New Aircraft, Aircraft Engines, and Propellers. (a) Except as provided in paragraph 3.2.2.4, the CAAI shall accept FAA Export Certificates of Airworthiness on new aircraft, aircraft engines and propellers, as identified in Section II, only when the FAA certifies that each aircraft, aircraft engine and propeller: (1) Conforms to a type design approved by the CAAI, as specified in the CAAI’s type certificate data sheet and any additional supplemental type certificates approved/accepted by the CAAI; (2) Is in a condition for safe operation, including compliance with applicable Israeli and U.S. Airworthiness Directives, as notified; (3) Meets all additional requirements prescribed by the CAAI, as notified; and (4) Has undergone a final operational check (only for aircraft engines and propellers). (b) Each aircraft, aircraft engine, and propeller exported to Israel with FAA airworthiness approval will have an FAA Form 8130-4, Export Certificate of Airworthiness, issued in accordance with the requirements of 14 CFR Part 21, Subpart L. (c) For aircraft, the FAA Export Certificate of Airworthiness should contain a statement such as: “The [INSERT MODEL] covered by the certificate conforms to the type design approved under CAAI Type Certificate Number [INSERT TYPE CERTIFICATE NUMBER AND TCDS REVISION LEVEL], and is found to be in a condition for safe operation,” and/or any other “import requirements” text as specified in the Israeli Type Certificate Data Sheet. (d) For aircraft engines and propellers, the FAA Export Certificate of Airworthiness should contain a statement such as: “The [INSERT AIRCRAFT ENGINE OR PROPELLER] covered by this certificate conforms to the type design approved under CAAI Type Certificate Number [INSERT TYPE CERTIFICATE NUMBER AND TCDS REVISION LEVEL], is found to be in a condition for safe operation and has undergone a final operational check,” and/or any other “import requirements” text as specified in the Israeli Type Certificate Data Sheet.
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Samples: Implementation Procedures, Implementation Procedures
New Aircraft, Aircraft Engines, and Propellers. (a) Except as provided in paragraph 3.2.2.4, the CAAI ANAC shall accept FAA Export Certificates of Airworthiness on new aircraft, aircraft engines and propellers, as identified in Section II, only when the FAA certifies that each aircraft, aircraft engine and propeller:
(1) Conforms to a type design approved by the CAAIANAC, as specified in the CAAIANAC’s type certificate data sheet (Airplane Data Sheet – EA; Rotorcraft Data Sheet – ER; Engine Data Sheet – EM; Propeller Data Sheet – EH; as applicable), except for aircraft, aircraft engines and any additional supplemental type certificates approved/accepted by propellers exempted from such approval per RBHA 21.29 and also referenced in the CAAIFAA AC 21-2, Export Airworthiness Approval Procedures (Appendix 2 - Brazilian Requirements);
(2) Is in a condition for safe operation, including compliance with applicable Israeli Brazilian and U.S. Airworthiness Directives, as notified;
(3) Meets all additional requirements prescribed by the CAAIANAC, as notified; and
(4) Has undergone a final operational check (only for aircraft engines and propellers).
(b) Each aircraft, aircraft engine, and propeller exported to Israel Brazil with FAA airworthiness approval will have an FAA Form 8130-4, Export Certificate of Airworthiness, issued in accordance with the requirements of 14 CFR Part 21, Subpart L.
(c) For aircraft, the FAA Export Certificate of Airworthiness should contain a statement such as: “The [INSERT AIRCRAFT MODEL] covered by the certificate conforms to the type design approved under CAAI ANAC Type Certificate Number [INSERT TYPE CERTIFICATE NUMBER AND TCDS REVISION LEVEL], and is found to be in a condition for safe operation,” and/or any other “import requirements” text as specified in the Israeli ANAC Type Certificate Data Sheet. For aircraft exempted from the Brazilian type certification process, as referred to in 3.2.2.0(a)(1), the statement above should include the FAA Type Certificate number. In addition, for either case, the FAA Export Certificate of Airworthiness should list all STCs and field approvals documents incorporated in the particular aircraft.
(d) For aircraft engines and propellers, the FAA Export Certificate of Airworthiness should contain a statement such as: “The [INSERT AIRCRAFT ENGINE OR PROPELLER] covered by this certificate conforms to the type design approved under CAAI ANAC Type Certificate Number [INSERT TYPE CERTIFICATE NUMBER AND TCDS REVISION LEVEL], is found to be in a condition for safe operation and has undergone a final operational check,” and/or any other “import requirements” text as specified in the Israeli ANAC Type Certificate Data Sheet. For aircraft engines and propellers exempted from the Brazilian type certification process, as referred to in 3.2.2.0(a)(1), the statement above should include the FAA Type Certificate number.
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Samples: Implementation Procedures
New Aircraft, Aircraft Engines, and Propellers. (a) Except as provided in paragraph 3.2.2.4, the CAAI CAA shall accept FAA Export Certificates of Airworthiness on new aircraft, aircraft engines and propellers, as identified in Section II, only when the FAA certifies that each aircraft, aircraft engine and propeller:
(1) Conforms to a an FAA-approved type design approved by the CAAI, as specified in the CAAI’s and type certificate data sheet and any additional supplemental type certificates approved/accepted by the CAAICAA under CAR Part 21 Subpart B. (Accepted types are listed in CAA AC 21-1.2);
(2) Is in a condition for safe operation, including compliance with applicable Israeli FAA and U.S. CAA Airworthiness Directives, as notified;
(3) Meets all additional requirements prescribed by the CAAICAA, as notified; and
(4) Has undergone a final operational check (only for aircraft engines and propellers).
(b) Each aircraft, aircraft engine, and propeller exported to Israel New Zealand with FAA airworthiness approval will have an FAA Form 8130-4, Export Certificate of Airworthiness, issued in accordance with the requirements of 14 CFR Part 21, Subpart L.
(c) For aircraft, the FAA Export Certificate of Airworthiness Airworthiness, Form 8130-4, should contain a statement such as: “The [INSERT AIRCRAFT MODEL] covered by the certificate conforms to the type design approved under CAAI Type Certificate U.S. TC Number [INSERT TYPE CERTIFICATE TC NUMBER AND TCDS REVISION LEVEL], and is found to be in a condition for safe operation,” and/or any other “import importing requirements” text as specified in the Israeli CAA Type Certificate Data Sheet.
(d) For aircraft engines and propellers, the FAA Export Certificate of Airworthiness should contain a statement such as: “The [INSERT AIRCRAFT ENGINE OR PROPELLER] covered by this certificate conforms to the type design approved under CAAI Type Certificate FAA TC Number [INSERT TYPE CERTIFICATE TC NUMBER AND TCDS REVISION LEVEL], is found to be in a condition for safe operation and has undergone a final operational check,” and/or any other “import requirements” text as specified in the Israeli CAA Type Certificate Data Sheet.
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Samples: Implementation Procedures