Common use of Environmental Testing and Approval Process Clause in Contracts

Environmental Testing and Approval Process. The typical process for environmental testing and approvals includes the following: (1) Environmental (noise, fuel venting, and exhaust emissions) certification compliance demonstration plans must be submitted to the FAA for review, comment, and subsequent approval prior to undertaking certification testing. (2) Information and data must be supplied to the FAA in order to conduct a finding in accordance with the Noise Control Act of 1972 (P.L. 92- 574). The FAA, before issuing an original type certificate for an aircraft of any category, must assess the extent of noise abatement technology incorporated into the type design and determine whether additional noise reduction is achievable. This examination must be initiated as soon as possible after the application for type certification in each original type certification project and reflect noise reduction potentials that become evident during the design and certification process. (3) Information and data must be supplied to the FAA in order to conduct an evaluation of the measurement and analysis methods and practices, and data correction procedures of the applicant for aircraft noise certification under 14 CFR Part 36, Subpart B and/or Subpart H. (4) Compliance demonstration aircraft noise test plans and engine exhaust emissions test plans to be used for demonstrating U.S. environmental certification compliance must be submitted to the FAA for review and comment, and subsequent approval not less than 90 days prior to commencing testing. (5) Proposed equivalent procedures to be used by the applicant during testing, data processing, data reduction, and data analysis must be specifically identified to the FAA and approved in advance by the FAA as part of items (1) and (4). (6) Compliance demonstration tests must be witnessed by FAA personnel, or FAA designated engineering representatives. Prior to the start of testing it is necessary to assure the conformity of the test article (aircraft or engine configuration) to that identified in the FAA approved compliance demonstration test plans. (7) Compliance demonstration reports must be submitted to the FAA for review and comment and subsequent approval prior to type certification approval.

Environmental Testing and Approval Process. (Reference Section III, Paragraph 3.0.1.3). The typical process for environmental testing and approvals in the United States includes the following: (1) Environmental (noise, fuel venting, and exhaust emissions) certification compliance demonstration plans must will be submitted to the FAA for review, comment, and subsequent approval prior to undertaking certification testing. (2) Information and data must will be supplied to the FAA in order to conduct a finding in accordance with the Noise Control Act of 1972 (P.L. 92- 92-574). The FAA, before issuing an original type certificate Type Certificate for an aircraft of any category, must will assess the extent of noise abatement technology incorporated into the type design and determine whether additional noise reduction is achievable. This examination must will be initiated as soon as possible after the application for type certification in each original type certification project and reflect noise reduction potentials that become evident during the design and certification process. (3) Information and data must will be supplied to the FAA in order to conduct an evaluation of the measurement and analysis methods and practices, and data correction procedures of the applicant for aircraft noise certification under 14 CFR Part part 36, Subpart B and/or Subpart H. (4) Compliance demonstration aircraft noise test plans and engine exhaust emissions test plans to be used for demonstrating U.S. United States environmental certification compliance must will be submitted to the FAA for review and comment, and subsequent approval not less than 90 days prior to commencing testing. (5) Proposed equivalent procedures to be used by the applicant during testing, data processing, data reduction, and data analysis must will be specifically identified to the FAA and approved in advance by the FAA as part of items (1) and (4)) above. (6) Compliance demonstration tests must will be witnessed by FAA personnel, or FAA designated engineering representatives. Prior to the start of testing it is necessary to assure the conformity of the test article (aircraft or engine configuration) to that identified in the FAA approved -approved compliance demonstration test plans. (7) Compliance demonstration reports must will be submitted to the FAA for review and comment and subsequent approval prior to type certification approval.

