CABLE *
WIRE
SEAL (CS)
SIZE
UNSEALED
AWG
(US)
US
CS
US
CS
US
US
CS
US
CS
US
22
18
20
18
20
14
16
14
16
2(18-20)
12
12
10
12
10
12
WIRE
SPEC.
AWG
WIRE
SIZE
METRIC
WIRE
SPEC
METRIC
CONDUCTOR
CRIMP HEIGHT
AWG
(SECT Z-Z)
(+/-0.05)
1.10
1.30
1.20
1.35
1.20
1.70
1.50
1.70
1.50
VARIABLE
1.95
N/A
N/A
2.25
1.95
CONDUCTOR
CRIMP HEIGHT
METRIC
(SECT Z-Z)
(+/-0.05)
1.10
1.30/1.40
1.25
1.30/1.40
1.25
1.80*/1.90
1.40*
1.80*/1.90
1.40*
VARIABLE
1.95
N/A
N/A
2.40*/2.50*
2.05
CONDUCTOR
CRIMP WIDTH
(SECT Z-Z)
(+/-0.10)
1.85
2.05
INSULATION
CRIMP HEIGHT
AWG
(SECT Z-Z)
(+/-0.05)
1.75
4.00
3.85
2.35
2.20
4.40
4.25
2.70
2.60
VARIABLE
4.80
INSULATION
CRIMP HEIGHT
METRIC
(SECT Z-Z)
(+/-0.05)
1.65
2.10
2.00
2.10/2.30
2.00
4.10*/4.35*
4.05*/4.15*
3.00*/3.10
2.55*/2.65
VARIABLE
4.40
3.30
INSULATION
CRIMP WIDTH
(SECT Y-Y)
(+/-0.10)
2.60
3.30
2.60
4.10
3.20
4.30
4.30
4.15
N/A
4.20
INSULATION
CRIMP
OPTION
INS
GRIP
FORM
TYPE
SECD-D
1
3
3
1
1
3
3
1
1
2
3
LTRS
REVISIONS
CHECKER
ENG APP
MATL APP
CRIMP TOOL INFORMATION, (REFERENCE ONLY)
INSULATION
CRIMP
CORE/
CRIMP
WIDTH INSULATION
OPTION
1.85
CONDUCTOR
---
2.05
CONDUCTOR
---
2.45
CONDUCTOR
---
2.60 INSULATION
2
3.05
CONDUCTOR
---
3.20 INSULATION
2
3.30 INSULATION
2
3.45
CONDUCTOR
---
4.10 INSULATION
2
4.15 INSULATION
2
4.20 INSULATION
1
4.30 INSULATION
2
4.30 INSULATION
1
E
#
0.03
0.83
0.92
1.09
---
1.36
---
---
1.54
---
---
---
---
---
F
#
0.03
0.48
0.53
0.63
---
0.79
---
---
0.89
---
---
---
---
---
G
#
0.03
0.11
0.12
0.16
---
0.22
---
---
0.26
---
---
---
---
---
J
#
0.03
2.31
2.56
3.06
---
3.81
---
---
4.31
---
---
---
---
---
K
#
0.03
1.79
1.99
2.38
---
2.96
---
---
3.35
---
---
---
---
---
L
#
0.03
OFFSET
BETWEEN AVILS
ORIGINATOR
PARTIAL SECTION A-A
ES-AU5T-1A348-AA
ESB-MIL123-A
0.35
0.75/1.00
0.50
0.75/1.00
0.50
2.00/2.50
1.50
2.00/2.50
1.50
2(.50/1.00)
3.00
3.00
5.00/6.00
4.00
5.00/6.00
4.00
M
#
0.03
N
#
0.03
---
---
---
0.18
---
0.23
0.24
---
0.32
0.33
0.33
0.34
0.34
P
#
0.03
---
---
---
3.25
---
4.00
4.12
---
5.12
5.19
5.25
5.38
5.38
R
#
0.03
---
---
---
2.53
---
3.11
3.20
---
3.98
4.03
4.08
4.17
4.17
S
#
0.03
---
---
---
2.50
---
3.08
3.17
---
3.94
3.99
4.04
4.13
4.13
T
#
0.03
---
---
---
N/A
---
N/A
N/A
---
---
---
1.87
---
1.92
U
#
0.03
---
---
---
N/A
---
N/A
N/A
---
---
---
1.08
---
1.11
GOLD INLAY
TOP SURFACE
ONLY
1. MATERIAL FOR ITEM#1 GOLD INLAY: USE
MATERIAL TYPE 3.
