AESI Aerospace Engineering Solutions International AESI Scope of

AESI Aerospace Engineering Solutions International (AESI) Scope of Work and Capabilities COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED.

AESI Introduction • AESI was established by a group of avionics and flight controls engineering and certification experts • AESI’s goal is to support OEMs and avionics suppliers with design, integration and certification capabilities: • Small companies and individual aircraft owners • Medium size companies • Large OEMs and system suppliers • To enable those projects, AESI relies on: • Internal expertise, experience and skills • Representation in China and Europe • Professional references available from: • • • Major OEM’s (COMAC, Bombardier, Boeing, Airbus, Embraer, Dassault, Gulfstream), Major systems suppliers (Honeywell, Rockwell-Collins, GE, Parker) Certification agencies (CAAC, FAA, EASA, ANAC, TCCA) People/experts/officials: Names and contact information for personal and professional references available at request COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED.

AESI Team and Organization COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED.

AESI Engineering Capabilities • • • AESI engineering capabilities: Avionics systems/SW experts - 5, System integration experts - 2 FCS system/SW/control design, handling quality experts - 3, Electrical system expert Aircraft operations and maintenance expert 2 DER’s (Pilot and Systems) and 1 Candidate DER (Systems, Safety, SW), Capability to engage EASA CVE System and SW support team • Aerospace regulation committee participation: Member of S-18 SAE Committee (ARP 4754 A/ARP-4761) Extensive design, integration and certification experience from multiple avionics and FCS programs/projects working with following companies: Boeing, Airbus, COMAC, FACRI, Bombardier, Embraer, Gulfstream, Pilatus, Rockwell Collins, Honeywell • • Copyright 2016 AESI. All rights reserved. Page 4

AESI Engineering Team • Education/professional training • • • 1 Phd (FCS, aerodynamics, control laws, handling qualities), 3 MSc (avionics/FMS, FCS, mechanical systems, aerospace general), 6 BScs (avionics, FCS, aerospace, electrical systems, aircraft operations and maintenance, computer science, human factors) Pilot DER with training license (subcontractor) – human factors, flight test support Candidate Systems DER (avionics, FCS, ARP-4754 A, safety) Systems DER (avionics/FCS, safety - part time) NOTE: most of team members have multiple fields of expertise. System and SW design/support team composed of computer science, aerospace and electrical engineers Subcontractors/suppliers engaged as needed • Aerospace regulation committees • Member of S-18 SAE Committee (ARP-4754 A/ARP-4761) • Other • Financial/business/contracts/legal expertise • Total aerospace experience of AESI team • More than 250 years of total experience in aerospace industry COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED.

AESI Engineering Team Professional Experience and Previous Programs/Projects • Projects/programs • • • • Air transport: C 919 (FCS, avionics, sensors, Landing Gear controls, ARP-4754 A), B 787 (FCS, FMS, avionics sensors and radios), A 350/380 (Surveillance System, FMS, Environmental Control System, ETLT) Regional: ARJ-21 (FCS, avionics), DASH 8 -100/200/300/400 (FCS, avionics, human factors), Ejets/E 2 (FCS, FMS, avionics platform, sensors), CRJ-700/900 (avionics platfor & displays, FMS, antennas), N 250 (avionics platform, systems integration, Cockpit Controls, Flight Test preparation) Business and General Aviation: G 650/G 500 (avionics platform, FCS, displays, FMS, Touch Screen Panel, systems integration), F 900/2000/7 X (avionics platform, FCS, displays, FMS, Touch Screen Panel, systems integration), Cessna Citation Sovereign (avionics platform, ADSB-Out STC), Military: KTX-1, Eagle/Galeb (military), DASH-8 Maritime Patrol and NAV Trainer Copyright 2016 AESI. All rights reserved.

