5 A&P Engineer Job Description Templates and Examples

Company Overview

[$COMPANY_OVERVIEW]

Role Overview

Join the [$COMPANY_NAME] airframe & powerplant engineering team as a Junior A&P Engineer, where you’ll support the certification, modification, and sustainment of turbine-powered aircraft under 14 CFR Parts 23, 25, 27, and 29. Working alongside DERs, ODA UM/ARs, and senior engineers, you’ll translate field maintenance data, service bulletins, and STC packages into production-ready work instructions while building a rock-solid foundation in structural analysis, powerplant integration, and FAA conformity processes.

Responsibilities

• Prepare elementary stress analyses and fatigue check sheets for metallic and composite repairs using classical hand calculations and Siemens Femap / NASTRAN.
• Generate engineering authorizations (EAs), repair sketches, and conformity inspection plans that comply with FAA AC 43.13-1B and the latest issue of [$COMPANY_NAME] Design Manual.
• Review OEM service bulletins, airworthiness directives, and STC data kits; extract relevant instructions and create clear, concise work cards for line and base maintenance teams.
• Support on-wing powerplant troubleshooting by collecting engine trend data, borescope findings, and oil-debris samples; summarize results in concise engineering reports.
• Coordinate with supply-chain and production control to ensure parts and materials meet TSO/PMA compliance and are properly documented on FAA Form 8130-3 tags.
• Participate in MRB and FRB meetings, document non-conformance dispositions in Corridor or similar MRO software, and track corrective actions to closure.
• Conduct fit-checks and functional tests on prototype installations; capture dimensional data with FARO Arm or laser tracker and update 3-D CATIA / SolidWorks models.
• Maintain strict revision control in [$COMPANY_NAME] PLM system (Teamcenter or ENOVIA) and ensure all deliverables meet DO-178C and DO-160G configuration standards.
• Shadow senior DERs during FAA conformity inspections and learn to prepare 8110-3 compliance statements for minor & major alterations.

Required Qualifications

• 1–3 years of hands-on experience in civilian or military aviation maintenance, manufacturing, or modification environment.
• FAA Airframe & Powerplant (A&P) certificate active and in good standing.
• Associate degree in Aerospace, Mechanical, or Aviation Technology (B.S. in progress acceptable).
• Fundamental understanding of 14 CFR Parts 21, 23, 25, 33, 43, and 91 regulatory framework.
• Working knowledge of aircraft structural materials (2024, 7075, Ti-6Al-4V, carbon/epoxy) and common corrosion types.
• Proficiency with Microsoft 365 (Excel, Word, Teams) and basic CAD navigation; CATIA V5 experience preferred.
• U.S. person status due to export-controlled hardware and ITAR requirements.
• Ability to lift 35 lbs, work from heights up to 40 ft on man-lifts, and pass FAA/DOT drug screening.

Preferred Qualifications

• B.S. in Aerospace or Mechanical Engineering (ABET-accredited) or graduation within 12 months.
• Experience with turbine engines (CF34, PW100, PT6, or similar) including borescope interpretation and vibration analysis.
• Familiarity with fatigue analysis tools: NASGRO, AFGROW, or equivalent crack-growth software.
• Basic scripting in MATLAB or Python for data reduction and test-cell performance plots.
• Completion of an OEM structural repair course (e.g., Boeing 737/787, Airbus A320/A350).
• Knowledge of additive manufacturing (metal & polymer) for rapid-repair prototyping.
• Six Sigma Yellow Belt or equivalent continuous-improvement training.

Technical Skills and Relevant Technologies

• Stress & fatigue: classical hand analysis, FEM preprocessing, and NASTRAN solver setup.
• CAD: CATIA V5, SolidWorks, or Siemens NX for part modeling and assembly clash detection.
• PLM & MRO: Teamcenter, ENOVIA, Corridor, TRAX, or SAP MRO for configuration control.
• Documentation: FAA Forms 337, 8110-3, 8130-3; ability to read Wiring Diagram Manuals (WDM) and Illustrated Parts Catalogs (IPC).
• Engine diagnostics: Engine Condition Trend Monitoring (ECTM), oil-analysis interpretation, vibration spectrum review.
• Standard tools: micrometers, strain gauges, load cells, FARO Arm, Artec 3-D scanner.

