MIL-STD-001591A COMMAND, CONTROL, AND COMMUNICATIONS SYSTEM AND COMPONENT (8 DEC 1978)., This standard establishes uniform criteria for conducting trade studies to determine the optimal design for command, control and communication system and component fault diagnosis/isolation subsystems.

MIL-STD-1500B (NOTICE 1), MILITARY STANDARD CADMIUM-TITANIUM PLATING, LOW EMBRITTLEMENT ELECTRO-DEPOSITION (9 DEC 1996)., MIL-STD-1500B, dated 2 April, 1990, and any subsequent revisions or change notices are inactive for new design and shall be no longer used as a guidance reference for new designs.

MIL-STD-1500B, MILITARY STANDARD CADMIUM-TITANIUM PLATING, LOW EMBRITTLEMENT ELECTRO-DEPOSITION (2 APR 1990). This standard covers the process and materials required for the electro-deposition of cadmium-titanium on high strength steel substrates.

MIL-STD-1501B (NOTICE 1), MILITARY STANDARD CHROMIUM PLATING, LOW EMBRITTLEMENT, ELECTRODEPOSITION (14 DEC 1984)., The following pages of MIL-STD-1501B(USAF) have been revised and supersede the pages listed.

MIL-STD-1501B (USAF), MILITARY STANDARD CHROMIUM PLATING, LOW EMBRITTLEMENT, ELECTRODEPOSITION (29 MAR 1978)., This standard covers the process and materials required for the electrodeposition of chromium on high-strength steel substrates.

MIL-STD-1503B (NOTICE 1) MILITARY STANDARD PREPARATION OF ALUMINUM ALLOYS FOR SURFACE TREATMENTS AND INORGANIC COATING (2 AUG 1994)., MIL-STD-1503(USAF), dated 30 April 1973, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1503B (NOTICE 2) MILITARY STANDARD PREPARATION OF ALUMINUM ALLOYS FOR SURFACE TREATMENTS AND INORGANIC COATING (9 DEC 1996)., MIL-STD-1503B, dated 13 November, 1989, and any subsequent revisions or change notices are inactive for new design and shall be no longer used as a guidance reference for new designs.

MIL-STD-1503B, MILITARY STANDARD PREPARATION OF ALUMINUM ALLOYS FOR SURFACE TREATMENTS AND INORGANIC COATING (13 NOV 1989)., This standard describes the cleaning, activation and underplating process, and material required for aluminum and aluminum alloys prior to applying inorganic coating. It is intended that this standard be used in conjunction with other process documents where the technical requirements are for the application of surface treatments and inorganic coatings on aluminum and aluminum alloys.

MIL-STD-1504B (NOTICE 1) MILITARY STANDARD ABRASIVE BLASTING. MIL-STD-1504B, dated 8 June, 1989, any any subsequent revisions or change notices are inactive for new design and shall be no longer used as a guidance reference for new designs.

MIL-STD-1504B, MILITARY STANDARD ABRASIVE BLASTING (8 JUN 1989)., This standard covers the processes and materials required for the abrasive blasting of aircraft and missile components.

MIL-STD-1510B (NOTICE 1) MILITARY STANDARD CONTAINER DESIGN RETRIEVAL SYSTEM PROCEDURES FOR USE OF. MIL-STD-1510B, dated 30 September 1988 is hereby cancelled. Future acquisitions should refer to MIL-STD-2073-1, Standard Practice for Military Packaging.

MIL-STD-1510B, MILITARY STANDARD CONTAINER DESIGN RETRIEVAL SYSTEM, PROCEDURES FOR USE OF. This standard provides DOD activities having packaging development/procurement responsibilities, and their contractors, the instructions for use of the Container Design Retrieval System (CDRD).

MIL-STD-1512 (USAF) (NOTICE 2), MILITARY STANDARD ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS. MILITARY STANDARD ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN REQUIREMENTS AND TEST METHODS MIL-STD-1512 (USAF), dated 21 March 1972 and Notice 1, dated 6 January 1976 are hereby canceled and superseded by MIL-HDBK-1512 (USAF), dated 30 September 1997.

MIL-STD-1512 (USAF), MILITARY STANDARD ELECTROEXPLOSIVE SUBSYSTEMS, ELECTRICALLY INITIATED, DESIGN RQMTS AND TEST METHODS. This standard establishes the general requirements and test methods for the design and development of electro-explosive subsystems and associated items to preclude hazards from unintentional initiation. These requirements apply to all subsystems utilizing electrically initiated, explosive, or pyrotechnic components.

MIL-STD-1514 (NOTICE 1) MILITARY STANDARD FITTINGS, TETRAFLOURETHLENE HOSE HIGH TEMPERATURE, HIGH PRESSURE (3000 psi) HYDRAULIC AND PNEMATIC CLASSIFICATION OF DEFECTS. MIL-STD-1514(USAF), dated 17 March 1971, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1514 (NOTICE 2) MILITARY STANDARD FITTINGS, TETRAFLOURETHLENE HOSE HIGH TEMPERATURE, HIGH PRESSURE (3000 PSI) HYDRAULIC AND PNEUMATIC CLASSIFICATION OF DEFECTS MIL-STD-1514, dated 17 March 1971, is hereby canceled without replacement.

MIL-STD-1514 (USAF), MILITARY STANDARD FITTINGS, TETRAFLUOROETHYLENE HOSE HIGH TEMPERATURE (3000 PSI) HYDRAULIC AND PNEUMATIC CLASSIFICATION OF DEFECTS. This standard covers the classification of defects for fittings covered by MIL-F-83296.

MIL-STD-1515A (NOTICE 1) MILITARY STANDARD FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (24 SEP 1979) [S/S BY NASM1515]., The following items of MIL-STD-1515A have been revised and supersede the items lised.

MIL-STD-1515A (NOTICE 2) FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (5 JUN 1981) [S/S BY NASM1515]., The following items of MIL-STD-1515A have been revised and supersede the items listed.

MIL-STD-1515A (NOTICE 3) MILITARY STANDARD, FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (24 JUN 1983) [S/S BY NASM1515]., The following items of MIL-STD-1515A have been revised and supersede the items listed.

MIL-STD-1515A (NOTICE 4) MILITARY STANDARD FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (4 MAY 1998) [S/S BY NASM1515]., MIL-STD-1515A, including Change Notice 3, dated 24 June 1983, is hereby canceled without replacement.

MIL-STD-1515A (NOTICE 5) MILITARY STANDARD FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (30 JUL 1999) [S/S BY NASM1515]., MIL-STD-1515, dated 4 May 1998, is hereby canceled. Future design should be done in accordance with NASM1515.

MIL-STD-1515A, MILITARY STANDARD FASTENER SYSTEMS FOR AEROSPACE APPLICATIONS (12 JUL 1978) [S/S BY NASM1515]., This standard covers the methods of fastening, materials, finishes, test methods, and hole size and criteria of fasteners and fastening systems used in the design and construction of aerospace systems. In addition, it provides a comprehensive presentation of approved engineering practices, procedures, processes, and characteristics for fasteners.

