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JUSTIFICATION FOR QUALIFICATION REQUIREMENTS

FAR 9.202(a) Policy and DoD 4120.24-M Defense Standardization Program, Policy and Procedures

7 Mar 2019 Section A & Section B & Section D

RMSC: C (AFMCI 21-113, Contract Maintenance Program for Depot Maintenance Activity Group)

SECTION A: ITEM IDENTIFICATION

1. National Stock Number (NSN): 6110-01-481-1994

2. Part Number (P/N): A27969-000

3. Noun: Distribution Box

4. Application: M3P, AN/MST-T1(V), Mini-MUTES

SECTION B:

1. JUSTIFICATION FOR ESTABLISHING A QUALIFICATION REQUIREMENT

a. Criticality: Repair/overhaul of this Distribution Box requires engineering source approval by the engineering support activity 415 SCMS/GUMAD in order to maintain the quality of the part.

Failure to procure repair services for this Distribution Box from a fully qualified repair source can result in structural or functional deficiencies that will degrade the mission capability of the M3P, AN/MST-T1(V), Mini-MUTES

b. Complexity, Repair Processes, and/or Material Considerations: N/A

c. Form, Fit, Function, and Interface: The qualification requirements specified herein are necessary to verify the structural and/or functional integrity and/or fit, form, and interface of the Distribution Box being procured.

2. REASON WHY QUALIFICATION REQUIREMENT MUST BE DEMONSTRATED PRIOR TO ANY CONTRACT

AWARD

a. Completion of the specified pre-contract award qualification requirements are necessary to assure the government that the offeror is capable of repairing the Distribution Box in compliance with the applicable technical specification/data within the schedule and economic constraints of our contracts. There are significant technical and schedule risks which can only be minimized by a completion of the requirements prior to contract award.

b. Qualification Requirement Cost Estimate: Estimated likely costs for testing and evaluation, which will be incurred by the potential offering party to become qualified are $0.

c. Qualification Time Completion Estimate: It is the estimate of the engineering support activity that completion of this qualification effort should require 60 days. This is based on complexity of the Distribution Box and other factors.

SECTION D: SIGNATURES

X Chief of Contracting Office (COCO)

415 SCMS/GUMBB Lead Engineer Engineer Support Activity (ESA)

415 SCMS/GUMAD Engineer

REPAIR QUALIFICATION REQUIREMENTS

NSN: 6110-01-481-1994

P/N: A27969-000 Noun: Distribution Box Application: M3P, AN/MST-T1(V), Mini-MUTES

7 Mar 2019 Supporting Information

Qualification Requirement Cost Estimate Estimate the likely cost for testing and evaluation which will be incurred by the potential offeror to become qualified. This is a requirement of FAR 9.202(a)(1)(ii) and 10USC2319(b)(3) (The following categories may not apply in all cases. The product engineer should identify the costs applicable to the project and indicate N/A on all sections that do not apply.)

N/A

Total cost is $ 0.00 Section A. Shipping, if required, use DD Form 1654, Evaluation of Transportation Cost Factors to develop the information. Refer any questions to the Procurement Contracting Officer for cost estimation.

Section B. Dimensional/Electronic Verification. Contact the science/engineering laboratory to obtain cost estimates (bids) for tests such as:

$ 0.00

a. Chemical N/A

b. Metallurgical $ 0.00

(1) Destructive N/A

(2) Non-Destructive N/A

c. Dimensional N/A

d. Electronic N/A

e. Mechanical N/A

f. Non-Destructive Inspection N/A Section C. Nuclear Hardness [This includes cost of shock, vibration, and Electro-Magnetic Pulse (EMP)]. Contact Systems Engineering Integration and Test Division for hourly rate.

Section D. Form, Fit, Function and Interface. Contact your organizational Production Management Specialist (PMS) to obtain information on the same or similar item where work has been accomplished in the past using AFMC Form 206, Temporary Work Request.

