PWS_10Mar2016.pdf

PDF 2 MB Posted

Attached to
Electroless Nickel Plating of C17 Landing Gear
Solicitation number
FA8224-16-R-0046
Issued by

View the file

Other files

File Type Posted
Annual_Quantity_Estimate.xls XLS spreadsheet
FA8224-16-R-0046_Solicitation.pdf PDF
CDRLs_29Mar2016.pdf PDF

On GovTribe

Work with this file

  • Download the original file
  • Contacts named in this file
  • Similar government files
  • Ask GovTribe AI about this file

Text version

PERFORMANCE-BASED WORK STATEMENT (PWS)

FOR

ELECTROLESS NICKEL PLATING

Commodities Maintenance Group (CMXG)

10 March 2016

TABLE OF CONTENTS

SECTION PAGE

1. DESCRIPTION OF SERVICES 3

2. BASIC SERVICES 3

3. REQUIREMENTS 3

4. CERTIFICATION REQUIREMENTS 3

5. SERVICES SUMMARY 4

6. QUALITY CONTROL 4

7. PROPERTY DAMAGE 5

APPENCICES:

APPENDIX A – Acronyms and Abbreviations 6

APPENDIX B – Workload Estimate 7

APPENDIX D – Work Instructions 8

1.0 DESCRIPTION OF SERVICES

1.1 The Contractor shall provide all labor, supplies, tooling, equipment, and certifications required to perform electroless nickel plating in accordance with Douglas Process

Specifications (DPS) 9.67 (most current revision) to C-17 landing gear components.

The services shall be performed at the contractor’s facility in support of the 309 th

Commodities Maintenance Group (309 CMXG) located at Hill Air Force Base (AFB), Utah.

2.0 BASIC SERVICES

2.1 Only contractors that are certified by Boeing to perform electroless nickel plating in accordance with DPS 9.67 (most current revision) may be considered. Contractors must also be certified by Goodrich/UTAS and listed on their DOC200 quality systems listing.

2.2 The Government will ship the asset(s) to the contractor’s facility. The contractor shall receive asset(s), provide secure storage as necessary, perform electroless nickel coating in accordance with the Government provided work instructions in accordance with

(IAW) Appendix (Appx) D, and repack in original packaging within 15 business days after receipt of assets. The contractor will ship completed assets, to Hill Air Force Base, in received packaging via 3-4 day expedited shipping at the contractor’s expense.

3.0 REQUIREMENTS

3.1 The contractor shall perform a visual and dimensional check of asset prior to acceptance of part. If damage is noted (during or prior to shipment), the contractor shall not begin work on asset and contact the Technical Program Manager (TPM). The

Contractor shall provide a report of damages, including appropriate documentation and photographs, within two (2) business days of receipt of asset. (CDRL A001) (Services

Summary)

3.2 Upon contractor acceptance, the contractor shall perform electroless nickel plating in accordance with (IAW) with Government provided work instructions referenced in

Appx D.

4.0 CERTIFICATION REQUIREMENTS

4.1 The contractor shall be certified by Boeing for electroless nickel plating in accordance with DPS 9.67 and shall be listed on the Boeing D1-4426 website for the process required. The contractor shall maintain all listed certifications throughout the duration of this contract. The contractor shall also be listed on the Goodrich/UTAS DOC200 quality systems approved processor list.

4.2 The contractor shall provide process documentation with each asset that shows compliance to DPS 9.67 and customer requirements.

(CDRL A002) (Services Summary)

5.0 SERVICES SUMMARY

6.0 QUALITY CONTROL

6.1 The contractor shall provide process documentation with each completed asset showing that all repairs were accomplished according to the applicable engineering drawings or other instructions provided by the Government. (CDRL A002) (Services Summary)

6.2 The Government TPM will perform final acceptance inspection at Government facility and prior to the Government accepting the invoice. Any quality defects that cause assets to fail the final acceptance inspection shall immediately be transported back to the contractor facility and be re-worked by the contractor at the contractor’s expense and completed within 15 business days.

# Performance Objective Paragraph Performance Threshold

The contractor shall complete electroless nickel and repackage within 15 business days after receipt of asset(s).

2.2

Performance is acceptable if there are no more than two (2) deviations.

The contractor shall provide the

TPM a report of damages within two (2) business days after receipt of asset. (CDRL A001)

3.1

Performance is acceptable if there are zero (0) deviations.

The contractor shall provide electroless nickel services IAW

Government provided work instructions

3.2 Performance is acceptable if there are

zero (0) deviations.

The contractor shall maintain continuous certification to DPS

9.67,listing on the Boeing D1-

4426 website, Goodrich/UTAS

DOC200 quality systems approved processor list (CDRL

A002)

4.1 Performance is acceptable if there

are zero (0) deviations.