MIL-STD-1516A, MILITARY STANDARD UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIEL. This standard is to establish a uniform code and to serve as a genera guide to the selection of suitable materials,procedures,and systems for cleaning,plating, painting and otherwise finishing metal, plastic,wood, and other surfaces,for use by the Department of Defense (DOD).

MIL-STD-1516B (NOTICE 1) MILITARY STANDARD UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL. MIL-STD-1516B, dated 13 November 1990, is hereby canceled without replacement.

MIL-STD-1516B, MILITARY STANDARD UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL. This standard establishes a uniform code and to serve as a general guide to the selection of suitable materials, procedures, and systems for cleaning, plating, painting, and otherwise finishing metal, plastic, wood, and other surfaces, for use by the Department of Defense (DOD).

MIL-STD-1518B (NOTICE 1) MILITARY STANDARD STORAGE, HANDLING, AND SERVICING OF AVIATION FUELS, LUBRICATING OILS, AND HYDRAULIC FLUIDS AT CONTRACTOR FACILITIES. This notice should be filed in front of MIL-STD-1518B, dated 3 March 1980. MIL-STD-15818B is Inactive for new design and is no longer used except for replacement purposes.

MIL-STD-1518B (NOTICE 2) STORAGE, HANDLING, AND SERVICING OF AVIATION FUELS, LUBRICATION OILS, AND HYDRAULIC FLUIDS AT CONTRACTOR LOCATIONS. MIL-STD-1518B, dated 3 March 1980, is hereby reactivated and may be used for new acquisition.

MIL-STD-1518B, MILITARY STANDARD STORAGE, HANDLING AND SERVICING OF AVIATION FUELS, LUBRICATING OILS AND HYDRAULIC FLUIDS AT CONTRACTOR FACILITIES. The purpose of this document is to set forth the performance requirements and quality control standards for receipt,storage, testing and servicing of all aviation fuels, lubricants and hydraulic fluids in support of USAF aircraft at manufacturing, maintenance or engine test facilities which are contractor operated.

MIL-STD-1518C, DEPARTMENT OF DEFENSE STANDARD PRACTICE STORAGE, HANDLING, AND SERVICING OF AVIATION FUELS, LUBRICATING OILS, AND HYDRAULIC FLUIDS AT CONTRACTOR FACILITIES. This standard establishes the minimum performance and quality requirements for the storage, handling, and servicing of aviation fuels, lubricating oils, and hydraulic fluids at contractor facilities.

MIL-STD-1519 (NOTICE 1) MILITARY STANDARD TEST REQUIREMENTS DOCUMENT. PREPARATION OF. To all holders of MIL-STD-1519 (USAF): 1. Pen and Ink Change: On self-cover change "Military Specification" to "Military Standard"

MIL-STD-1519 (NOTICE 2) MILITARY STANDARD TEST REQUIREMENTS DOCUMENT. PREPARATION OF MIL-STD-1519(USAF) dated September 1971 and Notice 1 dated 1 August 1977 have been reviewed and determined to be valid for use in acquisition

MIL-STD-1519 (NOTICE 3) MILITARY STANDARD TEST REQUIREMENTS DOCUMENT PREPARTION OF. MIL-STD-1519(usaf), dated 17 September 1971, NOTICE 1 of 1 August 1977, and NOTICE 2 of 26 February 1988 are hereby canceled without replacement.

MIL-STD-1519 (USAF), MILITARY SPECIFICATION TEST REQUIREMENTS DOCUMENTS, PREPARATION OF

MIL-STD-1520C (NOTICE 1), MILITARY STANDARD CORRECTIVE ACTION AND DISPOSITION SYSTEM FOR NONCONFORMING MATERIAL. The following pages of MIL-STD-1520C have been revised and supersede the pages listed.

MIL-STD-1520C (NOTICE 2), MILITARY STANDARD CORRECTIVE ACTION AND DISPOSITION SYSTEM FOR NONCONFORMING MATERIAL. MIL-STD-1520C, dated 27 June 1986, and Notice 1 dated 5 March 1993, are hereby canceled without replacement.

MIL-STD-1520C, MILITARY STANDARD CORRECTIVE ACTION AND DISPOSITION SYSTEM FOR NONCONFORMING MATERIAL. This standard sets forth the requirements for a cost-effective corrective action and disposition system for nonconforming material. It defines the requirements relative to the interface between the contractor and the contract administrative office on nonconforming material. This standard sets forth the DOD contracting activity requirements for a properly constituted Material Review Board (MRB).

MIL-STD-1521B (NOTICE 2) (USAF), MILITARY STANDARD TECHNICAL REVIEWS AND AUDITS FOR SYSTEMS, EQUIPMENTS, AND COMPUTER SOFTWARE (17 JUL 1992)., TO ALL HOLDERS OF MIL-STD-1521B (USAF) Pages 71 through 82, Appendix H, and Appendix I: DELETE. The contents of the pages listed are now contained in MIL-STD-973, “CONFIGURATION MANAGEMENT”.

MIL-STD-1521B (USAF) (NOTICE 3), MILITARY STANDARD TECHNICAL REVIEWS AND AUDITS FOR SYSTEMS, EQUIPMENTS, AND COMPUTER SOFTWARE (10 APR 1995)., MIL-STD-1521B (USAF), dated 4 June 1985, NOTICE 1 dated 19 December 1985, and NOTICE 2 dated 17 July 1992, are hereby canceled. Functional. Configuration Audit and physical Configuration Audit requirements were incorporated into MIL-STD-973, “Configuration Management.” All other areas have been canceled without replacement.

MIL-STD-1521B (USAF), MILITARY STANDARD TECHNICAL REVIEWS AND AUDITS FOR SYSTEMS, EQUIPMENTS, AND COMPUTER SOFTWARE (4 JUN 1985)., This standard prescribes the requirements for the conduct of Technical Reviews and Audits on Systems, Equipments, and Computer Software.

MIL-STD-1522A (NOTICE 1), MILITARY STANDARD STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS (21 DEC 1984)., MIL-STD-1520C, dated 27 June 1986, and Notice 1 dated 21 December 1984, are hereby canceled without replacement.

MIL-STD-1522A (NOTICE 2), STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS (20 NOV 1986)., The following pages of MIL-STD-1522A (USAF) have been revised and supersede the pages listed.

MIL-STD-1522A (NOTICE 3) STANDARD GENERAL REQUIREMENTS FOR SAFEDESIGN AND OPERATION OF PRESSURES MISSILE AND SPACE SYSTEMS MIL-STD-1522A (USAF), dated 28 May 84, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1522A (USAF), MILITARY STANDARD STANDARD GENERAL REQUIREMENTS FOR SAFE DESIGN AND OPERATION OF PRESSURIZED MISSILE AND SPACE SYSTEMS (28 MAY 1984)., This standard establishes requirements for the design and test of all pressurized systems for missiles, space vehicles and ground support equipment. These requirements, when implemented on a particular pressurized system, will assure a high level of confidence in achieving safe operation and mission success.