Environmental Testing and Approval Process. The typical process for environmental testing and approvals includes the following: (1) Environmental (noise, fuel venting, and exhaust emissions) certification compliance demonstration plans must be submitted to the FAA for review, comment, and subsequent approval prior to undertaking certification testing. (2) Information and data must be supplied to the FAA in order to conduct a finding in accordance with the Noise Control Act of 1972 (P.L. 92- 57492-574 §44715(a)(3)). The FAA, before issuing an original type certificate for an aircraft of any category, must assess the extent of noise abatement technology incorporated into the type design and determine whether additional noise reduction is achievable. This examination must be initiated as soon as possible after the application for type certification in each original type certification project and reflect noise reduction potentials that become evident during the design and certification process. (3) Information and data must be supplied to the FAA in order to conduct an evaluation of the measurement and analysis methods and practices, and data correction procedures of the applicant for aircraft noise certification under 14 CFR Part 36, Subpart B B, Subpart F, and/or Subpart H. (4) Compliance demonstration aircraft noise test plans and engine exhaust emissions test plans to be used for demonstrating U.S. environmental certification compliance must be submitted to the FAA for review and comment, and subsequent approval not less than 90 days prior to commencing testing. (5) Proposed equivalent procedures to be used by the applicant during testing, data processing, data reduction, and data analysis must be specifically identified to the FAA and approved in advance by the FAA as part of items (1) and (4). (6) Compliance demonstration tests must be witnessed by FAA personnel, personnel or FAA designated engineering representatives. Prior to the start of testing testing, it is necessary to assure the conformity of the test article (aircraft or engine configuration) to that identified in the FAA approved compliance demonstration test plans. (7) Compliance demonstration reports must be submitted to the FAA for review and comment and subsequent approval prior to type certification approval.

Environmental Testing and Approval Process. The typical process for environmental testing and approvals includes the followingfollowing interaction points: (1) Environmental The applicant must submit environmental (noise, fuel venting, noise and exhaust emissions) certification compliance demonstration plans must be submitted to the FAA for review, comment, and subsequent approval prior to undertaking U.S. environmental certification testing. (2) Information and data must be supplied to the FAA in order to conduct a finding in accordance with the Noise Control Act of 1972 (P.L. 92- 574)1972. The Noise Control Act of 1972 provides that the FAA, before issuing an original type certificate for an aircraft of any category, must assess the extent of noise abatement technology incorporated into the type design and determine whether additional noise reduction is achievable. This examination must be initiated as soon as possible after the application for type certification in each original type certification project and reflect noise reduction potentials that become evident during the design and certification process. (3) Information and data must be supplied to the FAA in order to conduct an evaluation and audit of the measurement and analysis methods and practices, and data correction procedures of the applicant for aircraft noise certification under 14 CFR Part 36, Subpart B and/or or Subpart H.F. (4) Compliance demonstration aircraft noise test plans and engine exhaust emissions test plans to be used for demonstrating U.S. environmental certification compliance must be submitted to the FAA for review and comment, and subsequent approval not less than 90 days prior to commencing testing. (5) Proposed equivalent procedures to be used by the applicant during testing, data processing, data reduction, and data analysis must be specifically identified to the FAA and approved in advance by the FAA as part of items (1) and (4). (6) Compliance demonstration tests must be witnessed by FAA personnel, personnel or FAA designated engineering representatives. Prior to the start of testing it is necessary to assure the conformity of the test article (aircraft or engine configuration) to that identified in the FAA approved compliance demonstration test plans. (7) Compliance demonstration reports must be submitted to the FAA for review and comment and subsequent approval prior to type certification approval.

