P-245-2003.doc

REVISION No. A .

CHANGE No. .

TITLE

PURCHASE SPECIFICATION FOR PROPELLERS

USED ON 175 FT

WLM BUOY TENDER

P-245-2003

ORGINATED BY MIKE GASKINS DATE 04/2009 .

ORGINATOR’S COMMAND ENGINEERING LOGISTICS CENTER (ELC)

DEPARTMENT / DIVISION EQUIPMENT MANAGEMENT DIVISION (CODE 026).

INTERNAL REVIEWER DATE .

SOWRB APPROVAL DATE .

PURCHASE SPECIFICATION FOR PROPELLERS

USED ON 175 FT WLM BUOY TENDERS

1.0 SCOPE

1.1. This document sets forth the requirements for the manufacture, testing, inspection, preservation, packaging packing and marking of right hand (RH) and left hand (LH) marine monobloc propellers applicable to the U.S. Coast Guard 175 foot WLM Buoy Tender Vessels. The quantity and type of propellers purchased under this specification will be indicated on each Contract Deliverables List.

1.2. CLASSIFICATION

1.2.1. Propeller Types

a Type 1 - Left Hand (LH), P/N 175-WLM-245-002LH b Type 2 – Right Hand (RH), P/N 175-WLM-245-002RH

1.2.2. GOVERNMENT FURNISHED EQUIPMENT (GFE) - The listed item is property of and managed by the USCG Engineering Logistics Center, Baltimore MD.

a Gauge Set, Type 1 - Consisting of a plug and ring gauge.

2.0 APPLICABLE DOCUMENTS

2.1. GENERAL – The documents listed in this section are specified in sections 3, 4, or 5 of this specification. This section does not include documents cited in other sections of this specification recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements cited in Sections 3, 4, or 5 of this specification, whether or not they are listed.

2.2. GOVERNMENT DOCUMENTS

2.2.1. SPECIFICATIONS, STANDARDS, PUBLICATIONS, AND HANDBOOKS – The following specifications, standards, publications, and handbooks form a part of this specification to the extent specified herein. Unless otherwise specified, the versions in effect are those listed in the GSA Index of Federal Specifications, Standards and Commercial Item Descriptions or the current Department of Defense Single Stock Point of Specifications And Standards, (DODSSP), and supplements thereto, cited in the solicitation or contract.

2.2.2. SPECIFICATIONS

a MIL-DTL-2845E(SH) - dated 18 AUG 1999, Propulsion Systems, Boat and Ship; Main Shafting, Propellers, Bearings, Gauges, Special Tools, and Associated Repair Parts; Preservation, Packaging, Packing and Storage of

2.2.3. STANDARDS

a MIL-STD-2035A(SH) - Dated 15 MAY 1995, Nondestructive Testing Acceptance Criteria b DOD-STD-2185(SH) - Dated 28 OCT 1986, Requirements for Repair and Straightening of Bronze Naval Ship Propellers

2.2.4. PUBLICATIONS & OTHER GOVERNMENT DOCUMENTS

a USCG Drawing No. 175-WLM-245-002 REV A, Dated 06/27/07 b COAST GUARD SPECIFICATION D-000-0100 - Dated 10/91 REV G 02/06, Bar Coding for USCG Engineering Logistics Center Procured Material c NAVSEA TECHNICAL MANUAL S9245-AR-TSM-010/PROP Dated 31 MARCH 1997, Technical Manual Marine Propeller Inspection, Repair and Certification, NSN 0910-LP-012-5880 d NAVSEA TECHNICAL MANUAL S9243-A5-MMD-010 Dated 30 November 1995 – Gages, Plug and Ring, Propellers and Propulsion Shafting; Repair, Inspection, Certification and Use e T9074-AS-GIB-010/271 - Dated 16 FEB 1999, Requirements for Nondestructive Testing Methods

2.3. COMMERCIAL DOCUMENTS

2.3.1. American Bureau of Shipping (ABS)

a Guide for Bronze and Stainless Steel Propeller Castings - Dated 2008

2.3.2. Society of Automotive Engineers (SAE)

a SAE-J-448A - Dated June 1963, Surface Texture Standard b SAE AMS-T-22085 - Dated 01 June 1999, Tapes, Pressure-Sensitive, Adhesive, Preservation and Sealing–FSC 7510

