Aerospace engineer CVs have a tool problem and a certification problem that together cost more shortlisting opportunities than any other pair of issues in the discipline. The tool problem: most engineering programmes teach ANSYS Mechanical, but civil aviation primary structure substantiation is built on MSC Nastran — the FEA solver whose results EASA and FAA-approved Design Organisations accept in formal stress reports. A structures engineer CV that lists "ANSYS" without "Nastran" looks like a mechanical engineering CV that happens to mention aircraft. The certification problem: aerospace design work that goes on a type-certified aircraft must be substantiated to an airworthiness standard — CS-25 Amendment 27 for large transport category aircraft, FAR Part 25 for FAA, CS-27 for rotorcraft — and a stress report or systems analysis bullet that doesn't cite the applicable standard and amendment looks like it could describe a research model, a non-certified modification, or a prototype. Aerospace engineering in 2026 spans four major specialisations — aerostructures, aerodynamics/CFD, systems engineering, and propulsion — each with distinct tool sets, certification standards, and deliverable types, and each demands a different CV emphasis.

What Aerospace Engineer Job Descriptions Require in 2026

Aerospace JDs divide sharply across specialisation, and a CV that doesn't signal the right one will fail ATS for both:

Aerostructures (stress and structures): Structural analysis and design of aircraft and spacecraft primary and secondary structure. JDs specify: MSC Nastran (SOL 101 linear static, SOL 103 normal modes, SOL 105 buckling, SOL 106 nonlinear, SOL 111 dynamic frequency response) with Patran or HyperMesh for pre/post-processing; CATIA V5/V6 for 3D structural design; fatigue and fracture mechanics analysis (NASGRO, AFGROW); damage tolerance per CS-25.571 or FAR 25.571; margin of safety calculations to MMPDS (Metallic Materials Properties Development and Standardization, the successor to MIL-HDBK-5) or ESDU; and stress report preparation for EASA or FAA DOA review. Senior roles add composite laminate design and analysis (Classical Laminate Theory, CFRP allowables, impact damage tolerance), finite element model correlation with test, and Designated Engineering Representative (DER) or equivalent signatory authority.

Aerodynamics and CFD: External aerodynamics, drag analysis, high-lift systems, and intake/nozzle design. JDs specify: ANSYS Fluent, Star-CCM+, or OpenFOAM for RANS CFD; mesh generation (ICEM-CFD, Pointwise, or Fluent Meshing); turbulence modelling selection (k-ω SST for boundary layer-sensitive applications; SA-RC for high-lift); wind tunnel testing experience (model design, instrumentation, data reduction); and aerofoil design tools (XFOIL for subsonic, SU2 for adjoint-based optimisation in academic/research roles). CFD roles increasingly require Python scripting for post-processing (matplotlib, NumPy, paraview scripting) and HPC (high-performance computing) job submission experience.

Systems engineering (avionics and safety): Aircraft system development and certification. JDs specify: ARP 4754A (guidelines for development of civil aircraft and systems) for the system development process, ARP 4761 (guidelines and methods for conducting safety assessments) for FHA (Functional Hazard Assessment), PSSA (Preliminary System Safety Assessment), and SSA (System Safety Assessment), DO-178C (software considerations in airborne systems) for software development assurance, and DO-254 (design assurance guidance for airborne electronic hardware) for hardware. Safety assessment tools: OpenFTA (FTA), Isograph Fault Tree+ or CAFTA for probabilistic modelling. Avionics roles add ARINC 429 databus specification, MIL-STD-1553, and ARINC 653 (partitioned operating system for IMA — Integrated Modular Avionics).

Propulsion: Gas turbine performance, combustion, and turbomachinery design. JDs specify: GasTurb (industry-standard thermodynamic cycle analysis tool for gas turbines), NPSS (Numerical Propulsion System Simulation), MATLAB/Simulink for engine performance modelling, CFD for internal flow (turbine blade cooling, combustor flow), and familiarity with aero-engine certification standards (CS-E for EASA, FAR Part 33 for FAA).

Aerospace engineer salaries in 2026: £32K–£58K UK for graduate and junior; £55K–£90K for chartered engineers and senior analysts; £80K–£130K for principal engineers, DOA signatories, and DERs.

ATS Keywords for an Aerospace Engineer Resume

Aerospace ATS filtering uses solver names, certification standard numbers, and professional body credential abbreviations. Specialisation matters — keyword lists must be discipline-specific.

