FA8203-18-R-0002_ATLAS_3_Drawings.pdf

PDF 28 MB Posted Dec 13, 2017

Attached to: ATLAS 3 RFP
Solicitation number: FA8203-18-R-0002
Issued by: Department of the Air Force Materiel Command Lifecycle Management Center Hill Air Force Base

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FA8203-18-R-0002, ATLAS 3. KC-135 Sidebrace Drawings

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File	Type	Posted
FA8119-16-D-0008_Boeing_Rights_Guard_Agreement_Sign_Last_Two_Pages.pdf	PDF	Dec 13, 2017
FA8203-18-R-0002_ATLAS_3_TDP_Docs.pdf	PDF	Dec 13, 2017
FA8203-18-R-0002_ATLAS_3Ref_Reports.pdf	PDF	Dec 13, 2017
ATLAS_3_-_KC-135_MLG_USS_Redesign_SOO_Amendment_01.pdf	PDF	Dec 5, 2017
ATLAS_3_-_PWS.pdf	PDF	Nov 21, 2017
ATLAS_3-Section_M.pdf	PDF	Nov 21, 2017
ATLAS_3_-_CDRLS.pdf	PDF	Nov 21, 2017
FA8203-18-R-0002_ATLAS_3_TDP_Docs.pdf	PDF	Nov 21, 2017
ATLAS_3_-_Section_L.pdf	PDF	Nov 21, 2017
ATLAS_3_-_KC-135_MLG_USS_Redesign_SOO.pdf	PDF	Nov 21, 2017
FA820318R0002-ATLAS_3_RFP.pdf	PDF	Nov 21, 2017

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ENGINEERING ORDER

1. ENGINEERING ORDER NO.

15A6019-H

DATE: 20150513 Page 1 of 2

2. DWG TITLE

ROLLER ASSY – SIDE STRUT, MLG

3. DWG CAGE CODE

81205

4. DWG NO.

3-95622

5. NEXT ASSY

458-56125

6. USED ON

KC-135 AIRCRAFT

7. OPR CAGE CODE

98747

DWG SIZE

DWG SHEET(S)

LATEST DWG REV LTR

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

ADVANCE CHANGE ERROR CORRECTION

DEVIATION AUTHORIZED DESIGN CHANGE 15. NDI SYMBOL DATE

CHANGE NOTICE DRAWING CLARIFICATION

INFORMATION X UPDATED DRAWING 12. EO PREPARED/REQUESTED BY

1 Lt John Hukka

SYMBOL

GUEA

DATE

20150512

16. SYMBOL DATE

X AESO

PHONE

801-775-6251

17. DWG CHANGED BY SYMBOL DATE

10. DISPOSITION OF SPARES OTHER COMMENTS:

Update to Drawing Specifications

REWORK

MODIFY 13. ENGINEERING APPROVAL

Chad Hogan

18. CHANGE CHECKED BY SYMBOL DATE

SCRAP

REPLACE PHONE

801-777-5739

19. EO/DWG RELEASED BY SYMBOL DATE

X REPLENISHMENT

20. DESCRIPTION OF CHANGES/REMARKS

This AESO is utilized for part number: 3-95622:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 3-95622 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing 201416605 Landing Gear Requirements Document (LGRD) as indicated:

Was Is Drawing Process Drawing Note Key Word LGRD Paragraph

N/A N/A MRB 5.1.1

Dimension and Tolerance Notes Dimension and Tolerance 4.2 Form Notes Form 10.10 Punch, Straighten Notes Fabricate 10.9 Machine Notes Machine 10.8 Part Marking (BAC 5307) Notes Part Marking 6.7.1 Surface Roughness (BACD2097) Notes Surface Roughness 4.1 Bushing Installation Notes Bushing Installation 12.1

DISTRIBUTION STATEMENT B

DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES ONLY:

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C. 2751 ET SEQ.) OR THE EXPORT ADMINISTRATION ACT OF 1979, AS AMENDED, TITLE 50, U.S.C., APP, 2401, ET SEQ. VIOLATION OF THESE EXPORT CONTROL LAWS IS SUBJECT TO SEVERE CRIMINAL PENALTIES. DISSEMINATION OF THIS DOCUMENT IS CONTROLLED UNDER DOD DIRECTIVE 5230.25

DESTRUCTION NOTICE

DESTROY BY ANY METHOD THAT WILL PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF THE DOCUMENT.

