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. USAF BAK‐12 Base – P/N: 201018916‐1 – 34 Each:

a. See attachment 1, 2, and 3.

b. Painted gloss green (MIL-PFR-852285 Rev E Type II Class H, Color Code

14052 per MIL-STD-3035 attached.)

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.

C

C

G

G

22.00

2.50 TYP

62.88

61.19

10.38

6.25

.110

9.13

67.69

11.00

29.00

2.88

3.81

81.75

.12 TYP 4X

2.75 TYP 4-PLACES

14.00

5.50

.06

12.0

24.0

4.75

3.5 TYP 2X

2.50 TYP 2X

28.38

9.50

.38 TYP

2X

3.63

TYP 2X

2.00 TYP 2X

6.00 TYP 2X

5.14 TYP 4X 29.76

29.75

84.50

11.25

6.13

BASE WELD ASSEMBLY

201018916 1/8 1 3

F3QCDA025BG002

2 PAD EYE 94658 F187-6 37

4 SUPPORT RING MOUNT 98752 201018916-81 3.5 X 3 X .5 ASTM A36 36

2 SHEAVE MOUNT STIFFENER 98752 201018916-77 ASTM A36 35

2 SHEAVE MOUNT STIFFENER TOP 98752 201018916-75 ASTM A36 34

2 ANCHOR LUG BACK PLATE 98752 201018916-73 6.0 X 5.75 X 0.5 ASTM A36 33

2 FWD STAKE TUBE 98752 201018916-71 4.5 OD X.5 WALL X 15.25L ASTM A519 32

4 FWD STAKE TUBE FLANGE 98752 201018916-67 ASTM A36 31

2 STAKE TUBE STIFFENER 98752 201018916-65 ASTM A36 30

2 ANCHOR LUG 98752 201018916-63 14.25 X 6 X 1.63 ASTM A36 29

1 SHEAVE MOUNT 98752 201018916-62 CHANNEL MC13 X 31.8 X 15.88L ASTM A36 28

1 SHEAVE MOUNT 98752 201018916-61 CHANNEL MC13 X 31.8 X 15.88L ASTM A36 27

2 SHEAVE REINFORCEMENT 98752 201018916-57 6 X 6 X .63 ASTM A36 26

1 FWD LOWER CROSSMEMBER 98752 201018916-55 ANGLE 8 X 8 X.75 28.69L ASTM A36 25

1 AFT LOWER CROSSMEMBER 98752 201018916-53 ANGLE 4 X 4 X.75 28.69L ASTM A36 24

1 TOP CROSSMEMBER 98752 201018916-51 ANGLE 8 X 4 X.5 28.69L ASTM A36 23

1 HYD CONTROL MOUNT 98752 201018916-47 9.25 X 8.0 X .88 ASTM A36 22

1 RESERVOIR MOUNT 98752 201018916-45 5.0 X 7.75 X .5 ASTM A36 21

1 CONTROL PANEL MOUNT 98752 201018916-43 4.5 X 8.5 X .25 ASTM A36 20

1 CHAIN TENSIONER MOUNT 98752 201018916-41 1.75 X 5 X 5 ASTM A36 19

1 CLUTCH PUMP MOUNT 98752 201018916-37 2.5 X 5.00 X 1.0 ASTM A36 18

1 SYNCRO GEAR MOUNT 98752 201018916-35 8.88 X 8.00 X 1.0 ASTM A36 17

1 GEAR BOX STIFFENER 98752 201018916-33 15.56 X 15.56 X .50 ASTM A36 16

1 GEAR BOX BASE 98752 201018916-31 25 X 5.5X .75 ASTM A36 15

2 REEL MOUNT BASE 98752 201018916-27 ASTM A36 14

8 REEL MOUNT STIFFENER 98752 201018916-25 5.63 X 2.13 X .75 ASTM A36 13

2 REEL MOUNT WEB 98752 201018916-23 30 X 5.63 X .75 ASTM A36 12

2 AFT STAKE TUBE 98752 201018916-21 4.5 OD X .5 WALL X 15.5L ASTM A519 11

4 AFT STAKE FLANGE 98752 201018916-17 ASTM A36 10