2.3.3. American National Standards Institute (ANSI)/National Conference of Standards Laboratories (NCSL) a ANSI/NCSL Z540-1-1994 – Dated 1994, General Requirements for Calibration Laboratories and Measuring and Test Equipment

2.3.4. American Society For Quality Control (ASQC)

a ANSI/ASQC Q9003-1994 - Dated 1994, Quality Systems - Model for Quality Assurance in Final Inspection and Test

2.3.5. International Organization For Standardization (ISO)

a ISO 484/2 – Shipbuilding-Ship Screw Propellers-Manufacturing Tolerances - Part 2: Propellers of Diameter Between 0.80 and 2.50 m Inclusive

2.4. DOCUMENT AVAILABILITY - To obtain the referenced documents see section 6.1.

2.5. ORDER OF PRECEDENCE - In the event of a conflict between the text of this specification and the references cited herein, the text of this specification takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

3.0 REQUIREMENTS

3.1. GENERAL – The Contractor shall provide all equipment, labor and materials to manufacture, test, inspect, preserve, package, pack and mark Left Hand (LH) propellers and Right Hand (RH) propellers in accordance with the referenced drawing(s) and data provided within this specification.

3.2. GOVERNMENT FURNISHED EQUIPMENT (GFE) - The Contractor shall provide protective storage for the GFE when not in use, and safe handling when in use.

3.2.1. The storage area shall, at a minimum, be closed on all sides, dry, and locked when unattended.

3.3. TEST AND INSPECTION PLAN - The Contractor shall submit a test and inspection plan to the Contracting Officer for approval. This plan shall include the specific inspections and tests specified herein, and all tests and inspections made by the Contractor to verify conformance to every requirement and tolerance as specified in the cited drawings, technical publications, and this specification.

3.4. MATERIAL - Each propeller shall be manufactured from ABS Type 4 Nickel Aluminum Bronze, consisting of the chemical composition and tensile properties listed in ABS Part 7 Section 10 entitled Guide for Bronze and Stainless Steel Propeller Castings (Dated 2008).

3.4.1. The Contractor shall perform a material chemical composition analysis and a tensile properties test for each propeller casting. The documented results shall be submitted to the Coast Guard Contracting Officer for review/approval.

3.4.2. All material chemical composition analysis and tensile property tests shall be made by a laboratory meeting the calibration requirements in section 4.6 of this specification.

3.5. CONSTRUCTION OF PROPELLER CASTINGS – Each propeller casting shall be constructed in accordance with ABS Part 7 Section 10 entitled Guide for Bronze and Stainless Steel Propeller Castings (Dated 2008), and USCG DWG. NO. 175-WLM-245-002 REV A, Dated 06/27/07.

3.5.1. Each propeller casting shall be formed with one continuous pour.

3.5.2. A separate test coupon shall be provided for every casting poured. This coupon shall be tested for it’s chemical composition and tensile properties referenced in 3.2.1 of this specification.

3.6. PROPELLER FINISHING – Each propeller may be finished using Computer Numerical Controlled (CNC) machining using equipment that can be programmed for automatic contouring of hydrodynamic surfaces or in the conventional casting manner that employs hand grinding and finishing for obtaining required blade contour and profile dimensions.

3.6.1. The tolerances specified at the design sections shall apply to all hydrodynamic surfaces.

3.6.2. The Contractor shall demonstrate a manufacturing or inspection process that ensures tolerances for all hydrodynamic surfaces are met.

3.6.3. Dimensional Inspection shall be in accordance with this specification and USCG DWG. NO. 175-WLM-245-002 REV A, Dated 06/27/07.

3.7. DIMENSIONAL TOLERANCES

3.7.1. Propeller tolerances shall be in accordance with USCG DWG. NO. 175-WLM-245-002 REV A, Dated 06/27/07 and this specification.

3.7.2. Blade thickness at each design section shall be within plus 2 percent or minus 1 percent of the maximum thickness of the blade section with a minimum of plus 2 mm or minus 1 mm.

3.7.3. Blade section width at each design radius shall be plus or minus 1.5 percent of the diameter divided by the number of blades.

3.7.4. Pitch deviation at each design section shall not exceed plus or minus 1.50 percent.

3.7.5. Pitch variation between adjacent design sections on each blade shall not exceed 0.75 percent.

3.7.6. Average Pitch deviation of all design sections on each blade shall not exceed plus or minus 1.00 percent.

3.7.7. Angular spacing of the blade center axes shall be plus or minus 0.50 degrees

3.7.8. Clearance under the fairing rod shall not exceed 1.5 mm (0.060”) and shall not vary at a rate greater than 0.25 mm per millimeter (0.010 inches per inch).

