ACCEPTANCE TEST PROCEDURE.pdf

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This document is an Acceptance Test Procedure (ATP) that defines the tests and inspections used to verify conformance to critical performance and conformance characteristics of the Advanced Technology Anti-G, Trousers, Pneumatic. It covers the requirements for Qualification, First Article, and Production acceptance testing for two versions of the Anti-G Trousers: the Basic ATAGS Type CSU-22/P and the F-22 ATAGS Type CSU-23/P.

The ATP outlines the plan and performance objectives for testing at every stage, including in-process inspections, qualification and first article testing, and production conformance testing. It specifies the required sample sizes, test sequence, acceptance criteria, and basis for rejection. Key tests include operating pressure, proof pressure, inflation time, cycle test, leakage test, and endurance test. The document also provides details on the test conditions, equipment, and calibration requirements, as well as procedures for addressing nonconformances and corrective actions.

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ACCEPTANCE TEST PROCEDURE

FOR

ANTI-G, TROUSERS, PNEUMATIC

BASIC ATAGS TYPE CSU-22/P &

F22 ATAGS TYPE CSU-23/P

AUTHENTICATED BY: AP PROVED BY :

MUSTANG SURVIVAL

3810 JACOMBS ROAD

RICHMOND BC V6VV 1Y6

(608) 270 8631

AFLCMC/WNUS

(HUMAN SYSTEMS DIVISION)

460 RICHARD RAY BLVD

ROBINS AFB GA 31098

(478) 472-7417

DATE: 17 August 2001

DATE: 24 MAY 2016

SPECIFICATION NUMBER

MSF880/5-ATP-GEN-0 REV B

CURRENT DESIGN ACTIVITY CODE 98752

US AIR FORCE

ROBINS, AFB GA 31098

Distribution Statement D. Authorized to the Department of Defense and DOD contractor only; critical technology;

8 May 2013. Other requests shall be referred to Human System Division, Robins AFB, GA 31098.

WARNING- This document contains technical data whose export is restricted by the Arms Export Control Act (title 22, U.S.C., Sec 2751, et seq.) or the Export Administration Act of 1979 (Title 50, U.S.C., App 2401 et seq.), as amended. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.

DESTRUCTION NOTICE: Destroy by any method that will prevent disclosure of contents or reconstruction of the document.

REVISION HISTORY.

REV B - REVISED PER ECO 2010C0001, 2016A0002-R AND 2016A0003-R 24 MAY 2016 Approved. JD/DW

ACCEPTANCE TEST PROCEDURE SPECIFICATION NUMBER

MSF880/5-ATP-GEN-0

Mustang Survival Corp. Table of Contents 3810 Jacombs Road, Richmond, BC, Canada V6V 1Y6

TABLE OF CONTENTS

1. OBJECTIVE

2. SCOPE

3. APPLICABLE DOCUMENTS

4. RESPONSIBILITY

5. CLASSIFICATION OF TEST

6. QUALIFICATION AND FIRST ARTICLE TESTING

6.1. Qualification and First Article Samples

6.2. Master List –Qualification and First Article Tests

6.3. Qualification/ First Article Test Grouping and Sequencing

6.4. Test Report

7. PRODUCTION

7.1. Lot Formation and Sampling Plan for Production Quantities

7.2. Master List –Production Test and Inspection

7.3. Production Test Sequence

7.4. Acceptance Test Report

8. TEST CONDITIONS AND EQUIPMENT

8.1. Test Conditions

8.2. Critical Equipment List

8.3. Equipment Calibration Requirements

9. TEST DESCRIPTION

9.1. In-Process Inspection

9.2. Qualification / First Article or Quality Conformance Test

10. NONCONFORMANCE

10.1. Classification of Defects

10.2. Basis for Rejection

10.3. Rejection and Retest

10.4. Continuation of Test

10.5. Corrective Action / Failure Analysis

APPENDIX A: ATP APPENDICIES 001 Through 006

APPENDIX 001-1: CLASSIFICATION OF DEFECTS

APPENDIX 002-1: QUALIFICATION OR FIRST ARTICLE TEST SEQUENCE

APPENDIX 003-1: PRODUCTION TEST SEQUENCE

APPENDIX 004-1: SUIT FITTING INSTRUCTIONS

APPENDIX 005-1: ANTI G TEST APPARATUS

Ph. (604) 270-8631, Fax. (604) 273-6466

REV B

Mustang Survival Corp. Table of Contents 3810 Jacombs Road, Richmond, BC, Canada V6V 1Y6

APPENDIX 006-1: INANIMATE TEST MODELS

APPENDIX B: ACCEPTANCE TEST INSTRUCTIONS T1.01 THROUGH T1.21

ATP/ATAGS/TI.01-1: IN-PROCESS – SEWING VISUAL INSPECTION

ATP/ATAGS/TI.02-1: BLADDER PANEL VISUAL INSPECTION

ATAGS/ATP/TI.03-1: PEEL TEST

ATP/ATAGS/TI.04a-1: SEAM ADHESION TEST

ATP/ATAGS/TI.04b-1: BLADDER SEAM BOND STRENGTH

ATP/ATAGS/TI.04c-1: ADHESION OF COATING

ATP/ATAGS/TI.05-1: BLADDER VISUAL INSPECTION

ATP/ATAGS/TI.06-1: BLADDER LEAKAGE TEST

ATP/ATAGS/TI.07-1: OPERATING PRESSURE TEST

ATP/ATAGS/TI.08-1: PROOF PRESSURE

ATP/ATAGS/TI.09-1: INFLATION TIME

ATP/ATAGS/TI.10-1: CYCLE TEST

ATP/ATAGS/TI.11-1: LEAKAGE TEST

ATP/ATAGS/TI.12-1: LOW PRESSURE LEAKAGE

ATP/ATAGS/TI.13-1: SECONDARY RESTRAINT STRENGTH

ATP/ATAGS/TI.14-1: ENDURANCE TEST

ATP/ATAGS/TI.15-1: HOSE/BLADDER STRENGTH

ATP/ATAGS/TI.16-1: DIMENSIONAL INSPECTION

ATP/ATAGS/TI.17-1: PRODUCT EXAMINATION

ATP/ATAGS/TI.18-1: LOW TEMPERATURE OPERATION

ATP/ATAGS/TI.19-1: LOW TEMPERATURE STORAGE

ATP/ATAGS/TI.20-1: HIGH TEMPERATURE STORAGE

ATP/ATAGS/TI.21-1: BLADDER DIMENSIONAL INSPECTION

Ph. (604) 270-8631, Fax. (604) 273-6466

1. OBJECTIVE

The Acceptance Test Procedure (ATP) defines the tests and inspections used to verify conformance to critical performance and conformance characteristics of the Advanced Technology Anti-G, Trousers, Pneumatic. This Acceptance Test Procedure will also serve as a managerial control document / reference for test preparation, execution, and reporting of test results. It outlines the plan and performance objectives at every level of product testing and inspection.

