military certification - dgaa.it regulatory framework... · armaereo 5/53 aer.p-7aer.p-7 “norms...

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July 2007July 2007

ITALIAN MINISTRY OF DEFENCEITALIAN MINISTRY OF DEFENCEDGAA DGAA –– DIREZIONE GENERALE DEGLI ARMAMENTI AERONAUTICIDIREZIONE GENERALE DEGLI ARMAMENTI AERONAUTICI

(AIR ARMAMENTS GENERAL DIRECTORATE)(AIR ARMAMENTS GENERAL DIRECTORATE)

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SUMMARYSUMMARY

FLIGHT CERTIFICATION APPROACHFLIGHT CERTIFICATION APPROACHFLIGHT CERTIFICATION APPROACH

UAV SAFETY REQUIREMENTSUAV SAFETY REQUIREMENTSUAV SAFETY REQUIREMENTS

LESSON LEARNED ON UAVs SAFETY CASESLESSON LEARNED ON LESSON LEARNED ON UAVsUAVs SAFETY CASESSAFETY CASES

COOPERATION IN THE FIELD OF UAV AIRWORTHINESSCOOPERATION IN THE FIELD OF UAV COOPERATION IN THE FIELD OF UAV AIRWORTHINESSAIRWORTHINESS

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SUMMARYSUMMARY





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NATIONAL APPLICABLE AIRWORTHINESS REGULATIONSNATIONAL APPLICABLE AIRWORTHINESS REGULATIONS

QUALIFICATIONQUALIFICATIONQUALIFICATION

AER.PAER.P--22

MILITARY AIRCRAFTREGISTRATION

MILITARY AIRCRAFTMILITARY AIRCRAFTREGISTRATIONREGISTRATION

AER.PAER.P--77

COMPLIANCE WITH A SET OF MINIMUM REQUIREMENTS AIMED TO SATISFY THE UAV AIRWORTHINESS SHALL BE DEMONSTRATED TO SUPPORT AIRCRAFT ADMISSION TO AIR NAVIGATION BY ITALIAN AUTHORITY (DGAA).

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AER.P-7AER.P-7

“Norms for registration and maintenance of theGovernment Aircraft Register " (R.A.M.)”““Norms for registration and maintenance of theNorms for registration and maintenance of theGovernment Aircraft Register " (R.A.M.)Government Aircraft Register " (R.A.M.)””

AER.PAER.P--77

• EXPERIMENTAL NATIONAL REGISTRATION NUMBER FOR PROTOTYPE

• EXPERIMENTAL NATIONAL REGISTRATION NUMBER FOR DEVELOPMENT AIRCRAFT (series A/C)

• NATIONAL REGISTRATION NUMBER FOR SERIES AIRCRAFT (in service)

“National registration and management procedure for

Military Aircraft”

THE PRESENT RULE CONTAINS THE PROCEDURES FOR OBTAINING ASSIGNMENT OF NATIONAL REGISTRATION NUMBER TO MILITARY AIRCRAFT/SYSTEM TO BE ADMITTED TO AIR NAVIGATION .

TYPOLOGIES OF REGISTRATION NUMBER DEPEND ON THE AIRCRAFT/SYSTEM USE AND ALLOCATED TASK, I.E.:

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THE SYSTEM RESPONSIBLE COMPANY/DELEGATED PARTNER COMPANY WILL PRESENT APPLICATION TO THE D.G.A.A. (U.G.C.T - 3° UFFICIO) FOR THE ASSIGNMENT OF A PROTOTYPE IDENTIFICATION.

THE DGAA WILL PROVIDE FOR REGISTRATION IN THE PROTOTYPE AIRCRAFT REGISTER AND IT WILL COMMUNICATE THE ASSIGNMENT.

