FUZE WELL THREAD CHASER CAD.pdf

N. P. WIGGINS 20070215

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

NOTE 3, MATERIAL WAS 3.50 DIA 4340 ... ASTM A322

HEAT TREAT TO RC-40. NOTE 4 WAS: PERMANENTLY

MARK" 18894-X20075022-01". ADDED HEAT TREAT

CHART , REVISED SHT 2. NPW 20160613

06-14-16 BTC

B

ADDED NOTE 7, HEAT TREAT TO RC 58. WAS: -01 HEAT

TREAT TO RC50, -03 HEAT TREAT TO RC58, -05 HEAT

TREAT TO RC65. REVISED SHT 2. DDH 20180803

C IN THE NOTES, ADDED NOTE 8. NPW 20181023 20181023 BTC

2:1

NOTES:

INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.1.

REMOVE ALL BURRS AND SHARP EDGES .06 MAX2.

MATERIAL: 3.50 DIA 01 ANNEALED ROUND BAR, STEEL, ASTM A686, HEAT TREAT 3.

PER CHART BELOW AFTER MACHINING.

4 PERMANENTLY MARK 18894-X20075022-01 IN APPROX AREA SHOWN, IN .125 HIGH

CHARACTERS, IAW MIL-STD-130.

5. 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.

6. SCREW THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE INSPECTED IAW

ANSI/ASME B1.3M, SYSTEM 21.

7. TREATMENT:

HEAT TREAT TO HARDNESS OF RC 58, PER MIL-H-6875H.

8. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE

INJURIOUS TO THE PART(S) OR THE ENVIRONMENT, NOR SHALL ANY PART BE

CONTAMINATED BY THE CLEANING AGENT. APPLY DRY FILM LUBRICANT IAW

MIL-L-46147B, CAGE CODE 81349. THE FILM APPEARANCE AND THICKNESS SHALL BE

UNIFORM IN COLOR AND SHALL BE SMOOTH, FREE OF ANY CRACKS, SCRATCHES,

PINHOLES, BLISTERS, BUBBLES, RUNS, SAGS, FOREIGN MATTER, GRIT, ROUGH

PARTICLES, SEPARATION OF INGREDIENTS OR OTHER SURFACE IMPERFECTIONS. THE

THICKNESS OF THE CURED FILM SHALL BE BETWEEN .008 AND .013mm (.0003 AND

.0005 INCH).

FINAL FINAL

M.LAPEE 20070215

B. CHAMBLISS 20070215

E. ZAMORSKI 20070509

J. MARKLE 20070509

08-16-18 BTC

X2

C

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

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

X20075022 -01-C

WELL

DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

OR RECONSTRUCTION OF THE DOCUMENT.

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

MATERIAL:

X20075022

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

MATERIAL:

OR RECONSTRUCTION OF THE DOCUMENT.

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

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

X20075022 -01-C

DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS,

SUBJECT TO SEVERE CRIMINAL PENALTIES.

2751, ET SEQ.). VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE

IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC.

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,

THREAD CHASE TOOL, FUZE

C

DETAIL -01

.075 X 65°

2.88

12X .11

65°

REVISIONS

LTR DESCRIPTION DATE APPROVED

A

IN ZONE D-7: THE NUMBER OF CUTOUTS WAS 6. ZN B-

6, CHANGED CHAMFER FROM .09 X 45 TO .063 X 65

N.P WIGGINS 20160613.

06-14-16 BTC

B

CONSOLIDATION OF VIEWS. OVERALL PART LENGETH

INCREASED FROM 3.25 TO 4.50. ZONE D-7,

CHANGED CUTOUT FROM 12X .25 TO 12X .375. ZONE

D-1, CHANGED DIAMETER FROM 3.13 TO 3.27. ZONE

D-3, CUT OUT DIA AND DEPTH CHANGED FROM 2.00

2.00 TO 2.38 3.50. CHAMFER ON BOTTOM OF

PART CHANGED FROM .25 X 45 TO .13 X 45 .

DDH 20180803

C SEE SHEET 1. NPW 20181023 10/23/201

8 BTC

2:1

DETAIL -01

08-16-18 BTC

B

3.500-12 UNS-1A

MAJOR DIA 3.4981 + 0000/-.0172

MINOR DIA 3.3959 MAX

PITCH DIA 3.4440 + .0000/-.0097

.09 X 45

2X .188

.375

1.151

2.31

2.80

.75

4.50

1.00

.13 X 45°

AA

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

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

X20075022 -01-C

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.

REV

FILENAME:GENERATED USING SOLIDWORKS

18894

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

X20075022 -01-C

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

X20075022

D

C

C

.507±.005

.507±.005

.254

.254

3X 2.000

6X 60°

12X 30°

12X .19

12X .375

12X R

SECTION A-A

SCALE 2 : 1

3.50

R.09 MAX

R.06

2.80

3.27

2.38 3.50

4X R.03+ .00 .03

DETAIL B

SCALE 4 : 1

12X

.075