2. SCOPE

The Advanced Technology Anti-G, Trousers, Pneumatic consist of two versions:

�� Anti-G Trousers, Pneumatic, Basic ATAGS Type CSU-22/P

�� Anti-G Trousers, Pneumatic, F-22 ATAGS Type CSU-23/P

This ATP covers the requirements for Qualification, First article and Production acceptance testing for the above-mentioned product versions.

3. APPLICABLE DOCUMENTS

�� Product Function Specification for ATAGS: 40470G-01KX-0, Latest Revision

�� Critical Items Development List for ATAGS: HSWATAGS-001, Latest Revision

�� Test Program Set (TPS) and Operational Test Program Set (OTPS) Acceptance Test Procedures (ATP): In accordance with Contractual Contract Data Requirements List

(CDRL)

�� Test Program Set (TPS) Acceptance Test Report (ATR):

�� ATAGS Drawing Package: Anti-G Trousers, Pneumatic Type CSU-22/P & CSU-23/P ATAGS drawing package including patterns is referenced through: 260000 Drawing Organization Chart Anti-G Trousers Pneumatic, Type CSU-22/P & CSU-23/P

Note:

In this document, Anti-G or Basic Anti-G trousers will be referred to as the “trousers” or “suit” hereafter.

4. RESPONSIBILITY

Unless otherwise specified in the contract or purchase order, it is the responsibility of the contractor to conform to all inspection and test requirements specified herein. Tests and inspections are to be conducted at the contractor’s premise, however other facilities suitable for the performance of test requirements may by used unless disapproved by the contracting agency.

All trousers shall pass the acceptance test requirements specified herein, either as a lot or as an individual item. All acceptance tests set forth in this acceptance test procedure and other contractor’s chosen in-process inspections shall become part of the contractor’s overall inspection system or quality program.

5. CLASSIFICATION OF TEST

The Acceptance Test Procedure details the requirements and acceptance criteria for:

�� Qualification Test �� First Article Test

Page 1of 67 �� Production Conformance Testing

6. QUALIFICATION AND FIRST ARTICLE TESTING

6.1. Qualification and First Article Samples

Qualification samples shall be submitted for approval to the procuring agency. Approved qualification samples is a requirement for approval as a qualified ATAGS manufacturer.

Approval of the qualification samples does not preclude the requirements for performing first article testing.

As specified by the procuring agency, First Article samples shall be submitted for approval prior to the start of manufacture of production quantities. All samples shall be representative of the materials, the components, the construction and the workmanship that would be intended for use in production items. The first article testing may be waived by the procuring agency upon successful application.

6.1.1. Tested Samples - Three trousers and one complete bladder assembly for each of Qualification and First Article Testing

The contractor shall perform testing on three trousers in accordance with section

6.2. The sizes of the trousers shall be size 2, size 5, and size 8 unless otherwise specified in the purchase order or contract agreement. The specific test sequence and grouping of tests are described in Appendix 002-1.

Endurance test shall be conducted on the Size 8 suit or the largest size suit specified by the procuring agency.

The contractor shall perform Bladder Seam Bond Strength testing on one complete bladder in accordance with Test Instruction ATP/ATAGS/TI.04b-1.

6.1.2. Untested Samples – One complete trouser and two complete bladders for each of Qualification and First Article Testing

Two complete bladder assemblies shall be provided to the procuring agency for examination, testing, and approval of the seam bonding and material conformance. Unless otherwise specified in the purchase order one bladder assembly without limiters (Size two) and one bladder assembly with limiters (Size

8) shall be submitted. Production individual testing shall be done on all untested samples

Any trousers used in the verification of requirements through destructive testing shall not be shipped against the contact quantities. Upon test completion, these trousers shall be marked across the abdomen of the trousers in letters that are at least one inch in height, with the following information: “SUBJECTED TO DESTRUCTIVE TESTING – NOT TO BE USED IN FLIGHT”. If the contractor is requested to ship suits that have undergone destructive testing, the shipping container shall be marked with the same information.

6.2. Master List –Qualification and First Article Tests

The qualification and first article testing for the trousers shall consist of the following In- Process and Qualification/First Article tests. Refer to section 9 for details of tests and inspections.

TEST CATEGORY TEST NAME Test Instruction No.

In Process Inspection – Sewing

ATP/ATAGS/TI.01-1

Bladder Panel Visual Inspection

ATP/ATAGS/TI.02-1

Peel Test ** ATP/ATAGS/TI.03-1

Seam Adhesion Test ** ATP/ATAGS/TI.04a-1

Bladder Visual Inspection ATP/ATAGS/TI.05-1

Bladder Dimensional Inspection

ATP/ATAGS/TI.21-1

Bladder Leakage Test ATP/ATAGS/TI.06-1

In-Process

Low Pressure Leakage Test ATP/ATAGS/TI.12-1

Operating Pressure Test ATP/ATAGS/TI.07-1

Cycle Test ATP/ATAGS/TI.10-1

Leakage Test ATP/ATAGS/TI.11-1

Dimensional Inspection ATP/ATAGS/TI.16-1

Product Examination ATP/ATAGS/TI.17-1

Endurance Test ATP/ATAGS/TI.14-1

Secondary Restraint Strength ATP/ATAGS/TI.13-1

Inflation Time ATP/ATAGS/TI.09-1

Proof Pressure Test ATP/ATAGS/TI.08-1

Low Temperature Operation ATP/ATAGS/TI.18-1

Low Temperature Storage ATP/ATAGS/TI.19-1

Hose / Bladder Strength ATP/ATAGS/TI.15-1

High Temperature Storage ATP/ATAGS/TI.20-1

Qualification and First Article

Bladder Seam Bond Strength ATP/ATAGS/TI.04b-1

** Note: Refer to section 7.1.3 for frequency of test

6.3. Qualification/ First Article Test Grouping and Sequencing

Qualification/First Article tests and inspections are grouped and sequenced to ensure that three samples are sufficient for completing all the tests and inspections. The endurance test shall be conducted on the largest ATAGS trouser (Size 8). Besides the in-process inspections and the qualification/first article testing specified in Appendix 002-1, no other qualification or first article testing shall be performed on this suit. Qualification and First Article tests and inspections shall be grouped and performed in the sequence described in Appendix 002-1.

