THE BOEING COMPANY
Federal contractor profile
Intelligence Summary
# Boeing Company - Vendor Assessment
## Agency Concentration Risk
Boeing demonstrates extreme concentration risk, with the Department of Defense accounting for 69% ($145.9B) of total obligated value across 968 awards. NASA represents the secondary revenue stream at 30.6% ($64.5B) with only 18 awards, indicating high-value contract dependency. Combined, these two agencies represent 99.6% of Boeing's federal portfolio, leaving minimal diversification across the remaining 6 agencies. This concentration creates significant vulnerability to budget fluctuations, policy shifts, or contract competition within defense and space sectors.
## Contract Expiry Exposure
Boeing faces substantial near-term renewal risk with $121.6B (57.7%) of total obligated value expiring within 18 months. This represents a critical recompete window, particularly concerning given the concentration within DoD and NASA contracts. The expiration timeline necessitates aggressive capture and proposal management strategies to maintain revenue continuity.
## NAICS Diversification
Boeing operates across 10 NAICS codes with heavy specialization in aerospace manufacturing. Aircraft parts manufacturing (336413) dominates with 476 awards, followed by aircraft manufacturing (336411) with 134 awards. These two codes represent the core business. Engineering services (541330) provides modest diversification with 72 awards, but overall portfolio remains tightly focused on aerospace production and related technical services.
## Strategic Outlook
Boeing's federal contracting position remains strategically strong but operationally constrained. The company must prioritize DoD and NASA contract renewals while exploring adjacent defense technology markets to reduce agency concentration. Expansion into emerging areas like space logistics, advanced manufacturing, or cybersecurity could provide portfolio resilience.
Generated May 31, 2026
Top Agencies
| Agency | Awards | Total Obligated |
|---|---|---|
| Department of Defense | 968 | $145.9B |
| National Aeronautics and Space Administration | 18 | $64.5B |
| Department of Energy | 4 | $192.2M |
| General Services Administration | 2 | $14.9M |
| Department of the Treasury | 4 | $4.5M |
| Department of Transportation | 1 | $2.3M |
| Department of State | 2 | $2.0M |
| Department of Justice | 1 | $154,315 |
Top NAICS Codes
| NAICS Code | Description | Awards |
|---|---|---|
| 336413 | OTHER AIRCRAFT PARTS AND AUXILIARY EQUIPMENT MANUFACTURING | 476 |
| 336411 | AIRCRAFT MANUFACTURING | 134 |
| 334511 | SEARCH, DETECTION, NAVIGATION, GUIDANCE, AERONAUTICAL, AND NAUTICAL SYSTEM AND INSTRUMENT MANUFACTURING | 94 |
| 541330 | ENGINEERING SERVICES | 72 |
| 336412 | AIRCRAFT ENGINE AND ENGINE PARTS MANUFACTURING | 38 |
| 488190 | OTHER SUPPORT ACTIVITIES FOR AIR TRANSPORTATION | 26 |
| 541511 | - | 26 |
| 541512 | - | 24 |
| 336414 | GUIDED MISSILE AND SPACE VEHICLE MANUFACTURING | 12 |
| 332993 | AMMUNITION (EXCEPT SMALL ARMS) MANUFACTURING | 11 |
Expiring Contracts (439)
INTERNATIONAL SPACE STATION
USN P-8A FRP II LONG LEAD MATERIAL
USN P-8A FRP II LONG LEAD MATERIAL
USN P-8A FRP II LONG LEAD MATERIAL
PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION; AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS; THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE; AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT.
F-15, FMS, F-15QA AIR VEHICLE DEVELOPMENT
KC-X MODERNIZATION PROGRAM
W58RGZ-16-C-0023 IS FOR THE AWARD OF ADVANCE PROCUREMENT IN THE AMOUNT OF $184,930,000.00 TO SUPPORT LOT 7 FULL RATE PRODUCTION LONG LEAD ITEMS.
28 KUWAIT KAF-18E/F AIRCRAFT AND 56 COMMERCIAL PXMC CARDS
28 KUWAIT KAF-18E/F AIRCRAFT AND 56 COMMERCIAL PXMC CARDS
F15EX LOT 2 LONG LEAD-ITEMS
F-15EX LOT 3 LONG-LEAD ITEMS
F-15EX LOT 3 LONG-LEAD ITEMS
LOT 91 PRODUCTION LONG LEAD ITEMS
F-15 EAGLE PASSIVE/ACTIVE WARNING & SURVIVABILITY SYSTEM (EPAWSS) LOW RATE ININITIAL PRODUCTION (LRIP)
F-15; ACAT II: RMP/V3 COMBINED RADAR BUY FY15
B-52 RADAR MODERNIZATION PROGRAM ENGINEERING AND MANUFACTURING DEVELOPMENT
APACHE PERFORMANCE BASED LOGISTICS(PBL) IV SERVICES OF AIRFRAME COMPONENTS FOR THE UNITED STATES GOVERNMENT'S AH-64 APACHE FLEET
MH-47G BLKII LOT 4 PRODUCTION
FY26 MXMODS ORDER ORDERING PERIOD VI 01 NOV 2025 - 31 OCT 2026
EAGLE TALON II/FULL RATE PRODUCTION 6-8 FISCAL YEAR 19-21
EAGLE TALON II/FULL RATE PRODUCTION 6-8 FISCAL YEAR 19-21
CH-47F AIRCRAFT PROCUREMENT
IGF::OT::IGF THE COMMERCIAL CREW PROGRAM (CCP) COMMERCIAL CREW TRANSPORTATION CAPABILITY (CCTCAP) CONTRACT WILL PROVIDE COMPLETION OF THE DESIGN, DEVELOPMENT, TEST, EVALUATION, AND CERTIFICATION OF AN INTEGRATED CREW TRANSPORTATION SYSTEM (CTS) CAPABLE OF TRANSPORTING NASA CREW TO AND FROM THE ISS, IN ACCORDANCE WITH THE DESIGN REFERENCE MISSIONS AND NASA'S CERTIFICATION STANDARDS AND REQUIREMENTS. CERTIFICATION OF THE CTS WILL BE DETERMINED BY NASA. NASA PLANS TO ISSUE TASK ORDERS FOR POST CERTIFICATION MISSIONS (PCM) TO AND FROM ISS THAT INCLUDE GROUND, LAUNCH, LIFEBOAT, ON-ORBIT, RETURN AND RECOVERY OPERATIONS. THE MINIMUM QUANTITY OF MISSIONS TO BE ORDERED IS TWO (2) AND THE MAXIMUM POTENTIAL QUANTITY OF MISSIONS WHICH MAY BE ORDERED IS SIX (6). IN ADDITION, NASA MAY ISSUE TASK ORDERS FOR SPECIAL STUDIES USED FOR RISK REDUCTION AND OTHER PURPOSES RELATED TO THE CTS. NASA CERTIFICATION UNDER CLIN 001 IS COMPLETE WHEN THE CONTRACTOR'S CREW TRANSPORTATION SYSTEM (CTS) HAS MET NASA S REQUIREMENTS FOR SAFELY TRANSPORTING CREW TO AND FROM THE INTERNATIONAL SPACE STATION (ISS) IN ACCORDANCE WITH DOCUMENTS IDENTIFIED IN SECTION C.1, SPECIFICATIONS/STATEMENT