Soft Skills and Cultural Fit

• Natural curiosity—asks “why” and digs into root causes before proposing fixes.
• Clear technical communicator; can explain rivet spacing rationale to AMTs in the hangar and sketch a free-body diagram for stress engineers in the office.
• Detail-oriented: catches missing fastener call-outs and verifies torque values against latest revision.
• Safety-first mindset—willing to stop the line for a potential crack indication.
• Collaborative: partners respectfully with inspectors, production, and program management under tight turnaround pressures.
• Growth attitude—actively seeks feedback and logs training hours toward DER/UM credential roadmap.

Benefits and Perks

Compensation: [$SALARY_RANGE] + overtime eligible + 10% annual bonus potential.

• Medical, dental, vision coverage effective day one; zero-premium HDHP option.
• 401(k) with 6% company match, immediate vesting.
• Tool allowance: $1,000/year plus company-issued electronic torque wrench set.
• Professional development: paid A&P recurrent training, DER mentoring program, and tuition reimbursement up to $10 k/year.
• Flight benefits: standby travel on [$COMPANY_NAME] cargo and passenger routes after 6 months.
• Relocation assistance for candidates moving >50 mi to [$COMPANY_LOCATION].

Equal Opportunity Statement

[$COMPANY_NAME] is an Equal Opportunity Employer. We celebrate diversity and are committed to creating an inclusive environment for all employees. All qualified applicants will receive consideration for employment without regard to race, color, religion, sex, sexual orientation, gender identity, national origin, disability, or veteran status.

Location

This position is based at [$COMPANY_LOCATION] with flexibility for hybrid schedules: three days on-site in the hangar/office and two days remote for analytical work. Occasional domestic travel to vendor or customer sites (≤15%).

Company Overview

[$COMPANY_OVERVIEW]

Role Overview

We’re looking for an A&P (Airframe & Powerplant) Engineer to own the structural integrity, maintainability, and certification compliance of [$COMPANY_NAME]’s next-generation aircraft. You’ll translate MRB, OEM, and regulatory guidance into engineering dispositions, create detailed repair schemes, and mentor junior engineers on fatigue-life management, corrosion-prevention programs, and fleet-wide reliability initiatives. If you love turning squawks into certifiable, data-driven solutions—and want your fingerprints on every flight hour—this role is for you.

Responsibilities

• Author and approve structural and mechanical engineering dispositions for line- and heavy-maintenance findings in accordance with 14 CFR §25.571, §25.613, and associated ACs.
• Develop fatigue-damage-tolerance analyses using NASGRO, AFGROW, or equivalent crack-growth software; substantiate repairs with static, fatigue, and damage-tolerance margins.
• Create 3D CAD-based repair drawings (CATIA v5/v6, SolidWorks, or NX) and pair them with classical hand calculations or FEA (NASTRAN, PATRAN, HyperMesh) for rapid AEG & DER concurrence.
• Lead multi-disciplinary MRB boards—collaborating with Structures, Systems, Interiors, and Avionics—to close findings within aircraft downtime windows.
• Drive fleet-wide reliability projects: convert AD/SB/SL data into predictive maintenance algorithms that reduce unscheduled removals by ≥15 %.
• Mentor junior engineers on MSG-3 logic, FAR repair classification, and novel composite repair techniques (autoclave, out-of-autoclave, bonded scarf, cold-bond).
• Interface directly with FAA/DERs and EASA/DOAs to obtain approved data (8110-3, 8100-9) and ensure continued operational safety assessments (COSA) are closed.
• Maintain digital thread traceability—linking inspection findings, engineering orders, and fleet performance metrics inside the ENOVIA or Teamcenter PLM backbone.

