ZipRecruiter

Log In

1

Senior Damage Tolerance Engineer Jobs (NOW HIRING)

Joby Aviation

Staff Airframe Stress Engineer

Santa Cruz, CA · On-site

$185K - $254K/yr

Overview Joby Aviation is seeking an experienced staff level Fatigue & Damage Tolerance (F&DT) engineer who believes in the ability of urban air mobility to positively impact our cities. This role is ...

Joby Aviation

Staff Airframe Stress Engineer

Santa Cruz, CA · On-site

$185K - $254K/yr

Overview Joby Aviation is seeking an experienced staff level Fatigue & Damage Tolerance (F&DT) engineer who believes in the ability of urban air mobility to positively impact our cities. This role is ...

AEVEX

Sr. Stress Engineer

Murrieta, CA · On-site

$60 - $82.25/hr

The Senior Stress Engineer at AEVEX Aerospace is responsible for analyzing primary & secondary ... Develops Fatigue & Damage Tolerance (F&DT) reports * Other functions may include basic thermal ...

Softcom Systems Inc

Stress Engineer

Wichita, KS · On-site

$58 - $70/hr

Stress Engineer - Aerospace Work Location with Zip code: Wichita, KS Minimum years of experience ... Detailed Perform Static, fatigue and damage tolerance analysis for Aircraft structures using ...

SOGECLAIR

Structural Design Engineer

Wichita, KS · On-site

Conduct finite element modeling (FEA), static stress, fatigue and damage tolerance, thermal, vibration, and structural analyses. Develop analytical models and engineering calculations to validate ...

SOGECLAIR

Structural Analysis Engineer

Wichita, KS · On-site

Conduct finite element modeling (FEA), static stress, fatigue and damage tolerance, thermal, vibration, and structural analyses. Develop analytical models and engineering calculations to validate ...

Softcom Systems Inc

Stress Engineer

Richardson, TX · On-site

$58 - $70/hr

Stress Engineer - Aerospace Work Location with Zip code: Richardson, TX Minimum years of experience ... Detailed Perform Static, fatigue and damage tolerance analysis for Aircraft structures using ...

Leidos

Senior Structural Engineer

Reston, VA · On-site

$104K - $142K/yr

Leidos is seeking a Senior Structural Engineer to serve as a recognized technical authority ... Damage Tolerance * Composite Materials * Mechanical Design * Proven ability to lead technical ...

AEVEX

Sr. Stress Engineer

San Diego, CA · On-site

$200K - $224K/yr

The Senior Stress Engineer at AEVEX Aerospace is responsible for analyzing primary & secondary ... Develops Fatigue & Damage Tolerance (F&DT) reports * Other functions may include basic thermal ...

SOGECLAIR

Structural Design Engineer

Wichita, KS · On-site

... damage tolerance, thermal, vibration, and structural analyses. • Develop analytical models and engineering calculations to validate structural designs. • Support structural sizing and ...

next page

Showing results 1-20

All JobsDamage Tolerance Engineer JobsSenior Damage Tolerance Engineer Jobs

Senior Damage Tolerance Engineer information

See salary details

$59.5K

$126.6K

$183.5K

How much do senior damage tolerance engineer jobs pay per year?

As of Aug 1, 2026, the average yearly pay for senior damage tolerance engineer in the United States is $126,557.00, according to ZipRecruiter salary data. Most workers in this role earn between $104,500.00 and $143,500.00 per year, depending on experience, location, and employer.

What are Senior Damage Tolerance Engineers?

Senior Damage Tolerance Engineers are specialized professionals who assess and predict the structural integrity and lifespan of materials and components, particularly in aerospace and automotive industries. They analyze how cracks, flaws, and other damage can affect the strength and safety of structures over time. Using advanced analytical methods and simulation tools, they help ensure that products meet safety standards and regulatory requirements. Their expertise is critical for maintaining the safety and reliability of aircraft, spacecraft, and other complex systems.

What are the key skills and qualifications needed to thrive as a Senior Damage Tolerance Engineer, and why are they important?

To thrive as a Senior Damage Tolerance Engineer, you need a deep understanding of fracture mechanics, fatigue analysis, and materials science, usually supported by an engineering degree and significant aerospace industry experience. Expertise with finite element analysis (FEA) software, damage tolerance assessment tools, and familiarity with industry standards and certification processes is essential. Strong problem-solving, attention to detail, and effective communication skills help you interpret complex data and collaborate with cross-functional teams. These skills and qualities are crucial for ensuring aircraft structural integrity and safety while meeting regulatory and operational requirements.

What is the difference between Senior Damage Tolerance Engineer vs Damage Tolerance Engineer?