OF WORK. SUBCLINS 001A AND 001B, IDENTIFIED IN TABLE B.3, DDTE/CERTIFICATION SUBCLINS, ARE DELIVERY MILESTONES THAT REPRESENT COMPLETION OF REQUIRED WORK NECESSARY TO ACHIEVE NASA CERTIFICATION. DELIVERY PAYMENT FOR THE ISS DESIGN CERTIFICATION REVIEW (DCR) FOR THE CREWED FLIGHT TO THE ISS INCLUDES ALL WORK UNDER THIS CLIN THAT OCCURS FROM THE CONTRACT EFFECTIVE DATE THROUGH THE ISS DCR COMPLETION. THE DELIVERY PAYMENT FOR THE CERTIFICATION REVIEW (CR) WILL INCLUDE ALL WORK THAT OCCURS FROMTHE ISS DCR DELIVERY DATE THROUGH THE END OF THE DDTE/CERTIFICATION CLIN 001. IN ACCORDANCE WITH CLAUSE C.1, SPECIFICATION/STATEMENT OF WORK, THE TASK ORDERING PROCEDURES AND OTHER TERMS AND CONDITIONS IN THE CONTRACT, THE CONTRACTING OFFICER MAY ISSUE POST CERTIFICATION MISSION (PCM) TASK ORDERS. THE CONTRACTOR SHALL USE THE MISSION PRICING RATES SHOWN IN TABLE B.4.1, POST CERTIFICATION MISSION PRICES. THE PER MISSION PRICES ARE FOR A SINGLE ORDER AT THE PRICE STATED PER THE CALENDAR YEAR (CY) BASED ON THE NUMBER OF MISSIONS ORDERED. CTS FULL MISSION CAPABILITY PRICES SHALL BE BASED ON (1) FULFILLMENT OF THE DESIGN REFERENCE MISSION TO THE ISS FOUND IN CCT-DRM-1110, CREW TRANSPORTATION SYSTEM DESIGN REFERENCE MISSIONS, ATTACHMENT J-03, CONTRACT PERFORMANCE WORK STATEMENT, AND OTHER TERMS AND CONDITIONS IN THE CONTRACT AND (2) ALL INHERENT CTS CAPABILITIES THAT ARE WITHIN THE PROPOSED MISSION PRICES. IN ACCORDANCE WITH ATTACHMENT J-03, CONTRACT PERFORMANCE WORK STATEMENT, THE TASK ORDERING PROCEDURES AND OTHER TERMS AND CONDITIONS IN THE CONTRACT, THE CONTRACTOR SHALL PERFORM SPECIAL STUDIES, TEST AND ANALYSES, AS INITIATED BY WRITTEN DIRECTION FROM THE CONTRACTING OFFICER. BOEING CCTCAP POST CERTIFICATION MISSION 1 (PCM-1) TASK ORDER AGAINST NNK14MA75C CLIN 002, AS DESCRIBED IN CLAUSE B.4 POST CERTIFICATION MISSIONS (IDIQ)(CLIN 002) AND ALL OTHER APPLICABLE TERMS AND CONDITIONS.
P-8A INC 3 BLOCK 2 COMBAT SYSTEMS ARCHITECTURE HARDWARE AND SOFTWARE PLATFORM INTEGRATION DEVELOPMENT EFFORT TO IMPLEMENT ENGINEERING CHANGE PROPOSALS (ECPS) 6 AND 7.
MISSILE NRE
ELEMENT SYSTEM ENGINEERING
ANNUAL MATERIAL ORDERS PLACED DURING G3 PHASE II, ORDERING PERIODS VI (01 NOV 2025 - 31 OCT 2026)
STOKER 3.0 PROGRAM. A DELIVERY ORDER FOR JOINT DIRECT ATTACK MUNITIONS (JDAM) EXTENDED RANGE WING KITS UNDER CONTRACT FA8213-24-D-B002.
STOKER 3.0 PROGRAM. A DELIVERY ORDER FOR JOINT DIRECT ATTACK MUNITIONS (JDAM) EXTENDED RANGE WING KITS UNDER CONTRACT FA8213-24-D-B002.
ANNUAL MATERIAL ORDERS PLACED DURING G3 PHASE II, ORDERING PERIOD VI (01 NOV 2025 - 31 OCT 2026)
IGF::OT::IGF THE COMMERCIAL CREW PROGRAM (CCP) COMMERCIAL CREW TRANSPORTATION CAPABILITY (CCTCAP) CONTRACT WILL PROVIDE COMPLETION OF THE DESIGN, DEVELOPMENT, TEST, EVALUATION, AND CERTIFICATION OF AN INTEGRATED CREW TRANSPORTATION SYSTEM (CTS) CAPABLE OF TRANSPORTING NASA CREW TO AND FROM THE ISS, IN ACCORDANCE WITH THE DESIGN REFERENCE MISSIONS AND NASA'S CERTIFICATION STANDARDS AND REQUIREMENTS. CERTIFICATION OF THE CTS WILL BE DETERMINED BY NASA. NASA PLANS TO ISSUE TASK ORDERS FOR POST CERTIFICATION MISSIONS (PCM) TO AND FROM ISS THAT INCLUDE GROUND, LAUNCH, LIFEBOAT, ON-ORBIT, RETURN AND RECOVERY OPERATIONS. THE MINIMUM QUANTITY OF MISSIONS TO BE ORDERED IS TWO (2) AND THE MAXIMUM POTENTIAL QUANTITY OF MISSIONS WHICH MAY BE ORDERED IS SIX (6). IN ADDITION, NASA MAY ISSUE TASK ORDERS FOR SPECIAL STUDIES USED FOR RISK REDUCTION AND OTHER PURPOSES RELATED TO THE CTS. NASA CERTIFICATION UNDER CLIN 001 IS COMPLETE WHEN THE CONTRACTOR'S CREW TRANSPORTATION SYSTEM (CTS) HAS MET NASA'S REQUIREMENTS FOR SAFELY TRANSPORTING CREW TO AND FROM THE INTERNATIONAL SPACE STATION (ISS) IN ACCORDANCE WITH DOCUMENTS IDENTIFIED IN SECTION C.1, SPECIFICATIONS/STATEMENT OF WORK. SUBCLINS 001A AND 001B, IDENTIFIED IN TABLE B.3, DDTE/CERTIFICATION SUBCLINS, ARE DELIVERY MILESTONES THAT REPRESENT COMPLETION OF REQUIRED WORK NECESSARY TO ACHIEVE NASA CERTIFICATION. DELIVERY PAYMENT FOR THE ISS DESIGN CERTIFICATION REVIEW (DCR) FOR THE CREWED FLIGHT TO THE ISS INCLUDES ALL WORK UNDER THIS CLIN THAT OCCURS FROM THE CONTRACT EFFECTIVE DATE THROUGH THE ISS DCR COMPLETION. THE DELIVERY PAYMENT FOR THE CERTIFICATION REVIEW (CR) WILL INCLUDE ALL WORK THAT OCCURS FROMTHE ISS DCR DELIVERY DATE THROUGH THE END OF THE DDTE/CERTIFICATION CLIN 001. IN ACCORDANCE WITH CLAUSE C.1, SPECIFICATION/STATEMENT OF WORK, THE TASK ORDERING PROCEDURES AND OTHER TERMS AND CONDITIONS IN THE CONTRACT, THE CONTRACTING OFFICER MAY ISSUE POST CERTIFICATION MISSION (PCM) TASK ORDERS. THE CONTRACTOR SHALL USE THE MISSION PRICING RATES SHOWN IN TABLE B.4.1, POST CERTIFICATION MISSION PRICES. THE PER MISSION PRICES ARE FOR A SINGLE ORDER AT THE PRICE STATED PER THE CALENDAR YEAR (CY) BASED ON THE NUMBER OF MISSIONS ORDERED. CTS FULL MISSION CAPABILITY PRICES SHALL BE BASED ON (1) FULFILLMENT OF THE DESIGN REFERENCE MISSION TO THE ISS FOUND IN CCT-DRM-1110, CREW TRANSPORTATION SYSTEM DESIGN REFERENCE MISSIONS, ATTACHMENT J-03, CONTRACT PERFORMANCE WORK STATEMENT, AND OTHER TERMS AND CONDITIONS IN THE CONTRACT AND (2) ALL INHERENT CTS CAPABILITIES THAT ARE WITHIN THE PROPOSED MISSION PRICES. IN ACCORDANCE WITH ATTACHMENT J-03, CONTRACT PERFORMANCE WORK STATEMENT, THE TASK ORDERING PROCEDURES AND OTHER TERMS AND CONDITIONS IN THE CONTRACT, THE CONTRACTOR SHALL PERFORM SPECIAL STUDIES, TEST AND ANALYSES, AS INITIATED BY WRITTEN DIRECTION FROM THE CONTRACTING OFFICER. BOEING CCTCAP POST CERTIFICATION MISSION 2 (PCM-2) TASK ORDER AGAINST NNK14MA75C CLIN 002, AS DESCRIBED IN CLAUSE B.4 POST CERTIFICATION MISSIONS (IDIQ)(CLIN 002) AND ALL OTHER APPLICABLE TERMS AND CONDITIONS.
