Statement_of_Work_w_Attachments.pdf

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B

A

C

D

78 6 5

G

E

F

H

4 3 2 1

SYM

QUANTITY REQUIRED PER DASH NO.

MATERIAL/SPECIFICATIONNOMENCLATURE CAGE CODE

PARTS LIST

IDENTIFYING NO. FIND NO.UNIT WT ZONE

FRACTIONS

DIMENSIONS ARE IN INCHES-TOLERANCES ON:

UNLESS OTHERWISE SPECIFIED

CAGE CODE

CURRENT

APPLICATION

NEXT ASSEMBLY USED ON

98752

AIR FORCE AUTHENTICATION

AIR FORCE RELEASE

CHK

ENG

SCALE

SIZE

TITLE

DECIMALS ANGLES

DRAWING NO.

SHEET OF

ENGINEERING DRAWING LAYOUT E

APPROVEDDATEDESCRIPTIONLTR

REVISIONS

Exception to AF Form 1656 for CAD generation approved by HQ AFMC/ENP (AutoCAD/Au toDesk)

WR-ALC, ROBINS AFB, GA 31098

U.S. AIR FORCECONTRACT NO.

TREATMENT

SIMILAR TO

FINISH

SPECIAL MARKING SYM

TECH

DISTRIBUTION A: APPROVED FOR PUBLIC RELEASE.

DISTRIBUTION IS UNLIMITED.

.XXX �#

.XX �# �#

THIRD ANGLE PROJECTIONTHIS DRAWING HAS BEEN GENERATED AND IS

MAINTAINED BY A CAD SYSTEM. CHANGES

SHALL ONLY BE INCORPORATED AS DIRECTED

BY THE GOVERNMENT DESIGN ACTIVITY.

25.750 BC

23.50

2.200 +.010 -.000

.625

TYP30�$

B.C15.440

.004 A B

12X THRU

1.812 TO DIMENSION SHOWN

IN SECTION A-A

.566�#.002

13.250

.635�#.010

1.890 +.005 -.005

1.375 +.001 -.000

BC20.093

.330�#.005

1.875�#.001

6.600 TYP

1.720

9.280 TYP

15�$

.33

1.72

.50 +.12 -.00

BRAKE CARRIER BODY ASSY

201018898 1/1 1 1

F3QCDA025BG002

- BRAKE CARRIER BODY ASSY 98752 201018898-10 1018/1025 HR ASTM A36 1

1 BRAKE CARRIER BODY 98752 201018898-01 2

5 LEE PLUG 31356 PLGA3431020A 3

VIEW D-D

.010 A B

BAK-12 AAS201018899-10

.01 .05�$

.005

NOTES:

1. DIMENSIONS AND TOLERANCES PER ASME Y14.5-1994.

DRAWING AND RELATED DOCUMENTATION PRACTICES PER ASME Y14.1-2005.

2. BREAK ALL SHARP EDGES.

3. SURFACE TEXTURE SYMBOLS PER ASME Y14.36-1996.

4. ZINC NICKLE PLATE PER SAE AMS 2417 TYPE II. ALL DIMENSIONS APPLY AFTER PLATING.

DO NOT PLATE FEATURES NOTED.

5. REMOVE MATERIAL IN THIS AREA TO ENLARGE OPENING TANGENT TO .312 DRILLED HOLE

FOR EACH BORE.

6. METAL STAMP OR ENGRAVE PART NUMBER AND MFG CAGE CODE

WHERE SHOWN PER MIL-STD-130. CHARACTERS SHALL BE .19

HIGH MINIMUM.

-10

5X

JNC

JD

JJK

JM

TLC

3X .843 +.008 -.001

THRU 1.156

+.008

TO

DIM SHOWN IN SECTION A-A

EQUALLY SPACED

.010 A B

5X .312 +.006

11.63

.312 HOLES MUST INTERSECT 3

1.375 BORES AS SHOWN

.3430 +.0008/-.0005 .500 +.005/-.000

12X SEE SECTION A-A

MACHINE PORT PER AND10050-6

MACHINE PORT PER

AND10050-4

SECTION A-A

.03 X 45�$ CHAMFER

.02 X 30�$

SECTION B-B

.312

THRU

1.25 TO CLEANUP

MACHINE PORT PER AND10050-4

-A-

-B-

8 7 6 5

4 3 1

.XX �#--

ENGINEERING DRAWING LAYOUT D

Exception to AF Form 1655 for CAD generation approved by HQ AFMC/ENP (AutoCAD/Au toDesk)