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

1231478198C

Typewritten Text

AFLCMC/LZPEM

2015-07-07

1012269516C

E3 /

, 65-3792

(Continuation Sheet)

15A6019-H

DATE: 20140513 Page 2 of 2

2. DWG TITLE 3. DWG CAGE CODE

ROLLER ASSY – SIDE STRUT, MLG 81205

5. DESCRIPTION OF CHANGES/REMARKS

B. Install Bolts and Nuts using best aircraft industry standards in lieu of BAC 5009.

C. “2012 Rights Guard Licensing Agreement” applies .The data required to manufacture this item is claimed to be P roprietary to Boeing. The right of the government to use the data to purchase this part from additional sources has been established under the "2012 Rights Guard Licensing Agreement” contract # FA8119-12-D-0015, t o provide DOD procuring agencies the use of data for competitive re-procurement of replenishment spares.

D. The following drawings are not required for manufacture and will not be furnished: BAC5602, BAC5004, D2-5000, AND D6-5000, BAC 5300, BAC

5009, BACD2074.

E. No material substitution in lieu of 65-88700.

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:09:27-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:17:04-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:40:47-0600

HEUGLY.WENDY.T.1231478198

15A6034-H

ARM – ROLLER SUPPORT SIDE STRUT, MLG

82918

458-56128

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 458-56128:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 458-56128 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

B. This item has been designated a Critical Safety Item (CSI). The Critical Characteristics described are as follows:

1. CSI Heat Treat

2. CSI Grind

N/A N/A MRB 5.1.1

Dimension and Tolerance Notes Dimension and Tolerance 4.2 Drill, Ream and Hone N/A Drill, Ream and Hone 10.3 Surface Texture GN 993 Surface Roughness 4.1

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

15A6034-H

2. DWG TITLE 3. DWG CAGE CODE

ARM – ROLLER SUPPORT SIDE STRUT, MLG 82918

3. CSI Inspection

4. CSI Material

C. “GPLR” APPLIES - The data required to manufacture this item is claimed to be proprietary to Boeing. The right of the government to use the data to purchase this part from additional sources has been established under the “Government Purpose License Rights” (GPLR) settlement agreement in CL. CT. #309-89C, to provide DOD procuring agencies the use of data for competitive re-procurement of replenishment spares.

D. Mark per drawing instructions and MIL-STD-130 in lieu of BAC5307. The drawing contains all marking instructions.

E. In lieu of finish code F-1.10: No finish is required except that temporary corrosion protection during handling, transportation and storage may be applied per MIL-PRF-16173 class II grade 3 or MIL-C-11796, class 3.

F. Break all sharp corners using best aircraft industry standards in lieu of BAC5300 (See GN 1).

G. The following drawings are not required for manufacture and will not be furnished: D2-5000, BACD5307, BACD2097, and 5-83006

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:19:25-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:17:45-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:46:49-0600

HEUGLY.WENDY.T.1231478198

15A6016-H

DATE: 20150513 Page 1 of 3

SIDE STRUT ASSY - UPPER MAIN, LANDING GEAR

200310057

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT.

MON.

SYMBOL DATE

Lt John Hukka

This AESO is utilized for part number: 458-56125-1:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 458-56125 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

N/A N/A MRB 5.1.1

Prime(F-12.37) -1, -3 notes Prime 11.7.2 Paint (F-12.101) -1, -3 notes Paint 11.7.3 Cadmium Plate (F-1.76) -3 notes LHE Zn-Ni Plate 11.1.2 Heat Treat -3 notes Heat Treat 8.1.1 Inspection N/A Temper Etch 7.6 Bushing Installation FL 6 Bushing Installation 12.1 Shot Peen FL 11 Shot Peen 10.2

