COMBINATION SPANNER WRENCH CAD.pdf

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GBU JDAM Tool Kits
Solicitation number
FA664825Q0024
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About this file

This is an engineering drawing for a U.S. Air Force Wrench Spanner, Combination, with drawing number X9018561. The technical drawing includes three sheets detailing two wrench body variations (-01 and -03) and an assembly drawing. The document specifies the wrench is made from 0.25-inch thick 4130 steel plate, with precision measurements including multiple radii, hole diameters, and specific dimensional tolerances.

Key technical specifications include a phosphate coating per MIL-DTL-16232 (Type M or Z, Class 3), with optional Black-T coating available. The drawing includes detailed workmanship requirements mandating parts be free from defects like burrs, cavities, pits, and other imperfections. Additional notes specify permanent marking requirements, allow for equivalent commercial hardware, and indicate components like dowel pins can be purchased from McMaster-Carr Supply. The drawing is marked with a Distribution Statement C, limiting distribution to U.S. government agencies and their contractors for administrative or operational use.

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Text version

4 2X

3 2X

-01 INTO -10 ASSEMBLY 2B5

-03 INTO -30 ASSEMBLY 3A4

2X .38 2X .38

.63

4.00 5.50

10.00 (-10 ASSY)

16.00 (-30 ASSY)

-10 ASSEMBLY SHOWN

-30 ASSEMBLY AS SHOWN SEE SHEET 3

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.

2. REMOVE ALL BURRS AND SHARP EDGES.

3. DELETED

4. DELETED

5. DELETED

6. WORKMANSHIP:

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 BE THOROUGH 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.

7. DELETED

8. DELETED

9 PERMANENTLY MARK "18894ASSYX9018561-(AND APPROPRIATE DASH NO.)IN

APPROXIMATE AREA SHOWN IN .25 HIGH CHARACTERS IAW MIL-STD-130.

10. FN 2 AND 3 MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE

CODE 0KVE6, PO BOX 740100, ATLANTA GA, 30374-0100.

11. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

12. FINISH: 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 BIRDSON &

ASSOCIATES, INC. 1435 MONTEREY ROAD, FLORENCE, MS. 39073, (601) 939-7448.

REVISIONS

LTR DESCRIPTION DATE APPROVED

D REDRAWN WITHOUT CHANGE. ADDED NOTE 12. ML 20220824 BC

-30 -10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

A/R A/R LOCKING COMPOUND MIL-S-22473 GRADE C 5

2 2 PIN, DOWEL 0KVE6 98385A238 .250 DIA X .625 LG, ALLOY STL, .001 OVERSIZE 1D3 4

2 2 PIN, DOWEL 0KVE6 98385A207 .187 DIA X .625 LG, ALLOY STL, .001 OVERSIZE 1C2 3

1 - WRENCH BODY -03 .25 THK 4130 STL PLATE IAW QQ-S-626 1D2 2

- 1 WRENCH BODY -01 .25 THK 4130 STL PLATE IAW QQ-S-626 1D2 1

APPV

AF FORM 2602 IN MMHE, EGLIN AFB

SIGNATURES ARE ON FILE ON

UNLESS OTHERWISE SPECIFIED

B

U.S. AIR FORCE

APPLICATION

PARTS LIST

SHEET

SIZE

TITLE

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

DR

CHK

ENG

X9018561 D

CURRENT

CODE IDENT NO.

AF FORM

FEB 74 1655

NEXT ASSEMBLY USED ON

.03

.010 .5°

D

X9018561-10-30_D

1 OF

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-

D

C

A

D

C

B

A

1345678 2

U.S. AIR FORCE

APPLICATION

PARTS LIST

SCALE:

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

FRACTIONS ANGLESDECIMALS

.XX±

.XXX±

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

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2022. 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.

WRENCH SPANNER,

COMBINATION

M. LAPEE

1:1

19920320

B. MILLER 19920323

FINAL FINAL 18894

F. ZABOROWSKI 19920323

X

DD

D

THIRD ANGLE PROJECTION

CAD MAINTAINED. CHANGES SHALL

ONLY BE INCORPORATED AT THE

DIRECTION OF THE DESIGN ACTIVITY

USING A COMPATIBLE CAD SYSYTEM.

.75

R1.28

R1.03

2X R.25

12X R .19 (OPTIONAL .19 X 45 )

2X .2497+

.0008 .0000

2X .1876+ .0006 .0000

2X R.19

4X R.25

.84

1.375 1.719

3.781 4.125

4.66

5.50

2.00

3.50

.500 .719

3.281 3.500

4.00

2.

3.

.4

.1

X

9.

X

.0

2.75 2.00

.2

X

6.

8.

7.

.25 (STK)

-01 WRENCH BODY

REVISIONS

LTR DESCRIPTION DATE APPROVED

D SEE SHEET 1. 20220824 BC

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655

D

X9018561-10-30_D

1:1 2 OF 3

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2022. 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.

X9018561 D

CAD MAINTAINED. CHANGES SHALL

ONLY BE INCORPORATED AT THE

DIRECTION OF THE DESIGN ACTIVITY

28 7 6 5 4 3 1

A

B

C

D

A

C

B

R1.03

2X .2497+ .0008 .0000

R.19 2X R.25

4X R.25

12X R.19 (OPTIONAL .19 X 45 ) R1.28

2X .1876+ .0006 .0000

1.25

.84

1.375 1.719 2.00

2.75

3.781 4.125

4.66

5.50

3.50

.500 .719

2.00

3.281 3.500

4.00

2.

3.

.4

5.

.6

.0

X

3.

6.

.0

X

.2

.25 (STK)

-03 WRENCH BODY

REVISIONS

LTR DESCRIPTION DATE APPROVED

D SEE SHEET 1 20220824 BC

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

AF FORM

FEB 74 1655

D

X9018561-10-30_D

1:1 3 OF 3

AF FORM

FEB 74 1655 ENGINEERING DRAWING LAYOUT D

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2022. 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.

X9018561 D

CAD MAINTAINED. CHANGES SHALL

ONLY BE INCORPORATED AT THE

DIRECTION OF THE DESIGN ACTIVITY

28 7 6 5 4 3 1

A

B

C

D

A

C

B

Sheet1
Drawing View8
Drawing View9
Drawing View10
Sheet2
Drawing View6
Drawing View5
Sheet3
Drawing View11
Drawing View12

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