ASSIGNMENT OF PROTOTYPE IDENTIFICATIONASSIGNMENT OF PROTOTYPE IDENTIFICATION


AER.PAER.P--77 “National registration and management procedure for


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BEFORE PRESENTING REQUEST, IT IS IMPORTANT THAT THE COMPANY HAS ALREADY:

1. DECIDED A TARGET ENVELOPE (TARGET LIMITS -BLOCK CLEARANCE)

2. DECIDED THE AIRCRAFT'S CURRENT OPERATION ENVELOPE (AIRWORTHINESS FLIGHT LIMITATIONS)

3. EXECUTED A SYSTEM SAFETY ANALYSIS



AER.PAER.P--77 “National registration and management procedure for


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3) SAFETY ANALYSIS:

A SYSTEM SAFETY ANALYSIS SHALL PROVIDE A TOTAL PROBABILITY FOR THE LOSS OF THE SYSTEM EXPRESSED FOR THE AIRCRAFT INTO FAILURE RATE FOR CATASTROPHIC EVENT AND SHALL DEMONSTRATE THAT THERE ARE NO SINGLE FAILURE OF A SYSTEM’S A.C. THAT LEAD TO THE LOSS OF THE AIRCRAFT.


“Qualification of military aircraft and pertaining systems - Suitability to installation”“Qualification of military aircraft and pertaining systems - Suitability to installation”

AER.PAER.P--22

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NATIONAL AUTHORIZATION PROCESSNATIONAL AUTHORIZATION PROCESS

DGAADGAADGAA

SMASMASMA

DGAADGAADGAA

UAV CONFIGURATION“AS DESIGNED” FLIGHT AREAS

FOR UAV ACTIVITIES

APPLICATION FOR SYSTEM

REGISTRATION NUMBER

APPLICATION FOR APPLICATION FOR SYSTEM SYSTEM

REGISTRATION REGISTRATION NUMBER NUMBER FLIGHT TEST

AREAS DESIGNATION

FLIGHT TEST FLIGHT TEST AREAS AREAS

DESIGNATION DESIGNATION

Operational Procedures Document

EXP NATIONAL

REG NUMBER

EXP EXP NATIONAL NATIONAL

REG NUMBERREG NUMBER

AIR STAFF (SMA)AIR STAFF (SMA)AIR STAFF (SMA)

ADMISSION TO ADMISSION TO AIR NAVIGATIONAIR NAVIGATION

• BLOCK CLEARANCE• SAFETY ANALYSIS• AWFL

FLIGHT TEST WORKING GROUP

(CUSTOMER/INDUSTRY)

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SUMMARYSUMMARY





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UAVS CLASSESUAVS CLASSES

SAFETY TARGET SAFETY TARGET REQsREQsUAVS Classes

(Mass of UAVS) DEFINITIONDEFINITIONMILITARY MILITARY AIRCRAFT AIRCRAFT

REGISTRATIONREGISTRATION

GCSGCSOPERATORSOPERATORS

CUMULATIVE CUMULATIVE PROBABILITY OF PROBABILITY OF CATASTROPHIC CATASTROPHIC

EVENTEVENT

10E10E--55

10E10E--66

10E10E--66

10E10E--66

500 <W <2720 kg500 <W <2720 kg 10E10E--66 10E10E--55

SUAVSUAV10E10E--77

REGISTER REGISTER AS A TYPEAS A TYPE

150 <W <500 kg150 <W <500 kg TUAVTUAV 10E10E--55

REGISTER REGISTER INDIVIDUAL INDIVIDUAL

AIRCRAFTAIRCRAFT

MILITARY MILITARY PILOTPILOT

CUMULATIVE CUMULATIVE RATE FOR RATE FOR

SYSTEM LOSSSYSTEM LOSS

W < 2 kgW < 2 kg MICRO MICRO 10E10E--33

2 <W< 20 kg2 <W< 20 kg MINIMINI 10E10E--44GROUND GROUND

MILITARY MILITARY OPERATOROPERATOR

20 <W <150 kg20 <W <150 kg LIGHTLIGHT 10E10E--55

W > 2720 kgW > 2720 kg10E10E--66

<<<<

5*E10E5*E10E--66

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UAV SAFETYUAV SAFETY

⎟⎟⎠

⎞⎜⎜⎝

⎛××=

=×=

debrisPopulationDensity

LossSystemUAV

PeopleHitting

LossSystemUAViccatastroph

ADPp

ppp

MINIMUM EQUIPMENTS/SYSTEMS:navigation and anti-collision lights (24 hours a day)Communication System “Earth/Board/Earth”a telephone inside the Ground Control StationTransponder