3.8. EDGE GAGES – The Contractor shall fabricate edge gages from 18 gauge galvanized steel sheet to demonstrate that the blade profile conforms to drawing requirements during final inspection.

3.8.1. Leading and trailing edge gages shall be provided for the .4, .7, .9 and .95 radii. Each gage shall be gapped in a manner that allows independent measurement of either the pressure or suction face contours for the relevant section. Each gage shall also include provisions to measure the edge radius. Refer to figure 4 of ISO 484/2 dated 08/15/1981 for general guidance.

a GAGE MARKING - Each edge gage shall be engraved or etched (no stamping) with the following information:

1. Drawing Number: 175-WLM-245-002

2. “SF” or “PF” in the appropriate upper or lower corner of the edge gage open end

3. “LE” or “TE” as applicable

4. Radius as applicable (example 0.4.)

3.8.2. All fabricated edge gages shall become the property of the USCG and shall be preserved, packaged, packed, and shipped to the Contracting Officer upon completion of the contract.

a A reusable wooden container shall be fabricated using marine grade plywood in the style of a footlocker with individual partitions to separate and protect each edge gage. The container shall have a hinged lid, a hasp style lock, and a handle on each end. All hardware shall be made of corrosion resistant stainless steel. The Contractor shall also provide a new keyed padlock such as Master Lock #5KA-K#A389 or equivalent with 4 keys to secure the container’s contents. All interior/exterior wood surfaces shall be sealed with a wood sealer/preservative.

b Each edge gage shall be placed in the container with the face or flat surface perpendicular to the container base.

3.9. HUB BORE INSPECTION – The Contractor shall demonstrate that the finished hub bore for each propeller meets dimensional requirements by utilizing a government furnished plug gage to perform the inspections outlined below. These inspections shall be conducted in accordance with Chapter 3 of NAVSEA Technical Manual S9243-A5-MMD-010 entitled Gages, Plug and Ring, Propellers and Propulsion Shafting; Repair, Inspection, Certification and Use. All inspection data shall be recorded and included with the final inspection report referenced in section 3.13 of this specification.

a Plug gage to hub bore contact impression - The tolerance shall be 80% contact uniformly distributed over the forward and aft lands of the propeller taper area.

b Plug gage depth of insertion (hub bore diameter) - The tolerance shall be calculated from Table 3-1 of NAVSEA Technical Manual S9243-A5-MMD-010.

c Plug gage key to propeller hub keyway side and top clearances at forward and aft end of keyways – The tolerance shall be calculated from Table 3-1 of NAVSEA Technical Manual S9243-A5-MMD-010.

3.10. WELD REPAIRS - If the castings require any weld repairs, welding procedures, welders, and welding operations shall be qualified in accordance with S9074-AQ-GIB-010/248 or approved in accordance with the procedures outlined in ABS Guide for Bronze and Stainless Steel Propeller Castings (dated 2008), paragraph 1.7.2. Certification documentation shall be maintained and available to the Contracting Officer for review at any time during the contract period.

3.10.1. No weld repair is authorized unless prior approval is received from the Contracting Officer.

3.10.2. Welding on the pressure face of any propeller casting in the critical area shall not be undertaken without prior approval of the Contracting Officer.

a The critical area is described as the pressure face of the blades between the fillet and the .4 radius and starting at the leading edge encompassing 80% of the chord length taken at the 0.4 radius. (Reference Figure 1 of DOD-STD-2185(SH).

b Welding repairs of propeller castings shall meet the requirements of DOD-STD-2185(SH) or ABS Guide for Bronze and Stainless Steel Propeller Castings (dated 2008).

