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SEMI G50-89 © SEMI 1989 4 10.3 Destructive Die Shear Testing — S hall be perform ed per Method 2019 of MIL-STD- 883. 10.4 W ire Bond Pill Testing — Sha l l be performed per Method 2011, C o ndition D of MI L-STD-883. 10.…

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SEMI G50-89 © SEMI 19893
Bottom surface — 0.051 mm (0.002"), maximum
Edges — 0.152 mm (0.006"), maximum
Terminal pads — 0.051 mm (0.002"), maximum
Wire bond fingers — 0.025 mm (0.001"), maximum
Die attach surface — 0.025 mm (0.001"), maximum
8.4 Camber — 0.004" inch/inch (mm/mm), maximum.
For dimensions less than 10.05 mm (0.750"), 0.127 mm
(0.003") camber is permitted along any planar
dimension of the device package.
8.5 Seal Area FlatnessThe seal area shall be flat
within the limits listed in Table l.
8.6 Die Attach Surface FlatnessThe die attach
surface shall be flat within the limits listed in Table 2.
Table 1 Seal Ring Flatness Limits
Seal Ring OD Ring Flatness
0–0.250" (0–6.35 mm) 0.002" max. (0.051 mm)
0.251"–0.550" (6.37–13.97 mm) 0.003" max. (0.076 mm)
0.501"–1.000" (12.7–25.40 mm) 0.004" max. (0.101 mm)
> 1.000" (> 25.40 mm) 0.004"/inch (0.101 mm/mm)
Table 2 Die Attach Area Flatness Limits
Die Attach Pad Dimension TIR Flatness
0–0.500" (0–12.7 mm) 0.002" max. (0.051 mm)
0.501"–0.750" (12.7–19.5 mm) 0.003" max. (0.076 mm)
8.7 Voids
8.7.1 Seal Area Void — A maximum of three voids
permitted. Not more than two voids per side of 0.010"
diameter. Any two voids must be separated by 0.762
mm (0.010") minimum, not to degrade the seal width
by more than 25%.
8.7.2 Terminal Void — A maximum of two voids per
terminal pad permissible. Maximum void diameter
acceptable is 0.127 mm (0.005"). Voids may never
reduce the minimum terminal width to less than two-
thirds of the nominal design dimension.
8.7.3 Wire Bond Finger Void — Void free 0.015"
back from the bond finger tip.
8.7.4 Die Attach Surface Voids — Three voids of
0.010" diameter are the maximum allowed separated by
0.030" minimum.
NOTE: Voids within 0.015" of the cavity wall not included.
8.7.5 Internal Metallization Voids Voids in internal
metallization planes or traces shall not break continuity.
Specific requirements for resistance and capacitance
parameters shall be specified in the purchase order, if
applicable.
8.8 Pattern Metallizations
8.8.1 Seal Plane Rundown (internal cavity) — Not to
exceed 25% of the cavity layer thickness.
8.8.2 Seal Plane Rundown (external to cavity) — Not
to exceed half the nominal design distance to adjacent
edge metallization. In no event shall the rundown be
closer than 0.254 mm (0.010") to any edge
metalization.
8.8.3 Wire Bond Rundown — Wire bond finger
rundown shall not exceed 25% of the cavity depth or
0.127 mm (0.005"), whichever is smaller.
8.8.4 Wire Bond Finger PullbackWire bond finger
pullback shall not exceed 0.127 mm (0.005") from the
nominal design dimension for finger end to cavity edge.
8.8.5 Seal Plane Pullback — Seal plane pullback shall
not exceed 0.127 mm (0.005") from the nominal design
dimension for seal plane metallization to edge.
8.9 Lead Attachment (when applicable)
8.9.1 Voids in Braze — Braze fillets must be 95% free
of voids.
8.9.2 Lead Alignment — Brazed leads shall not
overhang braze pads.
8.9.3 Lead Offset — Lead centerlines must be aligned
to within 0.0762 mm (0.003") of the centerlines of
corresponding braze pad metallizations.
8.9.4 Lead-to-Lead MisalignmentNot to exceed
10% of nominal spacing.
8.9.5 Dimensional Criteria — Per JEDEC JC-11
registered outline drawings in JEDEC Publication 95,
or as specified on the user drawings.
9 Sampling
Sample sizes must meet requirements of MIL-STD-105
or MIL-M-38510 as agreed to between vendor and
customer.
10 Test Methods (Mechanical, Electrical, and
Thermal)
10.1 Gold Plating Thickness — Shall conform to
MIL-G-45204. Gold thickness may be determined
using the Beta Backscatter Radiation Method or x-ray
fluorescence.
10.2 Nickel Plating — Shall conform to QQ-N-290.
Nickel thickness may be determined using the Beta
Backscatter Radiation Method or x-ray fluorescence.
SEMI G50-89 © SEMI 1989 4
10.3 Destructive Die Shear Testing Shall be
performed per Method 2019 of MIL-STD-883.
10.4 Wire Bond Pill Testing — Shall be performed per
Method 2011, Condition D of MIL-STD-883.
10.5 Temperature Cycling TestingShall be
performed per Method 1010, Condition C of MIL-STD-
883.
