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)

engineering, manufacturing, quality assurance, and others involved in the design, engineering development, and production of the aircraft structure.  The board's decisions are subject to USAF approval.

5.1.4.2    Critical part/process selection and controls.

Criteria shall be established to select aircraft structural critical parts/processes and the controls for these critical parts/processes.  The DDTCB described in 5.1.4.1 shall oversee this selection and control process. The impact on safety-of-flight, mission completion, and production and maintenance costs shall be considered in the selection of critical parts/processes.  Figure 1, along with the analyses described in 5.2, shall be part of the selection process and establishment of controls.  The DDTCB shall ensure the critical part/process list is updated as the design matures.

Structural Design

& Analysis

Could

Failure Cause Loss

of Aircraft or Aircrew or Inadvertent Store Release?

Yes (Safety-of-Flight)                     No (Not Safety-of-Flight)

Yes

Single Load

Path?

Yes

No

Sized

Degrade Mission or Increase Vulnerability ?

No

Sized by         No

by Durability or Damage

Tolerance?

No

Yes

Durability?

Yes

Requires               No

Special

Emphasis?

No          Economical

To Repair or

Replace?

FIGURE 1.  Critical part selection flow chart.

5.1.5    Corrosion Prevention and Control Program (CPCP).

A Corrosion Prevention and Control Program shall be established for the aircraft structure.  The program shall establish a Corrosion Prevention Advisory Board (CPAB) responsible for establishment and oversight of the execution of the program.  The board shall be comprised of representatives from engineering, manufacturing, quality assurance, and others involved in the design, engineering development, and production of the aircraft structure. The board's decisions are subject to USAF approval.  Corrosion prevention shall be a primary consideration in the development and implementation of the durability and damage tolerance control process and the force management process.  Materials and processes, finishes, coatings, and films which have been proven in service or by comparative testing in

the laboratory shall be selected to prevent corrosion as described by the Corrosion Prevention and Control

Plan described in 5.1.5.1.  Results of the susceptibility to corrosion evaluation described in 5.1.5.2 shall be used to control the impact of corrosion damage.  Corrosion prevention and control guidelines are provided in JSSG-2006, the DoD Corrosion Prevention and Control Planning Guidebook (Spiral II), MIL-HDBK-1568, DFARS 207.105(b)(13)(ii) Oct 04, AFPD 21-1, and AFI 21-105.

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