RFP_Attachment_7_Cross_Reference_Matrix_05Nov18.pdf

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Attached to
T-38A/B/C Pacer Classic III (PCIII) Phase III & Talon Repair Inspection and Maintenance (TRIM) Program
Solicitation number
FA8220-19-R-0001
Issued by

About this file

This document is a cross reference matrix for a request for proposal related to the T-38A/B/C Pacer Classic III Phase III and Talon Repair Inspection and Maintenance program. The matrix outlines nine subfactors under three categories: technical capabilities for parts manufacturing and procurement, technical capabilities for drawing interpretation, and program management. It provides references to statements of work and technical data packages for each evaluation item. Offerors are to demonstrate their ability to produce compliant parts, interpret engineering drawings, and manage subcontractors and risks. The solicitation number is FA8220-19-R-0001 and was posted by the Department of the Air Force Materiel Command Lifecycle Management Center at Hill Air Force Base to support the T-38 aircraft fleet.

Cross Reference Matrix

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RFP Attachment 7 – Cross Reference Matrix Sec. L, II.B.2 Sec. M, II.B.1

Subfactors

Technical Rqmts Doc

SOW, TDP

Section L Paragraph

Section M Paragraph CDRL

Proposal (Offeror

Completes) For each subfactor, identify risks, if any, associated proposed approach and actions offeror will take to mitigate identified risks.

SOW 3.10 Vol. II, C.2.

Vol. II, C.1

A005 B005

Subfactor A: Technical Capabilities; Parts Manufacturing and Procurement Plan

Vol. II, C.2

Vol. II, C.2.1

1. Demonstrate ability to produce parts compliant with the PCIII and TRIM TDPs, to include detailed description of:

--facilities and equipment, --manufacturing tooling, both existing and planned;

Explain how each pertains to the process of manufacturing and integration of PCIII and TRIM parts, to include fasteners. Proposal shall include: sources for all required forgings and extruded parts in the TDP; and sources for all items in the BOM. If no source, provide plan.

SOW 3.1

SOW 3.3 – 3.6

SOW 3.11 – 3.13

SOW 5.0 – 5.1.3

TDP to include EDL

Vol. II, C.3.1.1

Vol. II, C.2.1.1

A007 B007

2. For the following evaluated components:

--P/N 2-11756-523/-524, Bulkhead at

FS388.75

--P/N 3-11493-1/-2, Dorsal Shim --P/N 3-11613-19, Upper Skin, FS

445.00 to 531.00 --P/N 40S101-100, Tapered Shim --P/N 2-11668-5, Bolt Offeror shall describe capability and capacity to:

a) obtain required materials with applicable material certifications;

b) design/build/obtain tooling to aid in manufacturing of parts;

c) machine parts;

d) form/contour/manipulate large and small extrusions and unformed stock;

e) post process (i.e. heat treat, peen, anodize, plate, coat);

f) apply metrology and inspection for dimensional conformity;

g) perform nondestructive testing.

SOW 2.2

SOW 3.1

SOW 3.3 – 3.6

SOW 3.11 – 3.13

SOW 5.0 – 5.1.3

TDP to include EDL

Vol. II, C.3.1.2

Vol. II, C.2.1.2

Subfactor B: Technical Capabilities; Drawing Interpretation

Technical Rqmts Doc

SOW, TDP

Section L Paragraph

Section M Paragraph

CDRL Proposal (Offeror Completes)

3. Using the 3-11611 drawing and associated dimension data for the CFS 505.075 former assembly, P/N 3-11611-503, provide narrative with illustrations to demonstrate the ability to correctly determine the following characteristics:

a) In the plane of the CFS 505.075 and below the Horizontal Reference Plane (HRP), what is the distance between the trace of the Firewall Moldline on CFS 505.075 and the Fuselage Moldline at a distance of

12.5 inches outboard of the airplane centerline?

b) Determine the number of cooling holes, the corresponding diameter, and their locations above the Horizontal Reference Line (HRL) in the 3-11611-31/-32 Formers for this assembly configuration.