Environmental Testing and Approval Process. The typical process for environmental testing and approvals includes the following: (1) Environmental (noise, fuel venting, and exhaust emissions) certification compliance demonstration plans must be submitted to the FAA for review, comment, and subsequent approval concurrence prior to undertaking certification testing. (2) Information and data must be supplied to the FAA in order to conduct a finding in accordance with the Noise Control Act of 1972 (P.L. 92- 92-574). The FAA, before issuing an original type certificate for an any aircraft of any category, must assess the extent of noise abatement technology incorporated into the type design and determine whether additional noise reduction is achievable. This examination must be initiated as soon as possible after the application for type certification in each original type certification project and reflect noise reduction potentials that become evident during the design and certification process. (3) Information and data must be supplied to the FAA in order to conduct an evaluation and audit of the measurement and analysis methods and practices, and data correction procedures of the applicant for aircraft noise certification under 14 CFR Part 36, Subpart B and/or Subpart H. (4) Compliance demonstration aircraft noise test plans and engine exhaust emissions test plans to be used for demonstrating U.S. environmental certification compliance must be submitted to the FAA for review and comment, and subsequent approval not less than 90 days prior to commencing testing. (5) Proposed equivalent procedures to be used by the applicant during testing, data processing, data reduction, and data analysis must be specifically identified to the FAA and approved in advance by the FAA as part of items (1) and (4). (6) Compliance demonstration tests must be witnessed by FAA personnel, personnel or FAA designated engineering representatives. Prior to the start of testing testing, it is necessary to assure the conformity of the test article (aircraft or engine configuration) to that identified in the FAA approved compliance demonstration test plans. (7) Compliance demonstration reports must be submitted to the FAA for review and comment and subsequent approval prior to type certification approval.

Environmental Testing and Approval Process. The typical In the absence of any FAA delegation to TCCA, the process for environmental testing and approvals approvals, includes the following: (1) Environmental (noise, fuel venting, venting and exhaust emissions) certification compliance demonstration plans must be submitted to the FAA for review, comment, and subsequent approval prior to undertaking certification testing. (2) Information and data must be supplied to the FAA in order to conduct make a finding in accordance with the Noise Control Act of 1972 (P.L. 92- 574). The FAA, before issuing an original type certificate for an aircraft of any category, must assess the extent of noise abatement technology incorporated into the type design and determine whether additional noise reduction is achievable. This examination must be initiated as soon as possible after the application for type certification in each original type certification project and reflect noise reduction potentials that become evident during the design and certification process. (3) Information and data must be supplied to the FAA in order to conduct an evaluation of the measurement and analysis methods and practices, and data correction procedures of the applicant for aircraft noise certification under 14 CFR Part 36, Subpart B and/or Subpart H. (4) Compliance demonstration aircraft noise test plans and engine exhaust emissions test plans to be used for demonstrating U.S. environmental certification compliance must be submitted to the FAA for review and comment, and subsequent approval not less than 90 days prior to commencing testing. (5) Proposed equivalent procedures to be used by the applicant during testing, data processing, data reduction, and data analysis must be specifically identified to the FAA and approved in advance by the FAA as part of items (1) and (4). (6) Compliance demonstration tests must be witnessed by FAA personnel, or FAA designated engineering representatives, or TCCA when specifically requested to act on behalf of the FAA. Prior to the start of testing it is necessary to assure the conformity of the test article (aircraft or engine configuration) to that identified in the FAA approved compliance demonstration test plans. (7) Compliance demonstration reports must be submitted to the FAA for review and comment and subsequent approval prior to type certification approval.

Environmental Testing and Approval Process. The typical In the absence of any FAA delegation to CAA, the process for environmental testing and approvals includes the following: (1) Environmental (noise, fuel venting, and exhaust emissions) certification compliance demonstration plans must be submitted to the FAA for review, comment, and subsequent approval prior to undertaking certification testing. (2) Information and data must be supplied to the FAA in order to conduct a finding in accordance with the Noise Control Act of 1972 (P.L. 92- 92-574). The FAA, before issuing an original type certificate TC for an aircraft of any category, must assess the extent of noise abatement technology incorporated into the type design and determine whether additional noise reduction is achievable. This examination must be initiated as soon as possible after the application for type certification in each original type certification project and reflect noise reduction potentials that become evident during the design and certification process. (3) Information and data must be supplied to the FAA in order to conduct an evaluation and audit of the measurement and analysis methods and practices, and data correction procedures of the applicant for aircraft noise certification under 14 CFR Part 36, Subpart B and/or Subpart H. (4) Compliance demonstration aircraft noise test plans and engine exhaust emissions test plans to be used for demonstrating U.S. environmental certification compliance must be submitted to the FAA for review and comment, and subsequent approval not less than 90 days prior to commencing testing. (5) Proposed equivalent procedures to be used by the applicant during testing, data processing, data reduction, and data analysis must be specifically identified to the FAA and approved in advance by the FAA as part of items (1) and (4). (6) Compliance demonstration tests must be witnessed by FAA personnel, or FAA designated engineering representativesrepresentatives must witness compliance demonstration tests. Prior to the start of testing it is necessary to assure ensure the conformity of the test article (aircraft or engine configuration) to that identified in the FAA approved compliance demonstration test plans. (7) Compliance demonstration reports must be submitted to the FAA for review and comment and subsequent approval prior to type certification approval.

