MIL-B-7949E (NOTICE 1), MILITARY SPECIFICATION BEARINGS, BALL, AIRFRAME, ANTI-FRICTION (23 JUL 1998) (S/S BY SAE-AS7949)

MIL-B-7949E (NOTICE 1), MILITARY SPECIFICATION BEARINGS, BALL, AIRFRAME, ANTI-FRICTION (23 JUL 1998) (S/S BY SAE-AS7949)., MIL-B-7949E(1), dated 02 July 1987, is hereby canceled. Future acquisition of this item should refer to SAE-AS7949 of the same title and dated April 1998. (Application for copies of SAE Aerospace Standards should be addressed to SAE, 400 Commonwealth Drive, Warrendale, PA 15096-0001.)

MIL-B-7949E (AMENDMENT 1), MILITARY SPECIFICATION BEARINGS, BALL, AIRFRAME, ANTI-FRICTION (2 JUL 1987) (S/S BY SAE-AS7949)

MIL-B-7949E (AMENDMENT 1), MILITARY SPECIFICATION BEARINGS, BALL, AIRFRAME, ANTI-FRICTION (2 JUL 1987) (S/S BY SAE-AS7949)., This amendment forms a part of Military Specification MIL-B-7949 dated 9 April 1981, and is approved for use by al1 Departments and Agencies of the Department of Defense.

MIL-B-7949E (SUPPLEMENT 1), MILITARY SPECIFICATION BEARINGS, BALL, AIRFRAME, ANTI-FRICTION (9 APR 1981) (S/S BY SAE-AS7949)

MIL-B-7949E (SUPPLEMENT 1), MILITARY SPECIFICATION BEARINGS, BALL, AIRFRAME, ANTI-FRICTION (9 APR 1981) (S/S BY SAE-AS7949)., This supplement forms a part of Military specification MIL-G-79U9E dated 9 April 1981 and is approved for use by all Departments and Agencies of the Department of Defense .

MIL-B-7949E, MILITARY SPECIFICATION BEARINGS, BALL, AIRFRAME, ANTI-FRICTION (9 APR 1981) (S/S BY SAE-AS7949)

MIL-B-7949E, MILITARY SPECIFICATION BEARINGS, BALL, AIRFRAME, ANTI-FRICTION (9 APR 1981) (S/S BY SAE-AS7949)., This specification covers anti-fiction bearings in the -65°F to 3500F temperature range as specified on the applicable military standard.

NAVSEA SL720-MAN-AA-xxx, TECHNICAL INSTRUCTIONAL GUIDANCE DOCUMENT (VER: 1.3), SHIP CHANGE DOCUMENT (SCD) (TS9090-400A) (MAR 2006

NAVSEA SL720-MAN-AA-xxx, TECHNICAL INSTRUCTIONAL GUIDANCE DOCUMENT (VER: 1.3), SHIP CHANGE DOCUMENT (SCD) (TS9090-400A) (MAR 2006)., This specification provides criteria for the uniform preparation, processing, and approval of a Ship Change Document (SCD).

NAVSEA SL720-AA-MAN-020, TS9090-600A, TECHNICAL SPECIFICATION, SHIP ALTERATION DRAWINGS PREPARATION (JUN 2002)

NAVSEA SL720-AA-MAN-020, TECHNICAL SPECIFICATION, SHIP ALTERATION DRAWINGS PREPARATION (TS9090-600A) (JUN 2002)., This specification provides minimum requirements for the uniform preparation of non-nuclear Ship Alteration (SHIPALT) Drawings (hereafter referred to as drawings) used for the accomplishment of all non-nuclear SHIPALTs except as noted herein (see 1.3).

NAVSEA SL720-AA-MAN-020 (VOLUME 2) TECHNICAL SPECIFICATION LIAISON ACTION RECORD (LAR) (TS9090-100A) (JUN 2002).

NAVSEA SL720-AA-MAN-020 (VOLUME 2) TECHNICAL SPECIFICATION LIAISON ACTION RECORD (LAR) (TS9090-100A) (JUN 2002)., This specification establishes requirements for a formal technical liaison system among SHAPEC Activities, Planning Yards (PYs), Supervisors of Shipbuilding Conversion and Repair (SUPSHIPs), Overhaul Yards, Space and Naval Warfare Systems Command (SPAWAR), Participating Managers (PARMs), Alteration Installation Teams (AITs), Ship Program Managers (SPMs), and other organizations involved in the Ship Alteration (SHIPALT) process.

