Attachment_1-_SOW.pdf

PERFORMANCE WORK STATEMENT

AFLCMC/EZPAA - Air Force Packaging and Engineering Facility (AFPTEF)

25 January 2018

1.0 Description of Service: This Performance Work Statement (PWS) provides for painting of two lots of parts, a base performance period and an option period, to support the completion of a total of four trailers used to transport the fuselage, wings and tails of an aircraft.

Lot 1: Parts and assemblies for one fuselage trailer (P/N 20141251-10)

Parts and assemblies for one wings/tails trailer (P/N 20141300-10)

Lot 2 (Option): Parts and assemblies for one fuselage trailer (P/N 20141251-10)

Parts and assemblies for one wings/tails trailer (P/N 20141300-10)

Each lot of parts shall be finished (including cure time, as required) and ready for customer pickup within 15 business days of delivering parts to the paint facility.

2.0 Background: AFLCMC/EZPAA does not have in-house painting capabilities. The parts and assemblies for the trailer production project require painting in order to complete the project.

3.0 Scope: The scope of this effort includes painting the parts and assemblies for one fuselage trailer and one wings/tails trailer with an option for painting the parts and assemblies for one additional fuselage trailer and one additional wings/tails trailer. The painting and masking details for each individual part and assembly are included in the documents shown below:

“FT Trailer Paint Pkg 2018.pdf” “WT TRAILER Paint Pkg 2018.pdf”

4.0 Period of Performance:

Lot 1: TBD at time of award – 30 September 2018 Lot 2 (Option): 1 October 2018 - 31 December 2018

5.0 Hours of Operation/Principle Place of Performance: Work in support of this PWS shall be performed at the contractor’s facility within 70 miles of Wright Patterson AFB. The government will deliver and pick up parts to the contractors facility using base transportation services.

AFLCMC/EZPAA

Parts to be Painted

25 January 2018

FUSELAGE TRAILER

POC Brett Baver

937‐257‐7010

P/N Set 7 Qty Set 8 Qty Material Pretreat Prime Topcoat

20141254‐10 1 1 20141276‐10 2 2 20141280‐01 4 4 20141282‐01 1 1 20141282‐03 1 1 20141423‐10 1 1 20141424‐10 1 1 20141425‐10 1 1 20141426‐10 1 1 20141434‐10 1 1 20141435‐10 1 1 20141442‐10 1 1 20141443‐10 1 1 20141445‐10 2 2 20141446‐10 2 2 20141447‐01 4 4 20141448‐01 4 4 20141449‐01 2 2

20141450‐01 2 2

201443204‐10 1 1

201443205‐10 1 1

201443208‐01 2 2

201443209‐01 2 2

201443209‐03 1 1

201443209‐04 1 1

201443210‐01 2 2

201443211‐01 2 2

201443212‐01 2 2

201443212‐03 2 2

201443214‐10 1 1

201443218‐01 1 1

201443222‐01 2 2

201443228‐10 6 6

201443229‐10 1 1

201443235‐01 1 1

201443236‐01 2 2

201443238‐01 1 1

201443239‐01 1 1

201443240‐01 2 2

20152203‐10 1 1

20152209‐10 1 1

20152212‐10 1 1

20152216‐01 1 1

20141281‐01 2 2

20141378‐10 10 10

20141413‐01 4 4

20141414‐10 4 4

20141418‐10 4 4

201443219‐01 2 2

201443219‐03 2 2

201443248‐01 4 4

Aluminum

MIL‐C‐5541

Class 1A

MIL‐PRF‐23377

Type 1

MIL‐PRF‐85285

Type 1, FED‐STD‐

595 Color 26173

Steel

TT‐C‐490 Type 1

OR

Zinc Rich Primer

Mil‐P‐26915 and

Intermediate

Primer MIL‐P‐

53030

MIL‐PRF‐23377

Type 1

MIL‐PRF‐85285

Type 1, , FED‐STD‐

595 Color 26173

A

B

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

23.89

24.00

9.633.00

3.00

1OF1SHEET0.25SCALE

X201443204

DRAWING NO.AF. CODE IDENT NO.

0B275

SIZE

D

WELDMENT, CAPTURE, SPAR, A

TITLE

U.S. AIR FORCE

R. L. MILLER

AIR FORCE RELEASE

M. R. HARFF

AIR FORCE AUTHENTICATION

M. P. BOZZUTO

ENG

J. A. SULLIVAN

CHK

DR

CURRENT

CODE IDENT NO.

X2

PARTS LIST

PROTOTYPE 16-06-10

AFPTEF PROJ NO. 14-P-103

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

20141251-10201443202-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10 -10-

1201443206-01CORNER, CAPTURE, SPAR2

2201443207-01PIVOT, CAPTURE, SPAR, B2

320141277-01TUBE, SPAR CAPTURE, A2

420141277-05TUBE, SPAR CAPTURE, C1

520141277-07TUBE, SPAR CAPTURE, D1

NOTE:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO

METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.

