FMU-139 SPANNER-TORQUE ADAPTER CAD.pdf
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- GBU JDAM Tool Kits
- Solicitation number
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About this file
This is an engineering drawing for a Spanner/Torque Adapter for an FMU-139 Fuze Ring, created by the U.S. Air Force at Eglin AFB. The technical drawing (X200334027-01B) provides detailed specifications for a precision-machined component with two material options: 1) Alloy Steel Round (AISI 4340) with a tensile strength of 160-182 KSI, or 2) Stainless Steel Bar (17-4PH) with a tensile strength condition of H1150. The drawing includes specific requirements for heat treatment, surface finishing (phosphate or optional Black-T coating), and marking, with strict workmanship standards mandating the part be free from various potential defects. The document is marked with a Distribution Statement C, limiting access to U.S. government agencies and contractors, and includes a warning about export control restrictions.
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Text version
Z. FIELDING 20040107
1/2
NOTES:
INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.1.
REMOVE ALL BURRS AND SHARP EDGES.2.
MATERIAL: ALLOY STEEL ROUND 3.25 DIAMETER, AISI 4340. HEAT TREAT TO TENSILE STRENGTH 3 CONDITION OF 160-182 KSI (RC36 TO 40) IAW SAE-AMS-H-6875. CLEAN AND SURFACE TREAT
IAW TT-C-490, TYPE I OR II.
OPTION 2: 3.25 DIAMETER SST BAR 17-4PH, ASTM A564 OR SAE-AMS-5643. HEAT TREAT TO
TENSILE STRENGTH CONDITION OF H1150 (RC 26 TO 36) IAW SAE-AMS-6875. PASSIVATE IAW
SAE-AMS-QQ-P-35.
WORKMANSHIP: 4.
ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE
FROM DEFECTS SUCH AS, BUT NOT LIMITED TO, BLEMISHES, BURRS, CAVITIES, PITS, VOIDS, CORROSION, CRACKS, DENTS, DISTORTION, WARPAGE, GOUGES, SCORES, NICKS, INCLUSIONS, LAPS, POROSITY, SLIVERS, AND OTHER FOREIGN MATTER. EXCEPT AS PROVIDED
ON THE DRAWING, CLEANING SHALL BETHOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE,
OIL, FLUX CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING
METHOD AND AGENTS USED SHALL NOT BE INJURIOUS TO ANY PART OR TO THE
ENVIRONMENT, NOR SHALL ANY PART BE CONTAMINATED BY THE CLEANING AGENT.
TOOL FINISH:5.
PHOSPHATE COATING IAW MIL-DTL-16232, TYPE M OR Z, CLASS 3. EXCEPT
THAT NO COATING WEIGHT IS REQUIRED. COLOR MAY NOT BE UNIFORM AND MAY VARY
FROM LIGHT GREY TO BLACK. DIMENSIONS APPLY BEFORE APPLICATION OF FINISH.
OPTIONAL FINISH: BLACK-T COATING, NO. VS 1-3-1-165. W.E. BIRDSONG & ASSOCIATES,
INC.1435 MONTEREY ROAD, FLORENCE, MS. 39073, (601) 939-7448.
6 PERMANENTLY MARK 18894-X200334027-01 IN APPROX AREA SHOWN, IN .25 HIGH
CHARACTERS, IAW MIL-STD-130 USING PAINT IAW MIL-PRF-85285, TYPE I OR TYPE II
REQUIREMENTS, COLOR NO. 37038 (BLACK), IAW FED-STD-595.
M. LAPEE 20040127
E. ZAMORSKI 20040127
M. EVANS 20040127
G. L. HARRIS 20040203FINAL FINAL
REVISIONS
LTR DESCRIPTION DATE APPROVED
B REDRAWN IN SOLIDWORKS UPDATED
SPECIFICATIONS IN THE NOTES. NPW 20230428 4/28/2023 B.C.
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
UNLESS OTHERWISE SPECIFIED
REV
FILENAME:GENERATED USING SOLIDWORKS
D
C
B
A
D
C
B
A
1345678 2
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEETSCALE:
SIZE
TITLE
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONS ANGLESDECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATION AIR FORCE CODE IDENT NO. DRAWING NO.
CURRENT
CODE IDENT NO.
AF FORM
FEB 74 1655
NEXT ASSEMBLY USED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010 .5°
D
X200334027-01B
MATERIAL:
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.
GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:
ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988.
OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE
FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT
IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC.
