RD2F ECR0043 Drawings dated 30JUN2025.pdf

Kratos Training Solutions

8601 Transport Drive

Orlando, Florida 32832

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DISTRIBUTION STATEMENT D. Distribution authorized to the Department of Defense and U.S.

DOD contractors only, administrative or operational use, determined on 07 Jan 2014. Other requests shall be referred to Commander, Naval Air Systems

Command (PMA- 261), RADM William A Moffett

Bldg., 47123 Buse Rd, Bldg. 2272, Patuxent River, MD 20670-1547.

List Date: 08/10/20

Rev Date:

Rev: -

1 1 EA 8A244 13204930-101 PLATE, BASE STEEL, ASTM A 36, 1010 THRU 1026, .50 THK

2 1 EA 8A244 13204930-102 BLOCK STEEL, ASTM A108, CF 1018

3 1 EA 8A244 13204930-103 SUPPORT, BOTTOM STEEL, ASTM A36, 1010 THRU 1026, .50 THK

4 1 EA 8A244 13204930-104 SUPPORT, TOP STEEL, ASTM A36, 1010 THRU 1026, .50 THK

5 1 EA 8A244 13204930-105 PLATE, TOP STEEL, ASTM A36, 1010 THRU 1026

6 1 EA 8A244 13204930-106 GUSSET STEEL, ASTM A36, 1010 THRU 1026, .50 THK

7 1 EA 0KVE6 2934T17 BEARING, SLEEVE, FLANGED, .500 SFT DIA, 1.00 OD, 1.000 LG 954 ALUMINUM BRONZE

Reference DesignatorComponent Description

Revision History

Drawing Title: WELDMENT ASSEMBLY, SFT MOUNT, HEAT EXCHANGER

CommentsPart #

Parts List Cage No.: 8A244

FN QTY U/M

PL - 13204930

Contract: NA

Cage No.

Project: CH-53K MTDS

APPLICATION

NEXT ASSEMBLY

SHEET 1 OF 2 SCALE:

REVDWG NO.CODE IDENT NO.

D

SIZE

TITLE

TOLERANCES:

ALL DIMENSIONS ARE IN INCHES

UNLESS OTHERWISE SPECIFIED

.XX DECIMAL

.X DECIMAL

.XXX DECIMAL

ANGLES ±

THIRD ANGLE PROJECTION

PROJECT ENGINEER

QUALITY ASSURANCE

ENGINEER

DRAWN

DATEAPPROVALS

CONTRACT NO.

PROGRAM

3 2 1

D

C

B

A

REVISIONS

DESCRIPTIONREVZONE DATE APPROVED

3 12

8 7 6 5 4

45678

A

B

C

D

NEXT ASSEMBLY

APPLICATION 1~

.1

.03

.010 13204512

CH-53K MTDS

N00019-06-C-0081

8A244

O. GIPPLE

D. JACKSON

R

8601 TRANSPORT DRIVE

ORLANDO, FL 32832

MFG BY:

AND TRAINING SOLUTIONS

KRATOS TECHNOLOGY

DISTRIBUTION D: DISTRIBUTION AUTHORIZED TO THE DEPARTMENT OF

DEFENSE AND U.S. DEPARTMENT OF DEFENSE CONTRACTORS ONLY

DUE TO CRITICAL TECHNOLOGY, EFFECTIVE 04 JUNE 2004. OTHER REQUESTS

FOR THIS DOCUMENT SHALL BE REFERRED TO KRATOS TECHNOLOGY AND

TRAINING SOLUTIONS INC., 4820 EASTGATE MALL, SAN DIEGO, CA 92121.

ITAR STATEMENT: THIS INFORMATION IS SUBJECT TO THE CONTROLS OF

THE INTERNATIONAL TRAFFIC IN ARMS REGULATIONS \(ITAR\). THIS INFORMATION

SHALL NOT BE PROVIDED TO NON-U.S. PERSONS OR TRANSFERRED

BY ANY MEANS TO ANY LOCATION OUTSIDE THE UNITED STATES WITHOUT

ADVANCED WRITTEN PERMISSION FROM KRATOS AND APPROVAL FROM

THE UNITED STATES DEPARTMENT OF STATE.

DESTRUCTION NOTICE: UNCLASSIFIED-LIMITED DOCUMENT: DESTROY

BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS OR

RECONSTRUCTION OF THIS DOCUMENT.