MIL-STD-1523A (NOTICE 1) AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL. MIL-STD-1523A. dated 1 February 1984, is hereby canceled. Future acquisitions should refer to SAE AS 1933. Age Controls for Hose Containing Age-Sensitive Elastomeric Material.

MIL-STD-1523A (NOTICE 2) AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL (FOR AEROSPACE APPLICATIONS) MIL-STD-1523A, dated 1 February 1984, is hereby canceled. Future acquisition for this product should refer to SAE-AS1933, "Age Control for Hose Containing Age-Sensitive ELastomeric Material" for hose application and SAE_ARP5316, "Storage of Aerospace Elastomeric Seals and Seal Assemblies which include an Elastomer Element prior to Hardware Assembly for seal application.

MIL-STD-1523A, MILITARY STANDARD AGE CONTROLS OF AGE-SENSITIVE ELASTOMERIC MATERIAL (FOR AEROSPACE APPLICATIONS). This document establishes requirements for the maximum ages of age sensitive elastomeric items for use in military aircraft and missiles and for space vehicles at the time of acceptance by a Government acquiring activity. The provisions of this document apply to hoses and O-r-s from specific classes of elastomers which are resistant to lubricants,hydraulic fluids,and petroleum base fuels and which conform to the specifications cited herein.

MIL-STD-1524 (NOTICE 1) TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED The following pages of MIL-STD-1524 have been revised and supersede the pages listed

MIL-STD-1524 (NOTICE 2) TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED. MIL-STD-1524. dated 31 July 1972, has been reviewed adn determined to be valid for use in acquisition.

MIL-STD-1524 (NOTICE 3) TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED MIL-STD-1524 dated 31 July 1972, is hereby canceled without replacement.

MIL-STD-1524, MILITARY STANDARD TABLE OF DIFFERENTIAL PRESSURE IN RELATION TO CALIBRATED AIRSPEED. This standard presents differential pressures in inches of mercury and inches of water for values of calibrated airspeed in knots/

MIL-STD-1525B, DEPARTMENT OF DEFENSE STANDARD PRACTICE VERIFICATION TESTING OF PARACHUTE TEXTILE MATERIALS. This standard establishes the verification tests for parachute materials (subcontracted supplies) used in the fabrication of parachutes. These tests are for the purpose of confirming subcontractor test reports, determining conformance of material to contract specifications, and to provide data for the computation of reliability for these materials.

MIL-STD-1528A (NOTICE 1), MILITARY STANDARD MANUFACTURING MANAGEMENT PROGRAM. MIL-STD-1528A(USAF) , dated 9 September 1986, is hereby canceled without replacement.

MIL-STD-1528A, MILITARY STANDARD MANUFACTURING MANAGEMENT PROGRAM. The purpose of this standard is to prescribe the manufacturing management objectives and requirements which must be met by the contractor’s manufacturing management system on any contract which incorporates this standard. The system shall assure effective application of manufacturing management principles and methods to assure efficient manufacture, or preparation for manufacture, of defense acquisition programs hardware. The system shall establish, and assure application through program phases, crfterta for capability, capacity, producibility, productivity, manufacturing planning and risk reduction, strategic and critical materials conservation, and surge and mobilization to each aspect of hardware design, procurement, manufacture, and shipment.

MIL-STD-1529 (NOTICE 1) VENDOR SUBSTANTIATION FOR AEROSPACE PROPULSION SYSTEM ITEMS. Make the following pen and ink changes

MIL-STD-1529 (NOTICE 2) VENDOR SUBSTANATIATION FOR AEROSPACE PROPULSION SYSTEM ITEMS. MIL-STD-1529 dated 24 August 1972 and Notice 1 dated 28 February 1973, have been reviewed and determined to be valid for use in acquisition.

MIL-STD-1529 (NOTICE 3) VENDOR SUBSTANTABLE FOR AEROSPACE PROPULSION SYSTEM ITEMS MIL-STD-1529 dated 24 August 1972, is hereby canceled without replacement.

MIL-STD-1529 (USAF), MILITARY STANDARD VENDOR SUBSTANTIATION FOR AEROSPACE PROPULSION SYSTEM ITEMS. The purpose of this standard is to establish a requirement for and prescribe the procedure by which substantiation tests will be conducted for aerospace propulsion system items manufactured by fabrication sources not represented in the specific aerospace propulsion system which passed the aerospace propulsion system qualification tests.

MIL-STD-1530A (II), MILITARY STRUCTURAL INTEGRITY PROGRAM, AIRPLANE REQUIREMENTS. The purpose of this standard is to describe the Air Force Aircraft Structural Integrity Program, define the overall requirements necessary to achieve structural integrity of USAF airplanes, and specify acceptance methods of contractor compliance.

MIL-STD-1530A (USAF) (NOTICE 1), MILITARY STRUCTURAL INTEGRITY PROGRAM, AIRPLANE REQUIREMENTS. MIL-STD-1530A (USAF) dated 11 December 1975 has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1530A (USAF) (NOTICE 2), MILITARY STRUCTURAL INTEGRITY PROGRAM, AIRPLANE REQUIREMENTS. MIL-STD-1530A, dated 26 February 1988, is hereby cancelled. Future acquisition should refer to MILHDBK- 1530, “Aircraft Structural Integrity Program, General Guidelines for.”

MIL-STD-1531 (USAF), MILITARY STANDARD INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHELL SIZE A. This standard covers insert arrangements for use with MIL-C-83733 panel to rack connectors, shell size A. It is used to control the dimensions and configuration of insert patterns and contact sizes.

MIL-STD-1531A (NOTICE 1) INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHRLL SIZE A. MIL-STD-1531A, dated 25 March 1988, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1531A, DEPARTMENT OF DEFENSE INTERFACE STANDARD INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHELL SIZE A. This standard covers insert arrangements for use with MIL-C_83733 rack to panel connectors, shell size A. It is used to control the dimensions and configuration of insert patterns and the contact sizes.

MIL-STD-1532, MILITARY STANDARD INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHELL SIZE B. This standard covers insert arrangements for use with MIL-C-83733 rack to panel connectors, shell size B. It is sued to control the dimensions and configuration of insert panels and the contact sizes.

MIL-STD-1532A (NOTICE 1) INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHRLL SIZE B. MIL-STD-1532A, dated 25 March 1988 has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1532A, DEPARTMENT OF DEFENSE INTERFACE STANDARD INSERT ARRANGEMENTS FOR MIL-C-83733 RACK TO PANEL CONNECTORS, SHELL SIZE B. This standard covers insert arrangements for use with MIL-C-83733 rack to panel connectors, shell size B. It is used to control the dimensions and configuration of insert patterns and the contact sizes.