INVESTIGATE THE FEASIBILITY TO ADAPT AND USE SYSTEMS AS:

Traffic Collision Avoidance System (TCAS),Low Altitude Alerting System,Ground Proximity Warning System (GPWS),Terrain Awareness and Warning System (TAWS),Automatic Dependent Surveillance - Broadcast (ADS-B)

COURSE DEVIATION COMBINED WITHCOLLISION WITH

ANOTHER A/C

COURSE DEVIATION COURSE DEVIATION COMBINED WITHCOMBINED WITHCOLLISION WITH COLLISION WITH

ANOTHER A/CANOTHER A/C

UAV LOSScombined with

HITTING PEOPLE

UAV LOSSUAV LOSScombined withcombined with

HITTING PEOPLEHITTING PEOPLE

UAV CATASTROPHIC

EVENT

UAV UAV CATASTROPHIC CATASTROPHIC

EVENTEVENT

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SSA

P (SYSTEM LOSS)P (SYSTEM LOSS)P (SYSTEM LOSS)

REGULATIONS FOR UAVREGULATIONS FOR UAV

P (HITTING PEOPLE ON GROUND)

P (HITTING P (HITTING PEOPLE ON PEOPLE ON GROUND)GROUND)

THE INTRODUCTION OF THE THE INTRODUCTION OF THE POPULATION DENSITYPOPULATION DENSITYALLOWS TO CERTIFY THE DESIGN OF UAV SYSTEM ALLOWS TO CERTIFY THE DESIGN OF UAV SYSTEM WITH LOW INHERENT RELIABILITY (RATE OF WITH LOW INHERENT RELIABILITY (RATE OF SYSTEM LOSS), THOUGH MAINTAINING AN HIGH SYSTEM LOSS), THOUGH MAINTAINING AN HIGH DEGREE OF DEGREE OF SAFETY AGAINST THIRD PARTIESSAFETY AGAINST THIRD PARTIES

A/C INHERENT RELIABILITY

0303

POULATION DENSITY

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SUMMARYSUMMARY





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PREDATOR RQ 1APREDATOR RQ 1A

http://www.fas.org/irp/program/collect/predator-00000000.jpg

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PREDATOR SAFETY CASEPREDATOR SAFETY CASE

UNDER THE OPERATIVE CONTROL VOLUME UNDER THE OPERATIVE CONTROL VOLUME THE POPULATION DENSITY MUST BE LESS THE POPULATION DENSITY MUST BE LESS THAN 11.8 abit/kmTHAN 11.8 abit/km22

OPERATIVE CONTROL VOLUMEOPERATIVE CONTROL VOLUMEOPERATIVE CONTROL VOLUME

0303

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PREDATOR MISSION SAFETYPREDATOR MISSION SAFETY

• THE CALCULATION OF THE AVERAGE OF POPULATION DENSITY IS THEN REVIEW ACCORDING TO THE OPERATION (MISSION) TO BE PERFORMED IN THE DESIGNED GEOGRAPHICAL LOCATION.

• THE INTRODUCTION OF THE CONCEPT OF MISSION PHASE EXPOSURE TIME CAN ALLOW THE UAV SYSTEM TO FLY OVER AN HIGHER POPULATED AREA FOR A LIMITED PERIOD OF TIME.

∑ ×××=−i

iiiimissioncatastr TDPAPP %

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FALCO SURVEILLANCE UAV SYSTEMFALCO SURVEILLANCE UAV SYSTEM

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• Typical weight 420 Kg

• Internal payload capability > 70 Kg

• Optional extra fuel 40 Kg

• Max transfer speed 125 Kts

• Typical operational speed 80 Kts

• Max operational altitude 6000 m

• Endurance 8 h at max payload

• Max endurance with basic payload 14 hours

• Link range > 200 km.