AESI Engineering Team Professional Experience and Previous Programs/Projects – cont. • Systems • • • • Stand-alone and integrated FCS/AFCS systems and equipment, IMA Avionics Systems (EPIC/APEX, ARINC-664 based systems, Proline 4/Proline 21, Thales DASH 8 -400), Stand-alone avionics systems/equipment (FMC, displays, radios, ADS, IRS, cockpit controls/human factors, Touch Screen Panel, ETLT, …) Mission equipment (Nav Trainer, maritime patrol surveillance systems, FLIR, mission coordination system/FMS, …) Special purpose equipment (including integrated surveillance systems, maintenance system, …) Electrical Systems (power generation and distribution) Mechanical systems (landing gear controls, hydraulic) Maintenance and operations systems and equipment (for airlines) Functions / mandates ADS-B Out (currently working another STC with FAA), ADS-B In, Datalink, PM-CPDLC, FANS 1, FANS 2, WAAS LPV, RNP/RNP-AR, RAAS / Smart. Runway / Smart. Landing, Synthetic Vision/Integrated Navigation Moving Map, CDTI (AIR-B, VSA, SURF, ITP, etc. ), 2 D/3 D Airport Moving Maps, EFB, CAT I, III approaches, Etc. Copyright 2016 AESI. All rights reserved.

AESI Organization Copyright 2016 AESI. All rights reserved. Page 8

AESI Design Capabilities COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED.

AESI Expertise and Capabilities • • • • Systems and equipment design – conceptual and detailed System/Software architecture, based on safety analysis and on system requirements Controls design (where needed) to meet airplane functions, performances and handling qualities, implementation and verification, System integration (internal, with aircraft and other systems), Complex Integrated Systems Individual “black boxes” Functions integration with the rest of the aircraft or with the existing systems Creation of systems design, safety and certification processes and documents to comply with: Applicable TSO Regulations and advisory materials Industry guidance’s (DO-178 B/C, DO-254, DO-297, ARP-4754 A, ARP-4761) Perform supplier’s audits – available DERs Based on existing and/or developed AESI compliance documents templates Review and coordination of design and certification with certification authorities COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 10

AESI Design Expertise - General • • • • • Systems and equipment design, selection, integration and certification for both commercial and military programs: Flight Management System Integrated platforms Electronic Displays Systems Flight Controls/Autopilot/FBW Systems Comm and Nav Radio Systems (VHF, Satcom, Datalink, VOR/ILS/ADF) Surveillance Systems (TCAS (CDTI), TAWS, Rad Alt, Transponder, Weather Radar) Avionics Sensors (Air Data, IRS/AHRS, GPS) Electrical power supply/conversion, electrical distribution system and wiring integration Cockpit controls / human factors Mission equipment integration Mechanical systems and structures Aircraft maintenance and operations New functions added to the existing Avionics, Flight Control and mission systems FAA/EASA mandates New and novel aircraft functions (both commercial and military) Modernization / improvements Special functions (commercial and mission) Documents, processes, audits, requirements management, configuration management COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 11

AESI Design Expertise – Avionics Systems • For avionics systems (integrated platforms or stand-alone systems), AESI can provide: • • • • • Systems design, integration, certification To perform those general tasks, AESI would perform the following activities Define system functions and sub-functions Define system architecture and interfaces Create system and equipment requirements, including requirements management using selected tool Allocate those requirements to SW and/or hardware items Create and perform V&V process and activities Checklists for both validation and verification V&V plans, matrices and summaries Necessary Work Instruction, processes and guidance’s Test definition (formal validation and verification or functional tests) at both: system and item/SW levels Support and perform system audits (SR 1, SR 2, SR 3, SR 4) Integration of FMS with: Avionics system (displays, sensors, cockpit controls), FCS/AFCS and other aircraft systems Implementation support (SW, HW or both) if required by customer Certification, configuration management and process assurance support. Create design and certification documents, processes and configuration management COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 12

AESI Design Expertise - FMS • AESI can perform design, consulting and certification work for stand-alone or integrated Flight Management Systems (FMS) and its functions, as follows: • Design, integration, V&V and certification support for already selected FMS by customers • For the new design, AESI can provide the following: • • • Define system functions and sub-functions Create system and equipment requirements, including requirements management using selected tool (DOORS or other) FMS V&V process creation and deployment Checklists for both validation and verification V&V plans, matrices and summaries Necessary Work Instruction, processes and guidance’s Test definition (formal validation and verification or functional tests) at both: system and SW levels For both options AESI would perform the following: Integration of FMS with: Avionics system (displays, sensors, cockpit controls), FCS/AFCS and other aircraft systems If there is implementation support needed (SW, hardware or both) for FMS, AESI can offer to perform those activities as well. Certification, configuration management and process assurance support. COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 13

