X201516570_10 AIM-9X MAINTENANCE TABLE Drawing 5 May 2022.pdf

NP WIGGINS 20180322

AIM-9X MAINTENANCE TABLE

X201516570

X2

NOTES:

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

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

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. PERMANENTLY MARK 18894ASSYX201516570-10 IN APPROX AREA SHOWN, IN .25 HIGH CHARACTERS, MINIMUM IAW MIL-STD-130.

5. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

6. MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE 0KVE6, PO BOX 740100, ATLANTA

GA, 30374-0100.

7. APPLY LOCKING COMPOUND PRIMER (FIND NO. 39) AND LOCKING COMPOUND (FIND NO. 40) TO

THREADS ON SCREW (FIND NOS. 17, 18, 26, 29, 31, 32 AND 37.) IAW MANUFACTURERS

INSTRUCTION PRIOR TO INSTALLATION.

8. MATCH DRILL .196 THRU LOWER SHELF (FIND NO. 7 AND 8) THRU ONE WALL OF TUBE OF FWD AND

AFT END WELDMENT (FIND NO. 1 AND 2). INSTALL RIVET (FIND NO. 20).

9. POSITION DRAWER (FIND NO. 24) TO BE MOUNTED UNDER TOP TUBE OF AFT END WELDMENT (FIND NO. 1) APPROXIMATELY AS SHOWN. MATCH DRILL AND THREAD .250-20 UNC-2B (6 PLACES) TO

MOUNT DRAWER.

10. TRANSFER .281 DIA HOLES AT EACH END OF SLIDE ASSEMBLY (FIND NO. 5) THRU TABLE TOP (FIND NO. 6) AND THRU ONE WALL OF FWD AND AFT END WELDMENTS (FIND NO. 1 AND 2). THE HOLES

IN THE END WELDMENTS ARE TO BE .250-20 UNC-2B.

11. TRANSFER HOLES FROM TABLE TOP (FIND NO. 6) END WELDMENTS (FIND NO. 1 AND 2) . HOLES IN TABLE TOP ARE .281 DIA. ; HOLES IN END WELDMENTS ARE .250-20 UNC-2B THREAD THRU ONE WALL ONLY.

12. FINAL ASSEMBLY MAY REQUIRE SHIMMING UNDER TABLE TOP (FIND NO. 6) TO ACQUIRE A FLATNESS OF .010 OVER THE ENTIRE AREA OF BOTH TABLE TOPS. SHIM AS REQUIRED BETWEEN TABLE TOP AND TOP OF END WELDMENT USING STAINLESS STEEL SHIM STOCK OF VARRING THICKNESSES AT

FASTENER LOCATIONS.

13. TO DOCUMENT THE ACTUAL DAY, MONTH AND YEAR OF COMPLETING THE ACCEPTANCE TEST

(SEE NOTE 14), STENCIL, “PROOFLOADED (ddmmyyyy)” IN THE APPROXIMATE AREA SHOWN IN .50 HIGH CHARACTERS USING PAINT IAW MIL-PRF-85285, TYPE II REQUIREMENTS, COLOR NO.

37038 (BLACK) IAW FED-STD-595.

14. PRODUCTION ACCEPTANCE TEST:

EACH AIM-9X MAINTENANCE TABLE SHALL BE SUBJECTED TO A PROOF LOAD TEST PRIOR TO INITIAL ACCEPTANCE OR AFTER ANY STRUCTURAL REPAIRS HAVE BEEN PERFORMED. A PROOF LOAD OF 400 LBS SHALL BE EVENLY DISTRIBUTED ON THE SLIDE ASSEMBLY. TO ACHIVE THIS THE TOP HALF OF THE RING ASSEMBLIES ( FN 4) MUST BE REMOVED AND ITEM 3 MOVED AGAINST THE END STOPS OF ITEM 5. EVENLY DISTRIBUTED THE WEIGHT ACROSS THE FIVE RING CRADLE ASSEMBLIES (FN 5). THE LOAD SHALL BE APPLIED

FOR FIVE MINUTES MINIMUM.

ANY EVIDENCE OF PERMANENT DEFORMATION OR BREAKAGE OF ANY COMPONENTS DURING OR AFTER THE APPLICATION OF THE PROOF LOAD SHALL BE CAUSE FOR REJECTION OF THE AIM-9X MAINTENANCE TABLE.

A REJECTED AIM-9X MAINTENANCE TABLE SHALL NOT BE USED FOR ANY PURPOSE UNTIL THE DISCREPANCIES

ARE CORRECTED AND THE PROOF LOAD TEST HAS BEEN SUCCESSFULLY COMPLETED.

