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TO 00-5-1, TECHNICAL MANUAL AF TECHNICAL ORDER SYSTEM
TO 00-5-1, TECHNICAL MANUAL AF TECHNICAL ORDER SYSTEM. The purpose of this technical order (TO) is to describe the Air Force TO system established by Air Force Policy Directive (AFPD) 21-3, specify policies and responsibilities for operation and management of the TO system, and outline general procedures for use of the system. This TO identifies and explains the various types of TOs and the specific policies and procedures pertaining thereto.
Ident. Num:
TO 00-5-1
Rev. Num:
-
TO 00-5-1, TECHNICAL MANUAL AF TECHNICAL ORDER SYSTEM. The purpose of this technical order (TO) is to describe the Air Force TO system established by Air Force Policy Directive (AFPD) 21-3, specify policies and responsibilities for operation and management of the TO system, and outline general procedures for use of the system. This TO identifies and explains the various types of TOs and the specific policies and procedures pertaining thereto.
MIL-HDBK-1461A, DOD HANDBOOK AMMUNITION MANUFACTURERS AND THEIR SYMBOLS (1 APR 1999)
MIL-HDBK-1461A, DOD HANDBOOK AMMUNITION MANUFACTURERS AND THEIR SYMBOLS (1 APR 1999). This handbook establishes and describes the manufacturer's identification symbol used in the lot numbers for all DOD contracted manufacture, renovation, or regrouping of ammunition and ammunition components. The usage of manufacturer's identification symbols is defined and described in MIL-STD-1168, Ammunition Lot Numbering.
Ident. Num:
MIL-HDBK-1461
Rev. Num:
A
MIL-HDBK-1461A, DOD HANDBOOK AMMUNITION MANUFACTURERS AND THEIR SYMBOLS (1 APR 1999). This handbook establishes and describes the manufacturer's identification symbol used in the lot numbers for all DOD contracted manufacture, renovation, or regrouping of ammunition and ammunition components. The usage of manufacturer's identification symbols is defined and described in MIL-STD-1168, Ammunition Lot Numbering.
AEROSPACE REPORT NUMBER: TOR-2006(8583)-5236, TECHNICAL REQUIREMENTS FOR ELECTRONIC PARTS, MATERIALS, AND PROCESSES USED IN SPACE AND LAUNCH VEHICLES
AEROSPACE REPORT NUMBER: TOR-2006(8583)-5236, TECHNICAL REQUIREMENTS FOR ELECTRONIC PARTS, MATERIALS, AND PROCESSES USED IN SPACE AND LAUNCH VEHICLES (13 NOV 2006). The requirements of this document were developed for long mission life and/or high reliability space and launch vehicle equipment for successful operations of space hardware. Attention to every detail is required at every level of assembly throughout development, manufacture, qualification, and testing, starting with the parts, materials, and processes used. This document supersedes Aerospace Technical Operating Report TOR-2004(3909)-3316, titled Technical Requirements for Electronics Parts, Materials, and Processes Used in Space and Launch Vehicles, and shall be used for all future procurements of space, launch, and experimental programs. The objective of this document is to specify the technical baseline in the selection, application, procurement, control and standardization of parts (electrical and mechanical), materials, and processes for space and launch vehicles. This TOR is intended to be used in conjunction with TOR-2006(8583)-5235 (Parts, Materials, and Processes Control Program for Space and Launch Vehicles) in order to achieve a high reliability space program. Every effort was made to utilize standard document format, but this document retains the separately called out technical sections (starting with Section 100) to focus the user industry on the unique space quality items that are paramount for mission success in each technical section. The Referenced Documents Section includes active, inactive, or canceled specifications and standards. When no superseding document is called out, or the superseding document is believed not to include the necessary requirements, then the inactive or canceled specification is listed with the last known revision letter and annotated as either inactive or canceled.