7.0 PROPERTY DAMAGE

7.1 The contractor shall be responsible for any damage incurred at the contractor’s facility.

The contractor shall notify the Contracting Officer (CO), within eight (8) hours of any damage to Government property.

Appendix A – Acronyms and Abbreviations List

Acronym/Abbreviation Definition

AF Air Force

AFB Air Force Base

CDRL Contract Data Requirements List

CMXG Commodities Maintenance Group

CO Contracting Officer

COR Contracting Officer Representative

CMRA Contractor Manpower Reporting Application

FOD Foreign Object Damage

GR Government Representative

HAFB Hill Air Force Base

IAW In Accordance With

ISO International Standardization Organization

OO-ALC Ogden Air Logistics Center

POP Period of Performance

PWS Performance-Based Work Statement

QCP Quality Control Program

SME Subject Matter Expert

SS Services Summary

TPM Technical Program Manager

Appendix B – Estimated Annual Workload (Historical data)

Part Number Service

Estimated

Annual

Quantity

17P1C2001 Electroless Nickle 1

17P1C2006 Electroless Nickel 1

17P1C2059 Electroless Nickel 1

17P1C2064 Electroless Nickel 1

17P2C1009 Electroless Nickel 2

17P2C1028 Electroless Nickel 6

17P2C1029 Electroless Nickel 6

17P2C1037 Electroless Nickel 3

17P2C1062 Electroless Nickel 4

17P2C1093 Electroless Nickel 2

17P2C1100 Electroless Nickel 1

17P2C1179 Electroless Nickel 3

17P2C1185 Electroless Nickel 3

17P2C1194 Electroless Nickel 2

17P2C1229 Electroless Nickel 8

17P2C1279 Electroless Nickel 2

17P2C1280 Electroless Nickel 4

Appendix D –Work Instructions Part Name: C-17 Nose Axle

Part number: 17P1C2001

Serial number: _________________

Technical Order number: 4A4-52-3-2

Material: 300M steel (heat treated to 280-300 ksi)

Weight: approximately 50 lbs

Part Dimensions: 39”x 5”x 5”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached image, plate ID threaded area(s), adjacent relief, and chamfer.

Thickness: _____________ on serial number side

_____________ on non-serial number side

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Work Priority: Process and ship component within 7 working days of receipt of component. Return shipping to be 2 to 3 day shipping.

Ship To:

Building 507, C/O Dean Keyes

5760 Southgate Ave.

Hill AFB, UT 84056

Technical POC: Mark Robison 801-777-4183

Email: mark.robison.1@us.af.mil

Purchasing POC: Kimberly Langley 801-586-8147

Email: kimberly.langley.2@us.af.mil

Purchase Order Number: __________________

Part Name: C-17 Nose Outer Cylinder

Part number: 17P1C2006

Serial number: _________________

Technical Order number: 4A4-52-3-2

Material: 300M steel (heat treated to 280-300 ksi)

Weight: approximately 300 lbs

Part Dimensions: 52” long, 24” wide

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA

Post plating bake per DPS 5.00-1 Rev AV.

Location: Lower bore threads, see attached photos.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Electroless Nickel coat surface shown, from beginning of thread near outer edge to where chrome begins on the chamfer (all of the threads and internal groove surface)

Mask off and do not nickel plate flat face on outside edge

Part Name: Weld Assembly

Part number: 17P1C2059

Serial number: _________________

Technical Order number: 4A4-52-3-7

Material: 300M steel (heat treated to 280-300 ksi)

Weight: approximately 10 lbs

Part Dimensions: 13”x 6”x 4”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate OD threaded area.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Part Name: Piston Rod

Part number: 17P1C2064

Serial number: _________________

Technical Order number: 4A4-52-3-7

Material: 4340 steel (heat treated to > 180 ksi)

Weight: Approximately 10 lbs

Part Dimensions: 24.5” long, 4” diameter

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA

Post plating bake per DPS 5.00-1 Rev AV.

Location: Plate ID threads, see attached drawing and photo

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Electroless Nickel Repair of ID Threads

Electroless nickel plating extends onto the threads on the castellated area of the piston.

Part Name: C-17 Main Outer Cylinder

Part number: 17P2C1009

Serial number: _________________

Technical Order number: 4A4-55-3-3

Material: 300M steel (heat treated to 280-300 ksi)

Weight: Approximately 60 lbs

Part Dimensions: 40” long, 14” wide

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawings, plate threads at bore opening.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Figure 1: Area that needs electroless nickel coating.

Figure 2: Detail. Note PAK2 states to electroless nickel coat threads. Note 2UAL states that nickel plate runout to be 0 to 0.06”

Electroless nickel coat ID threads near open in red circled area. See figure 2 for detail of red circled area

(view H).