MIL-STD-1535, SUPPLIER QUALITY ASSURANCE PROGRAM REQUIREMENTS

MIL-STD-1535B, MILITARY STANDARD SUPPLIER QUALITY ASSURANCE PROGRAM REQUIREMENTS. The purpose of this standard is to establish contractor requirements and procedures for an effective quality assurance program for government acquisitions involving subcontracts when Higher-level Quality Assurance requirements, FAR 46.202-3, and this standard are requirements of the prime contract. The prim contractor shall tailor and include these requirements in purchase documents to suppliers.

MIL-STD-1537B (NOTICE 1) TEST METHOD STANDARD FOR ELECTRICAL CONDUCTIVITY TEST FOR VERIFICATION OF HEAT TREATMENT OF ALUMINUM ALLOYS EDDY CURRENT METHOD The following pages of MIL-STD_1537B have been revised and supersede the pages listed.

MIL-STD-1537B MILITARY STANDARD ELECTRICAL CONDUCTIVITY TEST FOR VERIFICATION OF HEAT TREATMENT OF ALUMINUM ALLOYS, EDDY CURRENT METHOD This standard contains procedures for verifying aluminum alloy heat treatment by means of eddy current techniques which measure electrical conductivity measurements are used in conjunction with hardness measurements.

MIL-STD-1537C, DEPARTMENT OF DEFENSE TEST METHOD STANDARD FOR ELECTRICAL CONDUCTIVITY TEST FOR VERIFICATION OF HEAT TREATMENT OF ALUMINUM ALLOYS EDDY CURRENT METHOD (25 JUN 2002)., This standard contains procedures for verifying aluminum alloy heat treatment by means of eddy current techniques, which measure electrical conductivity. Aluminum alloy heat treatment can be verified when electrical conductivity measurements are used in conjunction with hardness measurements.

MIL-STD-1538, MILITARY STANDARD, SPARE PARTS AND MAINTENANCE SUPPORT OF SPACE AND MISSILE SYSTEMS UNDERGOING RDT&E (11 APR 1973)., This standard establishes procedures under which the contractor shall provide spare parts and maintenance services.

MIL-STD-1539 (NOTICE 2), MILITARY STANDARD ELECTRICAL POWER, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS. MIL-STD-1539, dated 4 September 1992, is inactive for new design and is no longer used, except for replacement purposes.

MIL-STD-1539 (USAF) (NOTICE 1), MILITARY STANDARD ELECTRICAL POWER, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS. MIL-STD-1539 (USAF), dated 01 AUGUST 73, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1539 (USAF), MILITARY STANDARD ELECTRICAL POWER, DIRECT CURRENT, SPACE VEHICLE DESIGN REQUIREMENTS. This standard establishes the requirements for the direct current (DC) electrical power system for space vehicles.

MIL-STD-1540B (Notice 1) (USAF), MILITARY STANDARD TEST REQUIREMENTS FOR SPACE VEHICLES. Pages updated and superseded.

MIL-STD-1540B (Notice 2) (USAF), MILITARY STANDARD TEST REQUIREMENTS FOR SPACE VEHICLES. Pages updated and superseded.

This change notice incorporates special pyroshock screening tests for components that contain non-passivated microelectronic parts. THE FOLLOWING PAGES OF MIL-STD-1540B (USAF) HAVE BEEN REVISED AND SUPERSEDE THE PAGES LISTED:

MIL-STD-1540B, MILITARY STANDARD TEST REQUIREMENTS FOR SPACE VEHICLES. This standard establishes the environmental and structural ground testing requirements for launch vehicles, upper-stage vehicles, space vehicles, and for their subsystems and units.

MIL-STD-1540C, MILITARY STANDARD, TEST REQUIREMENTS FOR LAUNCH, UPPER-STAGE, AND SPACE VEHICLES (15 SEP 1994). This standard establishes the environmental and structural ground testing requirements for launch vehicles, upper-stage vehicles, space vehicles, and for their subsystems and units.

MIL-STD-1540D, PRODUCT VERIFICATION REQUIREMENTS FOR, LAUNCH, UPPER STAGE, AND SPACE VEHICLES. This standard establishes the environmental and structural ground testing requirements for launch vehicles, upper-stage vehicles, space vehicles, and for their subsystems and units.

MIL-STD-1541A, MILITARY STANDARD, ELECTROMAGNETIC COMPATIBILITY REQUIREMENTS FOR SPACE SYSTEMS (30 DEC 1987)., This standard establishes the electromagnetic compatibility requirements for space systems, including frequency management, and the related requirements for the electrical and electronic equipment used in space systems. It also includes requirements designed to establish an effective ground reference for the installed equipment and designed to inhibit adverse electrostatic effects.

MIL-STD-1542A, MILITARY STANDARD ELECTROMAGNETIC COMPATIBILITY AND GROUNDING REQUIREMENTS FOR SPACE SYSTEM FACILITIES (1 MAY 1988)., The purpose of this standard is to specify the design, performance, and verification requirements for electrical subsystems for space system facilities, including electromagnetic compatibility (EMC), electrical power grounding, bonding, shielding, lightning protection, and TEMPEST security. These requirements are interrelated and interdependent, and therefore require an integrated approach in the design. .

MIL-STD-1542B (USAF), MILITARY STANDARD ELECTROMAGNETIC COMPATIBILITY AND GROUNDING REQUIREMENTS FOR SPACE SYSTEM FACILITIES (15 NOV 1991)., The purpose of this standard is to specify the design, performance, and verification requirements for electrical subsystems for space system facilities, including electromagnetic compatibility (EMC), electrical power grounding, bonding, shielding, lightning protection, and TEMPEST security. These requirements are interrelated and interdependent, and therefore require an integrated approach in the design. .

MIL-STD-1543B (NOTICE 1), MILITARY STANDARD, RELIABILITY PROGRAM REQUIREMENTS FOR SPACE AND LAUNCH VEHICLES (4 MAY 1998)., MIL-STD-1543B, dated 25 October 1988, is hereby canceled without replacement.

MIL-STD-1543B, MILITARY STANDARD, RELIABILITY PROGRAM REQUIREMENTS FOR SPACE AND LAUNCH VEHICLES (USAF) (25 OCT 1988)., This standard establishes uniform reliability program requirements and tasks for use during design, development, fabrication, test, and operation of space and launch vehicles.

MIL-STD-1545 (USAF) (NOTICE 1), OPTIONAL SPARE PARTS, MAINTENANCE AND INVENTORY SUPPORT OF SPACE AND MISSILE SYSTEMS (4 SEP 1992)., This standard establishes procedures under which the contractor will provide spare parts, inventory and maintenance services for space and missile systems.

