Showing posts with label Part 145. Show all posts
Showing posts with label Part 145. Show all posts

3 August 2016

EASA Part 145 Frequently Asked Questions

EASA Part 145 Frequently Asked Questions

EASA Part 145 Frequently Asked Questions

EASA Part 145 Frequently Asked Questions

EASA Part 145 Frequently Asked Questions

EASA Part 145 Frequently Asked Questions

EASA Part 145 Frequently Asked Questions

EASA Part 145 Frequently Asked Questions

EASA Part 145 Frequently Asked Questions

Release to service of NDT tasks by part-145 organisations

Aircraft class A

Certifying staff required: The release of the works carried out on aircraft has to be performed by certifying staff holding a part-66 licence

Qualification system: Licencing of personnel has to follow part-66 regulation

General Release procedure: The release is either on the aircraft technical log or issuing an aircraft release to service statement

Release procedure for an NDT inspection:
A part-145 organisation holding an A approval rating on a particular aircraft type and having in its approved scope of work NDT inspections for this aircraft type.
This organization needs to have part-66 certifying staff and NDT personnel qualified in accordance with 145.A.30 (f).
In this case the NDT inspector performs the NDT task and signs the work order. The aircraft is released by appropriately qualified B1, B3 or C certifying staff under the organisation’s A rating.

Please note that the release  may include not only the NDT task but also the associated tasks (removal of panels, blankets, wires, re-installation, etc), or the NDT task may be part of a base maintenance check.


Engines Class B 

Certifying staff required: The release of the works carried out on engines has to be performed by engine’s certifying staff

Qualification system: The certifying staff is qualified following the procedures established by the organisation, part-66 licence is not required.

General Release procedure: The release of works performed under class B is done on an EASA form 1 (there are some exceptions for particular cases)

Release procedure for an NDT inspection:
A part-145 organisation holding a B rating approval on a particular engine type and having in its approved scope of work NDT inspections for this engine type.
This organization needs to have “engine” certifying staff (qualified in accordance with company procedures) and NDT personnel qualified in accordance with 145.A.30 (f).
In this case the NDT inspector performs the NDT task and signs the work order. The engine certifying staff releases the works performed to the engine (including NDT inspection) on an EASA form 1



Components Class C

Certifying staff required: The release of the works carried out on aircraft has to be performed by components certifying staff

Qualification system: certifying staff is qualified following the procedures established by the organisation, no need to have a part-66 licence

General Release procedure: The release of works performed under class C is done on an EASA form 1 (there are some exceptions for particular cases)

Release procedure for an NDT inspection:
A part-145 organisation holding a C rating approval on a particular component and having in its approved scope of work NDT inspections for this component.
This organization needs to have “component” certifying staff (qualified in accordance with company procedures) and NDT personnel qualified in accordance with 145.A.30 (f).
In this case the NDT inspector performs the NDT task and signs the Work Order / Engineering Order. The component certifying staff releases the works performed to the component (including NDT inspection) on an EASA form 1



Specialised services Class D

Certifying staff required: The release of the works carried out on aircraft has to be performed by “specialised services” certifying staff

Qualification system: The certifying staff is qualified following the procedures established by the organisation in compliance with EN4179, part-66 licence is not required.

General Release procedure: The release of works performed under class D rating is done on an EASA Form 1 or on a format defined by the organisation in the MOE in compliance with 145.A.50 and approved by the competent authority.

Release procedure for an NDT inspection:
A part-145 organisation holding an D approval on a particular NDT method. The approved scope of work will be NDT inspections on this method.
This organisation needs to have NDT certifying staff qualified in accordance with 145.A.30 (f).
In this case the NDT certifying staff performs and releases the NDT task on an EASA Form 1 or on a release to service document defined by the organisation in the MOE in compliance with 145.A.50 and approved by the competent authority

What are the training requirements for personnel within a Part-145 organisation, other than those contained in Part-66?