2. MATERIAL TO BE ELECTRO
MATTE TIN PLATED PER
ASTM-B-545-92 EXCEPT IN AREA OF
GOLD INLAY AND BARE STRIPES.
3. INLAY MATERIAL TO BE GOLD ALLOY, (WE#1)
PER ASTM B522 (69% Au, 25% Ag, 6% Pd)
0.00025mm MINIMUM OVER
A PALLADIM ALLOY, (60%PALLADIUM, 40%SILVER)
0.00051mm MIN, OVER NICKEL, NI-BP050 0.0203/0.0274mm.
OPTION 2
2.50
3.05
3.45
OPTIION 1
3.40
OPTION 2
1
3
3
1
1
3.45
N/A
N/A
N/A
N/A
4.20
4.30
USE 12 GA TERMINAL 3.90
---
---
---
0.00
---
0.40
0.60
---
0.80
0.40
0.80
1.10
0.60
1.78
1.97
2.36
---
---
---
---
3.32
---
---
4.04
---
---
(2.0)
EXPOSED BASE
MATERIAL
(Cu) 4 OUTER SIDES
OF TERMINAL BOX
REVISED AND REDRAWN AFTER INTERNAL
REVISION AB
AC1 ADDED METRIC EQUIVALENT WIRE CODES
AC2 REMOVED CRIMP INFORMATION AND VIEWS
AELE-E-11786306-131
B CUE
RJC
(4.3
3.3)
LENGTH OF
GOLD INLAY
ITEM
2
ITEM
1
10.1
(2.0)
EXPOSED
BASE MAT'L( Cu)
#
0.5
STOCK
EDGE
MATERIAL FOR ITEM#2 FOR GOLD PLATING:
USE MATERIAL TYPE 4. (NICKEL PLATED)
REVISED SHEET TWO; ADDED POGO PIN
INFORMATION, NOTES, VIEWS.
AD2 REVISED UN-SEALED VIEWS,
ADDED 18.60 DIM
AD3 UPDATED SHEET 1 TO SDS STANDARDS.
AD4 RELEASED P/N BU5T-14474-HAA,JAA,KAA
LAA,MAA,NAA
AELE-E-11786306-159
B CUE
RJC
AD1
4.3/3.3
INLAY
0.13 MIN.
OPTION 1
GOLD INLAY
SEE NOTE 3
NICKEL
ITEM
2
*NOT VERIFIED TO USCAR-21
NICKEL INLAY
SEE NOTE 3
PALLADIUM-SILVER
INLAY SEE NOTE 3
STANDARD
FORM TOOLING DESIGN
"B"
CONDUCTOR CRIMP
(R0.13)
J
(RAD)
M
E
P
(RAD) 2X
F
STANDARD "B"FORM TOOLING DESIGN
INSULATION CRIMP OPTION
(R0.13)
(RAD)
S
T
S
PUNCH AND ANVIL DESIGN
"D"
STANDARD
FORM TOOLING
INSULATION CRIMP OPTION
Z
2
1
Y
100% MATTE Sn
0.0025 MIN. THICK
ITEM
1
GOLD INLAY PLATING OPTION 2
1.60 MIN
GOLD WIDTH
ZONE "C"
(CW)
CRIMP WIDTH
(CH)
CRIMP HEIGHT
MATERIAL FOR SPOT GOLD: USE
TYPE 5 MATERIAL.
ZONE "C"
ZONE "A": BOTH SIDES: SULFAMATE DUCTILE
NICKEL, 0.00005mm MIN PER ASTM B689
TYPE 2.
ZONE "B": BOTH SIDES 100% ELECTRO MATTE
TIN, 0.00254-0.0038mm. PER ASTM B545. NO
NICKEL IN THIS AREA.
STOCK
WIDTH
ZONE "C": RAISED RIB SIDE ONLY: SULFAMATE
DUCTILE NICKEL, STRIPE PLATE
0.0013-0.0025mm. UNDER 99.0% PURE HARD
GOLD CAP SPOT PLATE 0.00076mm MIN. PER
ASTM B488-01 TYPE 2 CODE C.