AFTER WELDING, ALL WELDS SHALL BE MECHANICALLY CLEANED

BY WIRE BRUSHING WITH A STAINLESS STEEL WIRE BRUSH,

SANDING, GRINDING, OR POLISHING AND THEN CHEMICALLY

CLEANED (i.e. ALCOHOL, ETC.). WIRE SHALL BE USED

ON ALUMINUM MATERIALS ONLY.

4. FINISH:

PRETREAT WITH PREKOTE SP, ANY METHOD APPROVED BY MANUFACTURER

ALTERNATIVE PRETREATMENT: PRETREAT PER MIL-DTL-5541, CLASS 1A

PRIME PER MIL-PRF-23377 TYPE 1 CLASS C

TOPCOAT PER MIL-PRF-85285 TYPE 1, COLOR GRAY 26173 PER FED-STD-595

HOLE ALIGNMENT SHALL BE WITHIN �#�0.010

MASK HOLES TO PREVENT FINISH FROM ENTERING HOLE SURFACES.

2X

2X

2X

2X

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

(.19)

62X

(.19) 2X

.25 4X

.25

(.19) 2X

(.19)

(.19) 2X 6 4X

(.19) 3X

(.19)

(.19) G finish plug 2X plug 4X

1385697119.C Line

1385697119.C Line

1385697119.C Pencil

1385697119.C Line

A

B

C

D

A

B

C

D

12345678

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT DPREVIOUS EDITION WILL BE USED

FORM

FEB 74 1655AF

QUANTITY REQUIRED PER DASH NO.

23.89

24.00

3.00 9.63

3.00

1OF1SHEET0.25SCALE

X201443205

SIZE

D

WELDMENT, CAPTURE, SPAR, B

CODE IDENT NO.

X2

PARTS LIST

PROTOTYPE 16-06-10

AFPTEF PROJ NO. 14-P-103

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

ANGLESDECIMALSFRACTIONS

0.5�$�0.06 0.030

.XX�#�

.XXX�#�

20141251-10201443203-10

USED ONNEXT ASSEMBLY

APPLICATION

FIND NO.ZONEUNIT WTMATERIALS/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10 -10-

1201443206-01CORNER, CAPTURE, SPAR2

2201443207-01PIVOT, CAPTURE, SPAR, B2

320141277-01TUBE, SPAR CAPTURE, A2

420141277-05TUBE, SPAR CAPTURE, C1

520141277-07TUBE, SPAR CAPTURE, D1

NOTE:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR ENGLISH TO

METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.

AFTER WELDING, ALL WELDS SHALL BE MECHANICALLY CLEANED

BY WIRE BRUSHING WITH A STAINLESS STEEL WIRE BRUSH,

SANDING, GRINDING, OR POLISHING AND THEN CHEMICALLY

CLEANED (i.e. ALCOHOL, ETC.). WIRE SHALL BE USED

ON ALUMINUM MATERIALS ONLY.

4. FINISH:

PRETREAT WITH PREKOTE SP, ANY METHOD APPROVED BY MANUFACTURER

ALTERNATIVE PRETREATMENT: PRETREAT PER MIL-DTL-5541, CLASS 1A

PRIME PER MIL-PRF-23377 TYPE 1 CLASS C

TOPCOAT PER MIL-PRF-85285 TYPE 1, COLOR GRAY 26173 PER FED-STD-595

HOLE ALIGNMENT SHALL BE WITHIN �#�0.010

MASK HOLES TO PREVENT FINISH FROM ENTERING HOLE SURFACES.

2X

2X 2X

DISTRIBUTION STATEMENT D : DISTRIBUTION AUTHORIZED TO

THE DEPARTMENT OF DEFENSE AND U.S. DOD CONTRACTORS

ONLY; ADMINISTRATIVE/OPERATIONAL USE; 18-MAY-2011. OTHER

REQUESTS SHALL BE REFERRED TO THE AIR FORCE PACKAGING

TECHNOLOGY & ENGINEERING FACILITY, DAYTON, OH 45433.

DESTRUCTION NOTICE : DESTROY BY ANY METHOD THAT WILL

PREVENT DISCLOSURE OF CONTENTS OR RECONSTRUCTION OF

THE DOCUMENT

(.19) 2X

.25 4X

.25

(.19) 3X

(.19)

(.19) 2X

(.19)

(.19) 2X 6 4X

(.19) G

(.19)

62X finish plug 2X plug 4X

1385697119.C Line

1385697119.C Line

1385697119.C Line

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT CFORM

JUN 75 1654AF

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

8.31

2.000.625(2.38)

(2.88)

1OF1SHEET0.500SCALE

X20152203

SIZE

C

WELDMENT, TOW BAR PINTLE

CODE IDENT NO.

X2

PROTOTYPE 16-03-30

AFPTEF PROJ NO. 14-P-103

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10

-10-

120152207-01LUG, TOW BAR MOUNT1

220152205-01PLATE, TOW BAR MOUNT, FLAT1

320152206-01TUBE, TOW BAR MOUNT1

APPLICATION

USED ONNEXT ASSEMBLY

20141251-1020152202-10

0.50.06 0.03

.XX

.XXX

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.