WELDMENT, MOUNT, RH,

APU, EXHAUST DUCT

R. GONZALEZ

2/1

SEE SEPARATE PARTS LIST

R. PARE

2016/03/16

2016/03/16

2016/03/16

2016/03/16

13202170

- 2016/03/16 DJINITIAL RELEASENOTES:

1. APPLICABLE STANDARDS/SPECIFICATIONS:

-ASME Y14.5M-1994, DIMENSIONING AND TOLERANCING.

-ANSI/AWS A2.4, WELD SYMBOLS FOR WELDING

AND NONDESTRUCTIVE TESTING.

2. UNLESS OTHERWISE SPECIFIED:

-MINIMUM WELD SIZE WILL BE IAW AWS D1.2.

-ALL WELDS TO BE VISUALLY INSPECTED.

3. REMOVE ALL BURRS AND SHARP EDGES.

4. FINISH: PREP, PRIME AND PAINT IAW MANUFACTURER'S

SPECIFICATION. COLOR PER FED-STD-595B, NO. 26493,

GRAY, SEMIGLOSS.

5. ITEM IDENTIFICATION: MARK IDENTIFICATION NUMBER

8A244ASSY13204512 ON BAG OR TAG WITH .12 MINIMUM

HIGH CHARACTERS USING PERMANENT CONTRASTING

COLORED INK.

6 HOLES SHALL BE FREE OF PRIMER AND PAINT.

7 APPLY LOCTITE 609 TO SECURE COMPONENTS.

8 REAMED HOLES TO DIMENSION SHOWN AFTER INSTALLATION.

9 HOLES TO BE IN-LINE AFTER REAMING PROCESS.

.232X

1.752X

\(.500\)4X NO WELD

IN THIS REGION

9 97 7

\(1.28\)

.438n -.000 .002+

.250n -.000

.002+

.25-.75

.25-.75

.561 -.000 .005+

90°` .5°

\(-101\)

SCALE: 2/1

\(-102\)

SCALE: 2/1

\(-103\)

SCALE: 2/1

SHEET 2 OF 2 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204512 - 2/1

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

\(.19\)

1.75 2.31

.252X

1.8122X

.252X

1.2502X

R.134X

4X n .219 THRU

\(.13\)

1.85

R.53.376n -.000

.002+ THRU

\(.13\)

1.85

1.050

.312X

1.556

1.050

.312X

21° 12°

R.53

21° 12°1.556

.560n -.000

.002+ THRU

APPLICATION

NEXT ASSEMBLY

SHEET 1 OF 2 SCALE:

REVDWG NO.CODE IDENT NO.

D

SIZE

TITLE

TOLERANCES:

ALL DIMENSIONS ARE IN INCHES

UNLESS OTHERWISE SPECIFIED

.XX DECIMAL

.X DECIMAL

.XXX DECIMAL

ANGLES ±

THIRD ANGLE PROJECTION

PROJECT ENGINEER

QUALITY ASSURANCE

ENGINEER

DRAWN

DATEAPPROVALS

CONTRACT NO.

PROGRAM

3 2 1

D

C

B

A

REVISIONS

DESCRIPTIONREVZONE DATE APPROVED

3 12

8 7 6 5 4

45678

A

B

C

D

NEXT ASSEMBLY

APPLICATION 1~

.1

.03

.010 13204513

CH-53K MTDS

N00019-06-C-0081

8A244

O. GIPPLE

D. JACKSON

R

8601 TRANSPORT DRIVE

ORLANDO, FL 32832

MFG BY:

AND TRAINING SOLUTIONS

KRATOS TECHNOLOGY

DISTRIBUTION D: DISTRIBUTION AUTHORIZED TO THE DEPARTMENT OF

DEFENSE AND U.S. DEPARTMENT OF DEFENSE CONTRACTORS ONLY

DUE TO CRITICAL TECHNOLOGY, EFFECTIVE 04 JUNE 2004. OTHER REQUESTS

FOR THIS DOCUMENT SHALL BE REFERRED TO KRATOS TECHNOLOGY AND

TRAINING SOLUTIONS INC., 4820 EASTGATE MALL, SAN DIEGO, CA 92121.