15. PRIOR TO ASSEMBLY, PAINT THE INSIDE AND OUTSIDE OF THE DRAWER ASSEMBLY (FIND NO 24). CLEAN PART(S) USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT BE INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. PRIME ALL EXTERIOR SURFACES .0005 TO .0009 DRY FILM THICKNESS WITH EPOXY PRIMER, IAW MIL-DTL-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. 26173 (GRAY) IAW FED-STD-595.

16. PRIOR TO INSTALLATION OF GROUNDING STATIONS (FIND NO. 38) REMOVE THE 10 FOOT CORD FROM THE BACK OF THE STATION. APPLY CONDUCTIVE GREASE (FIND NO. 35) TO THE CENTER LUG OF THE STATION AN TO BOTH SIDES OF THE COPPER WASHER (FIND NO. 40) AND TO THE UNDER SIDE FO THE GROUNDING BAR (FIND NO. 10) IN THE LOCATION WHERE THE GROUNDING STATION WILL BE LOCATED, SEE DETAIL G, POSITION GROUNDING STATION (FIND NO. 38) UNDER THE GROUNDING BAR APPROXIMATELY AS SHOWN.

MATCH DRILL AND THREAD .190-20 UNF-2B (2 PLACES) PLACE COPPER WASHER BETWEEN STATION CENTER

TAB AND GROUNDING BAR AND INSTALL USING SCREWS (FIND 41). SEE VIEW GG.

17. AT INSTALLATION, SECURE THE ALIGNMENT TUBE (FIND NO. 41) IN TWO RING CRADLE ASSEMBLIES (FIND NO. 4). ADJUST THE SHIM, PART OF CRADLE, GUIDANCE UNIT (FIND NO. 3) UNTIL THE ADJUSTING TUBE

MAKES CONTACT WITH THE LOWER ROLLERS OF THE CRADLE, GUIDANCE UNIT.

18. ONLY ONE ALIGNMENT TUBE (FIND NO. 41)IS REQUIRED FOR EACH PRODUCTION RUN.

FINAL FINAL

M. LaPEE 20180404

19. CRADLE/SLIDE STORAGE BARS ARE USED FOR STORAGE PURPOSES ONLY. TO REMOVE UN NEEDED CRADLES, REMOVE THE SCREW FROM THE END OF THE SLIDE ASSEMBLY (FIND NO 5) AND SCREW THE STORAGE BAR (FIND NO 42) ON TO THE END OF THE SLIDE ASSEMBLY AND SLIDE THE UN NEEDED CRADLES ON TO THE BARS, UNSCREW THE BARS AND STORE FOR LATER USE.

20 CUT WIRE FLUSH WITH THE BACK SIDE OF THE GROUNDING STATION AND DISCARD WIRE.

21 USE FN 41, ALIGNMENT TUBE, SECURED IN FN 4, RING CRADLE ASSEMBLY OF THE FIRST TWO PIECES ON THE TABLE AS SHOWN ON SHEET 2. FN 3, CRADLE, GUIDANCE UNIT NEEDS TO BE ADJUSTED UP OR DOWN UNTIL THE BOTTOM ROLLERS OF THE GCU ALIGN WITH THE ALIGNMENT TUBE. DRAWING NUMBER X201516576 USES FN 16 SHIM, ROUND, PEEL-AWAY FOR THIS ADJUSTMENT. AFTER ADJUSTMENT THE GCU UNIT SHOULD EASILY SLIDE OVER THE ALIGNMENT TUBE WITH THE BOTTOM ROLLERS ON THE GCU JUST BEING IN CONTACT WITH

THE BOTTOM ROLLERS.

