Attachment 2 - Drawings and Specs of all tools.pdf

PDF 4 MB Posted Jul 20, 2022

Attached to: MMHE Tool Procurement Federal contract opportunity
Solicitation number: FA500422Q0030
Issued by: Department of the Air Force Pacific Air Forces

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Attachment 3- MMHE Tool Quantities.xlsx	XLSX spreadsheet	Jul 21, 2022
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Attachment 1 - Clauses and Provisions.pdf	PDF	Jul 20, 2022

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9532906-03_05_H.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN MMHE, EGLIN AFB

APPV

DISTRIBUTION STATEMENT C. DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR CONTRACTORS; ADMINISTRATIVE OR OPERATIONAL USE. 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.) OR THE EXPORT ADMINISTRATION ACT OF 1979 (TITLE 50, U.S.C. , APP.2401 ET SEQ), AS AMENDED. VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE IN ACCORDANCE WITH PROVISIONS OF DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

FMU-152 FUZE RING

SPANNER/TORQUE ADAPTER

9532906 H

FINAL FINAL

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

H REDRAWIN WITH CHANGE. ADDED (6) VIEWING

SLOTS. 20131119 R.P. MILLER

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

3. ALL DIMENSIONS APPLY AFTER PLATING.

4. MATERIAL: 3.25 DIAMETER, SST BAR 17-4PH, ASTM A564 OR SAE-AMS-5643. HEAT TREAT TO TENSILE STRENGTH CONDITION OF H1150 (Rc 26 – 36) IAW SAE-AMS-6875. PASSIVATE IAW SAE-AMS-QQ-P-35.

5. PERMANENTLY MARK “18894-9532906-(AND APPROPRIATE DASH NO.), USING INK, IAW A-A-56032, TYPE I, AND

COVER WITH CLEAR LACQUER IAW MIL-L-10287, TYPE II, IAW MIL-STD-130

6. STENCIL AS NOTED APPROXIMATELY WHERE SHOWN IN .25 HIGH CHARACTERS USING INK, IAW A-A-56032, TYPE I, AND COVER WITH CLEAR LACQUER IAW MIL-L-10287, TYPE II. .

7. 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.

8. NOTED DIMENSIONS IN SECTION B-B AND D-D TO BE HELD FOR FULL LENGTH OF TABS.

Z.FIELDING 960724

D. WOLFE 960822

E. ZAMORSKI 960823

D. CARBONNEAU 970319

T. GIOVANNI 970319 1 / 1

MATERIAL :

DETAIL -03

DETAIL -05

(34 - INCH DRIVE) (12 - INCH DRIVE)

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

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.). OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED (TITLE 50, U.S.C., APP. 2401, ET SEQ.) VIOLATIONS OF THESE EXPORT CONTROL LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATE OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25.

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

H SEE SHEET 1 20131119 R.P. MILLER

9532906 H

SECTION A -A

SECTION B-B

O 2.770 +.002 -.000

.228 +.000 -.0052X

.2502X

.600 +.010 +.0002X

O 3.240

O 2.760 +.005 -.000 l .010 M A B M l O .010 M A B M l O .010 M A

120° 1.040sO

.438

.750

.188 +.005 +.001

3.00R .450

R .250

A (TWO SURFACES)

1.7502X

B 60°

60°

2.000 +.000 +.010

2.000 +.000 -.010

.753 +.005 -.000

R .034X l .010 M A B M l .010 M A B M l .010 M A B M l .000 M C M l .000 M C M

C l O .010 M A B M

4X R

R .0636X

1 / 1

DETAIL -03

MAX

TORQUE

600 FT LBS

FMU-152

1.046X

1.406X.626X

R .3112X

60°6X

VIEW E-E

18894-9532906-XX

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

DESTRUCTION NOTICE - FOR UNCLASSIFIED, LIMITED DOCUMENTS, DESTROY BY ANY METHOD THAT WILL PREVENT

DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

9532906 H

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

H SEE SHEET 1 20131119 R.P. MILLER

SECTION C-C

SECTION D -D

O 2.770 +.002 -.000

.228 +.000 -.0052X

4X R l O .010 M A B M

O 3.240

O 2.760 +.005 +.000

.600 +.010 -.0002X l O .010 M A B l O .010 M A B M l .010 M A B M

.2502X

.790sO120°

.305

.750

3.00

1.7502X

.188 +.005 -.001

R .250

R .450

R .0636X

A (TWO SURFACES)

