THROUGH-HOLE SOLDERING MECHANICAL ASSEMBLY, SWAGED TERMINALS | |
Terminals are generally restricted to applications requiring components to be routinely removed and replaced, such as in high-gain analog tuning circuits. The installation of terminals increases the vertical profile of the printed wiring assembly (PWA) significantly, requiring the designer to ensure minimum electrical spacing requirements are not violated. |
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PREFERRED BIFURCATED TERMINAL The terminal is properly set, aligned and straight. Tines are straight. No exposed base metal. Flange is swaged sufficiently tight to prevent Z-axis movement, while allowing finger force twisting for adjustment. No damage to the PWB. |
PREFERRED ELLIPTICAL FUNNEL SWAGE The flange is uniformly shaped and concentric to the hole or termination pad. Strain/Stress marks are minimum, no splits or cracks. Flange is swaged sufficiently tight to prevent Z-axis movement, while allowing finger force twisting for adjustment. No damage to the PWB. |
PREFERRED ROLL FLANGE SWAGE The flange is uniformly rolled and concentric to the hole or termination pad. Strain/Stress marks are minimum, no splits or cracks. Flange is swaged sufficiently tight to prevent Z-axis movement, while allowing finger force twisting for adjustment. No damage to the PWB. |
PREFERRED TURRET TERMINAL The terminal is properly set and straight. No exposed base metal. Flange is swaged sufficiently tight to prevent Z-axis movement, while allowing finger force twisting for adjustment. No damage to the PWB. |
NASA WORKMANSHIP STANDARDS | |||
Released: 06.27.2002 |
Revision: |
Revision
Date: |
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Book: 6 |
Section: 6.05 |
Page: 1 |
THROUGH-HOLE SOLDERING MECHANICAL ASSEMBLY, SWAGED TERMINALS (cont.) | |
PREFERRED V-FUNNEL FLANGE The flange is uniformly swaged and concentric to the hole/pad, and is sufficiently tight to prevent Z-axis movement, while allowing finger force twisting for adjustment. Minimum stress marks, no splits or cracks. No damage to the PWB. |
MANDATORY ADJUSTABILITY Terminals shall be swaged such that they can be rotated (twisted) under finger force. NASA-STD-8739.3 [8.2.4] |
MANDATORY COMPONENT SIDE TERMINATION Swage type terminals in non-PTH's, designed to have the terminal shoulder soldered to the printed wiring conductor, shall be secured to the PWB by a roll swage. NASA-STD-8739.3 [8.2.2] |
ACCEPTABLE PLATED-THROUGH HOLE (PTH) TERM. Terminals mounted in plated-through holes (PTH) shall be secured with a V-funnel or elliptical funnel swage. The elliptical funnel is preferred. NASA-STD-8739.3 [8.2.4] |
MANDATORY PLATING Terminals shall be copper, hot dipped, tin-lead coated or hot reflowed, electrodeposited tin-lead solder. Finish shall be smooth and shiny. NASA-STD-8739.3 [9.1.12] |
UNACCEPTABLE PLATING DEFECTS Flaking or peeling plating shall be grounds for rejection. Best Workmanship Practice |
NASA WORKMANSHIP STANDARDS | |||
Released: 06.27.2002 |
Revision: |
Revision
Date: |
|
Book: 6 |
Section: 6.05 |
Page: 2 |
THROUGH-HOLE SOLDERING MECHANICAL ASSEMBLY, SWAGED TERMINALS (cont.) | |
MANDATORY SOLDER SIDE TERMINATION Designs calling for soldering of the swaged end of the terminal to the printed wiring conductor on a single-sided PWB shall be secured with a V-funnel swage. NASA-STD-8739.3 [8.2.3] |
