Aerotek Systems Engineer in GOLDSBORO, North Carolina
Responsible for various multi-disciplinary engineering tasks related to aircraft cargo handling systems with emphasis on functional analysis, requirements management, safety assessment and product reliability. Support development of aircraft cargo loading system with emphasis on structural integrity, customer specification and airworthiness of the product.
• Support design of aircraft cargo loading, cargo handling and aerial delivery systems with emphasis on system functionality, integrity, availability, performance and airworthiness to ensure flight safety and Part 25 certification • Prepare and review System Concept of Operations • Establish and manage high-level and low-level requirements for aircraft cargo loading, cargo handling and aerial delivery systems • Generate system deliverables and artifacts per ARP4754 • Perform safety assessment process in accordance with ARP4761, including but not limited to, Functional Hazard Assessment (FHA), System Safety Assessment (SSA), Fault Tree Analysis (FTA), Common Mode Analysis (CMA) • Conduct, analyze the results and document simulation laboratory tests of cargo handling and aerial delivery control systems • Support flight test activities, including troubleshooting, validation and verification of cargo handling and aerial delivery control systems • Work with the Electrical Systems team to successfully develop the aerial delivery control system to DO-254 and DO-178 DAL A requirements • Create, review and approve of technical documents reports covering the following topics: o System Description o System Safety Assessment o System Integration o System and Equipment Specifications o System and Equipment Compliance Documents o Environmental performance verification and qualification per DO-160, MIL-STD-810 o Dynamic and Thermal Analyses o Root Cause Analysis and Corrective Action Requests (RCCA) o Detail and Assembly Drawings per ANSI Y14.100, including advancing the use of Model o Change Requests and Change Orders
Top Skills Details:
Design electromechanical systems for aircraft Safety & reliability to Aviation standards Technical document generation Dynamic and Thermal Analysis
Additional Skills & Qualifications:
• Minimum: Bachelor of Science degree (B.S.) in Mechanical or Aeronautical/Aerospace Engineering from a four-year college or university • Master of Science degree (M.S.) in Mechanical or Aeronautical/Aerospace Engineering or related field of study is an asset • Knowledge of ARP4761 and ARP4754 • Intermediate Experience with IBM DOORS and CAFTA or similar Fault Tree Analysis tools • Knowledge of aircraft mechanical and electro-mechanical systems • Knowledge of reliability engineering theory • Experience in the troubleshooting of mechanisms in the context of the development cycle • Experience in the certification of mechanical and electro-mechanical components for civil or military aerospace applications • Software Safety experience is an asset • Experience in the creation, publication, and revision of engineering drawings in accordance with ANSY Y14.100 standards • Intermediate Experience with SolidWorks toolset or equivalent
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