ZONE "D": BOTH SIDES. TRANSITION AREA.
(TIN AND NICKEL MUST OVERLAP). MUST HAVE
MINIMUM OF 0.00005mm OF NICKEL PLATING
BOTH SIDES.
CARRIER: 0.00005mm MIN. TIN OR OPTIONAL
NO PLATING.
USE SPRING MATERIAL TYPE 4: ( NICKEL PLATED )
WORKING SURFACES
MUST BE POLISHED
ALL AROUND
0.40/0.30 x 45$
CHAMFER AROUND
FORM (BOTH SIDES)
(RAD)
U (RAD)
P (RAD)
INSULATION PUNCH
N
Z
Y
CONDUCTOR CRIMP
SECTION Z-Z
ZONE "A"
ZONE "D"
(R5.1) 2X
G
Y1
N
Y2
(R5.1) 2X
4.3
Y3
(R5.1) 2X
(CW)
4.3
CRIMP WIDTH
(CW)
CRIMP WIDTH
25.6
+0/-1.0
4.3
PUNCH
PUNCH
(CH)
(3.0°) 2X
ANVIL
K
0.20 FLAT 2X
VIEW Y2
(3.0°) 2X
R
ANVIL
0.20 FLAT 2X
VIEW Y3
(3.0°) 2X
R
INSULATION ANVIL
INSULATION CRIMP
CRIMP HEIGHT
INSULATION CRIMP
CRIMP HEIGHT
(CH)
16.4
+0.5/-0.5
ZONE "B"
0.20 FLAT 2X
VIEW
Y
"B"
OPTION
STYLE
1
"D"
OPTION
STYLE
2
(5.0 CARRIER)
CRIMP TOOL INFORMATION (REF. ONLY)
TABLE - 1 - TERMINAL GRIP
FORD PART NO.
XF2T-14474-CA
BU5T-14474-HAA
9U5T-14474-KA
AU5T-14474-CAA
XL3T-14474-DA
AU5T-14474-ZA
AU5T-14474-XA
8U5T-14474-GA
F8VB-14474-BA
BU5T-14474-JAA
YF1T-14474-CA
BU5T-14474-KAA
9U5T-14474-JA
4L3T-14474-AA
XL3T-14474-AA
AU5T-14474-AAA
AU5T-14474-YA
8U5T-14474-HA
F8VB-14474-AA
BU5T-14474-LAA
XL3T-14474-CA
4L3T-14474-CA
7L7T-14474-EA
BU5T-14474-MAA
XF2T-14474-BA
BU5T-14474-NAA
1.
1
1
1
1
FCI PART NO.
54002231
F067210
54001879
F703600
54001840
F703500
F903500
54001876
54001839
F167210
54001311
F267210
54001448
54001439
54001432
F803500
F013500
54001446
54001431
F367210
54001220
54001221
54001227
F467210
54001018
F567210
METRIC
WIRE
0.35
0.35
0.50,0.75
1.00
0.50,0.75
1.00
0.50,0.75
1.00
0.50,0.75
1.00
0.50,0.75
1.00
0.50,0.75
1.00
0.50,0.75
1.00
0.50,0.75
1.00
0.35/1.00
2 WIRE
0.35/1.00
2 WIRE
SECTION Y-Y
SECTION Y-Y
DIMENSION TABLE
(C1)
0.76
C2+/-0.30
1.7
(D1)
1.40
D2+/-0.30
2.10
L+/-0.10
0.00
V #
0.5
0.3
W #
0.30
7.5
GRIP
STAMP
22
NOTES:
SPOT GOLD PLATING OPTION 3
NOT AVAILABLE AT THIS TIME
AWG
WIRE
22
22
18,20
18,20
18,20
18,20
18,20
18,20
18,20
18,20
18/20
2 WIRE
18/20
2 WIRE
GRIP
STAMP
22
22
18
18
18
18
18
18
18
18
13
13
14
14
14
14
14
14
14
14
12
12
12
12
10
10
PLATING
TIN
TIN
GOLD
INLAY
CABLE/UN
GREASED
SEALED
CS/US
A+/-0.30
2.6
B+/-0.30
3.2
US
US
CS
CS
CS
CS
US
US
US
US
US
US
CS
CS
CS
CS
US
US
US
US
CS
CS
US
US
US
US
NO
YES
NO
YES
NO
NO