Required Qualifications

• U.S. FAA Airframe & Powerplant (A&P) license plus B.S. in Aerospace, Mechanical, or Civil Engineering (ABET-accredited).
• 5+ years of post-license experience performing structural substantiation on Part 25 transport-category aircraft (Boeing, Airbus, Embraer, or equivalent).
• Demonstrated ability to write and sign off engineering repairs under an FAA-approved RSM, CASS, or OEM DER system.
• Proficiency with metallic (2024, 7075, Ti-6Al-4V, 4340M) and composite (CFRP, GFRP, honeycomb) material allowables per MMPDS/CMH-17.
• Fluency in 14 CFR Parts 25, 43, 91, 121, 145 and familiarity with EASA CS-25 cross-reference tables.
• U.S. person status or ability to obtain a security clearance for defense-related projects.

Preferred Qualifications

• Advanced degree (M.S./Ph.D.) in Structural Engineering or Applied Mechanics.
• Current FAA DER (Structures) or ODA Unit Member authorization.
• Experience with next-gen air-taxi eVTOL or UAM platforms powered by distributed electric propulsion.
• Python or MATLAB scripting for automating load-path analyses and pulling fleet IoT sensor data.
• Hands-on composite field repairs in a Part 145 repair-station environment.
• Knowledge of additive-manufactured (titanium/aluminum) repair parts and associated FAA AMOC pathways.

Technical Skills and Relevant Technologies

• CAD: CATIA v5/v6, SolidWorks, NX, AutoCAD.
• FEA/Stress: NASTRAN, PATRAN, ABAQUS, HyperMesh, Ansys.
• Crack-Growth & DT: NASGRO, AFGROW, DARWIN.
• PLM/ MRO software: ENOVIA, Teamcenter, TRAX, AMOS, SAP MRO.
• Data visualization: Power BI, Tableau, Grafana.
• Regulatory portals: FSIMS, CMT, SDRS, EASA EASY.

Soft Skills and Cultural Fit

• High bias for action—you’d rather release a 90 % substantiation package on time and iterate than chase 100 % perfection in a vacuum.
• Comfortable presenting stress margins to both Ph.D. metallurgists and A&P mechanics on the hangar floor.
• Low-ego collaboration: you seek critiques from stress, interiors, and certification teams before affixing your signature.
• Relentless curiosity—reads every SB within 24 h of release and asks, “How does this scale across the fleet?”
• Champions safety culture: willing to stop the line when data says “unknown.”

Benefits and Perks

Compensation Range: [$SALARY_RANGE] per year, commensurate with DER/UM credentials and fleet size.

• Annual bonus target 12 % plus fleet-reliability performance kicker.
• Stock options or RSU grants pegged to certification milestones.
• 100 % employer-paid medical, dental, vision for employee + dependents.
• Global travel card—fly anywhere [$COMPANY_NAME] operates for $0 plus taxes.
• $3 k annual training stipend for DER refresher, composite repair, or Python bootcamp.
• 9/80 schedule with every other Friday off; optional 4-week paid sabbatical after five years.

Equal Opportunity Statement

[$COMPANY_NAME] is an Equal Opportunity Employer. We celebrate diversity and are committed to creating an inclusive environment for all employees—regardless of race, color, religion, gender, gender identity or expression, sexual orientation, national origin, genetics, disability, age, or veteran status. We encourage applications from women, people of color, veterans, and LGBTQ+ individuals who are excited about advancing aerospace safety.

Location

This position is based at [$COMPANY_LOCATION] with a hybrid schedule (three days on-site for MRB and hangar walkdowns). We welcome remote applicants within [$COMPANY_LOCATION] who can travel on 24-hour notice for AOG support.

Don’t meet every bullet? Studies show that under-represented groups hesitate unless they tick 100 % of the boxes. If you’re an A&P-licensed engineer with a passion for flight safety, we’d love to see your application and explore how you can grow with us.

Company Overview

[$COMPANY_OVERVIEW]

Role Overview

As a Senior Airframe & Powerplant (A&P) Engineer at [$COMPANY_NAME], you will own the structural and systems integrity of turbine-powered aircraft across our Part 121/135 fleet. You’ll translate FAA regulations, OEM service bulletins, and reliability data into engineering dispositions that keep metal flying safely and profitably. Expect to author major repair/alteration packages, lead cross-functional MRB boards, and mentor junior engineers on fatigue-life models, damage-tolerance analysis, and DER/ODA delegation pathways.

