Statement_of_Work _27_May_2016 _3_pages.pdf

STATEMENT OF WORK (SOW) FOR SUPPLIES

ILLINOIS AIR NATIONAL GUARD (ILANG) UNIT/DIRECTORATE

DATE: May 27 2016

TITLE: KC-135 R/Model Engine Intake Covers

1. PURPOSE: This SOW provides detailed specifications for purchasing the newly designed KC-135 R/Model Engine Intake Covers that will allow our aircraft maintenance personnel to quickly install and remove engine intake covers to protect the engine intakes during inclement weather conditions.

2. SCOPE OF WORK: Provide Custom designed KC-135 R/Model Engine Intake Covers and Frame Assemblies and required hardware to meet the specification requirements that are outlined within this SOW.

3. DELIVERY LOCATION AND DELIVERY DATE: KC-135 R/Model Engine Covers shall be delivered to the 126th MXG/AMXS Attn: Philip Becerra, 2210 East Dr, Scott Air Force Base, Illinois 62225.

4. QUANTITY REQUIRED: Nine (9) Engine Cover Sets are required, Total Quantity: 18 inboard covers, 18 outboard covers, 36 ea frame assemblies, 36 ea hinge assemblies

5. SPECIFICATIONS REQUIRED:

5.1

• Common Name/Nomenclature of items:

o KC-135 R/Model Engine Cover PN: TMR-R/MODEL-EC o KC-135 R/Model Engine Cover, Frame Assembly PN: TMR-R/MODLE-EC-F o KC-135 R/Model Engine Cover, Hinge Assembly PN: TMR-R/MODLE-EC-H

• Kind of Material:

o KC-135 R/Model Engine Cover PN: TMR-R/MODEL-EC

Engine cover must be made from Dura Print Material, 16 oz. laminated PVC material. Material must have the capability to be RF Welded. This material is proprietary to Topflight Military Resource. It was specifically manufactured to meet intended use requirements.

Material must provide direct print capability.

Frame assembly must be made from light weight, Stainless Steel alloy 316, rust resistant material.

Must have form fitted foam padding for frame assembly.

Must have fitted heat shrink (clear material) over foam padding of frame assembly.

Frame assembly must fold in half for movement/transportation to protect cover front.

o KC-135 R/Model Engine Cover, Hinge Assembly PN: TMR-R/MODLE-EC-H

Removable/ Replaceable Hinge Hinge assembly must have built in engine Chafing Shield Stainless Steel Attachment

• Electrical Data:

o No electrical data required for this product.

• Dimensions, Size or Capacity:

o KC-135 R/Model Engine Cover PN: TMR-R/MODEL-EC 80” diameter KC-135 Engine Cover, must meet frame assembly fit and installation requirements.

Covers must be interchangeable between the left and right side aircraft engines.

Covers must be manufactured using CNC cutting, marking, and labeling process.

Covers must be sewn together on industrial grade sewing machines.

RF welding manufacturing process must be used on all areas identified to ensure custom design fit design requirements are maintained.

Must include Restrictive Environmental Conditions (Include Hazardous Waste or Materials/Reusable

Material/Recyclable Materials Information) Must use Latex Inks which offer health and environmental advantages.

No solvent inks should be used in the manufacturing or printing process.

Must fit within the 80” diameter KC-135 Engine Cover, must meet cover assembly fit requirements.

Individual frame assemblies side must separate from each other.

Frame assemblies must fit to the left and right side aircraft engine connection requirements.

o KC-135 R/Model Frame assembly, Hinge PN: TMR-R/MODLE-EC-H

Hinge must be detachable/replaceable from hinge from frame assembly.

Must have an adjustable/movable hinge assembly.

Must have Stainless Steel hardware.

Hinge assembly must have built in engine Chafing Shield.

• Color:

o KC-135 R/Model Engine Cover PN: TMR-R/MODEL-EC Dura Print Material, 16 oz. laminated PVC material must be use for direct printing. capabilities to supply required custom color and logo requirements.

Must meet PMS colors identified for covers and direct print logo requirements.

Graphics Logo Design Printing must be provided at no cost.

• Principles of Operation:

o Covers must be designed and manufactured to allow aircraft maintenance personnel to quickly install and remove engine intake covers required to protect the engine intakes during inclement weather conditions or non-flight operations.

• Intended use, including location within an assembly:

o KC-135 R/Model Aircraft, Engine Intake Covers. Designed to cover the intake area of KC-135 R/Model engines.

• Essential operation conditions:

o Install and remove engine intake covers to protect the engine intakes during inclement weather conditions.

• Equipment with which the item is to be used:

o KC-135 R/Model Engine Intake Covers, Frame Assemblies, and Hinges.

o Cover KC-135 R/Model Engine Intake

• Quantity: Nine (9) Engine Cover Sets o Each set should contain 4 engine covers, 2 inboard and 2 outboard o One frame assembly per engine cover o One hinge assembly per engine cover

Suggested Product: TMR (Topflight Military Resource) . If not quoting this product, a specifications sheet must be included with your quote to show that the product is equal or greater that the quality and specifications of this suggested product.

END