MIL-STD-1545 (USAF), OPTIONAL SPARE PARTS, MAINTENANCE AND INVENTORY SUPPORT OF SPACE AND MISSILE SYSTEMS (15 JUN 1977)., This standard establishes procedures under which the contractor will provide spare parts, inventory and maintenance services for space and missile systems.

MIL-STD-1546B, MILITARY STANDARD, PARTS, MATERIALS, AND PROCESSES CONTROL PROGRAM FOR SPACE AND LAUNCH VEHICLES (27 JUL 1992)., This standard establishes the requirements for the preparation, implementation, and operation of a parts, materials, and processes control program for use during the design, development, and production of space and launch vehicles

MIL-STD-1547A, MILITARY STANDARD, ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES (1 DEC 1987) [S/S BY MIL-HDBK-1547]., This standard establishes the minimum technical requirements for parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles.

MIL-STD-1547B, MILITARY STANDARD, ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES (1 DEC 1992) [S/S BY MIL-HDBK-1547]., This standard establishes the minimum technical requirements for parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles.

MIL-STD-1548C (NOTICE 1) INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS MIL-STD-1548C, dated 31 January 1994, is inactive for new design and is no longer used, except for replacement purposes.

MIL-STD-1548C (NOTICE 2) INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS MIL-STD-1548C, dated 11 January 1994, is hereby reactivated and may be used for new acquisition.

MIL-STD-1548C MILITARY STANDARD INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS This standard establishes the minimum performance and quality requirements for the servicing of fuels to aircraft on US Government Into-Plane Servicing Contracts at commercial airports.

MIL-STD-1548D, MILITARY STANDARD, INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS (30 MAR 2000)., This standard establishes 2 types of standard practices for into-plane servicing of fuels at commercial airports.

MIL-STD-1548E, DEPARTMENT OF DEFENSE STANDARD PRACTICE INTO-PLANE SERVICING OF FUELS AT COMMERCIAL AIRPORTS. 1.1 This standard establishes two types of standard practices for into-plane servicing of fuels at commercial airports. Classification of into-plane servicing is as follows: Type I Into-Plane Refueling Guidance per ATA Specification 103, Standard For Jet Fuel Quality Control at Airports. Type II Into-Plane Refueling Guidance as per IATA's Guidelines for Aviation Fuel Quality Control and Operating Procedures for Joint Into-Plane Fueling Services (JIG).

MIL-STD-1549, MILITARY STANDARD COMMON TERMINATION SYSTEM FOR ELECTRICAL AND ELECTRONIC PARTS (19 JUL 1974)., This standard establishes the design, technical, and performance requirements necessary for implementing the Common Termination System (CTS) on any electrical or electric part or terminal junction system (modules and splices).

MIL-STD-1549A (NOTICE 1), MILITARY STANDARD COMMON TERMINATION SYSTEM FOR ELECTRICAL AND ELECTRONIC PARTS (5 DEC 1995).

MIL-STD-1549A, MILITARY STANDARD COMMON TERMINATION SYSTEM FOR ELECTRICAL AND ELECTRONIC PARTS (22 APR 1988)., This standard establishes the design, technical, and performance requirements necessary for implementing the Common Termination System (CTS) on any electrical or electric part or terminal junction system (modules and splices).

MIL-STD-1551C (NOTICE 1) QUALITY CONTROL OF GAEOUS AND LIQUID AVIATOR'S BREATHING OXYGEN AT AIRCRAFT CONTRACTOR FACILITIES MIL-STD-1551C (USAF), dated 1 April 1990, is hereby canceled without replacement.

MIL-STD-1551C QUALITY CONTORL OF GASEOUS AND LIQUID AVIATOR'S BREATHING OXYGEN AT AIRCRAFT CONTRACTOR FACILITIES The purpose of this standard is to provide minimum guidance, information, instructions, and procedures for quality control of Aviator's Breathing Oxygen.

MIL-STD-1553B (USAF) (NOTICE 1), MILITARY STANDARD AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS. The following pages of MIL-STD-1553B have been revised and supersede the pages listed.

MIL-STD-1553B (USAF) (NOTICE 1), MILITARY STANDARD AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS. Make the following pen and ink changes.

MIL-STD-1553B (USAF) (NOTICE 3), MILITARY STANDARD AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS. MIL-STD-1153B, dated 21 September 1978, has been reviewed and determined to be valid for acquisition.

MIL-STD-1553B (USAF) (NOTICE 4), MILITARY STANDARD AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS. The following pages of MIL-STD-1553B have been revised and supersede the pages listed.

MIL-STD-1553B (USAF), MILITARY STANDARD AIRCRAFT INTERNAL TIME DIVISION COMMAND/RESPONSE MULTIPLEX DATA BUS. This standard establishes requirements for digital, command/response, time division multiplexing (Data Bus) techniques on aircraft. It encompasses the data bus line and its interface electronics illustrated on Figure 1, and also defines the concept of operation and information flow on multiplex data bus and the electrical and functional formats to be employed.

MIL-STD-1554 ( NOTICE 1), MIL STD INSERT ARRANGEMENTS FOR MI1-C-83723 SERIES AND MIL-C-26500 ENVIRONMENT RESISTING, CIRCULAR, ELECTRICAL CONNECTORS. The following pages of MIL-STD-1554 have been revised and supersede the pages listed.

MIL-STD-1554 (NOTICE 1) INSERT ARRANGEMENTS FOR MIL-C-83723 SERIES III AND MIL-C-26500 ENVIRONMENT RESISTING, CIRCULAR, ELECTRICAL CONNECTORS MIL-STD-1554, dated 19 December 1989 has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1554 (NOTICE 2) INSERT ARRANGEMENTS FOR MIL-C-83723 SERIES III AND MIL-C-26500 ENVIRONMENT RESISTING, CIRCULAR, ELECTRICAL CONNECTORS The following pages of MIL-STD-1554 have been revised and supersede the pages listed.

MIL-STD-1554 (NOTICE 3) INSERT ARRANGEMENTS FOR MIL-C-83723 SERIES III AND MIL-C-26500 ENVIRONMENT RESISTING, CIRCULAR, ELECTRICAL CONNECTORS The following pages of MIL-STD-1554 have been revised and supersede the pages listed.

MIL-STD-1554 (NOTICE 4) INSERT ARRANGEMENTS FOR MIL-C-83723 SERIES III AND MIL-C-26500 ENVIRONMENT RESISTING, CIRCULAR, ELECTRICAL CONNECTORS The following pages of MIL-STD-1554 have been revised and supersede the pages listed.

MIL-STD-1554, MILITARY STANDARD INSERT ARRANGEMENTS FOR MI1-C-83723 SERIES AND MIL-C-26500 ENVIRONMENT RESISTING, CIRCULAR, ELECTRICAL CONNECTORS. This standard covers insert arrangements use with MIL-C-83723 series 111 and MIL-C-26500 environment resisting,circular,electrical connectors.