ITAR STATEMENT: THIS INFORMATION IS SUBJECT TO THE CONTROLS OF

THE INTERNATIONAL TRAFFIC IN ARMS REGULATIONS \(ITAR\). THIS INFORMATION

SHALL NOT BE PROVIDED TO NON-U.S. PERSONS OR TRANSFERRED

BY ANY MEANS TO ANY LOCATION OUTSIDE THE UNITED STATES WITHOUT

ADVANCED WRITTEN PERMISSION FROM KRATOS AND APPROVAL FROM

THE UNITED STATES DEPARTMENT OF STATE.

DESTRUCTION NOTICE: UNCLASSIFIED-LIMITED DOCUMENT: DESTROY

WELDMENT, MOUNT, LH,

APU, EXHAUST DUCT

R. GONZALEZ

2/1 A

SEE SEPARATE PARTS LIST

R. PARE

2016/03/16

2016/03/16

2016/03/16

2016/03/16

13202170

- 2016/03/16 DJINITIAL RELEASENOTES:

1. APPLICABLE STANDARDS/SPECIFICATIONS:

-ASME Y14.5M-1994, DIMENSIONING AND TOLERANCING.

-ANSI/AWS A2.4, WELD SYMBOLS FOR WELDING

AND NONDESTRUCTIVE TESTING.

2. UNLESS OTHERWISE SPECIFIED:

-MINIMUM WELD SIZE WILL BE IAW AWS D1.2.

-ALL WELDS TO BE VISUALLY INSPECTED.

3. REMOVE ALL BURRS AND SHARP EDGES.

4. FINISH: PREP, PRIME AND PAINT IAW MANUFACTURER'S

SPECIFICATION. COLOR PER FED-STD-595B, NO. 26493,

GRAY, SEMIGLOSS.

5. ITEM IDENTIFICATION: MARK IDENTIFICATION NUMBER

8A244ASSY13204513 ON BAG OR TAG WITH .12 MINIMUM

HIGH CHARACTERS USING PERMANENT CONTRASTING

COLORED INK.

6 HOLES SHALL BE FREE OF PRIMER AND PAINT.

7 APPLY LOCTITE 609 TO SECURE COMPONENTS.

8 REAMED HOLES TO DIMENSIONS SHOWN AFTER INSTALLATION.

9 HOLES TO BE IN-LINE AFTER REAMING PROCESS.

79 7 9 .438n -.000

.002+ .250n -.000

.002+

.504X NO WELD

IN THIS REGION

90°` .5°

.561 -.000 .005+

2.062X

.042X

\(1.44\)

INCORPORATED REDLINES R1A 2018/08/20 DJ

\(-101\)

SCALE: 2/1

\(-102\)

SCALE: 2/1

\(-103\)

SCALE: 2/1

SHEET 2 OF 2 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204513 A 2/1

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

1.75 2.31 \(.19\)

.252X

1.2502X

.252X

1.8122X

4X n .219 THRU

R.134X

2.23

1.400

.312X

1.871 10° 27°

R.53.376n -.000

.002+ THRU

6\(.13\)

2.23

1.400

.312X

1.871 27° 10°

R.53.560n -.000

.002+ THRU\(.13\)

ISO VIEW

SCALE 2/3

SECTION A-A

SCALE 1/1

A

A

APPLICATION

NEXT ASSEMBLY

SHEET 1 OF 8 SCALE:

REVDWG NO.CODE IDENT NO.

D

SIZE

TITLE

TOLERANCES:

ALL DIMENSIONS ARE IN INCHES

UNLESS OTHERWISE SPECIFIED

.XX DECIMAL

.X DECIMAL

.XXX DECIMAL

ANGLES ±

THIRD ANGLE PROJECTION

PROJECT ENGINEER

QUALITY ASSURANCE

ENGINEER

DRAWN

DATEAPPROVALS

CONTRACT NO.

PROGRAM

3 2 1

D

C

B

A

REVISIONS

DESCRIPTIONREVZONE DATE APPROVED

3 12

8 7 6 5 4

45678

A

B

C

D

NEXT ASSEMBLY

APPLICATION 1~

.1

.03

.010 13204930

CH-53K MTDS

N00019-06-C-0081

8A244

O. GIPPLE

D. JACKSON

R

8601 TRANSPORT DRIVE

ORLANDO, FL 32832

MFG BY:

AND TRAINING SOLUTIONS

KRATOS TECHNOLOGY

DISTRIBUTION D: DISTRIBUTION AUTHORIZED TO THE DEPARTMENT OF

DEFENSE AND U.S. DEPARTMENT OF DEFENSE CONTRACTORS ONLY

DUE TO CRITICAL TECHNOLOGY, EFFECTIVE 04 JUNE 2004. OTHER REQUESTS

FOR THIS DOCUMENT SHALL BE REFERRED TO KRATOS TECHNOLOGY AND

TRAINING SOLUTIONS INC., 4820 EASTGATE MALL, SAN DIEGO, CA 92121.