Part Name: C-17 Single Axle

Part number: 17P2C1028

Serial number: _________________

Technical Order number: 4A4-55-3-3

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 45 lbs

Part Dimensions: 23”x 5.25”x 5.25”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate ID threaded area and adjacent land.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Part Name: C-17 Dual Axle

Part number: 17P2C1029

Serial number: _________________

Technical Order number: 4A4-55-3-3

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 87 lbs

Part Dimensions: 47”x 5.5”x 5.5”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate ID threaded area and adjacent land.

Thickness: _____________ on serial number side

_____________ on non-serial number side

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Serial Number is Etched on the end face of the axle

Part Name: Post

Part number: 17P2C1037

Serial number: _________________

Technical Order number: 4A4-55-3-3

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 750 lbs

Part Dimensions: 60”x 65”x 20”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing and images, plate ID threaded area.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Electroless nickel plate ID threads.

Part Name: Retract Cylinder Weld Assembly

Part number: 17P2C1062

Serial number: _________________

Technical Order number: 4A4-55-3-12

Material: 4340 steel (heat treated to > 180 ksi)

Weight: approximately 15 lbs

Part Dimensions: 26” x 6” x 5”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate ID threaded area.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Part Name: Lower Brace Beam

Part number: 17P2C1093

Serial number: _________________

Technical Order number: 4A4-55-3-5

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 179 lbs

Part Dimensions: 49”x25”x4.5”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate threaded area.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Electroless nickel on the threads up to 0.004” thick

Part Name: Lower Brace Trunnion

Part number: 17P2C1100

Serial number: _________________

Technical Order number: 4A4-55-3-7

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 134 lbs

Part Dimensions: 35”x15”x9”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate threaded area(s) indicated.

Thickness: _____________ on Side A (small diameter side)

_____________ on Side B (large diameter side)

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Side A

Side B

Part Name: Fwd-Door Torque-Tube Drive

Part number: 17P2C1179

Serial number: _________________

Technical Order number: 4A4-55-3-11

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 79 lbs

Part Dimensions: 46”x20”x9”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate splines, journals, and areas noted.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Electroless Nickel plate this chamfer, 0.060” runout allowed on face

Electroless Nickel plate this area

Electroless Nickel plate the faces inside this slot

Part Name: C-17 Aft-Door Torque-Tube Drive

Part number: 17P2C1185

Serial number: _________________

Technical Order number: 4A4-55-3-11

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 30 lbs

Part Dimensions: 30”x27”x4”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached images, plate splines, journals, and other areas as noted.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Do not plate exterior face here

Electroless Nickel coat surface shown, from the outer edge of the face on the right to the outer end of the component. Plate face, journals, grooves and splines in noted area.

Part Name: Twist Inner Drag Link

Part number: 17P2C1194

Serial number: _________________

Technical Order number: 4A4-55-3-5

Material: 300M steel (heat treated to 280-300 ksi)

Weight: approximately 15 lbs

Part Dimensions: 10”x6.25”x3.25”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate threaded areas, extend plating beyond threads to area indicated in image.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Part Name: Lower Diagonal Brace

Part number: 17P2C1229

Serial number: _________________

Technical Order number: 4A4-55-3-5

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 190 lbs

Part Dimensions: 60”x 6.2” x 12”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate ID threaded area.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Part Name: C-17 Trunnion

Part number: 17P2C1279

Serial number: _________________

Technical Order number: 4A4-55-3-7

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 123 lbs

Part Dimensions: 40”x 10”x 23”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA.

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate threaded area(s) indicated.

Thickness: _____________ on Side A (small diameter side)

_____________ on Side B (large diameter side)

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Side A

Side B

Part Name: Forward Lower Brace Beam

Part number: 17P2C1280

Serial number: _________________

Technical Order number: 4A4-55-3-5

Material: 300M steel (heat treated to 280-300 ksi)

Weight: 179 lbs

Part Dimensions: 49”x25”x4.5”

Material condition: Component has had all paint and cadmium removed. Stress relief bake has already been performed. There may still be chrome plated surfaces intact, please take care not to damage these surfaces. The electroless nickel has been removed from the surface to be plated.

Required work:

Electroless nickel coat per DPS 9.67 Rev AA

Post plating bake per DPS 5.00-1 Rev AV.

Location: See attached drawing, plate threaded area.

Thickness: _____________

Visual Inspection: The plating shall be free from blisters, laminations, nodules, pits, discontinuities, porosity and other defects. The line of demarcation between plated and unplated areas shall be even and smooth.

Documentation: Process documentation shall be filled out by the processor and returned with the completed component. Documentation shall show all process steps taken and certify that the process was completed in accordance with applicable specifications. Documentation shall also include a certificate of compliance to applicable specifications.

Processor must maintain D1-4426 approval. Any subprocessors must also meet D1-4426 approval.

Purchasing POC: Kimberly Langley 801-586-8147

Electroless nickel on the threads up to 0.004” thick

File details come from the government source that posted it. Updated .