NAVSEA SL720-AA-MAN-020, TECHNICAL SPECIFICATION, SHIP SELECTED RECORD DRAWINGS (TS9090-800A) (JUN 2002)

NAVSEA SL720-AA-MAN-020, TECHNICAL SPECIFICATION, SHIP SELECTED RECORD DRAWINGS (TS9090-800A) (JUN 2002)., This specification establishes the procedures for preparation of technically adequate Selected Record Drawings (SRDs) and consistent format and revision methodology for all active fleet ships of the U. S. Navy. This specification does not apply to Selected Record Drawings under the technical cognizance of NAVSEA 08.

MIL-R-12221D, MILITARY SPECIFICATION RIVET, SOLID, ALUMINUM ALLOY, GRADE 7277, TEMPERED (25 FEB 1985)

MIL-R-12221D, MILITARY SPECIFICATION RIVET, SOLID, ALUMINUM ALLOY, GRADE 7277, TEMPERED (25 FEB 1985)., This specification covers 7277 aluminum alloy rivets for structural use. Rivets of this composition are to be hot driven only at temperatures between 850 Deg. F and 975 Deg. F.

MIL-C-3301C, MILITARY SPECIFICATION COMPOUND, ASPHALTIC, HOT MELT (CAVITY LINING) (15 SEP 1970)

MIL-C-3301C, MILITARY SPECIFICATION COMPOUND, ASPHALTIC, HOT MELT (CAVITY LINING) (15 SEP 1970)., This specification covers a hot-melt asphaltic compound for coating the inner walls of metal cases prior to filling with explosives.

MIL-M-13508C, MIRROR, FRONT SURFACED ALUMINIZED: FOR OPTICAL ELEMENTS (19 MAR 1973)

MIL-M-13508C, MIRROR, FRONT SURFACED ALUMINIZED: FOR OPTICAL ELEMENTS (19 MAR 1973)., This specification covers a mirror coating consisting of a deposited aluminum reflective film overlaid with a transparent dielectric protective film applied on the front surface of optical elements.

MIL-Y-1140H (AMENDMENT 1), MILITARY STANDARD YARN, CORD, SLEEVING, CLOTH, AND TAPE-GLASS (25 SEP 1985)

MIL-Y-1140H (AMENDMENT 1), MILITARY STANDARD YARN, CORD, SLEEVING, CLOTH, AND TAPE-GLASS (25 SEP 1985)., The amendment for& a part of Military Specification MIL-Y-1140H dated 13 Dec 1972, and is approved for use by ,all Departments and Agencies of the Department of Defense.

MIL-Y-1140H, MILITARY STANDARD YARN, CORD, SLEEVING, CLOTH, AND TAPE-GLASS (13 DEC 1972)

MIL-Y-1140H, MILITARY STANDARD YARN, CORD, SLEEVING, CLOTH, AND TAPE-GLASS (13 DEC 1972)., This specification primarily covers the basic forms of untreated glass fiber used by themselves or as components of other materials.

MIL-STD-1907, MILITARY STANDARD INSPECTION, LIQUID PENETRANT AND MAGNETIC PARTICLE, SOUNDNESS REQUIREMENTS FOR MATERIALS, PARTS AND WELDMENTS (7 SEP 1

MIL-STD-1907, MILITARY STANDARD INSPECTION, LIQUID PENETRANT AND MAGNETIC PARTICLE, SOUNDNESS REQUIREMENTS FOR MATERIALS, PARTS AND WELDMENTS (7 SEP 1989)., This standard describes the discontinuity limits allowed under four quality level classifications for penetrant inspected and three quality level classifications for magnetic particle inspection. The materials may be forgings, castings, tubes, sheets, bars, etc. Fabrication stages may be machined, unmachined, welded, or unwelded parts/materials.

BOSS, FLUID CONNECTION - INTERNAL MS33649C, BOSS, FLUID CONNECTION - INTERNAL STRAIGHT THREAD (2 AUG 1984) (S/S BY SAE-AS5202)

MS33649C, BOSS, FLUID CONNECTION - INTERNAL STRAIGHT THREAD (2 AUG 1984) (S/S BY SAE-AS5202).

