533305-8 TE Connectivity, 533305-8 Datasheet - Page 3

• Manufacturer Part Number: 533305-8
• Manufacturer: TE Connectivity

Specifications of 533305-8

• Product Line: AMP ECONOMATE
• Product Type: Contact
• Number Of Dual Positions: 35
• Post Type: Compliant Post
• Proprietary Name: AMP ECONOMATE
• Termination Post Length (mm [in]): 12.70 [0.500]
• Centerline (mm [in]): 2.54 [0.100]
• Contact Type: Socket
• Contact Plating, Mating Area, Material: Gold (50)
• Contact Base Material: Beryllium Copper
• Rohs/elv Compliance: Not reviewed for ELV/RoHS compliance
• Lead Free Solder Processes: Not reviewed for lead free solder process
• Packaging Method: Combs

Durability.
Engaging force.
Separating force.
Contact retention.
Torque.
Pin shield retention.
Therm al shock.
Salt spray.
Rev E
Test Description
See Note.
10 ounces m axim um average per
contact.
1 ounce m inim um average per
contact.
Contacts shall not dislodge when a
m inim um axial force of 15 pounds
for soldered contacts and 7 pounds
for press-fit contacts is applied in
either direction.
Contacts shall not dislodge when a
m axim um force of 3 inch-ounces is
applied in both directions.
Pin shield shall not separate from
the housing nor exhibit dam age or
defects that would im pair norm al
function when a m axim um force of
4 pounds is applied to each end of
each pin shield.
See Note.
See Note.
Figure 1 (continued)
ENVIRONMENTAL
Requirem ent
Mate and unm ate specim ens with a
corresponding blade header
assem bly for 100 cycles at a
m axim um rate of 10 cycles per
m inute.
Measure force required to m ate
specim ens with a corresponding
blade header assem bly.
Measure force required to withdraw
a m inim um size gage from each
individual contact.
See Figure 4.
Apply specified axial load to contact
posts in a direction toward the
connector and hold for 5 to 10
seconds.
Apply specified force to the base of
each contact post in both clockwise
and counterclockwise directions
and hold for 5 to 15 seconds.
MIL-C-28754, paragraph 4.9.6.
Apply specified force in a direction
norm al to a plane passing through
the center line of both keying pins
m idway between the first and
second cavities and .062 +.000/-
.031 inch from the bottom edge of
the shield.
See Figure 5.
MIL-STD-202, Method 107, Test
Condition A.
Subject specim ens to 5 cycles
between -55 and 105 C.
MIL-STD-202, Method 101, Test
Condition B.
Subject specim ens to 5% salt spray
solution for 48 hours. After
exposure, specim ens shall be
thoroughly washed using tap water
and dried at 100 F for 24 hours
before proceeding with additional
testing.
Procedure
108-12057
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