Boeing Mechanical Engineer Resume Keywords (2026): 60+ ATS Skills for Aerospace ME Roles
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Not getting Boeing mechanical engineering interviews? Your resume is missing aerospace-specific keywords.
Boeing's ATS scans for terms like CATIA V5, Structural Analysis, and Composite Materials before a recruiter ever sees your resume. Generic mechanical engineering terms like "CAD" or "FEA" are not specific enough.
Boeing mechanical engineers earn $84K to $174K annually (Source: Levels.fyi). But first, your resume needs to pass the ATS.
What Are Boeing Mechanical Engineer Resume Keywords?
Boeing mechanical engineer resume keywords are the specific CAD tools, analysis methods, aerospace standards, and manufacturing processes that Boeing's ATS and recruiters search for when reviewing mechanical engineering candidates.
Unlike generic mechanical engineering keywords, Boeing roles require aerospace-specific terminology:
- CAD Systems: CATIA V5/V6, NX, SolidWorks, AutoCAD
- Analysis Software: NASTRAN, ANSYS, Hypermesh, Patran
- Aerospace Standards: AS9100, FAA Regulations, MIL-STD, ITAR
- Materials: Composite Materials, Carbon Fiber, Aluminum Alloys, Titanium
- Methods: GD&T, Tolerance Stack-up, Fatigue Analysis, Damage Tolerance
If your resume says "performed FEA" without specifying NASTRAN, ANSYS, or aerospace load cases, Boeing's ATS will likely filter you out.
Boeing Mechanical Engineer Salary (2026)
Before diving into keywords, here is what Boeing pays mechanical engineers (Source: Levels.fyi):
| Level | Title | Base Salary | Total Compensation |
|---|---|---|---|
| L1 | Engineer I | $84,000 | $86,000 |
| L2 | Engineer II | $95,000 | $98,000 |
| L3 | Senior Engineer I | $110,000 | $115,000 |
| L4 | Senior Engineer II | $135,000 | $145,000 |
| L5 | Principal Engineer | $155,000+ | $165,000-$174,000 |
Manufacturing Engineers: $79K to $141K (Source: Levels.fyi)
Tooling Engineers: Average $103K, 15% above national average (Source: Indeed)
60+ Boeing Mechanical Engineer Resume Keywords (2026)
CAD and Design Tools
CATIA is Boeing's primary design system. List your proficiency level and version.
| Tool | Vendor | When to Use |
|---|---|---|
| CATIA V5/V6 | Dassault Systemes | All Boeing aircraft design, primary CAD |
| NX (Siemens NX) | Siemens | Defense programs, some commercial |
| SolidWorks | Dassault Systemes | Tooling, fixtures, smaller components |
| AutoCAD | Autodesk | 2D drawings, legacy documentation |
| CREO (Pro/E) | PTC | Supplier components, some programs |
Related Keywords:
- 3D Modeling, Part Design, Assembly Design, Surface Modeling
- Drafting, GD&T Annotation, Drawing Creation
- Design for Manufacturing (DFM), Design for Assembly (DFA)
Example bullet:
"Designed 787 Dreamliner wing structural components using CATIA V5, creating 200+ part models and 50+ assembly drawings with full GD&T annotation per ASME Y14.5."
Structural Analysis and FEA
Boeing mechanical engineers perform extensive structural analysis. These keywords are critical.
| Category | Keywords |
|---|---|
| FEA Software | NASTRAN (MSC/NX), ANSYS, Abaqus, LS-DYNA |
| Pre/Post Processors | Hypermesh, Patran, FEMAP, ANSA |
| Analysis Types | Static Analysis, Dynamic Analysis, Fatigue Analysis, Damage Tolerance |
| Structural Concepts | Stress Analysis, Load Analysis, Margin of Safety, Factor of Safety |
| Advanced Analysis | Buckling, Vibration, Modal Analysis, Thermal Analysis, Crash/Impact |
Example bullet:
"Performed fatigue and damage tolerance analysis for 737 MAX fuselage structure using NASTRAN and Patran, demonstrating compliance with FAR 25.571 and achieving positive margins of safety across all load cases."
