Annex I (Part 21) to Regulation (EU) No 748/2012 is amended as follows:

1. (1)

   Point 21A.4(a) to subpart A of section A is replaced by the following:

   1. ‘(a)

      The satisfactory coordination of design and production required by 21A.122, 21A.130(b)(3) and (4), 21A.133 and 21A.165(c)(2) and (3) as appropriate, and’;

2. (2)

   Point 21A.130(b) to subpart F of section A is replaced by the following:

   1. ‘(b)

      A statement of conformity shall include:

      1. 1.

         For each product, part or appliance a statement that the product or appliance, conforms to the approved design data and is in condition for safe operation; and

      2. 2.

         For each aircraft, a statement that the aircraft has been ground and flight checked in accordance with 21A.127(a); and

      3. 3.

         For each engine, or variable pitch propeller, a statement that the engine or propeller has been subjected by the manufacturer to a final functional test in accordance with 21A.128; and

      4. 4.

         Additionally, in the case of engines, a statement that the completed engine is in compliance with the applicable emissions requirements on the date of manufacture of the engine.’;

3. (3)

   In point 21A.165(c) to subpart G of section A, points 2 and 3 are replaced by the following:

   1. ‘2.

      Determine that other products, parts or appliances are complete and conform to the approved design data and are in a condition for safe operation before issuing an EASA Form 1 to certify conformity to approved design data and condition for safe operation;

   2. 3.

      Additionally, in the case of engines, determine that the completed engine is in compliance with the applicable emissions requirements on the date of manufacture of the engine;

   3. 4.

      Determine that other products, parts or appliances conform to the applicable data before issuing an EASA Form 1 as a conformity certificate.’