MIL-STD-801A (NOTICE 1), MILITARY SPECIFICATION, INSPECTION AND ACCEPTANCE STANDARDS FOR PROPULSION FLUID CELL AND FITTINGS (23 DEC 1998)., MIL-STD-801A, dated 13 May 1981, is hereby canceled.

MIL-STD-801A (NOTICE 2), MILITARY STANDARD, INSPECTION AND ACCEPTANCE STANDARDS FOR PROPULSION FLUID CELL AND FITTINGS (8 MAR 2002)., MIL-STD-801A, dated 13 May 1981, is hereby reinstated and may be used for acquisition.

MIL-STD-801A, MILITARY STANDARD, INSPECTION AND ACCEPTANCE STANDARDS FOR PROPULSION FLUID CELL AND FITTINGS (13 MAY 1981)., This standard applies to all fluid cells manufactured in accordance with: MIL-T-5578, MIL-T-6396, MIL-T-27422.

MIL-STD-801B, MILITARY STANDARD, TEST METHODS FOR INSPECTION AND ACCEPTANCE STANDARDS FOR PROPULSION FLUID CELLS AND FITTINGS (1 AUG 2002)., This standard establishes a test method standard for propulsion fluid cells and installed fittings. This standard applies to all fluid cells manufactured in accordance with MIL-T-5578, MIL-T-6396 (except type I), and MIL-DTL-27422.

MIL-STD-802 (NOTICE 1), MILITARY STANDARD, NUMBERS, AIRCRAFT ENGINES AND ENGINE CYLINDERS, COMBUSTION CHAMBERS, FLAME TUBES, INNER LINERS, AND SIMILAR ITEMS (12 NOV 1987)., MILITARY STANDARD MIL-STD-802 dated 17 August 1970 is hereby canceled.

MIL-STD-802, MILITARY STANDARD, NUMBER, AIRCRAFT ENGINES AND ENGINE CYLINDERS, COMBUSTION CHAMBERS, FLAME TUBES, INNER LINERS, AND SIMILAR ITEMS (17 APR 1970)., This standard is intended to designate unambiguously the position of aircraft engines and components.

MIL-STD-808A(USAF) (NOTICE 1), MILITARY STANDARD, FINISH, PROTECTIVE, AND CODES FOR FINISHING SCHEMES FOR GROUND AND GROUND SUPPORT AND EQUIPMENT. MIL-STD-808A(USAF), dated 18 January 1983, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-808A(USAF) (NOTICE 2), MILITARY STANDARD, FINISH, PROTECTIVE AND CODES FOR FINISHING SCHEMES FOR GROUND AND GROUND SUPPORT AND EQUIPMENT (18 JUL 1996)., MIL-STD808A(USAF), dated 18 January 1983 and Notice 1 dated 30 July 1987, is hereby canceled.

MIL-STD-808A(USAF), MILITARY STANDARD, FINISHES, MATERIALS, AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN SUPPORT EQUIPMENT (18 JAN 1983) [S/S BY MIL-HDBK-808]. The purpose of this standard is to establish acceptable requirements for materials selection, materials processing, cleaning processes, finishing materials and finishing processes and techniques for effective protection against corrosion for support equipment excluding munitions and electronic equipment. This standard covers both organic and inorganic finishes. A finish code system is provided for identifying the selected finish on engineering drawings.

MIL-STD-809B (NOTICE 1), MILITARY STANDARD, ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF (1 JUL 1999) [S/S BY SAE-AS8091]., MIL-STD-809B, dated 01 December 1986, is hereby canceled. Future design criteria for this item should refer to SAE-AS8-8091, "Adapter, Aircraft, Jacking Point, Design and Installation of," dated April 1999.

MIL-STD-809B, MILITARY STANDARD, ADAPTER, AIRCRAFT, JACKING POINT, DESIGN AND INSTALLATION OF (1 DEC 1986) [S/S BY SAE-AS8091]., This standard provides requirements for design and installation of aircraft jacking point adapters, as identified by ASCC AIR STD 25/7 Aircraft Jacking Pads, to permit use of standard jacking equipment.

