SAE AIR 5109 : 2012

1 Scope
  1.1 Purpose
  1.2 Relation to other PM documents
2 References
  2.1 Applicable documents
      2.1.1 SAE Publications
      2.1.2 U.S Government Publications
      2.1.3 Other References
  2.2 Acronyms
      2.2.1 Section 1
      2.2.2 Section 2
      2.2.3 Section 3
      2.2.4 Section 4
      2.2.5 Section 5
3 Mechanical Engineering
  3.1 Automotive Industry
  3.2 Power Generation
  3.3 Munitions Packaging
  3.4 Summary Sheets
      3.4.1 Reliability of Wheel Return
      3.4.2 Probabilistic Design Using Design of Experiments
             for Fuel Injector
      3.4.3 Door Structure Robustness and Drop-off
      3.4.4 Robustness of Driveline Imbalance NVH
  3.5 Detailed Example - Dimensional Control Team Variation
      Simulation Analysis Interference Between Steering Column
      Coupler and Duffy Pad
      3.5.1 Objective
      3.5.2 General Assumptions
      3.5.3 Discussion
      3.5.4 Results
      3.5.5 Conclusion
  3.6 Detailed Example - Munitions Packaging
      3.6.1 Introduction
      3.6.2 Nomenclature
      3.6.3 Conclusion
4 Aerospace Engineering
  4.1 Aircraft
      4.1.1 Airframe
      4.1.2 Gas Turbine Engines
      4.1.3 Rotorcraft
  4.2 Spacecraft
  4.3 Avionics
  4.4 Subsystems
  4.5 Summary Sheets
      4.5.1 Retirement for cause
      4.5.2 Rotorcraft Critical Dynamic Components
      4.5.3 Integrated Probabilistic Composite Design
      4.5.4 Probabilistic Analysis of an In-service Fatigue
             Cracking Problem of a High Pressure Turbine Bladed
             Disk
      4.5.5 Solder Reliability
      4.5.6 Structural Reliability Analysis of the HL-20 Personal
             Launch System Spacecraft
      4.5.7 Probabilistic Approaches for Design and Analysis of
             the Composite Tank for Single Stage to Orbit Program
      4.5.8 Joint Stars Risk Assessment
      4.5.9 Probability of Fragment Injury to a Pilot Following
             a Canopy Bird Strike
      4.5.10 Reliability Estimates of Lear Fan 2100 Aircraft Wing
             Using Developed Probabilistic Software for Composite
             Aircraft Components
      4.5.11 Reliability Estimates of Lear Fan 2100 and Sukhoy
             SU-29 Aircraft Wings Using Developed Probabilistic
             Software for Composite Aircraft Components
      4.5.12 Helicopter Cyclic Stick and Harness Connector Clearance
             Problem
      4.5.13 Capabilities and Applications of Probabilistic Methods
             in Finite Elements Analysis
      4.5.14 Efficient Composite Material Qualification Methods
  4.6 Probabilistic Thin Shell Structural Design for Evolved
      Expendable Launch Vehicle
      4.6.1 Introduction
      4.6.2 Structural Sizing Optimization
      4.6.3 Reliability Analysis
      4.6.4 Probability Density Function of CUS Structural Weight
      4.6.5 PDF of Manufacturing Cost
      4.6.6 Summary and Conclusions
      4.6.7 References
  4.7 Shuttle/Mir Probabilistic Docking Analysis
      4.7.1 General Description
      4.7.2 FEBREL-DOCKING Program
      4.7.3 Benefits of FEBREL-DOCKING for Shuttle/Mir Capture
             Analysis
      4.7.4 References
5 Summary

Addresses the following: 1) Captures previous experience and lessons learned in the application of PM. 2) Tabulates public-domain applications, and several representative examples discussed in detail. 3) Notes relative merits and barriers to implementation.