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Awards for “boeing

25 awards on this page · sorted by amount · page 205

Federal prime contract awards for boeing
Award IDRecipientAwarding agencyAmountStartEndNAICSDescription
0004THE BOEING COMPANYDepartment of Defense$3.03M
2015-07-242018-06-30336413C-17 TRANSITION TO POST PRODUCTION (TPP) CRITICAL ASSETS PHASE I
THH8THE BOEING COMPANYDepartment of Defense$3.02M
2013-07-302016-01-29336413WING SECTION,INNER
FA822024FB013THE BOEING COMPANYDepartment of Defense$3.02M
2024-09-232026-09-22336413WINDOWS 11 UPGRADE
0001INSITU, INC.Department of Defense$3.02M
2011-05-122013-09-30541712SCAN EAGLE SBIR PHASE III, FMS TO TUNISIA
NNL13AB38TTHE BOEING COMPANYNational Aeronautics and Space Administration$3.02M
2013-05-092015-04-10541712"IGF::OT::IGF" THE PRIMARY STRUCTURAL CONCEPT BEING DEVELOPED UNDER THE ERA PROGRAM IN THE AIRFRAME TECHNOLOGY ELEMENT IS THE PULTRUDED ROD STITCHED EFFICIENT UNITIZED STRUCTURE (PRSEUS) DESIGN. THE PRSEUS DESIGN APPROACH IS PART OF THE ERA EFFORT TO ADDRESS FUEL BURN (C02 EMISSIONS) BY REDUCING THE WEIGHT OF ADVANCED STRUCTURES. REDUCING FUEL BURN REDUCES THE NEED TO USE RESOURCES AND REDUCES POLLUTION. PRSEUS REPRESENTS A NEW CONCEPT IN COMPOSITE DESIGN THEORY AND MANUFACTURING METHODS. IT IS A CONSCIOUS PROGRESSION AWAY FROM CONVENTIONAL LAMINATED AND BONDED ASSEMBLIES TOWARD LARGER ONE-PIECE PANEL DESIGNS WITH SEAMLESS TRANSITIONS AND DAMAGE-ARREST INTERFACES SUCH AS STITCH ROWS AND TEAR STRAPS. IT FOCUSES ON A NEW STRUCTURAL CONCEPT THAT INTEGRATES SKIN, STRINGERS, AND FRAME ELEMENTS INTO A SINGLE LARGE PANEL IN WHICH ALL ELEMENTS ARE SIMULTANEOUSLY CURED (OR CO-CURED) IN ONE HIGH-TEMPERATURE CURE CYCLE. THE RESULTING STRUCTURE IS A NOVEL SOLUTION FOR ADDRESSING THE DEMANDING FUSELAGE LOADING REQUIREMENTS INHERENT IN A PRESSURIZED SHAPED VEHICLE LIKE THE HYBRID WING BODY (HWB) CONCEPT. THE PRSEUS CONCEPT BUILDS UPON, EXTENDS, AND TAILORS THESE STRUCTURAL TECHNOLOGIES IN ORDER TO MEET THE DEMANDING CHALLENGES ASSOCIATED WITH VEHICLES WITH SHAPES AND LOAD PATHS DIFFERENT FROM TODAY S TRADITIONAL WING AND CIRCULAR FUSELAGE STRUCTURES. HAVING DEMONSTRATED THE UNIQUE CAPABILITY OF THE HWB PRSEUS STRUCTURAL CONCEPT TO ECONOMICALLY PRODUCE LARGE INTEGRATED STRUCTURAL PANELS, THE PRIMARY AIRFRAME DESIGN CHALLENGE NOW BECOMES THE VALIDATION OF THE STRUCTURAL PERFORMANCE IN THE COMBINED LOADING ENVIRONMENT OF THE HWB PRESSURE SHELL. UNDER THESE CONDITIONS, SKIN PANELS MUST NOT ONLY HAVE CONTINUOUS LOAD PATHS IN BOTH DIRECTIONS (I.E., NX AND NY), THEY MUST ALSO BE EFFECTIVE IN TRANSMITTING INTERNAL PRESSURE