6.4. Test Report

The contractor shall summarize the tests and inspections performed as a part of the Qualification and/or First Article Testing. One copy of the test report shall be submitted to the procuring agency. This report shall include the results of each test or inspection and shall accompany the samples specified in section 7.1. The contractor shall include records of non-conformance and corrective action generated during the production of the qualification samples. The format of the report is at the discretion of the contractor, however the main content shall be in accordance with contractual contract data requirements list (CDRL).

7. PRODUCTION

7.1. Lot Formation and Sampling Plan for Production Quantities

7.1.1. Lot Formation: Production Quantities

The maximum lot size for the ATAGS trouser shall be 250 units. This lot may be comprised of a combination of CSU-22/P and CSU-23/P versions. The lot shall be manufactured essentially under the same conditions and submitted for inspection at substantially the same time. A fraction of a lot shall not be permitted for Sampling A test purposes unless the total quantity of the trousers required to be delivered during the specified period under contract is less than 250 units.

7.1.2. Sampling A Tests: Operating Pressure, Inflation Time, Endurance

One complete trouser is to be subjected to the above-mentioned tests prior to the start of the first production lot. This trouser is in addition to the quantity deliverable under the contract. This sample test may be omitted if first article testing is required.

Two complete trousers per lot of 250 units are to be selected and subjected to the above-mentioned tests. One trouser shall be randomly selected from the first 125 units and a second trouser randomly selected from the second 125 units within the lot. The two trousers used for this destructive testing are in addition to the quantity deliverable under the contract.

Note: Any trousers used in the verification of requirements through destructive testing shall not be shipped against the contact quantities. Upon test completion, these trousers shall be marked across the abdomen of the trousers in letters that are at least one inch in height, with the following information: “SUBJECTED TO DESTRUCTIVE TESTING – NOT TO BE USED IN FLIGHT”. If the contractor is requested to ship suits that have undergone destructive testing, the shipping container shall be marked with the same information.

7.1.3. Sampling B Tests: Seam Adhesion Test, Peel Test

The frequency of Sampling B tests are determined by the number of weld setups that occur during the production of the contract quantities. Sampling is performed at the beginning and end of each welding process in order to provide assurance of the consistency of the process and thus the conformance of the welds created during the process.

7.1.4. Sampling C Tests: Bladder Dimensional Inspection

The frequency of Sampling C tests is to be done once per size of CSU-22/P and once per size of CSU-23/P. If there is no change in size or style per lot, a sampling will be performed every 50 suits.

7.2. Master List –Production Test and Inspection

The following tests and inspections are performed as verification that the individual trousers and lot of trousers conforms to the critical requirements during the production stage. Refer to section 9 for details of tests and inspections.

Acceptance tests during the production stage are to be conducted either as an individual test or as a sampling test. Individual tests are conducted on each trouser while sampling tests are conducted at chosen intervals within the production process.

TEST CATEGORY TEST NAME Test Instruction No. Test Type In Process Inspection – Sewing

ATP/ATAGS/TI.01-1 Individual

Bladder Panel Visual Inspection

ATP/ATAGS/TI.02-1 Individual

Peel Test ATP/ATAGS/TI.03-1 Sampling B

Seam Adhesion Test ATP/ATAGS/TI.04a-1 Sampling B

Bladder Visual Inspection ATP/ATAGS/TI.05-1 Individual

Bladder Dimensional Inspection

ATP/ATAGS/TI.21-1 Sampling C

Bladder Leakage Test ATP/ATAGS/TI.06-1 Individual

In-Process

Low Pressure Leakage Test ATP/ATAGS/TI.12-1 Individual

Operating Pressure Test ATP/ATAGS/TI.07-1 Sampling A

Leakage Test ATP/ATAGS/TI.11-1 Individual

Dimensional Inspection ATP/ATAGS/TI.16-1 Individual

Product Examination ATP/ATAGS/TI.17-1 Individual

Inflation Time ATP/ATAGS/TI.09-1 Sampling A

Quality Conformance

Endurance Test ATP/ATAGS/TI.14-1 Sampling A

7.3. Production Test Sequence

Production tests and inspections have been sequenced to optimize test effectiveness as well as production throughput. The contractor may only deviate from the prescribed sequence for lot conformance testing with approval from the contracting agency. The production test sequence is described in Appendix 003-1.

7.4. Acceptance Test Report

An Acceptance Test Report shall be prepared for each contract that summarizes the test results for each lot. This report shall be supplied to the procuring agency at the completion of the contract. The contractor shall include records of non-conformance and corrective action generated during the production of the trousers. The format of the report is at the discretion of the contractor, however the minimum content shall be in accordance with Contractual Contract Data Requirements List (CDRL).

The contractor shall retain all acceptance test reports and data for a minimum period of six years after completion of the contract.

8. TEST CONDITIONS AND EQUIPMENT

8.1. Test Conditions

The atmospheric conditions during test shall be:

�� Temperature: 77 ºF +/- 10º

�� Humidity 80% or Less

The contractor shall employ good housekeeping and handling techniques to preserve the quality and integrity of the trousers at all stages of the production process. Welding areas must be kept free of dust and lint to limit the threat of contamination.

8.2. Critical Equipment List

It is the responsibility of the contractor to develop the needed tools and equipment to meet the performance specifications provided.

��Anti G-Testing Equipment or System (Refer to Appendix 005-1)

��Inanimate Models (Refer to Appendix 006-1)

8.3. Equipment Calibration Requirements

Testing equipment or tools shall be calibrated in accordance with industry standards and shall be controlled as a component of the contractors quality system. Any calibration records associated with the critical tools listed in section 8.2 shall be available for review by the procuring agency.

9. TEST DESCRIPTION

9.1. In-Process Inspection

9.1.1. Sewing Visual Inspection

Refer to Acceptance Test Instructions: ATP/ATAGS/TI.01-1

The sewing sub-assemblies shall be visually inspected for dimensional measurements, and sewing assembly requirements. Guidelines have been provided for the performance of in-process visual inspection. The specific content of these inspections and the inspection points may vary depending on the contractor’s production process. Regardless of the guidelines provided, the contractor is responsible to ensure that the suits comply with all specifications and requirements detailed in the product drawings.

