MIL-HDBK-1530 Aircraft Structural Integrity Program, General Guidelines for S/S by MIL-STD-1530This handbook contains general guidelines for the U.S. Air Force Aircraft Structural Integrity Program ASIP. These guidelines describe the processes proven successful in the achievement of structural integrity in USAF air vehicles while the cost of ownership is minimized; and cost and schedule risks managed through a series of disciplined, time-phased tasks. This handbook is for guidance only. This handbook cannot be cited as a requirement. If it is, the contractor does not have to comply.

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MIL-HDBK-1530B(USAF)

d.    Damage tolerance and durability control process (See 5.1.3.)

e.      Selection of materials, processes, and Joining methods (See 5.1.4.)

f.       Finish specification criteria (See 5.1.5.)

g.      Design service goal and design usage (See 5.1.5.)

h.      Material and Joint allowables (See 5.2.1.)

i.       Loads analysis (See 5.2.2.)

J.       Design service loads spectra (See 5.2.3.)

k.      Design chemical/thermal environment spectra (See 5.2.4.)

l.       Stress analysis (See 5.2.5.)

m.     Damage tolerance analysis (See 5.2.6.)

n.      Durability analysis (See 5.2.7.)

o.      Aeroacoustic durability analysis (See 5.2.8.)

p.      Vibration analysis (See 5.2.9.)

q.      Flutter analysis (See 5.2.10.)

r.       Nuclear weapons effects analyses (See 5.2.12.)

s.      Nonnuclear weapons effects analysis (See 5.2.13.)

t.       Static tests (See 5.3.1.)

u.      Durability tests (See 5.3.2.)

v.      Damage tolerance tests (See 5.3.3.)

w.     Flight and ground operations tests (See 5.3.4.)

x.      Aeroacoustic durability tests (See 5.3.5.)

y.      Flight vibration tests (See 5.3.6.)

z.      Flutter tests (see 5.3.7.)

aa.    Strength summary (See 5.4.2.)

bb.    Force structural maintenance plan (See 5.4.3.)

cc.    Loads/environment spectra survey (See 5.4.4.)

dd.    Individual air vehicle tracking program (See 5.4.5.)

ee.    Loads/environment spectra survey (See 5.5.1.)

ff.     Individual air vehicle tracking data (See 5.5.2.)

gg.    Individual air vehicle maintenance times (See 5.5.3.)

hh.    Structural maintenance records (See 5.5.4.)

ii.      Mass Properties Control and Management Process (MPCMP) data (See 5.2.11.) JJ.      Weight and Balance data for Air Vehicles (See 5.2.11 and 5.3.8.)

kk.    Sample Charts A and E data (See 5.5.5.)

ll.      Analytical Condition Inspection (ACI) results (See AFMCI 21-102.)

6.4   Subject term (key word) listing.

aeroacoustics aging aircraft airframe

ASIP

battle damage corrosion cracking

damage tolerance durability

fatigue flutter loads

maintenance mass

NDT/I

off-the-shelf aircraft

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