2.000 +.000 +.010

2.000 +.000 -.010

.507 ±.004

2.000 +.000 -.010

60°

60° l .010 M A B M

C l .000 M C M l .000 M C M l .010 M A B M l .010 M A B M

R .034X

1 / 1

DETAIL -05

MAX

TORQUE

600 FT LBS

FMU-152

1.046X

1.406X.626X

R .3112X

60°6X

X9018561-10_C.dft

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON

AF FORM 2602 IN MMHE, EGLIN AFB

APPV

WRENCH

SPANNER, COMBINATION

X9018561 C 1/1

FINAL FINAL

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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.

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5M-1994.

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX.

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 “18894-X9018561-(AND APPROPRIATE DASH NO.) IN

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

2 2X

2X3

A/R A/R LOCKING COMPOUND MIL-S-22473 GRADE C 1D3 4

2 2 PIN, .001 OVERSIZE OKVE6 98385A207 .187 DIA X .625 LG, ALLOY STL 1C2 3

2 2 PIN, .001 OVERSIZE OKVE6 98385A238 .25 DIA X .625 LG. ALLOY STL 1D3 2

1 1 SPANNER WRENCH BODY -01/-03 .25 THK 4130 STL PLATE IAW QQ-S-626 1D3 1

-30 -10 NOMENCLATURE CAGE IDENTIFYING NO. MATERIAL/SPECIFICATION ZN FN

.332X .382X

10.00 (-10 ASSY)

16.00 (-30 ASSY)

5.50 4.00

.62

-10 ASSEMBLY SHOWN

-30 ASSEMBLY AS SHOWN

SEE SHEET 3

2 B

3 B

ALL SHEETS ARE

SAME REVISION

M LAPEE 19920320

-01 INTO -10 ASSEMBLY

-03 INTO -30 ASSEMBLY

B. MILLER 19920323

F ZABOROWSKI 19920323

REDRAWN WITH CHANGE. DELETED NOTES 3, 4, 5,

7, 8. ADDED NOTE 9. IN THE PARTS LIST FIND NO 2

WAS SCREW, CAP MADE FROM NAS 1352-6-20;

FIND 3 WAS SCREW, CAP MADE FROM NAS1352-

4H16;FIND NO 4 WAS SEALING COMPOUND, MIL-S-

22473 GRADE H.

20070509 EJZ

C THE IDENTIFYING NUMBER FOR FN 2 WAS

9838A238 NPW 20120419 20120419 BTC

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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.

2.252X

4.47 3.222X

6.692X 7.062X

8.292X 9.16

9.622X 10.002X

.84 1.375

.75 .50

.719

2.562

1.719

2.75

3.78 4.12

4.66 5.50

3.812

2.0622.750

2.00 3.28

3.50 4.00

3.000

.25 (STK)

2X O.1876-.1882

14X R.19 OPTIONAL 45v X .192X O .2505-.2497

2.00

3.50

-01 WRENCH BODY

3.002X

4X R.25

X9018561 1/1

RR2X R.25

5.50

7.88

REVISIONS

LTR DESCRIPTION DATE APPROVED

B SEE SHEET 1 NPW 20070430 20070509 EJZ

C SEE SHEET 1 NPW 20120419 20120419 BTC

ENGINEERING DRAWING LAYOUT D1655

FEB 74

FORMAF

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE SHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE FILENAME:

REV

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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.

.25 (STK)

.50 .719

2.00 3.28

3.50

4.00

3.000 2.562

.75

.84 1.375

1.719

2.75 2.00

3.503.78 4.12

4.66

5.50

2.252X 3.0002X

4.47

15.6252X 16.002X

.38

2.75

3.8122.06

3.222X

14.292X 15.16

R .1914X OPTIONAL 45v X .19

R .254X

R .252X R R

2X O .2505-.2497

2X O.1876-.1882

X9018561 1/1

6.692X 13.072X

5.50

13.88

-03 WRENCH BODY1

REVISIONS

LTR DESCRIPTION DATE APPROVED

B SEE SHEET 1 NPW 20070430 20070509 EJZ

C SEE SHEET 1 NPW 20120419 20120419 BTC

AIR FORCE RELEASE D

ENGINEERING DRAWING LAYOUT D

USED ONNEXT ASSEMBLY

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

9330783-10_OE.dft

BOMB LIFTING BAR ASSEMBLY,

UNIVERSAL

X9330783 E 1 / 4

M. LAPEE 940329

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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 AAC/WMOM, 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.

2. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

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

4. AFTER INSTALLATION OF CARGO RING (FIND NO. 6) APPLY PRIMER CONFORMING TO MIL-P- 53022, TYPE I OR II TO A DRY FILM THICKNESS OF .0005 TO .0009 AND FINAL COAT WITH

PAINT CONFORMING TO MIL-PRF-85285, TYPE I OR II TO A DRY FILM THICKNESS OF .0017

TO .0024, COLOR NO. 24052 (GREEN) IAW FED-STD-595. OMIT PRIMER APPLICATION STEP

IF CARGO RING IS ALREADY PRIMED OR PRIMED AND PAINTED.

5. PERMANENTLY MARK 18894ASSYX9330783-10 IN APPROXIMATE AREA SHOWN, IN .25 HIGH

CHARACTERS, IAW MIL-STD-130.

6. TORQUE NUT (FIND NO. 13) TO 31 FOOT POUNDS ± 3 POUNDS.

7. PRIOR TO TIGHTENING NUTS (FIND NO. 13) ENSURE THAT PINS (FIND NO. 8) CAN BE INSERTED

THROUGH BOTH SIDES OF FRAME (FIND NO. 1) AND LUG BLOCK (FIND NO. 4).

8. APPLY RETAINING COMPOUND (FIND NO. 14) TO THREADS OF CARGO RING AND SCREW (FIND

NO.S 6 AND 15) BEFORE INSTALLING. FINAL POSITION OF CARGO RING SHALL BE INLINE

WITH FRAME (FIND NO. 1).

9. STENCIL “MAX CAPACITY 6000 POUNDS”, IN 1.00 HIGH GOTHIC CHARACTERS, IN

APPROXIMATE AREA SHOWN USING INK CONFORMING TO A-A-208, TYPE II COLOR NO 37038

OR PAINT CONFORMING TO MIL-PRF-85285, TYPE I OR II COLOR NO 37038 (BLACK) IAW

FED-STD-595.

F. ZABOROWSKI 940405

M. EVANS 940711

CIT

Y P

OF 2

AR RETAINING COMPOUND MIL-S-22473 GRADE C 14

10 NUT, HEX, LOCKING M45913/1-6CS6 .375-16UNC-2B, CRES, NON-METALIC LOCK 13

20 WASHER, FLAT NAS1149C0663R .375 NOM ID X .063 THK, CRES 12

10 BOLT, HEX HEAD ASME B18.2.1-1996 .375-16UNC-2A X 2.75 LG, DG 5, ZINC PLATE 11

5 LANYARD WITH TAB 83014 LW1023-1-12.00 10

1 PIN, QUICK RELEASE MS17990C840 .500 NOM DIA X 4.00 GRIP LGT, CRES 9

2 PIN, QUICK RELEASE MS17990C622 .375 NOM DIA X 2.20 GRIP LGT, CRES 8

2 PIN, QUICK RELEASE MS17990C1038 .625 NOM DIA X 3.80 GRIP LGT, CRES 7

1 RING, CARGO TIE DOWN MS21237-1B 6

1 SHACKLE 9330792-01 5

2 LUG BLOCK 9330787-01 4

2 SPACER BAR 9330786-01 3

1 LIFTING EYE 9330785-012 2

2 FRAME 9330784-01 1

-10 NOMENCLATURE CODE

IDENT

IDENTIFYING NO. MATERIAL/SPECIFICATION ZONE FIND

NO.

-10 BOMB LIFTING BAR ASSY

(SEE SHEET 2)

10. EACH BOMB LIFTING BAR ASSEMBLY SHALL BE SUBJECTED TO A PROOF LOAD TEST

BEFORE INITIAL ACCEPTANCE OR AFTER ANY STRUCTURAL REPAIRS HAVE BEEN

PERFORMED

A TOTAL PROOF LOAD OF 12000 – 12010 POUNDS SHALL BE EVENLY DISTRIBUTED

BETWEEN THE TWO LUG BLOCKS, (FIND NO. 4) IN THE 30-INCH LUG POSITION AND THE

ASSEMBLY IS SUSPENDED FORM THE CARGO RING (FIND NO. 6). APPLY LOAD FOR A MINIMUM

OF 10 MINUTES.

