JSGS-87231 Revision A:1995

1 SCOPE
  1.1 Structure
  1.2 Handbook
  1.3 Deviations
  1.4 Environmental impact statement
2 APPLICABLE DOCUMENTS
  2.1 General
  2.2 Government documents
  2.3 Non-Government publications
  2.4 Order of precedence
  2.5 Streamlining
3 REQUIREMENTS
  3.1 Design
  3.2 Performance and operability
  3.3 Environmental conditions
  3.4 Integrity
  3.5 Reliability and maintainability
  3.6 Combat survivability
  3.7 Subsystems
  3.8 Software resources
  3.9 Engine system controls and externals (C&E) evaluation
  3.10 Engine qualification
4 EVALUATION AND QUALIFICATION
  4.1 Design (configuration) and construction
  4.2 Performance and operability
  4.3 Environmental conditions
  4.4 Integrity
  4.5 Reliability and maintainability (R&M)
  4.6 Combat survivability
  4.7 Subsystems
  4.8 Software resources
  4.9 Engine system controls and external (C&E) evaluation
  4.10 Engine qualification
5 PACKAGING
  5.1 Preparation for storage and shipment
6 NOTES
  6.1 Intended use
  6.2 Acquisition requirements
  6.3 Consideration of data requirements
  6.4 Definitions
  6.5 Symbols, subscripts, abbreviations and acronyms
  6.6 Material safety data sheets
  6.7 Subject term (key word) listing
  6.8 Metrication
  6.9 Responsible engineering office
  6.10 Streamlining
  6.11 Spec tree
  6.12 Tables and figures
  6.13 Changes from previous issue
APPENDIX A - ENGINES, AIRCRAFT, TURBINE, HANDBOOK FOR

Describes establishes the item definition, performance, operating characteristics, reliability, maintainability, subsystems, physical characteristics, general design, installation, and interface requirements for manned aircraft gas turbine engines.

This specification establishes the item definition, performance, operating characteristics, reliability, maintainability, subsystems, physical characteristics, general design, installation, and interface requirements for manned aircraft gas turbine engines. This specification also establishes the analysis, inspections, demonstrations, and test procedures required by the Using Service for satisfactory completion and acceptance, of engine qualification Milestones IFR, FFR, ISR, and OCR for aircraft gas turbine engines. This specification also establishes the content and format to be used by the Using Service and/or contractor for the preparation of the acquisition and/or model specifications.