Section E. Original Equipment Manufacturer (OEM) Qualification Testing (If required) $ 0.00

a. Laboratory Costs (Costs are directly dependent on the type of testing to be accomplished and the location and duration of the testing. For example, landing gear laboratory testing is normally accomplished on a dynamometer and costs vary from $25,000 to $500,000 depending on the depth of testing. Aircraft and missile testing will vary as the requirement dictates and the cost will have to be identified by the source of testing).

b. Flight/Data Reduction & Analysis Costs. N/A Section F. Travel by Contractor to Test Site (if required) $ 0.00

a. Lodging N/A

b. Per Diem N/A

c. Rental Cars N/A

d. Incidentals (Verified) N/A Section G. SAR Package Development/Evaluation Cost: A potential new source’s development of a Source Approval (SAR) package may cost as much as:

In addition, the cost incurred for Government evaluation of their SAR may be as much as: N/A Evaluation cost may be born by the government if it is in the best interest of the Government to qualify alternate sources.

P/N: A27969-000

7 Mar 2019 Section C 1/3

SECTION C:

1. QUALIFICATION REQUIREMENTS THAT MUST BE SATISFIED TO BECOME A QUALIFIED SOURCE

a. Prequalification Notice: The offeror shall notify the appropriate government Small Business Office or, if responding to a solicitation, the contracting officer in the appropriate government contracting office, of intent to qualify as a source for this Distribution Box.

b. Facilities, Testing, and Inspection Capabilities: The offeror must certify to the government that they have, or have access to, the required facilities and equipment to repair, inspect, test, package, and store the item. These items are used on AN/MST-T1(V) system and can only be verified using in the AN/MST-T1(V) system or equivalent. The offeror shall make their facilities, equipment, tooling, and personnel available for evaluation and inspection by the government.

c. Data Verification: The offeror must verify that they have a complete data package. This verification must include a complete list of all procedures, drawings, and specifications, including change notices, in the offeror’s possession including, at a minimum ETM (8M906) drawing A26367. The offeror may also be required to produce copies of all applicable procedures, drawings, or specifications.

d. Repair Process Verification: The offeror must repair this item to conform to the government requirements as prescribed within the ESA-approved engineering/technical data package. The offeror must show compliance with Unique Identification (UID) requirements in accordance with DFARS 211.274 as prescribed within the ESA-approved engineering/technical data package. The offeror must provide, at their own expense, data showing the results of all quality, performance, and environmental evaluations conducted by the offeror to show compliance with the government requirements as prescribed by 415 SCMS/GUMAD. The offeror shall also identify its sources for materials and its standards for internally used processes.

e. Test and Evaluation and/or Verification: The offeror, at their own expense, shall prepare and submit to 415 SCMS/GUMAD for their prior approval, a qualification test plan/procedure detailing how they intend to verify compliance with all performance, environmental, mechanical, and quality assurance requirements identified by ESA-approved engineering/technical data package.

f. Qualification Article Verification: N/A

g. Qualification Requirement Cost Estimate: Estimated likely costs for testing and evaluation,

h. Qualification Time Completion Estimate: It is the estimate of the engineering support activity of the Distribution Box and other factors.

P/N: A27969-000

7 Mar 2019 Section C 2/3

i. Qualification Time Limitation: An offeror may not be denied the opportunity to submit and have considered an offer for a contract if the offeror can demonstrate to the satisfaction of the contracting officer that the offeror (or its product) meets these standards for qualification or can meet them before the date specified for award of the contract. The award will not be delayed to provide the vendor with an opportunity to demonstrate its ability to meet the standards specified in this qualification requirement.

j. Evaluation of Proposals Not Previously Qualified: The offeror must be fully qualified in order to be eligible for a contract award. Therefore, the offeror must fulfill all of the requirements stated, in writing, in the qualification requirement before the date specified for award of the contract. Once all requirements are met, the offeror will be listed as an approved repair source for this item. Approval, however, does not guarantee subsequent contract award.

