Mechanical Airframe Systems Design Specialist

Edge Group

Abu Dhabi

Sur place

AED 360 000 - 520 000

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Il y a 2 jours
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Résumé du poste

EDGE Group PJSC in collaboration with ADASI seeks a Mechanical Airframe Systems Design Specialist to own the design, integration, and validation of airframe subsystems for UAV platforms, including landing gear, fuel, ECS, hydraulics and actuation.

You will create 3D CAD models in CATIA/NX/SolidWorks, prepare manufacturing drawings and BOMs, perform analyses, ensure compliance with AS9100 and MIL-STD, and work with avionics, propulsion and flight controls to deliver airworthy solutions.

Qualifications

  • Bachelor's degree in Mechanical or Aerospace Engineering with 5+ years in aerospace mechanical design.
  • Proficiency in 3D CAD and PLM tools and working knowledge of AS9100 standards.

Responsabilités

  • Lead design, integration and validation of mechanical airframe systems (landing gear, fuel, ECS, hydraulics).
  • Develop 3D CAD models, drawings and BOMs for UAV platforms.
  • Perform structural, hydromechanical and thermal analyses to verify designs.
  • Collaborate with avionics, propulsion and flight-control teams for proper integration.
  • Ensure airworthiness compliance and support prototype tests and flight trials.

Connaissances

3D CAD modeling
GD&T
Cross-functional collaboration
Problem-solving

Formation

Bachelor's in Mechanical or Aerospace Engineering
Master's preferred

Outils

CATIA
NX
SolidWorks
FEA
CFD

Description du poste

Mechanical Airframe Systems Design Specialist

Date: 23 Sept 2026

Company: EDGE Group PJSC

External Job Description

Position - Mechanical Airframe Systems Design Engineer – Landing Gear, Fuel System, ECS, Hydraulics & Actuation

Entity : ADASI

Key Responsibilities
  • Lead and take ownership for the design, integration, and validation of mechanical airframe systems, including landing gear assemblies, fuel distribution systems, ECS, hydraulic circuits, and actuation mechanisms for UAV platforms.
  • Develop 3D CAD models, detailed engineering drawings, and manufacturing documentation using industry-standard tools (e.g., CATIA V5/V6, Siemens NX, or SolidWorks).
  • Perform structural, hydromechanical and thermal analyses to ensure system integrity and correct sizing under operational loads and environmental conditions.
  • Collaborate with cross-functional teams—avionics, propulsion, flight controls—to ensure seamless system integration.
  • Define system requirements, interface control documents (ICDs), and bill of materials (BOMs) in compliance with aerospace standards (e.g., MIL-STD, RTCA DO-160).
  • Support prototype builds, ground tests, and flight trials, troubleshooting and resolving design issues in real time.
  • Ensure compliance with airworthiness regulations and defense sector quality standards.
  • Drive continuous improvement initiatives to enhance system performance, manufacturability, and maintainability.
Educational background
  • Bachelor’s degree in Mechanical or Aerospace Engineering (Master’s preferred).
  • Minimum 5 years experience in aerospace mechanical systems design, with proven expertise in at least three of the following: landing gear, fuel systems, ECS, hydraulics, actuation.
Professional Experience
  • Proficiency in 3D CAD and PLM systems (CATIA, NX, or equivalent).
  • Strong understanding of aerospace materials, manufacturing processes, and GD&T.
  • Knowledge of hydraulic and pneumatic system design, fuel system architecture, and ECS thermodynamics.
  • Familiarity with finite element analysis (FEA) and computational fluid dynamics (CFD) tools.
  • Standards & Compliance: Experience with aerospace and defense standards (e.g., AS9100, MIL-STD, DO-160).
  • Soft Skills: Strong problem-solving ability, cross-disciplinary collaboration, and clear technical communication.
Technical Skills
  • Professional Engineer (PE) or Chartered Engineer (CEng) status.
  • EASA Part 21 or GCAA Design Organisation Approval (DOA) exposure.
  • Certification in Systems Engineering (INCOSE ASEP/CSEP) or Project Management (PMP/PRINCE2).
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