The Boeing Company
Div Engineering, Test & Technology
CAGE Code: 4JSW3
NCAGE Code: 4JSW3
Status: Active
Type: Manufacturer
Dun & Bradstreet (DUNS): 622377070
Stock Symbol: BA
Summary
The Boeing Company, Div Engineering, Test & Technology is an Active Manufacturer with the Cage Code 4JSW3 and is tracked by Dun & Bradstreet under DUNS Number 622377070..
Address
9725 E Marginal Way S
Tukwila WA 98108-4040
United States
Points of Contact
- Telephone:
- 3148826934
- http://www.boeing.com/INDEX.HTML
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Frequently Asked Questions (FAQ) for CAGE 4JSW3
- What is CAGE Code 4JSW3?
- 4JSW3 is the unique identifier used by NATO Organizations to reference the physical entity known as The Boeing Company Div Engineering, Test & Technology located at 9725 E Marginal Way S, Tukwila WA 98108-4040, United States.
- Who is CAGE Code 4JSW3?
- 4JSW3 refers to The Boeing Company Div Engineering, Test & Technology located at 9725 E Marginal Way S, Tukwila WA 98108-4040, United States.
- Where is CAGE Code 4JSW3 Located?
- CAGE Code 4JSW3 is located in Tukwila, WA, USA.
Contracting History for CAGE 4JSW3 Most Recent 25 Records
- DTRTVT3012
- Tmis Safety Management Transformation (Ssmt) Technology Support. Modification To Deobligate Funds And Closeout The Task Order
- 3 Apr 2023
- Tmis Safety Management Transformation (Ssmt) Technology Support. Modification To Deobligate Funds And Closeout The Task Order
- 6913G6 Volpe Natl. Trans. Sys Cntr
- Department Of Transportation (Dot)
- $1,093,866.34
- Department Of Transportation (Dot)
- N0001412C0153
- Research And Development In The Physical, Engineering, And Life Sciences (Except Biotechnology)
- 6 Apr 2021
- Research And Development In The Physical, Engineering, And Life Sciences (Except Biotechnology)
- Dcma Boeing Seattle
- Department Of Defense (Dod)
- $1,947,459.34
- Department Of Defense (Dod)
- FA865012C7208
- Passive Micro-Plasma Power Limiter For Rf Apertures
- 28 May 2021
- Passive Micro-Plasma Power Limiter For Rf Apertures
- Dcma Boeing Seattle
- Department Of Defense (Dod)
- $6,784,332.55
- Department Of Defense (Dod)
- HR001110C0090
- The Overall Program Goal Is To Reduce The Risks And Uncertainties Associated With Performing Extended Flights In Formations To A Sufficient Level While Still Achieving A Significant Aerodynamic Performance Benefit. The Contractor Shall Provide A Clear Understanding Of The Trade Space Between Aerodynamic Benefit And Limits Based On Safety, Engines, Airframe, And Crew Workload. This Effort Will Consist Of Two Phases.
- 20 Apr 2021
- The Overall Program Goal Is To Reduce The Risks And Uncertainties Associated With Performing Extended Flights In Formations To A Sufficient Level While Still Achieving A Significant Aerodynamic Performance Benefit. The Contractor Shall Provide A Clear Understanding Of The Trade Space Between Aerodynamic Benefit And Limits Based On Safety, Engines, Airframe, And Crew Workload. This Effort Will Consist Of Two Phases.
- Dcma Boeing Seattle
- Department Of Defense (Dod)
- $5,616,695.67
- Department Of Defense (Dod)
- HR001110C0090
- The Overall Program Goal Is To Reduce The Risks And Uncertainties Associated With Performing Extended Flights In Formations To A Sufficient Level While Still Achieving A Significant Aerodynamic Performance Benefit. The Contractor Shall Provide A Clear Understanding Of The Trade Space Between Aerodynamic Benefit And Limits Based On Safety, Engines, Airframe, And Crew Workload. This Effort Will Consist Of Two Phases.
- 12 Apr 2021
- The Overall Program Goal Is To Reduce The Risks And Uncertainties Associated With Performing Extended Flights In Formations To A Sufficient Level While Still Achieving A Significant Aerodynamic Performance Benefit. The Contractor Shall Provide A Clear Understanding Of The Trade Space Between Aerodynamic Benefit And Limits Based On Safety, Engines, Airframe, And Crew Workload. This Effort Will Consist Of Two Phases.
- Dcma Boeing Seattle
- Department Of Defense (Dod)
- $5,616,695.67
- Department Of Defense (Dod)
- 0021
- Tmis Air Traffic Systems Program And Engineering Support. Administrative Modification To Incorporate The Appointment Of A New Tocor.