The accountable manager shall demonstrate a basic understanding of Part-145.
145.A.30(a) point 3


.
The person or group of persons nominated responsible for ensuring that the organisation complies with Part-145 (including the Quality Manager) shall be able to demonstrate

  • relevant knowledge, background and satisfactory experience related to aircraft or components maintenance as applicable,
  • a working knowledge of Part-145,

145.A.30(b) point 3.


The organisation shall establish and control the competence of personnel involved in any maintenance, management and/or quality audits in accordance with a procedure and to a standard agreed by the competent authority.
In addition to the necessary expertise related to the job function, competence must include an understanding of the application of human factors and human performance issues appropriate to that person's function in the organisation.
This should include also:

  • Fuel Tank Safety training (Appendix IV to AMC 145.A.30(e) and 145.B.10(3)).
  • EWIS training (AMC 20-22)

145.A.30(e) and associated AMC/GM.
Appendix IV to AMC 145.A.30(e) and 145.B.10(3).
AMC 20-22.



The organisation shall ensure that personnel who carry out and/or control a continued airworthiness non-destructive test of aircraft structures and/or components are appropriately qualified for the particular non-destructive test in accordance with the European or equivalent Standard recognised by the Agency.
Personnel who carry out any other specialised task shall be appropriately qualified in accordance with officially recognised Standards.
By derogation to this paragraph those personnel specified in paragraphs (g) and (h)(1) and (h)(2), qualified in category B1 or B3 in accordance with Annex III (Part-66) may carry out and/or control colour contrast dye penetrant tests.
145.A.30(f) and AMC 145.A.30(f).



 By derogation to paragraphs (g) and (h), in relation to the obligation to comply with Annex III (Part-66), the organisation may use certifying staff qualified in accordance with the following provisions:


  1. For organisation facilities located outside the Community territory certifying staff may be qualified in accordance with the national aviation regulations of the State in which the organisation facility is registered subject to the conditions specified in Appendix IV to this Part.
  2. For line maintenance carried out at a line station of an organisation which is located outside the Community territory, the certifying staff may be qualified in accordance with the national aviation regulations of the State in which the line station is based, subject to the conditions specified in Appendix IV to this Part.
  3. For a repetitive pre-flight airworthiness directive which specifically states that the flight crew may carry out such airworthiness directive, the organisation may issue a limited certification authorisation to the aircraft commander and/or the flight engineer on the basis of the flight crew licence held. However, the organisation shall ensure thatsufficient practical training has been carried out to ensure that such aircraft commander or flight engineer can accomplish the airworthiness directive to the required standard.
  4. In the case of aircraft operating away from a supported location the organisation may issue a limited certification authorisation to the commander and/or the flight engineer on the basis of the flight crew licence held subject to being satisfied that sufficient practical training has been carried out to ensure that the commander or flight engineer can accomplish the specified task to the required standard. The provisions of this paragraph shall be detailed in an exposition procedure.
  5. In the following unforeseen cases, where an aircraft is grounded at a location other than the main base where no appropriate certifying staff are available, the organisation contracted to provide maintenance support may issue a one-off certification authorisation:

               (i)     to one of its employees holding equivalent type authorisations on aircraft of similar technology, construction and systems; or
               (ii)    to any person with not less than five years maintenance experience and holding a valid ICAO aircraft maintenance licence rated for the aircraft type requiring certification provided there is no organisation appropriately approved under this Part at that location and the contracted organisation obtains and holds on file evidence of the experience and the licence of that person.
      All such cases as specified in this subparagraph shall be reported to the competent authority within seven days of the issuance of such certification authorisation. The organisation issuing the one-off authorisation shall ensure that any such maintenance that could affect flight safety is re-checked by an appropriately approved organisation.

145.A.30(j) and associated AMC/GM.

