5_Quality_Assurance_Letter_of_Intstruction.pdf

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Attached to
Amendment to extend the due date. Remanufacture of ACES II, Vernier Rocket Motor (Seat Stabilization Rocket Motor)
Solicitation number
FA8213-21-R-1264
Issued by

About this file

This document contains a quality assurance letter of instruction and details of a related federal contract opportunity for remanufacturing ACES II Vernier Rocket Motors. The quality assurance letter outlines mandatory inspection points for the contractor such as stamps and signatures on manufacturing documentation, leak testing, x-ray inspection, and lot certification dates for energetic materials. Additional inspection points may be imposed. The related solicitation seeks the remanufacture of ACES II Vernier Rocket Motors used for seat stabilization in aircraft ejection systems. The one-pound explosive charge motors are predominantly steel and function to stabilize the ejection seat. The solicitation was issued by 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

PR No. FD2020-

Date Contract Awarded

Final Delivery Date (FDD)

Program Name

DODIC

Part Number

The contractor, at a minimum, shall allow DCMA to inspect the following points:

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

Witness - W: GSI required to attend per comment section.

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 per comment section.

Notify - N: By phone or email prior to action.

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

Prepared by:

Date

THIS PLANNING SHEET WILL BE UPDATED IF NECESSARY.

QUALITY ASSURANCE LETTER OF INSTRUCTION

Planning Requirements

COMMENTS

NOTICE

Engineer Signature

Rev Date: 5 May 2019

Sheet1

Text46: 9APR2021
2021-04-09T14:21:17-0600
JOHNSON.AVERY.STEVEN.1457505112
undefined_9: N
Text32: 9. Additional Requirements
undefined_8: M
Text31: 8. Shippers (DD250, Reports)
undefined_7: M
Text30: 7. AMMO Data Card Review
undefined_6: V
Text29: 6. Preparation for Shipment
undefined_5: W
Text28: 5. LAT
undefined_4: V
Text27: 4. LAT Sample Selection
undefined_3: V
Text26: 3. X-Ray/N-Ray
undefined_2: M
Text25: 2. Leak Test
undefined: V
Text36: 1. Explosive Weight

2. Verify gross leak and fine leak check are performed.

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

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

5. Testing should occur in accordance with latest government approved ATP. Prior to LAT ensure proper calibration and validation of all test equipment. Witness proper test setup and at least the first 3 functional tests. Further witnessing may be required if there are known concerns with the item or requested by Government Engineer.

6. Ensure Paperwork is correct.

7. Verify all energetic materials: list original manufacturer,original lot number, and latest certification/recertification date < 24 months.

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

9. Any additional requirements imposed by DCMA shall be approved by Government Project Engineer

Text24: 1.Inspection
Part Number: 50436-11
DODIC: MT32
Text20: 12116
Text19: NAMMO
Part Number Line 2:
Contract No: 21-51264
Date Contract Awarded:
Final Delivery Date FDD:
Program Name: ACES II Vernier RM

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