MIL-STD-810D (NOTICE 1), MILITARY STANDARD, ENVIRONMENTAL TEST METHODS AND ENGINEERING GUIDELINES (31 JUL 1986). The following pages of MIL-STD-810D have been revised and supersede the pages listed.

MIL-STD-810E (NOTICE 2), MILITARY STANDARD, ENVIRONMENTAL TEST METHODS AND ENGINEERING GUIDELINES (1 SEPT 1993)., The following pages of MIL-STD-810D have been revised and supersede the pages listed.

MIL-STD-810E (NOTICE 3), MILITARY STANDARD, ENVIRONMENTAL TEST METHODS AND ENGINEERING GUIDELINES (31 JUL 1995)., TO ALL HOLDERS OF MIL–STD–810E: 1. THE FOLLOWING PAGES OF MIL–STD–810E HAVE BEEN REVISED AND SUPERSEDE THE PAGES.

MIL-STD-810E, MILITARY STANDARD, ENVIRONMENTAL TEST METHODS AND ENGINEERING GUIDELINES (14 JUL 1989). Guidelines for conducting environmental engineering tasks to tailor environmental tests to end-item equipment applications. Test methods for determining the effects of natural and induced environments on equipment use din military applications.

MIL-STD-810F (NOTICE 1), MILITARY STANDARD, TEST METHODS, ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS (1 NOV 2000)., TO ALL HOLDERS OF MIL-STD-810F: THE FOLLOWING PAGES OF MIL-STD-810F HAVE BEEN REVISED AND SUPERSEDE THE PAGES LISTED:

MIL-STD-810F (NOTICE 2), MILITARY STANDARD, TEST METHODS, ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS (30 AUG 2002)., TO ALL HOLDERS OF MIL-STD-810F: THE FOLLOWING PAGES OF MIL-STD-810F HAVE BEEN REVISED AND SUPERSEDE THE PAGES

MIL-STD-810F (NOTICE 3), MILITARY STANDARD, TEST METHODS, ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS (5 MAY 2003)., TO ALL HOLDERS OF MIL-STD-810F: THE FOLLOWING PAGES OF MIL-STD-810F HAVE BEEN REVISED AND SUPERSEDE THE PAGES LISTED:

MIL-STD-810F, MILITARY STANDARD, TEST METHODS, ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS (1 JAN 2000)., This standard contains materiel acquisition program planning and engineering direction for considering the influences that environmental stresses have on materiel throughout all phases of its service life. It is important to note that this document does not impose design or test specifications. Rather, it describes the environmental tailoring process that results in realistic materiel designs and test methods based on materiel system performance requirements.

MIL-STD-814D (NOTICE 1), MILITARY STANDARD, REQUIREMENTS FOR TIEDOWN, SUSPENSION AND EXTRACTION PROVISIONS ON MILITARY MATERIAL FOR AIRDROP (11 JUN 2002). MIL-STD-814D, dated 3 February 1997, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-814D, MILITARY STANDARD, REQUIREMENTS FOR TIEDOWN, SUSPENSION AND EXTRACTION PROVISIONS ON MILITARY MATERIEL FOR AIRDROP (3 FEB 1997)., This standard establishes the design, number, and location requirements of airdrop, tiedown, suspension, and extraction provisions on airdrop items delivered by LVAD.

MIL-STD-831 (NOTICE 1), MILITARY STANDARD, TEST REPORTS, PREPARATION OF (23 APR 1999)., MIL-STD-831, dated 28 August 1963, is hereby canceled without replacement.

MIL-STD-831, MILITARY STANDARD, TEST REPORTS, PREPARATION OF (28 AUG 1963)., This standard delineates the format and content criteria to be used in the preparation of test reports covering tests on systems, subsystems, equipments, components, and parts.

MIL-STD-834C (NOTICE 1), MILITARY STANDARD, PACKAGING DATA FORMS, INSTRUCTIONS FOR PREPARATION AND USE OF (10 DEC 1974) [S/S BY MIL-STD-2073-1]., The following pages of this standard have been revised and supersede the pages listed.