ITAR STATEMENT: THIS INFORMATION IS SUBJECT TO THE CONTROLS OF

THE INTERNATIONAL TRAFFIC IN ARMS REGULATIONS \(ITAR\). THIS INFORMATION

SHALL NOT BE PROVIDED TO NON-U.S. PERSONS OR TRANSFERRED

BY ANY MEANS TO ANY LOCATION OUTSIDE THE UNITED STATES WITHOUT

ADVANCED WRITTEN PERMISSION FROM KRATOS AND APPROVAL FROM

THE UNITED STATES DEPARTMENT OF STATE.

DESTRUCTION NOTICE: UNCLASSIFIED-LIMITED DOCUMENT: DESTROY

WELDMENT ASSEMBLY,

SFT MOUNT,

HEAT EXCHANGER

Y. CHENG

1/1

SEE SEPARATE PARTS LIST

Y. CHENG

2018/04/13

2018/04/13

2018/04/13

2018/04/13

13202013

- 2018/04/13 DJINITIAL RELEASENOTES:

1. APPLICABLE STANDARDS/SPECIFICATIONS:

-ASME Y14.5M-1994, DIMENSIONING AND TOLERANCING.

-ANSI/AWS A2.4, WELD SYMBOLS FOR WELDING

AND NONDESTRUCTIVE TESTING.

2. UNLESS OTHERWISE SPECIFIED:

-MINIMUM WELD SIZE WILL BE IAW AWS D1.1.

-ALL WELDS TO BE VISUALLY INSPECTED.

3. REMOVE ALL BURRS AND SHARP EDGES.

4 USE Ø.250 HOLE OF FN 2 AND FN 5 AS THE PRIMARY

ALIGNMENT AND Ø.094 PILOT HOLES AS THE SECONDARY

ALIGNMENT TO POSITION TOGETHER FN 1 THRU FN 6

BEFORE WELDING.

5 UPON COMPLETION OF THE WELDMENT, MACHINE THE

Ø.250 HOLE OF FN 2 AND FN 5 TO DIMENSIONS SHOWN

ON THE FIELD OF THE DRAWING FOR SUBSEQUENT

OPERATION.

6 MODIFY FN 7 TO CONFIGURATION SHOWN ON THE FIELD

OF THE DRAWING PRIOR TO INSTALLATION.

7 SECURE FN 7 TO THE WELDMENT USING RETAINING

COMPOUND LOCTITE 680, OR EQUIVALENT. ALLOW

THE RETAINING COMPOUND TO FULLY CURE BEFORE

SUBSEQUENT PROCESS.

8 FINISH THE INTERNAL DIAMETER OF FN 7 TO DIMENSION

SHOWN ON THE FIELD OF THE DRAWING. CONCENTRICITY

WITH RESPECT TO THE Ø.376 HOLE OF FN 2 TO BE

MAINTAINED WITHIN +/- .005 AFTER MACHINING.

9 BORES, 1/4-20UNC AND 3/8-24UNF THREADS TO BE FREE

OF PRIMER AND PAINT.

10. FINISH: PREP, PRIME, AND PAINT IAW MANUFACTURER'S

SPECIFICATION. COLOR PER FED-STD-595B, NO. 26493,

GRAY, SEMIGLOSS.

11. ITEM IDENTIFICATION: MARK IDENTIFICATION NUMBER

8A244ASSY13204930 ON BAG OR TAG WITH .12 MINIMUM

HIGH CHARACTERS USING PERMANENT CONTRASTING

COLORED INK.