1 AFT BASE PLATE 98752 201018916-15 22.88" X 22" X .50 ASTM A36 9

1 MID BASE PLATE 98752 201018916-13 22 X 28 X .44 ASTM A36 8

1 FORWARD BASE PLATE 98752 201018916-11 8.63 X 22 X .50 ASTM A36 7

4 OUTER STIFFENER 98752 201018916-07 ASTM A36 6

4 INNER STIFFENER 98752 201018916-05 ASTM A36 5

1 TAPE GUIDE PLATE 98752 201018916-03 ASTM A36 4

1 I-BEAM 98752 201018916-02 W16 X 36 ASTM A36 3

1 I-BEAM 98752 201018916-01 W16 X 36 ASTM A36 2

BASE WELD ASSY 98752 201018916-10 1

NOTES:

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

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

2. WELDING AND INSPECTION PROCESS SHALL BE IN ACCORDANCE

WITH AWS D1.1 FOR CYCLICALLY LOADED STRUCTURES.ALL WELDERS

AND INSPECTORS SHALL BE CERTIFIED IN ACCORANCE WITH

AWS D1.1.

3. ESTABLISH CENTERLINE USING THE TWO .13 HOLES IN F/N 4 & F/N 23.

4. FOR F/N 3 OMIT THESE FEATURES.

5. GRIND FLUSH THIS SURFACE.

6. STRESS RELIEF PER PARA 3.20.2 ANNEALING PROCEDURE MIL-2-21157A, EXCEPT

PARA (C), WHERE THE TEMPERATURE OF THE FURNACE SHALL NOT EXCEED 600 �$F AT TIME

THE CHARGE IS LOADED.

JNC

JD

JJK

JM

TLC

BAK-1298752

-10

8X 2X

2X 2X

4X (.25)

2X TYP

2X 2X

2X

(.25)

2X TYP

(.38) 4X

2X TYP

(.25) (.25)

2X

2X

2X

.25 (.38)

TYP 2X

2X

4X

(REF)

201018919-10

4X

.25

.25

2X TYP

.03

2X

TYP 4X

.25

.25

TYP 4X

.25

F/N 3 MADE TRANSPARENT

FOR CLARITY

.25

.25

.25

.1915

.25

.5" R MIN.

36 36

.25

WRAP

.25

.25TYP

TYP

TYP

(.25)

SECTION C-C

.25

TYP 6-PLACES

.25 (.38)

.25 (.38)

SECTION G-G

.25

TYP 2X

.13

.13

.31

.31

TYP 2X

.25

AA

BB

D

D

F F

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.

2.88

2.75

.50

15.75

36.00

4.00

9.50

TYP1.56

13.25

3.75

2.50 TYP

2.50

7.00 TYP

7.00

2.00

7.50

.25

.25.125 +.006 -.001

.25

1.00

15.00

3.38

X 45�$ TYP.75

28.69

8.00 REF

8.00 REF

27.75

2.13 TYP

TYP45�$

28.69

4.00 REF

4.00 REF

27.75

1.65

.38

1.00

8.50

1.00

8.50

5.00

10.75

.50

8.00

7.75

R TYP1.0

6.00

1.63

4.69

7.0�$ 9.50

4.00

1.62

.97 6.50

201018916 2 3

.25

2X

TYP 8X

.25

TYP 2X

TYP 2X

(REF)

(REF)

(REF)

(REF)

(REF)

(REF)

(REF)

8X .812 +.008/-.001 THRU

SECTION A-A

.31

TYP 2-PLACES .25

TYP 2X

.31

.25

.25

.25

AVOID WELDING ALONG

TAPE SLOT TYP 2X

.31

.31

TYP 2X

TYP 4X

TYP 2X

2X TYP

.25

2X TYP .252X

SECTION B-B

.31

TYP 4X

.38 (.41)

TYP 2X

.38

TYP 2X

SECTION D-D

.38 .31

GRIND FLUSH

SECTION F-F

.25

.25

.31

.31

.25

.38

TYP 2X

.25

.5 X 45�$ CHAMFER TYP

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.