MIL-STD-834C (NOTICE 2), MILITARY STANDARD, PACKAGING DATA FORMS, INSTRUCTIONS FOR PREPARATION AND USE OF (8 SEPT 1989) [S/S BY MIL-STD-2073-1]., MIL-STD-834, dated 10 December 1974, is inactive for new design.

MIL-STD-834C (NOTICE 3), MILITARY STANDARD, PACKAGING DATA FORMS, INSTRUCTIONS FOR PREPARATION AND USE OF (23 JUN 1993) [S/S BY MIL-STD-2073-1]., MIL-STD-834C, dated 10 December 1974, is hereby canceled. Future acquisitions should refer to MIL-STD-2073-1, "DOD Materiel, Procedures for development and Applications of Packaging Requirements (Part 1 of 2 Parts).

MIL-STD-834C, MILITARY STANDARD, PACKAGING DATA FORMS, INSTRUCTIONS FOR PREPARATION AND USE OF (1 MAR 1974) [S/S BY MIL-STD-2073-1]., This standard outlines procedures and provides necessary guidance and instructions which shall be used in preparation, approval, use and transmittal of packaging data utilizing codes established by MIL-STD-726.

MIL-STD-838C (NOTICE 1), MILITARY STANDARD, LUBRICATION OF MILITARY EQUIPMENT (3 DEC 1997) [S/S BY MIL-HDNK-838]., MIL-STD-838c, dated, 30 December 1983, is hereby canceled and superseded by MIL-HDBK-838, dated.

MIL-STD-838C, MILITARY STANDARD, LUBRICATION OF MILITARY EQUIPMENT (30 DEC 1983)., This standard establishes the requirements and procedures applicable to the selection and application of lubricants required for the lubrication of flight and surface vehicles, and their associated equipment, electronic equipment, and shipboard equipment.

MIL-STD-841B(USAF) (NOTICE 1), MILITARY STANDARD, MARKING OF AIRCRAFT AND MISSILE PROPULSION SYSTEM PARTS FABRICATED FROM CRITICAL HIGH TEMPERATURE ALLOYS (18 MAY 1996)., MIL-STD-841B, dated 01 July 1971, is hereby canceled without replacement.

MIL-STD-841B(USAF), MILITARY STANDARD, MARKING OF AIRCRAFT AND MISSILE PROPULSION SYSTEM PARTS FABRICATED FROM CRITICAL HIGH TEMPERATURE ALLOYS (1 JUL 1971)., This document establishes physical item marking requirements for aircraft and missile propulsion system parts and assemblies fabricated from critical high temperature alloys. The requirements of this standard are in addition to the identification marking required by MIL-STD-130.

MIL-STD-845A (NOTICE 1), MILITARY STANDARD, FITTINGS, TETRAFLUOROETHYLENE HOSE HIGH TEMPERATURE, MEDIUM PRESSURE CLASSIFICATION OF DEFECTS (18 MAY 1996). MIL-STD-845A, "dated 30 June 1972" is hereby canceled without replacement .

MIL-STD-845A, MILITARY STANDARD, FITTINGS, TETRAFLUOROETHYLENE HOSE HIGH TEMPERATURE, MEDIUM PRESSURE CLASSIFICATION OF DEFECTS (30 JUN 1972)., This standard covers the classification of defects for fittings covered by MIL-F-27272.

MIL-STD-846C(USAF) (NOTICE 1), MILITARY STANDARD, ESCAPE SYSTEM TESTING: GROUND, TRACK, AND FLIGHT TEST (17 NOV 1977)., To all holders of MIL-STD-846C(USAF), Page 12 of MIL-STD-846C(USAF) has been revised and supersedes page 12 dated 22 January 1974.

MIL-STD-846C(USAF) (NOTICE 2), MILITARY STANDARD, ESCAPE SYSTEM TESTING: GROUND, TRACK, AND FLIGHT TEST (26 FEB 1988)., MIL-STD-846C(USAF) dated 22 January 1974 and Notice 1 dated 17 November 1977 have been reviewed and determined to be valid for use in acquisition.