P/N: A27969-000

7 Mar 2019 Section C 3/3

2. SOURCE QUALIFICATION WAIVER REQUIREMENTS

Sources who meet any of the following Source Qualification Waiver Criteria (QWC) may apply for a waiver of all or part of the qualification requirements. If a waiver is granted and the offeror is awarded a contract, the offeror may still be required to provide a post-contract award first article exhibit to verify production capability:

a. QWC1: The potential source submits written certification that the articles have been supplied to the government or original equipment manufacturer (e.g., DD Form 250, Material Inspection and Receiving Report, Purchase Order invoice, etc).

b. QWC2: The potential source is qualified on the right-hand article and requests to be qualified on the left-hand article. If the right-and left-hand articles are mirror images of each other, then approval can generally be given.

c. QWC3: A source qualified to provide an assembly is usually qualified to provide subassemblies, major components, and items of that assembly.

d. QWC4: A source qualified to provide earlier dash numbers of a basic P/N may be qualified to provide other dash numbers of that same basic P/N, provided there is no increase in complexity, criticality, or other relevant requirements.

e. QWC5: A source qualified to provide a similar or like item can be qualified to provide the required item. However, for approval, the engineering authority must verify that there is no increase in complexity, criticality, or other requirements over that of the similar item. At a minimum, the source shall provide a complete set of drawings for the similar item and written proof, such as purchase orders, shipping documents, etc., to show that the similar item was provided to the original equipment manufacturer or DoD.

f. QWC6: A source previously qualified to provide an item, but which has been purchased, sold, merged, absorbed, reformed, split, etc., may qualify if it can be established that the qualification is currently with the requester and that the requester has the same or equivalent facilities, tooling, equipment, personnel, and utilizes the original forging, castings, etc., in the repair process.

NA:

Total cost is:

NA_2:

000:

a Chemical:

b Metallurgical:

1 Destructive:

2 NonDestructive:

c Dimensional:

d Electronic:

e Mechanical:

f NonDestructive Inspection:

NA_3:

NA_4:

NA_5:

b FlightData Reduction Analysis Costs:

Section F Travel by Contractor to Test Site if required:

a Lodging:

b Per Diem:

c Rental Cars:

d Incidentals Verified:

NA_6:

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1. National Stock Number (NSN): 6110-01-478-4043

2. Part Number (P/N): A26144-000

3. Noun: Electrical System Protection Panel

a. Criticality: Repair/overhaul of this Electrical System Protection Panel requires engineering source approval by the engineering support activity 415 SCMS/GUMAD in order to maintain the quality of the part. Failure to procure repair services for this Electrical System Protection Panel from a fully qualified repair source can result in structural or functional deficiencies that will degrade the mission capability of the M3P, AN/MST-T1(V), Mini-MUTES to verify the structural and/or functional integrity and/or fit, form, and interface of the Electrical System Protection Panel being procured.

assure the government that the offeror is capable of repairing the Electrical System Protection Panel in compliance with the applicable technical specification/data within the schedule and economic constraints of our contracts. There are significant technical and schedule risks which can only be minimized by a completion of the requirements prior to contract award.

of the Electrical System Protection Panel and other factors.

NSN: 6110-01-478-4043

P/N: A26144-000 Noun: Electrical System Protection Panel offeror to become qualified. This is a requirement of FAR 9.202(a)(1)(ii) and 10USC2319(b)(3)

(1) Destructive N/A

(2) Non-Destructive N/A

c. Dimensional N/A

d. Electronic N/A

e. Mechanical N/A

f. Non-Destructive Inspection N/A the location and duration of the testing. For example, landing gear laboratory testing is normally accomplished on a dynamometer and costs vary from $25,000 to $500,000 depending on the

a. Lodging N/A

b. Per Diem N/A

c. Rental Cars N/A

d. Incidentals (Verified) N/A

P/N: A26144-000 contracting office, of intent to qualify as a source for this Electrical System Protection Panel.

drawing A26144. The offeror may also be required to produce copies of all applicable

DFARS 211.274 as prescribed within the ESA-approved engineering/technical data package. The offeror must provide, at their own expense, data showing the results of all quality, performance, and environmental evaluations conducted by the offeror to show compliance with the of the Electrical System Protection Panel and other factors.

