Statement_of_Work_with_Attachments.pdf

24 April 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.

3. First Article Testing (FAT):

1. The purpose of this section is to detail the work required to fulfill the First Article Testing component of this contract.

a. FAT shall be required of any contractor who has not undergone, completed and received FAT approval for the item purchased under this contract, and has produced it for the USAF within the last 60 months.

2. This is an Air Force designated Critical Safety Item (CSI). All requests for waivers or deviations must be forwarded to the contracting officer for review and approval.

3. FAT shall be coordinated through the Air Force AAS Engineer, Mr. Christopher Peisher. Contact information is listed below:

a. AAS Engineer Point of Contact Christopher S. Peisher Aircraft Arresting Systems Engineer

WRLCMC/WNZEC

235 Byron St., Suite 19A Robins AFB GA 31098-1813 Christopher.peisher@robins.af.mil 478-222-1371

4. The Delivery Period shall be adjusted if a FAT is required. The timeline to conduct the FAT shall be as follows:

a. Submit First Article to CEMIRT: 180 days Government Review: 30 days Delivery Period for Remaining Balance: 150 days

b. The contractor shall have a total of 180 days to produce their first article for government testing. Should the contractor produce this article prior to the completion of this 180 day period, the contractor will have the remaining time to correct any deficiencies noted during the FAT. For example, if the first article is produced within 120 days, the contractor will have 60 days to correct any deficiencies identified and return the item for additional testing. This total period shall not exceed 180 days.

i. The first article shall be considered as having been provided to the government for FAT on the date that it arrives at Tyndall CEMIRT for testing. Additionally, the date that notification of First Article deficiencies is provided to the contractor shall be considered the date that the contractors period for FAT submittal recommences.

c. Any return of a First Article for correction of deficiencies shall be at the contractor’s expense.

5. First Article Testing shall be conducted as follows:

a. Testing will be in accordance with applicable drawings, specifications and/or engineering instructions. The First Article offered shall be manufactured at the facilities in which production quantities are procured and produced under this contract.

b. Third Party Verification – The contractor shall be responsible for providing third party lab verification of all characteristics of the item to include all dimensions, materials, welds, hardware and components. These shall be verified by visual inspection, inspection of material certifications, inspection of welder’s certifications and inspection of shipment invoices.

Documentation of successful third party verification shall be included with the First Article.

c. Form, Fit and Function Check – The contractor shall provide the First Article Tyndall CEMIRT for inspection. When submitting the First Article for government testing, a copy of the contract and all applicable drawings, specifications, engineering instructions, certifications and inspection sheets (to include all applicable data identified during third party verification) shall be provided. Additionally, First Article packaging must be clearly marked as “FIRST ARTICLE TEST EXHIBIT.” Tyndall CEMIRT shall perform a form, fit and function check verifying all operational aspects of the first article.

6. Approved and conditionally approved First Articles shall be retained by the government for use. Retention of this item will qualify as the first production item.

7. Deliver Government First Article to:

a. CEMIRT

Attn: Bruce Goodwill 100 Mississippi Road Tyndall AFB, FL 32403

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

B

A

C

D

78 6 5

G

E

F

H

A

C

D

4 3 2 1

G

E

F

H

B

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

CAGE CODE

98752

AIR FORCE AUTHENTICATION

AIR FORCE RELEASE

CHK

ENG

E

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.

A

A

B

B

D

D

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

98752

JNC

JD

JJK

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3X .843 +.008 -.001

THRU 1.156

+.008 -.001

TO

DIM SHOWN IN SECTION A-A

EQUALLY SPACED

.010 A B

5X .312 +.006 -.001

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 +.006 -.001

THRU

1.25 TO CLEANUP

MACHINE PORT PER AND10050-4

-A-

-B-

8 7 6 5

C

D

A

B

4 3 1

C

D

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

CAGE CODE

98752

AIR FORCE AUTHENTICATION

AIR FORCE RELEASE

.XXX �#

.XX �#--

CHK

ENG

D

SCALE

SIZE

TITLE

DECIMALS ANGLES

DRAWING NO.

SHEET OF

ENGINEERING DRAWING LAYOUT D

APPROVEDDATEDESCRIPTIONLTR

REVISIONS

Exception to AF Form 1655 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

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.

DISTRIBUTION A: APPROVED FOR PUBLIC RELEASE.

DISTRIBUTION IS UNLIMITED. BRAKE CARRIER ASSEMBLY

F3QCDA025BG002

JNC

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JJK

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TLC

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

-10

1 1

98752

12X

NOTES:

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

51213

C

D

78 6 5

G

E

F

H

A

C

D

4 3 2 1

G

E

F

H

B

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

CAGE CODE

98752

AIR FORCE AUTHENTICATION

AIR FORCE RELEASE

CHK

ENG

E

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.

BRAKE ASSEMBLY

201018900 1/2 1 2

F3QCDA025BG002

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

-10

BAK-12 AAS201018915-10

NOTES:

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.

98752

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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

C

D

78 6 5

G

E

F

H

A

C

D

4 3 2 1

G

E

F

H

B

CAGE CODE

98752E

SCALE

SIZE DRAWING NO.

SHEET OF

ENGINEERING DRAWING LAYOUT E (Continuation Sheet)

APPROVEDDATEDESCRIPTIONLTR

REVISIONS

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

THIS DRAWING HAS BEEN GENERATED AND IS

MAINTAINED BY A CAD SYSTEM. CHANGES

SHALL ONLY BE INCORPORATED AS DIRECTED

BY THE GOVERNMENT DESIGN ACTIVITY.

75656565

14 13 12 1110

8 9

201018900

2 2

3X

4X 8X

4X

4X

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8X

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