NO
NO
NO
YES
2
NO
YES
2
NO
YES
2
NO
NO
NO
NO
NO
YES
2
NO
YES
NO
YES
2
NO
YES
2
2
2
2
19.0
TIN
TIN
GOLD
SPOT
GOLD
SPOT
GOLD
INLAY
3.0
5.1
1.00
1.9
3.00
3.70
0.60
19.5
8.0
18
1) CONFORMS TO ALL APPLICABLE SECTIONS OF:
SAE/USCAR-2 REV.3 EXCEPT TERMINAL BEND RESISTANCE
SECTION 5.2.2
SAE/USCAR-12 REV 2
SAE/USCAR-21
FORD SDS VER 11
TIN
TIN
TIN
TIN
GOLD
INLAY
3.0
3.8
1.00
1.9
1.75
2.70
0.00
19.0
7.5
18
SERRATION
10,12 GA
(15.24)
PROGRESSION
SERRATION
ALL OTHERS
2) MATERIALS
MATERIAL TYPE 1: C14530 CU TO ASTM B-152
THICKNESS 0.305
# 0.008
TENSILE STRENGTH 372-442 MPa
MINIMUM ELONGATION: 2.5% IN 51mm.
PLATING : 100% HOT TIN DIP : 0.0005-0.0025mm.
(2.54)
MATERIAL TYPE 2: C17410 BE CU TO ASTM B-768
THICKNESS: 0.203
# 0.008
TENSILE STRENGTH 758-897 MPa
YIELD STRENGTH 655-862 MPa
MINIMUM ELONGATION: 7% IN 51mm
PLATING: 100% HOT TIN DIP : 0.0005-0.0025mm.
MATERIAL TYPE 3: C14530 CU TO ASTM B-152
THICKNESS 0.305
# 0.008
TENSILE STRENGTH 324-394 MPa
MINIMUM ELONGATION: 2.0% IN 51mm.
PLATING : SEE SPECIAL PLATING SECTION FOR INLAY GOLD.
MATERIAL TYPE 4: C17410 BE CU TO ASTM B-768
THICKNESS: 0.203
# 0.008
TENSILE STRENGTH 758-897 MPa
YIELD STRENGTH 655-862 MPa
MINIMUM ELONGATION: 7% IN 51mm
PLATING: SULFMATE DUCTILE NICKEL 0.0013-0.0025mm.
TO ASTM B689 TYPE 2.
MATERIAL TYPE 5: C14530 CU TO ASTM B-152
THICKNESS 0.305
# 0.008
TENSILE STRENGTH 372-442 MPa
MINIMUM ELONGATION: 2.0% IN 51mm.
PLATING : SEE SPECIAL PLATING SECTION FOR SPOT GOLD.
3) THE APEX 2.80mm TERMINAL IS SYMMETRICAL
ABOUT CENTERLINE AND CAN BE INSERTED 180
4) DIMENSIONAL
1 PLACE
2 PLACE
ANGULAR
TOLERANCE:
#
0.25
#
0.10
# $
3
$
ACTUAL SIZE
4.60
6.6
1.50
3.7
2.55
6.00
0.60
19.0
7.5
13
(13.46)
1.50/2.50
14,16
1.50/2.50
14,16
1.50/2.50
14,16
1.50/2.50
14,16
1.50/2.50
14,16
1.50/2.50
14,16
1.50/2.50
14,16
1.50/2.50
14,16
TIN
TIN
GOLD
SPOT
GOLD
SPOT
GOLD
INLAY
3.8
6.1
1.45
2.3
3.80
4.60
0.80
19.5
8.0
14
(2.74)
3.8
4.7
1.45
2.3
2.25
3.20
0.40
19.0
7.5
14
(2.18)
MUST HAVE
RECTANGULAR SLOT
TIN
TIN
TIN
TIN
TIN
TIN
TIN
TIN
3.00
3.00
3.00
3.00
4.00/6.00
4.00/6.00
12
12
12
12
10
10
5.2
6.6
2.30
3.2
4.30
5.20
1.10
19.5
8.0
12
5.2
5.2
2.30
3.2
3.00
3.80
0.40
19.0
7.5
12
5.2
6.5
2.30
3.2
3.20
4.00
0.80
19.0
7.5
10
SPOT GOLD PLATING IS NOT AVAILABLE AT THIS TIME.