ANY EVIDENCE OF PERMANENT DEFORMATION OR BREAKAGE OF ANY COMPONENT DURING

OR AFTER THE APPLICATION OF THE PROOF LOAD SHALL BE CAUSE TO REJECT THE BOMB

LIFTING BAR ASSEMBLY. A REJECTED BOMB LIFTING BAR ASSEMBLY SHALL NOT BE USED

FOR ANY PURPOSE UNTIL THE DISCREPANCIES ARE CORRECTED AND THE PROOF LOAD IS

SUCCESSFULLY COMPLETED.

11. THE FOLLOWING NATIONAL STOCK NUMBERS ARE PROVIDED AS A REFERENCE:

FIND NO. NSN

6 1670-01-092-9236

10 4010-00-065-8877 11 5305-00-781-3926 12 5310-00-167-0821 15 5305-00-984-6193

E E REV REV STATUS

2 1 SHT OF SHEETS

3 SCREW, MACH, PAN-HD MS35206-245 .164-32UNC-2A X .50, CROSS-RECESS, STL 15

REVISIONS

LTR DESCRIPTION DATE APPROVED

D REDRAWN WITH CHANGE ML 20021026 20021212 M. EVANS

IN NOTE 11, CHANGED NSN FOR F/N 6; IN P/L, F/N 7

WAS MS17990C1037 3.70 GRIP LGT, F/N 8 WAS

MS17990C0622, F/N 9 WAS MS17990CO840 AND F/N

13 WAS M45913/1-6CS6N. ML 20050714

20050714 M. EVANS

DRAWING NO.AIR FORCE CODE IDENT NO.SIZE

SCALE OFSHEET

28 7 6 5 4 3 1

18894

GENERATED USING SOLID EDGE V12.00 FILENAME:

REV

9330783-10_OE.dft

X9330783 E 2 1 / 4

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

MAX CAPACITY 6000 POUNDS

CIT

Y P

1 2X

3 2X

4 2X

82X

10 5X

11 10X

12 20X

13 10X

-10 BOMB LIFTING BAR ASSEMBLY

7 2X

15 3X

9 BOTH SIDES

REVISIONS

LTR DESCRIPTION DATE APPROVED

D REDRAWN WITH CHANGE ML 20021026 20021212 M. EVANS

E SEE SHEET 1. ML 20050714 20050714 M. EVANS

USED ONNEXT ASSEMBLY

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330784-01_OC.dft

FRAME

X9330784 C 11 / 2

M. LAPEE 940329

9330783 9330783

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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 AAC/WMOM, 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.

SECTION A-A

7.5002X

8.0002X

14.5002X

1.0002X 1.0752X

7.000

29.000

28.500

5.500 20.500

2.000

2.002X

10.002X

12.502X

3.002X

1.122X

1.562X

5.252X

20.00

9.50

F. ZABOROWSKI 940405

M. EVANS 940711

.500 (STK)

R .25

R .252X

O .406 +.006 -.0016X

O .406 +.006 -.0014X

R .258X

R .508X

R .254X l O .030 M A B C l O .030 M A B C l O .030 M A B C

.3752X

9.50

44.00

MATERIAL:

ALUM ALLOY PLATE

7075-T651 IAW QQ-A-250/12

.500 THICK

4.75

1.000

O .379 .3754X

2. REMOVE ALL BURRS AND SHARP EDGES .03 MAX.

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

TO THE PART(S) OR THE ENVIRONMENT. PRETREAT WITH CHEMICAL CONVERSION COATING

IAW SAE-AMS-2473. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM

THICKNESS WITH EPOXY PRIMER, IAW TO MIL-P-53022, TYPE I OR II. PAINT ALL PRIMED

SURFACES .0017 TO .0024 DRY FILM THICKNESS WITH PAINT IAW MIL-PRF-85285., TYPE I

OR II, COLOR NO. 24052 (GREEN) IAW FED-STD-595.

