3_Quality_Assurance_Letter_of_InstructionI_F_16_CJRM.pdf

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Attached to
F-16 Rocket Motor
Solicitation number
FA8213-20-R-0080
Issued by

About this file

This document contains a quality assurance letter of instruction and related federal contract opportunity notice for rocket motors used in F-16 aircraft. The quality assurance letter provides inspection requirements for critical flight items to be imposed on work orders, including mandatory stamping and witness requirements. Specific inspection points are listed for explosive weight verification, leak testing, radiographic film reviews, lot acceptance testing sample selection and procedures, preparation for shipment, ammunition data card reviews, shipping documentation verification, and additional requirements. The related federal contract opportunity is a pre-solicitation notice seeking rocket motors identified by national stock numbers, part numbers, and descriptions for the F-16 aircraft. The opportunity specifies line items, quantities, destinations as FMS countries, an electronic solicitation procedure, and a contract period through final production and delivery of all units. The contracting agency is identified as the Department of the Air Force Materiel Command Lifecycle Management Center located at Hill Air Force Base.

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Text version

Contractor Name CAGE code

DCMA QAR Reviewer

Date Review Completed

Date Issued to Contractor

PR No. FD2020-

Date Contract Awarded

Final Delivery Date (FDD)

Program Name

DODIC

Part Number

The contractor is required to impose the listed below DCMA Inspection Points into the appropriate Work Orders.

All Work Orders pertaining to CRITICAL FLIGHT ITEMS must be identified on folders.

Mandatory - M: Stamp and/ or Signature on original documentation (i.e., Mfg. Planning, ATP, FAT Report, etc.)

Witness - W: GSI required to attend, may reduce level of effort after 50% of production lots found acceptable

Verification - V: Stamp and/or Signature required unless noted otherwise (may be done by written verification)

Monitor - R: Will monitor testing, may reduce to verification

Notify - N: By phone or email

Additional requirements: (DCMA reserves the right to impose additional inspection points as deemed necessary.)

Prepared by:

Date

Concurrence Signature by QAR/DCMA:

QAR/DCMA

THIS PLANNING SHEET WILL BE UPDATED IF NECESSARY.

QUALITY ASSURANCE LETTER OF INSTRUCTION

Planning Requirements

COMMENTS

NOTICE

Engineer

Date

Sheet1

Contract No: 20-50080
Date Contract Awarded:
Final Delivery Date FDD:
Program Name: F-16
DODIC: MT33, MT34
undefined: V
undefined_2: V
undefined_3: V
undefined_4: M
undefined_5: W
undefined_6: V
undefined_7: V
undefined_8: V
undefined_9: N
undefined_10:
undefined_11:
undefined_12:
Text19:
Text20:
Text21:
Text22:
Text23:
Text24: 1.Inspection
Text25: 2. Leak Test
Text26: 3. X-Ray/N-Ray
Text27: 4. LAT Sample Selection
Text28: 5. LAT
Text29: 6. Preparation for Shipment
Text30: 7. AMMO Data Card Review
Text31: 8. Shippers (DD250, DD1149, Reports)
Text32: 9. Additional Requirements
Text33:
Text34:
Text35:
Text36: 1. Verify that the Explosive Weight is identified and meets drawing and hazard classification requirements.

2. Verify gross/fine leak checks are performed per ATP requirements

3. Ensure film labeling correct. Ensure radiographic film readable / well-defined. DCMA not required to interpret film.

4. Randomly select LAT units per latest government approved ATP.

5. Prior to LAT ensure proper calibration and validation of all test equipment. Testing should occur in accordance with latest government approved ATP.

6. Ensure Paperwork is correct.

7. Verify all energetic materials: list original manufacturer, original lot no., and latest certification/recertification date < 24 months.

8. Ensure Paperwork is correct. Verify Packaging, Packing, Preservation & Marking (PPP&M)

9. Notify and obtain approval from the Project Engineer for any additional requirements imposed by DCMA.

2018-05-30T15:54:10-0600
TIDWELL.QUINN.RAY.1241451913
Text46: 29 April 2019
Text49:
Type name_1:
Type name_4:
Part Number:
Noun: 1517-001, 1517-002, 55000-1, 55000-2

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