MIL-STD-846C(USAF) (NOTICE 3), MILITARY STANDARD, ESCAPE SYSTEM TESTING: GROUND, TRACK, AND FLIGHT TEST (29 MAY 1996)., MIL-STD-846C, dated 22 January 1974, is hereby canceled without replacement.

MIL-STD-846C(USAF), MILITARY STANDARD, ESCAPE SYSTEM TESTING: GROUND, TRACK, AND FLIGHT TEST (20 JAN 1974)., This standard prescribes uniform test procedures to be used as the basis for system design approval of crew emergency escape systems. This standard is applicable to crew module, ejection seat, and tractor rocket extraction seat escape systems. It covers the following types of system tests: integration tests, static tests, track tests, and flight tests.

MIL-STD-847B (NOTICE 1), MILITARY STANDARD, FORMAT REQUIREMENTS FOR SCIENTIFIC AND TECHNICAL REPORTS PREPARED BY OR FOR THE DEPARTMENT OF DEFENSE (25 MAY 1988) [S/S BY ANSI Z39.18]. MIL-STD-847B, dated 7 November 1983, is hereby canceled and superseded by ANSI Z39.18.

MIL-STD-847B, MILITARY STANDARD, FORMAT REQUIREMENTS FOR SCIENTIFIC AND TECHNICAL REPORTS PREPARED BY OR FOR THE DEPARTMENT OF DEFENSE (7 NOV 1983) [S/S BY ANSI Z39.18]., This standard establishes format requirements for scientific and technical reports, including the DD form. Report documentation Page prepared by or for the Departments and Agencies of the Department of Defense. Its provisions are mandatory for in-house, contractor, or grantee reports according to the Defense Acquisition Regulation (DAR) and the Department of Defense Directives and Instructions.

MIL-STD-849A, MILITARY STANDARD, INSPECTION REQUIREMENTS, DEFINITIONS AND CLASSIFICATION OF DEFECTS FOR PARACHUTES (15 MAR 1974)., This standard establishes the inspection requirements and a standard classification and final assembly defects for parachutes.

MIL-STD-849B, MILITARY STANDARD, INSPECTION REQUIREMENTS, DEFINITIONS AND CLASSIFICATION OF DEFECTS FOR PARACHUTES (25 JUL 2001)., This standard establishes the inspection requirements and a standard classification of manufacturing and final assembly defects for parachutes.

MIL-STD-850B (NOTICE 1), MILITARY STANDARD, AIRCREW STATION VISION REQUIREMENTS FOR MILITARY AIRCRAFT (23 NOV 1984)., To all holders of MIl-STD-850B, the following pages of MIL-STD-850B have been revised and supersede the pages listed.

MIL-STD-850B (NOTICE 2), MILITARY STANDARD, AIRCREW STATION VISION REQUIREMENTS FOR MILITARY AIRCRAFT (5 DEC 1995). MIL-STD-850B dated 3 November 1970, is hereby canceled without replacement.

MIL-STD-850B, MILITARY STANDARD, AIRCREW STATION VISION REQUIREMENTS FOR MILITARY AIRCRAFT (3 NOV 1970)., The purpose of this document is to establish requirements for providing adequate external vision from within the aircrew stations of military aircraft.

MIL-STD-851A (NOTICE 1), MILITARY STANDARD, CODING: MANUFACTURER'S COLOR, NYLON PARACHUTE CLOTH (6 OCT 1970)., To the holders of MIL-STD-851A(ASG), the following pages of MIL-STD-851A have been revised and supersede the pages listed.

MIL-STD-851A (NOTICE 2), MILITARY STANDARD, CODING: MANUFACTURER'S COLOR, NYLON PARACHUTE CLOTH (15 APR 1975)., To all holders of MIL-STD-851 the following page of MIL-STD-851A has been revised and supersedes the page listed.

