MIL-E-5272C(ASG)
13 APRIL 1959
Seperaeding
lm.lwJ5272B(usAr)
5 Jima 1957
usEDlMLIElo2
HIIJ.%5272A
16 September W2
MZLITARYSPECIFICATION
sNVIRONMSNMLTSSTING, AERONAUTICALANDAsSXIATSD
EQUUM2NT,C2NERALSPECIFICATIONFOR
This specMicatlon baa been approved by the Department
ofthe Air Force ard by tbe Navy Bureau of Aaronautlcs..
,-
1.
.%OPE
1.1 ~.-
Tbia SpeCificatfOn eSMb~Bbea gen$?~ applicable
proccdurea for testing aeronautical and c.csooiatd equipeent tier slmuhted
md accelerated cllcnatic ati mvlrohmntel
conditions. Fmecdurw pxwwribad
herein are
to be utilized in aubjeating equipment to. simulated aod .ccaclerated
envircomental conditions in order
to ineure satisfactory o~ration end to reduoe
deterioration when the equiment ia operated or atmed in w global locality.
In the eaee of any paitlcular item
ofcquirment, teet proceduroa ara to be fcl.lmmd
to the extent specified in the applicable aquipment specification.
2. APPLICAMX
DOCUUENTS
i
2.1
The following documnta, of
the iaaue in effect on date of invitation
for bids, form a part
of this specffieatiom
JAN-B-U+
Shock-Testing-Meehanicm
for Rleatridal-
Iniicating In.ctrumente (2-1/2 and 3-1/2
Inch, Round, Fluch-Uount@, Panel-TyPe)
Mm-S-w SIcxkprwf Sqa@mnt j Clam NI (Nigh Impact),
SMptoard Application, Te#ta
fcr
MIl&-u56
Shock, Variable Duration, Ihthed ard Apparatua
for
MU-C-5572 Gemline, Aviatlcn, Oradea 80/%7, 9ti96,
100/130, 115/u5
NIW3-5705 Structural Criteria, ?510ted Airplanes, Famlage,
Boome, Engine MountAand Nmallee
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