4. WORKMANSHIP:

ALL PARTS SHALL BE IN THE CONDITION SPECIFIED BY THE DRAWINGS AND SHALL BE FREE

DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX

CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD

5. PERMANENTLY MARK “18894-X9330784-01” IN APPROX AREA SHOWN, IN .25 HIGH

6. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

3.000

REVISIONS

LTR DESCRIPTION DATE APPROVED

B REDRAWIN WITH CHANGE ML 20021018 20021212 M. EVANS

C ADDED DIM 3.000 (ZN A5) ZF 20040107

USED ONNEXT ASSEMBLY

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330785-01_OB.dft

LIFTING EYE

X9330785 B 11 / 2

M. LAPEE 940329

9330783 9330783

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

B REDRAWN WITH CHANGE. ML 20021017

F. ZABOROWSKI 940405

M. EVANS 940711

MATERIAL:

ALUM ALLOY PLATE

7075-T651 IAW QQ-A-250/12

1.00 THICK

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 AAC/WMOM, 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.

5.5002X

3.0002X 3.5002X

1.0001.0008X

2.0002X

3.0629X

4.752X

9.002X

11.562X

10.00

2.00

8.00

R .252X 1.000 (STK)

R .252X

O .531 +.006 -.0019X

O .406 +.006 -.0014X l O .030 M A B C l O .030 M A B C

2X R .25 R MAX

2. REMOVE ALL BURRS AND SHARP EDGES .03 MAX

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

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

INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. PRETREAT WITH CHEMICAL

CONVERSION COATING IAW SAE-AMS-2473. PRIME ALL EXTERIOR SURFACES

.0005 TO .0009 DRY FILM THICKNESS WITH EPOXY PRIMER, IAW TO MIL-P-53022,

TYPE I OR II. PAINT ALL PRIMED SURFACES .0017 TO .0024 DRY FILM THICKNESS

WITH PAINT IAW MIL-PRF-85285., TYPE I OR II, COLOR NO. 24052 (GREEN) IAW FED-

STD-595.

5. PERMANENTLY MARK “18894-X9330785-01” IN APPROXIMATE AREA SHOWN, IN .25

HIGH CHARACTERS, IAW MIL-STD-130.

USED ONNEXT ASSEMBLY

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330786-01_OB.dft

SPACER BAR

X9330786 B 11 / 2

M. LAPEE 940329

9330783 9330783

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

B REDRAWIN WITH CHANGE. ML 20021017

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 AAC/WMOM, 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.

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

TO THE PART(S) OR THE ENVIRONMENT. PRETREAT WITH CHEMICAL CONVERSION COATING

IAW SAE-AMS-2473. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM

THICKNESS WITH EPOXY PRIMER, IAW TO MIL-P-53022, TYPE I OR II. PAINT ALL PRIMED

DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX

CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD

5. PERMANENTLY MARK “18894-X9330786-01” IN APPROX AREA SHOWN, IN .25 HIGH

F. ZABOROWSKI 940405

M. EVANS 940711

14.500

7.500

1.0002X

1.000

2.00

16.50

1.25

9.50

R .50

R .255X

1.000 (STK)

R .252X

O .406 +.006 -.0013X l O .030 M A B C

.375

ISOMETRIC VIEW

MATERIAL:

ALUM ALLOY PLATE

6061-T6511 IAW QQ-A-250/11

1.00 THICK

USED ONNEXT ASSEMBLY

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330787-01_OC.dft

LUG BLOCK

X9330787 C 11 / 1

M. LAPEE 940329

9330783 9330783

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

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 AAC/WMOM, 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.

F. ZABOROWSKI 940405

M. EVANS 940711

MATERIAL:

ALUM ALLOY PLATE,

6061-T651 IAW QQ-A-250/11

2.00 THICK

.5982X

2.06

3.75

4.75

2.002X

.875

R .064X

C l .030 M A B M C

O .630 +.000 -.0052X

1.7502X

1.125 1.250

3.50

1.93

3.25

4.25

.312X

135°2X

R .254X

R .502X

O .468 +.006 -.001

2X .164-32UNC-2B `.50 MIN

l O .030 M A B M C O .006 M

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

B1.3M, SYSTEM 21.

