FMU-139 SPANNER-TORQUE ADAPTER CAD.pdf

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GBU JDAM Tool Kits
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FA664825Q0024
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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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