P/N: A26144-000 contracting officer that the offeror (or its product) meets these standards for qualification or can meet them before the date specified for award of the contract. The award will not be delayed

P/N: A26144-000 waiver of all or part of the qualification requirements. If a waiver is granted and the offeror is awarded a contract, the offeror may still be required to provide a post-contract award first article exhibit to verify minimum, the source shall provide a complete set of drawings for the similar item and written

NA:

Total cost is:

NA_2:

000:

a Chemical:

b Metallurgical:

1 Destructive:

2 NonDestructive:

c Dimensional:

d Electronic:

e Mechanical:

f NonDestructive Inspection:

NA_3:

NA_4:

NA_5:

b FlightData Reduction Analysis Costs:

Section F Travel by Contractor to Test Site if required:

a Lodging:

b Per Diem:

c Rental Cars:

d Incidentals Verified:

NA_6:

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5 Mar 2019 Section A & Section B & Section D

Application: M3P AN/MST-T1(V)

a. Criticality: Repair/overhaul of this Equipment Communication Interface Unit requires engineering source approval by the engineering support activity 415 SCMS/GUMBB in order to maintain the quality of the part. Failure to procure repair services for this Equipment Communication Interface Unit from a fully qualified repair source can result in structural or functional deficiencies that will degrade the mission capability of the M3P AN/MST-T1(V).

Equipment Communication Interface Unit being procured.

assure the government that the offeror is capable of repairing the Equipment Communication Interface Unit in compliance with the applicable technical specification/data within the schedule and economic constraints of our contracts. There are significant technical and schedule risks which can only be minimized by a completion of the requirements prior to contract award.

of the Equipment Communication Interface Unit and other factors.

Item Description NSN Part Number Equipment Communication Interface Unit 5895-01-477-7341 A26142-000 Equipment Communication Interface Unit 5895-01-480-9021 A27987-000

Multiple NSN’s

5 Mar 2019 Supporting Information offeror to become qualified. This is a requirement of FAR 9.202(a)(1)(ii) and 10USC2319(b)(3)

(1) Destructive N/A

(2) Non-Destructive N/A

c. Dimensional N/A

d. Electronic N/A

e. Mechanical N/A

f. Non-Destructive Inspection N/A the location and duration of the testing. For example, landing gear laboratory testing is normally accomplished on a dynamometer and costs vary from $25,000 to $500,000 depending on the

a. Lodging N/A

b. Per Diem N/A

c. Rental Cars N/A

d. Incidentals (Verified) N/A

5 Mar 2019 Section C 1/3 contracting office, of intent to qualify as a source for this Equipment Communication Interface Unit.

verified using in the AN/MST-T1(V) system or equivalent.The offeror shall make their facilities, including change notices, in the offeror’s possession including, at a minimum the reference documents in the following table.

The offeror may also be required to produce copies of all applicable procedures, drawings, or specifications.

offeror must show compliance with Unique Identification (UID) requirements in accordance with DFARS 211.274 as prescribed within the ESA-approved engineering/technical data package. The offeror must provide, at their own expense, data showing the results of all quality, performance, and environmental evaluations conducted by the offeror to show compliance with the government requirements as prescribed by 415 SCMS/GUMBB. The offeror shall also identify its sources for materials and its standards for internally used processes.