Ident. Num:
TOR-2006(8583)-5236
Rev. Num:
-
AEROSPACE REPORT NUMBER: TOR-2006(8583)-5236, TECHNICAL REQUIREMENTS FOR ELECTRONIC PARTS, MATERIALS, AND PROCESSES USED IN SPACE AND LAUNCH VEHICLES (13 NOV 2006). The requirements of this document were developed for long mission life and/or high reliability space and launch vehicle equipment for successful operations of space hardware. Attention to every detail is required at every level of assembly throughout development, manufacture, qualification, and testing, starting with the parts, materials, and processes used. This document supersedes Aerospace Technical Operating Report TOR-2004(3909)-3316, titled Technical Requirements for Electronics Parts, Materials, and Processes Used in Space and Launch Vehicles, and shall be used for all future procurements of space, launch, and experimental programs. The objective of this document is to specify the technical baseline in the selection, application, procurement, control and standardization of parts (electrical and mechanical), materials, and processes for space and launch vehicles. This TOR is intended to be used in conjunction with TOR-2006(8583)-5235 (Parts, Materials, and Processes Control Program for Space and Launch Vehicles) in order to achieve a high reliability space program. Every effort was made to utilize standard document format, but this document retains the separately called out technical sections (starting with Section 100) to focus the user industry on the unique space quality items that are paramount for mission success in each technical section. The Referenced Documents Section includes active, inactive, or canceled specifications and standards. When no superseding document is called out, or the superseding document is believed not to include the necessary requirements, then the inactive or canceled specification is listed with the last known revision letter and annotated as either inactive or canceled.
MIL-STD-1275B, DOD INTERFACE STANDARD CHARACTERISTICS OF 28 VOLT DC ELECTRICAL SYSTEMS IN MILITARY VEHICLES
MIL-STD-1275B, DOD INTERFACE STANDARD CHARACTERISTICS OF 28 VOLT DC ELECTRICAL SYSTEMS IN MILITARY VEHICLES. This standard covers the limits of transient voltage characteristics and steady state limits of the 28 volt (V) direct current (dc) electric power circuits of military vehicles.
Ident. Num:
MIL-STD-1275
Rev. Num:
B
MIL-STD-1275B, DOD INTERFACE STANDARD CHARACTERISTICS OF 28 VOLT DC ELECTRICAL SYSTEMS IN MILITARY VEHICLES. This standard covers the limits of transient voltage characteristics and steady state limits of the 28 volt (V) direct current (dc) electric power circuits of military vehicles.
GSFC PPL-21 (NOTICE 1), PREFERRED PARTS LIST
GSFC PPL-21 (NOTICE 1), PREFERRED PARTS LIST. The GSFC PPL-21 supersedes PPL-20 (Rev 1). This latest edition combines and updates information from MIL-STD-975 and PPL-20 to create a stand-alone document. It also incorporates screening requirements form GSFC 311-INST-001 to provide Grade 1 and Grade 2 screening requirements for all parts categories.
Ident. Num:
PPL-21
GSFC PPL-21 (NOTICE 1), PREFERRED PARTS LIST. The GSFC PPL-21 supersedes PPL-20 (Rev 1). This latest edition combines and updates information from MIL-STD-975 and PPL-20 to create a stand-alone document. It also incorporates screening requirements form GSFC 311-INST-001 to provide Grade 1 and Grade 2 screening requirements for all parts categories.
MIL-HDBK-1516, MILITARY HANDBOOK UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIEL
MIL-HDBK-1516, MILITARY HANDBOOK UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIEL. This handbook 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).
Ident. Num:
MIL-HDBK-1516
Rev. Num:
-
MIL-HDBK-1516, MILITARY HANDBOOK UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIEL. This handbook 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-961D, DEPARTMENT OF DEFENSE STANDARD PRACTICE DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT.
MIL-STD-961D, DEPARTMENT OF DEFENSE STANDARD PRACTICE DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT. This standard establishes the format and content requirements for the preparation of defense specification and program-unique specifications prepared either by DoD activities or by contractors for the DoD.