B. CHAMBLISS 20210120

B. CHAMBLISS 20210120

BUSCAVAGE 20210120

DELETED

REVISIONS

LTR DESCRIPTION DATE APPROVED

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

2 CRADLE/SLIDE STORAGE

BAR 20187561-10 2D6 42

1 ALIGNMENT TUBE 20187566-01 2C3 41

A/R THREADLOCK COMPOUND 0KVE6 91458A11 LOCTITE 22221 .34 OZ BOTTLE PURPLE 2D4 40

A/R THREADLOCK PRIMER 0KVE6 7614A16 LOCTITE 7649(N) 1.75 OZ BOTTLE 2D4 39

2 WASHER, FLAT 0KVE6 93744A120 COPPER, .203 ID X.500 OD .047 THK 4C6 38

4 SCREW, PAN HD 0KVE6 91772A830 CRES 18-8 .190-32 UNF 2A X .625 LG 4C3 37

4 SPACER 0KVE6 94639A761 .625 OD X .266 ID X .75 LG, NYLON 2B5 36

2 GROUNDING STATION 0KVE6 72555K66 4 BANANA JACKS 2B4 35

2 GROUNDING BRAID 0KVE6 69925K11 .06 THK X .875 WD X 30.00 LG 4 AWG COPPER, WITH

LUGS 2C6 34

A/R GREASE, CONDUCTIVE 0KVE6 1219K57 SYNTHETIC 85% SILVER 2B6 33

4 SCREW, PAN HD 0KVE6 91735A539 .250-20UNC X .625 LG CRES 2B4 32

20 SCREW, FLAT HD 0KVE6 91771A551 .250-20UNC X 2.25 LG CRES 2C6 31

2 HANDLE, PULL 0KVE6 1651A100 4.50 LG 1.06PROJECTION, ALUMINUM, BOLT ON 2B4 30

5 SCREW, PAN HD 0KVE6 91772A544 .250-20UNC X 1.25 LG CRES 2B2 29

4 WASHER, FLAT 0KVE6 92141A031 .406 ID X .875 OD X .050 THK CRES 2B5 28

1 CHAIN 0KVE6 3596T24 .19 DIA X 12.00 STL ZINC PL 3B7 27

12 SCREW, MACHINE, PAN HD 0KVE6 91772A557 .250-20UNC-2A X .50 LG, CRES 3B3 26

2 GROUNDING REEL 0KVE6 7223K15 20 FT CABLE, .50 CLAMP .09 GALV. CABLE 2C6 25

2 DRAWER 0KVE6 4772T46 20.00 WD X 20.00 DP X 6.00 HGT, STL, TRAY AND LOCK 2B4 24

56 NUT, HEX, LOCKING 0KVE6 94945A205 .250-20UNC, NYLON INSERT, GR 8 STL ZINC PL. 3B6 23

56 SCREW, MACHINE, PAN HD 0KVE6 91735A544 .250-20UNC X 1.25 LG, CRES 2C6 22

117 WASHER, FLAT 0KVE6 92141A029 .281 ID X .625 OD X .050 THK CRES 2C6 21

52 RIVET, BLIND, SEALING 0KVE6 97524A117 .188 DIA, .375-.500 GP LGT, ALUM 2C6 20

4 NUT, HEX, LOCKING 0KVE6 95615A140 .375-16UNC-2B, NYLON INSERT, STL ZINC PL. 2B5 19

4 SCREW 0KVE6 92198A639 .375-16 UNC-2A X 3.50 LG, CRES 2B5 18

24 SCREW, CAP HEX HD 0KVE6 92865A621 .375-16UNC X .625 LG GR 5 STL, ZINC PL. FULL THD 3B6 17

28 WASHER, FLAT 0KVE6 92141A030 .344 ID X .75 OD X .05 THK CRES 3C2 16

16 SPACER 0KVE6 94639A179 .625 OD X .266 ID X 1.00 LG, NYLON 2C6 15

6 CASTER, POLYURETHANE 0KVE6 9854T42 4.12-5.12 HT, 1000 LB CAP, LEVELING, DUAL WHEEL, SWIVEL 2A3 14

2 EDGE GUARD 201516581-02 2C3 13

2 EDGE GUARD 201516581-01 2C5 12

2 GROUNDING BAR

CONNECTOR 201516583-01 2B6 11

2 GROUNDING BAR 201516582-01 2C6 10

2 GROUNDING BAR 201516582-03 2B5 9

1 LOWER SHELF, FORWARD 201516599-01 2B6 8

3 LOWER SHELF 201516580-01 2B3 7

2 TABLE TOP 201516594-01 2B3 6

1 SLIDE ASSEMBLY 201516588-10 2C3 5

5 RING CRADLE ASSEMBLY 201516592-10 2C3 4

1 CRADLE, GUIDANCE UNIT 201516576-10 2C3 3

1 FORWARD END WELDMENT 201516572-10 2D6 2

1 AFT END WELDMENT 201516571-10 2B3 1

APPV

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-

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PARTS LIST

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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

X201516570_10_0

1:16 1 OF 4

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 07 JULY 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

OR RECONSTRUCTION OF THE DOCUMENT.