Key Responsibilities

• Certify major repairs and alterations (Form 8110-3/8100-9) for fuselage, wing, and empennage structures using strength/stiffness hand calcs, FEM (NASTRAN/PATRAN), and fatigue spectra derived from flight-data recorders
• Lead root-cause investigations on in-service discrepancies—corrosion, cracks, delamination, FOD—by coordinating non-destructive testing (NDI), teardown analysis, and fleet-wide SB/AD impact assessments
• Own the company’s Continuing Structural Integrity Program (CSIP): update corrosion-control documents, structural inspection intervals, and retirement life limits based on MSG-3 logic and OEM MPD revisions
• Drive DER/ODA delegation: interface with FAA ACOs and MIDOs to obtain approved data for composite doubler installations, avionics cooling mods, and cabin reconfigurations
• Mentor junior engineers on FAR 25.571 damage-tolerance requirements, SRM interpretation, and proper use of A-basis/B-basis allowables
• Partner with Maintenance, Supply Chain, and CAMO teams to optimize heavy-check workscopes, minimize aircraft downtime, and ensure parts obsolescence is mitigated through PMA or alternative certification paths
• Champion digital-twin initiatives: calibrate FEM models against strain-gauge flight loads, deploy predictive-maintenance algorithms, and integrate data streams from ACARS and health-monitoring sensors

Required Qualifications

• Bachelor of Science in Aerospace, Mechanical, or Civil Engineering (ABET-accredited); Master’s preferred
• Current FAA Airframe & Powerplant (A&P) certificate with 8+ years of turbine-aircraft structural engineering experience under FAR Part 121, 135, or 145
• Demonstrated authority sign-off history: minimum of 20 Form 8110-3 or equivalent major repair/alteration packages approved by FAA or ODA
• Proficiency with NASTRAN, FEMAP, or equivalent FEM suite; ability to perform static, fatigue, and buckling analyses on metallic and composite structures
• Deep knowledge of FAR Part 25 Subparts C & E, AC 20-107B (Composite A/C Structures), and MSG-3 analysis methodology
• Experience leading MRB/MEB boards and coordinating with NDI Level II/III inspectors on crack sizing and probability-of-detection studies
• U.S. person status required for ITAR-controlled technical data

Preferred Qualifications

• FAA Designated Engineering Representative (DER) or Organization Designation Authorization (ODA) Unit Member for Structures
• Experience with Boeing 737/777, Airbus A320 family, or regional-jet OEM structures and service bulletins
• Hands-on composite repair shop experience: autoclave cure cycles, scarf-patch design, bonded-joint allowables per CMH-17
• Scripting proficiency (Python/MATLAB) for automating load-spectrum extraction and fatigue-life calculations
• Exposure to digital twins, model-based systems engineering (MBSE), and ARINC 834 health-monitoring standards

Technical Skills & Relevant Technologies

• FEM/CAE: NASTRAN, FEMAP, PATRAN, Abaqus, HyperMesh
• Fatigue & DT: AFGROW, NASGRO, SWIFT, nCode
• Regulatory: FAA Orders 8110.4C, 8100.15B, AC 20-107B, EASA AMC 20-29
• Data: SQL, PowerBI, Tableau, ACARS parameter mining
• Doc control: ENOVIA, Teamcenter, SAP ECC, AMOS, TRAX

Soft Skills & Cultural Fit

• Track record of presenting complex structural analyses to flight-ops, finance, and C-suite stakeholders with clarity and data-backed confidence
• Collaborative style that thrives in a reliability-centered, safety-first culture—willing to red-tag production when airworthiness is at risk
• Coach/mentor mindset: derive satisfaction from elevating early-career engineers through design-review checklists and lunch-and-learn sessions
• Comfortable with ambiguity—can prioritize 50 open engineering orders during A-check crunch without compromising compliance