MIL-STD-1555, MILITARY STANDARD, AIRCREW STATION DISPLAYS AND ASSOCIATED EQUIPMENT, DEFINITIONS OF (19 OCT 1973)., The purpose of this standard is to achieve standardization of the definitions listed herein which will eliminate major problems in effecting communications among the DOD services.

MIL-STD-1556B (NOTICE 1), MILITARY STANDARD GOVERNMENT/INDUSTRY DATA EXCHANGE PROGRAM (GIDEP) CONTRACTOR PARTICIPATION REQUIREMENTS. MIL-STD-1556, dated 24 February 1986, is hereby canceled. Guidance on participation in the GIDEP is contained in the Defense Acquisition Deskbook under "Information Structure" at Section 2.6A.

MIL-STD-1556B, MILITARY STANDARD GOVERNMENT/INDUSTRY DATA EXCHANGE PROGRAM (GIDEP) CONTRACTOR PARTICIPATION REQUIREMENTS. This standard establishes the requirements for contractor participation in the Government-Industry Data Exchange Program (GIDEP).

MIL-STD-1557A, MILITARY STANDARD, DESIGNATION OF AIRCRAFT PROPULSION RECIPROCATING ENGINES (25 OCT 1983) [S/S BY MIL-STD-1812]., This standard describes the method of assignment used by the Military Services in establishing the type and model designation of aircraft propulsion reciprocating engines.

MIL-STD-1559A (NOTICE 1) NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE, AND ENGINE MODULE ASSIGNMENT OF MIL-STD-1559A, dated 1 January 1984, and Notice 2, dated 14 June 1991, are hereby canceled and superseded by MIL-HDBK-1559, dated 14 February 1997.

MIL-STD-1559A (NOTICE 1) NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE, AND ENGINE MODULE ASSIGNMENT OF MIL-STD-1559A, dated 1 January 1984, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1559A (NOTICE 2) NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF The following changes form A part of MIL-STD_1559A, dated 1 January 1984, and is approved for use by all departments and agencies of the Department of Defense

MIL-STD-1559A MILITARY STANDARD NUMBERS, SERIAL, AIRCRAFT GAS TURBINE ENGINE AND ENGINE MODULE ASSIGNMENT OF. This standard describes the method of assignment and arrangement of letters and numerals used by the Military Services to identify complete engines and module (major subassemblies thereof) as to the manufacturer and series in production. The engine/module serial number shall be the only one required for assignment and application to the complete engine and modules thereof. This standard applies to propulsion engines and airborne auxilary power units.

MIL-STD-1560 INSERT ARRANGEMENTS FOR MIL-DTL-38999, MIL-DTL-27599 AND MIL-C-29600 SERIES A ELECTRICAL CIRCULAR CONNECTORS. This standard covers insert arrangements for use with MIL-DTL-38999 series I, II, III, IV, MIL-DTL-27599 series I and II; and MIL-C-29600 series A circular connectors.

MIL-STD-1560A (NOT 1) INSERT ARRANGEMENTS FOR MIL-C-38999 AND MIL-C-275999 ELECTRICAL, CIRCULAR CONNECTORS The following pages of MIL-STD_1560A have been revised and supersede the pages listed.

MIL-STD-1560A (NOTICE 2) INSERT ARRANGEMENTS FOR MIL-C-38999 AND MIL-C-27599 ELECTRICAL, CIRCULAR CONNECTORS The following pages of MIL-STD-1560A have been revised and supersede the pages listed

MIL-STD-1560A (NOTICE 3) INSERT ARRANGEMENTS FOR MIL-C 38999 AND MIL-C-275999 ELECTRICAL CIRCULAR CONNECTORS The following pages of MIL-STD-1560A have been revised and supersede the pages listed.

MIL-STD-1560A (NOTICE 4) INSERT ARRANGEMENTS FOR MIL-C-38999 AND MIL-C-275999 ELECTRICAL CIRCULAR CONNECTORS The following pages of MIL-STD-1560A are new or have been revised and supersede the pages listed.

MIL-STD-1560A (NOTICE 5) INSERT ARRANGEMENTS FOR MIL-C-38999 AND MIL-C-27599 ELECTRICAL CIRCULAR CONNECTORS The following pages of MIL-STD-1560A have been revised and supersede the pages listed.

MIL-STD-1560A (NOTICE 6) INSERT ARRANGEMENTS FOR MIL-C-38999, MIL-C-29600 SERIES A, AND MIL-C-275999 ELECTRICAL, CIRCULAR CONNECTORS Make teh following pen and ink changes to pages listed.

MIL-STD-1560A (NOTICE 7) INSERT ARRANGEMENTS FOR MIL-C-38999 AND MIL-C-27599 ELECTRICAL, CIRCULAR CONNECTORS MIL-STD-1560A, dated 25 June 1993, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1560A (NOTICE 8) INSERT ARRANGEMENTS FOR MIL-DTL-38999, MIL-C-29600 SERIES A, AND MIL-C-27599 ELECTRICAL, CIRCULAR CONNECTORS The following pages of MIL-STD-1560A have been revised and supersede the pages listed.

MIL-STD-1560A, DEPARTMENT OF DEFENSE INTERFACE STANDARD INSERT ARRANGEMENTS FOR MIL-C-38999 AND MIL-C-27599 ELECTRICAL, CIRCULAR CONNECTORS. This standard covers insert arrangements for use with MIL-C-38999 and MIL-C-27599 circular connectors.

MIL-STD-1561B, MILITARY STANDARD, PROVISIONING PROCEDURES, UNIFORM DOD (17 NOV 1984)., This standard applies to all end items, including components and support items, procured by the Department of Defense for which provisioning is required when incorporated by reference to contracts which are executed in behalf of the United States of America.

MIL-STD-1562W (NOTICE 1) MILITARY STANDARD LISTS OF STANDARD MICROCIRCUITS MIL-STD-1562W dated 25 September 1992, is hereby canceled without replacement.

MIL-STD-1562W MILITARY STANDARD LISTS OF STANDARD MICROCIRCUITS. This standard establishes the requirements for the selection of microcircuits used in its design, manufacture, and support of military equipment and identifies those devices which are less acceptable for new designs because of their nonavailability or impending obsolesce, or their problems in performance, reliability, or other characteristics.

MIL-STD-1564A (NOTICE 1) PROCEDURE FOR CALIBRATION AND ANALYSIS OF TRACE CONTAMINANTS IN AVIATOR'S BREATHING OXYGEN BY INFRARED SPECTROSCOPY The following pages of MIL-STD_1564A have been revised and supersede the pages listed.