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

IAW SAE-AMS-2473. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM

THICKNESS WITH EPOXY PRIMER, IAW TO MIL-P-53022, TYPE I OR II. PAINT ALL PRIMED

5. WORKMANSHIP:

DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX

CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD

6. PERMANENTLY MARK “18894-X9330787-01” IN APPROX AREA SHOWN, IN .25 HIGH

7. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

1.750

LTR DESCRIPTION DATE APPROVED

B REDRAWN WITH CHANGE. ML 20021031 20021212 M. EVANS

ZN C3, ADD 1.750: ZN D2, 2X .164-32UNC-2B DP .50 MIN WAS

.164-32UNC-2B THRU; ZN D3, 2X 1.750 WAS 1.750. ZF 20040107

USED ONNEXT ASSEMBLY

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

GENERATED USING SOLID EDGE V12.00 FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

ENGENG

APPV

UNLESS OTHERWISE SPECIFIED CONTRACT NUMBER

FO8635-01-C-0002

SIGNATURES ARE ON FILE ON AF

FORM 2602 IN AAC/EDSC, EGLIN AFB

X9330792-01_OA.dft

SHACKLE

X9330792 A 11 / 1

9330783 X9330783

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

A REDRAWIN WITH CHANGE ML 20021031

2.00

1.25 1.09

3.59

2.25

3.75

1.000

3.252X

O .505 .5002X

A C

2X .164-32UNC-2B X `.50

l O .030 M A M B O .010 M

8X R .06 -.25

1.125-12UNF-2B X` 1.00 MIN FULL THD

l O .030 M B C M A M

MATERIAL:

ALUM ALLOY RECT BAR

2024-T351, QQ-A-225/6

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 AAC/WMOM, 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.

F. ZABOROWSKI 940711

M. EVANS 940711

Z. FIELDING 940516

1.002X

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

B1.3M, SYSTEM 21.

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

IAW SAE-AMS-2473. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM

THICKNESS WITH EPOXY PRIMER, IAW TO MIL-P-53022, TYPE I OR II. PAINT ALL PRIMED

DRAWING, CLEANING SHALL BE THOROUGH TO REMOVE ALL DIRT, CHIPS, GREASE, OIL, FLUX

CHEMICAL DEPOSITS, RESIDUES, AND OTHER FOREIGN MATTER. THE CLEANING METHOD

6. PERMANENTLY MARK “18894-X9330792-01” IN APPROX AREA SHOWN, IN .25 HIGH

7. ALL DIMENSIONS APPLY BEFORE APPLICATION OF COATING.

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

CONTRACT NUMBER:

FO8635-01-C-0002

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON

AF FORM 2602 IN MMHE, EGLIN AFB

APPV

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 AAC/YBCM, 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.

X20057663-10.dft

MAC TORQUE RETAINER

ASSEMBLY

X20057663 1:4

N. PELICAN 20050901

FINAL FINAL

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

LTR DESCRIPTION DATE APPROVEDNOTES:

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. PERMANENTLY MARK “18894ASSYX20057663-10” IN APPROX AREA SHOWN, IN .25 HIGH CHARACTERS, IAW MIL-STD-130.

4. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

5. APPLY LOCKING COMPOUND MIL-S-22473, GRADE C TO THREADS ON ( FIND NO 9 ) PRIOR TO

INSTALLATION.

6. TIGHTENING – TORQUE VALUES FOR SPECIFIED HARDWARE:

FIND NO TORQUE VALUE

7 35-45 FT LB

9 30-35 IN LB

7. THE FOLLOWING NATIONAL STOCK NUMBERS ARE PROVIDED AS A REFERENCE:

FIND NO NSN

7 5310-01-905-0243

1 ASSEMBLY, 20 INCH STRAP 4

1 ASSEMBLY, 34 INCH STRAP 20057667-30 5

2 CLAMP 20057666-01 3

2 SCREW, THUMB, WING HEAD OKVE6 90196A720 .500-13 UNC-2B X 2.00 LONG 8

1 BEAM 20057664-01 6061-T6 EXT CHANNEL ALUM ASSOC 4.00 X 2.331 LB/FT 1

4 NUT, HEX, LOCKING M45913/1-8CG5 .500-13 UNC 2B, STL, ZINC PLT 7

2 U-BOLT OKVE6 8896T85 U-BOLT CRES 3.00 ID X .500-13 UNC-2B WITH 2 NUTS 6

-10 NOMENCLATURE CAGE IDENTFYING NO MATERIAL / SPECIFICATION ZN FN

MAC A/E 32K-9

MAC A/E 32K-3

74X

6 2X

BACKING PLATE IS

PART OF U-BOLT (ITEM 7)