JAPAN AWACS MISSION COMPUTING UPGRADE (MCU) INSTALLATION&CHECKOUT (I&CO)
H20 SYSTEM CONFIGURATION SETS
ACQUISITION OF JDAM SABR-Y TAIL KITS FOR USAF AND USN.
GROUND-BASED MIDCOURSE DEFENSE READINESS
KOSS - UNDEFINITIZED DELIVERY ORDER
ADVANCED PILOT TRAINING
FY26 VIRTUAL FLEET COMMON AND UNIQUE LABOR SUSTAINMENT FOR C17 FLEET
F-15 -- RAPID RESPONSE DELIVERY ORDER
PARTS KIT,LANDING G
LAD/LPHUD REPAIR
SYSTEMS ENGINEERING AND INTEGRATION SERVICES
ENGINEERING SUPPORT SERVICES FOR MULTIPLE PLATFORMS.
ENGINEERING SUPPORT SERVICES OPTION YEAR IV IN SUPPORT OF MULTIPLE AIRCRAFT PLATFORMS.
CH-47 AIRCRAFT
SOFTWARE DEVELOPMENT
CIDD27 SYSTEM CONFIGURATION SET ORDER
CIDD27 SYSTEM CONFIGURATION SET ORDER
ENGINEERING SUPPORT SERVICES FOR MULTIPLE PLATFORMS.
E-4B PROGRAMMED DEPOT MAINTENANCE FOR A/C 74-0787
F-15 MUOS/SATURN PHASE 1
SPACE BASED SPACE SURVEILLANCE (SBSS) BLOCK 10 SUSTAINMENT CONTRACT
CIDD26 SYSTEM CONFIGURATION SET TASK ORDER
CIDD26 SYSTEM CONFIGURATION SET TASK ORDER
DCP CCA FIRST ARTICLE AND PRODUCTION UNITS
F-15 SCAT IV, FLIGHT TEST SUPPORT 2023-2028
F/A-18 AND EA-18G SYSTEMS CONFIGURATION SETS (SCS) SUPPORT -- GENERAL ENGINEERING TASK ORDER
F/A-18 AND EA-18G SYSTEMS CONFIGURATION SETS (SCS) SUPPORT -- GENERAL ENGINEERING TASK ORDER
FLIGHT TEST TELEMETRY AND TERMINATION (FT3) PRODUCTION FOR THE MMIII PROGRAM
F/A-18E/F SAT & FRCSW SLM AIRCRAFT
F-15 REPAIR RETURN SUPPORT (RRS) SERVICES IN SUPPORT OF THE ROYAL SAUDI AIR FORCE (RSAF)
F-15 REPAIR RETURN SUPPORT (RRS) SERVICES IN SUPPORT OF THE ROYAL SAUDI AIR FORCE (RSAF)
H12K SYSTEM CONFIGURATION SET TASK ORDER
UCA 2.0 FOR THE C-17 TRAINING SYSTEM TO PROVIDE ESSENTIAL TRAINING AND SUPPORT AS A BRIDGE CONTRACT.
F/A-18 KUWAIT INSTRUCTOR PILOT
DESIGN AND DEVELOPMENT, QUALIFICATION UNITS, VAL/VER KITS, RECURRING RETROFIT KITS
MAINTENANCE AND OVERHAUL OF 2 NSNS, FWD AND AFT ROTARY BLADES FOR THE CHINOOK WEAPON SYSTEM AND ASSOCIATED CDRLS.
TAIWAN APACHE AIRFRAME POST PRODUCTION SUPPORT SERVICE TASK ORDER
WING SECTION,INNER
DVRS TECHNICAL REFRESH JAX/WHIDBEY/RAAF WTT/OFT/BDS
POST PRODUCTION SUPPORT SERVICES (PPSS) IN SUPPORT OF SAUDI ARABIA MINISTRY OF NATIONAL GUARD (MNG)
1-YEAR NTE BASE AWARD OF A UCA TO PROVIDE MAINTENANCE AUGMENTATION TEAM (MAT) SERVICES FOR THE QATAR ARMED FORCES (QAF) CONSISTING OF 24 AH-64E APACHE AIRCRAFT. THIS IS A FOLLOW-ON EFFORT TO CONTRACT W58RGZ-19-C-0008.
H18 SCS/OFP/BLK III IVEMT SOFTWARE UPGRADE AND ANCILLARY ITEMS IN SUPPORT OF RAAF.
F/A-18 AND EA-18G FISCAL YEAR 2025 CAPABILITIES PRODUCTION SYSTEM CONFIGURATION SET (SCS) SUPPORT
MULTIFUNCTIONAL INFORMATION DISTRIBUTION SYSTEM (MIDS) - JOINT TACTICAL RADIO SYSTEM (JTRS) UPGRADE (MJU) - BOEING SUPPORT
SPARES ORDER FOR E4B AIRCRAFT ON CONTRACTOR LOGISTICS SUPPORT CONTRACT
F/A-18 AND EA-18G FISCAL YEAR 2025 CAPABILITY DEVELOPMENT FOR SYSTEM CONFIGURATION SETS (SCS).
CONTINUED SUSTAINMENT OF JAPAN AIRBORNE WARNING AND CONTROL SYSTEM E-767 MISSION SYSTEMS AND GROUND SYSTEMS WITH CONTRACTOR LOGISTICS SUPPORT (CLS)
PADS CEUI UPDATE FOR MINUTE MAN III MISSLE
PADS CEUI UPDATE FOR MINUTE MAN III MISSLE
FLIGHT TEST TELEMETRY AND TERMINATION (FT3) PRODUCTION FOR THE MMIII PROGRAM
B-1 B-52 ENGINEERING SERVICES
THIS EFFORT IS FOR THE PROCUREMENT OF STRUCTURAL REPAIR MANUAL (SRM) TOOLING, WHICH CONSISTS OF PECULIAR SUPPORT EQUIPMENT (PSE) AND NONDESTRUCTIVE INSPECTION (NDI) KITS.
