purpose of point 21A.130(a);
(c)
demonstrating that it is able to provide assistance in accordance with points 21A.3 and 21A.129(d).';
8.
in point 21A.125B(c), the reference to '21B.143' is replaced by the reference to 'point 21B.125';
9.
point 21A.126 is amended as follows:
(i)
in point (a), '21A.125' is replaced by '21A.125A(a)';
(i)
in point (b), '21A.125(a)' is replaced by '21A.125A(a)';
10.
in point 21A.127(a), '21A.125(a)' is replaced by '21A.125A(a)';
11.
in point 21A.128, '21A.125(a)' is replaced by '21A.125A(a)';
12.
point 21A.165 is amended as follows:
(i)
in point (c) point 2 is replaced by the following:
'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, and additionally in case of engines, determine according to data provided by the engine type-certificate holder that each completed engine is in compliance with the applicable emissions requirements as defined in point 21A.18(b), current at the date of manufacture of the engine, to certify emissions compliance, or';
(ii)
point (k) is replaced by the following:
'(k)
Where applicable, under the privilege of point 21A.163(e), establish compliance with point 21A.711(c) and (e) before issuing a permit to fly to an aircraft.';
13.
in point 21A.174(b)3(ii), '21A.184(c)' is replaced by '21B.327(c)';
14.
point 21A.183 is deleted;
15.
point 21A.184 is deleted;
16.
point 21A.205 is deleted;
17.
in point 21A.245, point (a) is replaced by the following:
'(a)
The staff in all technical departments are of sufficient numbers and experience and have been given appropriate authority to be able to discharge their allocated responsibilities and that these, together with the accommodation, facilities and equipment are adequate to enable the staff to achieve the airworthiness and environmental protection objectives for the product.';
18.
point 21A.263 is amended as follows:
(a)
in point (b), point 4 is replaced by the following
'4.
an ETSO authorisation under point 21A.602B(b)(1); or';
(b)
point (c) is amended as follows:
(i)
points 3 and 4 are replaced by the following:
'3.
to issue information or instructions containing the following statement: The technical content of this document is approved under the authority of DOA ref. EASA.21J.[XXXX].
4.
to approve documentary changes to the aircraft flight manual and supplements, and issue such changes containing the following statement: Revision No [YY] to AFM (or supplement) ref. [ZZ], is approved under the authority of DOA ref. EASA.21J.[XXXX].';
(ii)
point 7 is replaced by the following:
'7.
to issue a permit to fly in accordance with point 21A.711(b) for an aircraft it has designed or modified, or for which it has approved under point 21A.263(c)6 the conditions under which the permit to fly can be issued, and when the design organisation itself is controlling under its Design Organisation Approval the configuration of the aircraft and is attesting conformity with the design conditions approved for the flight.';
19.
in point 21A.265, point (g) is