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

20150714

15A6017-H

DATE: 20150513 Page 2 of 3

2. DWG TITLE 3. DWG CAGE CODE

SIDE STRUT ASSY - UPPER MAIN, LANDING GEAR 82918

B. This item has been designated a Critical Safety Item (CSI). The Critical Characteristics described are as follows:

2. CSI Grind

3. CSI Inspection

4. CSI Material

5. CSI Chrome Plating (Subassembly Components)

6. CSI Magnetic Particle Inspection (Forging/Subassembly Components)

7. CSI Fluorescent Penetrant Inspection (Subassembly Components)

D. Part Marking per MIL-STD-130 and IUID per Engineering Order 09A3097-H in lieu of BAC5307.

E. Apply one coat epoxy waterborne Primer per MIL-PRF-85582, Type I, Class C2 or N. Alternate one coat of epoxy polyamide primer per MIL-PRF- 23377, Type I, Class C2 and wipe off while still wet in lieu of 458-56002 (see FL 8).

F. Utilize grease per MIL-PRF-23827 to meet drawing requirements in lieu of BAC5008 and MIL-G-23827.

G. Weld per AWS D17.1 to meet drawing requirements in lieu of BAC5975. Use MIL-E-22200/8 in lieu of MIL-E-16589. Wire per SAE AMS6466 in lieu of AMS6466 (See FL15).

H. Installation of Safety Devices per AIA/NAS NASM 33540 in lieu of BAC5018 (See FL 16).

I. Nital Etch Inspect per MIL-STD-867 to meet drawing requirements in lieu of BAC5436 (See FL 20).

Threads (H-28) FL 9 Threads 10.5 Grind GN 22 Grind 10.1 Machine GN 22 Machine 10.8 Hole Preparation GN 22 Drill, Ream, and Hone 10.3 Surface Texture GN 23 Surface Roughness 4.1 Dimensioning and Tolerancing Std Drawing Notes Dimensioning and Tolerancing 4.2

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

15A6017-H

DATE: 20150513 Page 3 of 3

2. DWG TITLE 3. DWG CAGE CODE

SIDE STRUT ASSY - UPPER MAIN, LANDING GEAR 82918

J. Refer to AWS D17.1 for weld symbol explanation in lieu of BACD2022 (See GN931)

K. The following drawings are not required for manufacture and will not be furnished: 458-56002, D3-6002, BACD2097, D2-5000, BACD2074, BAC

5004, BAC 5047, D6-5000, D8-5000, and BAC 5005.

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:07:59-0600

HUKKA.JOHN.H.1148820488

2015-07-14T09:27:16-0600

HOGAN.CHAD.C.1243849396

2015-07-14T09:41:11-0600

HEUGLY.WENDY.T.1231478198

15A6036-H

SIDE STRUT, UPPER FORGE, ROUGH MACH & SWAGE, MLG

458-56126

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 458-56126:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 458-56126 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

N/A N/A MRB 5.1.1

300M Steel -3 notes 300m Steel Bars, Forgings & Tubing 9.1 Normalize, Subcritical Anneal -3 notes Heat Treat 8.1.1 Magnetic Particle Inspect (BAC 5424) -1, -2 notes, GN 13 Magnetic Particle Inspect 7.1 Forging Inspection (D3-6002) FL 8, FL 10 Forge and Inspect 13.1 Heat Treat (Coupons) FL 8, FL 12 Heat Treat 8.1.1

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

2. DWG TITLE 3. DWG CAGE CODE

SIDE STRUT, UPPER FORGE ROUGH MACH & SWAGE, MLG, 82918

A. (Continued)

B. This item has been designated a Critical Safety Item (CSI). The Critical Characteristics described are as follows:

2. CSI Inspection

3. CSI Material

4. CSI Magnetic Particle Inspection

D. Forging Source and Location of Forging dies:

1. Forging drawing: 458-56126-3 (82918) Boeing

a) Die #: 4828P

b) Location of forging dies:

Park-Ohio Industries Inc/Park Dropp Forge Div Kropp 5301 W. Roosevelt Rd.

Cicero, IL 60804

c) Poc: Rochelle Kosmos

d) Phone: (708) 652-6691 ext. 324

e) Cage: 1Y4W9

f) Email: rkosmos@park-ohio.com

Forge FL 8, GN 51 Forging Requirements 13.2 Form (BAC 5300) GN 912 Form 10.10 Surface Roughness GN 5, GN 933 Surface Roughness 4.1

Dimension and Tolerance Notes Dimension and Tolerance 4.2

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2. DWG TITLE 3. DWG CAGE CODE

F. Part marking per drawing instructions and MIL-STD-130 in lieu of BAC5307. The drawing contains all marking instructions.

