BOMB TURNER TOOL CAD.pdf
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- GBU JDAM Tool Kits
- Solicitation number
- FA664825Q0024
About this file
This document is an Air Force engineering drawing for a mechanical component, specifically a -10 assembly with multiple detailed parts including handles, bands, links, and mounting hardware. The technical drawing provides comprehensive manufacturing specifications, including dimensional tolerances (±.03 inches, ±.010 inches, ±0.5°), material requirements (cold finished steel, neoprene rubber), and strict workmanship standards that mandate parts be free from defects like corrosion, cracks, dents, burrs, and other surface imperfections.
The drawing includes specific assembly instructions, such as applying threadlock compound, transferring hole locations, and permanently marking the assembly with an identification number. The document is marked with a Distribution Statement C, authorizing distribution to U.S. government agencies and contractors for administrative or operational use, with a date of 01 April 2016. The technical drawing follows standards including ASME Y14.100, ASME Y14.5M-2018, and includes notes about welding (ANSI/AWS D1.1/D1.1M-2020), surface preparation, and painting specifications using military standard primers and color guidelines.
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27.63
8.88
D
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
QUANITY 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
1 3 4 5 6 7 82
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEET SCALE:
SIZE
TITLE
THIRD ANGLE PROJECTION
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONSANGLES DECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.
CURRENT
CODE IDENT NO.
AF
FORM
FEB 741655
NEXT ASSEMBLYUSED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010
X20168517-10_A
OF
D
.5°
MATERIAL:
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
QUANITY 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
1 3 4 5 6 7 82
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEET SCALE:
SIZE
TITLE
THIRD ANGLE PROJECTION
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONSANGLES DECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.
CURRENT
CODE IDENT NO.
AF
FORM
FEB 741655
NEXT ASSEMBLYUSED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010
OR RECONSTRUCTION OF THE DOCUMENT.X20168517 A
1:2
.5°
X20168517-10_A
MATERIAL:
BOMB TURNER TOOL
OF
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.
GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:
ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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
X20168517 A
M. LAPEE 20160407
REVISIONS
LTRDESCRIPTIONDATEAPPROVED
ANOTE 1 WAS.... ASME Y14.100 AND ASME Y14.5M
2010. ML 2022070520220705B.
CHAMBLISS
-10NOMENCLATURECAGEIDENTIFYING NOMATERIAL / SPECIFICATIONZONEFN
1THREADLOCK COPOUND0KVE691458A11LOCTITE NO. 222MS, PURPLE12
1PRIMER, THREADLOCK0KVE67614A16LOCTITE 7649(N) 1.75 OZ BOTTLE11
9SCREW, FH, 82 DEGREE0KVE690585A227.164-32UNC-2A X .44 LG, CRES10
ARADHESIVE0KVE675045A783M 2216 FLEXIBLE EPOXY9
1SCREW, HEX HD CAP0KVE691257A593.312-18UNC-2A X 2.50 LG, STEEL, GRADE 8, ZINC PLT8 2SCREW, HEX HD CAP0KVE691257A594.312-18UNC-2A X 3.25 LG, STEEL, GRADE 8, ZINC PLT7
3NUT, HEX LOCKING0KVE697135A220.312-18UNC-2B, .344 HGT,STEEL, ZINC PLT6
6WASHER, FLAT0KVE691922A223.312 ID X .734 OD X .06 THK, STEEL, ZINC PLT5
1PAD20168521-01 4
1BAND20168520-01 3
2LINK20168519-01 2
1HANDLE WELDMENT20168518-101
NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-2018.
2. 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.
3 TRANSFER HOLE LOCATIONS FROM BAND, (FIND NO. 3) TO PAD (FIND NO. 4) AND DRILL .177 DIA HOLE AND COUNTERBORE .375 DIA X .12 DEEP. INSTALL PAD USING ADHESIVE (FIND NO. 9) AND SCREWS (FIND
NO. 10).
4 MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE 0KVE6, PO BOX 740100, ATLANTA GA, 30374-0100.
5 PERMANENTLY MARK 18894ASSYX20168517-10 IN APPROX AREA SHOWN, IN .125 HIGH CHARACTERS, IAW
MIL-STD-130.
6. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.
7 APPLY LOCKING COMPOUND PRIMER (FIND NO. 11) AND LOCKING COMPOUND (FIND NO. 12) TO THE THREADS ON SCREW (FIND NO. 10) IAW MANUFACTURERS INSTRUCTIONS PRIOR TO INSTALLATION.
2X
FINAL FINAL
N. P. WIGGINS 20160814
W.A. SHIREY 20160816
B.CHAMBLISS 20160817
JAMIE HARBERT 20160817
CAD MAINTAINED. CHANGES SHALL
ONLY BE INCORPORATED AT THE
DIRECTION OF THE DESIGN ACTIVITY
USING A COMPATIBLE CAD SYSTEM.
2X
9X
2X
3X
-10 ASSEMBLY
53X
3.47
HANDLE WELDMENT
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
QUANITY 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
1 3 4 5 6 7 82
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEET SCALE:
SIZE
TITLE
THIRD ANGLE PROJECTION
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONSANGLES DECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.
