FedTALLY

Awards for “boeing

25 awards on this page · sorted by amount · page 93

Award IDRecipientAwarding agencyAmountStartEndNAICSDescription
0125BELL BOEING JOINT PROJECT OFFICEDepartment of Defense$14.93M
2011-02-072023-03-31541330NON RECURRING ENGINEERING (NRE) FOR 13 HARNESS
FA868124FB062THE BOEING COMPANYDepartment of Defense$14.92M
2024-09-302027-09-01332993MOP GBU-57 WEAPON SYSTEM COMPONENT TEST ASSET REPLENISHMENT (TAR) WITHOUT TAIL-KITS
0012THE BOEING COMPANY (0674)Department of Defense$14.89M
2008-06-252011-09-30336413"I" AND "O" LEVEL PECULIAR SUPPORT EQUIPMENT
0095THE BOEING COMPANYDepartment of Defense$14.88M
2007-09-252020-09-30336411DELIVERY ORDER 0095 CMB
N0001923F0523INSITU, INC.Department of Defense$14.86M
2023-07-072024-10-30541330SCANEAGLE SPARES, AVS, SITE PREP AND ACTIVATION IN SUPPORT OF IRAQ BPC CASE NV-P-LB.
FA821423F0001THE BOEING COMPANYDepartment of Defense$14.83M
2023-02-022024-02-01541330GUIDANCE SUBSYSTEM SUSTAINMENT CONTRACT (GUSSC 2.0) - 2023 TASK ORDER
TH20THE BOEING COMPANYDepartment of Defense$14.81M
2012-09-202015-04-08334519STABILIZER,HORIZONT
2063THE BOEING COMPANYDepartment of Defense$14.81M
2015-09-162017-09-30336411ECP AFT FUSELAGE
FA852623F0008THE BOEING COMPANYDepartment of Defense$14.8M
2023-09-302026-09-30336411FY23 MATERIAL IMPROVEMENT PROGRAM MATERIAL
865WTHE BOEING COMPANYDepartment of Defense$14.79M
2013-04-192019-01-313364138500185105!SUPPORT,STRUCTURAL
0009THE BOEING COMPANYDepartment of Defense$14.77M
2012-03-142014-10-31336414OPTION PRICING FOR TEST KITS
W58RGZ23F0480THE BOEING COMPANYDepartment of Defense$14.76M
2023-10-012024-03-31336413PERFORMANCE BASED LOGISTICS SUPPORT FOR THE H-47 HELICOPTER FORWARD AND AFT BLADES AND ASSOCIATED CONTAINERS.
N6134019F0167THE BOEING COMPANYDepartment of Defense$14.76M
2019-09-252021-11-30333318THIS EFFORT IS FOR THE FY17 UPGRADES TO BE MADE TO THE EXISTING F/A-18E/F INTEGRATED VISUAL ENVIRONMENT MAINTENANCE TRAINERS (IVEMTS) AT CNATT UNITS OCEANA, VA., LEMOORE, CA. AND EA-18G IVEMT + G AT WHIDBEY ISLAND.
FA810721F5001THE BOEING COMPANYDepartment of Defense$14.75M
2021-01-012021-12-31336411RECURRING TASK ORDER FOR B52 ENGINEERING SERVICES.
0015THE BOEING COMPANY (0674)Department of Defense$14.73M
2013-09-192022-06-30334511NAVY AVIATION
0018THE BOEING COMPANYDepartment of Defense$14.72M
2011-09-112012-04-30541330UAS ISR SERVICES
SD07THE BOEING COMPANYDepartment of Defense$14.72M
2015-09-292019-01-25336411B-52 LOW RATE INITIAL PRODUCTION AND FULL RATE PRODUCTION
M0014605C9004BOEING AEROSPACE OPERATIONS, IDepartment of Defense$14.72M
2005-01-062009-01-29488190200512!150064!1700!M00146!RECEIVING OFFICER !M0014605C9004 !A!N! !N! ! !20050106!20060201!194293544!085188316!009256819!N!BOEING AEROSPACE OPERATIONS, I!2601 LIBERTY PKWY !MIDWEST CITY !OK!73110!00000! !IZ!* !* !IRAQ !+000003919283!N!N!000013977973!J015!MAINT & REPAIR OF EQ/AIRCRAFT STRUCTURAL COMPS !S1 !SERVICES !000 !* !488190!E! !3! ! ! ! ! !20200930!B! ! !A! !D!U!Y!1!001!N!1A!Z!Y!Z! ! !N!M!N! ! ! ! ! !A!A!000!A!B!N! ! !Y!Y!1727!V09167!0001! !
0011THE BOEING COMPANYDepartment of Defense$14.7M