G. Sulfamate Nickel Plate per SAE AMS-QQ-N-290, Class 1, Grade G in lieu of BAC5746 (See -2 notes and FL 7).

H. The following drawings are not required for manufacture and will not be furnished: BAC5307, 458-56002, D3-6002, D2-5000, and BACD2097.

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:20:55-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:18:05-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:47:48-0600

HEUGLY.WENDY.T.1231478198

15A6021-H

ROLLER – SIDE STRUT, MLG

3-95623

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 3-95623:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 3-95623 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

N/A N/A MRB 5.1.1

Dimension and Tolerance Notes Dimension and Tolerance 4.2 Part Marking (MK T) -MD Notes Part Marking (Bag and Tag) 6.7.1 Cadmium Plating (F-1.181) -MD Notes LHE Zn-Ni 11.1.2 Material (4330 Steel) -MD Notes Material 9.6 or 9.7 Heat Treat (BAC 5617) -MD Notes Heat Treat 8.1.1 Chrome Plate (F-15.04) FL 3 Chrome Plate 11.3.3 Machine GN 1 Machine 10.8

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

15A6021-H

2. DWG TITLE 3. DWG CAGE CODE

ROLLER – SIDE STRUT, MLG 81205

B. Install Bolts and Nuts using best aircraft industry standards in lieu of BAC 5009.

D. The following drawings are not required for manufacture and will not be furnished: BAC5602, BAC5004, D2-5000, AND D6-5000, BAC 5300, BAC

5009, BAC 2074.

E. No material substitution in lieu of 65-88700.

Magnetic Inspect (BAC5424, MIL-I-6868) GN 3 Magnetic Particle Inspection 7.1 Shot Peen (BAC5424, MIL-S-13165) GN 4 Shot Peen 10.2 Form Notes Form 10.10 Punch, Straighten Notes Fabricate 10.9

N/A N/A Temper Etch 7.6

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:11:02-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:15:03-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:41:44-0600

HEUGLY.WENDY.T.1231478198

SIDE STRUT, UPPER FORGE, ROUGH MACH & SWAGE, MLG

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 458-56126:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 458-56126 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

N/A N/A MRB 5.1.1

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

2. DWG TITLE 3. DWG CAGE CODE

B. This item has been designated a Critical Safety Item (CSI). The Critical Characteristics described are as follows:

2. CSI Inspection

3. CSI Material

4. CSI Magnetic Particle Inspection

D. Forging Source and Location of Forging dies:

1. Forging drawing: 458-56126-3 (82918) Boeing

a) Die #: 4828P

b) Location of forging dies:

c) Poc: Rochelle Kosmos

d) Phone: (708) 652-6691 ext. 324

e) Cage: 1Y4W9

f) Email: rkosmos@park-ohio.com

Forge FL 8, GN 51 Forging Requirements 13.2 Form (BAC 5300) GN 912 Form 10.10 Surface Roughness GN 5, GN 933 Surface Roughness 4.1

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2. DWG TITLE 3. DWG CAGE CODE

F. Part marking per drawing instructions and MIL-STD-130 in lieu of BAC5307. The drawing contains all marking instructions.

G. Sulfamate Nickel Plate per SAE AMS-QQ-N-290, Class 1, Grade G in lieu of BAC5746 (See -2 notes and FL 7).

H. The following drawings are not required for manufacture and will not be furnished: BAC5307, 458-56002, D3-6002, D2-5000, and BACD2097.

