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understood that pending entry into force of Article 83 bis of the Convention, the foregoing action would only be a matter of
practical convenience and would not affect either the provisions of the Chicago Convention prescribing the duties of the State of
Registry or any third State. However, as Article 83 bis entered into force on 20 June 1997, such transfer agreements will have effect
in respect of those Contracting States which have ratified the related Protocol (Doc 9318) upon firlfilment of the conditions
established in Article 83 bis.
CHAPTER 1. TYPE CERTIFICATION
1.1 Applicability
The Standards of this chapter shall be applicable to all aircraft
of types for which the application for certification was submitted
to a Contracting State on or after 13 June 1960, except
that the provisions of 1.4 of this part shall only be applicable
to an aircraft type for which an application for a Type
Certificate is submitted to the State of Design on or after
2 March 2004.
Note.- Normally, a request for a Type Certijicate is submitted
by the aircraji manufacturer when the aircraji is
intended for serial production.
1.2.3 Where the design features of a particular aircraft
render any of the design aspects of the appropriate airworthiness
requirements or the Standards in Parts 111, N, V, VI or VII
inappropriate, the Contracting State shall apply appropriate
requirements that will give at least an equivalent level of
safety.
1.2.4 Where the design features of a particular aircraft
render any of the design aspects of the appropriate airworthiness
requirements or the Standards in Parts 111, IV, V, VI or VII
inadequate, additional requirements that are considered by the
Contracting State to give at least an equivalent level of safety
shall be applied.
Note.- An Airworthiness Manual (Do,c 9760) containing
guidance material has been published by ZCAO.
1.2 Design aspects of the appropriate
airworthiness requirements
1.2.1 The design aspects of the appropriate airworthiness
requirements, used by a Contracting State for type certification
in respect of a class of aircraft or for any change to such type
certification, shall be such that compliance with them will
ensure compliance with the Standards of Part I1 of this Annex
and, where applicable, with the Standards of Parts 111, IV, V,
VI or VII of this Annex.
1.2.2 The design shall not have any features or characteristics
that render it unsafe under the anticipated operating
conditions.
1.3 Proof of compliance with the
appropriate airworthiness requirements
1.3.1 There shall be an approved design consisting of
such drawings, specifications, reports and documentary evidence
as are necessary to define the design of the aircraft and
to show compliance with the design aspects of the appropriate
airworthiness requirements.
Note.- The approval of the design is facilitated, in some
States, by approving the design organization.
ANNEX 8 11-1-1 13/12/07
Anna 8 -Airworthiness of Aircraft Part N
1.3.2 The aircraft shall be subjected to such inspections
and ground and flight tests as are deemed necessary by the
State to show compliance with the design aspects of the appropriate
airworthiness requirements.
1.3.3 In addition to determining compliance with the
design aspects of the appropriate airworthiness requirements
for an aircraft, Contracting States shall take whatever other
steps they deem necessary to ensure that the design approval
is withheld if the aircraft is known or suspected to have
dangerous features not specifically guarded against by those
requirements.
1.3.4 A Contracting State issuing an approval for the
design of a modification, of a repair or of a replacement part
shall do so on the basis of satisfactory evidence that the aircraft
is in compliance with the airworthiness requirements
used for the issuance of the Type Certificate, its amendments
or later requirements when determined by the State.
Note I.- While a repair may be completed and shown to
be in compliance with the set of requirements that had been
selected for the original type certification of the aircraft, some
repairs may need to be shown to comply with the latest applicable
certzjication requirements. In such cases, States may
issue a repair design approval against the latest set of requirements
for that aircraft type.
Note 2.- The approval of the design of a modifcation to
an aircrafi is signified, in some States, by the issuance of a
supplemental 5pe Certifcate or amended 5pe Certifcate.
1.4 'Qpe Certificate
1.4.1 The State of Design, upon receipt of satisfactory
　
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