DISTRIBUTION IS UNLIMITED. BRAKE CARRIER ASSEMBLY

201018900-10 BAK-12 AAS 201018899

1/2

- BRAKE CARRIER ASSEMBLY 98752 201018899-10 1

1 SCREW NASM35207-261 10-32 X .375 LG 10

12 WIPER 98752 201018886-1 5

12 PISTON ASSEMBLY 98752 201018897-10 3

1 BRAKE CARRIER BODY ASSY 98752 201018898-10 2

1 LOCK WASHER NASM35338-43 #10 DIA 6

1 FLARE FITTING 45681 6 FF5OX-S 3/8 37�$FLARE TO 9/16-18 STRAIGHT 13

1 O-RING AS568A-906 .468 ID X .078W 12

1 BLEEDER VALVE AN 6204-1 11

1 O RING AS28778-8 TUBE OD .500 7

1 BUSHING AS21915C-8-4 .750-16 X .437-20 8

1 SEAT BLEEDER VALVE 98752 201018895-1 4

1 O RING AS28778-4 TUBE OD .250 9

1 1

12X

1. DRAWING AND RELATED DOCUMENTATION PRACTICES PER ASME Y14.1-2005.

51213

ENGINEERING DRAWING LAYOUT E

Exception to AF Form 1656 for CAD generation approved by HQ AFMC/ENP (AutoCAD/Au toDesk)

.XX �# �#

BRAKE ASSEMBLY

201018900 1/2 1 2

8 FLAT WASHER NAS1149E0963R .562 DIA 19

8 HEX HD CAP SCREW NASM3-20AN9-11A .562-18 X 1.281 LG 18

8 HEX HD CAP SCREW NASM3-20AN9-14A .562-18 X 1.656 LG 17

16 LOCK WASHER NASM35338-49 .562 DIA 16

3 COTTER PIN NASM24665-153 .062 X .750 LG 15

3 ADJUSTER NUT 98752 201018891-1 14

3 INNER SPRING 98752 201018887-1 13

3 ADJUSTER PIN 98752 201018890-1 12

3 OUTER SPRING 98752 201018888-1 11

3 ADJUSTER CUP ASSEMBLY 98752 201018889-10 10

8 STATOR KEY SOLID 98752 201018893-1 9

4 KEY WATER NOZZLE 98752 201018892-1 8

1 BACKING PLATE ASSEMBLY 98752 9843446-10 7

3 STATOR PLATE ASSEMBLY 98752 9843443-10 6

4 ROTOR PLATE ASSEMBLY 98752 9843445-10 5

1 PRESSURE PLATE ASSEMBLY 98752 9843444-10 4

1 TORQUE TUBE 98752 201018894-1 3

1 BRAKE CARRIER ASSEMBLY 98752 201018899-10 2

- BRAKE ASSEMBLY 98752 201018900-10 1

8 SELF LOCKING NUT 2V507 92501A445 9/16-18 ASTM A563 GRADE C 20

3 4 5

BAK-12 AAS201018915-10

1. ASSEMBLE BRAKE COMPONENTS AS SHOWN.

2. PRIOR TO INSTALLING INNER SPRINGS F/N 13 AND OUTER SPRINGS F/N 11

THE FREE LENGTH OF THE THREE SPRINGS OF EACH DIAMETER SHALL BE MEASURED

AND COMPARED. THE MAXIMUM ALLOWABLE LENGTH VARIATION BETWEEN ANY TWO

SPRINGS IN THE SET OF THREE IS .020". ENDS OF LONGER SPRINGS MAY BE

GROUND SLIGHTLY TO MEET THIS REQUIREMENT OR THE SPRING MUST BE REPLACED.

3. TORQUE SELF LOCKING NUTS F/N 20 TO 41 FT.- LBS. +/- 5 FT.- LBS.

4. TORQUE CAP SCREWS F/N'S 17 & 18 TO 83 FT.- LBS. +/- 5 FT.- LBS.

5. SELF LOCKING NUTS AND CAP SCREWS SHALL BE GRADUALLY TIGHTENED

TO FINAL TORQUE VALUES IN PAIRS ALTERNATING FRONT TO BACK AND IN

A 180�$ ROTATING PATTERN.