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:20:55-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:18:05-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:47:48-0600

HEUGLY.WENDY.T.1231478198

16A6313

DATE: PAGE: 1 of 2

2. DRAWING TITLE

ROLLER SIDE STRUT, MLG

3. DRAWING CAGE CODE

4. DRAWING NUMBER

5. NEXT ASSY DRAWING

KC-135 / E-3 LANDING GEAR

LATEST DWG REV LETTER

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other)

DEVIATION AUTHORIZED DESIGN CHANGE

INFORMATION X UPDATED DRAWING 12. EO PREPARED / REQUESTED BY

Jeff Naylor

GUEA 6/13/2016 X AESO

UPDATE TO DRAWING SPECIFICATIONS 801-777-5817 REWORK

GUEA 6/13/2016 SCRAP

REPLACE

801-777-5739 X REPLENISHMENT

DISTRIBUTION AUTHORIZED TO DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS ONLY; ADMINISTRATIVE OR OPERATIONAL USE. 6/13/2016. REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS

This AESO is utilized for dash number 3-95623 only.

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following drawing notes on drawing 3-95623 and parts list 3-95623 are superseded by the corresponding paragraphs from USAF drawing

Was IS

NA NA MRB 5.1.1

Machine (BAC 5440) NA Machine 10.8 Surface Roughness NA Surface Roughness 4.1 Dimension and Tolerance NA Dimension and Tolerance 4.2 Tag Note Part Marking 6.7.1 Material: 4330 Steel (AMS 6427) FL 1 Material: 4330 Steel 9.6 Optional Material: 4330 Steel (AMS 6411) FL 1 Optional Material: 4330 Steel 9.7 Heat Treat: 220-240 KSI (BAC 5617) Notes Heat Treat 8.1.1 Magnetic Inspect (BAC 5424) Notes Magnetic Particle Inspection 7.1

THIS AESO SUPERSEDES AESO 15A6021-H

1092629054C

20160706

1092629054C

AFLCMC/LZPEX

1281238406E

20160711

AFLCMC/LZPEX

16A6313

DATE: PAGE: 2 of 2

2. DRAWING TITLE 3. DRAWING CAGE CODE

4. DRAWINGG NUMBER

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

Was IS

Shot Peen (BAC 5730) Note Shot Peen 10.2 Chrome Plate (F-15.04) FL 3 Chrome Plate 11.3.2 Cadmium Plate (F-1.181) FL 4 LHE Zn-Ni 11.1.1

B. The following drawings are not required for manufacture and will not be furnished: BAC5602, BAC5004, D2-5000, D6-5000, BAC5300, BAC5009 and BAC2074.

2016-07-06T14:48:08-0600

PEREZ.DANIEL.P.1092629054

2016-07-11T09:40:03-0600

KINGSFORD.SCOTT.GEORGE.1281238406

15A6032-H

ROLLER SUPPORT ARM FORGING – SIDE STRUT, MLG

458-56129

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 458-56129:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 458-56129 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

N/A N/A MRB 5.1.1

Material Notes 300M Steel Bars, Forgings & Tubings 9.1 Heat Treat Notes Heat Treat 8.1.1 Serial Number (BAC 5307) FL 7 Marking 6.7.1 Drill, Ream and Hone N/A Drill, Ream and Hone 10.3 Forge and Inspect GN 2 Forge and Inspect 13.1.1 Forge GN 2 Forging Requirements 13.2

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

15A6032-H

2. DWG TITLE 3. DWG CAGE CODE

ROLLER SUPPORT ARM FORGING – SIDE STRUT, MLG 82918

458-56129

B. Forging Source and Location of Forging dies:

Forging drawing: 458-56129-1 (98897) Lockheed Martin

A) Die #: 7643

1) Location of forging dies:

2) Poc: Rochelle Kosmos

3) Phone: (708) 652-6691 ext. 324

4) Cage: 1Y4W9

5) Email: rkosmos@park-ohio.com

C. This item has been designated a Critical Safety Item (CSI). The Critical Characteristics described are as follows:

i. CSI Heat Treat

ii. CSI Material

D. “GPLR” APPLIES - The data required to manufacture this item is claimed to be proprietary to Boeing. The right of the government to use the data to purchase this part from additional sources has been established under the “Government Purpose License Rights” (GPLR) settlement agreement in CL. CT. #309-89C, to provide DOD procuring agencies the use of data for competitive re-procurement of replenishment spares.

E. In lieu of finish code F-1.10: No finish is required except that temporary corrosion protection during handling, transportation and storage may be applied per MIL-PRF-16173 Class II.