SAE-AS5202, ADOPTION NOTICE (17 JUL 2002)

SAE-AS5202, ADOPTION NOTICE (17 JUL 2002)., SAE AS5202 should be used instead of MS33649, which was cancelled on 17 July 2002. SAE-AS5202, "Port or Fitting End, Internal Straight Thread", was adopted on 17-JUL-02 for use by the Department of Defense (DoD). Proposed changes by DoD activities must be submitted to the DoD Adopting Activity: Defense Supply Center Columbus, P.O. Box 3990, Attn: DSCC-VAI, Columbus, OH 43216-5000. Copies of this document may be purchased from the Society of Automotive Engineers Inc., 400 Commonwealth Drive, Warrendale, PA 15096-0001 .

DOT/FAA/AR-07/39, REAL-TIME OPERATING SYSTEMS AND COMPONENT INTEGRATION CONSIDERATIONS IN INTEGRATED MODULAR AVIONICS SYSTEMS REPORT (AUG 2007) (FINAL

DOT/FAA/AR-07/39, REAL-TIME OPERATING SYSTEMS AND COMPONENT INTEGRATION CONSIDERATIONS IN INTEGRATED MODULAR AVIONICS SYSTEMS REPORT (AUG 2007) (FINAL REPORT)., The combination of rigorous development assurance and verification assurance has led to safe and reliable operation within civil aviation systems and equipment. Historically, such systems were designed as federated architectures, yet significantly successful efforts in integrated modular avionics (IMA) system integration have occurred, such as the Boeing 777 aircraft. This technical report can be used to formulate a basis for evaluating the integration of real-time operating systems (RTOS) and other associated modules that support partitioning in space, time, input/output, communications, and other shared resources on an IMA system. Several role players (platform supplier, RTOS supplier, application supplier, and the IMA system integrator) in IMA system development are discussed, and their roles of integrating multiple functions at different integration stages are detailed. [Key Words Integrated Modular Avionics, Software, DO-178, DO-297, RTOS, Partitioning]

MIL-STD-29A (NOTICE 1), MILITARY STANDARD SPRING, MECHANICAL, DRAWING REQUIREMENTS FOR (30 JAN 1998) (S/S BY ASME-Y14.13M)

MIL-STD-29A (NOTICE 1), MILITARY STANDARD SPRING, MECHANICAL, DRAWING REQUIREMENTS FOR (30 JAN 1998) (S/S BY ASME-Y14.13M)., MIL-STD-29A, dated 1 March 1962, is hereby canceled. Future acquisitions should refer to ASME Y1413M, Mechanical Spring Representation. (Application for copies of ASME publications should be addressed to the American Society of Mechanical Engineers, 345 East 47th Street, New York, NY 10017-2392)

MIL-STD-29A, MILITARY STANDARD SPRING, MECHANICAL, DRAWING REQUIREMENTS FOR (1 MAR 1962) (S/S BY ASME-Y14.13M)

MIL-STD-29A, MILITARY STANDARD SPRING, MECHANICAL, DRAWING REQUIREMENTS FOR (1 MAR 1962) (S/S BY ASME-Y14.13M). This standard illustrates the approved method of drawing, dimensioning, and specifying spring data on detailed drawings of each type of mechanical spring described herein.

AN818 (REV 19), AIR FORCE-NAVY AERONAUTICAL STANDARD NUT, TUBE COUPLING, SHORT (15 JUN 1994)

AN818 (REV 19), AIR FORCE-NAVY AERONAUTICAL STANDARD NUT, TUBE COUPLING, SHORT (15 JUN 1994).

MIL-C-83488C, DETAIL SPECIFICATION COATING, ALUMINUM, HIGH PURITY (1 DEC 1978)

MIL-C-83488C, DETAIL SPECIFICATION COATING, ALUMINUM, HIGH PURITY (1 DEC 1978)., This specification establishes the requirements for coating low alloy steel, stainless steel, aluminum alloy, copper alloy, and titanium alloy parts with high purity aluminum (99 percent plus) (see 6.1)

MIL-DTL-83488D, DETAIL SPECIFICATION COATING, ALUMINUM, HIGH PURITY (1 APR 1999)

MIL-DTL-83488D, DETAIL SPECIFICATION COATING, ALUMINUM, HIGH PURITY (1 APR 1999)., This specification establishes the requirements for coating low alloy steel, stainless steel, aluminum alloy, copper alloy, and titanium alloy parts with high purity aluminum (99 percent plus) (see 6.1).