MIL-STD-1564A (NOTICE 2) PROCEDURE FOR CALIBRATION AND ANALYSIS OF TRACE CONTAMINANTS IN AVIATOR'S BREATHING OXYGEN BY INFRARED SPECTROSCOPY The following pages of MIL-STD_1564A have been revised and supersede the pages listed

MIL-STD-1564A MILITARY STANDARD PROCEDURE FOR CALIBRATION AND ANALYSIS OF TRACE CONTAMINANTS IN AVIATOR'S BREATHING OXYGEN BY INFRARED SPECTROSCOPY. This Military Standard describes a procedure for determining trace gaseous contaminants in oxygen, nitrogen, and air by use of infrared spectroscopy.

MIL-STD-1567A (NOTICE 1) WORK MEASUREMENT The following pages of MIL-STD-1567A have been revised and supersede the pages listed.

MIL-STD-1567A (NOTICE 2) WORK MEASUREMENT The following pages of MIL-STD_1567A have been revised and supersede the pages listed.

MIL-STD-1567A (NOTICE 3) WORK MEASUREMENT MIL-STD-1567A, dated 11 March 1983, NOTICE 1 dated 3 May 1986, and NOTICE 2 dated 30 January 1987, are hereby canceled without replacement.

MIL-STD-1567A, MILITARY STANDARD, WORK MEASUREMENT (11 MAR 1983)., This standard requires the application of a discipline work management program as a management tool to improve productivity on those contracts to which it is applied. It establishes criteria which must be met by the Contractor's work measurement programs and provided guidance for implementation of these techniques and their use in assurance cost-effective development and production of systems and equipment.

MIL-STD-1568A MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS. This standard establishes the requirements for materials, processes, and techniques, and identifies the tasks required to implement an effective corrosion prevention and control program during the conceptual, validation, development, and production phases of aerospace weapons systems. The intent is to minimize life cycle cost due to corrosion.

MIL-STD-1568B (NOTICE 1) MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS The following pages of MIL-STD-1568B(USAF) have been revised and supersede the pages listed.

MIL-STD-1568B (NOTICE 2) MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS. MIL-STD-1568B(USAF) dated 12 October 1994 is hereby canceled.Future acquisition should refer to MIL-HDBK-1568, Materials and Processes for Corrosion Prevention and Control in Aerospace Weapons System. MIL-HDBK-1568 cannot be cited as a requirement. This document is to be used for guidance purposes only.

MIL-STD-1568B MILITARY STANDARD MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS. This standard establishes the requirements for materials, processes and techniques, and identifies the tasks required to implement an effective corrosion prevention and control program during the conceptual, validation, development, and production phases of aerospace weapon systems. The intent is to minimize life cycle cost due to corrosion and to obtain improved reliability.

MIL-STD-1570A, MILITARY STANDARD, OIL ANALYSIS IN EQUIPMENT DESIGN, PROVISIONS FOR (4 JUN 1987)., The purpose of this standard is to ensure that provisions for the Oil Analysis Program (OAP) are included in the design, development, and fabrication of equipment employing lubrication fluids in enclosed aeronautical and nonaeronautical mechanical systems. Design must facilitate OAP sampling to minimize manpower requirements and ensure the ability to take a representative sample.

MIL-STD-1574A MILITARY STANDARD SYSTEM SAFETY PROGRAM FOR SPACE AND MISSILE SYSTEMS. A system safety program, as specified herein, establishes administrative and technical means by which accident prevention requirements and policies are planned, managed, and implemented into the total program effort. The activities of the system safety program include: planning, management, design, analysis, research, operational functions, auditing, and training. The purpose of the program is to identify significant accident risk and define methods to cope effectively with that risk within program cost, schedule, performance, and technical acceptability parameters. This standard defines the requirements for implementation of system safety programs covering the life cycle of the system. It includes the safety requirements for the following activities/periods: design, development, test, checkout, modification, production, servicing, refurbishing, maintenance, transportation, handling, training, disposal, deployment, and normal and contingency operations. This standard also defines the management and technical tasks and controls required to minimize accident risks caused by human error, environment, deficiency/inadequacy of design, and component malfunction or interactions. Risks of concern are those those which could result in major injury of fatality to personnel including flight or ground crews, or damage to the system including support equipment and facilities.

MIL-STD-1576 (NOTICE 1), MILITARY STANDARD ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS (4 SEP 1992)., MIL-STS01576 (USAF), dated 28 MAY 1984, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-1576, MILITARY STANDARD ELECTROEXPLOSIVE SUBSYSTEM SAFETY REQUIREMENTS AND TEST METHODS FOR SPACE SYSTEMS (31 JUL 1984)., The purpose of this document is to insure the safety of personnel, launch site facilities, and space vehicles from the hazards resulting from electroexplosives subsystem unitentional initiation or failure to fire.

MIL-STD-1577A (USAF) (NOTICE 1), MILITARY STANDARD, INTERCONTINENTAL BALLISTIC MISSILE SYSTEMS TRAINING/TRAINING EQUIPMENT MANAGEMENT (25 MAR 1993) [SS BY MIL-STD-1379].

MIL-STD-1577A, MILITARY STANDARD, INTERCONTINENTAL BALLISTIC MISSILE SYSTEMS TRAINING/TRAINING EQUIPMENT MANAGEMENT (31 JUL 1985)., This Military Standard describes the functions, roles and responsibilities for development and management of Intercontinental Ballistic Missile (ICBM) Training and Training Systems. It is applicable to all agencies, offices, commands and contractors involved in the development, production or use of ICBM training equipment.

MIL-STD-1580A (NOTICE 1), TEST METHOD STANDARD DESTRUCTIVE PHYSICAL ANALYSIS FOR ELECTRONIC, ELECTROMAGNETIC, AND ELECTROMECHANICAL PARTS (18 AUG 2000)., TO ALL HOLDERS OF MIL-STD-1580A: 1. THE FOLLOWING PAGES OF MIL-STD-1580A HAVE BEEN REVISED AND SUPERSEDE THE PAGES LISTED:

MIL-STD-1580A (USAF), DOD TEST METHOD STANDARD DESTRUCTIVE PHYSICAL ANALYSIS FOR ELECTRONIC, ELECTROMAGNETIC, AND ELECTROMECHANICAL PARTS. This standard describes the general requirements for performane of destructive physical analysis (DPA) on samples of parts. In addition to the requirements for the analysis procedures, the general criteria for interpreting results, such as for the acceptance or rejection of associated production lots, is included for typical electronic, electromagnetic, and electromechanical parts.

MIL-STD-1580B (NOTICE 1), DOD TEST METHOD STANDARD DESTRUCTIVE PHYSICAL ANALYSIS (DPA) FOR ELECTRONIC, ELECTROMAGNETIC, AND ELECTROMECHANICAL (EEE) PARTS (23 APR 2003). TO ALL HOLDERS OF MIL-STD-1580B: 1. THE FOLLOWING PAGES OF REQUIREMENT 13 OF MIL-STD-1580B HAVE BEEN REVISED AND SUPERSEDE THE PAGES LISTED:

MIL-STD-1580B, DOD TEST METHOD STANDARD DESTRUCTIVE PHYSICAL ANALYSIS (DPA) FOR ELECTRONIC, ELECTROMAGNETIC, AND ELECTROMECHANICAL (EEE) PARTS (7 JAN 2003)., This standard describes the general requirements for performance of destructive physical analysis (DPA) on samples of parts. In addition to the requirements for the analysis procedures, the general criteria for interpreting results, such as for the acceptance or rejection of associated production lots, is included for typical electronic, electromagnetic, and electromechanical parts.

