scope:

Use/Relationship:

The Aircraft External Loads Analysis Report is used to obtain data that establishes, in detail, the magnitude and distributions of all applied and induced external loads which the aircraft structure may encounter when operated within the design envelope established by the structural design criteria.

a. This report is applicable to all programs as described in MIL-STD-1530, Aircraft Structural Integrity Program (ASIP). MIL-STD-1530 is applicable to all aircraft the United States Air Force (USAF) acquires, uses, or leases.

b. This Data Item Description (DID) contains the format, content, and intended use information for the data deliverable resulting from the work task described in the solicitation.

c. This DID interfaces with DI-SESS-82122, Structural Design Criteria (SDC) Report (Aircraft).

d. This DID supersedes canceled DI-S-30588.