CURRENT
CODE IDENT NO.
AF
FORM
FEB 741655
NEXT ASSEMBLYUSED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010.5°
D
X20168518-10_A
1:21OF2
MATERIAL:
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
QUANITY 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
1 3 4 5 6 7 82
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEET SCALE:
SIZE
TITLE
THIRD ANGLE PROJECTION
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONSANGLES DECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.
CURRENT
CODE IDENT NO.
AF
FORM
FEB 741655
NEXT ASSEMBLYUSED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010.5°
D
X20168518-10_A
1:21OF2
MATERIAL:
X20168518 A OR RECONSTRUCTION OF THE DOCUMENT.
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.
GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:
ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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
X20168518 A
4X
.88
2X.332
2X
1.82
M. LAPEE 20160407
REVISIONS
LTRDESCRIPTIONDATEAPPROVED
A
NOTE 1 WAS....ASME Y14.100 AND ASME Y14.5M-
1994. NOTE 3 WAS....ANSI/AWS D1.1/D1.M-2010.
NOTE 5 WAS CHANGED TO CLARIFY PAINT. ML
20220705
20220705B.
CHAMBLISS
-10NOMENCLATURECAGEIDENTIFYING NOMATERIAL / SPECIFICATIONZONEFN
2PIVOT-03STEEL, COLD FINISHED C1018, .25 X .752
1HANDLE-01PIPE, STEEL; 1 IPS (1.315 OD) X SCHED 40 (1.049 ID);
ASTM A-531
NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-2018.
2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX.
3. WELD IAW ANSI/AWS D1.1/D1.1M-2020.
4. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.
5. UNLESS OTHERWISE SPECIFIED: PRIMER ALL EXTERIOR SURFACES AND EDGES IAW MIL
-PRF-23377, TYPE II, CLASS C1, C2 OR N. PAINT ALL PRIMED SURFACES IAW MIL-PRF
-85285, TYPE II, COLOR GRAY, COLOR NO. 26173 IAW FED-STD-595.
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.
20168517 20168517
COAXIAL WITHIN .020
2 PLACES
B.CHAMBLISS 20160817
W.A. SHIREY 20160816
N.P. WIGGINS 20160814
JAMIE HARBERT 20160817
CAD MAINTAINED. CHANGES SHALL
ONLY BE INCORPORATED AT THE
DIRECTION OF THE DESIGN ACTIVITY
USING A COMPATIBLE CAD SYSTEM.
OR RECONSTRUCTION OF THE DOCUMENT.
X20168518 A
REV
FILENAME: GENERATED USING SOLIDWORKS
18894
D
C
B
D
C
B
A
1 3 4 5 6 7 82
SHEET SCALE:
SIZEAIR FORCE CODE IDENT NO.DRAWING NO.
AF
FORM
FEB 741655ENGINEERING DRAWING LAYOUT D
D
X20168518-10_A
1/22OF2
REV
FILENAME: GENERATED USING SOLIDWORKS
18894
D
C
B
D
C
B
A
1 3 4 5 6 7 82
SHEET
SIZEAIR FORCE CODE IDENT NO.DRAWING NO.
AF
FORM
FEB 741655ENGINEERING DRAWING LAYOUT D
D
2OF2
REV
FILENAME: GENERATED USING SOLIDWORKS
18894
D
C
B
D
C
B
A
1 3 4 5 6 7 82
SHEET SCALE:
SIZEAIR FORCE CODE IDENT NO.DRAWING NO.
AF
FORM
FEB 741655ENGINEERING DRAWING LAYOUT D
D
X20168518-10_A
2OF2
REV
FILENAME: GENERATED USING SOLIDWORKS
18894
D
C
B
D
C
B
A
1 3 4 5 6 7 82
SHEET
SIZEAIR FORCE CODE IDENT NO.DRAWING NO.
AF
FORM
FEB 741655ENGINEERING DRAWING LAYOUT D
D
2OF2
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.
GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:
ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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 X20168518 A
3.00
1.32(STK)
1.05(STK)
SCALE 1 : 2
17.75
2X .03 X 45°
.25(STK)
1.38
R.38
1.250
.75(STK)
2X .332
.332 THRU
2X .38
REVISIONS
LTRDESCRIPTIONDATEAPPROVED
ASEE SHEET 1.20220705B.
CHAMBLISS
DETAIL -03
DETAIL -01
SCALE : 2/1
CAD MAINTAINED. CHANGES SHALL
ONLY BE INCORPORATED AT THE
DIRECTION OF THE DESIGN ACTIVITY
4:1
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
QUANITY 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
1 3 4 5 6 7 82
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEET SCALE:
SIZE
TITLE
THIRD ANGLE PROJECTION
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONSANGLES DECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.
CURRENT
CODE IDENT NO.
AF
FORM
FEB 741655
NEXT ASSEMBLYUSED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010.5° .5°
4:1OF 1
D
1 OF
D
C1018
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
QUANITY 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
1 3 4 5 6 7 82
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEET SCALE:
SIZE
TITLE
THIRD ANGLE PROJECTION
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONSANGLES DECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.