F. Part marking per drawing instructions and MIL-STD-130 in lieu of BAC5307.

G. D2-5000 is not required for manufacture and will not be furnished.

Form GN 912 Form 10.10

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

mailto:rkosmos@park-ohio.com

2015-05-12T14:18:24-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:18:36-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:46:12-0600

HEUGLY.WENDY.T.1231478198

15A6029-H

BUSHING – SIDE STRUT, UPPER MLG

458-56131

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 458-56131:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 458-56131 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

N/A N/A MRB 5.1.1

Surface Roughness GN 5, GN 933 Surface Roughness 4.1 Drill, Ream and Hone N/A Drill, Ream and Hone 10.3 Part Marking FL 3, GN 915 Part Marking 6.7.1 Dimension and Tolerance Notes Dimension and Tolerance 4.2 Cadmium Plate (F 4.20) -MD Notes LHE Zn-Ni Plate 11.1.2 Penetrant Inspect (BAC5423) GN 924 Fluorescent Penetrant Inspection 7.2

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

15A6029-H

3. DWG CAGE CODE:

458-56131

B. “GPLR” APPLIES - The data required to manufacture this item is claimed to be proprietary to Boeing. The right of the government to use the data to purchase this part from additional sources has been established under the “Government Purpose License Rights” (GPLR) settlement agreement in CL. CT. #309-89C, to provide DOD procuring agencies the use of data for competitive re-procurement of replenishment spares.

C. Material: Nickel Aluminum Bronze material to meet drawing requirements per SAE AMS 4590 in lieu of AMS 4590. Alternate material, use SAE

AMS 4881 in lieu of AMS 4881.

D. Part marking per drawing instructions and MIL-STD-130 in lieu of BAC5307.

E. Break all sharp corners using best aircraft industry standards to meet drawing requirements in lieu of BAC5300.

F. The following drawings are not required for manufacture and will not be furnished: D2-5000, BAC5307, BAC5300, BAD52097

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:16:19-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:17:29-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:44:22-0600

HEUGLY.WENDY.T.1231478198

15A6022-H

BUSHING – SIDE STRUT, MLG

3-95624

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 3-95623:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 3-95623 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

Dimension and Tolerance Notes Dimension and Tolerance 4.2 Part Marking (MK T) -MD Notes Part Marking (Bag and Tag) 6.7.1 Form Notes Form 10.10 Punch, Straighten Notes Fabricate 10.9

Bushing Installation Notes Bushing Installation 12.1

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

20150714

15A6022-H

2. DWG TITLE 3. DWG CAGE CODE

BUSHING – SIDE STRUT, MLG 81205

3-95624

B. Material Aluminum Nickel Bronze per SAE AMS 4640 in lieu of AMS 4640.

C. Install anti-friction (rolling element) and friction (sliding element) bearings with a thin film of MIL-PRF-23827 grease applied to mating surfaces of bearing and housing in lieu of F-12.42.

D. “2012 Rights Guard Licensing Agreement” applies .The data required to manufacture this item is claimed to be P roprietary to Boeing. The right of the government to use the data to purchase this part from additional sources has been established under the "2012 Rights Guard Licensing Agreement” contract # FA8119-12-D-0015, t o provide DOD procuring agencies the use of data for competitive re-procurement of replenishment

E. The following drawings are not required for manufacture and will not be furnished: BAC5602, BAC5004, D2-5000, AND D6-5000, BAC 5300, BAC

F. No material substitution in lieu of 65-88700.

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

1 ENGINEERING ORDER NO 15A6022H:

Page 1 of 2:

2 DWG TITLE BUSHING SIDE STRUT MLG:

3 DWG CAGE CODE 81205:

4 DWG NO 395624:

5 NEXT ASSY 395622:

6 USED ON KC135 AIRCRAFT:

7 OPR CAGE CODE 98747:

DWG SIZE:

8 TYPE OF ENGINEERING ORDERRow1:

9 REASONS FOR CHANGEADVANCE CHANGE:

ERROR CORRECTION:

8 TYPE OF ENGINEERING ORDERRow2:

9 REASONS FOR CHANGEDEVIATION AUTHORIZED:

DESIGN CHANGE:

8 TYPE OF ENGINEERING ORDERRow3:

9 REASONS FOR CHANGECHANGE NOTICE:

DRAWING CLARIFICATION:

11 DOCUMENTS AFFECTED TOTCTOSPECOther:

14 CORROSION CONT MON:

SYMBOL:

DATE:

15 NDI:

SYMBOL_2:

DATE_2:

8 TYPE OF ENGINEERING ORDERRow4:

INFORMATION:

XAESO:

UPDATED DRAWINGAESO:

SYMBOL GUEA:

16:

SYMBOL_3:

DATE_3:

10 DISPOSITION OF SPARESRow1:

REWORK:

10 DISPOSITION OF SPARESRow2:

MODIFY:

10 DISPOSITION OF SPARESRow3:

SCRAP:

10 DISPOSITION OF SPARESRow4:

REPLACE:

X_2:

REPLENISHMENT:

OTHER COMMENTS Update to Drawing Specifications:

PHONE 8017756251:

17 DWG CHANGED BY:

SYMBOL_4:

DATE_4:

SYMBOL GUEA_2:

18 CHANGE CHECKED BY:

SYMBOL_5:

DATE_5:

PHONE 8017775739:

19 EODWG RELEASED BY:

SYMBOL_6:

DATE_6:

Was:

Is:

NA:

MRB:

Dimension and Tolerance:

Dimension and Tolerance_2:

Part Marking MK T:

Part Marking Bag and Tag:

Form:

Form_2:

Punch Straighten:

Fabricate:

Surface Roughness:

Bushing Installation:

Bushing Installation_2:

ENGINEERING ORDER Continuation Sheet:

Page 2 of 2:

2 DWG TITLE BUSHING SIDE STRUT MLG_2:

4 DWG NO 395624_2:

5 DESCRIPTION OF CHANGESREMARKS B Material Aluminum Nickel Bronze per SAE AMS 4640 in lieu of AMS 4640 C Install antifriction rolling element and friction sliding element bearings with a thin film of MILPRF23827 grease applied to mating surfaces of bearing and housing in lieu of F1242 D 2012 Rights Guard Licensing Agreement applies The data required to manufacture this item is claimed to be P roprietary to Boeing The right of the government to use the data to purchase this part from additional sources has been established under the 2012 Rights Guard Licensing Agreement contract FA811912D0015 t o provide DOD procuring agencies the use of data for competitive reprocurement of replenishment spares E The following drawings are not required for manufacture and will not be furnished BAC5602 BAC5004 D25000 AND D65000 BAC 5300 BAC 5009 BAC 2074 F No material substitution in lieu of 6588700:

2015-05-12T14:12:26-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:15:48-0600

HOGAN.CHAD.C.1243849396

2015-07-14T10:34:45-0600

HEUGLY.WENDY.T.1231478198

15A6025-H

WASHER – SIDE STRUT, MLG

3-95625

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 3-95625:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 3-95625 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

Dimension and Tolerance Notes Dimension and Tolerance 4.2 Part Marking (MK R, BAC 5307) -MD Notes Part Marking (Rubber Stamp) 6.7.1 Form Notes Form 10.10 Punch, Straighten Notes Fabricate 10.9

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

15A6025-H

DATE: 20140420 Page 2 of 2

2. DWG TITLE 3. DWG CAGE CODE

WASHER – SIDE STRUT, MLG 81205

3-95625

B. Material Aluminum Nickel Bronze per SAE AMS 4640 in lieu of AMS 4640.

D. The following drawings are not required for manufacture and will not be furnished: BAC5602, BAC5004, D2-5000, AND D6-5000, BAC 5300, BAC

E. No material substitution in lieu of 65-88700/BAC 5005.

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:13:29-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:20:20-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:42:35-0600

HEUGLY.WENDY.T.1231478198

15A6031-H

458-56132

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 458-56132:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 458-56132 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

N/A N/A MRB 5.1.1

Dimension and Tolerance Notes Dimension and Tolerance 4.2 Cadmium Plate (F 4.20) Notes LHE Zn-Ni Plate 11.1.2 Part Marking FL 3, GN 915 Part Marking 6.7.1 Surface Texture GN 6 Surface Roughness 4.1

Penetrant Inspect (BAC5423) GN 924 Fluorescent Penetrant Inspection 7.2

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

15A6031-H

2. DWG TITLE 3. DWG CAGE CODE

BUSHING – SIDE STRUT, UPPER MLG 82918

458-56132

B. Material: Aluminum Nickel Bronze per SAE AMS4590 in lieu of AMS 4590. Alternate Material per SAE AMS4881 in lieu of AMS4881.