SCALE 1 : 8

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REVISIONS

LTR DESCRIPTION DATE APPROVED

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FILENAME:GENERATED USING SOLIDWORKS

18894

D

C

B

D

C

B

A

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SHEETSCALE:

SIZE AIR FORCE CODE IDENT NO. DRAWING NO.

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FEB 74 1655 ENGINEERING DRAWING LAYOUT D

D

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18894

D

C

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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: 07 JULY 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,

27.26

44.62

34 REF

133.27

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BB

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E

F

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36 4X REF

164X

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FILENAME:GENERATED USING SOLIDWORKS

18894

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C

B

D

C

B

A

1345678 2

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AF FORM

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18894

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C

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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: 07 JULY 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,

G

G

HH

DETAIL F

SCALE 1 : 2

3C3

SECTION G-G

SCALE 1 : 2

SECTION H-H

SCALE 1 : 2

37 4X

352X

9 2X

X201516570

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REVISIONS

ZONE REV. DESCRIPTION DATE APPROVED

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

X201516570_10_0

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18894

D

C

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D

C

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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: 08 JULY 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,

16X

92X

4 3X

3 2X

82X 2 4X

62X

SEE DETAIL -13

3B3

72X

SEE DETAIL -15

4D7

NP WIGGINS 20180322

AFT END WELDMENT

X201516571

X2

NOTES:

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

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

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

ANSI/ASME B1.3M, SYSTEM 21.

4. 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.

5. FINISH: 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. WELD IAW ANSI/AWS D1.1/D1.1M-2010.

7. ALL SEALED TUBE ASSEMBLIES SHALL HAVE A .25 DIAMETER WEEP/DRAIN HOLE TO

PERMIT CONDENSATION DRAINAGE.

SEE DETAIL -01

3D6

SEE DETAIL -17

4B7

201516570 201516570

SEE DETAIL -03

4C4

SEE DETAIL -07

3A4

SEE DETAIL -21

3C3

SEE DETAIL -11

3B3

SEE DETAIL -05

3B7

M. LaPEE 20180404

BUSCAVAGE 20210120

B. CHAMBLISS 20210120

B. CHAMBLISS 20210120

REVISIONS

LTR DESCRIPTION DATE APPROVED

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

2 TUBE, VERTICAL, END -21 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1B4 9

2 CASTER PAD, END -17 .50 THK ASTM A36 STL PLT 1C5 8

2 END CAP -15 .19 THK, ASTM A-36 STL SHT 1C5 7

2 TUBE, VERTICAL, END -13 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1D5 6

1 TUBE, LOWER END -11 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1C5 5

3 TUBE, TOP -07 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1C1 4

2 TUBE, END CENTER -05 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1B1 3

4 TUBE, SPACER -03 .75 OD X .375 ID DOM TUBE 1C1 2

6 TUBE, SIDE, LONG -01 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1B5 1

APPV

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-

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

X201516571_10_0

1:4 1 OF 4

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 07 JULY 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,

20.00

66.00

25.83

.25 4X

.25 4X

4 SURFACES.020

.25

4X

.25

.25 2X

.25

.25 2X

.25

.25 4X

.25 2X

.25

.25 4X

.25

.25 4X

.25 2X

20.00

22.50

4X 8.00

7.09

.25 G

4X

.19 4X

.12 G

.12 G

4X

.25

.25 G

4X

.25

.25 4X

.25 6X

.25 6X

2X

X201516571

X2

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516571_10_0

1:4 2 OF 4

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: 07 JULY 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,

1.50 (STK)

.25 (STK)

63.00

DETAIL -01

1B5

1.50 (STK)

1.50 (STK)

.25 (STK)

17.00

SCALE 1 : 2

DETAIL -05

1C2

20.000

2X 45°

SCALE 1 : 2

DETAIL -07

1C2

1.50 (STK)

1.50 (STK)

.25 (STK)

SCALE 1 : 2

25.500

2X 45°

SCALE 1 : 2

DETAIL -11

1D6

1.50 (STK)

1.50 (STK)

.25 (STK)

2X .25

20.500

45°

DETAIL -13

1B6

1.50 (STK)

1.50 (STK)

.25 (STK)

10.250

45°

22.000

7.09 .75

4X .766+ .010 .001

1.50(STK)

1.50(STK)

.25(STK)

X2

X201516571

DETAIL -21

1B3

SCALE: 1:2

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516571_10_0

1:4 3 OF 4

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: 07 JULY 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,

R.50

1.75

1.25

SCALE: 1 : 1

.19 (STK)

.44

1.94

3.000 3.88

.44

1.94 3.000

3.88

.766+ .010 .001

SCALE 1 : 1

4X .375-16UNC-2B

.50 (STK)