Benefits & Perks

Annual base salary range: [$SALARY_RANGE] plus 15 % target bonus and annual continuing-education stipend for DER/ODA pathway

• Comprehensive medical, dental, vision, and aerospace-industry loss-of-license insurance
• 401(k) with 6 % company match and 3-year vesting
• Travel privileges on [$COMPANY_NAME] routes and reciprocal jumpseat agreements
• Paid attendance at SAE A-5, ASTM F44, and CMH-17 committee meetings to shape future regulations

Equal Opportunity Statement

[$COMPANY_NAME] is an Equal Opportunity Employer. We celebrate diversity and are committed to creating an inclusive environment for all employees. All qualified applicants will receive consideration for employment without regard to race, color, religion, sex, sexual orientation, gender identity, national origin, disability, or protected veteran status.

Location

Hybrid role based in [$COMPANY_LOCATION]; engineers expected on the flight-line and in the hangar at least 2 days per week for physical inspections and MRB support. Relocation assistance available.

Company Overview

[$COMPANY_OVERVIEW]

Role Overview

We are seeking a Lead Airframe & Powerplant (A&P) Engineer to spearhead the design, certification, and continuous airworthiness of next-generation aircraft systems at [$COMPANY_NAME]. You will own the technical authority for all structures, mechanical systems, and powerplant integration—translating FAA/EASA Part 25 requirements into certifiable, producible designs that push the boundaries of weight, performance, and safety. This is a player-coach role: you will personally solve the hardest fatigue, flutter, and engine-mount load-path problems while mentoring a multidisciplinary team of stress engineers, DERs, and certification liaisons.

Responsibilities

• Act as the delegated Part 25 Structural and Mechanical Systems DER/OAR, signing off on critical compliance artifacts (static strength, damage tolerance, fatigue, flutter, bird-strike, fireproof & flammability)
• Lead preliminary and detailed design of airframe primary structure—wing box, fuselage pressure vessel, empennage, and flight-control surface attachments—using Catia v5, NX, and FEMAP/NASTRAN for FE modeling and linear/non-linear analysis
• Define engine-mount and pylon architecture for high-bypass turbofans or electric-propulsion nacelles; generate load spectra for 1-cosine gust, crash, ultimate, and limit-load cases per FAR 25.571, 25.613, and 25.963
• Drive material selection trade studies: advanced CFRP, additive Ti-6Al-4V, Al-Li 2198, and thermoplastic composites—balancing specific strength, repairability, and production rate ramp-up
• Establish certification roadmap, coordinate with FAA ACO and MIDO teams, and author certification plans, issue papers, and compliance checklists (MOC1–MOC8)
• Own the structural test pyramid: coupon, element, detail, sub-component, and full-scale static & fatigue tests; develop DVT plans, instrumentation maps, and post-test correlation reports
• Mentor 6–10 engineers on stress methods, fatigue life prediction (NASGRO, AFGROW), and damage-tolerance best practices; conduct technical reviews and sign off on release to manufacturing
• Interface with suppliers (Spirit, GKN, PCC) to review forging, machining, and composite lay-up process specs; enforce SRM and MRB authority for non-conformance disposition
• Continuously monitor in-service fleet data via digital-twin models, updating inspection intervals and service bulletins to maintain dispatch reliability above 99.5 %

Required Qualifications

• B.S. in Aerospace, Mechanical, or Civil Engineering; M.S. preferred
• Current or previous FAA DER or EASA Part 21J DOA signatory authority for Structures/Mechanical Systems
• 10+ years of Part 25 aircraft design, analysis, and certification—至少 3 years in a lead or chief-engineer capacity
• Expert-level proficiency with FEM tools (NASTRAN, ABAQUS, ANSYS) and pre/post processors (FEMAP, HyperMesh)
• Deep knowledge of metallic and composite allowables generation, statistical basis (A- or B-basis), and joint analysis (bolted, bonded, hybrid)
• Demonstrated ownership of at least one major certification program from preliminary design through TC and PC issuance
• U.S. Person status or ability to obtain DoD security clearance if required

