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MIL-STD-3024 w/CHANGE 1 13 July 2015 SUPERSEDING MIL-STD-3024 15 April 2008 DEPARTMENT OF DEFENSE STANDARD PRACTICE PROPULSION SYSTEM INTEGRITY PROGRAM (PSIP) AMSC N/A AREA SESS DISTRIBUTION STATEMENT A. Approved for public release: distribution is unlimited. NOT MEASUREMENT SENSITIVE Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:53Z Check the source to verify that this is the current version before use. MIL-STD-3024 w/CHANGE 1 ii FOREWORD 1. This standard is approved for use by all Departments and Agencies of the Department of Defense. 2. The Department of Defense (DoD) is committed to ensuring a strong systems engineering approach in acquisition programs. This standard covers the procedures to be used to ensure propulsion system integrity during the Engineering and Manufact
ncy of this address information using the ASSIST Online database at https://assist.dla.mil. Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:53Z Check the source to verify that this is the current version before use. MIL-STD-3024 w/CHANGE 1 iii SUMMARY OF CHANGE 1 MODIFICATIONS 1. Changed the Uniform Resource Locator (URL) for the Acquisition Streamlining and Standardization Information System (ASSIST) database throughout the document 2. Updated source information for references in Sections 2 of the document 3. Updated acronym list 4. Updated Appendix A for Technical Review criteria. 5. Updated Review Activities in Concluding Material 6. Modifications have been made to MIL-STD-3024, as follow, to: a. Address airworthiness issues raised by recent developmental programs, b. Resolv
base requirements established. Initial material characterization plan issued. Material characteristics assessed based on design analysis and the potential impact of manufacturing processes changes. Component designs reflect accommodation of requirements. Material characteristics assessed based on design analysis and the potential impact of manufacturing processes changes. Material characterization complete. Source: https://assist.dla.mil -- Downloaded: 2026-07-20T01:53Z Check the source to verify that this is the current version before use. MIL-STD-3024 w/CHANGE 1 APPENDIX A 43 TABLE A-II. Engine Structures Task Completion Criteria - Continued. Program Milestone A B C Acquisition Phase Technology Development Engineering and Manufacturing Development Production and Deployment Operations an
Glossary of Definitions, Ground Rules, and Mission Profiles to Define Air Vehicle Performance Capability MIL-STD-3022 Documentation of Verification, Validation, and Accreditation (VV&A) for Models and Simulations MIL-STD-3024 Propulsion System Integrity Program (PSIP) MIL-STD-3050 Aircrew Breathing Systems (ACBS) MIL-STD-3063 Rotorcraft Structural Integrity Program (RSIP) MIL-STD-7080 Selection and Installation of Aircraft Electric Equipment MIL-STD-8591 Airborne Stores, Suspension Equipment and Aircraft-Store Interface (Carriage Phase) MIL-STD-38784 General Style and Format Requirements for Technical Manuals MIL-STD-40051 Preparation of Digital Technical Information for Technical Manuals (TMs) (Copies of these documents are available online at https://quicksearch.dla.mil). DEPARTMENT OF
ing, Military Flight Operations Quality Assurance, etc.) with the mandatory crash survivable recorder requirement when identifying an aircraft flight data parameter recording, storage, and transmission capability. DAFI20-101_ 63-101 16 FEBRUARY 2024 81 5.4.1.2. Product and System Integrity. For each Aircraft Mission Design Series, the DAF acquires, uses, or leases, the PM establishes integrity programs. 5.4.1.2.1. The PM develops, documents, and executes integrity programs by applying DAFI 63-140, and tailoring and integrating to the extent practicable: MIL-STD-1530D, Aircraft Structural Integrity Program (ASIP); MIL-STD-1796, Avionics Integrity Program (AVIP); MIL-STD-1798C, Mechanical Equipment and Subsystems Integrity Program; MIL-STD-3024, Propulsion System Integrity Program; and MIL-H
e recorder requirement when identifying an aircraft flight data parameter recording, storage, and transmission capability. 5.4.1.2. Product and System Integrity. For each Aircraft Mission Design Series, the DAF acquires, uses, or leases, the PM establishes integrity programs. 5.4.1.2.1. The PM develops, documents, and executes integrity programs by applying DAFI 63-140, and tailoring and integrating to the extent practicable: MIL-STD-1530D, Aircraft Structural Integrity Program (ASIP); MIL-STD-1796, Avionics Integrity Program (AVIP); MIL-STD-1798C, Mechanical Equipment and Subsystems Integrity Program; MIL-STD-3024, Propulsion System Integrity Program; and MIL-HDBK- 513, Low Observable Integrity Program. 5.4.1.2.2. PMs integrate corrosion prevention and control into the Mission Design Seri
rogram consistent with MIL-STD-3024, Propulsion System Integrity Program (PSIP). 7.3.2.3. Operational Usage and Verification. Periodic verification events (mission usage surveys, LtF/ACI engine teardowns, Accelerated Mission Tests, inspections, etc.) will provide data needed to ensure engine components reach mature life limits, while retaining required performance characteristics and provide inputs into the CIP, maintenance program, spares requirements, modification programs, and Science & Technology programs. Data gathered from these programs is used to establish program priorities and develop execution and out year budget requirements. 7.3.2.4. Condition Based Maintenance Plus (CBM+) (how it will be achieved). 7.3.2.4.1. Operational readiness through affordable, integrated, off-board and
T-2) 4.7.2. Prognostics and Health Management (PHM) and CBM+ programs must be based on RCM analysis, readiness requirements, and life-cycle cost goals. DoDI 4151.22, Condition-Based Maintenance Plus (CBM+) for Materiel Maintenance, directs implementation of RCM and establishes RCM as a key enabler of CBM+. (T-2) 4.8. AF RCM engine guidance resides in AFMAN 20-116, Propulsion Life Cycle Management for Aerial Vehicles. 4.9. MIL-STD-3024, Propulsion System Integrity Program (PSIP), cites AFMCI 21-103. 4.10. AFMAN 63-143, Centralized Asset Management Procedures, establishes maintenance requirements based on RCM. 4.11. TO 00-20-1, Technical Manual, Aerospace Equipment Maintenance Inspection, Documentation, Policies, and Procedures, establishes that changes to inspections intervals, concepts or
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