Ident. Num:
MIL-STD-961
Rev. Num:
D
MIL-STD-961D, DEPARTMENT OF DEFENSE STANDARD PRACTICE DEFENSE AND PROGRAM-UNIQUE SPECIFICATIONS FORMAT AND CONTENT. This standard establishes the format and content requirements for the preparation of defense specification and program-unique specifications prepared either by DoD activities or by contractors for the DoD.
MIL-HDBK-1547A, DOD HDBK ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES
MIL-HDBK-1547A, DOD HDBK ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES. This Handbook was developed to aid Designers and Parts, Materials, and Processes (PMP) specialists with the design, development, and fabrication of electronic systems required to have long life and/or high reliability while operating under extreme conditions/ environments of Space and Launch Vehicles. The purpose of this handbook is to establish and maintain consistent and uniform methods for development of technical requirements for electronic parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles. It provides a common basis for the estimation of Application Information, Design and Construction Considerations, and Quality Assurance Provisions for the proposed Design Application. It also establishes a common basis for comparing and evaluating of industry practices for related or competitive designs. This handbook is intended to be used as a tool to increase the performance and reliability of the system under design.
Ident. Num:
MIL-HDBK-1547
Rev. Num:
A
MIL-HDBK-1547A, DOD HDBK ELECTRONIC PARTS, MATERIALS, AND PROCESSES FOR SPACE AND LAUNCH VEHICLES. This Handbook was developed to aid Designers and Parts, Materials, and Processes (PMP) specialists with the design, development, and fabrication of electronic systems required to have long life and/or high reliability while operating under extreme conditions/ environments of Space and Launch Vehicles. The purpose of this handbook is to establish and maintain consistent and uniform methods for development of technical requirements for electronic parts, materials, and processes used in the design, development, and fabrication of space and launch vehicles. It provides a common basis for the estimation of Application Information, Design and Construction Considerations, and Quality Assurance Provisions for the proposed Design Application. It also establishes a common basis for comparing and evaluating of industry practices for related or competitive designs. This handbook is intended to be used as a tool to increase the performance and reliability of the system under design.
MIL-STD-794E, MILITARY STANDARD PARTS AND EQUIPMENT, PROCEDURES FOR PACKAGING OF
MIL-STD-794E, MILITARY STANDARD PARTS AND EQUIPMENT, PROCEDURES FOR PACKAGING OF. This standard provides procedures for packaging parts and equipment based on their material composition, surface finish, size, weight, fragility, configuration and the intended level of protection.
Ident. Num:
MIL-STD-794
Rev. Num:
E
MIL-STD-794E, MILITARY STANDARD PARTS AND EQUIPMENT, PROCEDURES FOR PACKAGING OF. This standard provides procedures for packaging parts and equipment based on their material composition, surface finish, size, weight, fragility, configuration and the intended level of protection.
ECSS-Q-70-71A REV. 1, SPACE PRODUCT ASSURANCE DATA FOR SELECTION OF SPACE MATERIALS AND PROCESSES
ECSS-Q-70-71A REV. 1, SPACE PRODUCT ASSURANCE DATA FOR SELECTION OF SPACE MATERIALS AND PROCESSES. General requirements for materials and their associated processes are provided in this Standard along with the environmental requirements for materials application in space. Annex A (informative) contains guidelines for each class of material used in the declared materials list (DML) in ECSS--Q--70 and factors to be considered for process selection. Annex B (informative) contains data sheets for materials that can be considered for use in space applications i.e. materials that were used successfully for some applications in space systems and associated equipment. Data sheets contain: property data -- either from manufacturers or determined by test, and comments onmaterial application in space conditions. The data sheets are grouped by their DML material class, using the class number, e.g. Class 1: Aluminium and Al-- alloys; and Class 10: Adhesives, coatings and varnishes.