MIL-STD-851A, MILITARY STANDARD, CODING: MANUFACTURER'S COLOR, NYLON PARACHUTE CLOTH (16 AUG 1968)., This military standard establishes the color codings to be used by textile manufacturers for the purpose of identifying their respective products, when so specified by the detail specification for the material or by the procuring company.

MIL-STD-852 (NOTICE 1), MILITARY STANDARD, GLASS BEAD PEENING PROCEDURES (18 APR 1988)., MIL-STD-852, dated 21 Sep 65, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-852 (NOTICE 2), MILITARY STANDARD, GLASS BEAD PEENING PROCEDURES (12 JAN 1996)., MIL-STD-852, dated 18 APRIL 1988, is hereby canceled without replacement.

MIL-STD-852, MILITARY STANDARD, GLASS BEAD PEENING PROCEDURES (21 SEPT 1965)., This standard establishes minimum requirements and procedures for glass bead peening of ferrous and non-ferrous parts which are subjected to repeated applications of stress such as the following: axles, landing gear parts, springs, gears, structural extrusions, and wing panels. The purpose of such peening is to relieve stress, increase fatigue life and increase resistance to stress corrosion.

MIL-STD-858 (NOTICE 1), MILITARY STANDARD, TESTING STANDARD FOR PERSONNEL PARACHUTES (5 DEC 1995)., MIL-STD-858 dated 26 June 1969, is hereby canceled without replacement.

MIL-STD-858, MILITARY STANDARD, TESTING STANDARD FOR PERSONNEL PARACHUTES (26 JUN 1969)., This standard establishes test methods and procedures for the developmental and qualification testing of experimental man-carrying parachute assemblies and components thereof, and outlines the general categories of personnel parachutes. The test methods and procedures contained herein are intended to specify suitable static and dynamic test conditions, to provide a wide range of data applicable to actual service conditions, and to obtain repeatability of the test results. It is not intended that this document contain detailed acceptance criteria for all test methods but that it provide the necessary performance standard relative to the escape requirements established for various weapons systems.

MIL-STD-859A (NOTICE 1), MILITARY STANDARD, STANDARD CALIBRATION TABLE FOR AERONAUTICAL PRESSURE MEASURING EQUIPMENT (1 FEB 1979)., To all holders of MIL-STD-859A, make the following pen and ink changes.

MIL-STD-859A (NOTICE 2), MILITARY STANDARD, STANDARD CALIBRATION TABLE FOR AERONAUTICAL PRESSURE MEASURING EQUIPMENT (20 SEPT 1995)., MIL-STD-859A, dated 13 November 1968, and NOTICE 1, dated 1 February 1979, are hereby canceled without replacement.

MIL-STD-859A, MILITARY STANDARD, STANDARD CALIBRATION TABLE FOR AERONAUTICAL PRESSURE MEASURING EQUIPMENT (13 NOV 1968)., This standard establishes the static pressure p in inches of mercury for values of pressure altitude H in geopotential feet to be used in the design and calibration of all aircraft equipment whose operation is a function of atmospheric pressure.

MIL-STD-864B (NOTICE 1), MILITARY STANDARD, SUPPORT EQUIPMENT FUNCTIONAL CLASSIFICATION CATEGORIES (18 MAY 1996)., MIL-STD-864B, dated 29 January 1982, is hereby canceled without replacement.

MIL-STD-864B, MILITARY STANDARD, SUPPORT EQUIPMENT FUNCTIONAL CLASSIFICATION CATEGORIES (29 JAN 1982)., Thus standard was established to provide Government personnel and contractors with a means of comparing Support Equipment and Mission Equipment according to functional and technical requirements.

MIL-STD-865C(USAF) (NOTICE 1), MILITARY STANDARD, SELECTIVE (BRUSH PLATING), ELECTRODEPOSITION (9 DEC 1996)., MIL-STD-865C, dated 1 November, 1988, 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-865C(USAF), MILITARY STANDARD, SELECTIVE (BRUSH PLATING), ELECTRODEPOSITION (1 NOV 1988)., This standard covers the process and materials for selective electrodeposition of various metals and alloys on ferrous alloys, aluminum alloys, copper alloys, nickel alloys, and corrosion-resistant steel, etc.

