This Engineering Order (EO) 2011C0360-T, dated September 13, 2010, details changes to the B-52 Aircraft Universal Nozzle Actuator Assembly (PN 9-23897). The primary purpose of this EO is to add Item Unique Identification (IUID) requirements to the drawing. Specifically, the B-52 Aircraft Universal Receptacle Toggles Actuator Assembly (PN 9-23897-2) must be marked with a Unique Item Identifier (UII) in accordance with MIL-STD-130. If a UID label is absent, a new label (PN 200733803-05) is to be fabricated and attached to the end item, with its placement detailed in AF Form 3926. The EO also includes a parts list change, adding one UID label (PN 200733803-05) made of PV6 Tesa Secure Tape or equivalent. The document was prepared by Brandon Kimbrell and approved by Chris Lee Dofflemeyer.

The document appears to be a technical specification or drawing for a component, likely a spring, within a larger system. It details dimensions, material specifications, and inspection criteria. Key features include an approximate total coils of 48, an outer diameter of 0.82 inches, and a free length of 3.28 inches. The material specified is 0.078 steel, with a maximum operating temperature of 500 degrees. The spring is designed for compression, with a minimum load of 22.0 lbs at a compressed length of 2.5 inches and a maximum load of 92.0 lbs at a compressed length of 1.625 inches. The document also includes revision information, indicating changes in descriptions and drawings, and references to related parts. This level of detail suggests it is part of a procurement or manufacturing process within a government project, likely an RFP or grant, requiring precise component specifications.

The document is a detailed engineering drawing or blueprint, likely for a component or assembly, given its technical annotations and revision history. It appears to be an internal government or contractor document, possibly related to procurement or manufacturing, judging by the

The document appears to be a technical specification or engineering drawing for a valve, likely within a government procurement or technical project context. It details critical dimensions, material specifications (e.g., 303 steel, 300 series stainless steel), tolerances, and manufacturing requirements. Key features include precise measurements for components like seats, balls, and bodies, along with instructions for surface finishes, heat treatment, and external deburring. The document also specifies quality control measures such as dimensional checks and pressure testing, emphasizing adherence to standards like ANV and military specifications. Revisions and change logs indicate ongoing modifications and approvals, highlighting a controlled engineering process. The detailed technical information is crucial for ensuring the valve meets specific operational and safety standards, typical for high-precision components in government applications.

This document outlines technical specifications and revisions for a government contract, focusing on detailed engineering and material requirements. It includes revisions for drawing, part numbers, and material specifications, particularly for plating and surface treatments. The document emphasizes strict adherence to quality control, inspection, and testing procedures, with specific instructions for material handling and finishing. It also addresses intellectual property rights, government access to data, and proper labeling. The revisions detail changes in dimensions, material compositions, and manufacturing processes, ensuring compliance with federal acquisition regulations and defense standards.

The document details a procurement request related to "S38003008d" and "S381703008d" for federal government use. It outlines financial authority, requiring approval from "7YONYVV" or "7Y181SCG'Vl", with specific codes for information requests and other uses. The file mentions various dates and reference numbers, suggesting revisions or different phases of the procurement process. Key elements include security classifications, specific item numbers, and quantities, indicating a detailed inventory or supply chain request. The document also includes instructions for handling and distribution, emphasizing authorized personnel and government internal procedures. Overall, it appears to be an internal government procurement document with strict controls and specific requirements for tracking and authorizing requests.

This government file, identified by drawing number 26828-G-1 and revision E, details specifications for a mechanical part, likely a component in an assembly. The document includes various technical drawings and associated data, outlining revisions made to the part over time. Key revisions include changes to dimensions, material, finish, and the addition of specific notes related to manufacturing and assembly. The file also references related parts and assemblies, indicating its role within a larger system. The presence of engineering change requests and approval signatures suggests a formal design and manufacturing process. This document is crucial for understanding the design, evolution, and interchangeability of this particular mechanical component within a broader government-related project or system.

This document outlines substitutions and revisions for various government specifications, primarily focusing on aerospace and mechanical components. It details changes to part numbers, materials, and procedures for items like actuators, cylinders, and rings. The revisions include updates to obsolete specifications, additions of general notes for assembly, and clarifications on handling proprietary technical data. Emphasizing adherence to DOD regulations and industrial security manuals, the document also restricts the export of technical data under the Arms Export Control Act. It highlights specific applications on B-52 and B-47E aircraft, with particular attention to material properties, assembly instructions, and testing procedures for functional components.