.75 (STK)

.390+ .006 .001

SCALE: 2 : 1

1.50

2X .12 X 45°

X2

X201516571

DETAIL -15

1B3

DETAIL -17

1C6

DETAIL -03

1C1

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516571_10_0

1:4 4 OF 4

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: 07 JULY 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,

16X

82X

62X

92X

72X

2 4X

SEE DETAIL -01

3D6

SEE DETAIL -23

4B3

SEE DETAIL -03

4D5

SEE DETAIL -21

3C2

SEE DETAIL -07

3A4

SEE DETAIL -05

3B6

4 3X

3 2X

NP WIGGINS 20180322

FOWARD END WELDMENT

X201516572

X2

NOTES:

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

2. REMOVE ALL BURRS AND SHARP EDGES.

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

ANSI/ASME B1.3M, SYSTEM 21.

4. 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. CLEAN PART(S) USING CLEANING METHODS

AND AGENTS, WHICH SHALL NOT BE INJURIOUS TO THE PART(S) OR THE ENVIRONMENT

5. FINISH: 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. WELD IAW ANSI/AWS D1.1/D1.1M-2010.

7. ALL SEALED TUBE ASSEMBLIES SHALL HAVE A .25 DIAMETER WEEP/DRAIN HOLE

TO PERMIT CONDENSATION DRAINAGE.

SEE DETAIL -17

4A7

SEE DETAIL -15

4C7

SEE DETAIL -13

3A2

SEE DETAIL -11

3B2

201516570 201516570

-10 ASSEMBLY

M. LaPEE 20180404

B. CHAMBLISS 20210120

B. CHAMBLISS 20210120

BUSCAVAGE 20210120

REVISIONS

LTR DESCRIPTION DATE APPROVED

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

1 CASTER PAD, CENTER -23 .50 THK ASTM A-36 STL PLT 1B1 10

2 TUBE, VERTICAL END -21 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1B3 9

2 CASTER PAD, END -17 .50 THK ASTM A36 STL PLT 1C5 8

2 END CAP -15 .19 THK, ASTM A-36 STL SHT 1C5 7

2 TUBE, VERTICAL, END -13 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1D5 6

1 TUBE, LOWER END -11 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1C5 5

3 TUBE, TOP -07 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1C1 4

2 TUBE, END CENTER -05 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1B1 3

4 TUBE, SPACER -03 .75 OD X .375 ID DOM TUBE 1C1 2

6 TUBE, SIDE, LONG -01 1.50 X 1.50 X .25 THK, ASTM A-500, GR B 1B5 1

APPV

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-

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

X201516572_10_0

1:4 1 OF 4

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 07 JULY 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,

26.00

67.94

3.00

.75 AREA FREE OF PAINT AND PRIMER

(FAR SIDE)

.19 4X

22.500

4X 8.00

.25 4X

.25

.25 2X

.25

.25

.25 8X

.25

.25 2X

.25

.25 12X

.25 2X

.25 2X

7.09

20.00

.020

.25

.25 4X

.25

.25 4X

4X

.25

.25 4X

.12 8X

.25 2X

.25 6X

X201516572

X2

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516572_10_0

1:4 2 OF 4

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: 07 JULY 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,

1.50 (STK) .25 (STK)

63.00

SCALE 1 : 4

DETAIL -01

1B4

1.50 (STK)

1.50 (STK)

.25 (STK)

17.00

SCALE 1 : 2

DETAIL -05

1B1

20.000

2X 45°

SCALE 1 : 2

1.50 (STK)

1.50 (STK)

.25 (STK)

45°

22.000

7.09 10.250

.75

2X .766+ .010 .001

SCALE 1 : 2

DETAIL -21

1B3

1.50(STK)

1.50(STK)

.25(STK)

25.500

2X .25

2X 45°

SCALE 1 : 2

DETAIL -11

1D5

1.50 (STK)

1.50 (STK)

.25 (STK)

20.500

45°

SCALE 1 : 2

DETAIL -13

1D5

DETAIL -07

1C1

1.50 (STK)

1.50 (STK)

.25 (STK)

X2

X201516572

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516572_10_0

1:4 3 OF 4

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: 07 JULY 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,

1.25

1.75

4X R .50

.19 (STK)

SCALE 1 : 1

.75 (STK) .390+

.006 .001 2X .12 X 45°

1.50

SCALE 2 : 1

.438 3.000

1.94

3.88

.438

1.94

3.000 3.88

.766+ .010 .001

4X 0.375-16 UNC-2B

SCALE 1 : 1

.50 (STK)