82X

32X

2 2X

9 2X1

2 NUT PLATE 20057665-01 CRES STEEL FLAT 300 SERIES 3.50 X .50 2

2 SCREW, FLAT HEAD 82 DEG OKVE6 91771A539 CRES STEEL .250-20 UNC-2B X .625 LNG 9

20057667-10

M. LAPEE 20060222

J. MARKLE 20061019

BRYAN PRICE 20061026

J. MARKLE 20061019

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

CONTRACT NUMBER:

FO8635-01-C-0002

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON

AF FORM 2602 IN MMHE, EGLIN AFB

APPV

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 AAC/YBCM, 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.

X20057664-10.dft

BEAM

X20057664 1:2

N. PELICAN 20050901

20057663 20057663

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

2. PERMANENTLY MARK “18894-X20057664-01” IN APPROXIMATE AREA SHOWN IN .12 HIGH CHARACTERS IAW MIL-

STD-130.

3. REMOVE ALL BURRS AND SHARP EDGES .03 MAX.

CLEANING AGENT.

5. FINISH:

CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. PRETREAT WITH CHEMICAL CONVERSION COATING IAW SAE-AMS-2473. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM THICKNESS WITH EPOXY PRIMER, IAW TO MIL-PRF-85582, TYPE I OR II.

PAINT ALL PRIMED SURFACES .0017 TO .0024 DRY FILM THICKNESS WITH PAINT IAW MIL-PRF-85285., TYPE I OR II, COLOR NO. 24052 (GREEN) IAW FED-STD-595.

30.62

2.25 (STK)

4.00 (STK)

.29 (STK)

.19 (STK)

O .2812X sO.500 X 82v

O .531 +.008 -.0018X

.502X 4.55 2X

3.50 2X

7.80 2X

2.77 2X

2.00 10X

MATERIAL:

6061-T6 EXT

CHANNEL, ALUM ASSOC

4.0 X 2.331 LB/FT

2 FAR SIDE

DETAIL -01

M. LAPEE 20060222

J. MARKLE 20061019

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

CONTRACT NUMBER:

FO8635-01-C-0002

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON

AF FORM 2602 IN MMHE, EGLIN AFB

APPV

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 AAC/YBCM, 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.

X20057665-10.dft

NUT PLATE

X20057665 1:1

N. PELICAN 20050901

20057663 20057663

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

2. PERMANENTLY MARK “18894-X200057665-01” IN APPROXIMATE AREA SHOWN IN .12 HIGH CHARACTERS IAW MIL-

STD-130.

3. WORKMANSHIP:

CLEANING AGENT.

4. REMOVE ALL SHARP EDGES AND BURRS .03 MAX

5. PASSIVATE IAW SAE AMS-QQ-P-35, TYPE II OR VII.

6. SCREW THREADS SHALL CONFORM TO FED-STD-H28/2, AND BE INSPECTED IAW ANSI/ASME B1.3M, SYSTEM 21.

.50 (STK)

5.55

2X .500-13 UNC-2A

.250-20 UNC-2A

.50

2.27

4.55

2X .12 X 45v

MATERIAL:

CRES STEEL, .500 THK

300 SERIES

3.39

1.683X

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

CONTRACT NUMBER:

FO8635-01-C-0002

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON

AF FORM 2602 IN MMHE, EGLIN AFB

APPV

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 AAC/YBCM, 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.

X20057666-01.dft

CLAMP

X20057666 2:1

N. PELICAN 20050901

20057663 20057663

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

2. REMOVE ALL BURRS AND SHARP EDGES .03 MAX

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

4. PERMANENTLY MARK “18894-X20057666-01” IN APPROXIMATE AREA SHOWN IN .12 HIGH CHARACTERS, IAW MIL-STD-130.

5. CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE INJURIOUS TO THE

PART(S) OR THE ENVIRONMENT. PRETREAT WITH CHEMICAL CONVERSION COATING IAW SAE-AMS-2473.

PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM THICKNESS WITH EPOXY PRIMER, IAW TO MIL-PRF-85582, TYPE I OR II CLASS N. PAINT ALL PRIMED SURFACES .0017 TO .0024 DRY FILM THICKNESS WITH PAINT IAW MIL-PRF-85285, TYPE I OR II, COLOR NO. 24052 (GREEN) IAW FED-STD- 595.