AspectSenior Damage Tolerance EngineerDamage Tolerance Engineer
QualificationsTypically requires 5+ years experience, advanced certificationsEntry to mid-level, relevant engineering degrees
ResponsibilitiesLeading damage assessments, overseeing projects, mentoringPerforming damage analysis, supporting design and testing
Work EnvironmentDesign offices, testing labs, aerospace or defense industriesDesign offices, testing labs, aerospace or defense industries

The main difference is experience level and responsibility. Senior Damage Tolerance Engineers lead damage assessments and mentor teams, while Damage Tolerance Engineers focus on analysis and supporting project tasks. Both roles are vital in aerospace and defense sectors, requiring similar credentials and work environments.

What are some common challenges faced by Senior Damage Tolerance Engineers when evaluating aircraft structural integrity?

Senior Damage Tolerance Engineers often encounter challenges when analyzing complex stress and fatigue data, especially for aging aircraft or when new materials are involved. Balancing safety margins with weight and cost constraints requires careful judgment and up-to-date knowledge of regulatory standards. Collaboration with design, materials, and maintenance teams is crucial to ensure that repairs and modifications meet both safety and operational requirements. Staying current with evolving industry guidelines and advanced simulation tools is also essential for success in this role.
What cities are hiring for Senior Damage Tolerance Engineer jobs? Cities with the most Senior Damage Tolerance Engineer job openings:
What are the most commonly searched types of Damage Tolerance Engineer jobs? The most popular types of Damage Tolerance Engineer jobs are:
What states have the most Senior Damage Tolerance Engineer jobs? States with the most job openings for Senior Damage Tolerance Engineer jobs include:
Senior Damage Tolerance Engineer jobs near you
Infographic showing various Senior Damage Tolerance Engineer job openings in the United States as of July 2026, with employment types broken down into 90% Full Time, 9% Part Time, and 1% Contract. Highlights an 99% Physical, and 1% Remote job distribution, with an average salary of $126,557 per year, or $60.8 per hour.

Lead, Aircraft Fatigue and Damage Tolerance Engineer

L3HHCM20

Waco, TX • On-site

Other

Posted 16 days ago

Job description

Job Title: Lead, Aircraft Fatigue and Damage Tolerance Engineer
Job Code: 40917
Job Location: Waco, TX (Onsite)
Job Schedule: 9/80


Job Description:

L3Harris MMG Division is seeking an experienced Aircraft Fatigue and Damage Tolerance Engineer for our onsite aircraft modification facility located in Waco, TX. We offer competitive benefits and a generous relocation package for those who qualify.


The Aircraft Fatigue and Damage Tolerance Engineer will be responsible for performing structural fatigue and damage tolerance analysis of aircraft modifications, including design support, and preparation of technical documentation necessary to ensure airworthiness.  This includes identification of critical load paths in primary aircraft structure resulting from applied and induced operational loads, as well as the determining the local stress concentrations, internal fastener load distributions, operational usage environments and design allowables. Additional responsibilities include development of tailored mission profiles and usage spectra for modified aircraft for use in calculation of service life.


Essential Functions:

  • Fatigue analysis of aircraft structures.
  • Crack growth analysis of aircraft structures.
  • Development of specific mission profiles and usage spectrum for modified aircraft.
  • Determination of inspection intervals for delivered aircraft.
  • Design support and drawing review.
  • Ability to generate free body diagrams, determine reaction forces, calculate internal load distributions, local stress concentrations, and operational usage environments.
  • Willingness and ability to travel as necessary.
  • Ability to obtain and maintain a Secret security clearance.
  • Willingness and ability to work any shift, weekends, and overtime as required.
  • Willingness to mentor less experienced engineers.
  • Effective and demonstrated leadership qualities.


Qualifications:

  • Bachelor's Degree in Mechanical Engineering, Aerospace Engineering, Civil Engineering and minimum 9 years of prior relevant experience. Graduate Degree (MSME, MSAE) and a minimum of 7 years of prior aircraft structural dynamics related experience. In lieu of a degree, minimum of 13 years of prior related experience.
  • Must be a US citizen.


Preferred Additional Skills:

  • Active security clearance.
  • Experience with predicting crack initiation lives and running industry-standard crack growth programs; e.g., AFGROW, NASGRO.
  • Working knowledge of one programming language.
  • Working knowledge of both military (Mil Standard) and civilian (14 CFRs) certification regulations and generating substantiation data to demonstrate compliance.
  • Working knowledge on how to develop the Airworthiness Limitations section of the Instructions for Continued Airworthiness for a structural modification.
  • Experience with standard Nondestructive Inspection (NDI) methods and corresponding crack growth detectable flaw sizes.
  • Experience with Dynamic Response Fatigue Analysis (High-Cycle Fatigue) due to high vibration environments and/or acoustic fatigue stresses.
  • CAD or analysis (FEA) tools exposure, and/or experience in mechanical design or analysis structures and mechanisms.
  • Familiarity with transducer instrumentation, data collection and or automation and software programming for numerical analysis.
  • Proficient in Microsoft Office, and have general computer knowledge.
  • Excellent verbal and written communication skills.

#LI-AS1

Apply