Associate System Engineer – Elect Power System

Job Description

Position Responsibilities:

Demonstrate excellence in Development and Review of high-integrity electric/network systems requirements, preferably in Aerospace domain.
Demonstrate excellence in Electrical Power System development & certification; System design, integration testing and hardware unit level testing.
Demonstrate excellence in development Assurance (ARP4754A);
Create Interface control Drawings, understand wiring diagrams, mechanical 2D/3D design models
Develop System test procedures.
Should perform or able to Review System level DO 254/DO178C compliant System level testing
Perform Requirements Management in DOORS.
Evaluates customer/operational needs to define and coordinate system performance requirements, functional requirements and regulatory requirements.
Applies an interdisciplinary, collaborative approach to plan, design, develop and verify a lifecycle balanced system of systems and system solutions.
Coordinates with engineering functions to define requirements related to safety, reliability, maintainability, testability, human systems integration, survivability, vulnerability, susceptibility, system security, regulatory, certification, product assurance and other specialty engineering groups.
Develops the planning, organization, implementation and monitoring of requirements management processes, tools, risk, issues, opportunity management and technology readiness assessment processes.
Resolves cross-functional technical issues.
Present requirement, design and/or development revision and changes to formal change boards.
Tests and validates to ensure system designs meet operational and functional requirements
Basic Qualifications (Required Skills/Experience):

Capable of developing and independently reviewing system requirements for Electrical Power systems; Electrical Power systems development & certification;
Very Good understanding of DO 254/DO178C/ARP4754A/ARP4761 standards is mandatory
Strong knowledge in DO 160 Standards / MIL STD 704 & MIL STD 461 requirement is required
Systems testing knowledge and Hands on experience in using test equipment’s is mandatory
Exposure to development of DO 160 Qualification test procedures, hardware test procedures is preferred
Hands on Experience on IBM Rational DOORS in Requirements Management is required
Good experience on System design ofAvionics LRU components is preferred
Familiarity of Reliability calculations such as FMEA, FTA and Reliability Tools is an added advantage
Familiarity with airplane power generation systems is preferred
Strong Written, verbal communication with engineers, management, and non-engineering support staff
Experience in working with suppliers or other external stakeholders is preferred
Ability to work in a virtual team environment
INCOSE certification on Systems Engineering is an added advantage
Detailed knowledge of FAA certification and airworthiness requirements is highly desired.
Preferred Qualifications (Desired Skills/Experience):

Must have a minimum of 3 years’ experience in test planning, setup, test development, execution, conducting tests in a lab or production environment
Must have a minimum of 1 year experience in performing design, integration, and/or testing on avionics sub-systems, performing environmental testing (for example, Thermal Cycling and Vibration)
Must have a minimum of 1 year experience with Test processes of Circuit Card Assemblies (CCAs)
Must have a minimum of 1 year experience with Automated Test Equipment (ATE) Setup/Programming