2.00

(STK)

.75

(STK)

3.50

.54

1.04

1.00

.2702X

1.25

2.75

R .50

3.00

1.48

2X R

2.00 (STK)

DETAIL -01

MATERIAL:

ALUM ALLOY, RECT

BAR OR PLATE, .75 X 2.00

6061-T6

USED ONNEXT ASSEMBLY

FEB 74

FORMAF

CODE IDENT NO.

CURRENT

DRAWING NO.AIR FORCE CODE IDENT NO.AIR FORCE AUTHENTICATION

ENG

CHK

.XXX±

.XX±

DECIMALS ANGLESFRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

THIRD ANGLE PROJECTION

TITLE

SIZE

SCALE: SHEET

PARTS LIST

APPLICATION

U.S. AIR FORCE

28 7 6 5 4 3 1

18894

- EGLIN A.F.B. FL

CONTRACT NUMBER:

FO8635-01-C-0002

GENERATED USING SOLID EDGE FILENAME:

REV

UNLESS OTHERWISE SPECIFIED

QUANITY REQUIRED PER DASH NO.

SIGNATURES ARE ON FILE ON

AF FORM 2602 IN MMHE, EGLIN AFB

APPV

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 AAC/YBCM, 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.

X20057667-10.dft

ASSEMBLY, STRAP

X20057667 1:2

N. PELICAN 20050901

20057663 20057663

.5°.010 .03

CAD MAINTAINED. CHANGES SHALL ONLY BE

INCORPORATED AT THE DIRECTION OF THE DESIGN

ACTIVITY USING A COMPATIBLE CAD SYSTEM.

REVISIONS

LTR DESCRIPTION DATE APPROVED

2. ALL MACHINE STITCHING SHALL BE IAW FED-STD-751 USING NYLON THREAD (FIND NO. 3), 4

TO 6 STITCHES PER INCH. STITCHING TO BE BACK STITCHED AT LEAST .50 INCH. STITCH

CONFIGURATION IS OPTIONAL.

3. FUSE ALL EXPOSED ENDS OF NYLON WEBBING TO PREVENT FRAYING. AVOID FORMING

SHARP EDGES.

4. KNOWN SUPPLIER – MCMASTER-CARR SUPPLY COMPANY

PO BOX 740100

ATLANTA, GEORGIA 30374-0100

PHONE: (404) 346-7000

FAX: (404) 349-9091

5. KNOWN SUPPLIER – TRANSTECHNOLOGY CORPORATION BREEZE

DIV BREEZE – EASTERN

700 LIBERTY AVENUE

UNION NJ 07083-8198

NSN # 8305-00-782-6734 REFERENCE

6. PERMANENTLY MARK AS “18894X20057667-(AND APPROPRIATE DASH NO) , USING .25 HIGH

GOTHIC CHARACTERS IN APPROXIMATE AREA SHOWN IAW MIL-STD-130, USING INK IAW AA-

59291-4, TYPE IV, COLOR (BLACK)

7. WORKMANSHIP:

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.

2.50 2X

3.702X MIN

(DIM A) (SEE TABLE)

1.718 (STK)

2 HOOK, SNAP OKVE6 3648T93 2100 LB CAPACITY, 2.00 WIDE WEBBING 1

1 STRAP, NYLON -01 STRAP, NYLON 1.718 WIDE X .06 - .10 THICK IAW MIL-W-4088 2

-10/-30 NOMENCLATURE CAGE IDENTFYING NO MATERIAL / SPECIFICATION ZN FN

DASH NO DIM. A ±.25 DIM. B ±.25

-10 19.75 12.25 -30 33.50 26.25

(DIM B) (SEE TABLE)

-01

-03

-10 ASSEMBLY

-30 ASSEMBLY

1 STRAP, NYLON -03 STRAP, NYLON 1.718 WIDE X .06 - .10 THICK IAW MIL-W-4088 3

M. LAPEE 20060222

J. MARKLE 20061019

N. P. WIGGINS 20070215

LTR DESCRIPTION DATE APPROVED

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

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).

M.LAPEE 20070215

B. CHAMBLISS 20070215

E. ZAMORSKI 20070509

J. MARKLE 20070509

08-16-18 BTC

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

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±

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°

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

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±

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°

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…

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