Ident. Num:
ECSS-Q-70-71
Rev. Num:
A
ECSS-Q-70-71A REV. 1, SPACE PRODUCT ASSURANCE DATA FOR SELECTION OF SPACE MATERIALS AND PROCESSES. General requirements for materials and their associated processes are provided in this Standard along with the environmental requirements for materials application in space. Annex A (informative) contains guidelines for each class of material used in the declared materials list (DML) in ECSS--Q--70 and factors to be considered for process selection. Annex B (informative) contains data sheets for materials that can be considered for use in space applications i.e. materials that were used successfully for some applications in space systems and associated equipment. Data sheets contain: property data -- either from manufacturers or determined by test, and comments onmaterial application in space conditions. The data sheets are grouped by their DML material class, using the class number, e.g. Class 1: Aluminium and Al-- alloys; and Class 10: Adhesives, coatings and varnishes.
MIL-STD-2219A, MILITARY STANDARD FUSION WELDING FOR AEROSPACE APPLICATIONS
MIL-STD-2219A, MILITARY STANDARD FUSION WELDING FOR AEROSPACE APPLICATIONS. The scope of this document is to provide minimum requirements for weld filler materials, workmanship, inspection and record requirements for fusion welding of alloys applicable to aircraft, missiles, other aerospace equipment, their parts and accessories.
Ident. Num:
MIL-STD-2219
Rev. Num:
A
MIL-STD-2219A, MILITARY STANDARD FUSION WELDING FOR AEROSPACE APPLICATIONS. The scope of this document is to provide minimum requirements for weld filler materials, workmanship, inspection and record requirements for fusion welding of alloys applicable to aircraft, missiles, other aerospace equipment, their parts and accessories.
MIL-STD-1646B, MILITARY STANDARD SERVICING TOOLS FOR ELECTRIC CONTACTS AND CONNECTIONS, SELECTION AND USE O
MIL-STD-1646B, MILITARY STANDARD SERVICING TOOLS FOR ELECTRIC CONTACTS AND CONNECTIONS, SELECTION AND USE OF. This standard provides selected electrical contact crimping tools, turret heads, positioners, die sets, wire wrap tools, installing tools, removal tools, and grommet sealing plugs which are mandatory for use with all military electrical connectors and connections.
Ident. Num:
MIL-STD-1646
Rev. Num:
B
MIL-STD-1646B, MILITARY STANDARD SERVICING TOOLS FOR ELECTRIC CONTACTS AND CONNECTIONS, SELECTION AND USE OF. This standard provides selected electrical contact crimping tools, turret heads, positioners, die sets, wire wrap tools, installing tools, removal tools, and grommet sealing plugs which are mandatory for use with all military electrical connectors and connections.
SSP 30237F, SPACE STATION ELECTROMAGNETIC EMISSION AND SUSCEPTIBILITY REQUIREMENTS
SSP 30237F, SPACE STATION ELECTROMAGNETIC EMISSION AND SUSCEPTIBILITY REQUIREMENTS. The Space Station Electromagnetic Emission and Susceptibility Requirements for Electromagnetic Compatibility document establishes the requirements for the control of the electromagnetic emission and susceptibility characteristics of electronic, electrical and electromechanical equipment and subsystems designed or procured for use by the International Space Station Alpha Program. The contents of this document are intended to be consistent with the requirements of SSP 30243, Space Station Requirements for Electromagnetic Effects and SSP 41000, System Specification for the Space Station. The Space Station Electromagnetic Emission and Susceptibility Requirements for Electromagnetic Compatibility shall be implemented on all SSP contracts and internal activities. This document is under the control of the Space Station Control Board.