AESI Design Expertise – Touch Screen Panel • TCS system/functions design, integration and certification support would include: • System design, • • • • Architecture definition Functional definition and allocation of Design Assurance Levels System requirements creation and allocation to SW/HW equipment and items, System Requirements management Safety process definition FHA, PSSA, SSA creation Coordination with supplier’s safety teams, Coordination with CAAC (and with FAA/EASA if needed) For SW detailed design, AESI could support customer in finding and evaluation of the subcontractor/supplier, who would develop the SW under AESI guidance and support. For customer selected equipment provider AESI can support customer in the following activities: Design guidance/direction/process, V&V process guidance and review Design review, Certification, Supplier interface definition and oversight Copyright 2016 AESI. All rights reserved. Page 14

AESI Design Expertise – Flight Controls • For Flight Controls System (FCS) AESI can organize, lead and perform the following: • • • System and controls design, Architecture definition, System requirements creation and allocation to SW/HW equipment and items, Safety process Creation of: FHA, PSSA, CMA, PRA, Zonal Coordination with suppliers safety teams, Coordination with CAAC For SW design, AESI can provide the following options: Find subcontractor/supplier who would develop the SW under AESI guidance and support or engage AESI SW team (depending on customer’s preferences and project complexity). If using AESI SW team, AESI would offer the complete design/development/integration/certification package. • If customer has already selected the FCS equipment provider AESI can: • • • Take over the package for design, integration and certification or Support customer in the following areas: Design and requirements management guidance, Design and implementation review, Certification, including audits Supplier oversight Copyright 2016 AESI. All rights reserved. Page 15

AESI Design Expertise - Software and Hardware • • • AESI performs SW and HW design using: AESI team in Europe, specialized in SW and general HW design Subcontractors in Phoenix (Arizona, USA) Subcontractors in India Full subcontractors/supplier process and quality oversight Design based on the process compliant with: DO-178 B / C (including DO-331 for model based development) DO-254 (including HAM models database) Design process aligned with IDAL allocations • • Design supports aerospace programs and projects Design interfaced with functional/system level definitions/requirements • SW and hardware items design requirements originated from AESI system design requirements document(s) Requirements tracing provided and used for V&V • • Configuration management and process assurance fully aligned with regulations and industry guidance’s Copyright 2016 AESI. All rights reserved. Page 16

AESI Design Process COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED.

AESI Requirements Creation and Management Expertise • Creation of system and/or aircraft Requirement Specification document containing: • • • • Systems/aircraft requirements creation and requirements management, FHA and safety/reliability/maintainability requirements for aircraft/system Requirements for system integration/IOC with aircraft and with other systems Avionics, FCS, electrical, landing gear, cockpit controls, etc. Regulations compliance requirements System requirements allocation to equipment and SW/hardware Items Create and deploy: Requirements management process Based on DOORS or other Requirements management tools Configuration control and management process Includes requirements problem reports defining/handling/closure System/aircraft requirements validation and verification: Requirements Validation process, plan, matrix and summary Requirements Verification process, plan, matrix (including verification test procedures) and summary Organize and perform system and items audits Coordination with and provide guidance to equipment, HW and SW suppliers COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 18

AESI Requirements Specification - Document • Create the Top Level Requirements aircraft/system specification which: • Serves as the ‘Top Level’ specification for the Aircraft and its Systems • Top Level Specification will contain: • Aircraft system overview, • Architecture definition and requirements • Functional/operational/performance/human factors requirements, • Aircraft/system integration definitions • Interfaces (electrical and mechanical), containing: Physical connector/pins Type of data transfer (A 429, A 664, etc. ), plus reference to integrated platform (where existing) I/O characteristics System ICD and integrated platform (where existing) I/O sources & destinations Signal characteristics and source selection • FHA/safety requirements (and most often the FDAL definitions), • List of applicable regulations and their compliance requirements COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 19

AESI Requirements Specification/Documents Organization COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 20