submit to 415 SCMS/GUMBB for their prior approval, a qualification test plan/procedure detailing how they intend to verify compliance with all performance, environmental, Item Description NSN Part Number Reference Docs Equipment Communication Interface Unit 5895-01-477-7341 A26142-000 A26142 Cage: 8M906 Equipment Communication Interface Unit 5895-01-480-9021 A27987-000 A27987Cage: 8M906

5 Mar 2019 Section C 2/3 of the Equipment Communication Interface Unit and other factors.

contracting officer that the offeror (or its product) meets these standards for qualification or can meet them before the date specified for award of the contract. The award will not be delayed

5 Mar 2019 Section C 3/3 waiver of all or part of the qualification requirements. If a waiver is granted and the offeror is awarded a contract, the offeror may still be required to provide a post-contract award first article exhibit to verify minimum, the source shall provide a complete set of drawings for the similar item and written

Item Description:

NSN:

Estimate the likely cost for testing and evaluation which will be incurred by the potential offeror to become qualified This is a requirement of FAR 9202a1ii and 10USC2319b3 The following categories may not apply in all cases The product engineer should identify the costs applicable to the project and indicate NA on all sections that do not apply:

Total cost is:

NA:

000:

a Chemical:

b Metallurgical:

1 Destructive:

2 NonDestructive:

c Dimensional:

d Electronic:

e Mechanical:

f NonDestructive Inspection:

NA_2:

NA_3:

NA_4:

b FlightData Reduction Analysis Costs:

Section F Travel by Contractor to Test Site if required:

a Lodging:

b Per Diem:

c Rental Cars:

d Incidentals Verified:

NA_5:

Item Description_2:

NSN_2:

Reference Docs:

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1. National Stock Number (NSN): 6130-01-478-2106

2. Part Number (P/N): A28018-000

3. Noun: Power Supply Assembly

a. Criticality: Repair/overhaul of this Power Supply Assembly requires engineering source approval by the engineering support activity 415 SCMS/GUMAD in order to maintain the quality of the part. Failure to procure repair services for this Power Supply Assembly from a fully qualified repair source can result in structural or functional deficiencies that will degrade the mission capability of the M3P, AN/MST-T1(V), Mini-MUTES to verify the structural and/or functional integrity and/or fit, form, and interface of the Power Supply Assembly being procured.

assure the government that the offeror is capable of repairing the Power Supply Assembly in compliance with the applicable technical specification/data within the schedule and economic of the Power Supply Assembly and other factors.

NSN: 6130-01-478-2106

P/N: A28018-000 Noun: Power Supply Assembly offeror to become qualified. This is a requirement of FAR 9.202(a)(1)(ii) and 10USC2319(b)(3)

(1) Destructive N/A

(2) Non-Destructive N/A

c. Dimensional N/A

d. Electronic N/A

e. Mechanical N/A

f. Non-Destructive Inspection N/A the location and duration of the testing. For example, landing gear laboratory testing is normally accomplished on a dynamometer and costs vary from $25,000 to $500,000 depending on the

a. Lodging N/A

b. Per Diem N/A

c. Rental Cars N/A

d. Incidentals (Verified) N/A

P/N: A28018-000 contracting office, of intent to qualify as a source for this Power Supply Assembly.

drawing A28018. The offeror may also be required to produce copies of all applicable

DFARS 211.274 as prescribed within the ESA-approved engineering/technical data package. The offeror must provide, at their own expense, data showing the results of all quality, performance, and environmental evaluations conducted by the offeror to show compliance with the of the Power Supply Assembly and other factors.