Ident. Num:
SSP 30237
Rev. Num:
F
SSP 30237F, SPACE STATION ELECTROMAGNETIC EMISSION AND SUSCEPTIBILITY REQUIREMENTS. The Space Station Electromagnetic Emission and Susceptibility Requirements for Electromagnetic Compatibility document establishes the requirements for the control of the electromagnetic emission and susceptibility characteristics of electronic, electrical and electromechanical equipment and subsystems designed or procured for use by the International Space Station Alpha Program. The contents of this document are intended to be consistent with the requirements of SSP 30243, Space Station Requirements for Electromagnetic Effects and SSP 41000, System Specification for the Space Station. The Space Station Electromagnetic Emission and Susceptibility Requirements for Electromagnetic Compatibility shall be implemented on all SSP contracts and internal activities. This document is under the control of the Space Station Control Board.
NAVEDTRA 14026, CONSTRUCTION ELECTRICIAN BASIC NON-RESIDENT TRAINING COURSE (JAN 1998)
NAVEDTRA 14026, CONSTRUCTION ELECTRICIAN BASIC NON-RESIDENT TRAINING COURSE (JAN 1998)., This training manual (TRAMAN) replaces Construction Electrician 3 and should be studied by those seeking advancement to Construction Electrician Third Class.
Ident. Num:
NAVEDTRA 14026
Rev. Num:
-
NAVEDTRA 14026, CONSTRUCTION ELECTRICIAN BASIC NON-RESIDENT TRAINING COURSE (JAN 1998)., This training manual (TRAMAN) replaces Construction Electrician 3 and should be studied by those seeking advancement to Construction Electrician Third Class.
MIL-STD-2000A, MILITARY STANDARD STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES
MIL-STD-2000A, MILITARY STANDARD STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES. This standard establishes requirements for materials and procedures for making soldered connections in electrical and electronic assemblies. Soldered connections for leads and wires inserted in holes, surface mounted to kinds, or attached to terminals shall be in accordance with this standard. In addition, component mounting requirements and acceptance criteria are provided to permit evaluation of complete assemblies.
Ident. Num:
MIL-STD-2000
Rev. Num:
A
MIL-STD-2000A, MILITARY STANDARD STANDARD REQUIREMENTS FOR SOLDERED ELECTRICAL AND ELECTRONIC ASSEMBLIES. This standard establishes requirements for materials and procedures for making soldered connections in electrical and electronic assemblies. Soldered connections for leads and wires inserted in holes, surface mounted to kinds, or attached to terminals shall be in accordance with this standard. In addition, component mounting requirements and acceptance criteria are provided to permit evaluation of complete assemblies.
MIL-STD-1327A, MILITARY STANDARD FLANGES, COAXIAL WAVEGUIDE; AND COUPLING ASSEMBLIES, SELECTION OF
MIL-STD-1327A, MILITARY STANDARD FLANGES, COAXIAL WAVEGUIDE; AND COUPLING ASSEMBLIES, SELECTION OF. This standard provides standard sizes of rectangular waveguide flanges, ridged waveguide flanges, rigid air dielectric coaxial flanges, and coupling assemblies for use with subminiature waveguide flanges considered by the Department of Defense as standard for use in military equipment and applications.
Ident. Num:
MIL-STD-1327
Rev. Num:
A
MIL-STD-1327A, MILITARY STANDARD FLANGES, COAXIAL WAVEGUIDE; AND COUPLING ASSEMBLIES, SELECTION OF. This standard provides standard sizes of rectangular waveguide flanges, ridged waveguide flanges, rigid air dielectric coaxial flanges, and coupling assemblies for use with subminiature waveguide flanges considered by the Department of Defense as standard for use in military equipment and applications.
MIL-HDBK-1222, MILITARY HANDBOOK GUIDE TO THE GENERAL STYLE AND FORMAT OF U.S. ARMY WORK PACKAGE TECHNICAL MANUALS
MIL-HDBK-1222, MILITARY HANDBOOK GUIDE TO THE GENERAL STYLE AND FORMAT OF U.S. ARMY WORK PACKAGE TECHNICAL MANUALS. This handbook provides non-regulatory guidance and information for the preparation of technical manuals (TM) required to operate and maintain the various types of equipment and weapon systems within the Department of the Army. It provides preferred format and general writing style, graphics, revisions, comprehensibility, and security guidance for the preparation of both paper and digital delivery of TMs. Although this handbook encourages the use of d@al files, the requirement for digital tiles, paper, or both will be specified by the squiring activity. This handbook provides guidance only. It cannot be cited as a requirement. If it is, the contractor does not have to comply.