(V)
C
2. GREASE USED IS NYE UNIFLOR 8917.
(W)
2.0
BEFORE COIN
3.80
BEFORE COIN
A
0.20/0.05
COIN ALL
GRIPS
B
B
D1/2
C1/2
D1/2
5) DRAWING CONFORMS TO AVP - ( T401/T406)-001
6) SEE USCAR DRAWING EWCAP-001 FOR DIRECT CONNECT MATING
BLADE INFORMATION
7) ANNUAL QUALITY REQUIREMENTS:
FCI SPECIFICATION #AQA-001 INSTEAD OF ANNUAL LAYOUT
ANNUAL PV REQUIREMENTS OF QS-9000 SECTION 2
IT IS PERMISSIBLE TO PERFORM CONTINUOUS CONFORMANCE PER
&
A
A
INSULATION HOLE SIZE
AND SHAPE OPTIONAL
FOR ALL CABLE SEAL GRIP
SIZES AND TYPES
C2
(
C1)
SECTION C-C
CORE GRIP
8) VENDOR,TOOL,GRIP
& WEEK CODES MUST BE PRESENT
& LEGIBLE
CORNER SEAM ON TOP, BOTH SIDES
MUST BE CLOSED.
D2
SECTION D-D
UNSEALED
INSULATION GRIP
(
D1)
D2
SECTION
D-D
SC
3X(
D1)
9) "SC" DESIGNATES SPC DIMENSION (2)
10 "K" INDICATES IN PROCESS INSPECTION FOR DIMENSIONS OR
SPECIFICATIONS (3)
11) CAVITY SPECIFICATIONS, SEE SHEET # 2
GREASE OVERFLOW
PERMISSIBLE IN THIS AREA
CABLE SEAL
INSULATION GRIP
4L3T-14474-AA
9U5T-14474-KA
9U5T-14474-JA
BU5T-14474-NAA
BU5T-14474-MAA
BU5T-14474-LAA
BU5T-14474-KAA
BU5T-14474-JAA
BU5T-14474-HAA
AU5T-14474-CAA
7L7T-14474-EA
YF1T-14474-CA
4L3T-14474-CA
DESIGN
VB
CHECKED
SSS
SCALE
4:1
DATE
20041215
DETAIL
RS
SAFETY
TITLE
REFERENCE
FCI - AUTOMOTIVE (7362)
FOR INFORMATION CONTACT: FCI - AUTOMOTIVE
(7362)
A
4.30
4.20
SC
2
8.2
( 3.90 )
0.20/0.05 COIN
TOP OF BOX AND
TRANSITION AREA
MEASURE BEFORE
FORMING.
PART MUST COMPLY WITH MATERIAL SPECI FICATION WSS-M99P9999-A1
TO HELP SAFEGAURD HEALTH, SAFETY AND
DRAFTED IN ACCORDANCE WITH FAO
ENGINEERING DRAFTING STANDARD
CURRENT AT INITIAL RELEASE
CAD TYPE
X-PROE
OPER. NO.
CAD LOC.
N/A
UNIT
DRAWING
CAD FILE
THE ENVIRONMENT.
3 RD ANGLE PROJ
DIMENSIONS IN
MILLIMETERS
DTM
IS MASTER
B
SC
1
2.90
B
C
D
A
B
D1/2
C1/2
8U5T-14474-HA
8U5T-14474-GA
XF2T-14474-CA
XF2T-14474-BA
XL3T-14474-DA
XL3T-14474-CA
F8VB-14474-AA
SHT
OF
1
2
A0/E
DRW SIZE
SECTION
B-B
PRESSURE FILL
NYE UNIFLOR 8917
FOR GREASED TERMS
(2.6)
2X
3.50
3.20
C
L
A-A
D
TIN PLATING OPTION 1.
USE MATERIAL TYPE 1
&2.
