Accomplishment Accomplishment Accomplishment Accomplishment Accomplishment

Accomplishments

Our list of current clientele range from the Boeing 787 Dreamliner partners, MRO companies, airlines, aerospace manufacturing companies and aerospace engineering support & services companies. Current and past programs the staff of Windspeed Technical Solutions have been involved in are as follows:

  • 787-9 Dreamliner Section 45 - Keel Beam Structure stress analysis & design development.
  • 787-9 Dreamliner Section 45 - Composite Horizontal Pressure Deck stress analysis and design development.
  • 787-9 Dreamliner Section 45 - Composite Aft Wheel Well Bulkhead stress analysis and design development.
  • 787-8 Dreamliner Section 15 (Wing Fixed Trailing Edge). Sizing and stress substantiation of Auxiliary-D Inboard FlapSupport Rib and Spoiler Flex Panels.
  • 787-8 Dreamliner section 45 (Keel/Wheel Well). Stacking definition/Stress sizing/Trade study of composite laminate stiffened panel structures (Pressure Deck & Wheel Well Bulkhead) using Boeing proprietary tools (FEADMS, Moss-Duberg, IAS) and Nastran / ABAQUS (linear / nonlinear) FEM.
  • 747-8 section 49 Structural substantiation of Landing Gear Doors structure, fittings and mechanisms.
  • 737 Winglet Structure stress analysis support.
  • P-8A (Multi-mission Maritime Aircraft) section 46 (Aft Fuselage). Stress analysis of antenna installations / floor structure modifications.
  • Structure engineering support for Lockheed L-1011 and L-1329 (JetStar) fleet, providing static/fatigue/DT substantiated repairs and other dispositions to customers. - Sustaining engineering for Continued Airworthiness items (Supplemental Inspection Document, Service Bulletins) of all FAA certified Lockheed out-of-production aircraft models.
  • Flight/ground loads and stress analysis of Aeros 40B airship for FAA Type Certification (Project# S0007LA) in accordance with FAR Part 23 and Airship Design Criteria.
  • Technical interface with FAA Los Angeles Aircraft Certification Office for structural substantiation, weight & balance, performance calculation, company & TIA flight tests, and Pilot's Operating Handbook.
  • Stress analysis and ground test (Static/DT/Fatigue) support for Lockheed Martin/Mitsubishi XF-2/F-2 fighter (Based on F-16 block 40) prototype and production variants center fuselage.
  • Load / stress analysis for fuselage modification of Lockheed/Kawasaki UP-3D electronic warfare aircraft.
  • Engineering support for production and maintenance MRB (I-TAG/IRAN) for C-130 / P-3C / E-2C / F-15EJ / T-4 / C-1.
  • Stress review of major dynamic components for XOH-1 scout helicopter prototype.
  • Stress analysis / finite element modeling for Gulfstream V-based special mission aircraft modifications .
  • Section 41 & 44 substantiation of existing and new structure for Boeing 747-400 LCF aircraft.
  • Wing Fixed Leading & Trailing Edge substantiation for Boeing 777-300ER+ & 777-300ER Enhanced.
  • Connexions by Boeing Antenna installation on a 777-300ER aircraft.
  • Main Landing Gear Door Analysis for the Boeing 747-400ER aircraft.
  • Floor beams, posts and frames stress analysis for the conversion of a Boeing 747-100 to a Combi Special Freighter.
  • Overhead Crew Rest Suppt. structure including rails & tie-rods analyses for the B777-200LR/300ER aircrafts.
  • Structural substantiation of existing over-wing floor beams of B727-100/-200 for Cargo Conversion.
  • Systems installation for Boeing 757 and Boeing 737 aircrafts.
  • System equipment and racks installation for a Convair Cv-580 research aircraft.
  • System equipment and racks installation for a DC-10 aircraft.