119.50

9.63

25.25

48.50

65.50

7.93

TYP 4X7.00

2.52 TYP 2X

2.88

R TYP1.00

7.57

4.56

3.00

67.134.13

2.95

8.13 8.56

9.00

2.50

74.639.00

6.00

2.75

15.86 (REF)

6.99 (REF)

4.50

TYP 2X7.00

.50

5.25

15.00

3.25 X 45�$ TYP.75

.50

2.50

R3.25

4.50

4.56

3.19

.8125

8.00

2.00

1.00

5.00

30.00

1.75

11.008.00

TYP45�$

15.88 REF

13.00 REF

THRU3.00

7.13

.50

6.50

2.50

1.25

.375

.125 1.00

4.56 .38

9.38

3.44

8.00

1.06.75

15.00

3.25

45�$ X CHAMFER TYP.50

28.69

4.00 REF

8.00 REF

.50

R.75

21.25

.45

1.00 TYP

.25.125 +.006 -.001.38

13.35

.25

4.50

8.50

R TYP.25

SHOWN (REF)

OPPOSITE HAND (REF)

(REF)

(REF)

(REF)

(REF)

201018916 3 3

(REF)

(REF)

(REF)

(REF)

SHOWN (REF)

OPPOSITE HAND WITH OMISSIONS (REF) 4

45�$ X .50 CHAMFER TYP

18.812

G

G

B.125

.125

.125

.125

85.000

WAS 84.50 @ F-5

62.880

11.000

5.625

WAS 5.50 @ F-6

3.500

2 PLCS

1.125

WAS .250

21.312

HOLD 6.500

18.812

30.977

4.000

C

C

ADDED P-N # 201018917 & 201018918

TO THE WELD ASSY.

P-N # 201018918 AFT ENG MNT

P-N # 201018917 FWD ENG MNT

SEE DETAIL

ITEM #21

SEE DETAIL

ITEM #20

SEE DETAIL

ITEM # 23

A A

D

SEE SHT 9

17.190

WAS 28.380 @ D-4

SEE DETAIL

ITEM #9

SEE DETAIL

ITEM #8

SEE DETAIL

ITEM #7

C

C

SECTION G-G

SECTION C-C

B

ALL DIMENSIONS NOTED REFLECT CHANGES,

FOR ALL OTHERS SEE: DWG. # 201018916 BASE WELD ASSY

PROVIDED BY THE U.S.A.F.

REVISIONS

ZONE REV. DESCRIPTION DATE APPROVED

B3 A

CHANGED

DIM PER

SAMPLE

3/13/2

TIM C., B.

GOODWILL

B3 B ADDED WELD

SYMBOLS

3/14/2

TIM C, B.

GOODWILL

C ADDED HOLES

ON ITEM 8/9

4/25/1

TIM C./ B.

GOODWILL

B3 D SEE SHT 9 FOR

DETAIL

10/9/2

TIM C/ B.

GOODWILL

D

C

B

AA

B

C

D

12345678

8 7 6 5 4 3 2 1

NEXT ASSY USED ON

APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

FINISH

MINIMUM

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:24

UNLESS OTHERWISE SPECIFIED:

C

REVISIONS ON

DWG # 201018916 SHT 1-3

SHEET 1 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

MINIMUM, UNLESS OTHERWISE NOTED.

3 : ALL BURRS TO BE REMOVED BEFORE INSPECTION.

3.000

.375

8.750

5.625

8.750

5.625

2.565 1.500

45.00°

3.125

.435

1 REQD PER ASSY

D

C

B

AA

B

C

D

12345678

8 7 6 5 4 3 2 1

NEXT ASSY USED ON

APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

L 3 X 3 X 3/8 A-53

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:2

UNLESS OTHERWISE SPECIFIED:

C

ITEM # 20 L.H.