2014-07-172019-06-30336411IFG:OT:IFG AIRCRAFT MODE 5 MATERIAL
NNL11AA68TTHE BOEING COMPANYNational Aeronautics and Space Administration$14.7M
2011-05-172015-08-31541712SMAAART TASK ORDER: STATEMENT OF WORK (SOW.) TASK TITLE: HWB MULTI BAY TEST ARTICLE ANALYSIS AND ASSEMBLY 1.0 INTRODUCTION/BACKGROUND: NASA CREATED THE ENVIRONMENTALLY RESPONSIBLE AVIATION (ERA) PROJECT TO EXPLORE AND DOCUMENT THE FEASIBILITY, BENEFITS, AND TECHNICAL RISK OF VEHICLE CONCEPTS AND ENABLING TECHNOLOGIES THAT WILL REDUCE THE IMPACT OF AVIATION ON THE ENVIRONMENT. TODAY'S CURRENT GENERATION OF AIRCRAFT HAS BENEFITTED FROM NASA INVESTMENTS IN AERONAUTICAL RESEARCH THAT HAVE IMPROVED FUEL EFFICIENCIES, LOWERED NOISE LEVELS, AND LESSENED HARMFUL EMISSIONS. ALTHOUGH SUBSTANTIAL PROGRESS HAS BEEN MADE, MUCH MORE NEEDS TO BE DONE. THE NATION'S AIR TRANSPORTATION SYSTEM WILL EXPAND BY A FACTOR OF TWO OR THREE WITHIN THE NEXT TWO DECADES, POTENTIALLY INCREASING AVIATION'S CONTRIBUTION TO CLIMATE CHANGE. THE ERA PROJECT WORKS TO REDUCE THE ENVIRONMENTAL HARM THAT COULD RESULT FROM SUCH AN EXPANSION. AMONG THE TECHNOLOGIES TO BE EXPLORED IN THE ERA PROJECT ARE THE FOLLOWING: UNCONVENTIONAL AIRCRAFT CONFIGURATIONS THAT HAVE HIGHER LIFT TO DRAG RATIO, REDUCED DRAG AND REDUCED COMMUNITY NOISE; DRAG REDUCTION THROUGH LAMINAR FLOW; ADVANCED COMPOSITE STRUCTURAL CONCEPTS FOR WEIGHT REDUCTION; LOW NOX COMBUSTORS; AND PROPULSION AND AIRFRAME INTEGRATION FOR NOISE REDUCTION AND FUEL-BURN IMPROVEMENTS. THE ERA PROJECT WILL FOCUS ON ENVIRONMENTAL ISSUES ASSOCIATED WITH AIRCRAFT, INCLUDING FUEL BURN, EMISSIONS, AND NOISE. THE PROJECT WILL EXPLORE AND DOCUMENT THE FEASIBILITY, BENEFITS, AND TECHNICAL RISK OF VEHICLE CONCEPTS AND ENABLING TECHNOLOGIES IDENTIFIED TO HAVE THE POTENTIAL TO MITIGATE THE IMPACT OF AVIATION ON THE ENVIRONMENT. THIS RESEARCH DIRECTLY SUPPORTS THE NATIONAL AERONAUTICS RESEARCH AND DEVELOPMENT POLICY TO DEVELOP APPROPRIATE ENVIRONMENTAL PROTECTION MEASURES TO ENSURE CONTINUED GROWTH IN AIR TRANSPORTATION. 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 TO THE ENVIRONMENT. THE APPROACH MOVES FROM SAFE-LIFE TO FAIL-SAFE DESIGN WITH A LIGHTWEIGHT COMPOSITE STRUCTURE. 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) OR BLENDED WING BODY (BWB) 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 HYBRID WING BODY (HWB) PULTRUDED ROD STITCHED EFFICIENT UNITIZED STRUCTURE (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 CAP
FA865019F2413THE BOEING COMPANYDepartment of Defense$14.7M
2019-01-302025-12-01541712IGF::OT::IGF BOEING LOCKHEED OR NORTHROP DEMONSTRATION INCLUDING ENGINE
0019THE BOEING COMPANYDepartment of Defense$14.7M
2011-09-112012-04-30541330UAS ISR SERVICES
N0001923F2630THE BOEING COMPANYDepartment of Defense$14.7M
2023-08-212028-06-01336412EN JOINT COMMON TEST SET
0001THE BOEING COMPANYDepartment of Defense$14.69M
2012-09-282023-06-30541712IGF::OT::IGF EATTS3 TASK ORDER 0001 AH 64D PRIORITY PARTS FATIGUE TESTING - PHASE II
0387THE BOEING COMPANYDepartment of Defense$14.69M
2015-07-162018-07-31336411ECP 6460 "AESA MULTI-MODULE REDESIGN"