SOW 3.1

SOW 3.3 – 3.6

SOW 3.11 – 3.13

SOW 5.0 – 5.1.3

TDP to include EDL

Vol. II, C.3.2.1, C.3.2.1.1, C.3.2.1.2

Vol. II, C.2.2, C.2.2.1- C.2.2.4.3

4. Provide a narrative with illustrations to demonstrate the ability to correctly interpret drawing 3-11805 located in the PCIII Technical Data Package. The technical proposal shall:

a) Provide the configuration to be produced and identification of the components of the 3-11805-49 assembly;

b) Provide the dimension (in inches) from the bottom edge of the doubler to the Horizontal Reference Line.

SOW 3.1

SOW 3.3 – 3.6

SOW 3.11 – 3.13

SOW 5.0 – 5.1.3

TDP to include EDL

Vol. II, C.3.2.2, C.3.2.2.1, C.2.2.2

Vol. II, C.2.2,

5. Provide a narrative with illustrations to demonstrate the ability to correctly interpret drawing 3-11613 located in the TRIM Technical Data Package. The technical proposal shall:

a) List all of the final skin thicknesses required to make for the -19 configuration;

b) Identify number and location of all cutouts (including circular) and provide dimensions for each on the -19 configuration

SOW 3.1

SOW 3.3 – 3.6

SOW 3.11 – 3.13

SOW 5.0 – 5.1.3

TDP to include EDL

Vol. II, C.3.2.3, C.3.2.3.1, C.3.2.3.2

Vol. II, C.2.2, Continued next page

Subfactor B: Technical Capabilities; Drawing Interpretation

Technical Rqmts Doc

SOW, TDP

Section L Paragraph

Section M Paragraph

CDRL Proposal (Offeror Completes)

6. Using the 2-11668 drawing and associated specifications, please identify and explain how the answer was determined for the following:

a) What is the minimum allowable distance from the forging flow lines between the intersection of the longitudinal axis of the bolt and the approximate transverse axis of the flow lines to the bearing surface of the bolt?

b) What is the minimum number of fatigue cycles that should be conducted in the fatigue test for a passing condition?

c) For a lot or batch size of 30, what is the required number of samples for fatigue testing?

SOW 3.1

SOW 3.3 – 3.6

SOW 3.11 – 3.13

SOW 5.0 – 5.1.3

TDP to include EDL

Vol. II, C.3.2.4, C.3.2.4.1, C.3.2.4.2, C.3.2.4.3

Vol. II, C.2.2, Subfactor C:

Program Management

Technical Rqmts Doc

SOW, TDP

Section L Paragraph

Section M Paragraph

CDRL Proposal (Offeror Completes)

Provide your supply chain management approach, risk management approach and a description of your logistical capacity for obtaining modification components. The technical proposal shall include:

SOW 2.2.1,

SOW 3.10

Vol. II, C.3.3

Vol. II, C2.3

7. RESOURCE MGMT: The prime contractor’s organizational structure which identifies key personnel. The proposal shall clearly document the primary roles and lines of responsibility, and technical interface with subject matter experts. The proposal shall illustrate all planned subcontractor relationships to include name and CAGE code with letter of intent between prime and sub agreeing to be on contract within 90 days of contract award. Proposal shall include a detailed IMS as specified.

SOW 2.2.1,

SOW 3.9,

SOW 3.11

Vol. II, C.3.3.1

Vol. II, C.2.3.1

A006 B006

8. SUBCONTRACTOR MGMT:

Offeror shall describe a clear and feasible approach to managing all subcontractors, partners, and sub-tier subcontractors/partners to meet quality system requirements, as well as supply chain partners and the process in which these partners are evaluated and selected. This includes supplier’s commitments to adequately demonstrate their ability to achieve Government desired full rate production.

SOW 2.1.1,

SOW 3.4.1,

SOW 5.1.1

Vol. II, C.3.3.2

Vol. II, C.2.3.2

9. RISK MGMT: Offeror shall provide a complete description of risk management processes, explaining the criteria, methods, and procedures that would be used to identify the critical items associated with the implementation of this contract.

SOW 2.2.1

SOW 3.10

Vol. II, C.3.3.3

Vol. II, C.2.3.3

A004 B004

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