6. ADJUSTER NUTS F/N 14 SHALL BE TIGHTENED COMPRESSING SPRINGS

F/N'S 11 & 13 TO JUST ALLOW COTTER PIN F/N 15 TO BE INSERTED FREELY.

7. INSTALL F/N 8 KEYS IN THE POSITIONS SHOWN.

8. DRAWING AND RELATED DOCUMENTATION PRACTICES PER ASME Y14.1-2005.

THE ITEM SPECIFIED BY THIS DRAWING WILL BE USED AS PART OF

A SYSTEM SUPPORTING RECOVERY OF HIGH-PERFORMANCE TAIL HOOK

EQUIPPED FIGHTER AIRCRAFT. ANY DEPARTURE FROM THE REQUIREMENTS

SPECIFIED OR REFERENCED HEREIN COULD RESULT IN LOSS OF LIFE,

SERIOUS PERSONNEL INJURY, AND/OR DAMAGE OR LOSS OF AIRCRAFT. AS

SUCH, THE ITEM HAS BEEN DESIGNATED AS A CRITICAL SAFETY ITEM

(CSI). ANY DEVIATION FROM THIS SPECIFICATION WITHOUT WRITTEN

APPROVAL FROM THE SUPPORT EQUIPMENT AND VEHICLES

DIVISION (AFMC) AT ROBINS AIR FORCE BASE, GEORGIA, IS

STRICTLY PROHIBITED.

CRITICAL SAFETY ITEM

98752E

SIZE DRAWING NO.

ENGINEERING DRAWING LAYOUT E (Continuation Sheet)

Exception to AF Form 1656A for CAD generation approved by HQ AFMC/ENP (AutoCAD/A utoDesk)

THIS DRAWING HAS BEEN GENERATED AND IS

75656565

14 13 12 1110

8 9

201018900

2 2

3X

4X 8X

4X

8X

Sheet 1

Views new_view_5 right_6 new_view_7

D

Spec 201018899.pdf

Sheet 1

Views new_view_4

Spec 201018900.pdf

Sheet 1

Views new_view_1 new_view_2

Sheet 2

Views new_view_3

THIS DRAWING HAS BEEN GENERATED AND IS

LTR DESCRIPTION DATE APPROVED

Exception to AF Form 1654 for CAD generation approved by HQ AFMC/ENP (AutoCAD/Au toDesk)ENGINEERING DRAWING LAYOUT C

CONTRACT NO. U.S. AIR FORCE

OFSHEET

ANGLESDECIMALS

.XX �#

USED ONNEXT ASSEMBLY

ZONEUNIT WT FIND NO.IDENTIFYING NO.

CAGE CODENOMENCLATURE MATERIAL/SPECIFICATION

THIRD ANGLE PROJECTION

4.00

6.25

8.38

TYP3�$

10.56

9.40

1.50

TYP3�$

TYP

3�$

1.04

90�$

201018857

201018858-10 BAK-12 AAS

SHEAVE CASTING

1/3 1 1

- SHEAVE CASTING 98752 201018857-1 SEE NOTE 2

FULL R

.38 R TYP

DRAWING AND RELATED DOCUMENTATION PRACTICES PER ASME Y14.1-2005.

2. MATERIAL SHALL BE ALUMINUM ALLOY A356-T6 SAND CASTED PER ASTM B26/B26M.

GRADE SHALL BE GRADE B OR C PER AMS 2175. CASTING INSPECTION SHALL BE CLASS 1 PER AMS 2175.

.03

Sheet 1

Views new_view_7 right_10

8 7 6 5

4 3 1

.XX �#--

ENGINEERING DRAWING LAYOUT D

Exception to AF Form 1655 for CAD generation approved by HQ AFMC/ENP (AutoCAD/Au toDesk)

.562 TYP

.001 A

5.125 +.002 -.002

-A-

4.9193 +.0016 -.0000

4.500

8.750 +.015 -.015

2.375 TYP

9.50

4.250

9.750 +.015

10.813 +.000

R 2 PLS5

TYP 4 PLS

30�$

.10 TYP 4 PLS

R TYP 2 PLS.015

R 2 PLS.09 2.500

9.250 +.000

7.13

THRU

4 PLACES

EQUALLY SPACED

.375

R 2 PLS.09

SHEAVE ASSEMBLY

X201018860-10 BAK-12 AAS 201018858

1 SHEAVE CASTING 98752 201018857-1 2

- SHEAVE ASSEMBLY 98752 201018858-10 1

1 1

.005

.01 .5�$

DRAWING AND RELATED DOCUMENTATION PRACTICES PER ASME Y14.1-2005.

