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)

Task I Design Information

Task II

Design Analyses & Development Testing

5.1.1

ASIP Master Plan

Design Service Life & Design Usage

5.1.2

Initial Analysis

(Loads, Mass Properties)

5.2.2, 5.2.12

Updated Analysis (Loads, Strength, Mass Properties, Spectra)

5.2.2-5.2.5, 5.2.12

Updated Analysis

(All Analyses)

5.2.2-5.2.13, 5.2.16

Structural Design Criteria

5.1.3

Initial Design

(Shape, Mold Lines)

Updated Design (Shape, Mold Lines, Sizing, Structural Layout)

Design Freeze

Durability & Damage Tolerance Control Program

5.1.4

Materials & Joint Tests

5.2.1

Design Development

Test

5.2.14

Corrosion Prevention & Control Program

5.1.5

Corrosion Assessment

5.2.8

Nondestructive

Inspection Program

5.1.6

Production NDI Capability Assessment

5.2.15

Selection of Materials, Processes, Joining Methods, & Structural Concepts

5.1.7

ASIP elements listed by number in bottom left corner of appropriate boxes.

FIGURE 2.  Aircraft Structural Integrity Program - Tasks I and II.

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