MIL-PRF-22710H
4.5.5.2 Operating force (applicable to switch modules or stacked switch modules, see 3.8.2). Thumbwheel
switches shall be tested by applying the specified force (see 3.1 and 6.1) tangentially to the thumbwheel of the
switch, parallel to the mounting surface.
4.5.6 Stops (when applicable, see 3.1 and 6.1) (see 3.9). Switches shall be tested in accordance with 4.5.6.1 as
applicable.
4.5.6.1 Thumbwheel switches. Unless otherwise specified (see 3.1 and 6.2.2), a tangential force of 15 pounds ±1
pound shall be applied first in an upward direction, then in a downward direction.
4.5.7 Thermal shock (see 3.10). Switches shall be tested in accordance with method 107 of MIL-STD-202. The
following details shall apply:
a. Test-condition letter:
A: For switches with temperature-life characteristic letter B and letter C.
B: For switches with temperature-life characteristic letter A and letter D.
b. Measurements before and after cycling: Not applicable.
After the test, switches shall be examined for mechanical and electrical damage, loosening of rivets, and other
fastening devices.
4.5.8 Terminal strength (applicable to switches having solder-type terminals, see 3.1 and 6.2.2) (see 3.11). Where
the circuit configuration permits, the following minimum number of terminals shall be tested:
a. Three terminals per section, one section per switch for multisection switches.
b. Four terminals for single-section switches.
Two of the terminals shall be adjacent at minimum spacing and located on opposite sides of a throughbolt, if used,
where the circuit configuration permits.
4.5.8.1 Pull (see 3.11.1).
4.5.8.1.1 Terminals (except flexible wire leads). Unless otherwise specified (see 3.1 and 6.2.2), a force of 15
pounds ±1 pound shall be applied to the terminals at the normal location for attaching lead wires. The pull force shall
be gradually applied to each terminal and maintained for 15 seconds minimum in each of three mutually
perpendicular directions as follows:
a. In a direction parallel to the plane of the section and perpendicular to the longitudinal axis of the terminal.
b. In a direction along the longitudinal axis of the terminal.
c. Perpendicular to the plane of the section in a direction in which there is minimum support provided by the
insulation.
4.5.8.1.2 Terminals (flexible wire leads). The pull test shall be the same as 4.5.8.1.1, except pull force shall be as
specified (see 3.1).
4.5.8.2 Bend (when applicable, see 3.11.2). Terminals bent permanently out of position as a result of the pull test
(see 4.5.8.1), shall be tested in accordance with method 211 of MIL-STD-202. The following details and exception
shall apply:
a. Test-condition letter: B.
b. Number of bends: Two.
c. Direction of applied force: Perpendicular to the plane of the section in a direction in which there is minimum
support provided by the insulation.
After this test, switches shall be examined for evidence of breakage of terminals and visible cracks in either the
terminals or the insulating material.
16
For Parts Inquires call Parts Hangar, Inc (727) 493-0744
© Copyright 2015 Integrated Publishing, Inc.
A Service Disabled Veteran Owned Small Business