DCA
CYPRUS



AIC C 015/2007 - Effective 14 Nov 2007
ISSUE OF AN EASA PERMIT TO FLY

GENERAL

A Permit to Fly is issued by the Department of Civil Aviation, Safety Regulation Unit or by an organisation that has an EASA Part 21 Production or Design approval with privileges to issue such a Permit. It is generally issued when a certificate of airworthiness is temporarily invalid, for example as the result of damage, or when a certificate of airworthiness cannot be issued. These are the instances when the aircraft does not comply with the essential requirements for airworthiness or when compliance with those requirements has not yet been shown, but the aircraft is nevertheless capable of performing a safe flight.
Permits to fly shall be issued in accordance with EASA Part 21, Subpart P under defined conditions and for the following purposes:
In order for a Permit to Fly to be approved by the Department, an approval of the flight conditions must be obtained. Flight conditions are approved by EASA when this approval is related to the safety of the design. In all other cases the flight conditions are approved by the Department. Flight conditions can also be approved by an organisation that has an EASA Part 21 Production or Design approval with privileges to approve such conditions.
Flight conditions include:
  1. The configuration(s) for which the permit to fly is requested;
  2. Any condition or restriction necessary for safe operation of the aircraft, including:
    • The conditions or restrictions put on itineraries or airspace, or both, required for the flight(s);
    • The conditions and restrictions put on the flight crew to fly the aircraft;
    • The restrictions regarding carriage of persons other than flight crew;
    • The operating limitations, specific procedures or technical conditions to be met;
    • The specific flight test programme (if applicable);
    • The specific continuing airworthiness arrangements including maintenance instructions and regime under which they will be performed;
  3. The substantiation that the aircraft is capable of safe flight under the conditions or restrictions of subparagraph (b);
  4. The method used for the control of the aircraft configuration, in order to remain within the established conditions.

PROCEDURE WHEN THE APPROVAL OF FLIGHT CONDITIONS IS RELATED TO THE SAFETY OF THE DESIGN

Examples of flight conditions, the approval of which is related to the safety of design are when:
The applicant must apply for approval of such flight conditions directly to EASA, using EASA Form 37. This form can be downloaded from the EASA website, http://www.easa.europa.eu/home/c_permittofly.html, or obtained from the Safety Regulation Unit of the Department.
EASA will approve the flight conditions and return EASA Form 18B to the applicant. The applicant must submit this form together with an application for an EASA Permit to Fly, EASA (DCA) Form 21, to the Department.
Establishing compliance with the conditions of an EASA Permit to fly will require either direct inspection of the aircraft by the Department or certification and issue of a Flight Release Certificate by an authorised person.
If a Flight Release Certificate is to be issued, the Standard Form SF-50 Flight Release Certificate document shall be used.
The Flight Release Certificate can only be issued by the following persons
The validity of the Flight Release Certificate must be stated and shall not exceed 14 days. If the airworthiness condition of the aircraft is changed during the period of validity, the certificate shall be re-issued. Each certificate shall be issued in duplicate, one copy must go on the aircraft, and the other retained in the aircraft’s technical records.
Any maintenance performed on the aircraft whilst operating on a Permit to Fly, with the exception of a pre-flight inspection, will require the issue of a Certificate of Release to Service.

PROCEDURE WHEN THE APPROVAL OF FLIGHT CONDITIONS IS NOT RELATED TO THE SAFETY OF THE DESIGN

Examples of flight conditions, the approval of which is not related to the safety of design are when:
The applicant must apply for approval of such flight conditions directly to the Department, using EASA (DCA) Form 37. The applicant must submit this form together with an application for an EASA Permit to Fly, EASA (DCA) Form 21, to the Safety Regulation Unit.
Establishing compliance with the conditions of an EASA Permit to fly will require either direct inspection of the aircraft by the Department or certification and issue of a Flight Release Certificate by an authorised person.
If a Flight Release Certificate is to be issued, the Standard Form SF-50 Flight Release Certificate document shall be used.
The Flight Release Certificate can only be issued by the following persons
The validity of the Flight Release Certificate must be stated and shall not exceed 14 days. If the airworthiness condition of the aircraft is changed during the period of validity, the certificate shall be re-issued. Each certificate shall be issued in duplicate, one copy must go on the aircraft, and the other retained in the aircraft’s technical records.
Any maintenance performed on the aircraft whilst operating on a Permit to Fly, with the exception of a pre-flight inspection, will require the issue of a Certificate of Release to Service.

CHANGES

Any change that invalidates the flight conditions or associated substantiation established for the Permit shall be approved by the DCA. When relevant, an application shall be made. A change affecting the content of the Permit requires the issuance of a new Permit.

OPERATIONAL REQUIREMENTS

An EASA Permit to Fly issued under EU regulations is valid in all EU member states, however national operational requirements remain applicable. Any person conducting a flight in an aircraft operating on a Permit to Fly must ensure that they comply with any operational requirements applicable to such aircraft for the airspace they are using (if any). Applicants should consult with relevant National Authorities in case of doubt.