Materials and Manufacturing
Boeing uses advanced materials requiring specialized knowledge.
| Category | Keywords |
|---|---|
| Composites | Composite Materials, Carbon Fiber (CFRP), Fiberglass, Honeycomb Core |
| Metals | Aluminum Alloys (2024, 7075), Titanium, Inconel, Steel |
| Composite Processes | Autoclave Processing, Out-of-Autoclave (OOA), Layup, Cure Cycle |
| Metal Processes | CNC Machining, Sheet Metal Forming, Welding, Heat Treatment |
| Fastening | Riveting, Hi-Lok, Lockbolt, Blind Fasteners, Bonding, Adhesives |
787 Dreamliner fact: The 787 is approximately 50% composite by weight, making composite experience highly valuable for Boeing commercial aircraft roles.
Example bullet:
"Led design of composite wing skin panels for 787 Dreamliner using carbon fiber/epoxy prepreg, optimizing ply orientation and drop-off sequences to reduce weight by 12% while meeting damage tolerance requirements."
Aerospace Standards and Compliance
Every Boeing mechanical engineer must understand aerospace regulations and quality standards.
| Category | Keywords |
|---|---|
| Quality Standards | AS9100, ISO 9001, Quality Management System (QMS) |
| FAA Regulations | FAA Regulations, FAR Part 25, Airworthiness, Type Certificate |
| Military Standards | MIL-STD, MIL-HDBK-5, MIL-HDBK-17, JSSG (Joint Service Specification Guide) |
| Compliance | ITAR, Export Control, Regulatory Compliance |
| Documentation | Engineering Change Order (ECO), Drawing Release, Configuration Management |
Example bullet:
"Ensured AS9100 compliance throughout design process, supporting FAA type certification for 777X wing design with zero audit findings."
GD&T and Tolerancing
Geometric Dimensioning and Tolerancing is fundamental for aircraft design.
| Category | Keywords |
|---|---|
| Standards | GD&T, ASME Y14.5, Geometric Tolerancing, Feature Control Frames |
| Tolerance Analysis | Tolerance Stack-up, Tolerance Analysis, Worst-Case Analysis, RSS Analysis |
| Inspection | CMM (Coordinate Measuring Machine), First Article Inspection (FAI), Dimensional Inspection |
| Concepts | Datum Reference Frame, Position Tolerance, Profile Tolerance, Flatness, Perpendicularity |
Example bullet:
"Performed tolerance stack-up analysis for wing-to-fuselage interface using 3DCS and ASME Y14.5 GD&T, achieving assembly fit within 0.010" tolerance across 50+ mating features."
PLM and Data Management
Boeing uses enterprise systems to manage design data.
| Category | Keywords |
|---|---|
| PLM Systems | Teamcenter, Windchill, Enovia, Product Lifecycle Management (PLM) |
| Data Management | Product Data Management (PDM), Configuration Management, Version Control |
| Workflow | Engineering Change Order (ECO), Drawing Release, Approval Workflow |
| Collaboration | Cross-Functional Collaboration, Supplier Integration, IPT (Integrated Product Team) |
Example bullet:
"Managed design releases through Teamcenter PLM, processing 100+ Engineering Change Orders (ECOs) and coordinating configuration control across 5 supplier teams."
Boeing Programs and Aircraft
Mentioning specific Boeing programs demonstrates relevant domain experience.
| Category | Programs |
|---|---|
| Narrow-Body Commercial | 737, 737 MAX, 737-800, 737-900, 757 |
| Wide-Body Commercial | 787 Dreamliner, 777, 777X, 767, 747-8 |
| Military Fixed-Wing | F/A-18 Super Hornet, F-15EX, EA-18G Growler, P-8 Poseidon |
| Military Rotorcraft | AH-64 Apache, CH-47 Chinook, MH-139 Grey Wolf |
| Tanker/Transport | KC-46 Pegasus, C-17 Globemaster III, KC-135 |
| Space | Space Launch System (SLS), CST-100 Starliner, International Space Station (ISS) |
Example bullet:
"Designed thrust reverser structural components for 777X using CATIA V5 and NASTRAN FEA, achieving 15% weight reduction while maintaining structural margins."
👉 Applying to Boeing mechanical engineering roles? Make sure your resume includes the right aerospace keywords.
