AC) / Acceptable Means of Compliance (AMC)

In this way, the industry is a partner of the regulator – through standardisation

The trend is for increasing reliance on industry standards to support, and even

play a leading role in regulatory work

STANDARDS AND REGULATIONS – KEY PRINCIPLES

SAE INTERNATIONAL 16

INDUSTRY STANDARDS IN REGULATION

ARINC, 32

ASTM*, 101

CMH-17, 1

EN, 0 EUROCAE, 45

RTCA, 192

IEC, 36

ICAO, 53

ISO, 17

NAS, 12

Military Specifications, 336

SAE, 306

Amount of Unique Industry Standards Referenced in FAA TSOs, ACs†, FAA-STDs and FARs

Total: 1131 †Airport Design Excluded

SAE INTERNATIONAL

AC 27-1B Certification of Normal Category Rotorcraft & AC 29-2C Certification of Transport Rotorcraft (Changes 1 – 4 incorporated) SAE Document Title SAE Committee

J211 Instrumentation for Impact Tests Safety Test Instrumentation Standards

J202 Synthetic Skins for Automotive Testing

ARP5412 Aircraft Lightning Environment and Related Test Waveforms AE-2, Lightning ARP5414 Aircraft Lightning Zoning AE-2, Lightning

ARP5416 Aircraft Lightning Test Methods AE-2, Lightning ARP5672 Aircraft Precipitation Static Certification AE-2, Lightning AS143B Heaters, Aircraft, Internal Combustion Heat Exchanger Type AC-9 Aircraft Environmental Systems AIR4003 Report on Aircraft Engine Containment – 1976-1983 (AC 29-2C only) Engine Containment Ad Hoc Committee

AIR4770 Report on Aircraft Engine Containment – 1984-1989 (AC 29-2C only) Engine Containment Ad Hoc Committee

ARP1401 Aircraft Fuel System and Component Icing Test AE-5 Aerospace Fuel, Oil And Oxidizer Systems

ARP926A Fault/Failure Analysis Procedure (AC 27-1B only) S-18, Aircraft And Sys Dev And Safety Assessment

ARP492 Aircraft Engine Fuel Pump Cavitation Endurance Test (AC 27-1B only) AE-5B Engine Related Components & Airframe

Mounted Pumps AS8034 Minimum Performance Standard for Airborne Multipurpose A-4ED Electronics Display ARP4754A Guidelines for Development of Civil Aircraft and Systems S-18, Aircraft And Sys Dev And Safety Assessment ARP4761 Guidelines and Methods for Conducting the Safety Assessment Process on Civil

Airborne Systems and Equipment S-18, Aircraft And Sys Dev And Safety Assessment

SAE AE4L Report

AE4L-81-2

Test Waveforms and Techniques for Assessing the Effects of Lightning-Induced

Transients

AE-4, Electromagnetic Environmental Effects

SAE 100R14A SAE Specifications for stainless braided hoses

ARP1217 Instrumentation Requirements for Turboshaft Engine Performance Measurements S-12 Helicopter Powerplant

ARP1702 Defining and Measuring Factors Affecting Helicopter Turbine Engine Power Available S-12 Helicopter Powerplant 17

SAE STANDARDS REFERENCED IN FAA ROTORCRAFT ADVISORY

CIRCULARS

SAE INTERNATIONAL

REGULATIONS AND GOVERNMENT DOCUMENTS REFERENCE SAE

STANDARDS TO CERTIFY AIRCRAFT BEFORE ENTERING THE MARKET

Example FAA TSO

Mandatory compliance

Example FAA AC

Guidance material

Example EASA ETSO

Mandatory compliance

Example EASA AMC

Guidance material

Example ICAO Annex

Mandatory compliance

18

New/

updated regulation

Need for standard

Tasking letter

Standard Writing:

Industry+ Regulator

Publication and

reference

SAE has received

14 standards

tasking requests

since 2008

Authority SAE Committee Subject Status

FAA A-4, Aircraft Instruments AS8045A, Minimum Performance Standard for Underwater Locating Devices

(Acoustic) (Self-Powered)

Published August 2011

FAA A-4, Aircraft Instruments AS6254, Minimum Performance Standard for Low Frequency Underwater

Locating Devices (Acoustic) (Self-Powered)