SFT MOUNT WELDMENT

.564n -.002

.000+ THRU

ON FN 7 ONLY

.564\(Ø \)

6 7

\(3/8-24 UNF - 2B\)

.376\(Ø \)

\( \)7

1/4-20 UNC - 2B\(12X \)

SFT MOUNT WELDMENT

SCALE 2/3

SECTION J-J

SCALE 2/3

SECTION K-K

SCALE 2/3

SECTION L-L

SCALE 2/3

J

J

K K

L L

SHEET 2 OF 8 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204930 - 1/1

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

\(4.74\)

1.13

.754\(Ø \) n .754 -.000

.003+ THRU

NEAR SIDE ONLY

2X

2X

\( \)1

\( \)4

\( \)5

\( \)3

\( \)1

\( \)4

\( \)3

\( \)5

\( \)2

\( \)1

\( \)2

\( \)4

\( \)1

\( \)5

\( \)6

\( \)3

\( \)5

3/8-24 UNF - 2B

v n .376 -.000

.010+ x .81

2X

2X

-101

SCALE 1/1

SHEET 3 OF 8 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204930 - 1/1

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

\(.50\)

.953X

1.8222X

1.2502X

6.5442X

.97 1.750

3.500

1.1252X 1.2502X

1.313 .875

5.44

8.23

4.94

1.672X

R1.404X

R.582X

.502X

1.2502X

2.2252X

2.5002X 4.475

6.2242X

2.750

4.844

.563

1.722.000

1.2202X

.125

3.2202X

2.125

.3332X

.2502.250

1.0002X \(R.58\)

2X n .221 THRU w n .406 X 100°

12X 1/4-20 UNC - 2B x .38

MINIMUM THREADS

n .094 x .139X

\(PILOT HOLES FOR ALIGNMENT\)

-002

SCALE 2/1

VIEW C-C

SCALE 2/1

SECTION B-B

SCALE 2/1

B

B

CC

SHEET 4 OF 8 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204930 - 1/1

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

n 1.00

\(n .250\)

\(1.00\)

\(1.00\)

R.504X

2.00

2.00

2.14 -.03 .00+

1.002X n .375 THRU

.382X

1.2502X

.382X 1.2502X n .094 x .134X

PILOT HOLES FOR ALIGNMENT

.74

.30 -.00 .03+

\(1.40\)

\(1.00\)

.22

.22

1.00\(Ø \) 4

.250 -.000 .005+ x .313

-103

VIEW E-E

SCALE 2/1

E

E

SHEET 5 OF 8 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204930 - 1/1

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

\(.50\) 1.58

.79

.99

.50

.20

\(4.24\)

4.78

.20

.312X

.88

.44 n .094 x .132X

PILOT HOLES FOR ALIGNMENT

.25 n .094 x .13

PILOT HOLE FOR ALIGNMENT

-104

SCALE 3/2

VIEW F-F

SCALE 3/2

F

F

SHEET 6 OF 8 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204930 - 1/1

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

2.50

4.44

2.22

1.25

\(4.24\)

\(.50\)

.14

.14

4.55

1.75 .88

.252X n .094 x .132X

PILOT HOLES FOR ALIGNMENT

.273X

1.75

3.50 n .094 x .133X

PILOT HOLES FOR ALIGNMENT

-105

SCALE 3/2

VIEW G-G

SCALE 3/2

VIEW H-H

SCALE 3/2

G

G

H

H

SHEET 7 OF 8 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204930 - 1/1

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

.98 -.03 .00+ .16

\(n 1.25\) n 1.25 n .250 -.000

.005+ THRU

1.26

.28

.39

1.28

2.57

.392X n .250 THRU\( \) \(3.14\)

.25 n .094 x .13

PILOT HOLE FOR ALIGNMENT

.252X

.78

1.75

.87 n .094 x .132X

PILOT HOLES FOR ALIGNMENT

\(1.26\)

3.81

\(.97\)

\(2.44\)

R.13

-106

FN 7 AFTER MODIFICATION

SCALE 3/1

FN 7 BEFORE MODIFICATION

SCALE 3/1

SHEET 8 OF 8 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204930 - 1/1

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

1.00

\(.50\)

2.87

2.47

\(n 1.000\)\(n .501\)

\(.875\)

\(.125\)

\(n 1.000\)

\(n .752\)

\(n .752\)

.065

\(.875\)

-001

SCALE 1/3

APPLICATION

NEXT ASSEMBLY

SHEET 1 OF 2 SCALE:

REVDWG NO.CODE IDENT NO.

D

SIZE

TITLE

TOLERANCES:

ALL DIMENSIONS ARE IN INCHES

UNLESS OTHERWISE SPECIFIED

.XX DECIMAL

.X DECIMAL

.XXX DECIMAL

ANGLES ±

THIRD ANGLE PROJECTION

PROJECT ENGINEER

QUALITY ASSURANCE

ENGINEER

DRAWN

DATEAPPROVALS

CONTRACT NO.