2X .766+ .010

.001 THRU

3.88

.438 .438

1.500 3.000

.438 3.000

1.500

13.00 26.00

1.500

3.000

SCALE 1 : 2

.250-20UNC-2B

8X .375-16UNC-2B

.50 (STK)

X2

X201516572

DETAIL -15

1C5

DETAIL -03

1C1

DETAIL -17

1C5

DETAIL -23

1B2

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516572_10_0

1:4 4 OF 4

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: 07 JULY 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,

.093

.56

.052

.208

.75 (STK)

.31

.44

(.312-18UNC-2A)

NP WIGGINS 20180322

SHOULDER BOLT

X201516573

X2

NOTES:

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

2. REMOVE ALL BURRS AND SHARP EDGES.

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

ANSI/ASME B1.3M, SYSTEM 21.

4. 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.

5. MAKE FROM McMASTER CARR PART NO. 91273A307. MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE 0KVE6, PO BOX 740100, ATLANTA GA, 30374-0100.

6. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

ALTERED ITEM DRAWING

201516597 201516570

M. LaPEE 20180404

201516589 201516570 B. CHAMBLISS 20210120

B. CHAMBLISS 20210120

BUSCAVAGE 20210120

REVISIONS

LTR DESCRIPTION DATE APPROVED

APPV

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-

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

X201516573_01_0

4:1 1 OF 1

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 08 JULY 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,

88X

11 2X

5 2X

NP WIGGINS 20180926

CRADLE, GUIDANCE UNIT

X201516576

X2

NOTES:

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

2. TIGHTEN NUT (FIND NO.7) TO REMOVE VERTICAL PLAY IN ASSEMBLY. DO NOT

OVERTIGHTEN.

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

ANSI/ASME B1.3M, SYSTEM 21.

4. 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.

5. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

6. MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE 0KVE6, PO

BOX 740100, ATLANTA GA, 30374-0100.

7. MAY BE PURCHASED FROM LINTECH, CAGE CODE 0JN439, 1845 ENTERPRISE

WAY, MONROVIA, CA. 91016. (PHONE) 1-800 435-7494

201516570 201516570

M. LaPEE 20180403

B.CHAMBLISS 20210120

B.CHAMBLISS 20210120

BUSCAVAGE 20210120

REVISIONS

LTR DESCRIPTION DATE APPROVED

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

A/R SHIM, ROUND, PEEL-AWAY 0KVE6 90902A227 .625 ID X 1.00 OD X .125 THK, LAYER THICKNESS .002, 18-8 SST 2C7 16

1 PIN, DOWEL 0KVE6 97395A511 CRES 316, .312 DIA X 2.00 LG, SMOOTH 2B2 15

1 PLUNGER, SPRING,

RETRACTABLE 0KVE6 31265A66 CRES 18-8, .375-16UNC 2A X 1.2 LG, HANDLE,1.5 LG. 2C7 14

1 NUT, HEX, THIN 0KVE6 94846A031 STL. ZINC PL, .375-16 UNC 2B, GR 5 2C7 13

8 SCREW, HEX SOCKET HD 0KVE6 92196A197 CRES 18-8 .164-32 UNC 3A X .75 LG ROCKWELL B70 2A5 12

2 SCREW, HEX DR. BUTTON

HD 0KVE6 92949A269 CRES 18-8 .190-32 UNF 3A X .75 LG ROCKWELL B55,

PASSIVATED 1B4 11

1 NUT, THIN, HEX 0KVE6 94846A030 STL ZINC PL, .312-18 UNC, GR 5 1B4 10

1 PLUNGER, WITH KNOB 0KVE6 8692A131 CRES 316, .312-18UNC X .625 LG, KNOB .625 DIA

KNURLED 1B4 9

8 SCREW, FLAT HD, 90 DEG 0KVE6 92125A203 CRES 18-8 THD CLASS 6g M4 X .7mm X 30mm LG 1C6 8

1 NUT, HEX, LOCKING 0KVE6 95615A210 .50-13UNC, NYLON INSERT, STL ZINC PL 2B5 7

1 WASHER, FLAT 0KVE6 98017A210 CRES 18.8 .515 ID X 875 OD X .069 THK 2B5 6

2 RAIL, BALL TYPE 0N439 ARC15MNBZV1H-1-

215-17.5-17.5

ALLOY STL BEARING, RAIL AND BALL, DUST PROOF,

EQUAL LOAD IN ALL DIRECTIONS 1C4 5

1 STOP MOUNT 20187050-01 1B4 4

1 BEARING PLATE, LOWER 201516618-10 1C6 3

1 CRADLE ASSEMBLY 201516579-10 1D4 2

1 CARRIAGE ASSEMBLY 201516605-10 ALTERED ITEM DRAWING 1B6 1

APPV

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-

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

X201516576-10_0

1:4 1 OF 2

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 07 JULY 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,