Environmental Testing and Approval Process. The typical FAA process for environmental testing and approvals includes the following: (1) Environmental (noise, fuel venting, and exhaust emissions) certification compliance demonstration plans must be submitted to the FAA for review, comment, and subsequent approval prior to undertaking certification testing. (2) Information and data must be supplied to the FAA in order to conduct a finding in accordance with the Noise Control Act of 1972 (P.L. 92- 92-574). The FAA, before issuing an original type certificate for an aircraft airplane of any category, must assess the extent of noise abatement technology incorporated into the type design and determine whether additional noise reduction is achievable. This examination must be initiated as soon as possible after the application for type certification in each original type certification project and reflect noise reduction potentials that become evident during the design and certification process. (3) Information and data must be supplied to the FAA in order to conduct an evaluation and audit of the measurement and analysis methods and practices, and data correction procedures of the applicant for aircraft noise certification under 14 CFR Part 36, Subpart B and/or Subpart H. (4) Compliance demonstration aircraft noise test plans and engine exhaust emissions test plans to be used for demonstrating U.S. environmental certification compliance must be submitted to the FAA for review and comment, and subsequent approval not less than 90 days prior to commencing testing. (5) Proposed equivalent procedures to be used by the applicant during testing, data processing, data reduction, and data analysis must be specifically identified to the FAA and approved in advance by the FAA as part of items (1) and (4). (6) Compliance demonstration tests must be witnessed by FAA personnel, or FAA designated engineering representativesrepresentatives when specifically delegated to act on behalf of the FAA, must witness compliance demonstration tests. Prior to the start of testing testing, it is necessary to assure the conformity of the test article (aircraft airplane or engine configuration) to that identified in the FAA approved compliance demonstration test plans. (7) Compliance demonstration reports must be submitted to the FAA for review and comment and subsequent approval prior to type certification approval.

Environmental Testing and Approval Process. The typical FAA process for environmental testing and approvals includes the following: (1) Environmental (noise, fuel venting, and exhaust emissions) certification compliance demonstration plans must be submitted to the FAA for review, comment, and subsequent approval prior to undertaking certification testing. (2) Information and data must be supplied to the FAA in order to conduct a finding in accordance with the Noise Control Act of 1972 (P.L. 92- 574). The FAA, before issuing an original type certificate TC for an aircraft of any category, must assess the extent of noise abatement technology incorporated into the type design and determine whether additional noise reduction is achievable. This examination must be initiated as soon as possible after the application for type certification in each original type certification project and reflect noise reduction potentials that become evident during the design and certification process. (3) Information and data must be supplied to the FAA in order to conduct an evaluation of the measurement and analysis methods and practices, and data correction procedures of the applicant for aircraft noise certification under 14 CFR Part 36, Subpart B and/or Subpart H. (4) Compliance demonstration aircraft noise test plans and engine exhaust emissions test plans to be used for demonstrating U.S. environmental certification compliance must be submitted to the FAA for review and comment, and subsequent approval not less than 90 days prior to commencing testing. (5) Proposed equivalent procedures to be used by the applicant during testing, data processing, data reduction, and data analysis must be specifically identified to the FAA and approved in advance by the FAA as part of items (1) and (4). (6) Compliance demonstration tests must be witnessed by FAA personnel, or FAA designated engineering representatives. Prior to the start of testing it is necessary to assure the conformity of the test article (aircraft or engine configuration) to that identified in the FAA approved compliance demonstration test plans. (7) Compliance demonstration reports must be submitted to the FAA for review and comment and subsequent approval prior to type certification approval.