EASA Procedures. (a) EASA is required to make findings of compliance to the environmental essential requirements, found in Article 6 of the Basic Regulation, the requirements of Part 21A.18, and in accordance with the procedures as defined in CS34 and CS36 (b) Upon request to FAA, and after mutual agreement, EASA may delegate environmental findings of compliance to FAA to be performed on behalf of EASA. For tests conducted prior to a TC or STC application being made to EASA, EASA may accept FAA-approved noise and emissions certification compliance data, provided the data meets the applicable EU regulations, and EASA guidance and policy material. (c) In the absence of any delegation to FAA, or acceptable previously undertaken environmental testing, the EASA 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 EASA for review, comment, and subsequent approval prior to undertaking certification testing. (2) Information and data must be supplied to the EASA in 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. (3) Aircraft noise compliance demonstration 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. (4) 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), (2) and
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Samples: Technical Implementation Procedures, Technical Implementation Procedures
EASA Procedures. (a) EASA is required to make findings of compliance to the environmental essential requirements, found in Article 6 of the Basic Regulation, the requirements of Part 21A.18, and in accordance with the procedures as defined in CS34 and CS36. EASA shall review and approve all compliance demonstration plans and reports submitted via the FAA.
(b) Upon request to FAA, and after mutual agreement, EASA may delegate environmental findings of compliance test witnessing and other functions to FAA to be performed on behalf of EASA. For tests conducted prior to a TC or STC application being made to EASA, EASA may accept FAA-approved noise and emissions certification compliance data, provided the data meets the applicable EU regulations, and EASA guidance and policy material.
(c) In the absence of any delegation to FAA, or acceptable previously undertaken environmental testing, the EASA 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 EASA for review, comment, and subsequent approval prior to undertaking certification testing.undertaking
(2) Information and data must be supplied to the EASA in 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.
(3) Aircraft noise compliance demonstration 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.
(4) 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), (2) and
Appears in 1 contract
Samples: Technical Implementation Procedures
EASA Procedures. (a) EASA is required to make findings of compliance to the environmental essential requirements, found in Article 6 of the Basic Regulation, the requirements of Part 21A.18, and in accordance with the procedures as defined in CS34 and CS36. EASA shall review and approve all compliance demonstration plans and reports submitted via the FAA.
(b) Upon request to FAA, and after mutual agreement, EASA may delegate environmental findings of compliance test witnessing and other functions to FAA to be performed on behalf of EASA. For tests conducted prior to a TC or STC application being made to EASA, EASA may accept FAA-approved noise and emissions certification compliance data, provided the data meets the applicable EU regulations, and EASA guidance and policy material.
(c) In the absence of any delegation to FAA, or acceptable previously undertaken environmental testing, the EASA 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 EASA for review, comment, and subsequent approval prior to undertaking 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 EASA in 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.
(3) Aircraft noise compliance demonstration 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.
(4) 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), (2) and
Appears in 1 contract
Samples: Technical Implementation Procedures