UNACCEPTABLE IMPROPER SWAGE USED Designs calling for soldering of the swaged end of the terminal to the printed wiring conductor on a single-sided PWB shall be secured with a V-funnel swage. NASA-STD-8739.3 [13.6.2.a.14] |
ACCEPTABLE SWAGE SETTING The terminal shall be swaged sufficiently tight to prevent Z-axis movement, while allowing finger force twisting for adjustment. Swaging shall not damage the PWB or the termination pad. NASA-STD-8739.3 [8.2.1.a] |
ACCEPTABLE SMOOTH IMPRESSION MARKS Smooth impression marks (base metal not exposed) resulting from tool holding forces shall not be cause for rejection. NASA-STD-8739.3 [7.2.3] |
ACCEPTABLE RADIAL ALIGNMENT The terminal is slightly twisted out of radial alignment, but the alignment will not adversely affect component installation or strain relief. Best Workmanship Practice |
UNACCEPTABLE IMPROPER ALIGNMENT Bifurcated terminals shall be aligned to allow the proper termination of leads or conductors. Best Workmanship Practice |
NASA WORKMANSHIP STANDARDS | |||
Released: 06.27.2002 |
Revision: |
Revision
Date: |
|
Book: 6 |
Section: 6.05 |
Page: 3 |
THROUGH-HOLE SOLDERING MECHANICAL ASSEMBLY, SWAGED TERMINALS (cont.) | |
ACCEPTABLE RADIAL SPLITS/CRACKS The rolled area or flange may have a maximum of 3 radial splits or cracks, which are separated by at least 90°, and/or which do not extend beyond the coiled or flared area. NASA-STD-8739.3 [8.2.1.b] |
UNACCEPTABLE RADIAL SPLITS/CRACKS The rolled area or flange shall not have more than 3 radial splits or cracks, which are separated by less than 90°, and/or which extend beyond the coiled or flared area. NASA-STD-8739.3 [8.2.1.b], [13.6.2.a.14] |
ACCEPTABLE VERTICAL MISALIGNMENT The terminal is slightly bent, but the top edge does not extend beyond the base, and alignment will not violate minimum electrical clearance. Best Workmanship Practice |
UNACCEPTABLE CIRCUMFERENTIAL SPLITS/CRACKS After swaging or flaring, the rolled area or flange shall be free of circumferential splits or cracks. NASA-STD-8739.3 [8.2.1.b], [13.6.2.a.14] |
UNACCEPTABLE IMPROPER SWAGE USED Roll swages shall not be used on plated-through holes. NASA-STD-8739.3 [8.2.2] |
UNACCEPTABLE INCOMPLETE SWAGE The flange shall be swaged sufficiently tight to prevent movement in the Z-axis. Best Workmanship Practice |
NASA WORKMANSHIP STANDARDS | |||
Released: 06.27.2002 |
Revision: |
Revision
Date: |
|
Book: 6 |
Section: 6.05 |
Page: 4 |
THROUGH-HOLE SOLDERING MECHANICAL ASSEMBLY, SWAGED TERMINALS (cont.) | |
UNACCEPTABLE INTERFACIAL CONNECTIONS Terminals shall not be used as interfacial connections in non-plated through holes. NASA-STD-8739.3 [8.2.1.a], [13.6.2.a.14] |
UNACCEPTABLE MODIFICATIONS Terminals shall not be modified to accommodate improper conductor sizes. NASA-STD-8739.3 [7.3.2], [13.6.2.a.19] |
UNACCEPTABLE NONCONCENTRIC SWAGE The swage shall be set approximately concentric to the hole and/or termination pad. Best Workmanship Practice |
UNACCEPTABLE PWB DAMAGE The terminal has been swaged to the point that the substrate has been fractured and glass fiber is exposed. NASA-STD-8739.3 [8.2.1.a] |
UNACCEPTABLE TERMINAL DAMAGE Terminals exhibitng physical damage (i.e.: nicks, gouging, bent/missing tines, reduced cross-section, etc.) shall be rejected. Best Workmanship Practice |
NASA WORKMANSHIP STANDARDS | |||
Released: 06.27.2002 |
Revision: |
Revision
Date: |
|
Book: 6 |
Section: 6.05 |
Page: 5 |
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