P-8A CONTRACTOR LOGISTICS SUPPORT TO THE ROYAL NEW ZEALAND AIR FORCE
P-8A CONTRACTOR LOGISTICS SUPPORT TO THE ROYAL NEW ZEALAND AIR FORCE
B-1/B-52 ENGINEERING SERVICES
WING ASSEMBLY,AIRCR
OCONUS CONTRACTOR LOGISTICS SUPPORT FOR FMS GERMANY P-8A AIRCRAFT.
VERTICAL STABILATOR HOIST
ACTC LEVEL 1 TRAINING DEVELOPMENT PART 1
FY21 USN SPARE PARTS
C-17 SOFTWARE UPGRADE SERVICES FOR INDIA AND UAE
NON-RECURRING ENGINEERING SUSTAINMENT SERVICES IAW PWS EA-CUI-25C135-02-BCR1
REPAIR OF AIRCRAFT GUIDANCE AND NAVIGATION INSTRUMENTS.
IGF::CT::IGF THE PURPOSE OF THIS CONTRACT IS TO PROVIDE ENGINEERING SERVICES FOR THE GUIDANCE SYSTEM OF THE MINUTEMAN III MISSILE.
REPAIR OF AVIATION NAVIGATIONAL AND GUIDANCE INSTRUMENTS
REIMBURSABLE SERVICES AT SANTA SUSANA FIELD LABORATORY (SSFL)
B61-12 TAIL KIT ASSEMBLY TEST VARIANT SERVICES
ENGINEERING SERVICES IN SUPPORT OF PRESIDENTIAL NAOC AIRCRAFT
JOINT DIRECT ATTACK MUNITIONS GBU-56V3 INTEGRATION AND FIELDING
REPAIR OF AIRCRAFT GUIDANCE AND NAVIGATIONAL INSTRUMENTS
REPAIR OF AIRCRAFT GUIDANCE AND NAVIGATIONAL INSTRUMENTS
RESEARCH AND DEVELOPMENT
DEVELOP, INTEGRATE, AND DEMONSTRATE A MARITIME SEEKER.
FIRST YEAR CPFF DO FOR AH64 CH47 GLOBAL MATERIAL SUPPORT (UNPRICED ITEMS)
THIS REQUIREMENT IS TO BRING ALL FMS PARTNERS' SOFTWARE TO CONFIGURATION READY TO RECEIVE BLOS UPGRADE.
RESEARCH AND DEVELOPMENT
THE OBJECTIVE OF THIS EFFORT IS TO CONTINUE THE OPERATIONS AND MAINTENANCE OF THE AITS LABS TO THE UNITED STATES AIR FORCE (USAF) IN SUPPORT OF INTERNATIONAL AWACS PROGRAMS.
2025 LGSE3 SUPPORT
REPAIR OF AIRCRAFT GUIDANCE AND NAVIGATION EQUIPMENT.
VIRTUAL BLACK FLAG 26-27 (VBF 26-27)
F-15 AIRCRAFT STRUCTURAL INTEGRITY PROGRAM (ASIP) IN SUPPORT OF ROYAL SAUDI AIR FORCE (RSAF)
REPAIR OF THE ACQ-7 INTEGRATED CONVENTIONAL STORES MANAGEMENT SYSTEM (ICSMS)
B-1 ENGINEERING SERVICES (BBES)
ENGINEERING SUPPORT - DEU YEAR 1
REPAIR OF AIRCRAFT GUIDANCE AND NAVIGATION EQUIPMENT.
APS PALLET
RADIO SET
SUBSCRIPTIONS, DATABASES, AND LICENSES.
C-32/C-40 SUSTAINMENT TRAINING 2026
THE BOEING COMPANY CONTRACT TBD TO FUND FUTURE AIR NAVIGATION SYSTEM FANS SUPPORT CLIN 1000 FANS 1A PROBLEM EVALUATION BASE YEAR
THE PURPOSE OF THIS FIRM FIXED PRICED PURCHASE ORDER IS TO PROCURE BRAND NAME BOEING MULTIMEDIA MESSAGE MANAGER (M3) MAINTENANCE SUPPORT.
REPAIR OF GUIDANCE AND NAVIGATION COMPONENTS (MULTI NSN)
MULTIPLATFORM ENGINEERING SERVICES
REPAIR OF AIRCRAFT GUIDANCE AND NAVIGATION INSTRUMENTS.
REPAIR OF AIRCRAFT GUIDANCE AND NAVIGATION INSTRUMENTS.
PURCHASING E4B CONTRACTOR LOGISTICS SERVICES
PURCHASING E4B CONTRACTOR LOGISTICS SERVICES
T-7A MISSION MANAGEMENT PROCESSOR (MMP) STUDY POP: 12 MONTHS FROM DATE OF AWARD
SPARES ORDER
P-8A SYSTEMS AND SOFTWARE ENGINEERING PLATFORM SUSTAINMENT REQUIREMENTS DEVELOPMENT SUPPORT AND GENERAL REPORTING
CORPORATE BASIC ORDERING AGREEMENT (BOA) WITH THE BOEING COMPANY AND NAVAL AIR SYSTEMS COMMAND. (FPA)
ASIP MINI-TEARDOWN NRE DESCRIBES THE SERVICES REQUIRED TO DEVELOP A SERIES OF HEAVY MAINTENANCE (HM) TASKS. JCN-TBC-G3_WR-0059
DO 3 P8A AIRCRAFT SPARE PARTS
UAE REGRESSION TEST
CORPORATE BASIC ORDERING AGREEMENT (BOA) WITH THE BOEING COMPANY AND NAVAL AIR SYSTEMS COMMAND. (FPA)
CORPORATE BASIC ORDERING AGREEMENT (BOA) WITH THE BOEING COMPANY AND NAVAL AIR SYSTEMS COMMAND. (FPA)
ENGINEERING SUPPORT SERVICES (ESS) TO FOR TECHNICAL TASKINGS DIRECTIVES (TTD)
ENGINEERING SUPPORT SERVICES (ESS) TO FOR TECHNICAL TASKINGS DIRECTIVES (TTD)
SERVOCYLINDER
SOFTWARE LICENSES UPDATES
F-15//EAGLE TALON II//TESN
PROGRAM SUPPORT FOR INTEGRATION OF THE SDBII WEAPON (GBU-53/B) AND FUTURE MINIATURE MUNITION VARIANTS ONTO USAF AND DON AIRCRAFT.