C2
SECTION
C-C
DOUBLE WIRE
(13GA) CORE GRIP
2X(
C1)
D2
SECTION D-D
DOUBLE WIRE
(13GA) INSULATION GRIP
XL3T-14474-AA
2X(
D1)
F8VB-14474-AA
F8VB-14474-BA
TERMINAL - (2.80MM)
WIRE SNAP ON FEMALE
DIVISION
PLANT
B
SECTION
6.50
#
0.20
0.00 MIN.
6.50
#
0.20
LTRS
ORIGINATOR
REVISIONS
CHECKER
ENG APP
MATL APP
A
A
SEE SHEET 1
DATE:20100928
AELE-E-11786306-131
B CUE
RJC
SEE SHEET 1
DATE:20110718
AELE-E-11786306-159
A
SECTION
SECTION A-A
TPA IN PRE-LOCK POSITION
POGO PIN
TARGET AREA
1.50 MIN.
A
SECTION A-A
TPA IN PRE-LOCK POSITION
B CUE
RJC
B-B
MINIMUM POGO
PIN HEIGTH.
2.60 MAX.
SECTION
B-B
A
30.00 MIN FOR
STRAIGHT WIRE
DRESS
SHOULDER MUST STOP
ON PLASTIC.
SECTION A-A
TPA IN FINAL-LOCK POSITION
18.60
MINIMUM RECOMMENDED
DISTANCE FOR MAT SEAL
LOCATION
B
B
6.50
SECTION A-A
TPA IN FINAL-LOCK POSITION
ASSEMBLY DETAIL
ASSEMBLY DETAIL
3.50
MAXIMUM
A
B
B
6.40
REAR OF
CONNECTOR
A
6.50
SECTION
A-A
4.50
5.25
ACCEPTABLE
POGO PIN TIPS
FEMALE CAVITY DETAIL
A
5.25
SEAL ZONE
AREA TO BE USED
FOR MAT SEAL. DEPENDANT
ON THE MAT SEAL DESIGN.
1. IT IS THE RESPONSIBILITY OF THE TEST FIXTURE
MANUFACTURER TO ALIGN AND SIZE THE POGO
PIN TIP TO ALWAYS CONTACT THE TERMINAL
TARGET AREA.
2. IT IS THE RESPONSIBILITY OF THE TEST FIXTURE
MANUFACTURER TO PROPERLY ALIGN THE
CONNECTOR AND POGO PINS TO PREVENT THE
POGO PINS FROM CAUSING DAMAGE TO THE
TERMINAL OR CONNECTOR.
3. THE TIP OF THE POGO PIN IS NOT ALLOWED TO
ENTER THE OPENING OF THE TERMIAL.
THE EXAMPLES OIN THIS GRAPHIC ILLUSTRATE THE SOLID
SHAFT OF SPRING LOADED TEST PROBE DESIGNS. THE
SHOULDERS SHOWN ON THE ROUND DESIGNS ARE INTENDED
TO STOP ON THE PLASTIC CONNECTOR HOUSING AND PREVENT
THE TIP OF THE PROBE FROM ENTERING THE FEMALE TERMINAL.
THE BLADE DESGN IS INTENDED TO TOUCH THE FEMALE
TERMINAL AT 90 DEGREES TO THE ORIENTATION OF THE
MATING MALE TERMINAL BLADE AS TO PREVENT THE BLADE
FROM ENTERING THE FEMALE TERMINAL.
5.90
6.40
(R 2.25 )
SECTION
A-A
OVAL SEAL CAVITIES
[OPTIONAL CONSTRUCTION]
FEMALE CAVITY DETAIL
4. MAXIMUM FORCE OF A POGO PIN IS NOT TO EXCEED
3.0 NEWTONS WHEN CONTACTING ANTY PORTION
OF THE CONNECTOR SYSTEM.
UN-SEALED OPTION
A
( 1.80 )
0.60
0.2
A
B
( 1.15 )
POGO PIN DESIGN CRITERIA
CABLE SEAL OPTIONS
CAVITY DETAIL [SHOWN UNSEALED OPTION]
( 10.0 )
OF
R
-C-
0.10
0.05
( 0.5 )
P PERMISSIBLE
L
R 0.15
0.70
#
0.05
1.00
0.1 MAX.
MISMATCH PERMISSIBLE IN
THE DIRECTION SHOWN
CAVITY DETAIL NOTES:
4.425
W/TERMINAL
#
0.075
4.50
2.31+0.15
-0.25
0.75
5 $
A B
DETAIL
SCALE
2.51+0.10
-0.25
1. CAVITY, TPA DESIGN SHOWN IS BASED ON
UTILIZATION OF A SPECIFIC MATERIAL
(NYLON 6/6 35% GLASS FILLED)
USER OF THIS CAVITY DESIGN IS RESPONSIBLE
FOR ANY NECESSARY MODIFICATIONS
REQUIRED FOR A SPECIFIC APPLICATION
OR MATERIAL.