Typical Characteristics

FALCO SURVEILLANCE UAV SYSTEMFALCO SURVEILLANCE UAV SYSTEM

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ENAC ISSUED THE FIRST EUROPEAN “PERMIT TO

FLY” CLEARANCE AND THE FIRST UAV CIVIL

IDENTIFICATION CODE (I –RAIE) TO THE BASIC FALCO

UAVS

ENAC ISSUED THE ENAC ISSUED THE FIRST FIRST EUROPEAN EUROPEAN ““PERMIT TO PERMIT TO

FLYFLY”” CLEARANCECLEARANCE AND THE AND THE FIRST UAV CIVIL FIRST UAV CIVIL

IDENTIFICATION CODE (I IDENTIFICATION CODE (I ––RAIE) TO THE BASIC FALCO RAIE) TO THE BASIC FALCO

UAVSUAVS

FALCO: CIVIL CERTIFICATION HISTORICAL BACKGROUNDFALCO: CIVIL CERTIFICATION HISTORICAL BACKGROUND

14 June14 June’’0505

FALCO FALCO startedstarted CivilCivil CertificationCertification ((AirworthinessAirworthiness) ) withwith ENAC ENAC UsingUsing 2 2 aircraftsaircrafts specimenspecimen

Official UAVsRegulation derived from JAR-VLA and

JAR 23JAA/Eurocontrol A

Concept for European

Regulations for Civil UAVs

ENACENACENACCOMPLIANCECOMPLIANCE

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FALCO: MILITARY QUALIFICATIONFALCO: MILITARY QUALIFICATION

MILITARY CERTIFICATIONMILITARY CERTIFICATIONMILITARY CERTIFICATION

AER.PAER.P--22

DGAA FORMALLY REQUIRED COMPLIANCE WITH AER.P-2

SAFETY SEVERITY DEFINITIONS, PROBABILITY LEVELS AND

POPULATION DENSITYAPPROACH

THE COMPANY HAS ACCOMPLISHED A REDESIGN PROCESS FOR THOSE FEATURES NOT COMPLIANT WITH

DGAA REQUIREMENTS

JulyJuly 0606

OctOct 0606

DGAADGAADGAA

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FALCO: MILITARY QUALIFICATIONFALCO: MILITARY QUALIFICATION

SAFETY TARGET SAFETY TARGET REQsREQsUAVS Classes

(Mass of UAVS) DEFINITIONDEFINITIONMILITARY MILITARY AIRCRAFT AIRCRAFT

REGISTRATIONREGISTRATIONOPERATORSOPERATORS CUMULATIVE CUMULATIVE

PROBABILITY OF PROBABILITY OF CATASTROPHIC CATASTROPHIC

EVENTEVENT

150 <W <500 kg150 <W <500 kg TUAVTUAV 10E10E--66

500 <W <2720 kg500 <W <2720 kg 10E10E--66 10E10E--55

SUAVSUAV

10E10E--55

10E10E--77

REGISTER REGISTER INDIVIDUAL INDIVIDUAL

AIRCRAFTAIRCRAFT

MILITARY MILITARY PILOTPILOT

CUMULATIVE CUMULATIVE RATE FOR RATE FOR

SYSTEM LOSSSYSTEM LOSS

W > 2720 kgW > 2720 kg10E10E--66

<<<<

5*E10E5*E10E--66

SAFETY CASE FIGURE

SAFETY CASE SAFETY CASE FIGUREFIGURE

FALCOSYSTEM SAFETY

ANALYSIS

FALCOSYSTEM SAFETY

ANALYSIS

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• ACCORDING TO AC23-11A, FOR MANY ASPECTS DGAA DOESN’T CONSIDER APPLICABLE THE CS-VLA (THOUGH THE MTOW IS 500KG).

• THE APPLICATION OF CS23 STANDARDS WERE CONSIDERED MORE SUITABLE FOR THE APPLICATION.

• DGAA AND THE COMPANY AGREED TO INSTALL ENGINE AND PROPELLER CERTIFIED AGAINST CS-E AND CS-P.

FALCO: MILITARY QUALIFICATION PROCESSFALCO: MILITARY QUALIFICATION PROCESS

FLA

CO

Q

UA

LIFI

CA

TIO

N

PR

OC

ESS

FLA

CO

FL

AC

O

QU

ALI

FIC

ATI

ON

Q

UA

LIFI

CA

TIO

N

PR

OC

ESS

PR

OC

ESS

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• DGAA FORMALLY REQUIRED COMPLIANCE WITH RTCA-DO-178 SOFTWARE REQUIREMENTS.