AESI Safety and Reliability Expertise • • • AESI can provide Aircraft / system safety process definition/creation Safety objectives definition in accordance with ARP-4754 A (based on aircraft or system architecture) Using ARP-4761 guidance Creation and/or review of safety documents/artifacts Safety requirements definition, tracing and validation / verification • AESI can create the following safety documents/artifacts (in accordance with ARP 4754 A and ARP-4761): • Safety Program Plan • Aircraft PASA (Preliminary Aircraft Safety Assessment) and/or System PSSA (as required) • Aircraft / System FHA • Aircraft / system Safety Requirements • FDALs and IDALs assigned • Final ASA (Aircraft Safety Analysis) and/or SSA (System Safety Assessment) • Safety review of derived requirements • Proposed safety mitigations • Independence criteria and independence review • AESI safety process will ensure compliance with AC/AMJ 25. 1309 COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 21

AESI Aircraft / System Validation Expertise • Create Aircraft / System Validation and Verification processes which are compliant with ARP-4754 A • Based on ARP-4754 A V&V objectives • Aircraft / System Validation process will cover integrated system and equipment • Validation process will contain: • • • Validation work instruction/process guidance, including: Coverage analysis Other validation methods Validation Checklists System Review (SR 2) preparation and execution Relationship with requirements management tool Documents/artifacts as follows: Validation Plan, Validation Matrix, Validation Summary Defined relationship between system and equipment validation activities Coordination with customers, subcontractors, suppliers and certification authorities COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 22

AESI Aircraft/System Verification Expertise • • • • • Aircraft / System verification process will cover integrated system and equipment Verification process will contain: Verification work instruction/process guidance, including Verification methods (test, review, analysis, simulation, coverage analysis, verification credit) Verification Checklist Verification System Review (SR 3) preparation and execution Relationship with requirements management tool Documents/artifacts creation, as follows: Verification Plan, Verification Test Procedures (including test tools and expected PASS/FAIL criteria and boundaries) Verification Matrix, Verification Summary Test rigs definition/design Simulation and/or real equipment based Conformity Configuration management Defined relationship between system and equipment verification activities Include verification credit (as applicable) Coordination with customers, subcontractors, suppliers and certification authorities COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 23

AESI Items (SW and HW) Validation and Verification Expertise • AESI created SW and hardware items V&V process is based on: • • DO-178 B/C for SW, DO-254 for AEH and DO-160 for simple hardware SW/HW requirements documents (High and Low Level Requirements) V&V process will contain: V&V work instruction/process guidance’s, including V&V methods (test, review, analysis, simulation, coverage analysis, verification credit) V&V Checklist SOI 1 -4 audits preparation guidance Interface with system and/or aircraft requirements Documents/artifacts as follows: V&V Plan, Verification Test Procedures (including test tools and expected PASS/FAIL criteria and boundaries) Verification Summary Include V&V credit (as applicable) from system level V&V process Other V&V documents/artifacts/processes needed to ensure the compliance with DO-178 B/C, DO 254 and/or DO-160 • • • • Coordination with customers, subcontractors and certification authorities COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 24

AESI Certification and Training COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED.

AESI Certification Expertise and Capabilities - General • • • • • AESI can offer to perform the following certification activities: Show compliance with applicable: CAAC/FAA/EASA regulations, TSO, advisory materials, and Issue Papers Create certification plan, define certification process including templates and work instructions Prepare and/or review all certification documents, Perform system/SW/HW audits, Create certification package and offer additional certification work, if so requested for: Software: SW development guidance / process, Compliance with DO-178 B or C, SW audits (internal and suppliers audits), Work instructions creation, Coordination with CAAC and with Suppliers. HW compliance effort (DO-160, HIRF/IEL, DO-254) System: Complete system design/safety and certification process based on ARP-4754 A (AESI has the substantial expertise in that area), ARP-4761/safety, DO-297 (if needed) COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 26

AESI Certification Process – Integrated Complex Systems • • Regulatory / Industry guidance: • Complex integrated systems certification, using: • • • DO-297, TSO-C 153 / functional TSO / non-TSO functions, IMA ETSO (in creation) ARP-4754/4754 A, ARP-4761, DO-160, DO-178 B/C, DO-254 Audits: System Reviews, SOI Process Assurance / Suppliers oversight • Other compliance activities as required by: • • Aircraft / program Certification Plan(s) Other certification documents/plans (system, safety, SW and hardware, as described in the previous slides) • Meetings / discussions / audits / compliance agreements with the certification authorities: • • • CAAC (China) Direct contacts in defining and reviewing the cert process for C 919 FCS FAA, EASA/EUROCAE/FOCA, ANAC, TCCA. COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 27