9.1.2. Bladder Panel Visual Inspection

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 02-1

Cut bladder panels shall be visually inspected for any defects prior to being welded. Any coating defects shall be identified, separated and recorded. All bladder panels with imperfections shall be rejected. Guidelines have been provided for the performance of in-process visual inspection. The specific content of these inspections and the inspection points may vary depending on the contractor’s production process.

9.1.3. Peel Test

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 03-1

The peel test provides a preliminary indication of the adequacy of the welding process to ensure the weld is of consistent strength through the length of the weld. The peel test is performed on a sample of the bladder material.

9.1.4. Seam Adhesion Test

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 04a-1

For each die setup, the weld bond seam adhesion will be tested using a sample of the bladder material. The seam adhesion value for any sample in warp or fill shall be a minimum of 24 lb/in.

9.1.5. Bladder Visual Inspection

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 05-1

Each finished bladder is to be visually inspected for major and minor defects prior to being sewn into the garment. The bladder shall have no major defects and a maximum of two minor defects. Regardless of the guidelines provided, the contractor is responsible to ensure that the bladders comply with all specifications and requirements detailed in the product drawings.

9.1.6. Bladder Dimensional Inspection

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 21-1

The finished bladder is to be dimensionally inspected in accordance with the product drawings prior to being sewn into the garment.

9.1.7. Bladder Leakage Test

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 06-1

The bladder shall withstand a pressure of 8 psig for 60 seconds with no seam distortion and less than or equal to 0.5 psig leakage. The bladder shall be restrained in a 3” diameter tube during this test.

9.1.8. Low Pressure Leakage Test

Refer to Acceptance Test Instruction: ATP/ATAGS/TI.12-1

The trouser shall withstand an inflation pressure of 2.5 psig for 60 seconds in an unrestrained condition (Not fitted to a mannequin) with a pressure loss of no more than 0.5 psi.

9.2. Qualification / First Article or Quality Conformance Test

9.2.1. Performance Related Tests

9.2.1.1. Operating Pressure

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 07-1

The donned suit shall withstand a step function pressure input of 12 pounds per square inch (PSIG) for 15 seconds without damaging normal operating seams or permanently stretching material.

9.2.1.2. Proof Pressure Test

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 08-1

The donned suit shall withstand pressures of 13.7 psig for 15 seconds without damaging normal operating seams or permanently stretching material.

9.2.1.3. Inflation Time

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 09-1

The trouser shall inflate to a pressure of 8.0 psig in not more than 3 seconds with a free airflow of 10 cubic feet per minute and a backpressure of 12.0 psig from the pressure source.

9.2.1.4. Cycle Test

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 10-1

The trouser shall withstand 25 inflation/deflation cycles of 11 psig without resulting in any structural failure or leakage. Following completion of this test, a Leakage test (Refer to 9.2.1.5) shall be conducted to verify compliance.

9.2.1.5. Leakage Test

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 11-1

Leakage pressure loss, with the item inflated to 11.0 psig, shall be less than or equal to 0.5 psi in 1 minute.

9.2.1.6. Secondary Restraint Strength

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 13-1

With one of the leg zippers open, the secondary restraint and the restraint layer shall withstand for at least 15 seconds a suit pressure of 12 psig or the pressure that the bladder fails whichever is lower.

9.2.1.7. Endurance Test

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 14-1

The suit shall be structurally intact after being inflated 6000 times to 11 psig. The suit shall not exhibit any structural defects to include rips or torn material, or seam separation. After completion of the endurance test, the leakage pressure loss, with the item inflated to 10.0 psig, shall be less than or equal to 2 psig in 1 minute. No parts may be replaced as preventive maintenance during the endurance testing.

9.2.2. Physical / Configuration Tests

9.2.2.1. Hose Bladder Strength

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 15-1

The suit shall withstand a pull force in any direction of 30 pounds applied at the end of the suit hose connector for a period of not less than 5 seconds without tearing or separating. Following exposure to this force, the suit shall meet all the performance requirements.

9.2.2.2. Dimensional Inspection

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 16-1

Critical dimensions of the trouser are verified against the measurements specified on the product drawing.

9.2.2.3. Product Examination

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 17-1

A final product examination is conducted to ensure that the finished trousers are manufactured in accordance with the specification and contain no major defects and a maximum of five minor defects.

9.2.2.4. Low Temperature Operation

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 18-1

The trouser shall be subjected to a temperature of minus 30 degrees Fahrenheit, or lower, for a period of 4 hours. During the 4-hour period, the suit shall be inflated at the rate of 10 times per hour to a pressure of not less than 6.0 psig.

Upon completion of this test, the trouser shall be examined for failure or defects in materials or workmanship. Structural or any other defects shall be cause for rejection of the garment.

9.2.2.5. Low Temperature Storage

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 19-1

The suit shall meet the performance requirements before and after exposure to storage temperatures below - 60º F for 8 hours.

9.2.2.6. High Temperature Storage

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 20-1

The suit shall meet the performance requirements before and after exposure to storage temperatures above +160º F for 8 hours.

9.2.2.7. Bladder Seam Bond Strength

Refer to Acceptance Test Instruction: ATP/ATAGS/TI. 04-2

The seam adhesion value for any sample cut from a finished bladder perpendicular to the weld in warp or fill shall be a minimum of 24 lb/in.

10. NONCONFORMANCE

10.1. Classification of Defects

Refer to Appendix 001-1: Classification of Defects Table

10.1.1 Major Defects:

No major defects are allowable.

10.1.2 Minor Defects:

A maximum of two minor defects is allowable on the bladder assembly. A maximum of three minor defects is allowable on the shell assembly. A total of five minor defects are therefore allowable on the finished trouser. Since minor defects are not cumulative, the individual maximum for the bladder or shell assembly shall not be exceeded.

10.2. Basis for Rejection

10.2.1. Individual Test Rejection

When any trouser fails to meet the acceptance criteria during individual test, the trouser shall be rejected.

10.2.2. Sampling Test Rejection

When any trouser fails to meet the acceptance criteria during a sampling (lot) test, the individual trouser shall be rejected and the acceptance of the entire production lot shall be withheld until the extent and cause of failure have been determined and communicated to the procuring agency.