Essential ATS terms for an aerospace engineer resume:

  • Title variants: Aerospace Engineer, Senior Aerospace Engineer, Graduate Aerospace Engineer, Stress Engineer, Structures Engineer, Aerostructures Engineer, Loads Engineer, Systems Engineer (Aerospace), Avionics Engineer, Flight Mechanics Engineer, CFD Engineer, Aerodynamicist, Propulsion Engineer
  • Structures tools: MSC Nastran, NX Nastran, Patran, HyperMesh, Abaqus, OptiStruct, NASGRO, AFGROW, CATIA V5, CATIA V6, NX, 3DEXPERIENCE, ENOVIA, Windchill, Teamcenter
  • CFD tools: ANSYS Fluent, Star-CCM+, OpenFOAM, ICEM-CFD, Pointwise, XFOIL, SU2, HPC, k-ω SST, RANS, turbulence modelling
  • Systems and safety: ARP 4754A, ARP 4761, DO-178C, DO-254, ARINC 429, MIL-STD-1553, FHA, PSSA, SSA, FTA, FMEA, safety assessment, DAL, Design Assurance Level
  • Propulsion: GasTurb, NPSS, thermodynamic cycle, gas turbine, turbomachinery, combustion, MATLAB, Simulink
  • Certification standards: CS-25, FAR Part 25, CS-23, CS-27, CS-29, FAR Part 33, CS-E, EASA, FAA, DOA, CAA, type certificate, supplemental type certificate, STC, airworthiness
  • Quality and special processes: AS9100, AS9102, NADCAP, FAI, first article inspection, special processes, NDT
  • Structures analysis vocabulary: Margin of Safety, MS, ultimate load, limit load, proof load, fail-safe, damage tolerance, fatigue life, fracture mechanics, MMPDS, ESDU, allowables, composite, CFRP, laminate
  • Professional credentials: RAeS, MRAeS, AFRAeS, FRAeS, CEng, IEng, IMechE, IET
  • Long-tail phrases: aerospace engineer resume, aerospace engineer cv, how to write an aerospace engineer resume, stress engineer resume, aerospace engineer resume 2026, aerostructures engineer resume, CFD engineer resume, systems engineer aerospace resume, avionics engineer resume

Placement: Specialisation (Structures/CFD/Systems/Propulsion) in the headline — aerospace is too broad without it. MSC Nastran in the Skills section for structures roles — it is the primary ATS filter for aerostructures positions. CS-25 or relevant airworthiness standard in at least one experience bullet. RAeS membership grade (MRAeS, AFRAeS, FRAeS) plus CEng/IEng in the headline.

Aerospace Engineer CV Structure and Bullets That Show Certification Depth

Section order:

  1. Headline — "Aerospace Engineer | Aerostructures · Nastran · CATIA V5 · CS-25 · MRAeS CEng"
  2. Professional credentials — RAeS grade, CEng/IEng, DOA signatory authority if applicable
  3. Skills — FEA & Analysis / CAD & PLM / CFD (if applicable) / Certification Standards / Quality / Programming
  4. Experience — 4–5 bullets per role; analysis tool, certification standard cited, Margin of Safety or safety objective stated, DOA/EASA review outcome per bullet
  5. Education — MEng/BEng Aerospace Engineering (RAeS-accredited preferred); at bottom

Two pages for 5+ years. Certification standard with amendment in every certified aircraft analysis bullet. Margin of Safety stated in every structural analysis result. EASA DOA acceptance outcome (first review, second review) where applicable. Solver name and solution type (SOL 101, SOL 106, SOL 103) in every FEA bullet.

Three elements make an aerospace engineering bullet convincing: the analysis type and component (Nastran SOL 101 linear static, composite wing spar fitting), the certification context (CS-25 Amendment 27, MMPDS allowables), and the substantiation result (Margin of Safety +0.06 at ultimate load, DOA accepted on first review). Three examples:

  • Performed FEA stress analysis of a composite winglet attachment bracket for a regional turboprop — Nastran SOL 101 linear static analysis, 1.2M DOF model with Patran pre/post-processing, MMPDS-based material allowables for IM7/8552 CFRP laminate; CS-25 Amendment 27 compliance demonstrated, Margin of Safety +0.06 at ultimate load under 2.5g pull-up manoeuvre; stress substantiation report accepted by EASA-approved DOA on first review
  • Conducted RANS CFD analysis of nacelle-pylon aerodynamic interference on a narrow-body transport aircraft — ANSYS Fluent, k-ω SST turbulence model, structured mesh (14M cells, ICEM-CFD), cruise Mach 0.82 and ±2° angle-of-attack sweep; 3 pylon geometry configurations compared; recommended geometry achieved 8.3 drag count reduction vs baseline; CFD results validated against wind tunnel pressure data within 6% on section Cd at cruise condition
  • Led ARP 4761 system safety assessment for a fuel quantity measurement system STC modification — FHA identifying 4 failure conditions (1 catastrophic, 2 hazardous, 1 major), PSSA and SSA with FTA and FMEA for single-channel gauging loss, 1×10⁻⁹ per flight hour objective demonstrated for catastrophic failure condition; SSA package accepted by EASA Designated Avionics Engineer within 2 review cycles; modification embodied on 340 production aircraft under EASA STC

Aerospace engineer interviews include technical exercises (here is a box beam cross-section — calculate the shear flow distribution), certification scenario questions (walk me through how you'd substantiate a new bracket design for CS-25 compliance), and tools discussions (what Nastran solution sequence would you use for a dynamic response problem?). Your CV's tool specificity, certification standard citation, and margin of safety evidence determine whether the interview explores your engineering judgment or tests your academic knowledge.

Three Aerospace Engineer CV Mistakes That Lose the Certification Signal

Nastran not mentioned for aerostructures roles — ANSYS listed instead. MSC Nastran is the dominant FEA solver for primary aircraft structure substantiation in civil aviation. EASA-approved and FAA-approved Design Organisations submit stress reports with Nastran results — it is the accepted standard. ANSYS Mechanical is widely used in mechanical and automotive engineering but has very limited presence in civil aircraft primary structure work at the major primes and tier-1 suppliers. A structures engineer CV that lists only ANSYS sends the signal that the candidate's FEA experience is from non-aerospace or academic contexts. If you have used Nastran — even on a university project, an internship, or through self-study on the MSC One academic license — name it in the Skills section alongside the solution sequence (SOL 101 for linear static, SOL 103 for normal modes, SOL 105 for buckling). If you have used only ANSYS, say so honestly — but also demonstrate awareness of Nastran and signal that you are learning it.

Certification standard not cited with amendment despite work on type-certified aircraft. Aerospace is the most heavily regulated engineering discipline. Every structural, systems, or avionics analysis that substantiates a design feature on a type-certified aircraft must demonstrate compliance with a specific airworthiness standard and amendment: CS-25 Amendment 27 (the current amendment for large transport category aircraft), FAR Part 25 Amendment 154, CS-27/CS-29 for rotorcraft, CS-23 for general aviation. The amendment number matters — CS-25 has been amended multiple times, and the applicable amendment is specified in the Type Certificate Data Sheet. A CV that says "structural analysis for commercial aircraft" without citing the standard gives the recruiter no information about whether the analysis was substantiation-quality or exploratory. Add the standard and amendment to every bullet describing certified aircraft work: "CS-25 Amendment 27" or "FAR Part 25 Amendment 154" or "CS-27 Amendment 8". One line, but a significant signal.

Margin of Safety not quoted in structural analysis results. Margin of Safety (MS = Allowable/Applied - 1) is the fundamental result of aerospace structural analysis. It must be ≥ 0.0 at limit load and ≥ 0.0 at ultimate load for a structure to be substantiated — and a well-designed structure will have a positive but small MS (e.g. +0.04 to +0.12) indicating both compliance and weight efficiency. An analysis bullet that describes what was analysed and the tool used, but omits the Margin of Safety, is missing the result. "FEA stress analysis of a main landing gear trunnion fitting — Nastran SOL 101, Patran post-processing, aluminium alloy 7075-T7351 MMPDS allowables" reads like a description of work done. "FEA stress analysis of a main landing gear trunnion fitting — Nastran SOL 101, Patran, 7075-T7351 MMPDS allowables; CS-25 Am.27 compliance, MS +0.09 at ultimate load (3.0g landing); stress report accepted by DOA on first review" is the engineering evidence. Quote the Margin of Safety and the load case.

If you are applying to aerospace engineer, stress engineer, or aerostructures roles and want your CV rebuilt around the specific certification standards, analysis tools, and DOA requirements in a target job description, Resumegpt generates your aerospace engineer CV from your work history in under 60 seconds — Nastran and certification depth named, Margin of Safety evidenced, RAeS grade and CEng status stated, ATS-optimised, and exported as a PDF ready to submit.