• DGAA AND THE COMPANY AGREED THE SW LEVELS REQUIRED FOR EACH PIECE OF SW, ACCORDING TO THE SPECIFIC SYSTEM ARCHITECTURE AND TO ARP-4754 GUIDELINES.

• THE SAFETY TARGET AND FUNCTIONAL HAZARD ANALYSIS HAVE BEEN AMENDED AND AGREED, GIVING NEW DESIGN DRIVERS.

FALCO: MILITARY QUALIFICATION PROCESSFALCO: MILITARY QUALIFICATION PROCESS

FALC

O

QU

ALI

FIC

ATI

ON

P

RO

CES

S

FALC

O

FALC

O

QU

ALI

FIC

ATI

ON

Q

UA

LIFI

CA

TIO

N

PR

OC

ESS

PR

OC

ESS

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RAVEN BRAVEN B

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• Typical weight 4,2 lbs

• Payload capability 6,5 oz

• Link Range 10 Km

• Endurance 60-90 mins

• Typical operational speed 20 - 57 km/h, 17-50 knots

• Max operational altitude 100-500 ft (30-152 m) AGL, 14,000 ft MSL max launch altitude

Typical Characteristics

RAVEN BRAVEN B

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RAVEN B: MILITARY CERTIFICATIONRAVEN B: MILITARY CERTIFICATION

USAGE IN MILITARY CONTROLLED RANGES

REGISTRATION AS A TYPE

DGAA FORMALLY REQUIRED COMPLIANCE WITH AER.P-2SAFETY SEVERITY DEFINITIONS, PROBABILITY LEVELS AND POPULATION DENSITY APPROACH FOR MICRO UAV (W<2 KG)

THE COMPANY IS DEVELOPING IT RAVEN B IT RAVEN B

QUALIFICATION PLANQUALIFICATION PLAN

AprilApril 0707

MayMay 0606

DGAADGAADGAA

MILITARY CERTIFICATIONMILITARY CERTIFICATIONMILITARY CERTIFICATION

AER.PAER.P--22

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SUMMARYSUMMARY





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INTERNATIONAL DGAA POSITIONINTERNATIONAL DGAA POSITION

DGAADGAADGAA

EASAEASAEASA

Needs and approaches toCertification are verydifferent

NeedsNeeds and and approachesapproaches totoCertificationCertification are are veryverydifferentdifferent