10.3. Rejection and Retest

10.3.1. Trouser Repairs

Defects found during in-process and conformance testing can be reworked to meet the original specification as long as the repair method is feasible and does not cause additional damage to the suit. The result of this rework shall not degrade the performance or physical appearance of the trousers. Rework of load-bearing seams or stitching defects can only be completed a maximum of twice per location, including during in-process manufacturing, to minimize material degradation. Load-bearing stitching includes, but is not limited to, main suit panel seams, bladder installation stitching, knee darts, all zippers excluding calf pocket zippers, knife pocket installation, lacing installation, secondary restrain buckle installation, and reinforcement installation. All rework shall be recorded under the contractor's nonconformance and corrective action system (Section 11.5). After rework, any previously completed tests deemed as affected by these changes shall be repeated. If rework cannot be completed without damage to the suit, or if the maximum number of allowable reworks would be exceeded, the suit shall be discarded and not sold as part of that or any lot to the US Government.

10.4. Continuation of Test

10.4.1. Test Failures

For production reasons, individual tests or sampling test may be continued pending the investigation of a failure to meet the acceptance criteria. In the case of failures during sampling test (other than endurance), corrective actions can include individual testing of all units within the lot as deemed necessary by the contractor in consultation with the procuring agency. Final acceptance of the entire lot(s) shall not be made until it is deemed that the lot(s) meet all acceptance criteria.

10.4.2. Notification of Test Failure

The procuring agency shall be notified within 24 hours of the failure or end of next business day after 10 or more suits have failed individual testing. In the case of Lot Sampling Failure, the procuring agency shall be notified within 24 hours of the failure or end of next business day. The procuring agency, quality assurance representative or government technical authority has the right to stop production after notification of 10 individual testing failures or lot sampling failure.

10.5. Corrective Action / Failure Analysis

10.5.1. Contractor Nonconformance System

The contractor shall utilize their internal nonconformance and corrective action system to record nonconformances that occur during qualification testing, first article inspection, and the production stages of the acceptance testing. These records shall be made available for viewing by the procuring activity or the designated Quality Assurance Representative.

10.5.2. Failure Analysis Report

Should the procuring agency be notified of a lot sampling failure, or 10 or more individual testing failures, a failure analysis report shall be submitted in accordance with Contractual Contract Data Requirements List (CDRL).

10.5.3. Deviation of Waiver

If a request for deviation or waiver is required to request performance, functionality or design changes, the contractor shall follow the requirements of MIL-STD-193, Appendix E. This request shall be coordinated with the designated Quality Assurance Representative and/or the procurement agency.

Any trouser that has experienced more that 110 inflation test cycles at 11 psi or above shall be deemed as having undergone destructive test. This trouser is not acceptable for shipment against the quantities of serviceable finished end items required by contract unless approved by the procuring agency.

10.3.2. Maximum Number of Inflation Test Cycles

APPENDIX A: ATP APPENDICIES 001 Through 006

APPENDIX 001-1: CLASSIFICATION OF DEFECTS

Table A: General

DEFECTS MAJOR MINOR

POCKETS

�� Any pocket out of horizontal or vertical alignment more that 3/8 inch but less than ½ inch X

�� Any pocket out of horizontal or vertical alignment by more than ½ inch X

�� Missing or misplaced X

MATERIALS

�� Materials not conforming to specified product drawing requirements (ATAGS Drawing Package 260000) X

�� For metallic components, any surface defects such as roughness, corrosion, nick, burr, sharp edge, scale, crack, dent, or pit X

�� Inherent material contamination or embedded foreign matter on material surface that will affect functionality, serviceability and general appearance of the product

X

FABRIC IMPERFECTIONS

�� Refer to FED-STD-4 (Note: all fabric imperfections that would affect the appearance or the function of the suit shall be considered major defects)

FED

STD 4

FED

STD 4

HOSE CONNECTORS

�� Hose clamp not securely crimped or fastened, loose connector X

SLIDE FASTENERS

�� Fabric tape catching in the slider, slider not operating freely. X

�� Type, style, or length not as specified X

�� Any part omitted, bent or broken X

�� Pull tabs missing; not of the type specified X

COLOR

�� Color Shall Conform To FED-STD-595 (Standard Classifies major / minor defects)

FED

STD

FED

STD

DEFECTS MAJOR MINOR

SNAP FASTENERS

�� Insecurely clinched stud, damaged spring, damaged/missing snap fastener, cracking of snap rivet X

�� Stud not aligned with socket causing noticeable bulge or twist when snapped.

X

�� Stud mismatch with socket X

�� Snap fasteners not separating under normal pull (Engage and disengage three times

X

�� snap rivet studs not fully rolled over X

FASTENER TAPE (Velcro) �� Fastener tape does not conform to requirements specified in

Product Drawing Specification (Not specified type, style, or size) X

�� 10 to 25 % of hooks flattened or missing from the tape X

�� 25 % of hooks or more flattened or missing from tape X

�� When the tape is engaged, excessive wrinkles exist. (Wrinkles affect the taping strength)

X

ASSEMBLY

�� Incorrectly assembled (Reversed seams, seam type not as specified, stitch type not as specified, misplaced or reversed components)

X

�� Incompletely assembled (Missing component, required operation was missed)

X

IDENTIFICATION OF PRODUCT

�� Any label that is missing, illegible, or contains incorrect or incomplete information X

�� Improper location of the label:

a. Affecting functionality or other construction lines

b. Affecting only physical appearance

X

X

WORKMANSHIP

�� Holes, cuts, tears, or needle chews X

�� Darns or mends that affect serviceability X

�� Darns or mends that affect appearance X

�� Stains, oil spots, or dirt over ¼ inch in diameter X

�� Stains, oil spots, or dirt, up to ¼ inch in diameter X

�� Thread ends not trimmed to a maximum of ¼” X

DEFECTS MAJOR MINOR

MEASUREMENTS

Any finished measurements not in accordance with drawing specifications. Refer to Table B of this chart for classification of tolerance defects unless noted otherwise in the drawings. (ATAGS Drawing Package 260000)

Table B Table B

STITCHES AND SEAMS

�� Open seams X

�� Stitching missing, broken, skipped or cut X

�� Run-offs X

�� End of stitching not caught in other seams or not securely backstitched for more than ½ inch

X

�� Stitching margins outside of the tolerances stated on the drawing.

Minor/Major assignment is done in reference to Table B of this chart.