2.CAVITY DETAIL IS VALID FOR BOTH SEALED AND
UNSEALED APPLICATIONS. THE MAT-SEAL MUST
FALL BEHIND THE CAVITY PROPER AS INDICATED,
AND THE DESIGN WILL BE DETERMINED BY THE
CONNECTOR DESIGN REQUIREMENTS.
3. CAVITY DESIGN IS GENERIC IN NATURE. IT IS
INTENDED TO DOCUMENT CAVITY DIMENSIONS
REQUIRED FOR PROPER TERMINAL FIT. DESIGN
HAS BEEN SHOWN TO BE FUNCTIONAL. ALTERNATE
DESIGNS MEETING CAVITY DIMENSIONS MY ALSO BE
ACCEPTABLE.
4. UNLESS SPECIFIED ALL RADIUS TO BE 0.30MM
GENERAL TOLERANCES
#
0.10 ALL TWO PLACES
DIM
#
1.0 $ON ANGULAR DIMS.
4X
R 1.00
+0.10
-0.25
R
5.80
5. UNDIMENSIONED FEATURES ARE AT THE
DISCRETION OF THE COMPONENT DESIGNER.
6. INDICATES IN-PROCESS INSPECTION FOR
MANUFACTURING DIMENSIONS OR
SPECIFICATIONS.(2)
7. DENOTES GAGE REQUIRMENTS FOR
USER AND MANUFACTURER.(3)
8. VENDOR MUST SUBMIT FOR ENGINEERING
APPROVAL, THE LOCATION OF PARTING LINES
PRIOR TO CONSTRUCTION OF MOLD.
4X
R 0.30
9. TO BE USED WITH 2.80mm
APEX FEMALE TERMINAL SYSTEM SEE SHEET 1.
10. UNLESS OTHERWISE SPECIFIED ALL DRAFT TO
BE WITHIN DIMENSIONAL TOLERANCE ONLY.
CABLE SEAL
OPENING
PARTIAL VIEW
FOR CLARITY.
11. EXTERNAL CAVITY PROFILE FOR REFERENCE
ONLY.
10. REFERENCE: FCI CAVITY DRAWING C15001.DWG REV. E
TOLERANCES: 1 PLACE
2 PLACE
ANGULAR
#
0.25
#
0.10
# $
2
1.12
#
0.05
R0.3
#
0.1
R FULL
SECTION
PARTIAL VIEW
1.91
1.75
OF
1.80
2X
2.80
0.2
A B
1.85
0.2
3.20
0.1
#
0.05
A B
A B
A
SECTION
ROTATED 90
1.60
+0.15
-0.15
-B-
1.30
D-D
0.4
A B
0.2
B-B
$CLOCKWISE
F
10.0
C
A
( 1.20 )
45 $TYP.
R 0.3
4.43
OF
( 3.05 )
-C-
4.0
B
B
7.3
8.2
4.10
1.61
1.20
0.1
A C
D
A
D
R FULL
1.81
2X
1.81
1.15
( 13.9 )
6.1
0.75
SECTION
2.0
OF
-C-
2X
R
0.25
0.10
C
C-C
NOTES:
1. BY USING ANY INFORMATION CONTAINED IN THIS DRAWING
(FCI AUTOMOTIVE), THE USER AGREES TO THE FOLLOWING:
6.33
A
2.4
7.3
PRE-LOCK POSTION
TO FACE OF HOUSING
15.30
3.90
W/TERMINAL
( 0.85 )
1.05
2X
2.85
3.75
10.0
2X
30 $
1.60
#
0.15
A. USING FCI AUTOMOTIVE INFORMATION SHOWN IN THE DRAWING FOR ANY PURPOSE
OTHER THAN CAVITY DESIGN IS PROHIBITED.
