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HIRF Regualtion Jean-Christophe LAMY 15/12/2015 MR

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Presentation on theme: "HIRF Regualtion Jean-Christophe LAMY 15/12/2015 MR"— Presentation transcript:

1 HIRF Regualtion Jean-Christophe LAMY 15/12/2015 MR 05.002

2 Table of Content Introduction Historical HIRF Regulation
Latest EASA HIRF Regulation CS , INT POLs Method of showing compliance Applicable HIRF Requirement New TC Products STC/Major Change

3 INTRODUCTION Origin? Why Effect on Systems? Composite Material
HIRF: Human (Radars, Antennas) Why Effect on Systems? Composite Material Critical Computers

4 HIRF (High Intensity Radiation Field)

5 Frequency Band (10 kHz-40GHz)

6 HIRF Regulation (History)
Before 1988 in Europe NO Regulation for HIRF Protection Only concern at Equipment level (Equipment qualification DO160 sec 20)

7 HIRF Regulation (History)
After 1988 in Europe (from A320 TC) With Introduction of „super“ critical systems (FADEC, FBW) and EFIS HIRF requirements introduced via Special Conditions (CRI/SC)

8 HIRF Regulation (History)
Requirement for Critical System Level A system not perturbated when exposed to External Certification Envrionment Requirement for Essential System Level B/C systems not perturbated when exposed to External Normal Environment

9 HIRF Regulation (History)
After 1988 in USA HIRF requirements introduced via Special Conditions (Issue Paper/SC) Level A system not perturbated when exposed to External Certification I (Certification) or level A equipment not pertubated when exposed to 100V/m, Cat W DO160 sec20) Level B/C NO requirements

10 HIRF Regulation (History)
In early 90’ JAA were presently developing in co-operation with the FAA, a regulatory project for HIRF (cordinated JAA/FAA Electromagnetic Effects Harmonisation Working Group). The objective of the project is the issuance of an NPA (Notice of Proposed Amendment) in parallel with an FAA NPRM leading to a final regulation and associated advisory material and Users Guide. The EEHWG adopted a set of HIRF environment levels in November 1998

11 HIRF JAA/EASA Policy INT POLs
JAA has temporary adopted EEHWG activity with INT POLs (INT POL25/2, 23/1, 27&29/1) with: External HIRF Environments (Certification, Normal, Severe) Set of requirements (Critical, Essentials)

12 Equipment Qualification (introducing INT POLs)
HIRF Requirements (Time frame) 1988 End 90’ Begin 20’ End 2007 NO YES YES YES Equipment Qualification Special Condition Special Condition (introducing INT POLs) FAR 27/ CS 27/

13 Definition of the Regulatory HIRF Environments
This environment is based on the available data representing all authorised transmitters in Western Europe and the United States. Certification HIRF Environment Normal HIRF Environment FREQUENCY FIELD STRENGTH (V/m) PEAK AVERAGE 10 kHz – 500 kHz 500 kHz - 2 MHz 2 MHz - 30 MHz 30 MHz – 100 MHz 100 MHz – 200 MHz 200 MHz – 400 MHz 400 MHz - 1 GHz 1 GHz - 2 GHz 1, 2 GHz - 4 GHz 3, 4 GHz - 6 GHz 3, 6 GHz - 8 GHz 8 GHz - 12 GHz 1, 12 GHz - 18 GHz 18 GHz - 40 GHz FREQUENCY FIELD STRENGTH (V/m) PEAK AVERAGE 10 kHz - 2 MHz 2 MHz - 30 MHz 30 MHz MHz 100 MHz – 400 MHz 400 MHz – 700 MHz 700 MHz - 1 GHz 1 GHz - 2 GHz 2, 2 GHz - 6 GHz 3, 6 GHz - 8 GHz 1, 8 GHz - 12 GHz 3, 12 GHz - 18 GHz 2, 18 GHz - 40 GHz