CIVIL-MILITARY AUTHORITIES COOPERATIONCIVIL-MILITARY AUTHORITIES COOPERATION

DGAA DON’T CONSIDER APPLICABLE TO PURSUE

A CIVIL-MILITARY COOPERATION AIMED

TO SET COMMONSTANDARDS /

PROCEDURES / REQUIREMENTS

DGAA DONDGAA DON’’T CONSIDER T CONSIDER APPLICABLE TO PURSUE APPLICABLE TO PURSUE

A A CIVILCIVIL--MILITARY MILITARY COOPERATION COOPERATION AIMED AIMED

TO SET TO SET COMMONCOMMONSTANDARDS / STANDARDS /

PROCEDURES / PROCEDURES / REQUIREMENTSREQUIREMENTS

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DGAADGAADGAA

OTHER EUROPEAN MILITARY AUTHORITIES

OTHER EUROPEAN OTHER EUROPEAN MILITARY AUTHORITIESMILITARY AUTHORITIES

Common needs, thoughdifferent approaches toCertification

Common needs, thoughdifferent approaches toCertification

EUROPEAN MILITARY AUTHORITIES COOPERATIONEUROPEAN MILITARY AUTHORITIES COOPERATION

DGAA CONSIDER A DGAA CONSIDER A NEED TO PURSUE NEED TO PURSUE

COOPERATIONCOOPERATION AMONG AMONG EUROPEAN MILITARY EUROPEAN MILITARY

AUTHORITIESAUTHORITIESAIMED TO SET AIMED TO SET COMMONCOMMON

STANDARDS / STANDARDS / PROCEDURES / PROCEDURES /

REQUIREMENTS FOR REQUIREMENTS FOR FUTURE COMMON FUTURE COMMON

PROGRAMSPROGRAMS

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OCCAROCCAROCCAR

There is a potential risk of redundances

ThereThere isis a a potentialpotential riskrisk of of redundancesredundances


ETAPETAPETAP

EDAEDAEDA

EMAAGEMAAGEMAAG

………

DGAA POSITION ISDGAA POSITION ISTHATTHAT EDA EDA IS IS

THE RIGHT FORUMTHE RIGHT FORUMCAPABLE TO COLLECT CAPABLE TO COLLECT ALLALL THE EUROPEAN THE EUROPEAN

MAA (Military Aviation MAA (Military Aviation Authorities)Authorities)……

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B U TB U T……THISTHIS COULD BE DONE ONLY COULD BE DONE ONLY

WHEN THE WHEN THE ““CORE CORE REGULATORY FRAMEWORKREGULATORY FRAMEWORK””

HAS BEEN DEVELOPED BY HAS BEEN DEVELOPED BY EXISTING EXISTING PROJECTSPROJECTS……


OCCAR - JMAGOCCAR OCCAR -- JMAGJMAG

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OCCAR JMAGOCCAR JMAG

• THE TASK OF THE OCCAR JMAG (JOINT MILITARY AIRWORTHINESS GROUP) IS TO WORK ON THE DRAFTING OF HARMONIZED AIRWORTHINESS CERTIFICATION AND CONTINUED AIRWORTHINESS PROCEDURES FOR MILITARY AIRCRAFT.

• THE OCCAR JMAG IS THE ONLY OFFICIALLY CREATED GROUP, REPORTING TO DEFENCE MINISTERS OF OCCAR MEMBER STATES, HAVING THE PURPOSE OF DEVELOPING HARMONISED AIRWORTHINESS CONCEPTS AND PROCEDURES.

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SHORT TERM CONSIDERATIONSHORT TERM CONSIDERATION

1. DGAA CONSIDER OCCAR JMAAG THE RIGHT PLACETO ESTABLISH A STRUCTURE OF COMMON KEY PRINCIPLES FOR MILITARY AIRWORTHINESS PROCESSES AND PROCEDURES TO BE UTILISED IN CO-OPERATIVE PROGRAMMES.

OCCAR - JMAGOCCAR OCCAR -- JMAGJMAG

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SHORT TERM CONSIDERATIONSHORT TERM CONSIDERATION

2. DGAA IS ACTIVE MEMBER OF FINAS WG TO PRODUCE A COMPLETE AIRWORTHINESS CODE FOR UAVS THAT COULD BE ADOPTED BY NATO AS A STANAG

• IT MoD Intention to ratify STANAG 4671

• Reservations on 1309 (System Safety i.a.w. AER.P-2)

FINASFINASFINAS

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LONGER TERM CONSIDERATIONLONGER TERM CONSIDERATION

• THERE IS A RELEVANT POTENTIAL IN THE FUTURE FOR EDA TO PICK UP THE WORK DONE

• FINAS IS AN ESSENTIAL 1ST STEP FOR STATE “UAVS, IN PARALLEL THERE IS THE NEED TO THINK HOW TO INSERT UAVS IN GENERAL AIR TRAFFIC TO ALLOW UNLIMITED USE OVER ANY TERRITORY AND WITHOUT VERY LONG LEAD TIMES “FILE AND FLY” !

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ITALIAN MINISTRY OF DEFENCEITALIAN MINISTRY OF DEFENCEDGAA DGAA –– DIREZIONE GENERALE DEGLI ARMAMENTI AERONAUTICIDIREZIONE GENERALE DEGLI ARMAMENTI AERONAUTICI

(AIR ARMAMENTS GENERAL DIRECTORATE)(AIR ARMAMENTS GENERAL DIRECTORATE)

THANK YOU FOR THANK YOU FOR YOUR YOUR

ATTENTIONATTENTION

military certification - dgaa.it regulatory framework... · armaereo 5/53 aer.p-7aer.p-7 “norms...

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