A

B

B

16 A/RX

C

SECTION A-A

SCALE 1 : 2

15.94

D

D

SECTION B-B

SCALE 1 : 2

DETAIL C

SCALE 1 : 1

SECTION D-D

SCALE 1 : 2

12 8X

X201516576

X2

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516576-10_0

1:4 2 OF 2

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: 07 JULY 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,

NP WIGGINS 20181108

BEARING PLATE

X201516577

X2

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.

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

INJURIOUS TO THE PART(S) OR THE ENVIRONMENT. ANODIZE IAW MIL-A-8625F

1993, TYPE II CLASS 2, COLOR BLACK.

201516618 201516570

ALUM PLATE 1.00 THK

6061-T651, IAW ASTM-B209

M. LaPEE 20180404

B.CHAMBLISS 20210120

B.CHAMBLISS 20210120

BUSCAVAGE 20210120

REVISIONS

LTR DESCRIPTION DATE APPROVED

APPV

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-

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

X201516577-01_0

1:1 1 OF 2

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 07 JULY 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,

.375

.75

7.50

9.00

2X R .19

4X R .25

1.14 1.3775-1.3770 .340+.003-.000

BOTH SIDES

2.000

B

B

A

A

5X .2764 -2762 .400

.5

.0

2.08

3.53

4.98

6.43

7.88

A

11X .3945 -.3942

.2496 -.2488

8X .177+ .005 .001

.325 X 90

X

.6

.8

.9

1.

X

1.

X 1.

X

2.

X

3.

X

4.

.0

5.

.0

4X 1.250

4X 2.270

2.375 2.480 2.782

3.252

3.840

3X 4.500

5.160

5.748

6.218 6.520 6.625

9.00

BC

.812

SECTION B-B

2X .34

.31

SECTION A-A

X201516577

X2

.015 M A B C

.010 M A B C

.010 M A B C

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516577-01_0

1:1 2 OF 2

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: 07 JULY 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,

BEARING, SHAFT

X201516578

X2

NOTES:

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

2. REMOVE ALL BURRS AND SHARP EDGES .06 MAX

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

INSPECTED IAW ANSI/ASME B1.3M, SYSTEM 21.

4. 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.

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

2.00 X 2.00 300 SERIES SST

SQ.

201516579 201516570

M. LaPEE 20180404

B.CHAMBLISS 20210120

B.CHAMBLISS 20210120

BUSCAVAGE 20210120

REVISIONS

LTR DESCRIPTION DATE APPROVED

APPV

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-

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

X201516578-01_0

2:1 1 OF 2

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 08 JULY 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,

1.000

.6245-.6243

2.00 (STK)

.375

1.000

1.000

.375

2.00 (STK)

4X R .25 4X .250 28-UNF-2B

1.625

1.625

B

C

R.030

.230+ .000 .003

.050+ .000 .003

1.150

.875

2.31

.030 X 45

.500-13 UNC-2A

THREAD RELIEF

AS REQUIRED

A

X201516578

X2

.030 M A B C

.015 M A B C

.030 M A B C

.015 M A B C

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516578-01_0

2:1 2 OF 2

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: 08 JULY 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,

6 2X

10 2X

NP WIGGINS 20180322

CRADLE ASSEMBLY

X201516579

X2

NOTES:

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

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

B1.3M, SYSTEM 21.

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. EQUIVALENT, INTERCHANGEABLE COMMERCIAL HARDWARE ACCEPTABLE.

5. MAY BE PURCHASED FROM McMASTER-CARR SUPPLY, CAGE CODE 0KVE6, PO BOX

740100, ATLANTA GA, 30374-0100.

6. APPLY LOCKING COMPOUND PRIMER (FIND NO. 12) AND LOCKING COMPOUND

(FIND NO. 13) TO THREADS ON SCREW (FIND NOS. 6, 8, AND 9) IAW MANUFACTURERS

INSTRUCTION PRIOR TO INSTALLATION.