Published February 2012

FAA G-20, Airport Lighting Adverse Impact to EFVS Operations due to transitioning airport lighting

systems to LED

In process; hybrid light bulb

undergoing testing

FAA A-10, Aircraft Oxygen Equipment AS8059, Carry-On Portable Oxygen Concentrators Published June 2012

EASA S-9, Cabin Safety Provisions AS6271, Halocarbon Clean Agent Hand-Held Fire Extinguisher Published January 2013

EASA S-9, Cabin Safety Provisions AS6272, Automatic Fire Extinguisher for Trash Receptacles In process

FAA AGE-2A, Cargo Handling AS6163, Active Temperature Controlled Shipping Container – Performance

Requirements and Test Parameter

In process

FAA A-4, Aircraft Instruments AS8036A, Cargo Compartment Fire Detection Instruments Published December 2013

FAA A-4, Aircraft Instruments AS8006A, Minimum Performance Standard for Pitot and Pitot-Static Tubes Complete

FAA AGE-2A, Cargo Handling AS3610x, Pallet Net Test Method Standard In process

FAA A-4, Aircraft Instruments AS6296, Minimum Performance Standard for Electronic Flight Instrument

System (EFIS) Displays

In process

FAA A-4, Aircraft Instruments

G-10, Behavioral Engineering

Technology

ARP60494, Touch Interactive Display Systems: Human Factors Considerations,

System Design and Performance Guidelines

In process

FAA G-18, RFID Minimum Performance Standards for Active Radio Frequency Identification

Tags and Sensors

Request received October

2014

FAA New Committee Minimum Performance Standard for Helicopter

Hoists

TC in formation

SAE INTERNATIONAL

KEY SAE STANDARDS ACTIVITIES OF INTEREST TO ROTORCRAFT

19

Composite

Materials

Touch

Screens

Environmental

Standards

Lightning

Protection

EFIS

Integrated Vehicle

Health Management

& HUMS

Counterfeit Parts

Avoidance

Rotorcraft Inlet

Icing

Additive

Manufacturing

SAE INTERNATIONAL 20

INTEGRATED VEHICLE HEALTH MANAGEMENT

Integrated Vehicle Health Management is an end

to end capability that transforms system data into

operational support information enabling:

Optimized maintenance actions

Improved readiness and availability

Enhanced Vehicle safety and reliability

Product life extension

Product improvement and new design paradigms

Airlines and operators see the major time, resource and economic benefits

of aircraft availability and optimised maintenance

SAE INTERNATIONAL 21

Scope:

The scope of this document is to clearly lay out the path for an organization to implement a CBM

approach to maintenance. The practices will include both CBM in design and in the support phase

for fielded equipment.

ARP6204 CONDITION BASED MAINTENANCE (CBM) RECOMMENDED PRACTICE

1. Define glossary of terms

2. Definition and Scope of CBM

3. Potential elements of CBM

4. RCM as the method used to determine CBM

requirements

5. Steps to implement CBM => define process

6. Relationship of CBM to other supportability

and product support processes

7. Design considerations in new programs

8. Design considerations for legacy

systems

9. Supportability considerations for

implemented CBM infrastructure

10. Expected benefits, outcomes and

metrics of a properly implemented CBM

solution

11. Example of successful implementation

of CBM

Current Layout:

SAE G-11 M (Maintainability) Committee

SAE INTERNATIONAL 22

SAE HM-1, G-11SHM COMMITTEE COMPOSITION – ROTORCRAFT RELATED

Acellent

Epsilon Inc

Metis Design

PREDICT

Global Strategic

Solutions

Impact Technologies

Astronics

Howell Instrument

Humaware

Critical Software

NRG Systems

OSYS

Ridgetop

EASA ICAO

FAA TCCA

ANAC

DND (Canada)

DSO (Aus.)

MoD/MAA (UK)

NAVAIR (US)

US Army

US Air Force

Crane Aerospace

UTAS

Meggitt

Messier Bugatti-Dowty

ADSE

Hess PHM Group

PHM Technology

Pty Ltd

Treble-One LLC

NVH

PHI

Airbus Helicopters

Boeing Rotorcraft

Systems

Bell Helicopter

Sikorsky

GE Aviation

Pratt & Whitney

Rolls-Royce

Honeywell

CAPE

CIRA

Cranfield University

DSTO

Fraunhofer Institute

IABG

NLR

DLR

NASA

National Research

Council National

Aerospace

Laboratories

Sandia National

Laboratories

Stanford University

TU Delft

University of Bristol

University of Tokyo

SAE INTERNATIONAL

DOCUMENT SCOPE

* Provide guidance on the implementation of

SHM in aircraft applications to assist

developers in specifying the measurements,

accuracy, reliability and other requirements

of the system to be designed.