PROGRAM

3 2 1

D

C

B

A

REVISIONS

DESCRIPTIONREVZONE DATE APPROVED

3 12

8 7 6 5 4

45678

A

B

C

D

NEXT ASSEMBLY

APPLICATION 1~

.1

.03

.010 13204931

CH-53K MTDS

N00019-06-C-0081

8A244

O. GIPPLE

D. JACKSON

R

8601 TRANSPORT DRIVE

ORLANDO, FL 32832

MFG BY:

AND TRAINING SOLUTIONS

KRATOS TECHNOLOGY

DISTRIBUTION D: DISTRIBUTION AUTHORIZED TO THE DEPARTMENT OF

DEFENSE AND U.S. DEPARTMENT OF DEFENSE CONTRACTORS ONLY

DUE TO CRITICAL TECHNOLOGY, EFFECTIVE 04 JUNE 2004. OTHER REQUESTS

FOR THIS DOCUMENT SHALL BE REFERRED TO KRATOS TECHNOLOGY AND

TRAINING SOLUTIONS INC., 4820 EASTGATE MALL, SAN DIEGO, CA 92121.

ITAR STATEMENT: THIS INFORMATION IS SUBJECT TO THE CONTROLS OF

THE INTERNATIONAL TRAFFIC IN ARMS REGULATIONS \(ITAR\). THIS INFORMATION

SHALL NOT BE PROVIDED TO NON-U.S. PERSONS OR TRANSFERRED

BY ANY MEANS TO ANY LOCATION OUTSIDE THE UNITED STATES WITHOUT

ADVANCED WRITTEN PERMISSION FROM KRATOS AND APPROVAL FROM

THE UNITED STATES DEPARTMENT OF STATE.

DESTRUCTION NOTICE: UNCLASSIFIED-LIMITED DOCUMENT: DESTROY

BODY, PRINTED, FAN,

DUAL HEAT EXCHANGER

Y. CHENG

1/3

Y. CHENG

2018/04/12

2018/04/12

2018/04/12

2018/04/12

13202013 13204938

- 2018/04/12 DJINITIAL RELEASE

NOTES:

1. APPLICABLE STANDARDS/SPECIFICATIONS PER ASME

Y14.5M-1994, DIMENSIONING AND TOLERANCING.

2. FOR MANUFACTURING PURPOSES, THIS DRAWING SHALL

BE THE MASTER DEFINITION. 3D MODEL \(S\) FILE NAME:

13204931-XXX.STL CURRENT REVISION WILL BE

SUPPLIED BY THE CONTRACTING OFFICER. IT SHALL BE

USED FOR ALL UNDIMENSIONED FEATURES.

3. UNLESS OTHERWISE SPECIFIED, DIMENSIONAL TOLERANCES

ON THE MODEL \(S\) SHALL BE +/- .020 IN. OR +/- 0.003 IN./IN.,

WHICHEVER IS GREATER.

4. UNSUPPORTED REFERENCE DIMENSIONS TO BE FOR

CONFIGURATION VERIFICATION.

5. PRINTING PROCESS: SLS.

6. MATERIAL: NYTEK 1200GF - GLASS FILLED NYLON 12 OR

EQUIVALENT. MATERIAL SUBSTITUTIONS MUST BE

APPROVED BY CONTRACTING OFFICERS.

7. SURFACE PREP: NONE.

8. REMOVE ALL BURRS AND SHARP EDGES.

9 NO PRIMER OR PAINT ON INDICATED SURFACES.

10. FINISH: PREP, PRIME, AND PAINT IAW MANUFACTURER'S

SPECIFICATION. COLOR PER FED-STD-595B, NO. 26493,

GRAY, SEMIGLOSS.

11. ITEM IDENTIFICATION: MARK IDENTIFICATION NUMBER

8A244-13204931-XXX ON BAG OR TAG WITH .12 MINIMUM

HIGH CHARACTERS USING PERMANENT CONTRASTING

COLORED INK.

\(11.23\)

\(12.71\)

\(1.50\)

\(12.48\)

\(5.06\)

-002

SCALE 1/3VIEW A-A

SCALE 1/3

AA

SHEET 2 OF 2 SCALE:

D

REVDWG NO.CODE IDENT NO.SIZE

A

B

C

DD

C

B

A

8 7 6 5 4

45678

13204931 - 1/3

8A244THIS DOCUMENT IS SUBJECT TO U.S. GOVERNMENT EXPORT REGULATIONS.