3.11. SURFACE FINISH - Surfaces of the propeller blades and hub shall be ground fair and polished in accordance with SAE-J-448 to meet the following requirements:

3.11.1. Propeller blade surfaces – 1.6 micro-meters (64 micro- inches) or better.

3.11.2. Propeller Hub – 3.2 micro-meters (125 micro-inches) or better.

3.12. BALANCING – After completion of all required manufacturing processes, each propeller shall be single plane balanced on dynamic (rotating) balancing equipment. The residual unbalance in each plane of correction shall not exceed the value determined by calculating the following formula: U = 62.3W/N2 where:

U = Maximum allowable residual unbalance in N-m W = Weight of rotating part in Kg (660 kg estimated)

N = Maximum operating speed of unit (403 RPM)

U = 0.25 N-m (25.8 kg-mm) Prior to performing any balance tests, the Contractor shall demonstrate the sensitivity of the balance machine using a weight determined from the following formula: Ws = 0.1(U)/r where:

Ws = Sensitivity Weight

U = Propeller Residual Unbalance Tolerance r = radial location of the weight

The addition of this weight shall be easily detected and discernable to the balance machine operator.

3.12.1. The mandrel or concentric rings used to support the propeller during balancing shall not exceed a total indicated run-out (TIR) of 0.025 mm.

3.12.2. Material removed to effect balancing shall be taken from the suction face of the heavy blade. Care shall be taken to keep a fair surface.

a The area from which metal is taken shall not come within 10 percent of the chord length to the leading or trailing edges.

3.12.3. The actual amount of unbalance for each propeller shall be documented on each Final Inspection Report.

3.13. SURFACE INSPECTIONS

3.0 A visual inspection shall be performed on all exterior blade surfaces in accordance with MIL-STD-2035(SH), section 4.

a All visual defects, even though deemed acceptable, shall be documented on the inspection report.

3.13.2. The Contractor shall perform a dye penetrant inspection over 100 percent of the blade surfaces including the hub in accordance with T9074-AS-GIB-010/271. The acceptance criteria of MIL-STD-2035(SH) Table IV shall be used for evaluations.

3.13.3. The Contractor shall document all propeller defects resulting from the visual and dye penetrant inspections. These defects shall be indicated by type and size on visual inspection sheets. Each propeller will require individual inspection sheets for the pressure face of the blades, suction face of the blades, the fillet, and the hub.

3.14. TEST AND INSPECTION DATA REQUIREMENTS, FINAL INSPECTION REPORT – The Contractor shall perform final dimensional, balancing, visual, and dye penetrant surface inspections for each propeller manufactured and record this data on a final inspection report. This report shall accurately reflect the final condition of each propeller.

3.14.1. The final inspection report shall contain, at a minimum, the following data:

a Propeller blade radius.

b Pitch at the 0.3 through 0.95 radii.

c Average pitch of each blade at the 0.3 through

0.95 radii.

d Blade section widths at the 0.3 through 0.95 radii.

e Thickness at every 10 percent station for each blade section from the 0.3 through 0.95 radii.

f Leading and trailing edge profiles at the 0.4, 0.7, 0.9, and 0.95 radii g Rake h Track i Angular spacing of blade center axes.

j Fairing rod clearances k All propeller hub dimensions including taper and

Keyway using a government furnished plug gage l Surface finish of blade and hub areas m Surface inspection (visual and 100 percent dye penetrant) n Material composition o Balancing Data

3.14.2. The Final Inspection Report shall be submitted to the Contracting Officer for review. If this report is determined to be acceptable, the Contracting Officer will authorize ELC’s Quality Assurance Branch to schedule final inspections/tests outlined in section 4.4. of this specification.

3.15. PROPELLER STAMPING - Each propeller shall be stamped in accordance with the Marking data provided on USCG DWG. NO. 175-

WLM-245-002 REV A, DATED 06/27/07.

3.15.1. The stampings shall be at least 1/4" high, neat and legible.

NOTE: THE SERIAL NUMBER FOR EACH NEW PROPELLER MANUFACTURED IN ACCORDANCE WITH THIS SPECIFICATION WILL BE PROVIDED BY THE CONTRACTING OFFICER.

3.16. PHOTO DOCUMENTATION – The Contractor shall provide Photo Documentation to the Contracting Officer during in-process welding repairs of the casting (if applicable), after final inspection, and during preservation, packaging, and packing. Each photograph shall include the propeller serial number and date the photograph was taken. The color photographs shall be taken with a digital camera and the images provided electronically in “jpg format” to the Contracting Officer during the manufacturing phases outlined below.

3.16.1. PHOTO DOCUMENTATION PHASES:

a During the dye penetrant inspection showing any linear/non-linear discontinuities of the propeller casting.

b During repair of the propeller casting whenever welding is required.

c After final inspection prior to preservation showing surface texture/finish of the suction face, pressure face, fillet and hub. Stamped markings shall also be photographed.

d Prior to inserting the propeller in the shipping container, showing strippable compound application and sheet metal blade edge protectors installed.

e Prior to shipment, showing container markings.