- 27 Sep 2023
- Tmis Air Traffic Systems Program And Engineering Support. Administrative Modification To Incorporate The Appointment Of A New Tocor.
- 6913G6 Volpe Natl. Trans. Sys Cntr
- Department Of Transportation (Dot)
- $17,074,872.10
- Department Of Transportation (Dot)
- NNC13TA51T
- Igf::Ot::Igf The Contractor Shall Provide The Engineering Development, Mechanical Design, Specifications, Tolerances, Instrumentation Plan, Flap Design And Actuation System, Quality Assurance And Inspection Requirements Required To Develop A Fabrication Bid Package For The Construction Of The Three Models. The Contactor Shall Work With The Nasa/Illinois Nra Research Team In Order To Facilitate Communication Of Model Geometry And Testing Requirements. The Contractor Shall Apply Its Expertise In Airframe Design/Manufacturing And Its Expertise In Icing-Tunnel Model Design/Manufacturing To Guide The Development Of These Models From Conceptual Design And Sizing To Fabrication Readiness. The Contractor Shall Develop A Cost Estimate To Fabricate And Deliver The Three Models To The Nasa Irt For Testing. All Engineering Information Such As Drawings, Sketches, Specifications, Tolerances And Component Descriptions, Shall Be Provided To The Government. The Contractor Shall Also Provide A Detailed Breakdown Of Their Cost Estimate Including Categories For Manufacturing Design, Structural Analysis, Inspection, Instrumentation And Oversight/Management.
- 7 Feb 2014
- Igf::Ot::Igf The Contractor Shall Provide The Engineering Development, Mechanical Design, Specifications, Tolerances, Instrumentation Plan, Flap Design And Actuation System, Quality Assurance And Inspection Requirements Required To Develop A Fabrication Bid Package For The Construction Of The Three Models. The Contactor Shall Work With The Nasa/Illinois Nra Research Team In Order To Facilitate Communication Of Model Geometry And Testing Requirements. The Contractor Shall Apply Its Expertise In Airframe Design/Manufacturing And Its Expertise In Icing-Tunnel Model Design/Manufacturing To Guide The Development Of These Models From Conceptual Design And Sizing To Fabrication Readiness. The Contractor Shall Develop A Cost Estimate To Fabricate And Deliver The Three Models To The Nasa Irt For Testing. All Engineering Information Such As Drawings, Sketches, Specifications, Tolerances And Component Descriptions, Shall Be Provided To The Government. The Contractor Shall Also Provide A Detailed Breakdown Of Their Cost Estimate Including Categories For Manufacturing Design, Structural Analysis, Inspection, Instrumentation And Oversight/Management.
- Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $193,975.27
- National Aeronautics And Space Administration (Nasa)
- NNC14TA36T
- Large-Scale, Swept-Wing Test Articles Fabrication Research And Test Support For Nasa Icing Research Tunnel. Under The Auspices Of The Atmospheric Environment Safety Technologies Project Of Nasa's Aviation Safety Program, Research Is Being Directed At Understanding Ice Accretion And Aerodynamic Effects For Large-Scale Swept Wings. Nasa Is Planning To Conduct A Series Of Icing Tests In The Irt To Characterize Ice Formations On Large-Scale Swept Wings Representative Of Modern Commercial Transport Airplanes. The Ultimate Goal Of The Icing Tests Is To Generate Representative Ice Accretion On Swept Wings That Can Be Used For Subsequent Aerodynamic Evaluation In Other Experimental Facilities And For Validation Of Ice-Accretion Prediction Codes.
- 3 Aug 2021
- Large-Scale, Swept-Wing Test Articles Fabrication Research And Test Support For Nasa Icing Research Tunnel. Under The Auspices Of The Atmospheric Environment Safety Technologies Project Of Nasa's Aviation Safety Program, Research Is Being Directed At Understanding Ice Accretion And Aerodynamic Effects For Large-Scale Swept Wings. Nasa Is Planning To Conduct A Series Of Icing Tests In The Irt To Characterize Ice Formations On Large-Scale Swept Wings Representative Of Modern Commercial Transport Airplanes. The Ultimate Goal Of The Icing Tests Is To Generate Representative Ice Accretion On Swept Wings That Can Be Used For Subsequent Aerodynamic Evaluation In Other Experimental Facilities And For Validation Of Ice-Accretion Prediction Codes.
- Nasa Glenn Research Center
- National Aeronautics And Space Administration (Nasa)
- $1,775,975.04
- National Aeronautics And Space Administration (Nasa)