Ident. Num:
MIL-HDBK-1222,
Rev. Num:
-
MIL-HDBK-1222, MILITARY HANDBOOK GUIDE TO THE GENERAL STYLE AND FORMAT OF U.S. ARMY WORK PACKAGE TECHNICAL MANUALS. This handbook provides non-regulatory guidance and information for the preparation of technical manuals (TM) required to operate and maintain the various types of equipment and weapon systems within the Department of the Army. It provides preferred format and general writing style, graphics, revisions, comprehensibility, and security guidance for the preparation of both paper and digital delivery of TMs. Although this handbook encourages the use of d@al files, the requirement for digital tiles, paper, or both will be specified by the squiring activity. This handbook provides guidance only. It cannot be cited as a requirement. If it is, the contractor does not have to comply.
MS16142C, MILITARY STANDARD BOSS, GASKET SEAL STRAIGHT THREAD TUBE FITTING, STANDARD DIMENSIONS FOR (21 JUN 1979) (S/S BY SAE-J1926/1 AND ISO725)
MS16142C, MILITARY STANDARD BOSS, GASKET SEAL STRAIGHT THREAD TUBE FITTING, STANDARD DIMENSIONS FOR (21 JUN 1979) (S/S BY SAE-J1926/1 AND ISO725).
Ident. Num:
MS16142
Rev. Num:
C
MS16142C, MILITARY STANDARD BOSS, GASKET SEAL STRAIGHT THREAD TUBE FITTING, STANDARD DIMENSIONS FOR (21 JUN 1979) (S/S BY SAE-J1926/1 AND ISO725).
DI-ADMN-81249A, CONFERENCE AGENDA
DI-ADMN-81249A, CONFERENCE AGENDA. The conference agenda provides information concerning purpose, location, and schedule of conferences required to manage the acquisition of systems equipment, related items, and services.
Ident. Num:
DI-ADMN-81249
Rev. Num:
A
DI-ADMN-81249A, CONFERENCE AGENDA. The conference agenda provides information concerning purpose, location, and schedule of conferences required to manage the acquisition of systems equipment, related items, and services.
MIL-STD-1623D(SH), DEPARTMENT OF DEFENSE DESIGN CRITERIA STANDARD FIRE PERFORMANCE REQUIREMENTS AND APPROVED SPECIFICATIONS FOR INTERIOR FINISH MATER
MIL-STD-1623D(SH), DEPARTMENT OF DEFENSE DESIGN CRITERIA STANDARD FIRE PERFORMANCE REQUIREMENTS AND APPROVED SPECIFICATIONS FOR INTERIOR FINISH MATERIALS AND FURNISHINGS (NAVAL SHIPBOARD USE). The purpose of this standard is to establish fire performance criteria and provide a list of approved specifications for interior finish materials and furnishings to be used on Naval surface ships and submarines. Although the development of limits for toxic products of combustion is of major concern, the information generally available is not refined to the degree to allow inclusion of finite limits in this standard at this time.
Ident. Num:
MIL-STD-1623
Rev. Num:
D
MIL-STD-1623D(SH), DEPARTMENT OF DEFENSE DESIGN CRITERIA STANDARD FIRE PERFORMANCE REQUIREMENTS AND APPROVED SPECIFICATIONS FOR INTERIOR FINISH MATERIALS AND FURNISHINGS (NAVAL SHIPBOARD USE). The purpose of this standard is to establish fire performance criteria and provide a list of approved specifications for interior finish materials and furnishings to be used on Naval surface ships and submarines. Although the development of limits for toxic products of combustion is of major concern, the information generally available is not refined to the degree to allow inclusion of finite limits in this standard at this time.