Role-Specific Keyword Sets
Structural Engineer Keywords
| Category | Keywords |
|---|---|
| Core | Structural Analysis, Structural Design, Load Paths, Structural Integrity |
| Analysis | Stress Analysis, Fatigue Analysis, Damage Tolerance, Static Strength |
| Methods | Finite Element Analysis (FEA), Hand Calculations, Margin of Safety |
| Regulations | FAR 25.571, Fatigue and Damage Tolerance Evaluation, Fail-Safe Design |
Design Engineer Keywords
| Category | Keywords |
|---|---|
| Core | Detail Design, Conceptual Design, Preliminary Design, Design Optimization |
| CAD | CATIA V5, NX, SolidWorks, 3D Modeling, Surface Modeling |
| DFX | Design for Manufacturing (DFM), Design for Assembly (DFA), Producibility |
| Output | Engineering Drawings, BOM (Bill of Materials), Design Documentation |
Systems Integration Engineer Keywords
| Category | Keywords |
|---|---|
| Core | Systems Engineering, Systems Integration, Interface Control |
| Documents | Interface Control Document (ICD), System Requirements, Specifications |
| Methods | Requirements Flow-down, Verification and Validation (V&V), FMEA |
| Tools | DOORS, Jama, Model-Based Systems Engineering (MBSE) |
Test Engineer Keywords
| Category | Keywords |
|---|---|
| Core | Structural Testing, Environmental Testing, Certification Testing |
| Test Types | Static Test, Fatigue Test, Limit Load, Ultimate Load, Fail Test |
| Facilities | Test Lab, Load Frame, Iron Bird, Ground Test |
| Analysis | Test Correlation, Model Validation, Test Instrumentation |
Security Clearance for Defense Roles
Many Boeing mechanical engineering positions require security clearance.
| Category | Keywords |
|---|---|
| Clearance Levels | Secret Clearance, Top Secret, TS/SCI, Security Clearance Eligible |
| Export Control | ITAR Compliance, Export Control, EAR, Controlled Unclassified Information (CUI) |
Note: If you have active clearance, list it prominently at the top of your resume. If you are clearance-eligible (US citizen with clean background), include "Security Clearance Eligible" in your summary.
How to Integrate Keywords Into Your Resume
Strong Example: Keyword-Optimized Resume
Experience Section:
Senior Mechanical Engineer | Aerospace Contractor | 2019 - Present Security Clearance: Secret
- Designed wing leading edge structures for 787 Dreamliner using CATIA V5, creating 150+ detail parts and 25 assembly models with full GD&T per ASME Y14.5
- Performed static and fatigue analysis using NASTRAN and Hypermesh, demonstrating positive margins of safety for limit and ultimate load conditions per FAR Part 25
- Led composite design for carbon fiber wing skins, optimizing ply schedules and stacking sequences to achieve 10% weight savings while meeting damage tolerance requirements
- Managed tolerance stack-up analysis for 200+ assembly interfaces, ensuring fit within specification using worst-case and RSS methods
- Supported First Article Inspection (FAI) and AS9100 compliance, resolving 15 non-conformances through root cause analysis and corrective action
- Coordinated design releases through Teamcenter PLM, processing 50+ ECOs with zero release defects
Skills Section:
CAD: CATIA V5, NX, SolidWorks, AutoCAD Analysis: NASTRAN, ANSYS, Hypermesh, Patran, Hand Calculations Materials: Composite Materials (CFRP), Aluminum (2024, 7075), Titanium Standards: AS9100, FAR Part 25, MIL-HDBK-5, ASME Y14.5 GD&T Methods: Structural Analysis, Fatigue Analysis, Damage Tolerance, Tolerance Stack-up PLM: Teamcenter, Engineering Change Orders (ECO), Configuration Management Security: Secret Clearance, ITAR Compliance
Weak Example: Missing Keywords
Experience Section:
Mechanical Engineer | Company | 2019 - Present
- Designed aircraft parts using CAD
- Performed FEA analysis
- Worked with composites
- Created drawings
Why it fails:
- No specific CAD tool (CATIA? NX? SolidWorks?)
- No specific FEA software (NASTRAN? ANSYS?)
- No aerospace standards (AS9100, FAR Part 25)
- No Boeing programs or aircraft mentioned
- No metrics or quantifiable results
- Generic terms that do not pass ATS filters
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Ready to Apply to Boeing Mechanical Engineering Roles?
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Boeing mechanical engineers earn $84K to $174K. Do not let missing keywords keep you from getting the interview.