P/N: A28018-000 contracting officer that the offeror (or its product) meets these standards for qualification or can meet them before the date specified for award of the contract. The award will not be delayed

P/N: A28018-000 waiver of all or part of the qualification requirements. If a waiver is granted and the offeror is awarded a contract, the offeror may still be required to provide a post-contract award first article exhibit to verify minimum, the source shall provide a complete set of drawings for the similar item and written

NA:

Total cost is:

NA_2:

000:

a Chemical:

b Metallurgical:

1 Destructive:

2 NonDestructive:

c Dimensional:

d Electronic:

e Mechanical:

f NonDestructive Inspection:

NA_3:

NA_4:

NA_5:

b FlightData Reduction Analysis Costs:

Section F Travel by Contractor to Test Site if required:

a Lodging:

b Per Diem:

c Rental Cars:

d Incidentals Verified:

NA_6:

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1. National Stock Number (NSN): 5840-01-480-4328

2. Part Number (P/N): A26161-000

3. Noun: Radar Modulator

a. Criticality: Repair/overhaul of this Radar Modulator requires engineering source approval by the engineering support activity 415 SCMS/GUMAD in order to maintain the quality of the part.

Failure to procure repair services for this Radar Modulator from a fully qualified repair source can result in structural or functional deficiencies that will degrade the mission capability of the M3P, AN/MST-T1(V), Mini-MUTES to verify the structural and/or functional integrity and/or fit, form, and interface of the Radar Modulator being procured.

assure the government that the offeror is capable of repairing the Radar Modulator in compliance with the applicable technical specification/data within the schedule and economic of the Radar Modulator and other factors.

NSN: 5840-01-480-4328

P/N: A26161-000 Noun: Radar Modulator offeror to become qualified. This is a requirement of FAR 9.202(a)(1)(ii) and 10USC2319(b)(3)

(1) Destructive N/A

(2) Non-Destructive N/A

c. Dimensional N/A

d. Electronic N/A

e. Mechanical N/A

f. Non-Destructive Inspection N/A the location and duration of the testing. For example, landing gear laboratory testing is normally accomplished on a dynamometer and costs vary from $25,000 to $500,000 depending on the

a. Lodging N/A

b. Per Diem N/A

c. Rental Cars N/A

d. Incidentals (Verified) N/A

P/N: A26161-000 contracting office, of intent to qualify as a source for this Radar Modulator.

drawing A26161. The offeror may also be required to produce copies of all applicable

DFARS 211.274 as prescribed within the ESA-approved engineering/technical data package. The offeror must provide, at their own expense, data showing the results of all quality, performance, and environmental evaluations conducted by the offeror to show compliance with the of the Radar Modulator and other factors.

P/N: A26161-000 contracting officer that the offeror (or its product) meets these standards for qualification or can meet them before the date specified for award of the contract. The award will not be delayed

P/N: A26161-000 waiver of all or part of the qualification requirements. If a waiver is granted and the offeror is awarded a contract, the offeror may still be required to provide a post-contract award first article exhibit to verify minimum, the source shall provide a complete set of drawings for the similar item and written

NA:

Total cost is:

NA_2:

000:

a Chemical:

b Metallurgical:

1 Destructive:

2 NonDestructive:

c Dimensional:

d Electronic:

e Mechanical:

f NonDestructive Inspection:

NA_3:

NA_4:

NA_5:

b FlightData Reduction Analysis Costs:

Section F Travel by Contractor to Test Site if required:

a Lodging:

b Per Diem:

c Rental Cars:

d Incidentals Verified:

NA_6:

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1. National Stock Number (NSN): 5895-01-480-3308

2. Part Number (P/N): A27969-000

3. Noun: Radio Frequency Tuning Unit

a. Criticality: Repair/overhaul of this Radio Frequency Tuning Unit requires engineering source approval by the engineering support activity 415 SCMS/GUMAD in order to maintain the quality of the part. Failure to procure repair services for this Radio Frequency Tuning Unit from a fully qualified repair source can result in structural or functional deficiencies that will degrade the mission capability of the M3P, AN/MST-T1(V), Mini-MUTES to verify the structural and/or functional integrity and/or fit, form, and interface of the Radio Frequency Tuning Unit being procured.

assure the government that the offeror is capable of repairing the Radio Frequency Tuning Unit in compliance with the applicable technical specification/data within the schedule and economic of the Radio Frequency Tuning Unit and other factors.