2751, ET SEQ.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE
SUBJECT TO SEVERE CRIMINAL PENALTIES.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS,
DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS
OR RECONSTRUCTION OF THE DOCUMENT.
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
QUANTITY REQUIRED PER DASH NO.
UNLESS OTHERWISE SPECIFIED
REV
FILENAME:GENERATED USING SOLIDWORKS
EGLIN A.F.B. FL-
18894
D
C
B
A
D
C
B
A
1345678 2
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEETSCALE:
SIZE
TITLE
THIRD ANGLE PROJECTION
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONS ANGLESDECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATION AIR FORCE CODE IDENT NO. DRAWING NO.
CURRENT
CODE IDENT NO.
AF FORM
FEB 74 1655
NEXT ASSEMBLY USED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010 .5°
D
X200334027-01B
MATERIAL:
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.
GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:
ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988.
OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE
FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT
IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC.
2751, ET SEQ.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE
SUBJECT TO SEVERE CRIMINAL PENALTIES.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS,
DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS
OR RECONSTRUCTION OF THE DOCUMENT.
X200334027 B
SPANNER/TORQUE ADAPTER
FMU-139 FUZE RING
X2
B
4X .205
4X .200
C
C
SECTION B-B
SCALE 1 : 1
.030 M A B M
.630
SECTION C-C
SCALE 1 : 1
.030 M A B M
2.000+ .000 .010
2.000+ .000 .010
2.000+ .000 .010
60°
60°
90°
A
A
C
.201+ .005 .001
R.250
2X 1.750 2X .250 R.500
R.063
.790 X 30
.305
SECTION A-A
SCALE 1 : 1
.020 M A C M
3.000
3.225+ .000 .005
2.00 B
A
2X .600+ .005 .000 4X R .120
.507±.004
.507±.004
4X R .03 MAX
2.775+ .005 .000
1/2
OPTIONAL BALL RETENTION DETAIL
SEE OPTIONAL BALL
RETENTION DETAIL
.010 M B M A
.000 M C M
.000 M C M
.030 M A B M
.010 M A B M
0.010 M A B M
.030 M A B M
REVISIONS
LTR DESCRIPTION DATE APPROVED
B SEE SHEET 1. NPW 20230428 4/28/2023 B.C.
REV
FILENAME:GENERATED USING SOLIDWORKS
D
C
B
D
C
B
A
1345678 2
SHEETSCALE:
SIZE AIR FORCE CODE IDENT NO. DRAWING NO.
AF FORM
FEB 74 1655 ENGINEERING DRAWING LAYOUT D
D
X200334027-01B
REV
FILENAME:GENERATED USING SOLIDWORKS
D
C
B
D
C
B
A
1345678 2
SHEET
SIZE AIR FORCE CODE IDENT NO. DRAWING NO.
AF FORM
FEB 74 1655 ENGINEERING DRAWING LAYOUT D
D
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.
GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:
ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988.
OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE
FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT
IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC.
2751, ET SEQ.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE
SUBJECT TO SEVERE CRIMINAL PENALTIES.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS,
DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS
OR RECONSTRUCTION OF THE DOCUMENT.
REV
FILENAME:GENERATED USING SOLIDWORKS
D
C
B
D
C
B
A
1345678 2
SHEETSCALE:
SIZE AIR FORCE CODE IDENT NO. DRAWING NO.
AF FORM
FEB 74 1655 ENGINEERING DRAWING LAYOUT D
D
X200334027-01B
REV
FILENAME:GENERATED USING SOLIDWORKS
18894
D
C
B
D
C
B
A
1345678 2
SHEET
SIZE AIR FORCE CODE IDENT NO. DRAWING NO.
AF FORM
FEB 74 1655 ENGINEERING DRAWING LAYOUT D
D
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.
GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:
ADMINISTRATIVE OR OPERATIONAL USE. DATE: 15 SEPTEMBER 1988.
OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO MMHE
FOCAL POINT, EGLIN AFB, FL 32542-5000.
WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT
IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC.
2751, ET SEQ.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE
SUBJECT TO SEVERE CRIMINAL PENALTIES.
DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS,
DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS
OR RECONSTRUCTION OF THE DOCUMENT.
X2
X200334027 B
| Sheet1 |
| Drawing View4 |
| Sheet2 |
| Drawing View6 |
| Section View B-B |
| Section View C-C |
| Drawing View13 |
| Section View A-A |
| Drawing View16 |
| Drawing View17 |
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