SHEET 2 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

.375 8.750

5.625

1.500

45.00°

.435

8.750

5.625

3.000

1 REQD PER ASSY

D

C

B

AA

B

C

D

12345678

8 7 6 5 4 3 2 1

NEXT ASSY USED ON

APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

L 3 X 3 X 3/8 A-53

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:2

UNLESS OTHERWISE SPECIFIED:

C

ITEM # 20 R.H.

SHEET 3 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

7.500

7.500

.250 X 45

4 PLCS

.500

1 REQD PER ASSY

D

C

B

AA

B

C

D

12345678

8 7 6 5 4 3 2 1

NEXT ASSY USED ON

APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

1/2'' A-36

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:2

UNLESS OTHERWISE SPECIFIED:

C

ITEM # 21

SHEET 4 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

4.000

.500

2 PLCS

.450

2 PLCS

.500

2 PLCS

45.00°

2 PLCS

28.690

21.250

10.625

28.690

WAS 26.690

8.000

28.690 14.345

A

.500

8.000

4.000

DETAIL A

SCALE 1 : 4

.125 .250 DP.

D

C

B

AA

B

C

D

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8 7 6 5 4 3 2 1

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APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

L 8 X 4 X 1/2 A-53

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:8

UNLESS OTHERWISE SPECIFIED:

C

ITEM # 23

SHEET 5 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

22.000

8.500

WAS 8.630

.500

D

C

B

AA

B

C

D

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8 7 6 5 4 3 2 1

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APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

3/8 '' A-36

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:4

UNLESS OTHERWISE SPECIFIED:

C

ITEM # 7

SHEET 6 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

50.540

7.630

1.000

2.750

.500

D

C

B

AA

B

C

D

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8 7 6 5 4 3 2 1

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APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

3/8'' A-36

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:6

UNLESS OTHERWISE SPECIFIED:

C

ITEM # 8

SHEET 7 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

48.240

WAS 22.880

7.875

2.750

1.000

.500

D

C

B

AA

B

C

D

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8 7 6 5 4 3 2 1

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APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

3/8'' A-36

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:6

UNLESS OTHERWISE SPECIFIED:

C

ITEM # 9

SHEET 8 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

61.000 65.500

R3.500

WAS 7.000 HOLE

70.750

63.250

HD

R.650 2 PLCS THRU

TOP FLANGE ONLY .500

2 PLCS

DETAIL H

SCALE 1 : 5

D

REVISIONS

ZONE REV. DESCRIPTION DATE APPROVED

C-5 D ADDED .6502 RAD. 2 PLCS 10-9-17 TIM C.

D

C

B

AA

B

C

D

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8 7 6 5 4 3 2 1

NEXT ASSY USED ON

APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

W16 X 36# ASTM A-36

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:10

UNLESS OTHERWISE SPECIFIED:

C

ITEM # 2

SHEET 9 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

65.500 70.000

R3.500

WAS 7.000 HOLE

D

C

B

AA

B

C

D

12345678

8 7 6 5 4 3 2 1

NEXT ASSY USED ON

APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

W16 X 36# ASTM A-36

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:10

UNLESS OTHERWISE SPECIFIED:

C

ITEM #3

SHEET 10 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

29.750

( WAS 25.00)

5.500

.750

D

C

B

AA

B

C

D

12345678

8 7 6 5 4 3 2 1

NEXT ASSY USED ON

APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

MATERIAL

3/4'' A-36 PLT

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:4

UNLESS OTHERWISE SPECIFIED:

C

ITEM # 15

SHEET 11 OF 11

201018916-1 WELD ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

Y +

X +

D7 D8

D9 D10

D5

D6

D1

D2

B21 B22

B23B24

D3

D4

B

A

37.630

2 PLCS

1.250

2 PLCS

1.875

2 PLCS

3.630 2 PLCS

.438

4 PLCS

B

6.000

TYP

1.000

2.000 10.750

2 PLCS

3/8-16 TAPPED

THRU 4 PLCS

1 : ONLY THE REVISIONS ARE SHOWN, ALL

OTHER HOLE LOCATIONS ARE AS TO # 201018919

BASE FINISH MACHINING ASSY SEE SHT-2

FOR HOLE LOCATION CHART.

