Division (b) A statement of conformity shall include all of the below:F1

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

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

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

additionally, in the case of environmental requirements:

1. (i)

   a statement that the completed engine is in compliance with the applicable engine exhaust emissions requirements on the date of manufacture of the engine, and;

2. (ii)

   a statement that the completed aeroplane is in compliance with the applicable CO ₂ emissions requirements on the date its first certificate of airworthiness is issued.