MIL-STD-865D(USAF), MILITARY STANDARD, SELECTIVE (BRUSH PLATING), ELECTRO-DESPOSITION (1 MAR 2007)., This standard covers the process and materials for selective electro-desposition of various metals and alloys on ferrous alloys, aluminum alloys, copper alloys, nickel alloys and corrosion-resistant steel, etc.

MIL-STD-866B(USAF) (NOTICE 2), MILITARY STANDARD, GRINDING OF CHROME PLATED STEEL AND STEEL PARTS HEAT TREATED TO 180,000 PSI OR OVER (9 DEC 1996). MIL-STD-866B, dated 28 June, 1978, 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-866B(USAF), MILITARY STANDARD, GRINDING OF CHROME PLATED STEEL AND STEEL PARTS HEAT TREATED TO 180,000 PSI OR OVER (28 JUN 1978). This standard covers the requirements for grinding of martensitic high strength steel heat-treated to 180,000 pounds per square inch (PSI), ultimate tensile strength (UTS) and above, and the grinding of chromium plating applied to such high strength steel, when such parts are intended for use in components for man-rated flight hardware.

MIL-STD-867A(USAF) (NOTICE 1), MILITARY STANDARD, TEMPER ETCH INSPECTION (9 DEC 1996)., MIL-STD-867A, dated 23 March, 1979, 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-867A(USAF), MILITARY STANDARD, TEMPER ETCH INSPECTION (23 MAR 1979)., This standard establishes requirements and tests for performing temper etch inspection of carburized steels and took and low alloy steels which are heat treated above 1.24 x 10^9 Pascal (PA) [1.26 x 10^2 kilogram-force/square millimeter (Kgf/mm^2) 1.8 x 10^5 pound-force/square inch (psi)]

MIL-STD-868A(USAF) (NOTICE 1), MILITARY STANDARD, NICKEL PLATING, LOW EMBRITTLEMENT, ELECTRODEPOSITION (24 MAR 1986)., MIL-STD-868A, dated 23 March 1979, is hereby validated, and determined adequate for acquisition.

MIL-STD-868A(USAF) (NOTICE 2), MILITARY STANDARD, NICKEL PLATING, LOW EMBRITTLEMENT, ELECTRODEPOSITION (9 DEC 1996)., MIL-STD-868A, dated 23 March, 1979, 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-868A(USAF), MILITARY STANDARD, NICKEL PLATING, LOW EMBRITTLEMENT, ELECTRODEPOSITION (23 MAR 1979)., This standard covers the process and materials required for the electrodeposition of nickel on high strength steel substrates. Subsequent heat treating techniques needed to insure low embrittlement of steel are also described.

MIL-STD-869C(USAF) (NOTICE 1), MILITARY STANDARD, FLAME SPRAYING (9 DEC 1996)., MIL-STD-869C, dated 20 October, 1988, 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-869C(USAF), MILITARY STANDARD, FLAME SPRAYING (20 OCT 1988)., This standard covers the materials, procedures, and equipment for flame spraying of parts. Flame spraying is defined as the process of melting materials in a heating zone and propelling them in the molten state onto a part to form a coating. This process can be applied to build up worn areas on parts, for abrasion resistance and/or corrosion protection. It is not intended to rebuild damage by nicks, gouges, etc., without building an entire area.

MIL-STD-870B (NOTICE 1), MILITARY STANDARD, CADMIUM PLATING, LOW EMBRITTLEMENT, ELECTRODEPOSITION (9 DEC 1996)., MIL-STD-870B, dated 30 July, 1986, 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-870B(USAF), MILITARY STANDARD, CADMIUM PLATING, LOW EMBRITTLEMENT, ELECTRODEPOSITION (30 JUL 1986). This standard covers the process and materials required for the electrodeposition of cadmium on high strength steel substrates. Subsequent heat treating techniques needed to insure low embrittlement of steel are also described.