Table B Table B

�� Number of stitches per inch:

a. More or less than specified: one stitch

b. More or less than specified: two or more stitches X

X

BLADDER SUBASSEMBLY

�� Burns that extend into the weld line seam greater than 1/32” X

�� Burns that extend into the weld line seam less than 1/32” X

�� Burns on the air holding edge (inside edge) of the weld line seam X

�� Missing sewing tab X

�� Missing Polyurethane tab X

�� Tunnel leaks in t-joint welds (Intersection of two or more panels) X

�� Pinholes in bladder fabric X �� Missing components (ABDOMEN LIMITER; BLADDER SPACER; HOSE

SPACER; REINFORCEMENT TAPE, HIP; REINFORCEMENT TAPE, GROIN;

LIMITERS, SUBASSEMBLY)

X

�� Outside of the tolerances or specifications or requirements detailed in the product drawings

X

�� Non-continuous weld seam behind hip or groin reinforcement tape X

�� Foreign object within the bladder X

�� Weaving inconsistencies or defects X

�� Foreign objects imbedded in the coating of the bladder fabric X

�� Surface contamination on coated side of bladder fabric X

Table B: CLASSIFICATION OF DIMENSIONAL TOLERANCE DEFECTS

2/ Defect classification measurements are to be read as "up to" the specified measurement. Any margin deviations exceeding 0.375 inches are major defects.

Figure 002-1 : QUALIFICATION OR FIRST ARTICLE TEST SEQUENCE

QUALIFICATION AND FIRST ARTICLE INSPECTIONINDIVIDUAL TESTINGSEWING& WELDING

IN-PROCESS SEWING VISUAL

INSPECTION:

ATP/ATAGS/TI.01-01

IN PROCESS INSPECTION AND TESTING

(WELDING):

Bladder Panel Visual Inspection:

ATP/ATAGS/TI.02-1

Peel Test: ATP/ATAGS/TI.03-1 Seam Adhesion Test: ATP/ATAGS/TI.04a-1 Bladder Visual Inspection: ATP/ATAGS/TI.05-1 Bladder Dimensional Inspection: ATP/ATAGS/

TI.21-1

Bladder Leakage Test: ATP/ATAGS/TI.06-1

Note: 1. UNLESS OTHERWISE NOTIFIED, ARROWS DEFINE THE SEQUENCE FOR TESTING

2. SHADED BOXES INDICATE INDIVIDUAL TEST, NON-SHADED BOXES INDICATE SAMPLING TEST (Except on Peel Test and Seam Adhesion Test which are Sampling )

ACCEPTANCE TEST PLAN

Endurance

Product Examination

Low Temperature Operation

Low Temperature Storage

High Temperature Storage

Product Examination

Leakage Test

SAMPLE 1: Size 8

SAMPLE 2: Size 5

SAMPLE 3 : Size 2

Low Pressure Leakage Test Operating Pressure Test

Cycle Test Leakage Test

Dimensional Inspection Product Examination

Secondary Restraint Strength

Product Examination

Product Examination

Hose/Bladder Strength

Proof Pressure Test

Inflation Time

Leakage Test

SAMPLE 4 : Bladder Bladder Seam Bond Strength

Proof Pressure Test

Product Examination

Secondary Restraint Strength

Inflation Time

APPENDIX 002-1: QUALIFICATION OR FIRST ARTICLE TEST SEQUENCE

IN PROCESS INSPECTION AND TESTING

(WELDING):

Bladder Panel Visual Inspection:

ATP/ATAGS/TI.02-1

Peel Test: ATP/ATAGS/TI.03-1 Seam Adhesion Test: ATP/ATAGS/TI.04a-1 Bladder Visual Inspection: ATP/ATAGS/TI.05-1 Bladder Dimensional Inspection: ATP/ATAGS/

TI.21-1

Bladder Leakage Test: ATP/ATAGS/TI.06-1

Figure 003-1 : ACCEPTANCE TEST SEQUENCE (PRODUCTION - ATAGS)

ASSEMBLY & TRIMMING LOT CONFORMANCESEWING& WELDING

Low Pressure Leakage Test: ATP/

ATAGS/TI.12-1

IN-PROCESS SEWING VISUAL

INSPECTION:

ATP/ATAGS/TI.01-01

Leakage Test

Product Examination

Dimensional Check

Inflation Time Test

Operating Pressure Test

Endurance Test

Notes

1. UNLESS OTHERWISE NOTIFIED, ARROWS DEFINE THE SEQUENCE FOR TESTING

2. SHADED BOXES INDICATE INDIVIDUAL TEST, NON-SHADED BOXES INDICATE SAMPLING TEST (Except Peel Test, Seam Adhesion Test and Bladder Dimensional Inspection. which are sampling )

ACCEPTANCE TEST PLAN

Product Examination

APPENDIX 003-1: PRODUCTION TEST SEQUENCE

APPENDIX 004-1: SUIT FITTING INSTRUCTIONS

Fitting of ATAGS trousers on the inanimate models shall be accomplished as follows:

Step 1:

The comfort zippers, secondary restraint devices, waist and leg slide fasteners shall be opened. The adjustment laces shall be adequately extended.

Step 2:

Trousers shall then be fitted onto the inanimate test model: See Appendix 006-1, the test model shall be a suitable representative of the size and seated orientation of the pilot for which the suit is designed.

Step 3:

The adjustment laces of the ATAGS trousers shall then be taken up and tied so that the trousers will fit snugly, but not tightly, around the abdomen, thighs and calves.

Step 4:

All slide and snap fasteners on the suit shall be in the fully closed position or fastened.

Unless otherwise indicated, this shall include: the leg fasteners, the waist fastener, the comfort fasteners, secondary restraints and other related snap fasteners.

Note: The secondary restraint strength test requires that one of the leg slide fasteners be open during the test.

APPENDIX 005-1: ANTI G TEST APPARATUS

The Anti G Test Apparatus shall be any apparatus that will provide air to inflate, hold and deflate the trouser as specified in the various performance tests (Such as: leakage testing, endurance testing, inflation testing, etc.). The apparatus shall be capable of delivering air to the suit at a free stream flow rate of 10 cubic feet per minute. The apparatus shall have the ability to monitor the internal pressure of the trouser and time. The apparatus shall incorporate all measures so that fill rate, target pressure and inflation/hold/deflation durations are all achieved as outlined in the various performance test plans.

APPENDIX 006-1: INANIMATE TEST MODELS

The inanimate test models are intended to represent a pilot. Hence the manikin(s) used to test the trousers shall be representative of the orientation of pilot in a seated position and also representative of the size of the pilot for which the suit was designed. The table below can be used as a guideline for determining a suitably sized manikin(s) to represent the size of the pilot for each trouser size.