B9

B11

B13

B17B10

B12

B14 B18

B20B19

D

C

B

AA

B

C

D

12345678

8 7 6 5 4 3 2 1

THE INFORMATION CONTAINED IN THIS

DRAWING IS THE SOLE PROPERTY OF

HOLMES TOOL & ENGINEERING. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

HOLMES TOOL & ENGINEERING IS

PROHIBITED.

PROPRIETARY AND CONFIDENTIAL

NEXT ASSY USED ON

APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME Holmes Tool & Engineering

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:20

UNLESS OTHERWISE SPECIFIED:

Tim C.

REVISIONS ON

DWG# 201018919

SHEET 1 OF 2

201018919-1 MACHINING ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

General Table

HOLE LOCATION X Y DESCRIPTION

OMITT HOLES B1 THRU B8

B9 -42.060 -16.621 .437 THRU

B10 -40.500 -12.621 .437 THRU

B11 -59.250 -23.250 3/8-16 TAPPED THRU

B12 -52.250 -23.250 3/8-16 TAPPED THRU

B13 -52.250 -17.500 3/8-16 TAPPED THRU

B14 -59.250 -17.500 3/8-16 TAPPED THRU

B17 -35.125 -13.218 3/8-16 TAPPED THRU

B18 -33.562 -13.218 3/8-16 TAPPED THRU

B19 -33.562 -9.468 3/8-16 TAPPED THRU

B20 -35.125 -9.468 3/8-16 TAPPED THRU

D1 17.790 16.360 1/2-13 TAPPED THRU

D2 17.790 12.050 1/2-13 TAPPED THRU

D3 -53.710 16.125 1/2-13 TAPPED THRU

D4 -53.710 22.125 1/2-13 TAPPED THRU

D5 -33.750 +10.125 1/2-13 TAPPED THRU

D6 -36.937 -7.875 1/2-13 TAPPED THRU

D7 -37.882 -20.975 9/16 THRU

D8 -31.869 -20.975 9/16 THRU

D9 -31.869 -15.495 1/2-13 TAPPED THRU

D10 -37.882 -15.495 1/2-13 TAPPED THRU

B21 -65.004 16.410 3/8-16 TAPPED THRU

B22 -61.500 16.410 3/8-16 TAPPED THRU

B23 -61.500 22.500 3/8-16 TAPPED THRU

B24 -65.004 22.500 3/8-16 TAPPED THRU

D

C

B

AA

B

C

D

12345678

8 7 6 5 4 3 2 1

THE INFORMATION CONTAINED IN THIS

DRAWING IS THE SOLE PROPERTY OF

HOLMES TOOL & ENGINEERING. ANY

REPRODUCTION IN PART OR AS A WHOLE

WITHOUT THE WRITTEN PERMISSION OF

HOLMES TOOL & ENGINEERING IS

PROHIBITED.

PROPRIETARY AND CONFIDENTIAL

NEXT ASSY USED ON

APPLICATION

DIMENSIONS ARE IN INCHES

TOLERANCES:

FRACTIONAL 1/32

ANGULAR: MACH 1.0 BEND 2.0

TWO PLACE DECIMAL .015

THREE PLACE DECIMAL .005

INTERPRET GEOMETRIC

TOLERANCING PER:

DRAWN

CHECKED

ENG APPR.

MFG APPR.

Q.A.

COMMENTS:

DATENAME Holmes Tool & Engineering

TITLE:

SIZE

B

DWG. NO. REV

WEIGHT: SCALE: 1:20

UNLESS OTHERWISE SPECIFIED:

Tim C.

REVISION TO HOLE CHART

ON 201018919 SHT 2 &3

SHEET 2 OF 2

201018919-1 MACHINING ASSY

DO NOT SCALE DRAWING

1 : BREAK ALL SHARP EDGES .010 MIN.

UNLESS OTHERWISE NOTED.

2 : ALL MACHINED SURFACES TO HAVE A

FINISH

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