MIL-STD-875A (NOTICE 1), MILITARY STANDARD, TYPE DESIGNATION SYSTEM FOR AERONAUTICAL AND SUPPORT EQUIPMENT (26 FEB 1988) [S/S BY MIL ST-1812]. MIL-STD-875A dated 30 April 1974 has been reviewed and determined to be valid for use in acquisition.

MIL-STD-875A (NOTICE 2), MILITARY STANDARD, TYPE DESIGNATION SYSTEM FOR AERONAUTICAL AND SUPPORT EQUIPMENT (16 JUL 1993) [S/S BY MIL ST-1812]., MIL-STD-875A, dated 30 April 1974, is hereby canceled and superseded by MIL-STD-1812, Type Designation, Assignment and Method for Obtaining.

MIL-STD-875A, MILITARY STANDARD, TYPE DESIGNATION SYSTEM FOR AERONAUTICAL AND SUPPORT EQUIPMENT (30 APR 1974) [S/S BY MIL ST-1812]. The purpose of this standard is to provide a type designation system, and procedures for its use, for the Department of Defense to standardize the identification of Aeronautical and Support Equipment as defined herein.

MIL-STD-877 (NOTICE 1), MILITARY STANDARD, ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF (8 NOV 1968)., The following pages of MIL-STD-877 have been revised and supersede the pages listed.

MIL-STD-877 (NOTICE 2), MILITARY STANDARD, ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF (26 FEB 1988)., The following pages of MIL-STD-877 have been revised and supersede the pages listed.

MIL-STD-877 (NOTICE 3), MILITARY STANDARD, ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF (28 SEPT 1995)., MIL-STD-877 dated 9 July 1968, is hereby canceled without replacement.

MIL-STD-877, MILITARY STANDARD, ANTENNA SUBSYSTEMS, AIRBORNE, CRITERIA FOR DESIGN AND LOCATION OF (9 JUL 1968)., This standard covers the general criteria for the design and location of all antenna subsystems used on flight vehicles. It is not intended to preclude techniques, processes, materials, and methods of design and location which will lead to improvement of military airborne antenna sub-systems. This standard is primarily for use by the flight vehicle manufacturer.

MIL-STD-878B (USAF), DEPARTMENT OF DEFENSE STANDARD PRACTICE METHOD OF DIMENSIONING AND DETERMINING CLEARANCE FOR AIRCRAFT TIRES AND RIMS (21 NOV 2006)., This standard establishes the procedures for dimensioning and determining clearance for aircraft tires and rims.

MIL-STD-881A, MILITARY STANDARD, WORK BREAKDOWN STRUCTURES FOR DEFENSE MATERIEL ITEMS (25 APR 1975)., This standard establishes criteria governing the preparation and employment of work breakdown structures for use during the acquisition of designated defense materiel items to display and define the products to be developed or produced.

MIL-STD-881B (NOTICE 1), MILITARY STANDARD, WORK BREAKDOWN STRUCTURES FOR DEFENSE MATERIEL ITEMS (2 JAN 1998) [S/S BY MIL-HDK-881]., MIL-STD-881B, dated 25 March 1993, is hereby canceled. Information and guidance for Work Breakdown Structures (WBS) is now contained in MIL-HDBK-881, “Work Breakdown Structure”.

MIL-STD-881B, MILITARY STANDARD, WORK BREAKDOWN STRUCTURES FOR DEFENSE MATERIEL ITEMS (25 MAR 1993) [S/S BY MIL-HDK-881]., This standard establishes criteria governing the preparation and employment of work breakdown structures for use during the acquisition of designated defense materiel items to display and define the products to be developed or produced.

MIL-STD-882C (NOTICE 1), MILITARY STANDARD, SYSTEM SAFETY PROGRAM REQUIREMENTS (19 JAN 1996)., To all holders of MIL-STD-882C, make the following pen and ink changes.

MIL-STD-882C, MILITARY STANDARD, SYSTEM SAFETY PROGRAM REQUIREMENTS (19 JAN 1993)., This standard applies to all DOD systems and facilities. It provides uniform requirements for developing and implementing a system and safety program of sufficient comprehensiveness to identify the hazards of a system and to impose design requirements and management controls to prevent mishaps.