2. BREAK ALL SHARP EDGES.

3. ANODIC COATING PER MIL-A-8625, TYPE III, EXCEPT FOR ALL INSIDE DIAMETERS

4. METAL STAMP OR ENGRAVE PART NUMBER AND MFG CAGE CODE WHERE SHOWN

PER MIL-STD-130. CHARACTERS SHALL BE .19 HIGH MINIMUM.

5. FINISHED PART SHALL MEET THE REQUIREMENTS OF CASTING GRADE B OR C OF

AMS 2175. CASTING INSPECTION SHALL BE CLASS 2 PER AMS 2175.

Sheet 1

Views new_view_1 right_2

ENGINEERING ORDER

1. ENGINEERING ORDER NO.

ENGINEERING ORDERAFMC Form 3925, 20150402

2. RELEASE DATE:

PAGE 1 OF PAGES

3. DWG TITLE 4. DWG ODA CAGE CODE 5. DWG NO. 6. DOC TYPE

7. NEXT HIGHER ASSY 8. USED ON 9. OPR CAGE CODE 10. DWG SIZE 11. DWG SHEET(s) AFFECTED 12. LATEST DWG REV

13. TYPE OF ENGINEERING ORDER 14. REASONS FOR CHANGE

ADVANCE ENGINEERING CHANGE ORDER (AECO)

AGAINST AIR FORCE OWNED DRAWINGS

DEVIATION AUTHORIZED

CHANGE NOTICE ENGINEERING ORDER (CNEO)

AIR FORCE CHANGES BEING INCORPORATED

INFORMATION "NON-TECHNICAL"

ADVANCED ENGINEERING SUPPLEMENTAL ORDER (AESO)

AIR FORCE REQUIREMENTS AGAINST A VENDOR OWNED DRAWING

ERROR CORRECTION

DESIGN CHANGE

DRAWING CLARIFICATION

UPDATED DRAWING

CRITICAL SAFETY ITEM (CSI)

15. EO PREPARED BY

16. CONFIG MANAGEMENT

17. DWG CHANGED BY

18. MATERIALS ENGINEER

19. CHECKER 20. CORROSION CONTROL

21. PROJECT ENGINEER 22. HCI / HARDNESS

24. ENG APPROVAL 25. NDI

23. DISPOSITION OF SPARES

N/A REWORK SCRAP REPLACE

27. AF AUTHENTICATION 28. SYSTEM SAFETY

26. DOCUMENTS AFFECTED (TO/TCTO/SPEC/OTHER)

30. AF RELEASE

29. OTHER COMMENTS

32. DESCRIPTION OF APPROVED CHANGES/REMARKS

33. DISTRIBUTION STATEMENT: (REQUIRED PER DoDI 5230.24)

SIGNATURE OFFICE SYM / PHONE OFFICE SYM / PHONESIGNATURE

31.

AFMC Form 3925, 20150402

PAGE

OF

PAGES

13. TYPE OF ENGINEERING ORDER

14. REASONS FOR CHANGE

AGAINST AIR FORCE OWNED DRAWINGS

AIR FORCE CHANGES BEING INCORPORATED

"NON-TECHNICAL"

AIR FORCE REQUIREMENTS AGAINST A VENDOR OWNED DRAWING

23. DISPOSITION OF SPARES

SIGNATURE

OFFICE SYM / PHONE

OFFICE SYM / PHONE

SIGNATURE

31.

11.0.1.20130826.2.901444.899636

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TextField1: BAK-12 AAS

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TextField1: Location D4:

WAS "MATERIAL SHALL BE ALUMINUM ALLOY A356-T6 SAND CASTED PER ASTM B26/B26M.

GRADE SHALL BE GRADE B OR C PER AMS 2175. CASTING INSPECTION SHALL BE CLASS 1 PER AMS 2175."

IS "CAST MATERIAL SHALL BE ALUMINUM ALLOY A356-T6 SAND CASTED PER ASTM B26/B26M OR BILLET 6061-T6.

GRADE SHALL BE GRADE B OR C PER AMS 2175. CASTING INSPECTION SHALL BE CLASS 1 PER AMS 2175. "

TextField1:

DISTRIBUTION STATEMENT A: Approved for public release: distribution unlimited.