10.6 Thermal Shock Testing — Shall be performed per
Method 1011, Condition C of MIL-STD-883.
10.7 Constant Acceleration Testing Shall be
performed per Method 2001, Condition E, Y axis only,
of MIL-STD-883.
10.8 Mechanical Shock TestingShall be performed
per Method 2002 of MIL-STD-883.
10.9 Insulation Resistance TestingShall be
performed per Method 2002 of MIL-STD-883.
10.10 Internal Water Vapor Content Testing — Shall
be performed per Method 1018 of MIL-STD-883.
10.11 Hermeticity Testing — Shall be performed per
Method 1014, Condition A of MIL-STD-883. The
hermetic integrity of the packaged device must be
maintained after all testing.
10.12 Lead Integrity Testing — Shall be performed
per Method 2004, Condition A, B1, and B2 of MIL-
STD-883.
10.13 Solderability Testing — Shall be performed per
Method 2003 of MIL-STD-883.
10.14 Moisture Resistance — Shall be performed per
Method 2003 of MIL-STD-883.
11 Packaging and Marking
11.1 Packing — Containers selected shall be strong
enough and suitably designed to provide maximum
protection against crushing, spillage, and other forms of
damage to the container or its contents. Containers shall
afford protection of the contents to contamination from
exposure to excessive moisture or oxidation by gases.
Packaging materials shall be so selected to prevent any
contamination of the ceramic component part with
paper fibers or organic particles.
11.2 Marking — The outer containers shall be clearly
marked identifying:
1. Vendor part number
2. Customer part number
3. Quantity
4. Date of manufacture
5. Vendor lot number
12 Applicability
This specification is intended to apply to packages
fabricated to the outline requirements for the fine pitch
leaded and leadless chip carriers included in JEDEC
Publication 95.
NOTICE: These standards do not purport to address
safety issues, if any, associated with their use. It is the
responsibility of the user of these standards to establish
appropriate safety and health practices and determine
the applicability of regulatory limitations prior to use.
SEMI makes no warranties or representations as to the
suitability of the standards set forth herein for any
particular application. The determination of the
suitability of the standard is solely the responsibility of
the user. Users are cautioned to refer to manufacturer’s
instructions, product labels, product data sheets, and
other relevant literature respecting any materials
mentioned herein. These standards are subject to
change without notice.
The user’s attention is called to the possibility that
compliance with this standard may require use of
copyrighted material or of an invention covered by
patent rights. By publication of this standard, SEMI
takes no position respecting the validity of any patent
rights or copyrights asserted in connection with any
item mentioned in this standard. Users of this standard
are expressly advised that determination of any such
patent rights or copyrights, and the risk of infringement
of such rights, are entirely their own responsibility.
Copyright by SEMI® (Semiconductor Equipment and Materials
International), 3081 Zanker Road, San Jose, CA 95134. Reproduction o
f
the contents in whole or in part is forbidden without express written
consent of SEMI.
SEMI G51-90 © SEMI 19901
SEMI G51-90
SPECIFICATION FOR PLASTIC MOLDED (METRIC) QUAD FLAT PACK
LEADFRAMES
1 Preface
This specification defines the acceptance criteria for
leadframes designed for assembly of JEDEC proposed
registered Publication 95 Standard Outlines for the
Metric Quad Flat Pack Family Packages. It is a design
guideline for packaging engineers, leadframe stampers
and etchers, and mold and trim/form tooling
manufacturers. It has been developed to meet the
requirements of assemblers using automatic and manual
equipment.
2 Applicable Documents
2.1 Order of Precedence — To avoid conflicts, the
order of precedence when ordering tooling shall be as
follows:
Purchase Order
This Specification
Referenced Documents
2.2 Reference Documents
2.2.1 SEMI Specifications
SEMI G4 — Specification for Integrated Circuit
Leadframe Materials Used in the Production of
Stamped Frames
SEMI G10 — Standard Method Mechanical
Measurement for Plastic Package Leadframes
SEMI G18 — Specification for Integrated Circuit
Leadframe Material Used in the Production of Etched
Frames
SEMI G21 — Specification, Plating Integrated Circuit
Leadframes
2.2.2 ANSI Specification
1
S Y 14.5 M-1982 — Dimensioning and Tolerancing
2.2.3 JEDEC Specification
2
Reg.Prop. 11-286 — Metric Quad Flat Pack Family
(Gullwing)
1 ANSI, 1430 Broadway, New York, NY 10018
2 JEDEC, 2001 Eye Street N.W., Washington, D.C. 20006
2.2.4 Military Specification
3
MIL-STD-105 — Sampling Procedures and Tables for
Inspection by Attributes
3 Selected Definitions
burr — a fragment of excess material either horizontal
or vertical attached to the leadframe.
cambercurvature of the leadframe strip edge (see
Figure 1).
Figure 1
Camber
coil set — longitudinal bowing of the leadframe (see
Figure 2).
Figure 2
Coil Set
coined areathat area at the tip end of the bond
fingers coined to produce a flattened area for functional
use (see Figure 3).
3 Military Standards, Naval Publications and Form Center, 5801
Tabor Avenue, Philadelphia, PA 19120