Software Engineer

Individuals will work with, and auditing our Suppliers, to assess compliance to airworthiness criteria for Flight Critical Computing Systems (software and hardware) used in military aircraft.

Basic Qualifications:
- At least 10 years of safety critical Computing System/Software/Hardware development, verification, or certification experience, in one or more of the following areas:
- Processing Hardware / Electronics, including Programmable Logic for FPGA or ASIC

#URGENT

Required Skills

Basic Qualifications:
- At least 10 years of safety critical Computing System/Software/Hardware development, verification, or certification experience, in one or more of the following areas:
- Processing Hardware / Electronics, including Programmable Logic for FPGA or ASIC
- Software (SW) Development including Architecture, Design, and Qualifications
o Experience designing, developing, verifying and/or certifying safety critical SW
o Experience designing, developing, verifying and/or certifying SW for Multicore processors
o Experience with SW Partitioning (e.g. ARINC653)
o Experience with SW build, load & CM process for airborne equipment
o Experience conducting MIL-HBK-516C and/or DO-178B/C (SOI) audits on SW
o Experience with Standards: RTCA DO-178C, Emerging Mil Standard, FAA CAST-32A, RTCA DO-331, RTCA DO-330, RTCA DO-332, ARINC Specification 653, RTCA DO-278A, FAA CAST-2, FAA CATS-12, FAA CAST-17, FAA CAST-19, FAA Order 8110.49 CHG2, RTCA DO-248C, Joint Software Systems Safety Engineering Handbook, FAA AC 20-115C
- Processing Hardware / Electronics:
o Experience designing, developing, verifying and/or certifying safety critical Electronic hardware & Firmware
o Experience with Programmable Logic Devices (PLDs) such as Field Programmable Gate Arrays (FPGAs) or Application Specific Integrated Circuits (ASICS).
o Experience conducting MIL-HBK-516C Airworthiness Assessments or DO-254 Stage of Involvement (SOI) audits on Complex (CEH) or Simple (SEH) Electronic Hardware
o Experience with Standards: RTCA DO-254, FAA Order 8110.105A, EASA-CM-SWCEH-001, MIL-STD-704F, RTCA DO-160E, MIL-STD-461, FAA AC 20-152, FAA CAST-30, FAA CAST-31
- System Processing Architecture (SPA)
o Architecture and Design of Safety Critical Systems & Subsystems for aircraft
o Development of Physical and Functional ICDs between Elements of the System
o Development of Safety Critical Thread Analysis (SCFTA) and Safety Interlocks (SI) Analysis
o Understanding of Computer Software Integrity Level CSIL used in MIL-HBK-516C and its relationship to Design Assurance Level (DAL) used in DO-178C and DO-254.
o Experience/familiarity with PLOC (Probability of Loss of Control) and PLOA (Probability of Loss of Aircraft) analyses
o Experience conducting MIL-HBK-516C Airworthiness Assessments or FAA/EASA Audits on systems and subsystems and associated System, Safety & Reliability artifacts
o Experience with Standards: MIL-HDBK-516C, AC-17-01, SAE ARP 4754A, MIL-STD-882E, MIL-NDBK-217, and JSSG-2008\

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Location

Melbourne, FL

Openings

1

Anticipated Start Date

Monday, May 9, 2022

Job Type

Contract

Anticipated Duration

12 Months

Date Posted

Thursday, April 21, 2022

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Elite Technical Services, Inc. is an equal opportunity employer and all qualified applicants will receive consideration for employment without regard to race, color, religion, sex, national origin, disability status, protected veteran status, or any other characteristic protected by law.