MIL-STD-882D, MILITARY STANDARD, STANDARD PRACTICE FOR SYSTEM SAFETY (10 FEB 2000)., This document outlines a standard practice for conducting system safety. The system safety practice as defined herein conforms to the acquisition procedures in DoD Regulation 5000.2-R and provides a consistent means of evaluating identified risks.

MIL-STD-883E (NOTICE 1), MILITARY STANDARD, MICROCIRCUITS, TEST STANDARDS (1 DEC 1997)., The following test methods of MIL-STD-883E have been revised and supersede the test methods listed.

MIL-STD-883E (NOTICE 2), MILITARY STANDARD, MICROCIRCUITS, TEST STANDARDS (24 AUG 1998)., The following test methods of MIL-STD-883E have been revised and supersede the test methods listed.

MIL-STD-883E (NOTICE 3), MILITARY STANDARD, MICROCIRCUITS, TEST STANDARDS (5 NOV 1999)., The following test methods of MIL-STD-883E have been revised and supersede the test methods listed.

MIL-STD-883E (NOTICE 4), MILITARY STANDARD, MICROCIRCUITS, TEST STANDARDS (18 DEC 2000)., The following test methods of MIL-STD-883E have been revised and supersede the test methods listed.

MIL-STD-883E (NOTICE 5), MILITARY STANDARD, MICROCIRCUITS, TEST STANDARDS (7 MAR 2003)., The following test methods of MIL-STD-883E have been revised and supersede the test methods listed.

MIL-STD-883E, MILITARY STANDARD, MICROCIRCUITS, TEST STANDARDS (31 DEC 1996)., This standard establishes uniform methods, controls, and procedures for testing microelectronic devices suitable for use within Military and Aerospace electronic systems including basic environmental tests to determine resistance to deleterious effects of natural elements and conditions surrounding military and space operations, mechanical and electrical tests workmanship and training procedures and such other controls and constraints as have been deemed necessary to ensure a uniform level of quality and reliability suitable to the intended applications of those devices.

MIL-STD-883F, MILITARY STANDARD, MICROCIRCUITS, TEST STANDARDS (18 JUN 2004)., This standard establishes uniform methods, controls, and procedures for testing microelectronic devices suitable for use within Military and Aerospace electronic systems including basic environmental tests to determine resistance to deleterious effects of natural elements and conditions surrounding military and space operations, mechanical and electrical tests workmanship and training procedures and such other controls and constraints as have been deemed necessary to ensure a uniform level of quality and reliability suitable to the intended applications of those devices.

MIL-STD-884C (NOTICE 1), MILITARY STANDARD, ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION (5 NOV 1988)., MIL-STD-884C, dated 25 April 1975, has been reviewed and determined to be valid for use in acquisition.

MIL-STD-884C (NOTICE 2), MILITARY STANDARD, ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION (1 DEC 1993)., MIL-STD-884C, dated 25 April 1975, is hereby canceled without replacement.

MIL-STD-884C, MILITARY STANDARD, ELECTRONICALLY OR OPTICALLY GENERATED DISPLAYS FOR AIRCRAFT CONTROL AND COMBAT CUE INFORMATION (25 APR 1975)., The purpose of this standard is to establish design requirements for electronically and optically generated aircraft displays which provide visual cues of flight and combat information for fixed-wing aircraft. Electronically and optically generated displays are those devices by which an image is presented to the observer directly on the image-generating surface and indirectly through an optical projection system. For this standard, the term E/O display is restricted to those devices used in aircraft for the purpose of flight or mission control. Separate radar or electronic warfare displays are not included.

MIL-STD-889B (NOTICE 1), MILITARY STANDARD, DISSIMILAR METALS (21 NOV 1979)., The following pages of MIL-SD-889B have been revised and supersede the pages listed.

MIL-STD-889B (NOTICE 2), MILITARY STANDARD, DISSIMILAR METALS (4 MAR 1988)., MIL_STD-889B dated 7 July 1976 and Notice 1 dated 21 November 1979 have been reviewed an