Preferred Qualifications

• Ph.D. research in fatigue or composite progressive failure
• Experience with eVTOL or hybrid-electric propulsion airframes
• Python or MATLAB scripting for automated post-processing and machine-learning-enhanced loads prediction
• Hands-on composite manufacturing: AFP, RTM, or out-of-autoclave cure cycles
• Published technical papers at AIAA, ASTM, or ICCM conferences

Technical Skills and Relevant Technologies

• FAA/EASA Part 25, Part 21, Part 43, Part 145 regulations
• Catia v5 3D Experience, Siemens NX, SolidWorks, ENOVIA PLM
• NASTRAN, ABAQUS, ANSYS, OptiStruct, LS-DYNA for explicit crash
• Fatigue & damage-tolerance: NASGRO, AFGROW, DARWIN, SMART
• Flutter & aeroelasticity: ZAERO, Nastran SOL 145, MSC FlightLoads
• Process automation: Python, VBA, MATLAB, Altair HyperStudy
• Configuration & requirements management: IBM DOORS, Jama, Polarion

Soft Skills and Cultural Fit

• Decisive technical leadership with a data-driven, risk-based mindset
• Ability to communicate complex certification issues to non-technical executives and airline operators
• Collaborative style that thrives in an Agile hardware environment—daily stand-ups, sprint reviews, and Confluence documentation
• Relentless attention to safety, quality, and regulatory rigor without compromising innovation speed

Benefits and Perks

• Competitive base salary: [$SALARY_RANGE] + annual performance bonus
• Equity or long-term incentive plan (RSUs or stock options)
• 100 % employer-paid medical, dental, vision for employee and dependents
• 401(k) with 6 % match, immediate vesting
• Relocation stipend or temporary housing assistance
• Professional development: FAA/EASA DER renewal fees, conference travel, and internal technical symposiums
• On-site fitness center and concierge services at [$COMPANY_LOCATION]

Equal Opportunity Statement

[$COMPANY_NAME] is an Equal Opportunity Employer. We celebrate diversity and are committed to creating an inclusive environment for all employees. All qualified applicants will receive consideration for employment without regard to race, color, religion, sex, sexual orientation, gender identity, national origin, disability, or veteran status.

Location

This position is based at our advanced manufacturing and engineering campus in [$COMPANY_LOCATION]. Hybrid schedule available: three days on-site for test labs and certification reviews, two days remote for focused analysis work.

Company Overview

[$COMPANY_OVERVIEW]

Role Overview

We are searching for a Chief A&P (Airframe & Powerplant) Engineer to serve as the technical authority for all aircraft maintenance engineering activities across [$COMPANY_NAME]’s growing fleet. You will set the strategic direction for airworthiness programs, certify major repairs and alterations, and lead a multidisciplinary team of licensed A&P engineers ensuring 100 % regulatory compliance with 14 CFR Parts 21, 43, 65, 91, 121, and 145. This executive-level position reports directly to the VP of Engineering and interfaces with the FAA, EASA, and other global aviation authorities.

Responsibilities

• Own the technical approval of all maintenance, preventive maintenance, rebuilding, and alteration activities on turbine and piston-powered fixed-wing and rotorcraft airframes, engines, and avionics systems.
• Author, review, and sign Engineering Authorizations (EAs), FAA Form 337s, Supplemental Type Certificates (STCs), and Repair Specification Approvals while ensuring conformity to accepted data and industry best practices.
• Architect reliability-centered maintenance (RCM) programs, MSG-3 analyses, and predictive maintenance roadmaps that reduce unscheduled downtime by ≥15 % year-over-year.
• Lead root-cause investigations for in-service failures using FRACAS, Ishikawa, and 5-Why methodologies; present findings to the FAA within 24 hours of significant events.
• Mentor and technically assess a distributed team of A&P engineers, DERs, DARs, and repair station inspectors; conduct quarterly peer reviews and approve training curricula for continuing education credits.
• Negotiate with OEMs, suppliers, and MRO vendors to secure DER-approved replacement parts, alternate inspection intervals, and cost-effective repair schemes that save >$2 M annually.
• Champion digital transformation by specifying requirements for aircraft maintenance software (AMOS, TRAX, or similar) and integrating IoT sensor data into digital twin models for trend monitoring.
• Represent [$COMPANY_NAME] at industry forums (SAE, ATA, A4A, NBAA, HAI) and influence upcoming regulatory changes such as MOSAIC, Part 23 rewrite, and Sustainable Aviation Fuel (SAF) mandates.

