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)

y.       First flight verification ground tests (See 5.3.2.)

z.       Flight tests (See 5.3.3.)

aa.     Durability tests (See 5.3.4.)

bb.     Damage tolerance tests (See 5.3.5.)

cc.     Climatic tests (See 5.3.6.)

dd.     Interpretation and evaluation of test results (See 5.3.7.)

ee.     Certification analyses (See 5.4.1.)

ff.      Strength Summary & Operating Restrictions (SSOR) (See 5.4.2.) gg.     Force Structural Maintenance Plan (FSMP) (See 5.4.3 and 5.5.6.) hh.     Loads/Environment Spectra Survey (L/ESS) (See 5.4.4 and 5.5.3.) ii.       Individual Aircraft Tracking (IAT) Program (See 5.4.5 and 5.5.1.)

JJ.       Rotorcraft Dynamic Component Tracking (RDCT) Program (See 5.4.6 and 5.5.2.)

kk.     Aircraft structural records (See 5.5.5.)

ll.       ASIP Manual (See 5.5.4.)

mm.   Probability of failure limits (See 5.5.6.3.)

nn.     Recertification (See 5.5.7.)

6.4    Subject term (key word) listing.

aeroacoustics aircraft structure corrosion cracking

damage tolerance durability economic life fatigue

flight test flutter

force management ground test

loads mass

nondestructive inspection (NDI)

probability of failure proof test

risk

service life static test strength sustainment vibration

weight and balance widespread fatigue damage

6.5    Changes from previous issue.

Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes.

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