MIL-STD-1530 Aircraft Structural Integrity Program AsipThis standard describes the USAF Aircraft Structural Integrity Program ASIP which defines the requirements necessary to achieve structural integrity in USAF aircraft while managing cost and schedule risks through a series of disciplined, time-phased tasks. It provides direction to government personnel and contractors engaged in the development, production, modification, acquisition, and/or sustainment of USAF aircraft.

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MIL-STD-1530C(USAF)

FOREWORD

1. This standard is approved for use by the Department of the Air Force and is available for use by all Departments and Agencies of the Department of Defense.

2. This standard implements Air Force Policy Directive (AFPD) 63-10, Aircraft Structural Integrity; and Air Force Instruction (AFI) 63-1001, Aircraft Structural Integrity Program. These two documents define policies, procedures, and responsibilities that ensure the safe operation of USAF aircraft. The requirements of these two documents are not repeated in higher-level policy (e.g., DoD-5000 Series documents) and have no commercial equivalent (e.g., Federal Aviation Administration [FAA] regulations).

3. Comments, suggestions, or questions on this document should be addressed to: ASC/ENOI, 2530

LOOP ROAD WEST, WRIGHT-PATTERSON AFB OH 45433-7101; or e-mailed to Engineering.Standards@wpafb.af.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST online database at https://assist.daps.dla.mil .