COMBINATION SPANNER WRENCH CAD.pdf
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- Attached to
- GBU JDAM Tool Kits
- Solicitation number
- FA664825Q0024
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 |
File details come from the government source that posted it. Updated .