Required Qualifications

• FAA Airframe & Powerplant (A&P) license with Inspection Authorization (IA) active for ≥10 years.
• Bachelor of Science in Aerospace, Mechanical, or Electrical Engineering; Master’s preferred.
• Minimum 12 years of progressive experience in Part 121/135/145 maintenance environments, including 5 years in a senior engineering leadership role overseeing multi-fleet types.
• Current FAA Designated Engineering Representative (DER) or ability to obtain delegation within 6 months.
• Demonstrated history of certifying at least 10 STCs or major repairs on turbine-powered aircraft valued >$1 M each.
• Proficiency with fatigue and damage-tolerance analysis tools (NASGRO, AFGROW, nCode) and familiarity with composite laminate allowable generation (CMH-17, FAA AC 20-107B).
• U.S. Person status for ITAR-controlled technical data.

Preferred Qualifications

• Dual FAA & EASA Part-66 B1/B2 license with type ratings on Airbus A320/350 or Boeing 737 MAX families.
• Experience leading DER delegation for electrified propulsion, hydrogen fuel cells, or eVTOL platforms.
• Certified Six Sigma Black Belt or Lean Maintenance implementation resulting in ≥20 % cycle-time reduction.
• Published technical papers on aging aircraft programs, WFD, or corrosion prevention & control (CPCP).
• Active membership in SAE committees G-11 (Reliability) or A-5 (Aerospace Structures).

Technical Skills and Relevant Technologies

• Advanced knowledge of 14 CFR, EASA Part 21/145, Transport Canada CAR 571/573, and ICAO Annex 6 standards.
• Expert user of CAD/CAE suites (CATIA v5, Siemens NX, SolidWorks) and PLM systems (Teamcenter, Enovia).
• Proficient with maintenance tracking platforms (AMOS, CAMP, AVTRAC) and reliability databases (ReliaSoft, Isograph).
• Strong data analytics skills using Python, MATLAB, or R for Weibull survival analysis and prognostics.
• Familiarity with additive manufacturing (DED, PBF) for rapid replacement part certification under AC 20-185.

Soft Skills and Cultural Fit

• Executive presence with the ability to brief C-suite and board members on airworthiness risk in business-critical language.
• Collaborative leadership style that empowers licensed technicians while enforcing strict regulatory discipline.
• High tolerance for ambiguity and rapid decision-making during AOG situations across global time zones.
• Commitment to safety management systems (SMS) and just culture principles.

Benefits and Perks

Compensation: [$SALARY_RANGE] plus annual performance bonus and long-term incentive plan.

• Company-paid relocation to [$COMPANY_LOCATION] or remote work stipend if fully remote.
• Executive medical, dental, vision, and loss-of-license insurance; 100 % employer-paid premiums.
• Company aircraft usage for personal travel (seat-available program).
• Professional development: unlimited training budget, FAA IA renewal fees, DER maintenance, and conference attendance.
• 401(k) with 10 % employer contribution (no match required) and 3-year vesting.
• 20 weeks paid parental leave and flexible sabbatical after 5 years.

Equal Opportunity Statement

[$COMPANY_NAME] is an Equal Opportunity Employer. We celebrate diversity and are committed to creating an inclusive environment for all employees. All qualified applicants will receive consideration for employment without regard to race, color, religion, sex, sexual orientation, gender identity, national origin, disability, veteran status, or any other protected characteristic. Candidates who meet 60 % of the requirements are strongly encouraged to apply; we value potential as much as pedigree.

Location

This is a hybrid position based in [$COMPANY_LOCATION]. Expect 3 days per week on-site at our MRO facility and flight operations center, with the remainder flexible remote to support global fleet oversight.