Airworthiness Considerations in Conformity with DOC 9760 Requirements

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Doc 9760 is presented in 5 Parts:

» 
Part I ( Definitions and Abbreviations)
» Part II ( Airworthiness Organization Structure and Responsibilities of State)
» Part III ( State of Registry)
» Part IV ( State of the Operator)
» Part V ( State of Design and Manufacture)

Additional guidance on the contents of forms and the processing of applications

» Roles and Responsibilities
» Certificate of Registration (C of R)
» Certificate of Airworthiness (C of A)
» Noise certificate
» Export C of A
» Special flight permit
» Major repairs and modifications approval
» Maintenance program approval
» Approval of maintenance organization
» Continuing airworthiness of aircraft

State of Registry roles and responsibilities (Article 12 of the Convention)

Each contracting State undertakes to adopt measures to insure that every aircraft flying over and maneuvering within its territory and that every aircraft carrying its nationality mark, wherever such aircraft may be, shall comply with the rules and regulations relating to the flight and maneuver of aircraft there in force.

» Each contracting State undertakes to keep its own regulations in these respects uniform, to the greatest extent, with those established from time to time under this Convention.
» Develops and promulgates regulations:
» Registration of aircraft
» Airworthiness and continuing airworthiness of aircraft
» Noise certification
» Issuance, validation, or acceptance of type certificates
» Issues certificates and permits:
» Certificate of Registration
» Certificate of Airworthiness
» Noise certificate
» Special flight permit
» Export Certificate of Airworthiness
» Approves

o   Modification and repair

o   Maintenance Organizations

o   Maintenance programme

» Ensures the continuing airworthiness of aircraft

o   Conducts surveillance

o   Take appropriate enforcement action, when required.

o   Ensure that it informs the State of Design when it first enters on its register an aircraft of a particular type b. Determine the continuing airworthiness of an aircraft in relation to the appropriate airworthiness requirements.

o   Develop or adopt requirements to ensure the continuing airworthiness of aircraft during its service life including requirements that the aircraft:

o   Continues to comply with the appropriate airworthiness requirements after a modification, repair, or installation of a replacement part.

o   Is maintained in an airworthy condition and in compliance with maintenance requirements of Annex 6.

» Upon receipt of MCAI from the State of Design adopt directly or assess the information received and take appropriate action.
» Ensure the transmission to the State of Design all MCAI issued by the State of Registry in respect of a product or modification originated from that aircraft.
» Ensure there exist a system whereby information on faults, malfunctions, defects, and other occurrences that might cause adverse effects on continuing airworthiness is transmitted to the type design organization. If this is a modification, then the organization responsible for the design modification should be informed.

Each Contracting State should establish

In respect of large aircraft, the type of service information that is to be reported to its airworthiness authority by operators, organizations responsible for type design, and maintenance organizations. Procedures for reporting this information should also be established.

» Part III of Doc 9760 Certificate of Airworthiness State of Registry has to ensure that the design of the aircraft meets the appropriate airworthiness requirements.
» This can be done through:

o   Type Certification - Full certification exercise

o   Type Validation - certification review to the differences that exist between the State of Registry and State of Design

o   Type Acceptance - recognition and direct acceptance of type certification already done by the State of Design

Maintenance program

An approved maintenance program is required for each aircraft type. The information in a maintenance program should contain at least the following:

» Maintenance tasks and the intervals at which these are to be performed
» When applicable, a continuing structural integrity program
» Procedures for changing and deviating from the above
» When applicable, conditioning monitoring and reliability program, descriptions of aircraft systems, components, and engines.
» Maintenance tasks and that have been specified as mandatory in the approval of the type design should be identified as such in the maintenance program.

Certificate of Airworthiness (Article 31)

Every aircraft engaged in international navigation shall be provided with a valid Certificate of Airworthiness issued or rendered valid by the State in which the aircraft is registered (Annex 8, Part II, Para 3.2.1)

A Certificate of Airworthiness shall be issued by a Contracting State on the basis of satisfactory evidence that the aircraft complies with the design aspects of the appropriate airworthiness requirements

Certificate of Airworthiness

A Certificate of Airworthiness shall be:

» Issued or
» Validated

States should develop regulations and procedures for:

» The issuance of a C of A
» The validation of a C of A
» The renewal of a C of A and
» The delegation for the issuance or renewal of a C of A

Application for the issue of C of A:

» 
Review application form
» Duly completed and submitted with all supporting documents
» Identify aircraft configuration
» To identify which components and changes to the type design have been made
» For new aircraft, the manufacturer should identify any changes
» For old aircraft, records from the previous State that issued the C of A
» Review documentation
» AFM
» Maintenance program
» Status of maintenance tasks with respect to the maintenance program
» Certification of any major repairs or modifications
» Status of MCAI compliance mandated by the State of Registry
» Mass and balance report together with an equipment list
» Aircraft and engine or propeller logbooks and maintenance records
» Records that demonstrate the origin of parts that were installed new or repaired
» Export C of A, if applicable
» Inspection of aircraft
» Exterior
» Damage to aircraft
» Verify major modifications and repairs
» Aircraft, engines/propellers identification plates
» Components serial numbers conformity with aircraft records
» Interior
» Conformity of aircraft interior configuration, emergency and safety equipment
» Markings and placards location and language
» Additional markings as required by local regulations

Note: All non-conformities observed should be reported to the applicant in writing.

The C of A is only issued after all non-conformities are satisfactorily addressed.

Certificate of Airworthiness - Issuance of a C of A

» 
The aircraft must be registered in the State.
» Application form completed and signed by the owner or appropriately delegated person on behalf of the operator.
» Particulars of all work done to restore the aircraft to an airworthy condition.
» Full particulars of work done should be entered in the appropriate logbook and a maintenance release should be completed and the aircraft certified airworthy by an organization or suitably authorized person.
» An organization or suitably qualified person should certify the aircraft's airworthiness.
» All MCAI and other applicable requirements are carried out and certified.

Issue C of A when all requirements are met.

Note: The C of A is only issued after all non-conformities are satisfactorily addressed.

Next Steps

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