NSN: 5895-01-480-3308

P/N: A27969-000 Noun: Radio Frequency Tuning Unit offeror to become qualified. This is a requirement of FAR 9.202(a)(1)(ii) and 10USC2319(b)(3)

(1) Destructive N/A

(2) Non-Destructive N/A

c. Dimensional N/A

d. Electronic N/A

e. Mechanical N/A

f. Non-Destructive Inspection N/A the location and duration of the testing. For example, landing gear laboratory testing is normally accomplished on a dynamometer and costs vary from $25,000 to $500,000 depending on the

a. Lodging N/A

b. Per Diem N/A

c. Rental Cars N/A

d. Incidentals (Verified) N/A

P/N: A27969-000 contracting office, of intent to qualify as a source for this Radio Frequency Tuning Unit.

drawing A27969. The offeror may also be required to produce copies of all applicable

DFARS 211.274 as prescribed within the ESA-approved engineering/technical data package. The offeror must provide, at their own expense, data showing the results of all quality, performance, and environmental evaluations conducted by the offeror to show compliance with the of the Radio Frequency Tuning Unit and other factors.

P/N: A27969-000 contracting officer that the offeror (or its product) meets these standards for qualification or can meet them before the date specified for award of the contract. The award will not be delayed

P/N: A27969-000 waiver of all or part of the qualification requirements. If a waiver is granted and the offeror is awarded a contract, the offeror may still be required to provide a post-contract award first article exhibit to verify minimum, the source shall provide a complete set of drawings for the similar item and written

NA:

Total cost is:

NA_2:

000:

a Chemical:

b Metallurgical:

1 Destructive:

2 NonDestructive:

c Dimensional:

d Electronic:

e Mechanical:

f NonDestructive Inspection:

NA_3:

NA_4:

NA_5:

b FlightData Reduction Analysis Costs:

Section F Travel by Contractor to Test Site if required:

a Lodging:

b Per Diem:

c Rental Cars:

d Incidentals Verified:

NA_6:

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1. National Stock Number (NSN): 6110-01-478-3509

2. Part Number (P/N): A26366-000

3. Noun: Voltage Regulator Assembly

a. Criticality: Repair/overhaul of this Voltage Regulator Assembly requires engineering source approval by the engineering support activity 415 SCMS/GUMAD in order to maintain the quality of the part. Failure to procure repair services for this Voltage Regulator Assembly from a fully qualified repair source can result in structural or functional deficiencies that will degrade the mission capability of the M3P, AN/MST-T1(V), Mini-MUTES to verify the structural and/or functional integrity and/or fit, form, and interface of the Voltage Regulator Assembly being procured.

assure the government that the offeror is capable of repairing the Voltage Regulator Assembly in compliance with the applicable technical specification/data within the schedule and economic of the Voltage Regulator Assembly and other factors.

NSN: 6110-01-478-3509

P/N: A26366-000 Noun: Voltage Regulator Assembly offeror to become qualified. This is a requirement of FAR 9.202(a)(1)(ii) and 10USC2319(b)(3)

(1) Destructive N/A

(2) Non-Destructive N/A

c. Dimensional N/A

d. Electronic N/A

e. Mechanical N/A

f. Non-Destructive Inspection N/A the location and duration of the testing. For example, landing gear laboratory testing is normally accomplished on a dynamometer and costs vary from $25,000 to $500,000 depending on the

a. Lodging N/A

b. Per Diem N/A

c. Rental Cars N/A

d. Incidentals (Verified) N/A

P/N: A26366-000 contracting office, of intent to qualify as a source for this Voltage Regulator Assembly.

drawing A26366. The offeror may also be required to produce copies of all applicable

DFARS 211.274 as prescribed within the ESA-approved engineering/technical data package. The offeror must provide, at their own expense, data showing the results of all quality, performance, and environmental evaluations conducted by the offeror to show compliance with the of the Voltage Regulator Assembly and other factors.