3.16.2. In addition to providing electronic photographs at the various manufacturing phases indicated, the Contractor shall provide a final Compact Disc (CD) to the Contracting Officer that includes all of the pictures referenced in 3.14.1. The pictures on this CD shall be organized in “jpg format” within folders labeled as follows: NDT Inspection (photos referenced in 3.14.1.a); Welding Repair (photos referenced in 3.14.1.b); Surface Finish/Hub Stamping(photos referenced in 3.14.1.c); and Preservation, Packaging, and Markings (photos referenced in 3.14.1.d and e).

3.17. NOTIFICATIONS & INSPECTIONS - The Contractor shall be responsible for notifying the Contracting Officer at least seven (7) calendar days prior to inspections or monitored testing required herein.

4.0 QUALITY ASSURANCE (Q.A.)

4.1. GENERAL - The Contractor shall provide and maintain an inspection system which shall ensure each item offered to the Government for acceptance conforms to contract requirements. The system shall be documented and meet the requirements of ANSI/ASQC-Q9003.

4.2. RESPONSIBILITY FOR INSPECTION - The Contractor shall be responsible for the performance of all inspection requirements as specified herein. The Contractor may use his own or any other facilities for the performance of the inspections and tests, unless disapproved by the government. The government reserves the right to perform any of the inspections and tests set forth in this specification at any time.

4.3. RESPONSIBILITY FOR COMPLIANCE - All items shall meet the requirements of this specification. The inspections set forth in this specification shall become part of the Contractor's overall inspection system or quality program. The absence of any inspection requirements in the specification shall not relieve the Contractor of the responsibility of assuring that all products or supplies submitted to the Government for acceptance comply with all requirements of the contract. Sampling for quality conformance does not authorize submission of known defective material (either indicated or actual) nor does it commit the Government to acceptance of defective material.

4.4. INSPECTIONS/TESTS - The inspections and tests required herein are the minimum necessary and are not intended to replace any controls, examinations or tests normally employed by the Contractor to assure the quality of the product. The following are required and will be monitored by a Government Quality Assurance Representative.

4.4.1. Dimensional inspections, including the hub bore, in accordance with section 3.6 of this specification.

4.4.2. Leading and Trailing edge profiles on both the suction and pressure faces of each blade using the gages fabricated in section 3.7.

4.4.3. Surface inspections in accordance with section 3.9 of this specification.

4.4.4. Balancing inspection in accordance with section 3.10 of this specification.

4.4.5. Stamping inspection in accordance with section 3.13 of this specification.

4.4.6. Preservation, packaging and marking in accordance with 5.0 of this specification.

4.5. TEST AND INSPECTION REPORTS - One copy of any inspection, test or tolerance check report shall be sent to the Contracting Officer.

4.5.1. A copy of any test, inspection or tolerance check report shall also be provided to the Coast Guard Quality Assurance Representative upon arrival at the Contractor's plant.

4.5.2. All out of tolerance readings on any inspection, test or tolerance check report submitted to any Coast Guard representative shall be easily identified through highlighting, color coding, shading, circling or other prominent marking.

4.6. CALIBRATION SYSTEM - The Contractor as well as any subcontractors shall be required to maintain a test equipment calibration program in compliance with ANSI/NCSL Z540-1. The program shall be documented and traceable to the National Institute of Standards (NIST).

4.6.1. The calibration system records shall be maintained for inspection for the duration of any contract referencing this specification.

4.7. PACKING INSPECTION - The Contracting Officer shall be notified prior to the preservation, packaging, packing, and marking of the completed units in accordance with section 3.14.

5.0 PRESERVATION, PACKAGING & PACKING, & MARKING

5.1. PRESERVATION & PACKAGING

5.1.1. PROPELLERS: Type 1 – Left Handed (LH), P/N 175-WLM-245-002LH; Type 2 – Right Handed (RH), P/N 175-WLM-245-002RH a Prior to preservation, each propeller shall be cleaned by any process or combination of processes which will accomplish thorough cleaning without damage to the propeller.

b After cleaning, tape conforming to SAE-AMS-T-22085, TYPE II and strippable compound preservative shall be applied to each propeller in accordance with MIL-DTL-2845(SH), paragraph 3.14.1.3.

c After the application of strippable compound, galvanized sheet metal blade edge protectors shall be installed in accordance with MIL-DTL-2845(SH), paragraph 3.14.1.4.