14 Definition of the Regulatory HIRF Environments
Severe HIRF Environment FREQUENCY FIELD STRENGTH (V/m) PEAK AVERAGE 10 kHz kHz 100 kHz MHz 400 MHz – 700 MHz 700 MHz - 1 GHz 1 GHz - 2 GHz 5, 2 GHz - 4 GHz 6, 4 GHz - 6 GHz 7, 6 GHz - 8 GHz 1, 8 GHz - 12 GHz 5, 12 GHz - 18 GHz 2, 18 GHz - 40 GHz 1,

15 HIRF - Requirements  Critical systems must function normally when the aircraft is exposed to the normal HIRF environment Critical systems must be designed and installed such that to ensure their critical functions when the aircraft is exposed to the certification HIRF environment Essential systems, equipment providing essential function are not affected when exposed to DO 160 Cat R/T NB: Non-essential systems do not have regulatory constraints for HIRF

16 B or C (ESSENTIAL SYSTEM)
ENVIRONMENT CERTIFICATION LEVEL CERTIFICATION NORMAL EQUIPMENT LEVEL A (CRITICAL SYSTEM) Function must not be adversely affected during and after exposure to HIRF. Any system interruptions should be evaluated to assure continued performance of the aircraft function and should be approved by the cognisant aviation certification authority. Affected systems must automatically recover upon removal of HIRF effects, Systems must not be adversely affected during an after aircraft exposure to HIRF. As required by the equipment qualification procedures. B or C (ESSENTIAL SYSTEM) No requirement Equipment must not be adversely affected during and after exposure to the defined test level

17 Methods of Compliance (ED 107)
Level A system

18 Methods of Compliance (ED 107)
Level A system (classical Method for Radiated Susceptibility): A) ESTABLISH ATTENUATION CURVES TESTS ON SYSTEM/EQUIPMENT

19 Methods of Compliance (ED 107)
PHASE A): GENERIC ATTENUATION CURVES (100MHz-18GHz) or LOW LEVEL TESTS (LLSF)

20 Methods of Compliance (ED 107)
PHASE B: The Category level = f (Ext Env * ATT curves) + Margin Use of Categories of DO 160 Section 20

21 Generic Attenuation Curve

22 Less Classical Method  Test on Aircraft level with real threat
Similarity Approach (reuse of data of similar system with similar location on similar Aircraft Futur development: HIRF-SE project (virtual environment)

23 Methods of Compliance (ED 107)
Level B/C systems: Level B system: Equipment Test DO 160 section 20 Cat R (150 V/m peak) or Normal HIRF Environment + Attenuation DO 160 section 20 Cat D, E, F, G Level C system: Equipment Test DO 160 section 20 Cat T (5V/m average)

24 Methods of Compliance (ED 107)
DO 160 section 20 Categories

25 Regulatory References HIRF (Advisory)
AC/AMCs AC/AMC Certification of Systems for HIRF Effects USER‘S GUIDE ED-107A/ARP5583A HIRF User‘s Guide ED14/DO160 Section 20 HIRF

26 Latest HIRF Regulation
FAR , , 27/ published in September 2007 (adoption of HIRF NPRM) and associated AC CS July 2015 and AMC ( , 27/ published in futur CS Adts) Both Regulations are now harmonized

27 Applicable HIRF Regulation for new TC
Large A/C (+ AMC for guidance) General Aviation + Rotorcraft HIRF SC (+ED 107A for guidance) ( and 27/ AMC released in the near futur)

28 Applicable HIRF Regulation for Changes/STC
(installation/modification of susceptible systems) A/C certified before 1988 - Dedicated HIRF Special Condition/Interpretative Material based on latest INT POL 25/2, 23/1 or 27&29/1) (Authority Request) or - Elect to comply with latest regulation (Applicant’s Request) (+ AMC for guidance) (or , 27/ when new CSs released ) A/C certified after 1988 - Use of HIRF Special Condition of the TCDS or - Elect to comply with latest AMC for guidance(or , 27/ once CSs released) (Applicant’s Request, if HIRF SC not based on latest INT POLs)


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