MIL-S-81733D, SEALING AND COATING COMPOUND, CORROSION INHIBITIVE (13 MAR 1980)

MIL-S-81733D, SEALING AND COATING COMPOUND, CORROSION INHIBITIVE (13 MAR 1980)., This specification covers accelerated, room temperature curing synthetic rubber compounds used in the sealing and coating of metal components on weapons and aircraft systems for protection against corrosion.

DI-SESS-81527B, TRAINING SYSTEM SUPPORT DOCUMENT

DI-SESS-81527B, TRAINING SYSTEM SUPPORT DOCUMENT., The Training System Support Document provides complete procedures for utilization of all software utility programs, support software file generation, and system performance characteristics verification for life cycle maintenance.

DI-MCCR-80700, COMPUTER SOFTWARE PRODUCT END ITEMS

DI-MCCR-80700, COMPUTER SOFTWARE PRODUCT END ITEMS, The Computer Software Product End Item provides data formatted for review or maintenance to assure significant milestones are met.

MIL-PRF-7808L, PERFORMANCE SPECIFICATION LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE (2 MAY 1997)

MIL-PRF-7808L, PERFORMANCE SPECIFICATION LUBRICATING OIL, AIRCRAFT TURBINE ENGINE, SYNTHETIC BASE (2 MAY 1997)., This specification covers the requirements for two grades of aircraft turbine engine lubricating oil.

MIL-STD-2204 (NOTICE 1), MILITARY STANDARD SURVIVABLE ADAPTABLE FIBER OPTIC EMBEDDED NETWORK (SAFENET) (4 MAY 1998)

MIL-STD-2204 (NOTICE 1), MILITARY STANDARD SURVIVABLE ADAPTABLE FIBER OPTIC EMBEDDED NETWORK (SAFENET) (4 MAY 1998)., MIL-STD-2204, dated 31 October 1992, is hereby canceled without replacement.

MIL-STD-2204, MILITARY STANDARD SURVIVABLE ADAPTABLE FIBER OPTIC EMBEDDED NETWORK (SAFENET) (31 OCT 1992)

MIL-STD-2204, MILITARY STANDARD SURVIVABLE ADAPTABLE FIBER OPTIC EMBEDDED NETWORK (SAFENET) (31 OCT 1992)., This standard establishes requirements for the implementation of a Survivable Adaptable Fiber Optic Embedded Network, SAFENET.

MIL-DTL-26500F (SUPPLEMENT 1), DETAIL SPECIFICATION CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING, GENERAL SPECI

MIL-DTL-26500F (SUPPLEMENT 1), DETAIL SPECIFICATION CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING, GENERAL SPECIFICATION FOR (6 FEB 2004)., This supplement forms a part of MIL-DTL-26500F, dated 6 February 2004.

MIL-DTL-26500F, DETAIL SPECIFICATION CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING, GENERAL SPECIFICATION FOR 6

MIL-DTL-26500F, DETAIL SPECIFICATION CONNECTORS, GENERAL PURPOSE, ELECTRICAL, MINIATURE, CIRCULAR, ENVIRONMENT RESISTING, GENERAL SPECIFICATION FOR (6 FEB 2004)., This specification covers an environment-resisting family of miniature, circular, electrical connectors (plugs and receptacles), designed to meet the requirements of aerospace vehicles.

MS24264P, DETAIL SPECIFICATION SHEET CONNECTORS, RECEPTACLE, ELECTRICAL, FLANGE MOUNTING, MINIATURE, CLASSES F, G AND R (6 FEB 2004)

MS24264P, DETAIL SPECIFICATION SHEET CONNECTORS, RECEPTACLE, ELECTRICAL, FLANGE MOUNTING, MINIATURE, CLASSES F, G AND R (6 FEB 2004)., The requirements for acquiring the product described herein shall consist of this specification sheet and MIL-DTL-26500.

MIL-STD-637A (NOTICE 1), MILITARY STANDARD MACHINE AND AUTOMATIC GUNS AND MACHINE GUN TRAINERS THROUGH 30-MM (10 DEC 1962)

MIL-STD-637A (NOTICE 1), MILITARY STANDARD MACHINE AND AUTOMATIC GUNS AND MACHINE GUN TRAINERS THROUGH 30-MM (10 DEC 1962)., The following pages of Mil-Std-637A have been revised and supersede the pages listed.

