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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M1L-STD-1530C(USAF)

TABLE 11. USAF AS1P Tasks and elements aligned with U.S. Department of Defense acquisition events - Continued.

111 • Full•Scale Testing	5.3.1 Static Tests					INITIAL	CONTINUE
	5.3.2. First Flight Verification Ground Tests					FINAL
	5.3.3 Flight Tests						FINAL
	5.3.4 Durability Tests						FINAL
	5.3.5 Damage Tolerance Tests						FINAL
	5.3.6 Climatic Tests						FINAL
	5.3.7 Interpretation & Evaluation of Test Results						FINAL
1V • Certification & Force Management Development	5.4.1 Certification Analyses						FINAL
	5.4.2 Strength Summary & Operating Restrictions (SSOR)							FINAL
	5.4.3 Force Structural Maintenance Plan (FSMP)							FINAL
	5.4.4 Loads/ Environment Spectra Survey (L/ESS) Development							FINAL
	5.4.5 Individual Aircraft Tracking (IAT) Program Development							FINAL
	5.4.6 Rotorcraft Dynamic Component Tracking (RDCT) Program Development							FINAL
V • Force Management	5.5.1 Individual Aircraft Tracking (IAT) Program									EXECUTE
	5.5.2 Rotorcraft Dynamic Component Tracking (RDCT) Program									EXECUTE
	5.5.3 Loads/Environment Spectra Survey (L/ESS)									EXECUTE
	5.5.4 ASIP Manual									CREATE/MAINTAIN
	5.5.5 Aircraft Structural Records									CREATE/MAINTAIN
	5.5.6 Force Management Updates									UPDATE
	5.5.7 Recertification									CREATE/UPDATE
	REVIEWS & AUDITS >>> (per MIL-STD-1521)	SRR	SDR [SFR]	PDR	CDR	TRR	FCA [SVR]	PRR	PCA
	ACQUISITION PHASES >>>	Tech Development	System Development & Demonstration						Production & Deployment	Operations & Support
	MILESTONES >>>	A	B						C