7. MAY BE PURCHASED FROM HEINRICH KIPP WERK KP, SULZ, GERMANY

8. TIGHTEN SCREW (FIND NO. 6) TO REMOVE SPACE TO PLATE (FIND NO. 2) PIVOT CRADLE

ASSEMBLY SHOULD ROTATE FREELY WITH SCREWS (FIND NO. 6).

201516576 201516570

B.CHAMBLISS 20210120

B.CHAMBLISS 20210120

BUSCAVAGE 20210120

REVISIONS

LTR DESCRIPTION DATE APPROVED

-10 NOMENCLATURE CAGE IDENTIFYING NO MATERIAL / SPECIFICATION ZONE FN

A/R THREADLOCK COMPOUND 0KVE6 91458A11 LOCTITE 22221 .34 OZ BOTTLE PURPLE 13

A/R THREADLOCK PRIMER 0KVE6 7614A16 LOCTITE 7649(N) 1.75 OZ BOTTLE 12

1 PLUNGER, INDEXING D2050 K0630.203105 M10X1 THD, 5mm DIA PLUNGER CRES 1D2 11

2 PIN, DOWEL 0KVE6 90145A540 CRES 18-8 .250 DIA X .75 LG 1D2 10

4 SCREW, MACHINE, FLT HD 0KVE6 91500A544 CRES 316 .250-20UNC X 1.25 LG ROCKWELL B80 2B6 9 4 SCREW, FLAT, HEX DR 0KVE6 92210A334 CRES18-8 .250-28UNF X .75 LG. ROCKWELL B55 1C3 8 2 BEARING, SLEEVE 0KVE6 9368T137 BRONZE SAE 841.375 ID X .562 OD X .50 LG GRAPHITE 2C2 7 2 SCREW, SHOULDER 0KVE6 90298A619 CRES .375 DIA SHOULDER X .50 LG, .312-18UNC THD 2C7 6

1 BEARING, SHAFT 201516578-01 2B7 5

1 PIVOT CRADLE ASSEMBLY 201516585-10 1D2 4

1 SIDE PLATE 201516620-01 1D3 3

1 SIDE PLATE 201516600-01 1C2 2

1 BASE, PIVOT 201516584-01 1C3 1

APPV

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-

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

X201516579-10_0

1:2 1 OF 2

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 07 JULY 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,

94X

9.00

12.50

AA

62X

5.00

B

B

SECTION A-A

8 4X

SECTION B-B

7 2X

X201516579

X2

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516579-10_0

1:2 2 OF 2

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: 07 JULY 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,

NP. WIGGINS 20180322

LOWER SHELF

X201516580

X2

NOTES:

INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2018.1.

2. REMOVE ALL BURRS AND SHARP EDGES.

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.

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.

5. FINISH: 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.

.190 THK 6061-T6

ALUM SHT. ASTM-B209

201516570 201516570

M. LaPEE 20180404

B.CHAMBLISS 20210120

B.CHAMBLISS 20210120

BUSCAVAGE 20210120

REVISIONS

LTR DESCRIPTION DATE APPROVED

APPV

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-

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

X201516580-01_0

1:4 1 OF 2

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE OR OPERATIONAL USE. DATE: 07 JULY 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,

13X .125+ .004 .001

.75 2X 1.75 2.50

10.03

17.50 2X 18.25 19.25 20.00

.7

X

1.

2.

.7

X

.1

X

.2

X

.5

X

.1

4.

.19 (STK)

X201516580

X2

REVISIONS

LTR DESCRIPTION DATE APPROVED

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

X201516580-01_0

1:4 2 OF 2

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: 07 JULY 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,

-01

-02

NP WIGGINS 20150713

EDGE GUARD

X201516581

X2

NOTES:

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

2. REMOVE ALL BURRS AND SHARP EDGES.

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.

4. CLEAN PART USING CLEANING METHOD AND AGENTS, WHICH SHALL NOT

BE INJURIOUS TO THE PART(S) OR TO THE ENVIRONMENT.

5. FINISH: 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.

201516570 201516570

1.50 X .75 X .125 THK

ANGLE, 6063-T52 AL.

IAW ASTM-B221

M. LaPEE 20180404

B.CHAMBLISS 20210120

B.CHAMBLISS 20210120

BUSCAVAGE 20210120

REVISIONS

LTR DESCRIPTION DATE APPROVED

APPV

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-

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

X201516581-01_0

1:8 1 OF 2

MATERIAL:

DISTRIBUTION STATEMENT C DISTRIBUTION AUTHORIZED TO U.S.

GOVERNMENT AGENCIES AND THEIR CONTRACTORS. REASON:

ADMINISTRATIVE…