LOADS (I.E., NZ) FOR THE NEAR-FLAT PANEL GEOMETRY. DEMONSTRATION OF THIS CAPABILITY IS THE PRIMARY PURPOSE OF THE MULTI-BAY BOX TEST ARTICLE. LARC WILL SUBJECT THE MULTI-BAY BOX TEST ARTICLE TO A SERIES OF TESTS IN THE COMBINED LOADS TEST SYSTEM (COLTS) TEST FACILITY AT LARC. AMONG OTHER CONDITIONS, THE LARGE LOADING PLATENS IN COLTS WILL BE USED TO IMPART A BENDING MOMENT ON THE TEST ARTICLE AS IT IS SIMULTANEOUSLY PRESSURIZED. THIS NONLINEAR DESIGN REGIME WILL BE USED TO DEMONSTRATE THE STRUCTURAL PERFORMANCE OF THE PRSEUS CONCEPT, SO THAT THE WEIGHT PENALTY ASSOCIATED WITH THE NON-CIRCULAR HWB PRESSURE CABIN CAN BE QUANTITATIVELY ASSESSED. THE MULTI-BAY BOX TEST ARTICLE, INCLUDING 11 PRSEUS PANELS, WAS DESIGNED UNDER NASA LARC CONTRACT/TASK ORDER NNL04AA11B/NNL10AB00T WITH BOEING. UNDER NNL10AB68T, BOEING SHALL ASSEMBLE THE MULTI-BAY BOX TEST ARTICLE. 2.0 OBJECTIVE/SCOPE: THE OBJECTIVE/SCOPE OF THIS TASK ORDER IS THE FABRICATION AND DELIVERY OF STRUCTURAL PANELS USING THE PRSEUS CONCEPT FOR USE IN THE LARGE SCALE MULTI-BAY BOX TEST ARTICLE. 3.0 DESCRIPTION OF THE WORK/TASKS TO BE PERFORMED: THE CONTRACTOR SHALL PERFORM THE FOLLOWING TASKS: 3.1 MULTI-BAY BOX TEST ARTICLE PANEL FABRICATION THE CONTRACTOR SHALL USE TOOLING IDENTIFIED IN SOW 6.2 TO FABRICATE PRSEUS STRUCTURAL PANELS FOR USE IN THE ASSEMBLY OF THE MULTI-BAY BOX TEST ARTICLE. (DELIVERABLE ITEM 4.7) 3.2 PREPARATION OF UNTRIMMED PANELS FOR ASSEMBLY PRSEUS STRUCTURAL PANELS FOR THE MULTI-BAY BOX TEST ARTICLE WILL BE PROVIDED AS GFP AS SPECIFIED UNDER SOW 6.1. THE CONTRACTOR SHALL TRIM THE PANELS, BOND SHIMS IF NEEDED AND MACHINE THE SHIMS, AND VISUALLY INSPECT THE PANELS TO PREPARE THEM FOR ASSEMBLY IN THE MULTI-BAY BOX TEST ARTICLE. (DELIVERABLE ITEM 4.5)
W58RGZ19F0220THE BOEING COMPANYDepartment of Defense$3.02M
2019-07-012023-09-30541330CH 47 AIRCRAFT ENGINEERING AND LOGISTICS SUPPORT SERVICES (ELSS)
0289THE BOEING COMPANYDepartment of Defense$3.01M
2013-03-112016-03-11336411TASK ORDER FOR CH-47 SYSTEM SPECIFICATION MAINTENANCE AND UPDATE AND STATEMENT OF AIRWORTHINESS QUALIFICATION (SAQ) SUPPORT.
0014DIGITAL RECEIVER TECHNOLOGY, INC.Department of Defense$3.01M
2014-05-082016-11-18339999FABSV2.2 DEVELOPMENT&PROTOTYPE
1006THE BOEING COMPANYDepartment of Defense$3.01M
2015-08-102016-04-30336413IGF::OT::IGF CY15 DELIVERY ORDER FOR LINK 16 TASKING.
0017THE BOEING COMPANYDepartment of Defense$3.01M
2016-02-182016-12-31336411QATAR PRODUCTION ASSETS FOR QA-5, QA-6, QA-7, AND QA-8
70B06C19F00001186DIGITAL RECEIVER TECHNOLOGY, INC.Department of Homeland Security$3M
2019-09-242020-05-31334220SOFTWARE DEFINED RADIOS FOR CBP OI.
