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|  MIL-A-23622
.
- The actuator shall be tested in accordance
Salt
4.6.12
with procedure I, Specification MIL-E-5272. Within one hour after compli-
ance with this test procedure$ the actuator shall be subject to the moni-
tored operational check (4.6.2.2) and shall meet the requirements specified
therein. There shall be no corrosion or other defect that affects the
.
operation or structural strength of any load carrying part.
dust - The actuator shall be tested in accord-
4,6.13
ance with Procedure II, Specification MIL-E-5272 for a period of 24 hours.
Immediately after completion of this test, the actuator shall be removed
from the chamber and subject to the monitored operational check (4,6.2.2)
and shall meet the requirements specified therein. Accumulated sand or
dust within the actuator shall have no detrimental effects upon its opera-
tion and shall not be allowed in locations where excessive wear or failure
might result. There shall be no damage to the exterior protective finishes.
Reliabilitv - The actuator shall be subject to 10,000
4.6,14
full stroke cycles at the-rated load, duty cycle, and voltage and at
maximum altitude and standard temperature. Load shall average not less
than the rated load, whether or not it is applied uniformly, and shall
change direction so as to oppose the actuating force throughout both the
extend and retract strokes. There shall be no failure to operate during
this test. There shall be no replacement of' parts during this test. At
the conclusion of this test, the actuator shall be subject to the monitored
operational check (4.6.2.2) and shall meet the requirements thereof.
Interference - The actuator shall be tested in accordance
4.6,15
with specification MIL-I-6181. Interference limits shall be within those
specified up to 150mc only.
Explosion proof - The actuator shall meet the require-
4.6.16
ments for explosion testing, "specified in Specification MIL-E-5272, pro-
cedure III.
Ultimate load - When specified in Table I, the actuator
4.6.17
shall be subject to an ultimate static load of 150 percent of the static
limit load. The actuator may be permanently deformed and it may become
inoperative, but it shall not have any structural failure as a result of
this test.
PREPARATION FOR DELIVERY
5'
Preservation and packaging - The actuators shall be
5.1
unit packaged in accordance with Specification MIL-P-7936, levels A or C
as specified. (see 6.2)
10
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