VALUE SELF-SEALING MATERIALS FOR FUEL BLADDERS
8510357597!DAMPER,AIR DUCT
PROBE,REFUELING,AIR
PROBE,REFUELING,AIR
KC-46 FMS ISRAEL - SUPPORT EQUIPMENT ORDER (BOEING), OFF OF THE KC-46 SUPPORT EQUIPMENT (KSE) MULTIPLE AWARD PROGRAM. PROPOSAL IDENTIFIER: FA860924RB002 AMEND 002DATE: 20FEB2024
CYLINDER,ACTUATING,
JOINT DIRECT ATTACK MUNITION TAIWAN/MOROCCO INTEGRATION
JOINT DIRECT ATTACK MUNITION TAIWAN/MOROCCO INTEGRATION
8511723986!KEYBOARD,DATA ENTRY
8511774449!NUT,SELF-LOCKING,PL
WHEEL AND TIRE ASSY
PECULIAR SUPPORT EQUIPMENT (PSE) BUY ROYAL AUSTRALIAN AIR FORCE (RAAF)
PECULIAR SUPPORT EQUIPMENT (PSE) BUY ROYAL AUSTRALIAN AIR FORCE (RAAF)
E-3 AIRBORNE WARNING AND COMMUNICATIONS SYSTEM (AWACS) SUSTAINMENT ENGINEERING SERVICES
8511707427!SUPPORT,STRUCTURAL
A/MH-6R PRIMARY AIRCRAFT STRUCTURE (PAS) LIMITED FLIGHT LOAD SURVEY (LFLS)
DOOR,ACCESS,AIRCRAF
8511681847!ANTENNA
AIRBORNE WARNING AND COMMUNICATION SYSTEM (AWACS) SUSTAINMENT ENGINEERING SUPPORT
CONTRACTOR LOGISTICS SUPPORT FOR THE C-32/C-40 AIRCRAFT FLEETS
CONTROL UNIT,ANTIS,
C-32/C-40 CONTRACTOR LOGISTICS SUPPORT FLEET
8508658336!INNER WING INTERCHA
SLAT,AIRCRAFT
SPARES
CORPORATE BASIC ORDERING AGREEMENT (BOA) WITH THE BOEING COMPANY AND NAVAL AIR SYSTEMS COMMAND. (FPA)
MASP DRIVE
8511598084!RESTRICTOR,FLUID F
8511384296!BOLT,SHEAR
8511682343!HINGE ASSEMBLY,AIRC
8511739866!FILLER CAN,COLLECTO
COUPLER,ANTENNA
8509820316!BOLT ASSEMBLY,ROTAR
8506970845!HEAD,PISTON-SHOCK A
CHILLER
F/A-18E/F & EA-18G CHANGES (MODS)
F/A-18E/F & EA-18G CHANGES (MODS)
MASP DRIVE
8511688159!CLIP,RETAINING
DIGITAL COMP
DIGITAL COMP
ADVANCED AIRBORNE V
DIGITAL COMPUTER
COMPUTER DIGITAL
COMPUTER DIGITAL
COMPOUTER DIGITAL
COMPUTER DIGITAL
COMPUTER DIGITAL
INTERFACE UNIT
AFT PNEUMATIC SOURC
REPAIR OF PANEL,CONTROL, ELECT IN SUPPORT OF THE KC-46 AIRCRAFT.
REPAIR OF PANEL,CONTROL,ELECT IN SUPPORT OF THE KC-46 AIRCRAFT.
REPAIR OF PANEL,CONTROL,ELECT IN SUPPORT OF THE KC-46 AIRCRAFT.
REPAIR OF PANEL,CONTROL, ELECT IN SUPPORT OF THE KC-46 AIRCRAFT.
DIGITAL COMP
DIGITAL COMP
8511354421!SHEET,RESISTIVE
8511761297!SKIN,AIRCRAFT
KOREA SDB-I SIL TESTING
LEFT HAND LBI B
8511704811!BALANCE WEIGHT,ELEV
8511727016!WASHER,SPRING TENSI
8511727016!WASHER,SPRING TENSI
8511735236!RING,WING TANK ACCE
8511792454!STIFFENER,AIRCRAFT
CONTROLLER PRESS
MWS-LBI,RADOME
ACTUATOR MECHANICAL
8511682654!CABLE ASSEMBLY,POWE
8509929017!LATCH ASSEMBLY,AIRC
8509929017!LATCH ASSEMBLY,AIRC
REPAIR OF COMPRESSOR BLADE SETS IN SUPPORT OF THE KC46 AIRCRAFT
8511679011!SUPPORT,STRUCTURAL
SLAT BOX ASSEMBLY
COMMERCIAL AOG DELIVERY ORDER
8511688655!LIP,UPPER
8511688264!PANEL,STRUCTURAL,AI
CONTROL,INTERCOMMUN
8511723157!SKIN,AIRCRAFT
ACTUATOR,AUTOPILOT
8509167859!RIGGING,SET
8511761765!FITTING,STRUCTURAL
PANEL INDICATOR
NETHERLANDS SDB-I GBU-39/B SRR
COMM PROCESSOR
COMMUNICATOR PROCESSOR
8511753707!STIFFENER,AIRCRAFT
8511686623!TUBE ASSEMBLY, AIRCR
8510958102!TRANSFORMER,POWER
8509884292!DOOR,ACCESS,AIRCRAF
NAVIGATIONAL LIGHT
THE CONTRACTOR SHALL DELIVER FOUR (4) ELECTRICAL EXECUTION TESTING (ELX) TAILS. THE CONTRACTOR SHALL ACQUIRE ALL MATERIAL AND COMPONENTS NECESSARY TO PRODUCE THE FOUR (4) ELX TAILS, EXCEPT FOR THE ITEMS IDENTIFIED BY ATTACHMENT 2 IN SECTION J.
COMMERICAL AOG DELIVERY ORDER
8511694412!CABLE ASSEMBLY,SPEC
8511641328!SPROCKET WHEEL
8511732476!CABLE ASSEMBLY,SPEC
FAIRING,AIRCRAFT
8511716161!SUPPORT,STRUCTURAL
8509793599!SLING ASSEMBLY
8509834912!SLING ASSEMBLY
AIRCRAFT ELEVATOR
PANEL ASSEMBLY,AIRC
MID RH FITTING DEIC
ACTUATOR
8511758660!CABLE ASSEMBLY,SPEC
8511759520!STIFFENER,AIRCRAFT
NATO E-3 AIRBORNE WARNING AND COMMUNICATION SYSTEM (AWACS) SUSTAINMENT ENGINEERING AND TECHNICAL SUPPORT
PROBE,REFUELING,AIR
8511698616!HOUSING,MECHANICAL
8511707566!SUPPORT,STRUCTURAL
8511598335!FILTER,BAND PASS
ELECTRONIC COMPONEN
COMMUN PROCESSOR
SENSOR,SMOKE DETECT
8511734699!BUMPER
REPAIR OF POWER CONTROL ASSEMBLY IN SUPPORT OF THE KC-46 AIRCRAFT.