5.2. PACKING

5.2.1. PROPELLERS: Type 1 – Left Handed (LH), P/N 175-WLM-245-002LH and Type 2 – Right Handed (RH), P/N 175-WLM-245-002RH a Each propeller shall be individually packed in a new Contractor furnished multiple trip wooden container consisting of a skid type base and a one piece container cover (ends, sides, and top fastened together). Construction shall be in accordance with MIL-DTL-2845(SH), paragraph 3.14.2.2.2.

5.3. MARKING - Each packaged, and packed propeller shall be marked in the upper left-hand side of the two longest sides, (two opposite sides if square) of each wooden container. The container lettering shall be black painted stencil and permanently affixed. The lettering shall be at least 1” high, and be applied on a highly contrasting, painted background.

5.3.1. This marking shall consist of the STOCK NUMBER, ITEM NAME, PART NUMBER, SERIAL NUMBER, SHIPPING WEIGHT (in lbs.), CONTRACT NUMBER, CONDITION CODE ie. CONDITION A, UNIT OF ISSUE with QUANTITY (1) and the words COAST GUARD ELC MATERIAL.

5.3.2. MARKING LAYOUT

a TYPE 1 - PROPELLER, LEFT HAND (LH)

STOCK NUMBER 2010-01-F07-1221

ITEM NAME PROPELLER, LH

PART NUMBER 175-WLM-245-002LH

SERIAL NUMBER As provided by Contracting Officer SHIPPING WEIGHT As determined by Contractor

CONTRACT NUMBER As indicated on the contract

CONDITION CODE CONDITION A

QUANTITY & UNIT OF ISSUE 1- EA

COAST GUARD ELC MATERIAL

REUSABLE CONTAINER DO NOT DESTROY

b TYPE 2 – PROPELLER, RIGHT HAND (RH)

STOCK NUMBER 2010-01-F07-1222

ITEM NAME PROPELLER, RH

PART NUMBER 175-WLM-245-002RH

SERIAL NUMBER As provided by Contracting Officer

SHIPPING WEIGHT As determined by Contractor CONTRACT NUMBER As indicated on the contract

CONDITION CODE CONDITION A

QUANTITY & UNIT OF ISSUE 1- EA

COAST GUARD ELC MATERIAL

REUSABLE CONTAINER DO NOT DESTROY

5.4. BAR CODING - Bar code labels shall be supplied on all CLIN's except for those that require data submissions only.

5.4.1. All bar coded labels shall be in accordance with ELC specification D-000-0100 REV G, dated 02/06.

a The actual labels shall be Type "V", Grade "A", Style "2", Composition "b" with plastic laminate.

b Each label shall contain encoded data for the Stock Number.

6.0 NOTES

6.1. GOVERNMENT & COMMERCIAL DOCUMENT SOURCES

6.1.1. GOVERNMENT DOCUMENTS

a. DOD & Navy Publications & Forms (Other Than DODSSP) Naval Publication and Forms Center

5801 Tabor Ave.

Philadelphia PA. 19120

215-697-2000

b. Department of Defense Single Stock Point (DODSSP)

Building 4, Section D

700 Robbins Avenue

Philadelphia, PA 19111-5094

215-697-2667/2179 FAX 215-697-1462

6.1.2. COMMERCIAL DOCUMENTS

a American Bureau of Shipping (ABS) ABS Plaza 16855 Northchase Drive Houston, TX 77060

PH 281-877-6000

FAX 281-877-6001

b Society of Automotive Engineers, Inc. (SAE) 400 Commonwealth Drive Warrendale, PA 15096

PH 412-776-4841

FAX 412-776-5760

E-MAIL www.sae.org c American Society For Quality Control (ASQC) 611 East Wisconsin Avenue Milwaukee, Wisconsin 53202

PH 414-272-8575

FAX 414-272-1734

d American National Standards Institute (ANSI) 25 West 42nd Street New York, NY 10018

PH 212-642-4900

FAX 212-398-0023

6.1.3. OTHER GOVERNMENT DOCUMENTS

a USCG Engineering Logistics Center MAIL STOP #026 BLDG 31 2nd FL.

2401 Hawkins Point Road Baltimore, MD. 21226-5000 410-762-6503 Attn: Code 046