\(12.56\)

\(23.63\)

\(1.50\)

\(6.49\)

\(.75\)

\(5.06\)\(12.40\)

\(23.16\)

Orlando, Florida 32832

HANDLING AND DESTRUCTION NOTICE – Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

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 laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DODD 5230.25.

DISTRIBUTION STATEMENT D. Distribution authorized to the Department of Defense and U.S.

DOD contractors only, administrative or operational use, determined on 07 Jan 2014. Other requests shall be referred to Commander, Naval Air Systems

Command (PMA- 261), RADM William A Moffett

Bldg., 47123 Buse Rd, Bldg. 2272, Patuxent River, MD 20670-1547.

List Date: 08/10/20

Rev Date:

1 1 EA 8A244 13202545-101 MOUNT PLATE, FUEL NOZZLE MATERIAL: ALUMINUM ALLOY, 6061-T651

2 1 EA 8A244 13202545-102 ROD, BODY, FUEL NOZZLE

MATERIAL: ALUMINUM ALLOY, 6061-T651, SQUARE

STOCK, .25 X .25

3 1 EA 8A244 13202545-103 ROD, VERTICAL, FUEL NOZZLE

MATERIAL: ALUMINUM ALLOY, 6061-T651, ROD,

.63 DIA.

4 1 EA 8A244 13202545-104 ROD, ANGLED, FUEL NOZZLE

MATERIAL: ALUMINUM ALLOY, 6061-T651, ROD,

1.00 DIA.

Drawing Title: WELDMENT, FUEL NOZZLE

CommentsPart #

Parts List Cage No.: 8A244

FN QTY U/M

PL - 13202545

Contract: NA

Cage No.

Orlando, Florida 32832

HANDLING AND DESTRUCTION NOTICE – Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

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 laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DODD 5230.25.

DISTRIBUTION STATEMENT D. Distribution authorized to the Department of Defense and U.S.

DOD contractors only, administrative or operational use, determined on 07 Jan 2014. Other requests shall be referred to Commander, Naval Air Systems

Command (PMA- 261), RADM William A Moffett

Bldg., 47123 Buse Rd, Bldg. 2272, Patuxent River, MD 20670-1547.

List Date: 08/10/20

Rev Date:

1 1 EA 8A244 13204412-101 FLANGE, MOUNTING ALUMINUM ALLOY, 5052-H32, .120 THK

2 1 EA 8A244 13204412-102 PLATE, REAR MOUNTING ALUMINUM ALLOY, 5052-H32, .120 THK

3 1 EA 8A244 13204412-103 PLATE, SIDE, FWD ALUMINUM ALLOY, 5052-H32, .120 THK

4 1 EA 8A244 13204412-104 PLATE, SIDE, AFT ALUMINUM ALLOY, 5052-H32, .120 THK

5 1 EA 8A244 13204412-105 COVER, BOTTOM ALUMINUM ALLOY, 5052-H32, .120 THK

6 1 EA 8A244 13204412-106 COVER, TOP ALUMINUM ALLOY, 5052-H32, .120 THK

7 2 EA 8A244 13204412-107 COVER, INNER ALUMINUM ALLOY, 5052-H32, .120 THK

8 17 EA 80205 MS21075-4N NUT,PLAT,SLF-LKG,NON DRY,FLTG,2 LG,W/O EYLT,1/4-28 THD,ST,C

9 34 EA 11815 CCR264SS-3-03 RIVET, BLIND, FLUSH HD, 100 DEG, PULL-THRU, .093 DIA, .186G

10 10 EA 78276 ALS4-632-130 INSERT, KNURLED, STD HD, THD, 6-32, .080-.130 GP, ST, ZINC Y

Drawing Title: WELDMENT ASSEMBLY, HEAT EXCHANGER

CommentsPart #

Parts List Cage No.: 8A244

FN QTY U/M

PL - 13204412

Contract: NA

Cage No.

Orlando, Florida 32832

HANDLING AND DESTRUCTION NOTICE – Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

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 laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DODD 5230.25.

DISTRIBUTION STATEMENT D. Distribution authorized to the Department of Defense and U.S.

DOD contractors only, administrative or operational use, determined on 07 Jan 2014. Other requests shall be referred to Commander, Naval Air Systems

Command (PMA- 261), RADM William A Moffett

Bldg., 47123 Buse Rd, Bldg. 2272, Patuxent River, MD 20670-1547.