MISSION CRITICAL -IN SUPPORT OF LAW ENFORCEMENT OPERATIONS BOEING 737 FLIGHT OPERATIONS AND MAINTENANCE MANUALS
FAIRING,AIRCRAFT
CONTROL BOX,ELECTRI
AIR LAUNCH CRUISE MISSILE (ALCM) ENGINEERING SERVICES
8511702138!STIFFENER,AIRCRAFT
8507265594!DOOR,AIRCRAFT
8511687803!CLIP,RETAINING
8511042708!PROTECTIVE PLUG
LOCK LINEAR ACTUATO
8508612769!TUBE ASSEMBLY NOSE
BUTTERFLY VALVE
ANTENNA
ELECTRONIC COMPONEN
ADAPTER,TEST,MAVERI
8511697409!CONTROL PANEL,AIRCR
8511697409!CONTROL PANEL,AIRCR
8511737281!FIXTURE, AIRCRAFT MA
8511716108!SUPPORT,STRUCTURAL
8511726539!RETAINER,BEARING,LE
LIGHT ASSEMBLY
LIGHT ASSEMBLY
OVEN,WARMING,ELECTR
HYDRAULIC MOTOR
CYLINDER,ACTUATING,
8511651492!PANEL,STRUCTURAL,AI
8511001248!PIN-RIVET
POWER SUPPLY
CORPORATE BASIC ORDERING AGREEMENT (BOA) WITH THE BOEING COMPANY AND NAVAL AIR SYSTEMS COMMAND. (FPA)
INSULATION BLANKET,
8511100217!SUPPORT,STRUCTURAL
8511624036!SLING ASSY MAIN ROT
REPAIR OF DISPLAY UNIT, FLIGHT IN SUPPORT OF THE KC46 AIRCRAFT.
8511597130!PARTS KIT,FASTENER
8511769106!HINGE,ACCESS DOOR
NAVIGATIONAL
NRP,SLAT BOX SUB-AS
8508612079!SPECIAL KIT
8511636421!BOOT,ELASTOMERIC,AI
LEADING EDGE,AIRCRA
8511697317!SWITCH ASSEMBLY,STA
8510840853!CIRCUIT CARD ASSEMB
OTHER DIRECT COST
TEST ADAPTER SET
8511415810!SKIN,AIRCRAFT
NRP,SLAT BOX SUB-AS
8511285841!FITTING,STRUCTURAL
8511713193!END CAP,BLADE
8511721708!BRACKET,MOUNTING,AI
8511759601!PANEL,STRUCTURAL,AI
8511750212!NUT BLANK
8509844187!MODIFICATION KIT,AI
8509038761!ADAPTER,POWER PLANT
8511725817!FAIRING,TRAILING
8511758942!CONTROL ASSEMBLY,QU
8511752428!MAINTENANCE PLATFOR
8511716759!INSULATION PIPE COV
LH SHORT BASELINE I
8507332158!WIRING HARNESS,BRAN
8511774974!GAGE,PROFILE
8511774974!GAGE,PROFILE
8511707442!HINGE,ACCESS DOOR
8511711290!STIFFENER,AIRCRAFT
8511711290!STIFFENER,AIRCRAFT
8511699306!SKIN,AIRCRAFT
8511686649!SWITCH,TRIGGER
8511704643!FRAME,WINDOW,AIRCRA
8511694413!STIFFENER,AIRCRAFT
RADOME B387
8511747532!VALVE,FLOW CONTROL
8511707345!SUPPORT,STRUCTURAL
8511707345!SUPPORT,STRUCTURAL
8510500938!PLENUM,OXYGEN
8511723344!BALANCE WEIGHT,ELEV
8511723344!BALANCE WEIGHT,ELEV
REPAIR RECORDER, FLIGHT DAT
8511761346!MANIFOLD ASSEMBLY,H
8511731162!TUBE ASSEMBLY,METAL
8506730876!ANTENNA
8511306896!VHF UHF IFF ATC ANT
8511701446!PANEL,STRUCTURAL,AI
8511701480!STIFFENER,AIRCRAFT
8511728083!TRAILER,AIRCRAFT,TR
CIRCUIT CARD ASSEMB
CIRCUIT CARD ASSEMB
8511721920!PAWL,UPLATCH,ASSEMB
8511660804!FOOTREST,AIRCRAFT S
8509699642!CABLE ASSEMBLY,POWE
8511464943!SUPPORT,STRUCTURAL
8511701926!FASTENER,KIT
ACTUATOR,ELECTRO-PN
8511583396!WIRING HARNESS
8511583396!WIRING HARNESS
8510991230!CABLE ASSEMBLY,SPEC
8511586913!SEAT,AIRCRAFT
8511251887!PAD,CUSHIONING
SLAT,AIRCRAFT
SLAT,AIRCRAFT
8511753538!PARTS KIT,GRAPHITE
8511780692!FIXTURE,AIRCRAFT MA
8511728361!SKIN, UPPER SIDEFWD FUSE, Y20
8511728361!SKIN, UPPER SIDEFWD FUSE, Y20
8511755427!BOLT,FLUID PASSAGE
8510440500!TIE-ROD ASSEMBLY,AI
8511686551!CABLE ASSEMBLY,RADI
8511713992!BUSHING,SLEEVE
8511682107!PAWL,UPLATCH,ASSEMB
8511471954!RIB,ELEVATOR
8511697027!SHIM
8511730926!DUCT ASSEMBLY,TRANS
8511496392!COVER,ACCESS,AIRCRA
8509519443!SKIN,AIRCRAFT
8511761954!SPROCKET WHEEL
8511565593!PIN,STRAIGHT,HEADLE
8511532431!FAIRING ASSEMBLY,CA
8511716577!PIN ASSEMBLY,DRAG S
8511602666!CONNECTING LINK,RIG
8511714002!FITTING,STRUCTURAL
8511714002!FITTING,STRUCTURAL
8511775319!PANEL,FIRE DETECTIO
NRP,SPOILER ASSY -
NRP,INNER CYLINDER
8511743749!BOLT,MACHINE
8511774399!BRACKET,MOUNTING
8511519746!FITTING,STRUCTURAL
ACTUATOR,HYDRAULIC-
8511699528!PLATE,STRUCTURAL,AI
8511726941!DUCT,CABIN AIR
8511706836!HINGE,ACCESS DOOR
8511688949!CABLE ASSEMBLY,CONT
8511688949!CABLE ASSEMBLY,CONT
8511761482!SHAFT,SHOULDERED
8511522134!SCREW,MACHINE
8511213740!PRESSURE SEAL
8511213740!PRESSURE SEAL
8511730734!FRAME ASSY,AIRFRAME
8511701372!SUPPORT,STRUCTURAL
8511701372!SUPPORT,STRUCTURAL
8511689419!CABLE ASSEMBLY,SPEC
8511491272!SPACER,SLEEVE
8507171789!COVER,ACCESS,AIRCRA
8511688584!BEAM,AIRCRAFT
8511539073!SUPPORT,STRUCTURAL
8510977742!STIFFENER,AIRCRAFT
8511750124!PLATE,MOUNTING
8510775321!PACKING,PREFORMED
8511747828!BOLT,SHOULDER
8511640794!CABLE ASSEMBLY,SPEC
8511697205!BRACKET,STRUCTURAL
8511716001!TRUSS ASSEMBLY,AIRC
8511025170!LENS,LEVER,CONTROL
8511711697!SPLASH GUARD RETAIN
8511694398!LIGHT-SWITCH
8511610300!STIFFENER,AIRCRAFT
8511369742!STIFFENER,AIRCRAFT
8511695317!NONMETALLIC SPECIAL
8511682167!NONMETALLIC SPECIAL
OVEN,WARMING,ELECTR
OVEN,WARMING,ELECTR
8511774950!SUPPORT,STRUCTURAL
8511690802!COVER,ACCESS,AIRCRA
CABLE ASSEMBLY
COVER,ACCESS,AIRCRA
CANOPY
8511787225!COVER,CARGO HOOK,LH
8510962493!LENS,LEVER,CONTROL
8510962493!LENS,LEVER,CONTROL
8511695238!PLUG,PROTECTIVE,DUS
8511714293!LATCH ASSEMBLY,AIRC
8511768592!COVER ASSEMBLY,HARN
8511724002!FLOOR,AIRCRAFT
8511690903!PANEL,STRUCTURAL,AI
8511685046!CABLE,RADIO FREQUEN
8511774007!GASKET AND SEAL SET
8511743008!NONMETALLIC SPECIAL
8511720995!BOLT,MACHINE
8511720995!BOLT,MACHINE
8511301690!RETENTION CONNECTOR
8511157033!RETENTION CONNECTOR
All Awards
INTERNATIONAL SPACE STATION
USN P-8A FRP II LONG LEAD MATERIAL
USN P-8A FRP II LONG LEAD MATERIAL
USN P-8A FRP II LONG LEAD MATERIAL
PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION; AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS; THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE; AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT.
PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION; AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS; THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE; AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT.
PROVIDE DEVELOPMENTAL HARDWARE AND TEST ARTICLES, AND MANUFACTURE AND ASSEMBLE ARES I UPPER STAGES. THE UPPER STAGE (US) ELEMENT IS AN INTEGRAL PART OF THE ARES I LAUNCH VEHICLE AND PROVIDES THE SECOND STAGE OF FLIGHT. THE US ELEMENT IS RESPONSIBLE FOR THE ROLL CONTROL DURING THE FIRST STAGE BURN AND SEPARATION; AND WILL PROVIDE THE GUIDANCE AND NAVIGATION, COMMAND AND DATA HANDLING, AND OTHER AVIONICS FUNCTIONS FOR THE ARES I DURING ALL PHASES OF THE ASCENT FLIGHT. THE US ELEMENT IS A NEW DESIGN THAT EMPHASIZES SAFETY, OPERABILITY, AND MINIMUM LIFE CYCLE COST. THE OVERALL DESIGN, DEVELOPMENT, TEST AND EVALUATION (DDT&E), PRODUCTION, AND SUSTAINING ENGINEERING EFFORTS INCLUDE ACTIVITIES PERFORMED BY THREE ORGANIZATIONS; THE NASA DESIGN TEAM (NDT), THE UPPER STAGE PRODUCTION CONTRACTOR (USPC) AND THE INSTRUMENT UNIT PRODUCTION CONTRACTOR (IUPC). FOR CLARITY, THE USPC WILL BE REFERRED TO AS THE CONTRACTOR THROUGHOUT THIS DOCUMENT. NASA IS RESPONSIBLE FOR THE INTEGRATION OF THE PRIMARY ELEMENTS OF THE ARES I LAUNCH VEHICLE INCLUDING: THE FIRST STAGE, US INCLUDING INSTRUMENT UNIT (IU), AND US ENGINE; AND WILL ALSO INTEGRATE THE ARES I LAUNCH VEHICLE AT THE LAUNCH SITE. NASA IS RESPONSIBLE FOR THE DDT&E, INCLUDING TECHNICAL AND PROGRAMMATIC INTEGRATION OF THE US SUBSYSTEMS AND GOVERNMENT-FURNISHED PROPERTY. NASA WILL LEAD THE EFFORT TO DEVELOP THE REQUIREMENTS AND SPECIFICATIONS OF THE US ELEMENT, THE DEVELOPMENT PLAN AND TESTING REQUIREMENTS, AND ALL DESIGN DOCUMENTATION, INITIAL MANUFACTURING AND ASSEMBLY PROCESS PLANNING, LOGISTICS PLANNING, AND OPERATIONS SUPPORT PLANNING. DEVELOPMENT, QUALIFICATION, AND ACCEPTANCE TESTING WILL BE CONDUCTED BY NASA AND THE CONTRACTOR TO SATISFY REQUIREMENTS AND FOR RISK MITIGATION. NASA IS RESPONSIBLE FOR THE OVERALL UPPER STAGE VERIFICATION AND VALIDATION PROCESS AND WILL REQUIRE SUPPORT FROM THE CONTRACTOR. THE CONTRACTOR IS RESPONSIBLE FOR THE MANUFACTURE AND ASSEMBLY OF THE UPPER STAGE TEST FLIGHT AND OPERATIONAL UPPER STAGE UNITS INCLUDING THE INSTALLATION OF UPPER STAGE INSTRUMENT UNIT, THE GOVERNMENT-FURNISHED US ENGINE, BOOSTER SEPARATION MOTORS, AND OTHER GOVERNMENT-FURNISHED PROPERTY. A DESCRIPTION OF THE NASA MANAGED AND PERFORMED EFFORTS IS CONTAINED IN THE US WORK PACKAGES AND WILL BE MADE AVAILABLE TO THE CONTRACTOR TO ENSURE THEIR UNDERSTANDING OF THE ROLES AND RESPONSIBILITIES OF THE NDT, IUPC, AND CONTRACTOR DURING THE DESIGN, DEVELOPMENT, AND OPERATION OF THE US ELEMENT. THE US CONCEPTUAL DESIGN DESCRIBED IN THE USO-CLV-SE-25704 US DESIGN DEFINITION DOCUMENT (DDD) IS THE BASELINE DESIGN FOR THIS CONTRACT. THE CONTRACTORS EARLY ROLE WILL BE TO PROVIDE PRODUCIBILITY ENGINEERING SUPPORT TO NASA VIA THE ESTABLISHED US OFFICE STRUCTURE AND TO PROVIDE INPUTS INTO THE FINAL DESIGN CONFIGURATION, SPECIFICATIONS, AND STANDARDS. NASA WILL TRANSITION THE MANUFACTURING AND ASSEMBLY, LOGISTICS SUPPORT INFRASTRUCTURE, CONFIGURATION MANAGEMENT, AND THE SUSTAINING ENGINEERING FUNCTIONS TO THE CONTRACTOR AT THE KEY POINTS DURING THE DEVELOPMENT AND IMPLEMENTATION OF THE PROGRAM CURRENTLY PLANNED TO OCCUR NO LATER THAN 90 DAYS AFTER THE COMPLETION OF THE FOLLOWING MAJOR MILESTONES: MANUFACTURING AND ASSEMBLY US PRELIMINARY DESIGN REVIEW (PDR) LOGISTICS SUPPORT INFRASTRUCTURE US PDR CONFIGURATION MANAGEMENT US CRITICAL DESIGN REVIEW CDR) SUSTAINING ENGINEERING US DESIGN CERTIFICATION REVIEW (DCR) AFTER THE COMPLETION OF AN ORDERLY TRANSITION OF ROLES AND RESPONSIBILITIES TO THE CONTRACTOR, NASA WILL ASSUME AN INSIGHT ROLE INTO THE CONTRACTORS PRODUCTION, SUSTAINING ENGINEERING, AND OPERATIONS SUPPORT OF THE ARES I US TEST PROGRAM AND FLIGHT HARDWARE. AFTER DCR, THE CONTRACTOR WILL BE RESPONSIBLE FOR SUSTAINING ENGINEERING PER SOW SECTION 4.7, AS NECESSARY TO MAINTAIN AND SUPPORT THE US CONFIGURATION AND FOR PRODUCTION AND OPERATIONS SUPPORT.