CURRENT
CODE IDENT NO.
AF
FORM
FEB 741655
NEXT ASSEMBLYUSED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010
X20168519-01_A
LINK
OR RECONSTRUCTION OF THE DOCUMENT.X20168519 A
X20168519-01_A
MATERIAL:
COLD FINISHED STEEL
MATERIAL:
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.
GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:
ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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
X20168519 A
CAD MAINTAINED. CHANGES SHALL
ONLY BE INCORPORATED AT THE
DIRECTION OF THE DESIGN ACTIVITY
USING A COMPATIBLE CAD SYSTEM.
.38
3.53
M. LAPEE 20160407
REVISIONS
LTRDESCRIPTIONDATEAPPROVED
ANOTE 1 WAS ........ASME Y14.100 AND ASME Y14.5-
2009. ML 202207057/5/2022 NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.
2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX
3. 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.
4. UNLESS OTHERWISE SPECIFIED: PRIMER ALL EXTERIOR SURFACES AND EDGES IAW
MIL-PRF-23377, TYPE II, CLASS C1, C2 OR N. PAINT ALL PRIMED SURFACES IAW
MIL-PRF-85285, TYPE II, COLOR GRAY, COLOR NO. 26173 IAW FED-STD-595.
20168517 20168517
B.CHAMBLISS 20160817
W.A. SHIREY 20160816
N. P. WIGGINS 20160814
JAMIE HARBERT 20160817
.332
R1.06
2X
R1.81
2X R.38
2.78
1.39
.38
1.81
2X 2.34
9X .88
OF
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
QUANITY 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
1 3 4 5 6 7 82
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEET SCALE:
SIZE
TITLE
THIRD ANGLE PROJECTION
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONSANGLES DECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.
CURRENT
CODE IDENT NO.
AF
FORM
FEB 741655
NEXT ASSEMBLYUSED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010
1:1 X20168520-01_A
.5°
D 1 1:12
OR RECONSTRUCTION OF THE DOCUMENT.
OF
C1018
APPV
AF FORM 2602 IN MMHE, EGLIN AFB
SIGNATURES ARE ON FILE ON
QUANITY 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
1 3 4 5 6 7 82
U.S. AIR FORCE
APPLICATION
PARTS LIST
SHEET SCALE:
SIZE
TITLE
THIRD ANGLE PROJECTION
DIMENSIONS ARE IN INCHES-TOLERANCES ON:
FRACTIONSANGLES DECIMALS
.XX±
.XXX±
DR
CHK
ENG
AIR FORCE AUTHENTICATIONAIR FORCE CODE IDENT NO.DRAWING NO.
CURRENT
CODE IDENT NO.
AF
FORM
FEB 741655
NEXT ASSEMBLYUSED ON
ENGINEERING DRAWING LAYOUT D
AIR FORCE RELEASE
.03
.010
DX20168520 A
.5°
BAND
X20168520-01_A
MATERIAL:
COLD FINISHED STEEL
MATERIAL:
DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.
GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:
ADMINISTRATIVE OR OPERATIONAL USE. DATE: 01 APRIL 2016. 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
X20168520 A
M. LAPEE 20160407
REVISIONS
LTRDESCRIPTIONDATEAPPROVED
A
NOTE 1 WAS ....ASME Y14.100 AND ASME Y14.5-1994.
NOTE 3 WAS ....ANSI/AWS D1.1/D1-1M -98. NOTE 5
WAS CHANGED TO CLARIFY PAINT. ML 20220705
20220705B.
CHAMBLISS
NOTES:
1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-2019.
2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX.
3. WELD IAW ANSI/AWS D1.1/D1.1M-2020.
4. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.
5. UNLESS OTHERWISE SPECIFIED: PRIMER ALL EXTERIOR SURFACES AND EDGES
IAW MIL-PRF-23377, TYPE II, CLASS C1, C2 OR N. PAINT ALL PRIMED SURFACES
IAW MIL-PRF-85285, TYPE II, COLOR GRAY, COLOR NO. 26173 IAW FED-STD
-595.
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. SEE SHEET 2 FOR FLAT PATTERN.
20168517 20168517
B.CHAMBLISS 20160817
W.A. SHIREY 20160816
N. P. WIGGINS 20160814
JAMIE HARBERT 20160817
CAD MAINTAINED. CHANGES SHALL
ONLY BE INCORPORATED AT THE
DIRECTION OF THE DESIGN ACTIVITY
USING A COMPATIBLE CAD SYSTEM.
A
ASECTION A-A
9X .164-32UNC-2B
2X 60°
2X 35°
2X 45°
DETAIL -01
.19
2.44
2X 45°
R4.25
2X R.25
1.22
.188
1.75
2X .19
SCALE 1 : 2
.19
.19 2X
2X R.12
11X .09 PILOT HOLES
.88
.79
5.14
7.03
9.31
12.72
19.55
22.96
25.24
27.14
31.48
16.14
X20168520-01_A
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LTRDESCRIPTIONDATEAPPROVED
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BLEMISHES, BURRS, CAVITIES, PITS, VOIDS,CORROSION, CRACKS, DENTS,
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