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DATA ITEM DESCRIPTION
f- 4ommd
OMB No. 0706-0186
Err). fire: MI 30.1986
!.
TITLE
2, 1DENTIF1UTION NuMBER
INTSRNALLOADSAND STATICSTRR6CTEIANALYSISRSPORT
DI-sDRQ-80198
b..?Es%P&O%$’Om&Ewes-ts the derivationof Interod lCI~S.resultiw Btressee~ strewh
:qtati~ -t ~yticdly substantiatethe stmcturcl abilityof aircraftand aircraft-
umxiad
stores to raact criticd externalloadingconditions.
ThisalsE12y6isis used to moEsi-
:orthestructuraladequacyof the designfor
meeting contractrequirements,to evaluate my
asgineerissgcbengeproposals.to seineae a baaia for wd.ificatiom. st~ctur~ reP~r. ~ta~
lishingdmnagelimits,and to evaluateany possibleincidentsor accidentsduring‘operation.
L.w#v& OATS
5.
OFFICE OF PRIMARY R6EWNSIB!UW (OPRI 6a. OTIC REOUIREO
6b, OIOEP REOLHRED
860731
ASD/SNSSS.
!.~m~-&~am~&&m~~riptim (DID)complieswith the functionaltaskgeneratedby 5.2.5
>f3E11-sTD-1530A,3.10 of KIL+-8856A, and 4.10of MIL-A-87221. ThisD~ inrludesthe f-mat
snd contentpreparationim.atructioasraqssiredby 3.8.1 of X33.-A-8868A.
~.2 Ihi.eDID is applicable
to the am.lysesof aircraft,missi3es.aircraft-carriedstores.
d f02kw—oo
.modificationprograms.
T.3 -Portionsof thisDEI are subjectto de3etionteilorfng,‘dependingupon theprogram
?&es in wbitb it is appliedin tbc solicitation
or contract.
1.AWROVAl UhUTATiEiN
9a. APPLICABLE FORMS
9b. AMSC NUMBER
F3902
O. PREPARATIONINSTRUCTIONS
10..2
Sossrcedocument. The applicableissueof the doc-ts citedhereio.includingtheir
WWOWJ
datas and datesof any applicable
mendments and revisions,sbcU be as reflectedin
be contract.
10.2 _
Format .
The 2ateraa3bads and .StaticStrength&ialysis‘&port. shall include the
FormatWICMD 3.8.1of M13.-A-8868.
10.3
content. The reportshn33presentdete.iledassa.lysesof major componentsand abbre-
tited amalysesof all eecmdcry componentsof the scructoreto demonstrate.loadparhsof
6dequatestrength.
InternalloadswiU be tabd.atedfor allmembers,
but repetitivetype
z
tmctarea may be subetmti.atedby analysisof the common
structuralmemberbavi.ssgthe
MxilF& lodfng.
10.3.1 Aircraftstructure. TIM?reportshall be subdivided,ae applicable,
to pra.cent
ma3yacc of
the followingmajoretructurd compmen
ta or
groups:
a. Wing, includingall attachmentsand actuating
structures. move.sblecosstrol
surfaces,ving— ted speedreductioodevicesand auriliaryliftdevices,enginemoudts,
d Oacdlac.
b.
~ge. imkdins CCSSOPY.fuselaw-tte~ed W -ts. ~ti-=t~
speedreductiondevices,tie-dotmstructurefor seats. litter,tcrgo.and equ.ipmantracka,
md c.U actuatingstructureand attachments.
C. ~we. imthding fixcd
horizontal and vertid surfates.nuveablesurfaces.
theixattathmcnts,and artuatingsupportstructures.
d. controlsystcsu.either manual or powered,includingcables.rodk.bel.lcranks,
~tacic parts,devices.ad act-era.
e. LCIUMSWd takeoffgear. IIXMILW =-tors and a-tits
● -~wt ~
m-resting gears, beachinggearamd a~w flOats.
u—
●cm CCmEC
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