THE MISSILE DEFENSE AGENCY (MDA), GROUND-BASED MIDCOURSE DEFENSE (GMD) DEVELOPMENT AND SUSTAINMENT CONTRACT (DSC) THE GMD DSC WORK INCLUDES, BUT IS NOT LIMITED TO: 1) FUTURE DEVELOPMENT; 2) FIELDING; 3) TEST; 4) SYSTEMS ENGINEERING, INTEGRATION AND CONFIGURATION MANAGEMENT; 5) EQUIPMENT MANUFACTURING AND REFURBISHMENT; 6) TRAINING; AND 7) OPERATIONS AND SUSTAINMENT SUPPORT FOR THE GMD WEAPON SYSTEM AND ASSOCIATED SUPPORT FACILITIES.
F-15, FMS, F-15QA AIR VEHICLE DEVELOPMENT
P-8A FRP LOT I LONG LEAD MATERIAL
KC-X MODERNIZATION PROGRAM
GBI/AUR PROGRAM MANAGEMENT/SYSTEMS ENG
W58RGZ-16-C-0023 IS FOR THE AWARD OF ADVANCE PROCUREMENT IN THE AMOUNT OF $184,930,000.00 TO SUPPORT LOT 7 FULL RATE PRODUCTION LONG LEAD ITEMS.
CH-47F CARGO HELICOPTER MULTIYEAR II. 34 NEW BUILD HELICOPTERS AND 121 RENEW HELICOPTERS.
W58RGZ-16-C-0023 IS FOR THE AWARD OF ADVANCE PROCUREMENT IN THE AMOUNT OF $184,930,000.00 TO SUPPORT LOT 7 FULL RATE PRODUCTION LONG LEAD ITEMS.
CANADA AND GERMANY LOT 13 P-8A AIRCRAFT
APACHE NEW BUILD ATTACK HELICOPTERS (AH)-64E FOR FOREIGN MILITARY SALE CUSTOMERS POLAND (QTY OF 96), EGYPT (QTY OF 2) AND KUWAIT (QTY OF 8). THIS INCLUDES ASSOCIATED COMPONENTS AND ACCESSORIES AND LONGBOW CREW TRAINERS (LCTS)
IGF::OT::IGF THE COMMERCIAL CREW PROGRAM (CCP) COMMERCIAL CREW TRANSPORTATION CAPABILITY (CCTCAP) CONTRACT WILL PROVIDE COMPLETION OF THE DESIGN, DEVELOPMENT, TEST, EVALUATION, AND CERTIFICATION OF AN INTEGRATED CREW TRANSPORTATION SYSTEM (CTS) CAPABLE OF TRANSPORTING NASA CREW TO AND FROM THE ISS, IN ACCORDANCE WITH THE DESIGN REFERENCE MISSIONS AND NASA S CERTIFICATION STANDARDS AND REQUIREMENTS. CERTIFICATION OF THE CTS WILL BE DETERMINED BY NASA. NASA PLANS TO ISSUE TASK ORDERS FOR POST CERTIFICATION MISSIONS (PCM) TO AND FROM ISS THAT INCLUDE GROUND, LAUNCH, LIFEBOAT, ON-ORBIT, RETURN AND RECOVERY OPERATIONS. THE MINIMUM QUANTITY OF MISSIONS TO BE ORDERED IS TWO (2) AND THE MAXIMUM POTENTIAL QUANTITY OF MISSIONS WHICH MAY BE ORDERED IS SIX (6). IN ADDITION, NASA MAY ISSUE TASK ORDERS FOR SPECIAL STUDIES USED FOR RISK REDUCTION AND OTHER PURPOSES RELATED TO THE CTS. NASA CERTIFICATION UNDER CLIN 001 IS COMPLETE WHEN THE CONTRACTOR S CREW TRANSPORTATION SYSTEM (CTS) HAS MET NASA S REQUIREMENTS FOR SAFELY TRANSPORTING CREW TO AND FROM THE INTERNATIONAL SPACE STATION (ISS) IN ACCORDANCE WITH DOCUMENTS IDENTIFIED IN SECTION C.1, SPECIFICATIONS/STATEMENT OF WORK. SUBCLINS 001A AND 001B, IDENTIFIED IN TABLE B.3, DDTE/CERTIFICATION SUBCLINS, ARE DELIVERY MILESTONES THAT REPRESENT COMPLETION OF REQUIRED WORK NECESSARY TO ACHIEVE NASA CERTIFICATION. DELIVERY PAYMENT FOR THE ISS DESIGN CERTIFICATION REVIEW (DCR) FOR THE CREWED FLIGHT TO THE ISS INCLUDES ALL WORK UNDER THIS CLIN THAT OCCURS FROM THE CONTRACT EFFECTIVE DATE THROUGH THE ISS DCR COMPLETION. THE DELIVERY PAYMENT FOR THE CERTIFICATION REVIEW (CR) WILL INCLUDE ALL WORK THAT OCCURS FROMTHE ISS DCR DELIVERY DATE THROUGH THE END OF THE DDTE/CERTIFICATION CLIN 001. IN ACCORDANCE WITH CLAUSE C.1, SPECIFICATION/STATEMENT OF WORK, THE TASK ORDERING PROCEDURES AND OTHER TERMS AND CONDITIONS IN THE CONTRACT, THE CONTRACTING OFFICER MAY ISSUE POST CERTIFICATION MISSION (PCM) TASK ORDERS. THE CONTRACTOR SHALL USE THE MISSION PRICING RATES SHOWN IN TABLE B.4.1, POST CERTIFICATION MISSION PRICES. THE PER MISSION PRICES ARE FOR A SINGLE ORDER AT THE PRICE STATED PER THE CALENDAR YEAR (CY) BASED ON THE NUMBER OF MISSIONS ORDERED. CTS FULL MISSION CAPABILITY PRICES SHALL BE BASED ON (1) FULFILLMENT OF THE DESIGN REFERENCE MISSION TO THE ISS FOUND IN CCT-DRM-1110, CREW TRANSPORTATION SYSTEM DESIGN REFERENCE MISSIONS, ATTACHMENT J-03, CONTRACT PERFORMANCE WORK STATEMENT, AND OTHER TERMS AND CONDITIONS IN THE CONTRACT AND (2) ALL INHERENT CTS CAPABILITIES THAT ARE WITHIN THE PROPOSED MISSION PRICES. IN ACCORDANCE WITH ATTACHMENT J-03, CONTRACT PERFORMANCE WORK STATEMENT, THE TASK ORDERING PROCEDURES AND OTHER TERMS AND CONDITIONS IN THE CONTRACT, THE CONTRACTOR SHALL PERFORM SPECIAL STUDIES, TEST AND ANALYSES, AS INITIATED BY WRITTEN DIRECTION FROM THE CONTRACTING OFFICER
SPACE LAUNCH SYSTEM (SLS) STAGES PRODUCTION AND EVOLUTION CONTRACT (SPEC)
SPACE LAUNCH SYSTEM (SLS) STAGES PRODUCTION AND EVOLUTION CONTRACT (SPEC)
E-7A RAPID PROTOTYPING
APACHE ADVANCED PROCUREMENT AWARD FOR LOT 12 FULL RATE PRODUCTION.
28 KUWAIT KAF-18E/F AIRCRAFT AND 56 COMMERCIAL PXMC CARDS
28 KUWAIT KAF-18E/F AIRCRAFT AND 56 COMMERCIAL PXMC CARDS
UH-1N REPLACEMENT HELICOPTER SYSTEM
Contract Vehicles
Where THE BOEING COMPANY wins as a prime — aggregated by the IDIQ contract vehicle each task order flows through.