* Provide information on structural

maintenance practices and provide

guidance on how SHM can be incorporated

within or as modifications to current

maintenance and airworthiness

documents.

* Standardize and harmonize worldwide

understanding about SHM (including

terminology).

* Provide basic requirements to guide SHM

technology development.

* Review certification matters that are

relevant to SHM.

ARP6461, Guidelines for

Implementation of Structural Health

Monitoring on Fixed Wing Aircraft

Next Phase:

SAE G-11SHM Rotorcraft Task Group

Develop SHM Guidelines for Rotorcraft

…in progress…

SAE INTERNATIONAL

HM-1 IVHM Technical Committee

BUSINESS INFRASTRUCTURE TECHNOLOGIES APPLICATION

ARP6290 Architecture of an IVHM

System

ARP6407 Guidelines for the Design of

an IVHM System

AIR6212 Volcanic Ash ARP6275 Cost Benefit Analysis of

IVHM Systems

ARPXXXX Guidelines for Certification

of IVHM Systems

SAE IVHM Steering Group Oversight

IVHM Cornerstone Document ARP6803

ARP6887 Verification & Validation of

IVHM Systems and Software

ARPXXXX Guidelines For IVHM System

Software And Airborne Electronic Hardware

Assurance Levels

ARP6883 Requirements of an IVHM

System

AS5391 HUMS Accelerometer

Interface

AS5392 HUMS Rotational System

Indexing Sensor

AS5393 HUMS Blade Tracker

Interface

AS5394 HUMS Advanced Multipoint

Interface

AS5395 HUMS Data Interchange

SAE IVHM STANDARDS LANDSCAPE

ARP6268 Design & Online

Communication Standards for Health

Ready Components

AS4138A Software Interfaces for

Ground-Based Monitoring Systems

ARPXXXX Data Interoperability

standards for Aerospace IVHM

AIR6334 Power Usage Metric

SAE INTERNATIONAL

The premier SAE Aerospace Conference and Exhibition

25

UPCOMING SAE EVENTS

Reliability

Propulsion

Safety

Systems Engineering

Unmanned Vehicles

Business & Economics

Aircraft Operations

Aircraft Interiors

Testing

Environmental impact

Avionics

Environmental Systems

Integrated Vehicle Health Management

Human Factors

Maintenance

Manufacture & Assembly

Materials

Aircraft Structures

Aircraft Power

Questions?

SAE Aircraft Standards Walkaround

SAE INTERNATIONAL 27

PARTNERING: SAE AND ICAO

• Noise and Emissions – CAEP

• Deicing

• Fuel Systems

• Volcanic Ash – membership in IVATF

• Multi-Crew Pilot Licenses

• SAE observer attendance at the 38th ICAO Assembly on invitation

• Application to join ICAO’s List of International Organizations pending

• Air Traffic Management

o SAE member of the ICAO Standards Roundtable

o SAE ATM Steering Group Scorecards supporting ICAO Functional Block Upgrades

o Global Human Factors Standardisation

MoU Signed in 2009

SAE INTERNATIONAL

AIA

AIAA

ARINC

ASTM

ATA

28

SAE PARTNERS AND LIAISONS WORLDWIDE

EUROCAE ASD

EASA

CAPE

IATA

SJAC

ISO

IEC FAA HAI U.S. DoD RTCA AWS

ICAO

Transport Canada

NIISU NATO

ADS

EDA

SAE INTERNATIONAL

SAE ORGANIZATIONAL STRUCTURE: COUNCIL LEVEL

Technical Standards Committees

Aero

General

Projects

Airport &

Ground

Support Aircraft

Aero

Electronics

& Electrical

Systems

Aero

Mech &

Fluids

Systems

Aero

Propulsion

Reliability,

Maint,

Support,

Logistics

Avionics

Systems

Aerospace Council

IVHM

ATM

Aerospace

Materials

Systems Groups

Technical

Standards

Board

SAE Board of Directors

Engineering

Meetings

Board

Sections

Board

Aerospace

Council

Engineering

Education

Board

Foundation

Board of

Trustees

Membership

Services

Board

Publications

Board

Performance

Review

Institute

Staff

Systems

&

Process