This government file, likely an engineering drawing or specification sheet, outlines detailed requirements for manufacturing metal parts, possibly for a federal contract or grant. It specifies material properties, dimensions, tolerances, and surface finishes, including callouts for different types of steel, corner radii, and critical dimensions in inches. The document references various standards and procedures for manufacturing, inspection, and quality control, emphasizing adherence to specific material grades and processing techniques like forging. It includes revision history and approval signatures, indicating a controlled document lifecycle. Key details include part numbers, material types, and specific manufacturing or inspection notes, suggesting a component in a larger assembly. The overall purpose is to provide precise technical instructions for producing compliant parts, ensuring consistency and quality in a government-related project.

This document, part of federal government RFPs, outlines specifications for an aircraft component, likely a cylinder or related assembly. It details various parts, their materials, dimensions, and assembly instructions, with a focus on precision manufacturing and specific tolerances. Key components include internal and external cylinders, connecting rods, and a manifold, all requiring precise machining and finishing. The document also highlights quality control measures, such as internal inspection, and specific testing requirements for components like springs. It emphasizes the need for adherence to detailed drawings and revisions, indicating a complex manufacturing process. The presence of multiple revision notes and part numbers suggests an ongoing development or refinement of the aircraft component. The overall purpose is to provide a comprehensive technical directive for the production and assembly of this critical aerospace part.

The document details engineering specifications and revisions for various mechanical and structural components, likely related to a manufacturing or construction project. It outlines dimensions, materials, and processes for items such as metal sheets, pins, and possibly assemblies. Key information includes revisions made on specific dates, part numbers, and descriptions of modifications like "REPLACE TO," "ADD," or "CHANGE." The file emphasizes precise measurements, material specifications, and instructions for assembly or installation. It also references internal and external standards for manufacturing and quality control, indicating a focus on detailed design and adherence to technical requirements. The frequent revisions suggest an evolving project with iterative design improvements and adjustments.

This document, BACD2101 SPOTFACING, is a Boeing standard from January 2000, now in corporate archives. It requires checking the 590-SUPERSESSION-LIST or calling the PSDS Help Desk at (253) 657-5902 to verify if it's still active for procurement. The document is marked with a distribution statement restricting it to the U.S. Department of Defense and its authorized contractors due to Critical Technology and Export Control. It contains technical data subject to U.S. export laws, specifically the Arms Export Control Act and the Export Administration Act. Violations carry severe criminal penalties. A destruction notice warns against disclosure and mandates destruction methods that prevent reconstruction of its contents.

This Engineering Data List, dated October 28, 2025, with revision 8, details the components and specifications for an ELECTRO-ME ACTUATOR manufactured by THE BOEING COMPANY. The document, identified by NSN 1680002108808RK and reference number 9-23897-2, outlines various engineering drawings and accompanying documents for parts such as the ACTUATOR ASS'Y, VALVE SEAT, SPRING TERMINAL, COMPRESSION SPRING, TERMINAL ASS'Y, ACTUATOR CYLINDER ASS'Y, FORGING, PISTON, and GLAND NUT. It also lists functional test procedures and design details. Furthermore, the list includes numerous industry and military specifications and standards for materials, processes, and finishes, covering aspects like surface texture, dimensions, heat treatment, plating, and marking methods. The document also contains important remarks regarding foreign disclosure approval and the prohibition of Class 1 ODS, emphasizing the use of current amendments for all specifications.

The document,

This government file contains a warning about technical data restricted by the ARMS CONTROL ACT, specifically regarding export control regulations. It outlines strict rules for disseminating export-controlled technical data, including release to foreign nationals within the United States. The document details that obtaining approval or a license from the Department of State (for ITAR-controlled items) or the Department of Commerce (for EAR-controlled items) is mandatory. It also specifies severe penalties for violations, including significant fines and imprisonment under both the ITAR and EAR. Furthermore, the U.S. Government disclaims liability for patent infringement, misuse of technical data, or any loss, damage, or injury resulting from the manufacture or use of products based on the furnished data. The file explicitly states that the release of this data does not include or involve any license rights.

This government file outlines the qualification requirements for an electro-mechanical actuator (NSN 1680-00-210-8808, Part 9-23897-2), detailing distinct criteria based on whether requirements were established before or after October 19, 1984. For pre-1984 qualifications, Section F.1 exempts the item from FAR 9.202(a) due to prequalification being essential for quality and safety. Section F.2 specifies that only manufacturers who have successfully completed all required testing, either by the original designer or on similar government-approved items, can be considered approved sources. Section F.3 references FAR and DFARS provisions. For post-1984 qualifications, a Justification for Qualification Requirement (JQR) is mandatory, and FAR 9.202(a) applies. Section F.2 maintains the strict manufacturer qualification criteria, similar to the pre-1984 guidelines. The document underscores the complexity and criticality of the part, emphasizing the need for rigorous testing and approved sourcing to ensure operational safety and high quality.