Thomas W. Deiters Engineering frequently provides static, fatigue, design construction, and damage tolerance services in the following categories, though the company's expertise spans beyond these typical functions:
Services to ensure compliance with:
14 CFR Part 23, Airworthiness Standards: Normal, Utility, Acrobatic and Commuter Category Airplanes
14 CFR Part 25, Airworthiness Standards: Transport Category Airplanes
14 CFR Part 26, Continued Airworthiness and Safety Improvement
Preparation of substantiation reports and drawings
Preparation of FAA Form 8110-3, Statement of Compliance with Airworthiness Standards
Preparation, development, and substantiation of type design data for FAA Airworthiness Directives (AD) Alternate Method of Compliance (AMOC), for FAA Amended Type Certificates and Supplemental Type Certificates, and for special one-off projects
Support for changes in FAA Airworthiness Certificates
Static structural strength/stress analysis - strength substantiation
Damage tolerance assessment and/or analysis - structural or mechanical life prediction
Preparation of instructions on and provision of support for continuing airworthiness
Crack growth and fatigue analysis, and fracture research
Repair substantiation - evaluation, design and analysis
External and internal loads development
Mission spectra development
Proof load determination
Structural integrity and structural adequacy evaluations
Aircraft Structural Integrity Program (ASIP) projects
Failure analysis
Cost/benefit analysis, man-hour estimates, and similar cost projections
Aircraft Battle Damage Assessment Repairs/Reports (ABDR)
info@twdeng.com (470) 313 - 5542