List Date: 08/10/20

Rev Date: 09/06/16

1 1 EA 8A244 13204512-101 BLOCK, MOUNTING, APU, EXHAUST DUCT ALUMINUM ALOOY, 6061-T6

2 1 EA 8A244 13204512-102 GUSSET, APU, EXHAUST DUCT ALUMINUM ALOOY, 6061-T6

3 1 EA 8A244 13204512-103 GUSSET, APU, EXHAUST DUCT ALUMINUM ALOOY, 6061-T6

4 1 EA 8A244 13203999-7-015 BUSHING, SLEEVE, FLANGED, .438 HOLE, .422 ID, .564 OD, 697

5 1 EA 8A244 13203999-4-011 BUSHING, SLEEVE, FLANGED, .250 HOLE, .238 ID, .376 OD, .510

Drawing Title: WELDMENT, MOUNT, RH, APU, EXHAUST DUCT

CommentsPart #

Parts List Cage No.: 8A244

FN QTY U/M

PL - 13204512

Contract: NA

Cage No.

Orlando, Florida 32832

HANDLING AND DESTRUCTION NOTICE – Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

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 laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DODD 5230.25.

DISTRIBUTION STATEMENT D. Distribution authorized to the Department of Defense and U.S.

DOD contractors only, administrative or operational use, determined on 07 Jan 2014. Other requests shall be referred to Commander, Naval Air Systems

Command (PMA- 261), RADM William A Moffett

Bldg., 47123 Buse Rd, Bldg. 2272, Patuxent River, MD 20670-1547.

List Date: 08/10/20

Rev Date: 09/06/16

1 1 EA 8A244 13204513-101 BLOCK, MOUNTING, APU, EXHAUST DUCT ALUMINUM ALLOY, 6061-T6

2 1 EA 8A244 13204513-102 GUSSET, APU, EXHAUST DUCT ALUMINUM ALLOY, 6061-T6

3 1 EA 8A244 13204513-103 GUSSET, APU, EXHAUST DUCT ALUMINUM ALLOY, 6061-T6

4 1 EA 8A244 13203999-7-015 BUSHING, SLEEVE, FLANGED, .438 HOLE, .422 ID, .564 OD, 697

5 1 EA 8A244 13203999-4-011 BUSHING, SLEEVE, FLANGED, .250 HOLE, .238 ID, .376 OD, .510

Drawing Title: WELDMENT, MOUNT, LH, APU, EXHAUST DUCT

CommentsPart #

Parts List Cage No.: 8A244

FN QTY U/M

PL - 13204513

Contract: NA

Cage No.

Orlando, Florida 32832

HANDLING AND DESTRUCTION NOTICE – Comply with distribution statement and destroy by any method that will prevent disclosure of contents or reconstruction of the document.

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 laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DODD 5230.25.

DISTRIBUTION STATEMENT D. Distribution authorized to the Department of Defense and U.S.

DOD contractors only, administrative or operational use, determined on 07 Jan 2014. Other requests shall be referred to Commander, Naval Air Systems

Command (PMA- 261), RADM William A Moffett

Bldg., 47123 Buse Rd, Bldg. 2272, Patuxent River, MD 20670-1547.

List Date: 08/10/20

Rev Date:

1 1 EA 8A244 13204071-101 BASE ALUMINUM ALLOY, 6061-T6, .50 THK

2 1 EA 8A244 13204071-102 PLATE ALUMINUM ALLOY, 6061-T6, .50 THK

3 1 EA 8A244 13204071-103 PLATE ALUMINUM ALLOY, 6061-T6, .50 THK

4 2 EA 8A244 13204071-104 GUSSET ALUMINUM ALLOY, 6061-T6, .25 THK

5 2 EA 8A244 13204071-105 GUSSET ALUMINUM ALLOY, 6061-T6, .25 THK

6 1 EA 0KVE6 2934T15 BEARING, SLEEVE, FLANGED, .500 SFT DIA, 1.00 OD, .500 LG

7 1 EA 0KVE6 2934T37 BEARING, SLEEVE, FLANGED, .3125 SFT DIA, .875 OD, .750 LG

Drawing Title: WELDMENT ASSEMBLY, MOUNT, THREE WAY,DUAL HEAT EXCHANGER, ECS

CommentsPart #

Parts List Cage No.: 8A244

FN QTY U/M

PL - 13204071

Contract: NA

Cage No.