MIL-STD-637A, MILITARY STANDARD MACHINE AND AUTOMATIC GUNS AND MACHINE GUN TRAINERS THROUGH 30-MM (13 FEB 1961)

MIL-STD-637A, MILITARY STANDARD MACHINE AND AUTOMATIC GUNS AND MACHINE GUN TRAINERS THROUGH 30-MM (13 FEB 1961)., The purpose of this standard list guide design selection and limit procurement for stock and issue of adopted Machine and Automatic Guns and Machinegun Trainers through 30-MM in FSC 1005. Prepared by the Army Ordnance Corps in conjunction with the Department of Defense Standardization Program, it is one of a series of limitation standards which will encompass all FSC 1005 weapons, accessories, and related-equipment.

QQ-B-637A, FEDERAL SPECIFICATION BRASS, NAVAL: ROD, WIRE, SHAPES, FORGINGS, AND FLAT PRODUCTS WITH FINISHED EDGES (BAR, FLAT WIRE, AND STRIP) (14 MAR

QQ-B-637A, FEDERAL SPECIFICATION BRASS, NAVAL: ROD, WIRE, SHAPES, FORGINGS, AND FLAT PRODUCTS WITH FINISHED EDGES (BAR, FLAT WIRE, AND STRIP) (14 MAR 1967) (S/S BY PORTIONS OF ASTM-B21, AND ASTM-B21M, ASTM-B124 AND ASTM-B283)., This specification covers alloys of leaded and nonleaded naval brass rod, wire, forgings, and flat products with finished edges (flat wire, strip, and bar). but does not include strip or bar finished with slit, sheared, sawed, or machined edges.

PRC-5001, REV D, PROCESS SPECIFICATION FOR CLEANING OF HARDWARE (JAN 2006)

PRC-5001, REV D, PROCESS SPECIFICATION FOR CLEANING OF HARDWARE (JAN 2006)., This process specification establishes surface cleanliness requirements for cleaning and packaging of JSC flight hardware and ground support equipment (GSE).

MIL-STD-2001, MANUALS, TECHNICAL, SYSTEMS OPERATOR'S INTERFACE PROCEDURES FOR WRITING MARKING OF ELECTRIC SYSTEMS (14 JAN 1987)

MIL-STD-2001, MANUALS, TECHNICAL, SYSTEMS OPERATOR'S INTERFACE PROCEDURES FOR WRITING MARKING OF ELECTRIC SYSTEMS (14 JAN 1987)., This standard establishes uniform style and format requirements for preparation of Systems Operator's Interface Technical Manuals.

MIL-L-40051E, LEATHER, CATTLEHIDE, FOR GLOVES (29 MAR 1991)

MIL-L-40051E, LEATHER, CATTLEHIDE, FOR GLOVES (29 MAR 1991)., This specification covers full grain cattlehide leather for gloves.

MIL-STD-361-1 (TM), MANUALS, TECHNICAL: WRITING STYLE AND FORMAT REQUIREMENTS (15 JUL 1992) (S/S BY MIL-STD-40051)

MIL-STD-361-1 (TM), MANUALS, TECHNICAL: WRITING STYLE AND FORMAT REQUIREMENTS (15 JUL 1992) (S/S BY MIL-STD-40051)., This document establishes the style and format for preparation of technical manuals (TMS), revisions, supplements, and changes.

MIL-T-5683A, MILITARY SPECIFICATION TERMINAL, TIE ROD, THREADED CLEVIS TYPE, AIRCRAFT (16 MAY 1950)

MIL-T-5683A, MILITARY SPECIFICATION TERMINAL, TIE ROD, THREADED CLEVIS TYPE, AIRCRAFT (16 MAY 1950)., This specification establishes the requirements for one type of tie rod terminals for aircraft applications.

AN665 AIR FORCE-NAVY AERONAUTICAL STANDARD TERMINAL-THREADED CLEVIS TYPE TIE ROD (25 MAR 1965)

AN665 (REV. 4), AIR FORCE-NAVY AERONAUTICAL STANDARD TERMINAL-THREADED CLEVIS TYPE TIE ROD (25 MAR 1965).