AFTER WELDING, ALL WELDS SHALL BE MECHANICALLY CLEANED

BY WIRE BRUSHING WITH A STAINLESS STEEL WIRE BRUSH,

SANDING, GRINDING, OR POLISHING AND THEN CHEMICALLY

CLEANED (i.e. ALCOHOL, ETC.). WIRE SHALL BE USED

ON ALUMINUM MATERIALS ONLY.

4. FINISH:

PRETREAT WITH PREKOTE SP, ANY METHOD APPROVED BY MANUFACTURER

ALTERNATIVE PRETREATMENT: PRETREAT PER MIL-DTL-5541, CLASS 1A

PRIME PER MIL-PRF-23377 TYPE 1 CLASS C

TOPCOAT PER MIL-PRF-85285 TYPE 1, COLOR GRAY 26173 PER FED-STD-595

1 2 3

COMPUTER GENERATED, (PRO/ENGINEER, AFPTEF)ENGINEERING DRAWING LAYOUT CFORM

JUN 75 1654AF

B

A

C

D

B

A

C

D

PARTS LISTQUANTITY REQUIRED PER DASH NO.

2X 3.25

(4.25)

(2.00)

(4.75)

(4.25)

1OF1SHEET0.50SCALE

X20152212

SIZE

C

WELDMENT, TOW BAR END

CODE IDENT NO.

X2

PROTOTYPE 16-03-30

AFPTEF PROJ NO. 14-P-103

REVISIONS

APPROVEDDATEDESCRIPTIONLTR

FIND NO.ZONEUNIT WTMATERIAL/SPECIFICATIONIDENTIFYING NO.CODE IDENTNOMENCLATURESYM-10

-10-

120152213-01GUSSET, TOW BAR MOUNT2

220152210-03PLATE, TOW BAR MOUNT, BENT, END1

APPLICATION

USED ONNEXT ASSEMBLY

20141251-1020152211-10

0.50.06 0.03

.XX

.XXX

ANGLESDECIMALSFRACTIONS

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES - TOLERANCES ON:

NOTES:

1. INTERPRET DRAWING IAW ASME Y14.100 AND ASME Y14.5-2009.

2. ALL CONVERSIONS FROM METRIC TO ENGLISH AND/OR

ENGLISH TO METRIC UNITS SHALL BE IAW IEEE/ASTM SI 10.

3. WELD PER AWS D1.2 WITH 5356 WELDING WIRE PER AWS A5.10.

AFTER WELDING, ALL WELDS SHALL BE MECHANICALLY CLEANED

BY WIRE BRUSHING WITH A STAINLESS STEEL WIRE BRUSH,

SANDING, GRINDING, OR POLISHING AND THEN CHEMICALLY

CLEANED (i.e. ALCOHOL, ETC.). WIRE SHALL BE USED

ON ALUMINUM MATERIALS ONLY.

4. FINISH:

PRETREAT WITH PREKOTE SP, ANY METHOD APPROVED BY MANUFACTURER

ALTERNATIVE PRETREATMENT: PRETREAT PER MIL-DTL-5541, CLASS 1A

PRIME PER MIL-PRF-23377 TYPE 1 CLASS C

TOPCOAT PER MIL-PRF-85285 TYPE 1, COLOR GRAY 26173 PER FED-STD-595

Latch has been removed, mask opening to prevent paint entering.

steel

AFLCMC/EZPAA

Parts to be Painted

25 JAN 2018

WINGS/TAILS TRAILER

POC Brett Baver

937‐257‐7010

P/N Set 4 Qty Set 5 Qty Material Pretreat Prime Topcoat

20141397‐10 1 1

20141302‐10 1 1

20141315‐10 1 1

20141330‐10 1 1

20141331‐01 3 3

20141333‐10 2 2

20141335‐10 2 2

20141336‐10 2 2

20141341‐10 1 1

20141345‐10 1 1

20141347‐10 1 1

20141354‐01 3 3

20141354‐03 2 2

20141360‐10 1 1

20141362‐10 1 1

20141369‐10 1 1

20141383‐01 1 1

20141383‐03 1 1

20141384‐01 1 1

20141384‐03 1 1

20141385‐10 1 1

20141389‐01 2 2

20141394‐01 1 1

20141395‐01 1 1

20141378‐10 10 10

20141381‐01 3 3

Steel

TT‐C‐490 Type 1

OR

Zinc Rich Primer

Mil‐P‐26915 and

Intermediate

Primer MIL‐P‐

53030

MIL‐PRF‐23377

Type 1

MIL‐PRF‐85285

Type 1, , FED‐STD‐

595 Color 26173

Aluminum

Prekote SP, OR

MIL‐C‐5541 Class

1A

MIL‐PRF‐23377

Type 1

MIL‐PRF‐85285

Type 1, FED‐STD‐

595 Color 26173

20141397 plug all threaded holes no specifically marked

Plug end of tubes to prevent paint entering.

Updated Drawings2