D. Part marking per drawing instructions and MIL-STD-130 in lieu of BAC5307.

E. Break all sharp corners using best aircraft industry standards to meet drawing requirements in lieu of BAC5300.

F. The following drawings are not required for manufacture and will not be furnished: D2-5000, BAC5307, BAC5300, BACD2097.

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:17:29-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:18:50-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:45:19-0600

HEUGLY.WENDY.T.1231478198

15A6026-H

WASHER – ROLLER RETAINER, MLG

3-95626

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

This AESO is utilized for part number: 3-95626:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 3-95626 and associated Parts Listing are superseded by the corresponding paragraphs from USAF drawing

Dimension and Tolerance Notes Dimension and Tolerance 4.2 Part Marking (MK R, BAC 5307) -MD Notes Part Marking (Rubber Stamp) 6.7.1 Cadmium Plate (F-1.20) -MD Notes LHE Zn-Ni 11.1.2 Form Notes Form 10.10 Punch, Straighten Notes Fabricate 10.9

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

15A6026-H

2. DWG TITLE 3. DWG CAGE CODE

WASHER – ROLLER RETAINER, MLG 81205

3-95626

B. Material shall be 4130 Steel per SAE AMS 6350 in lieu of AN-QQ-S-685 and AN-S-12.

D. The following drawings are not required for manufacture and will not be furnished: BAC5602, BAC5004, D2-5000, AND D6-5000, BAC 5300, BAC

E. No material substitution in lieu of 65-88700/BAC 5005.

AF IMT 3926, 20030819, V1 REPLACES AF FORM 2601, 19940701, WHICH IS OBSOLETE

2015-05-12T14:14:40-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:16:14-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:43:34-0600

HEUGLY.WENDY.T.1231478198

15A6015-H

DATE: 20150513 PAGE 1 OF 1 PAGES

SIDE STRUT ASSY - UPPER

200310057

200310056

8. TYPE OF ENGINEERING ORDER 9. REASONS FOR CHANGE 11. DOCUMENTS AFFECTED (TO/TCTO/SPEC/Other) 14. CORROSION CONT. MON. SYMBOL DATE

20. DESCRIPTION OF CHANGES/REMARKS:

This AESO is utilized for part number: 200310057-10:

1. The following specifications/standards, etc., will be used in lieu of the data indicated. The superseded data will not be furnished unless so indicated.

A. The following notes from drawing 200310057 and Parts Listing are superseded by the corresponding paragraphs from USAF drawing 201416605 Landing Gear Requirements Document (LGRD) as indicated:

B. “2012 Rights Guard Licensing Agreement” applies .The data required to manufacture this item is claimed to be Proprietary to Boeing. The right of the government to use the data to purchase this part from additional sources has been established under the "2012 Rights Guard Licensing Agreement” contract # FA8119-12-D-0015, to provide DOD procuring agencies the use of data for competitive re-procurement of replenishment spares.

C. This assembly has been designated a Critical Safety Item (CSI). Critical Characteristics of the assembly are identified in the subassembly drawings/engineering orders.

Dimension and Tolerance 2 Dimension and Tolerance 4.2

AF IMT 3925, 20030819, V1 REPLACES AF FORM 2600, 19940701, WHICH IS OBSOLETE

PROPRIETARY INFORMATION (03-04-08). REFER OTHER REQUESTS FOR THIS DOCUMENT TO 417 SCMS/GUEA, HILL AFB, UT 84056.

WARNING

2015-05-12T14:05:25-0600

HUKKA.JOHN.H.1148820488

2015-05-19T12:16:31-0600

HOGAN.CHAD.C.1243849396

2015-07-07T14:38:53-0600

HEUGLY.WENDY.T.1231478198

File details come from the government source that posted it.