Page 236 - UK Regulation Part 21 Initial Airworthiness Annex I (consolidated) March 2022
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PART 21 - INITIAL AIRWORTHINESS (ANNEX I)


                                              certificate issued by the CAA
                                              The CAA may issue under its own legislation a document to list and identify all necessary
                                              conditions, restrictions and limitations that result from the investigation by the CAA. This
                                              document could take the form of an addendum to the approved flight manual or operating
                                              instruction or comparable document and should be referenced in Block 5
                                              (limitations/remarks) of the appropriate certificate of airworthiness.
             21.B.325                Issue of airworthiness certificate
                                          (a)  The CAA shall issue or change a certificate of airworthiness (CAA Form 25, see Appendix
                                              VI) without undue delay when it is satisfied that the requirements of point 21.B.326 and the
                                              applicable requirements of Section A of Subpart H of this Annex I (Part 21) are met.
                                          (b)  The CAA shall issue or change a Restricted certificate of airworthiness (CAA Form 24,
                                              see Appendix V) without undue delay when it is satisfied that requirements of point
                                              21.B.327 and the applicable requirements of Section A of Subpart H of this Annex I (Part
                                              21) are met.
                                          (c)  for a new aircraft or used aircraft originating from a non-member State, in addition to the
                                              appropriate airworthiness certificate referred to in point (a) or (b), the CAA shall issue an
                                              initial airworthiness review certificate (CAA Form 15a or 15c, see Appendix II).
             21.B.325(a) GM          Airworthiness certificates
                                           1.  Completion of the certificate of airworthiness
                                              Block 5: Insert restrictions developed in accordance with Part 21, including any reference
                                              to limitations as indicated in GM 21.B.320(b)(6).
                                           2.  Completion of the restricted certificate of airworthiness
                                              Block 5: Insert restrictions developed in accordance with Part 21, including any reference
                                              to limitations as indicated in GM 21.B.320(b)(6).
             21.B.325(b) GM          Completion of the Airworthiness Review Certificate
                                           1.  Purpose
                                              In accordance with the applicable continuing airworthiness requirements a certificate of
                                              airworthiness is valid only if a valid airworthiness review certificate is attached to it. For
                                              new aircraft, the CAA will issue the airworthiness review certificate when issuing the
                                              certificate of airworthiness.
             21.B.326                Certificate of airworthiness
                                      The CAA shall issue a certificate of airworthiness for:
                                          (a)  new aircraft:
                                               1.  upon presentation of the documentation required by point 21.A.174(b)(2);
                                               2.  where the CAA is satisfied that the aircraft conforms to an approved design and is in
                                                  a condition for safe operation; this may include inspections by the CAA; and
                                               3.  where the CAA is satisfied that the aircraft is in compliance with the applicable CO2
                                                  emissions requirements on the date on which the certificate of airworthiness is first
                                                  issued.
                                          (b)  used aircraft:
                                               1.  upon presentation of the documentation required by point 21.A.174(b)(3)
                                                  demonstrating that:
                                                   (i) the aircraft conforms to a type design approved under a type-certificate and
                                                      any supplemental type- certificate, change or repair approved in accordance
                                                      with this Annex I (Part 21) and;
                                                  (ii)  the applicable airworthiness directives have been complied with and;
                                                  (iii) the aircraft has been inspected in accordance with the provisions of Annex I
                                                      (Part-M) or Annex Vb (Part-ML) of Regulation (EU) No 1321/2014, as
                                                      appropriate.
                                                  (iv) the aircraft was in compliance with the applicable CO2 emissions
                                                      requirements on the date on which the certificate of airworthiness was first
                                                      issued;
                                               2.  where the CAA is satisfied that the aircraft conforms to an approved design and is in
                                                  a condition for safe operation; this may include inspections by the CAA and
                                               3.  where the CAA is satisfied that the aircraft was in compliance with the applicable
                                                  CO2 emissions requirements on the date on which the certificate of airworthiness
                                                  was first issued.
             21.B.327                Restricted certificate of airworthiness
                                          (a)  The CAA shall issue a restricted certificate of airworthiness for:
                                               1.  new aircraft:
                                                   (i) upon presentation of the documentation required by point 21.A.174(b)(2);
                                                  (ii)  when the CAA is satisfied that the aircraft conforms to a design approved by
                                                      the CAA under a restricted type- certificate or in accordance with specific
                                                      airworthiness specifications, and is in a condition for safe operation. This may
                                                      include inspections by the CAA;
                                               2.  used aircraft:
                                                   (i) upon presentation of the documentation required by point 21.A.174(b)(3)
                                                      demonstrating that:
                                                      (A)  the aircraft conforms to a design approved by the CAA under a
                                                          restricted type-certificate or in accordance with specific airworthiness
                                                          specifications and any supplemental type-certificate change or repair
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