Size M in im um

W ai st

H ei gh t

M ax st

H ei gh t

M in st

C irc um fe re nc e

M ax st irc um fe re nc e

M in

Th ig h

C irc um fe re nc e

M ax

Th ig h

C irc um fe re nc e

M in al f

C irc um fe re nc e

M ax al f

C irc um fe re nc e

0 35 1/2 39 24 28 1/2 16 7/8 22 3/8 12 15

1 37 1/2 40 1/2 28 1/2 33 19 24 1/2 12 1/2 15 1/2

2 40 1/2 43 1/2 28 1/2 33 19 24 1/2 12 1/2 15 1/2

3 43 1/2 46 1/2 28 1/2 33 19 24 1/2 12 1/2 15 1/2

4 37 1/2 40 1/2 33 37 1/2 20 26 1/2 13 16

5 40 1/2 43 1/2 33 37 1/2 20 26 1/2 13 16

6 43 1/2 46 1/2 33 37 1/2 20 26 1/2 13 16

7 37 1/2 40 1/2 37 1/2 42 22 28 1/2 13 1/2 17 1/2

8 40 1/2 43 1/2 37 1/2 42 22 28 1/2 13 1/2 17 1/2

9 43 1/2 46 1/2 37 1/2 42 22 28 1/2 13 1/2 17 1/2

10 43 1/2 46 1/2 42 46 1/2 23 3/4 30 1/4 14 3/4 18 3/4

Note: Waist Height measurement is taken from the navel to the floor while wearing boots. Waist circumference is taken at the navel.

APPENDIX B: ACCEPTANCE TEST INSTRUCTIONS T1.01 THROUGH T1.21

Test Name Sewing Visual Inspection Doc. Number ATP/ATAGS/TI.01-01 Test Classification In-Process Date / Revision 01 Feb 2001 / Nil Verification Method Inspection Contract # Test Type F-22 / Basic Anti –G Suit Prepared by

ATP/ATAGS/TI.01-1: IN-PROCESS – SEWING VISUAL INSPECTION

1. PURPOSE

To identify the critical inspection points for in-process sewing.

2. REFERENCE

2.1. Appendix 001-1: Classification of Defects.

2.2. Product Drawing Specifications (Reference ATAGS Drawing Package, #260000).

3. RESPONSIBILITY

It is the responsibility of the contractor to conduct adequate in-process visual inspections to ensure that the trousers conform to the specified requirements. This instruction is only provided as a guideline for critical inspection items. The specific content of these inspections and the inspection points may vary depending on the contractor’s production process.

4. REQUIREMENT

4.1. Sample Requirement:

Qualification, First Article & Production

Subassemblies shall be inspected during the production process.

REV B SPECIFICATION NUMBER MSF880/5-ATP-GEN-0

Test Classification In-Process Date / Revision 01 Feb 2001 / Nil Verification Method Inspection Contract # Test Type F-22 / Basic Anti –G Suit Prepared by

5. PROCEDURE

CUT PANELS CRITICAL INSPECTION POINT REFERENCE

Cut Panels �� As a minimum, all cut panels that are a component of the restraint layer shall be visually inspected to ensure that they have been oriented correctly, are dimensionally correct and are free from fabric imperfections, notches on the cut edges, damage, etc. Refer to 260000, Drawing Organization Chart, for a breakdown of applicable pattern pieces.

260000, 262001, 262002

SUB-ASSEMBLIES CRITICAL INSPECTION POINT REFERENCE

Leg Zipper Flap Buckle Assembly

�� Restraint buckle webbing attachment is in accordance with the drawing requirement.

�� Edges of the black reinforcement webbing (Leg zipper flap stiffener) is NOT heat sealed (Could abrade the bladder).

�� Zipper opens and closes freely. Cycle three times.

(Not affected by inherent waviness along the zipper teeth)

Drawing 262240

N/A

N/A

Comfort Zipper Subassemblies

�� Length of extension at the top of the zipper conforms to drawing requirements

�� Comfort zipper stitching extends through all fabric layers.

�� Zipper opens and closes freely. Cycle three times.

(Not affected by inherent waviness along the zipper teeth)

262260, 262270

262260, 262270

N/A

Leg Pocket Subassemblies

�� Leather patch is not sewn directly to the zipper (Maintenance issue)

�� Length dimension of the pocket assembly is in accordance with drawing requirements.

262500, 262600

262500, 262600

Test Classification In-Process Date / Revision 01 Feb 2001 / Nil Verification Method Inspection Contract # Test Type F-22 / Basic Anti –G Suit Prepared by

SUB-ASSEMBLIES CRITICAL INSPECTION POINT REFERENCE

Outer Restraint Layer �� Zipper is located in the middle of seam between shell front and back

�� Knee pleats are stitched so that the seam allowance is oriented downwards.

�� Measure the dimension from top knee pleat stitch line to the bottom knee pleat stitch line. Ensure that the length is in accordance with drawing requirement.

�� Measure the distance from the bottom of the leg pockets to the bottom of the leg hem. Ensure that the length is in accordance with drawing requirements.

�� Finished width of the leg lacing cover is within tolerances specified by drawing.

262001, 262002

262001, 262002

267011, 267012

262001, 262002, 267011, 267012

267011, 267012

GARMENT ASSEMBLY CRITICAL INSPECTION POINT REFERENCE

Assembly of Liner to Shell

�� Ensure that the correct size bladder is being sewn into the corresponding shell.

�� Once the bladder is installed, the bladder material should be loose between the bladder tabs. (Tension between the bladder attachment points may result in rupture during inflation)

�� Ensure that bladder is not damaged by the needle.

�� Number of bladder tabs should be verified in accordance with the drawing (39 tabs).

N/A

N/A

N/A

267012

Any other defects that affect functionality, serviceability, or appearance of the product shall also be identified during in-process inspection.

6. BASIS OF ACCEPTABILITY

6.1. Acceptance Criteria: Refer to Appendix 001-1: Classification of Defects.

7. TEST REPORT

7.1. Acceptance Test Report(s): shall indicate “acceptance” or “rejection” based on acceptance criteria described above.

7.2. Nonconformance Report or Failure Analysis in the case of rejection.

Test Name Bladder Panel Visual Inspection

Doc. Number ATP/ATAGS/TI.02-1

Test Classification In-Process Date / Revision 01 Feb 2001 / Nil Verification Method Inspection Contract # Test Type F-22 /Basic Anti –G Suit Prepared by

ATP/ATAGS/TI.02-1: BLADDER PANEL VISUAL INSPECTION

1. PURPOSE

To ensure that the cut panels of the bladder subassembly are free from defects prior to being welded.