Appendix IV to Part-145.
In addition to the appropriate requirements of 145.A.30(g) and (h), the organisation shall ensure that certifying staff and support staff have an adequate understanding of the relevant aircraft and/or components to be maintained together with the associated organisation procedures. In the case of certifying staff, this shall be accomplished before the issue or re-issue of the certification authorisation.
145.A.35(a) and AMC 145.A.35(a).


The organisation shall ensure that all certifying staff and support staff are involved in at least six months of actual relevant aircraft or component maintenance experience in any consecutive two year period.
145.A.35(c) and AMC 145.A.35(c).


The organisation shall ensure that all certifying staff and support staff receive sufficient continuation training in each two year period to ensure that such staff have up-to-date knowledge of relevant technology, organisation procedures and human factor issues.
145.A.35(d) and AMC 145.A.35(d).


The organisation shall establish a programme for continuation training for certifying staff and support staff, including a procedure to ensure compliance with the relevant paragraphs of 145.A.35 as the basis for issuing certification authorisations under this Part to certifying staff, and a procedure to ensure compliance with Part 66.
145.A.35(e) and AMC 145.A.35(e).


Except where any of the unforeseen cases of 145.A.30(j)(5) apply, the organisation shall assess all prospective certifying staff for their competence, qualification and capability to carry out their intended certifying duties in accordance with a procedure as specified in the exposition prior to the issue or re-issue of a certification authorisation under this Part.
145.A.35(f) and AMC 145.A.35(f).


The holder of a category A aircraft maintenance licence may only exercise certification privileges on a specific aircraft type following the satisfactory completion of the relevant category A aircraft task training carried out by an organisation appropriately approved in accordance with Annex II (Part-145) or Annex IV (Part-147). This training shall include practical hands on training and theoretical training as appropriate for each task authorised. Satisfactory completion of training shall be demonstrated by an examination or by workplace assessment carried out by the organisation.
145.A.35(n) and AMC 145.A.35(n).


The holder of a category B2 aircraft maintenance licence may only exercise the certification privileges described in point 66.A.20(a)(3)(ii) of Annex III (Part-66) following the satisfactory completion of (i) the relevant category A aircraft task training and (ii) six months of documented practical experience covering the scope of the authorisation that will be issued. The task training shall include practical hands on training and theoretical training as appropriate for each task authorised. Satisfactory completion of training shall be demonstrated by an examination or by workplace assessment. Task training and examination/assessment shall be carried out by the maintenance organisation issuing the certifying staff authorisation. The practical experience shall be also obtained within such maintenance organisation.
145.A.35(o) and AMC 145.A.35(o).


Pre-flight inspections (when the 145 organisation has an agreement with an operator)
It should be demonstrated that the personnel carrying out pre-flight inspections have received appropriate training for the relevant pre-flight inspection tasks based on the operator’s CAME.
AMC M.A.301-1

24 November 2015

EASA Part-145 Valid MRO-Maintenance Organisation List

FOREIGN EASA PART-145 VALID APPROVALS
LIST OF NON-BILATERAL EASA PART-145 APPROVED ORGANISATIONS,2015


COUNTRY EASA CERT NR COMPANY NAME 

24 March 2014

EASA Part 66 Category B2 Aircraft Type Training Syllabus


ATA ref. Licence
cat B2
Level

EASA Part 66 PRACTICAL TRAINING MATRIX


PRACTICAL TRAINING MATRIX
ATA REF TYPE TRAINING SUBJECTS
INTRODUCTION
6 Dımensıons And Areas 
5 Tıme Lımıts - Maıntenance Checks 
7 Lıftıng And Shorıng

Basic Maintenance Experience Logbook For EASA Part 66 license

General:

This document has been developed by Civil Aviation Authority to assist applicant to comply with Commission
regulation (EC) No 2042/2003 by record his/her basic practical maintenance experience.

18 March 2014

What does ‘Certifying Staff’ mean?

Personnel responsible for  the release of an aircraft or a component after maintenance.








What does’Line Maintenance’ mean?

Any maintenance that is carried out before flight to 
ensure that the aircraft is fit for the inetended flight.