MIL-STD-1587C (NOTICE 1) MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEMS MIL-STD-1587C(USAF), dated July 1992, is hereby cancelled. Future acquisition should refer to MIL-HDBK-1587, Materials and Process Requirements for Air Force Weapon Systems. MIL-HDBK-1587 cannot be cited as a requirement. This document is to be used for guidance purposes only

MIL-STD-1587C (USAF), MILITARY STANDARD MATERIALS AND PROCESS REQUIREMENTS FOR AIR FORCE WEAPON SYSTEMS (21 JUL 1992)., This standard establishes the requirements for materials and processes used during design and production of aerospace weapon systems. When used in conjunction with MIL-STD-1 530, the other integrity program documents (MIL-STD-1783, 1798, etc.), and MIL-STD-1568, it is expected that structurally reliable aerospace systems having a good balance between acquisition costs and life cycle costs will result.

MIL-STD-1589C, MILITARY STANDARD, JOVIAL (J73) (6 JUL 1984)., MIL-STD-1589C (USAF) defines the upgraded JOVIAL (J73) programming language.

MIL-STD-1591 (NOTICE 1), MILITARY STANDARD, ON-AIRCRAFT, FAULT DIAGNOSIS, SUB-SYSTEMS, ANALYSIS/SYNTHESIS OF (27 JAN 1994)., MIL-STD-1591 dated 3 January 1977 is hereby cancelled.

MIL-STD-1591, MILITARY STANDARD, ON-AIRCRAFT, FAULT DIAGNOSIS, SUB-SYSTEMS, ANALYSIS/SYNTHESIS OF (3 JAN 1977)., This standard establishes uniform criteria for conducting trade studies to determine the optimal design for an on-aircraft fault diagnosis/isolation system, hereafter referred to as the On-Board Built-In Test System (OBBIT).

MIL-STD-1595A (NOTICE 1), MILITARY STANDARD, QUALIFICATION OF AIRCRAFT, MISSILE & AEROSPACE FUSION WELDERS (30 JUL 1987) [SUPERSEDED BY SAE-AMS-STD-1595].

MIL-STD-1595A (NOTICE 2), MILITARY STANDARD, QUALIFICATION OF AIRCRAFT, MISSILE & AEROSPACE FUSION WELDERS (16 JUN 1998) [SUPERSEDED BY SAE-AMS-STD-1595]., MIL-STD-1595A, dated 26 February 1982 is hereby canceled. Users may consider AMS-STD- 1595, “Qualification of Aircraft Missile and Aerospace Fusion Welders”, as a possible replacement. Users are cautioned to evaluate AMS-STD-1595 for their particular application before citing it as a replacement document.

MIL-STD-1595A, MILITARY STANDARD, QUALIFICATION OF AIRCRAFT, MISSILE & AEROSPACE FUSION WELDERS (26 FEB 1982) [SUPERSEDED BY SAE-AMS-STD-1595]., This standard establishes the procedure for qualification of welders and welding operators engaged in the welding of aircraft, missiles, other aerospace equipment, and their parts and accessories by fusion welding processes. This standard is applicable to aircraft, missile, and aerospace ground support equipment or other welding, when included in the contracting documents or when invoked in the absence of a specified welder qualification document.

MIL-STD-1597A (NOTICE 1), MILITARY STANDARD, QUALITY CONTROL OF LIQUID MISSILE PROPELLANTS AT CONTROL STORAGE POINTS (7 JUN 1997).

MIL-STD-1597A (NOTICE 2), MILITARY STANDARD, QUALITY CONTROL OF LIQUID MISSILE PROPELLANTS AT CONTROL STORAGE POINTS (25 AUG 1997).

MIL-STD-1597A, MILITARY STANDARD, QUALITY CONTROL OF LIQUID MISSILE PROPELLANTS AT CONTROL STORAGE POINTS (16 FEB 1987)., This military standard provides minimum guidance for quality control of liquid missile propellants at contractor's control storage points which store propellants owned by SA-ALC/SF, Kelly AFB TX, under the Fuels Division, Air Force Stock Fund for AF, other DOD agencies, NASA, Department of Energy (DOE).

MIL-STD-1598 (NOTICE 1), MILITARY STANDARD, STUDS PREFERRED FOR DESIGN, LISTING OF (27 JUL 1995)., MIL- STD-1598, dated 7 April 1978, is hereby cancelled without replacement .

MIL-STD-1598, MILITARY STANDARD, STUDS PREFERRED FOR DESIGN, LISTING OF (7 APR 1998)., This standard provides a listing of preferred studs encompassing the following characteristics: a. Configuration, b. Size, c. Materials, d. Protective Coatings and Finishes.

MIL-STD-1599, MILITARY STANDARD BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS (31 JAN 1980) [S/S BY MIL-HDBK-1599]., This standard covers bearings, control system components, and associated hardware, required methods of using these components, and materials, finishes, and test methods of these components for use in design and construction of’ aerospace mechanical systems, and covers the comprehensive presentation of approved engineering practices, procedures, and characteristics for the interface of these components.

MIL-STD-1599A (NOTICE 1),MILITARY STANDARD BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS (7 OCT 1982) [S/S BY MIL-HDBK-1599]. TO ALL HOLDERS OF MIL-STD-1599: 1. REPLACE OR ADD THE FOLLOWING PAGES TO MIL-STD-1599:

MIL-STD-1599A (NOTICE 2),MILITARY STANDARD BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS (7 OCT 1982) [S/S BY MIL-HDBK-1599]., TO ALL HOLDERS OF MIL-STD-1599: 1. REPLACE OR ADD THE FOLLOWING PAGES TO MIL-STD-1599:

MIL-STD-1599A (NOTICE 3),MILITARY STANDARD BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS (8 JUN 1988) [S/S BY MIL-HDBK-1599]., TO ALL HOLDERS OF MIL-STD-1599 1. ADD THE FOLLOWING PAGES TO MIL-STD-1599

MIL-STD-1599A (NOTICE 4),MILITARY STANDARD BEARINGS, CONTROL SYSTEM COMPONENTS, AND ASSOCIATED HARDWARE USED IN THE DESIGN AND CONSTRUCTION OF AEROSPACE MECHANICAL SYSTEMS AND SUBSYSTEMS (4 JAN 1993) [S/S BY MIL-HDBK-1599]., TO ALL HOLDERS OF MIL-STD-1599 1. Add the following pages to MIL-STD-1599