The basic standard for any aircraft repair is that the repaired structure should be as strong as the original structure and be equivalent to the original in rigidity and aerodynamic shape
- AC 43.13-1B
The maximum interior lighting levels vary significantly among different airplane models. In addition, there is usually a great deal of
flexibility in providing different levels of lighting by utilizing only parts of the overall
normal lighting system for any given model.
-AC 25.812-2
We are specialized in approvals of VIP cabin door panels and galley modifications. Our engineers can design, evaluate, and approve your concept modification and provide you with a complete set of design approval documents.
specializing in the FAA/EASA approval of Part 23 and Part 25 aircraft, aircraft components and aircraft systems.
Aircraft Structures Engineering Solutions LLC is a family operated aerospace engineering services company specializing in the FAA/EASA approval of Part 23 and Part 25 aircraft, aircraft components and aircraft systems. We provide engineering support (Design, Analysis, and Testing) and FAA DER/ EASA CVE approvals to the aviation industry.
Structural design is our true passion. Having worked in the aerospace industry for over a decade, our engineers possess a great wealth of knowledge in design and analysis of complex repairs and alterations.
We understand there are plenty of choices out there when it comes to engineering companies. But here at ASES, we value project completion and around-the-clock support for our customers. Our pledge is to provide the highest quality engineering services at a expeditious time frame.
A corroded spar or a ding in the leading edge may be repaired. Our team is well-experienced in guiding you with the necessary support to restore the strength loss due to the damage in your aircraft.
When a pressurized aircraft is in need of an antenna, careful consideration and analysis are required for the feed-thru hole. We can generate reports with DER approvals so you can rest assured and enjoy your flight.
Our engineering and certification teams can lead you to obtain a PMA or an STC for your camera installation on any Part 23 or Part 25 aircraft.
Pressure bulkheads are essential in maintaining the internal pressure of the cabin. Any repairs related to pressure bulkheads require meticulous engineering calculations and DER approvals before the repairs are considered acceptable. Our team can assist you in obtaining all documents related toa pressure bulkhead repair.
Firefighting conversions are a growing industry as wildfires outstretch the current capability of aerial or ground-based firefighting. Our team can accommodate generating engineering documentation from start to finish for your efforts in making your idea a reality.
We can help you navigate through the engineering and approval paperwork for your floor panel and beam repairs or replacements.
We can provide major repair and alteration data approvals for Owner/Operator under 14 CFR Part 43, or Certified Repair stations under 14 CFR Part 145.
Our certification projects for Part 23 and Part 25 airplanes can range from filed approvals (8110-3) to FAA design and modification approvals under 14 CFR Part 21 (STC and PMA). With the integrity and quality of work, our engineers have formed a trusted working relationship with the regulatory authorities. We work closely with FAA, EASA, ODAs and DOAs. Also, we are currently involved with the Transport Canada (TACA) and South African Civil Aviation Authority (SACAA). Our services includes,