AESI Process Assurance Expertise • Process Assurance: • Create and perform • Processes, guidances and process documents/work instructions/checklists • Process deployment • Internal • Coordination with customers and/or suppliers, • Coordination with certification authorities and military customers • Audits • Design audits (create the audits checklists and other materials) • Compliance Validation & Verification audits • Systems audits • Software audits • Safety reviews • Process assurance audits at suppliers • Training COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 28

AESI Training Capabilities and Expertise • Training • • • • Basic Certification Training FAA/EASA/CAAC regulations, compliance process and organization Systems ARP-4754 A Basic Advanced Safety ARP-4761 Integrated complex systems DO-297 Flight Controls integration and certification Pilots Ground School and Flight Training US based pilots licenses approval Ground/Flight Training for modified aircraft systems (STCs, Field Approvals) COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED. Page 29

AESI References Copyright 2016 AESI. All rights reserved.

AESI Main Companies Design References • Systems Design and Production: • Rockwell – Collins • • • • Tom Olson – Systems Integration Department Manager Mary Little – TSO Specialist Steve Wilson – Systems Certification Lead Warren Prashun – Systems Safety Lead GE: Mike Little – Chief Design Engineer, display systems Vahid Navidi – Engineering Director, GE Shanghai Michael Abourizk – Systems Integration Lead Dr. Mohamed Eladl – FCS Design Lead Honeywell: Victor Valente – Avionics Business VP Vojislav Soronda – FCS expert Uros Terzic – Avionics Application Lead for C 919 Rod Beal – Systems Director on site in Xian Welsh Pond – FCS design lead Milos Kafka – Design Director, Czech Republic Copyright 2016 AESI. All rights reserved. Page 31

AESI Main Companies Design References • OEMs: • Boeing: • • • • John Dalton – Safety Fellow Steve Beland – Systems Integration and FCS fellow Daniel Fogarty – System integration lead Richard Herald – AR coordinator Airbus: Anne Jany – Certification Director Chris Lacey – Systems and Safety lead engineer Nicholas Olivier – Safety Systems Manager Embraer: Marco Tulio Grassi – Product Integrity/Certification VP Marcos Viana Tavares – Senior Manager, Systems Integration Ney Moscati – Manager, Flight Controls team Emilio Matcushito – VP, Chief Engineering Copyright 2016 AESI. All rights reserved. Page 32

AESI Certification Authorities References • FAA key references: • • • Kirk Baker (AIR-120) Lihn Lee (TAD) – Safety Section head Peter Scaves (TAD) – National resource, systems Daniel Bui, Brett Portwood (LAACO) – Safety, systems, SW experts Thomas Phan – Mechanical Systems Expert • EASA key references: • • Wilhelm Runge – Avionics Section Manager Jean Baron, Kevin Hallworth – system/safety experts Frans Van Gorkum – human factors expert Pipa Van More, Gauillome Soudian – SW experts Alexandra Florin – System Safety expert, ARP-4754 A focal Christian Gunitzberger – Program Manager, large airplanes Charles Leboeuf – Project Manager – large airplanes Copyright 2016 AESI. All rights reserved. Page 33

AESI Summary and Conclusions COPYRIGHT 2016 AESI. ALL RIGHTS RESERVED.

AESI Summary • Based on expertise and experience presented in the previous slides, AESI is offering: • Full support for systems development and certification effort for aircraft program or system supplier • Includes integration with other aircraft systems such as avionics, FCS/AFCS, electrical, mechanical • Work remotely and on-site with customer, as needed • • • AESI has representation in China Conveniently located in USA (Phoenix, Arizona) for coordination with other USA based suppliers and FAA Strong connections with European aerospace industry and EASA • Create Statement of Work and coordinate project milestones with customer’s Integrated Master Schedule • Coordinate all development and certification activities with equipment suppliers and CAAC/FAA/EASA • Complete AESI support to the program will be within the export license approval/restrictions as required by the USA government • Equivalent Chinese government restrictions will be fully respected and followed by AESI Copyright 2016 AESI. All rights reserved. Page 35