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1. ENGINEERING ORDER NO.

ENGINEERING ORDERAFMC Form 3925, 20150402

2. RELEASE DATE:

PAGE 1 OF PAGES

3. DWG TITLE 4. DWG ODA CAGE CODE 5. DWG NO. 6. DOC TYPE

7. NEXT HIGHER ASSY 8. USED ON 9. OPR CAGE CODE 10. DWG SIZE 11. DWG SHEET(s) AFFECTED 12. LATEST DWG REV

13. TYPE OF ENGINEERING ORDER 14. REASONS FOR CHANGE

ADVANCE ENGINEERING CHANGE ORDER (AECO)

AGAINST AIR FORCE OWNED DRAWINGS

DEVIATION AUTHORIZED

CHANGE NOTICE ENGINEERING ORDER (CNEO)

AIR FORCE CHANGES BEING INCORPORATED

INFORMATION "NON-TECHNICAL"

ADVANCED ENGINEERING SUPPLEMENTAL ORDER (AESO)

AIR FORCE REQUIREMENTS AGAINST A VENDOR OWNED DRAWING

ERROR CORRECTION

DESIGN CHANGE

DRAWING CLARIFICATION

UPDATED DRAWING

CRITICAL SAFETY ITEM (CSI)

15. EO PREPARED BY

16. CONFIG MANAGEMENT

17. DWG CHANGED BY

18. MATERIALS ENGINEER

19. CHECKER 20. CORROSION CONTROL

21. PROJECT ENGINEER 22. HCI / HARDNESS

24. ENG APPROVAL 25. NDI

23. DISPOSITION OF SPARES

N/A REWORK SCRAP REPLACE

27. AF AUTHENTICATION 28. SYSTEM SAFETY

26. DOCUMENTS AFFECTED (TO/TCTO/SPEC/OTHER)

30. AF RELEASE

29. OTHER COMMENTS

32. DESCRIPTION OF APPROVED CHANGES/REMARKS

33. DISTRIBUTION STATEMENT: (REQUIRED PER DoDI 5230.24)

SIGNATURE OFFICE SYM / PHONE OFFICE SYM / PHONESIGNATURE

31.

AFMC Form 3925, 20150402

PAGE

OF

PAGES

13. TYPE OF ENGINEERING ORDER

14. REASONS FOR CHANGE

AGAINST AIR FORCE OWNED DRAWINGS

AIR FORCE CHANGES BEING INCORPORATED

"NON-TECHNICAL"

AIR FORCE REQUIREMENTS AGAINST A VENDOR OWNED DRAWING

23. DISPOSITION OF SPARES

SIGNATURE

OFFICE SYM / PHONE

OFFICE SYM / PHONE

SIGNATURE

31.

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WAS "MFINISHED PART SHALL MEET THE REQUIREMENTS OF CASTING GRADE B OR C OF

AMS 2175. CASTING INSPECTION SHALL BE CLASS 2 PER AMS 2175.."

IS "FINISHED PART SHALL MEET THE REQUIREMENTS OF CASTING GRADE B OR C OF

AMS 2175. CASTING INSPECTION SHALL BE CLASS 2 PER AMS 2175. OR BILLET 6061-T6."

TextField1:

DISTRIBUTION STATEMENT A: Approved for public release: distribution unlimited.

TextField1: AFLCMC/WNE-SEV

TextField1: 472-1371

TextField1: AFLCMC/WNE-SEV

TextField1: 472-1371

TextField1: AFLCMC/WNE-SEV

TextField1: 472-1825

TextField1: AFLCMC/LZPEM

TextField1: 472-3027

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20 March 2019

Statement of Work CEMIRT MAAS Parts and Equipment

1. PURPOSE: The contractor shall furnish all required parts, equipment, material, and labor to provide the following items in accordance with (IAW) all applicable codes, specifications, and industry/federal standards to CEMIRT at Tyndall AFB, Florida.

2. SCOPE:

1. Brake Carrier – P/N: 52E901‐1 – 100 Each:

a. See attachment 1.

2. Pulley, Flat (Sheave Roller) – P/N: 52E901‐1 – 120 Each:

a. See attachment 2, 3, 4, 5, and 6.

3. Plate Reel – P/N: 200622844-01 – 100 Each:

The contracting officer can provide additional engineering drawings, specifications and instructions as needed upon request.