2. REFERENCE

2.1. Appendix 001-1: Classification of Defects

3. RESPONSIBILITY

It is the responsibility of the contractor to conduct adequate in-process visual inspections to ensure that the trousers conform to the specified requirements. This instruction is only provided as a guideline for critical inspection items. The specific content of these inspections and the inspection points may vary depending on the contractor’s production process.

4. REQUIREMENT

4.1. Sample Requirement:

Qualification, First Article, & Production

Every cut panel of bladder to be visually inspected prior to being welded

5. PROCEDURE

5.1. Inspect each cut bladder panel prior to being welded.

5.2. Both sides of the panel are to be visually checked for the following:

�� Contamination on the material surface

�� Uneven coating or coating defects

�� Foreign objects imbedded in the coating

�� Holes, tears, weave inconsistencies, or other base fabric defects

6. BASIS OF ACCEPTABILITY

6.1. Acceptance Criteria:

No major defects and a maximum of two minor defects are allowable on the finished bladder assembly (Ref. Appendix 001-1: Classification of Defects).

7. TEST REPORT

7.1. Acceptance Test Report(s): N/A

7.2. Nonconformance Report or Failure Analysis in the case of rejection.

Test Name Peel Test Doc. Number ATP/ATAGS/TI.03-1 Test Classification In-Process Date / Revision 01 Feb 2001 / Nil Verification Method Inspection Contract # Test Type F-22 / Basic Anti –G Suit Prepared by

ATAGS/ATP/TI.03-1: PEEL TEST

1. PURPOSE

This test provides a preliminary indication of the adequacy of the welding process to ensure the weld is of consistent strength through the length of the weld. This test allows the operator to proceed with welding pending the results of the seam adhesion test. (ATP/ATAGS/TI.04a- 1). This is not a mandatory test, but is included as a method to optimize production throughput as necessary.

2. REFERENCE

None

3. REQUIREMENT

3.1. Sample Requirement:

One welded assembly from the current die being utilized in the process.

4. PROCEDURE

4.1. After setup, make a weld hit with the die that is in use.

4.2. Manually pull apart the two layers of material to cause separation at the weld line.

4.3. Observe the weld line to ensure that the coating has adhered to one layer of material and that the base cloth is exposed on the opposite side. This indicates the integrity of the weld is adequate to continue with the welding process.

4.4. Ensure that the corresponding seam adhesion test results are received and reviewed for adequacy to quantitatively confirm the peel test result.

5. BASIS OF ACCEPTABILITY

5.1. Acceptance Criteria:

When manually pulled apart, the entire weld line separates from the base material on one side of the fabric.

Test Name Seam Adhesion Test Doc. Number ATP/ATAGS/TI.04a-1 Test Classification In-Process Date / Revision 01 Feb 2001 / Nil Verification Method Inspection Contract # Test Type F-22 / Basic Anti –G Suit Prepared by

ATP/ATAGS/TI.04a-1: SEAM ADHESION TEST

1. PURPOSE:

To demonstrate conformance to the minimum welded seam adhesion requirement of 24 lb/in in the warp or fill direction.

2. REFERENCE

2.1. FED-STD 191, Method 5100: Standard Methods of Seam Adhesion Test.

3. REQUIREMENT

3.1. Sample Size: Three (3) samples at the beginning and end of each welding process.

3.2. Test Conditions: N/A

3.3. Test Equipment / Support: Refer to FED-STD 191

4. PROCEDURE

4.1. Make one complete weld at the beginning and end of the welding process for each die.

The material used must be indicative of the material being used in-process (same manufacturer’s lot number). The sample weld must include Polyurethane film and/or 200 denier nylon cloth in the applicable seams.

4.2. Cut three specimens from various areas of the weld. Ensure that the specimens include areas with Polyurethane film and/or 200 denier nylon cloth, as applicable.

The specimens shall be cut across and perpendicular to the seam and shall be:

��1 inch (+/- 1/16 inch wide) by 6 inches (+/- 1/16 inch long) if welded seam line is straight OR ��0.5 inch (+/- 1/16 inch wide) by 6 inches (+/- 1/16 inch long) if welded seam line is curved

4.3. Set the initial jaw separation is three inches.

4.4. Set the rate of jaw separation to be at pulling speed of 12 +/- 0.5 inch per minute.

4.5. Place the specimen between the opened jaws. One free end of the specimen is placed in the upper jaw of the inspection apparatus and the other free end is placed in the lower jaw. Ensure that the bonded portion of the specimen is centered between the two jaws.

4.6. Securely tighten the clamps to ensure a strong hold on the specimen.

4.7. Run the seam adhesion test with a constant rate of 12 inches per minute (+/- 0.5 inch).

4.8. The jaws shall be separated until breakage of the fabric or separation of the bond occurs.

4.9. Record the value achieved at the point of separation.

4.10. Repeat the steps above for the remaining 2 specimens.

Test Name Seam Adhesion Test Doc. Number ATP/ATAGS/TI.04a-1 Test Classification In-Process Date / Revision 01 Feb 2001 / Nil Verification Method Inspection Contract # Test Type F-22 / Basic Anti –G Suit Prepared by

4.11. Upon completion of all of three specimens, record the lowest value as the test result.

5. BASIS OF ACCEPTABILITY

5.1. Acceptance Criteria:

The minimum seam adhesion value for any sample is 24 lb/in. in the warp and fill directions.

6. TEST REPORT

6.1. Record the results of all sample tests.

6.2. Record the applicable lot number of the weldable fabric tested during the process.

Test Name Bladder Seam Bond Strength Doc. Number ATP/ATAGS/TI.04b-1 Test Classification Qualification & First Article Date / Revision 01 Feb 2001 / Nil Verification Method Inspection Contract # Test Type F-22 / Basic Anti –G Suit Prepared by

ATP/ATAGS/TI.04b-1: BLADDER SEAM BOND STRENGTH

1. PURPOSE:

To demonstrate conformance of the finished bladder to the minimum welded seam adhesion requirement of 24 lb/in. in the warp and fill direction.

2. REFERENCE

2.1. FED-STD 191, Method 5100: Standard Methods of Seam Adhesion Test.

3. REQUIREMENT

3.1. Sample Requirement:

Qualification, First Article One completed bladder subassembly

3.2. Sample Size: Five (5) samples from different locations of the bladder to ensure that the specimens are representative of the sealing of the entire bladder.

3.3. Test Conditions: N/A

3.4. Test Equipment / Support: Refer to FED-STD 191

4. PROCEDURE

4.1. Five specimens shall be cut from different locations of the bladder so that the specimens will be…

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