B. ANY IMPLIED WARRANTIES OF MERCHANTABILITY, FITNESS FOR A PARTICULAR
OR NON-FRINGMENT OF ANY THIRD PARTY INTELLECTUAL PROPERTY ARE EXPRESSLY
DISCLAIMED AND EXCLUDED. THE ENTIRE RISK AS TO THE RESULT OBTAINED BY
THE FCI AUTOMOTIVE INFORMATION IS ASSUMED BY THE USER.
C.
FCI AUTOMOTIVE SHALL NOT BE LIABLE FOR ANY LOSS OR INJURY TO EARNINGS,
PROFITS, GOODWILL, OR ANY PUNITIVE. EXEMPLARY, DIRECT CHAIN, SPECIAL,
INDIRECT, INCIDENTAL, OR CONSEQUENTIAL DANGERS.
THE USER OF THE FCI AUTOMOTIVE INFORMATION AGREES TO DEFEND, IDENTIFY
AND HOLD HARMLESS FCI AUTOMOTIVE AND ITS AFFLIATED ENTITIES, RESPECTIVE
EMPLOYEES, AND AGENTS FROM ANY AND ALL CLAIMS. COSTS, EXPENSES, DAMAGES.
JUDGEMENTS, OR OTHER LOSSES INCLUDING THE COST OF INVESTIGATION AND
AND REASONABLE ATTORNEY'S FEES ARISING OUT OF THE USE OF THE
FCI AUTOMOTIVE INFORMATION.
OFFICIERS,
LITIGATION
PURPOSE
USING
X
REFERENCE
FCI - AUTOMOTIVE (7362)
FOR INFORMATION CONTACT: FCI - AUTOMOTIVE
(7362)
2.48
4.08
1.62
7.50
TERMINAL
3.05
W/TERMINAL
5.63
C
R 0.3
AROUND
FACES
#
0.05
4.70
0.2
A C
D.
PART MUST COMPLY WITH MATERIAL SPECI FICATION WSS-M99P9999-A1
TO HELP SAFEGAURD HEALTH, SAFETY AND
DRAFTED IN ACCORDANCE WITH FAO
ENGINEERING DRAFTING STANDARD
CURRENT AT INITIAL RELEASE
CAD TYPE
X-PROE
OPER. NO.
CAD LOC.
N/A
UNIT
DETAIL
SAFETY
DATE
DRAWING
TITLE
CAD FILE
THE ENVIRONMENT.
3 RD ANGLE PROJ
DIMENSIONS IN
MILLIMETERS
DTM
IS MASTER
9.6
2.41
1.30
OF
-C-
30 $
CONST.
E. ANY PROPOSED TERMINAL /CONNECTOR COMBINATION MUST BE TESTED AND VALIDATED
FUNCTION PROPR TO IMPLEMENTATION IN A HARNESS DESIGN. THE OEM SHALL DEFINE
RESPONSIBILITY FOR TERMINAL/CONNECTOR VALIDATION.
F.
G.
USER IS RESPONSIBLE FOR ANY SPECIFIC APPLICATION OF THE
FCI AUTOMOTIVE INFORMATION.
MANUFACTURER RECOMMENDS USE OF FCI AUTOMOTIVE SUPPLIED TERMINALS WITH THE
DESIGN SHOWN IN DRAWING.
FCI AUTOMOTIVE INFORMATION CANNOT BE USED BY ANY PERSON OR ENTITY FOR ANY
OTHER THAN FORD APPLICATION.
ANY USE OF THE INFORMATION SHOWN ON THE DRAWING REQUIRES THE PRIOR WRITTEN
OF FCI AUTOMOTIVE OR FORD MOTOR COMPANY.
FOR
SHT
OF
TPA MUST HAVE
PRE LOCK AND
FINAL LOCK FEATURE.
THIS IS DEPENDANT
ON THE CONNECTOR
DESIGN.
X
TPA DETAIL
( 13.9 )
2.6
9.9
10.3
SEE DETAIL
( 23.65 )
J.
SECTION
CONSENT
SECTION X-X
A-A
SCALE
DIVISION
PLANT
DRW SIZE
F
0.65
CONST.
H.
PURPOSE
CHECKED
WIRE SNAP ON FEMALE
A0/E
2.8
CAVITY
DESIGN
Embedded System
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