6480FJ_AFMC_Form_807_Quality_Productions.pdf

RECOMMENDED QUALITY ASSURANCE PROVISIONS

AND SPECIAL INSPECTION REQUIREMENTS

1. PR / MIPR NUMBER

2. NATIONAL STOCK NUMBER

1560010596480FJ

3. POINT OF INSPECTION

SOURCE DESTINATION

X

SEE DFARS 246.402

4. POINT OF ACCEPTANCE

SOURCE DESTINATION

X

5. ITEM MANAGER / PHONE

Salas, Audrey C / 801-775-4292

6. EQUIPMENT SPEC / PHONE

Flook, Robert G / 801-586-4370

7. CONTRACT QUALITY REQUIREMENTS/SPECIAL INSPECTION REQUIREMENTS

CERTIFICATE OF CONFORMANCE

FAR 52.246-15

CONTRACT RESPONSIBILITY

FOR INSPECTION

FAR 52.246-1

STANDARD INSPECTION

FAR 52.246-2,-3,-4,-5 OR -6

AS APPLICABLE TO CONTRACT

X HIGHER LEVEL CONTRACT QUALITY REQUIREMENTS

AS 9100

COMMERCIAL ITEM INSPECTION

FAR 52.212-4

OTHER (Describe in Block 8)

8. REMARKS

Moore, Ryan SNAME: 07 DEC 2020DATE:

Component requires inspection and acceptance at source because the following criteria as required in AFMCI 23-102:

- Significant Technical Requirements to ensure configuration baseline.

- Critical production features to ensure Safety of Flight aspects of this component; this component is classified as a Fatigue and Fracture Critical Part, Class 1B (IAW SM160M1000) and is a Critical Safety Item (CSI).

- Contract is awarded to manufacturer of this item.

Defense Contract Management Agency (DCMA) will provide the necessary technical and administrative oversight to ensure the requirements in section 7 and the Technical Data Package (TDP) provided by the contract are complied with. Specific aircraft components perform critical functions and are essential for mission success.

Therefore, the following characteristics should be considered in the evaluation by DCMA:

- Material Certifications and use of appropriate raw materials,

- Non-destructive inspections (ultrasonic, penetrant, magnetic particle) to support processing in the manufacture of critical aircraft components and assemblies,

- Corrosion inhibiting applications,

- Dimensional requirements to meet requirements of fit-form-function of critical aircraft components and assemblies to include surface finish and mismatch requirements,

- Peening operations.

The TDP provides the specific requirements for 'accept/reject' criteria that support the areas identified above.

8a. OZONE DEPLETING SUBSTANCES (ODS)

X STATEMENT

"I HAVE REVIEWED THE REQUIREMENT, INCLUDING AVAILABLE TECHNICAL DOCUMENTATION, AND BELIEVE THAT IT DOES NOT REQUIRE THE CONTRACTOR USE CLASS I OZONE DEPLETING SUBSTANCES (ODS) IDENTIFIED IN AIR FORCE POLICY, NOR IS IT WRITTEN SO THAT IT CAN

ONLY BE MET BY THE USE OF A CLASS I ODS."

WAIVER (SEE AF FARS 5323)

NOTE: Quality provisions as annotated hereon will not be downgraded without Technical Authority coordination. The Technical Authority must be notified if award selection is made to a new source using Acquisition Method Code (AMC) 3, 4, or 5.

9. QUALITY PRE-AWARD SURVEY

YES NEW SOURCE

PREVIOUS SOURCEX NO

AFMC PARTICIPATION

RECOMMENDED

10. CODES

A. I&A

B. CQR

G

11. SIGNATURE OF TECHNICAL AUTHORITY

Moore, Ryan S

ORGANIZATION / SYMBOL

416 SCMS / GUMBA

PHONE

801-777-9920 / 777-9920

DATE

07 DEC 2020

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