N0001921F0668INSITU, INC.Department of Defense$3M
2021-08-162023-05-02336411TEST CY22
0068THE BOEING COMPANYDepartment of Defense$3M
2006-03-142009-11-03541710200606!005314!5700!FA8650!DET 1 AFRL/PK !F3361500D3052 !A!N! !Y!0068 ! !20060314!20090608!039267141!039267141!009256819!N!THE BOEING COMPANY !7755 E MARGINAL WAY !SEATTLE !WA!98124!63000!033!53!SEATTLE !KING !WASHINGTON!+000000450000!N!N!000000000000!AD92!RDTE/OTHER DEFENSE-APPLIED RESEARCH !A1A!AIRFRAMES AND SPARES !000 !NOT DISCERNABLE !541710!E! !5!B!M! !A! !99990909!B! ! !N!Z!A!N!U!2!002!B! !Z!N!Z! ! !N!C!N! ! ! !A!A!A!A!000!A!B!N! ! ! !Y! ! !0001! !
FA862907C2350THE BOEING COMPANYDepartment of Defense$3M
2006-11-092012-03-15336411COMBAT SEARCH AND RESCUE (CSAR-X) SYSTEM DESIGN AND DEVELOPMENT (SDD) AND LOW RATE INITIAL PRODUCTION (LRIP) OPTIONS
N0001917F0253INSITU, INC.Department of Defense$3M
2017-04-272017-12-15336411IGF::OT::IGF DELIVERY ORDER TO PROCURE PARTS FOR NSW SCANEAGLE
N0001921C0028THE BOEING COMPANYDepartment of Defense$3M
2021-01-312022-07-10541330AURA MBSE, CBM+ AND IDE
FA857523C0001THE BOEING COMPANYDepartment of Defense$3M
2022-12-202026-12-21541330F-15 AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) IN SUPPORT OF ROYAL SAUDI AIR FORCE (RSAF)
FA853918F0106THE BOEING COMPANYDepartment of Defense$3M
2018-09-282021-12-31811219REPAIR OF COMPONENTS APPLICABLE TOT HE ACQ-7 SYSTEM.
0055THE BOEING COMPANY (0674)Department of Defense$3M
2005-12-222006-12-31336413200604!000024!5700!FA8621!ASC/YWK !F3365797D0025 !A!N! !N!0055 ! !20051222!20061231!103206264!006265946!009256819!N!MCDONNELL DOUGLAS CORP !J S MCDONNELL BLVD !SAINT LOUIS !MO!63166!65000!510!29!ST. LOUIS !ST. LOUIS (CITY) !MISSOURI !+000002983520!N!N!000000000000!R412!SIMULATION !S1 !SERVICES !000 !NOT DISCERNABLE !541990!E! !5!A!S! ! ! !99990909!B! ! !N!Z!A!N!J!2!002!B! !C!N!Z! ! !Y!C!N! ! ! !Z!C!A!A!000!A!C!N! ! ! ! ! ! !0001! !
FA868111C0041THE BOEING COMPANYDepartment of Defense$3M
2010-11-222011-08-01334511B61
0002THE BOEING COMPANYDepartment of Defense$3M
2006-01-312010-09-16336413200606!000089!5700!FA8106!OC-ALC/LAD CLS !FA810606D0001 !A!N! !N!0002 ! !20060131!20061130!007237241!007237241!009256819!N!THE BOEING COMPANY !4615 SOUTH OLIVER !WICHITA !KS!67210!79000!173!20!WICHITA !SEDGWICK !KANSAS !+000000200000!N!N!000000000000!1510!AIRCRAFT FIXED WING !S1 !SERVICES !000 !NOT DISCERNABLE !336413!E! !5!B!S! ! ! !99990909!B! ! !N!Z!D!N!J!1!001!N!1A!A!Y!Z! ! !N!C!N! ! ! !A!A!A!A!000!A!B!N! ! ! ! ! ! !0001! !
0016BELL BOEING JOINT PROJECT OFFICEDepartment of Defense$2.99M
2007-09-282011-01-07336413NAVY AVIATION
N0018923PZ096JEPPESEN FOREFLIGHT, INC.Department of Defense$2.99M
2023-04-272024-04-30518210MISSION PLANNING AND DISPATCH SUPPORT
0289THE BOEING COMPANYDepartment of Defense$2.99M
2009-09-302012-05-30336411C-32A EPU REPAIR: DMS DIRECTED EIU AND SENSOR REPLACEMENT (V1 TO V3)
FA810721F5003THE BOEING COMPANYDepartment of Defense$2.99M
2021-06-302025-07-29336411B52 ENGINEERING SERVICES