P/N: A26366-000 contracting officer that the offeror (or its product) meets these standards for qualification or can meet them before the date specified for award of the contract. The award will not be delayed

P/N: A26366-000 waiver of all or part of the qualification requirements. If a waiver is granted and the offeror is awarded a contract, the offeror may still be required to provide a post-contract award first article exhibit to verify minimum, the source shall provide a complete set of drawings for the similar item and written

NA:

Total cost is:

NA_2:

000:

a Chemical:

b Metallurgical:

1 Destructive:

2 NonDestructive:

c Dimensional:

d Electronic:

e Mechanical:

f NonDestructive Inspection:

NA_3:

NA_4:

NA_5:

b FlightData Reduction Analysis Costs:

Section F Travel by Contractor to Test Site if required:

a Lodging:

b Per Diem:

c Rental Cars:

d Incidentals Verified:

NA_6:

2019-03-13T06:03:44-0600

NGUYEN.THI.D.1515727392

2019-03-13T06:39:33-0600

KENT.BRYSON.C.1385517986

2019-03-25T11:17:46-0600

GARDUNO.KEVIN.J.1249732865

a. Criticality: Repair/overhaul of this Waveguide Assembly requires engineering source approval by the engineering support activity 415 SCMS/GUMBB in order to maintain the quality of the part.

Failure to procure repair services for this Waveguide Assembly from a fully qualified repair source can result in structural or functional deficiencies that will degrade the mission capability of the M3P AN/MST-T1(V).

Waveguide Assembly being procured.

assure the government that the offeror is capable of repairing the Waveguide Assembly in compliance with the applicable technical specification/data within the schedule and economic of the Waveguide Assembly and other factors.

Item Description NSN Part Number Waveguide Assembly 5985-01-480-6043 A27984-000 Waveguide Assembly 5985-01-477-9573 A26057-000 Waveguide Assembly 5985-01-499-2005 A26362-000

5 Mar 2019 Supporting Information offeror to become qualified. This is a requirement of FAR 9.202(a)(1)(ii) and 10USC2319(b)(3)

(1) Destructive N/A

(2) Non-Destructive N/A

c. Dimensional N/A

d. Electronic N/A

e. Mechanical N/A

f. Non-Destructive Inspection N/A the location and duration of the testing. For example, landing gear laboratory testing is normally accomplished on a dynamometer and costs vary from $25,000 to $500,000 depending on the

a. Lodging N/A

b. Per Diem N/A

c. Rental Cars N/A

d. Incidentals (Verified) N/A

5 Mar 2019 Section C 1/3 contracting office, of intent to qualify as a source for this Waveguide Assembly.

verified using in the AN/MST-T1(V) system or equivalent.The offeror shall make their facilities, including change notices, in the offeror’s possession including, at a minimum the reference documents in the following table.

The offeror may also be required to produce copies of all applicable procedures, drawings, or specifications.

offeror must show compliance with Unique Identification (UID) requirements in accordance with DFARS 211.274 as prescribed within the ESA-approved engineering/technical data package. The offeror must provide, at their own expense, data showing the results of all quality, performance, and environmental evaluations conducted by the offeror to show compliance with the government requirements as prescribed by 415 SCMS/GUMBB. The offeror shall also identify its sources for materials and its standards for internally used processes.

submit to 415 SCMS/GUMBB for their prior approval, a qualification test plan/procedure detailing how they intend to verify compliance with all performance, environmental, Item Description NSN Part Number Reference Docs Waveguide Assembly 5985-01-480-6043 A27984-000 A26142 Cage: 8M906 Waveguide Assembly 5985-01-477-9573 A26057-000 A27987Cage: 8M906 Waveguide Assembly 5985-01-499-2005 A26362-000 A26362 Cage: 8M906

5 Mar 2019 Section C 2/3 of the Waveguide Assembly an