MIL-STD-756 Revision B:1981
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
RELIABILITY MODELING AND PREDICTION
04-05-1998
Paragraph
1 Scope
1.1 Scope
1.2 Application
1.3 Purpose
1.4 Numbering system
1.4.1 Classification of task sections, tasks and
methods
1.5 Revisions
1.5.1 Standard
1.5.2 Task sections, tasks, and methods
1.6 Method of reference
2 Referenced documents
2.1 Issues of documents
2.2 Other publications
3 Definitions
3.1 Terms
4 General requirements
4.1 General
4.2 Implementation
4.3 Ground rules and assumptions
4.4 Indenture level
4.5 Coding system
4.6 Mission success definition
4.7 Coordination of effort
4.8 General procedures
4.8.1 Item definition
4.8.2 Service use profile
4.8.2.1 Logistic cycle
4.8.2.2 Operational cycle
4.8.2.2.1 Mission profile
4.8.2.3 Environmental profile
4.9 Reliability modeling and prediction report
4.9.1 Summary
4.9.2 Reliability critical element lists
5 Detailed requirements
5.1 Task description and methods
5.1.1 Details to be specified
Figures
1 Service use events in the logistic and
operational cycles
102.1 Performance parameters, limits and failure
criteria
2003.1 Failure-rate estimating chart for electronic
analog function
2003.2 Failure-rate estimating chart for digital
electronics functions
2003.3 Failure-rate estimation chart for mechanical
devices
Tables
1002-I Truth table calculation for the mission
reliability diagram
1002-II Reduction tabulation
1003-I Logic diagram examples
1004-I Success/failure array for the mission
reliability diagram
200-I Environmental symbol identification and
description
2003-I Weighting factors for different classes of
electronic AEGs used in estimating analog
complexity for Figure 2003.1
2003-II Weighting factors for estimating digital
electronics AEG complexity for use with
Figure 2003.2
2003-III Weighting factors for shipboard mechanical
elements for use in conjunction with Figure
2003.3
Task Sections
100 Reliability modeling
200 Reliability prediction
Tasks
101 Basic reliability model
102 Mission reliability model
201 Basic reliability prediction
202 Mission reliability prediction
Methods
1001 Conventional probability
1002 Boolean truth table
1003 Logic diagram
1004 Monte carlo simulation
2001 Similar item method
2002 Similar circuit method
2003 Active element group method
2004 Parts count method
2005 Parts stress analysis method
Appendix A. Application and tailoring guide
Paragraph
10 General
10.1 Scope
10.2 Tailoring requirements
10.3 Duplication of effort
10.4 Limitations
20 Referenced documents
30 Definitions
40 General
40.1 Ordering data
40.2 Data item descriptions
50 Application criteria
50.1 General considerations
50.1.1 Level of detail
50.1.2 Timing
50.1.3 Intended use
Gives criteria for preparation of Mission and Basic Reliability models and predictions for electromechanical, electronic, electrical, mechanical and ordnance systems and equipment. Coverage includes application, referenced documents, coding system, service use profile, logistic cycle, indenture level, item definition, and reliability critical element lists. Also gives detailed diagrams.
DocumentType |
Standard
|
Pages |
88
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Withdrawn
|
ISO/TR 19972-1:2009 | Hydraulic fluid power Methods to assess the reliability of hydraulic components Part 1: General procedures and calculation method |
MIL-STD-1629 Revision A:1980 | PROCEDURES FOR PERFORMING A FAILURE MODE, EFFECTS AND CRITICALITY ANALYSIS |
MIL-A-85055 Base Document:1979 | Avionics System Performance Specification for A-4M/AV-8 Bombing Set, Angle Rate AN/ASB-19(V) |
MIL-T-5483 Revision D:1964 | TRANSMITTER, PRESSURE, SYNCHRO AIRCRAFT 165 DEGREE MOVEMENT |
PD ISO/TR 19972-1:2009 | Hydraulic fluid power. Methods to assess the reliability of hydraulic components General procedures and calculation method |
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BS EN 62308:2006 | Equipment reliability. Reliability assessment methods |
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MIL-T-28764 Base Document:1971 | TEST SET, RADAR, AN/UPM-136 |
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DEFSTAN 00-41/3(1993) : 1993 | RELIABILITY AND MAINTAINABILITY MOD GUIDE TO PRACTICES AND PROCEDURES |
04/30101075 DC : DRAFT JUN 2004 | |
MIL C 83867 : B | CONNECTOR, OXYGEN MASK HOSE NON-EJECTION TYPE |
MIL-A-81917 Base Document:1973 | Aircraft Firing Circuit Test Set AN/AWM-54 |
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MIL-D-28963 Revision A:1975 | |
MIL-D-81357 Revision A:1970 | Display Group, Tactical Data AN/ASA-70 |
MIL-T-24309 Base Document:1967 | TECHNICAL SUPPORT PLAN FOR ELECTRONIC EQUIPMENT |
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MIL D 49446 : A | DETECTOR DEWAR DT-591A/UA |
MIL-P-28739 Base Document:1970 | Pedestal Group, Antenna, for IFF Antennas AN/UPA-57 |
MIL-P-24764 Base Document:1991 | POWER SUPPLIES, SHIPBOARD, ELECTRONIC, GENERAL SPECIFICATION FOR |
MIL-C-81883 Base Document:1976 | CONTROL GROUP, ELECTRIC POWER OK-XXX (V) A GENERAL SPECIFICATION FOR |
MIL-F-8785 Revision C:1980 | FLYING QUALITIES OF PILOTED AIRPLANES |
MIL-I-23832 Revision A:1980 | Indicator, Tachometer, Triple Pointer, Helicopter |
MIL-P-23141 Revision D:1968 | PLOTTING TABLE, ANTI SUBMARINE AND DEAD RECKONING (NAVAL SHIPBOARD) |
EIA RB4 : A1969 | RELIABILITY QUANTIFICATION |
IEC 62308:2006 | Equipment reliability - Reliability assessment methods |
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MIL-STD-1591 Base Document:1977 | ON AIRCRAFT, FAULT DIAGNOSIS, SUBSYSTEMS, ANALYSIS SYNTHESIS OF |
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MIL-STD-882 Revision E:2012 | System Safety |
MIL-STD-780 Revision G:1992 | WORK UNIT CODES FOR AERONAUTICAL EQUIPMENT, UNIFORM NUMBERING SYSTEM |
MIL-STD-1670 Revision A:1976 | ENVIRONMENTAL CRITERIA AND GUIDELINES FOR AIR LAUNCHED WEAPONS |
MIL-STD-881 Revision C:2011 | WORK BREAKDOWN STRUCTURES FOR DEFENSE MATERIAL ITEMS |
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