Attachment_Z_-_QA_Form.pdf

QUALITY ASSURANCE REQUIREMENTS

Note: This form as completed by the customer shall be incorporated into the solicitation/contractual award document.

Inspection:

[ ] Inspection and Acceptance at Source (I&AS)

[ ] Acceptance at Destination

[X] Initial Inspection at Source with Final Inspection and Acceptance at Destination (based on repeat sample of I&AS.)

[ ] Inspection Time Frame:

Certifications:

One copy of these certifications must accompany the parts upon delivery. The packet/envelope holding these documents must be legibly marked “Certifications Enclosed” and must protect them in transit.

One copy of these certifications must be forwarded to:

NSWC Indian Head Explosive Ordnance Disposal Technology Division System Engineering Department Attention: Kyle Foley 3703 Benson Road, Building 3157 Indian Head, MD 20640

Inspection Tests for Adhesive Bonded Composite Structures

Acceptance Tests: see note 1

Q ua lit at iv e Visual Inspection, see note 2

Glove Test, see note 3

Tap Test, see note 4

Q ua nt ita tiv e

Adhesive Film Bond Test, see note 5

Finished Part Weight, ± 0.10 lb, for information only

Inspection Tests for Adhesive Bonded Composite Structures (Continued)

The Following Notes Apply to Acceptance Inspections Test Setup and Methods

Document and archive the material lots and material certifications used by fin serial number.

Note 1: If a fin fails any acceptance inspection test, define and archive corrective action and approvals. Indicate location and area of any defects.

Note 2: Visual Inspection – Perform a visual inspection per MIL-HDBK-349 (Manufacture and Inspection of Adhesive Bonded, Aluminum Honeycomb Sandwich Assemblies for Aircraft). Mark the location of any surface defects on the glove test and visual inspection sheet.

Note 3: Glove Test – Wearing a cotton inspection glove place extended palm of your hand on the fin’s surface.

Gently move your hand over the entire surface (both sides). Mark the location of any surface irregularities, voids, or paint defects on the glove test and visual inspection sheet. Use Dow Corning 93-076, or equivalent, to fill any voids and refinish the fin. Repeat the glove test on any reworked hardware.

Note 4: Tap Test – Perform a tap test per 1030-9006. If manual tap test is performed MIL-HDBK-349 (Manufacture and Inspection of Adhesive Bonded, Aluminum Honeycomb Sandwich Assemblies for Aircraft) provides the methodology and requirements for the tap hammer.

Note: 5 Adhesive Film Bond Test – Prepare 3 samples per fin kit and perform bond test in accordance with ASTM C 297(Standard Test Method for Flatwise Tensile Strength of Sandwich Constructions). Test samples shall be prepared using the same material lots and production practices as the fins and be cured with the fins.

Acceptance criteria shall be established by the contractor as part of the quality program plan.

Certifications Are Required For The Following:

X- Indicates Required. NR- Indicates Not Required. Two sets of certifications must be submitted.

Part Name:GQM-163A BOOSTER FIN Part Number: 1030-5082-002 Revision: 1

Certificate of Analysis

Certificate of Compliance

Certify that fins meeting all requirements of 1030-5082 X Dimensional inspection data for all features and notes, drawings 1030-

5082 FIN, BOOSTER MK 70, ME46195 TERRIER 4.8 SQ FT FIN

ASSEMBLY, C34242 FIN POST BUSHING FOR (TERRIER/Mk70), ME52224 BRACE, 1181AS302 FIN CANT BLOCK , ME46329

LEADING EDGE, ME46310 CAP, ME46309 DISC, ME46060

BOTTOM FITTING, ME46039 SPAR, ME52225 FILLER PLATE,

ME46062 CHANNEL, and ME46279 SKIN

X X

Tap test per 1030-5082 find 4 (1030-9006) X X

Glove test and visual inspection sheet X X Zinc Chromate, certification to TTP17578-1YC-001P per parts list 1030-5082 find 5 and 1181AS302 note 4 X

Part Name:GQM-163A BOOSTER FIN Part Number: 1030-5082-002 Revision: 1

Certificate of Analysis

Certificate of Compliance

Hardware certification for item numbers 8, 9, 10, 11, 12, 13, 19, 20, 22, and 23 of drawing ME46195 X

Plane Surface Flatness per note 8 of drawing ME46195 X

Chord Plane per note 9 of drawing ME46195 X

HT 424 Adhesive Film or equivalent certification to SAE AMS-A- 25463 Type III X X

Core Aluminum Honeycomb 1/4-5056.002P (Perforated Aluminum 5056-H39) X X

Dow Corning 93-076 (or equivalent) certification if used, note 13 drawing ME46195 X X

Aluminum, certification to 2024-T3 per drawing ME46279 X X

Aluminum, certification to 6061-T6 per C34242, ME46310, ME46060, ME52225, ME46062 X X

Steel, certification to 4140 per drawing ME46039 X X

Cadmium plate, certification to AMS 2400P per drawing ME46039 X

Heat treat, ultimate strength=150 ksi, yield strength=132 ksi per drawing ME46039 note 6 X X

Aluminum, certification to 6061-T6 1/8” stock per drawing ME46309 X X

Stainless Steel 0.032” thick, certification per drawing ME46329 X

Steel, certification to 4140 or 4340 per note 2 of drawing 1181AS302 X X

Heat treat, certification per note 2 of drawing 1181AS302 X

Hardness, certification to Rockwell C hardness 38-42 per drawing 1181AS302 note 2 X X

Stainless Steel, certification to 304 Stainless Steel per drawing

ME52224 X X

Note: Customer is to select the Special Clause(s) below as applicable. The selected clause(s) shall be incorporated into the solicitation/contractual award document.

Special Clauses:

[X] IHD 45 – SAMPLING OF RECEIVED MATERIAL – ORDNANCE MATERIAL AND

ORDNANCE COMPONENTS (NAVSEA/IHD) FEB 2000

a. When NSWC IHEODTD, Naval Sea Systems Command, Indian Head, Maryland, receipt inspects ordnance material or ordnance components under this contract for Naval rockets or missiles, the following sampling procedures will be used:

MIL-STD-1916

Level V for Critical Dimensions Level II N<200 Level III N>200 for majors Level I N<100 Level II N>100 for minors

b. In all cases, the acceptance number will be zero (0); the entire lot will be rejected for any defect.

c. Notwithstanding the above NSWC IHEODTD, Naval Sea Systems Command, Indian Head, Maryland, may at its discretion, accept a defect on a waiver on a case-by-case basis.

[ ] IHD 46 – SAMPLING OF RECEIVED MATERIAL – MANRATED MATERIAL

(NAVSEA/IHD) FEB 2000

a. When NSWC IHEODTD, Naval Sea Systems Command, Indian Head, Maryland, receipt inspects man-rated material under this contract for rockets, catapults, cartridge actuated devices and their components, the following sampling procedures will be used:

MIL-STD-1916

Level VI for Critical Dimensions Level II N<200 Level III N >200 for majors Level I N<100 Level II N>100 for minors

b. In all cases, the acceptance number will be zero (0); the entire lot will be rejected for any defect.

c. Notwithstanding the above, NSWC IHEODTD, Naval Sea Systems Command, Indian Head, Maryland, may at its discretion, accept a defect on a waiver on a case-by-case basis