Senior Advanced Project Engineer - Turbofan Engines

Honeywell Aerospace•Phoenix, AZ

4d•Hybrid

About The Position

As a Senior Advanced Project Engineer, you will lead high-impact engineering initiatives supporting the renowned CFE738 and TFE731 turbofan engine programs. In this highly visible role, you will collaborate with world-class engineers, customers, suppliers, certification authorities, and executive leadership to maintain design excellence and drive innovative product improvements across legacy turbofan platforms. You will spearhead complex, multidisciplinary projects spanning engine systems including the fan, compressor, combustor, turbine, exhaust, and powerplant installation systems, ensuring technical integrity, regulatory compliance, and successful project execution. This is an exceptional opportunity for a strategic engineering leader who thrives on solving complex technical challenges, driving continuous improvement, and delivering results that directly impact the safety, performance, and future evolution of Honeywell's aerospace product portfolio. If you are passionate about aerospace engineering, project leadership, and influencing the success of globally recognized propulsion systems, we invite you to join our team in Phoenix, Arizona, and make a lasting impact. You will report directly to our Sr. Project Engineering Manager at the Honeywell Aerospace facility located at 111 S 34th St. Phoenix, Arizona, 85034. This role is eligible for hybrid work per Honeywell Aerospace Policy, except for the first 90 days.

Requirements

Bachelor's degree from an accredited institution in a technical discipline such as the sciences, technology, engineering or mathematics.
Minimum of 5 years of Project engineering or Program management experience within the aerospace industry.
Candidate must be a U.S. Person, which is defined as, a U.S. citizen, a U.S. permanent resident, or have protected status in the U.S. under asylum or refugee status or have the ability to obtain an export authorization.

Nice To Haves

Technical publications and maintenance manual experience related to aerospace products.
Direct experience with the design, development and certification of turbomachinery or complex aircraft systems.
Experience with turbomachine engine installations.
Knowledge of 14 CFR Part 33 or equivalent certification requirements.
Aircraft manufacturer and/or part 25 hardware experience.
Direct experience with root cause-corrective action investigations, cost reduction programs or new product development.
Experience working with collaboratively with suppliers to turn designs into hardware and solve problems in production.
Demonstrated ability to plan technical programs, including budget and schedule estimation, resource planning and risk and requirements management.
Demonstrated ability to recognize cost and schedule risks before they can cause significant program impact, and the ability to develop and execute sound risk mitigation plans.
The ability to provide technical contributions essential to the successful completion of projects.

Responsibilities

Leading root cause investigations and implementing corrective actions.
Executing changes to designs and approved source lists for engine and powerplant components.
Schedule and milestone development/management.
Cost and budget management, including estimate development and project planning.
Technical requirements development.
Project performance and technical execution.
Risk/opportunity development and management.
Vendor interface and management of technical requirements.
Presenting project plans and status to customers, operators, and internal stakeholders.
Orchestrate documentation efforts for various levels of engine/component certification and/or qualification projects.
Performs co-authoring/writing of documents for organization, technical congruency, compliance to customer requirements, and internal and external standards.
Participates in efforts with team members and outside vendors to revise and maintain technical publications.