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Position Paper on Value of Technical Publications in the Pharmaceutical Industry
Position Paper on Value of Technical Publications in the Indian Aerospace and Defence Industry
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For the purpose of this Part, the competent authority shall be the authority designated by the Member State to whom a
person applies for the issuance of an aircraft maintenance licence.
AIRCRAFT MAINTENANCE LICENCE AEROPLANES AND HELICOPTERS
(a) This section establishes the requirements for the issue of an aircraft maintenance licence and conditions of its validity
and use, for aeroplanes and helicopters of the following categories:
— Category A
— Category B1
— Category B2
— Category C
(b) Categories A and B1 are subdivided into subcategories relative to combinations of aeroplanes, helicopters, turbine
and piston engines. The subcategories are:
— A1 and B1.1 Aeroplanes Turbine
— A2 and B1.2 Aeroplanes Piston
— A3 and B1.3 Helicopters Turbine
— A4 and B1.4 Helicopters Piston
An application for an aircraft maintenance licence or amendment to such licence shall be made on EASA Form 19 and
in a manner established by the competent authority and submitted thereto. An application for the amendment to an
aircraft maintenance licence shall be made to the competent authority that issued the aircraft maintenance licence.
An applicant for an aircraft maintenance licence shall be at least 18 years of age.
(a) Subject to compliance with paragraph (b), the following privileges shall apply:
1. A category A aircraft maintenance licence permits the holder to issue certificates of release to service following
minor scheduled line maintenance and simple defect rectification within the limits of tasks specifically endorsed
on the authorisation. The certification privileges shall be restricted to work that the licence holder has personally
performed in a Part-145 organisation.
2. A category B1 aircraft maintenance licence shall permit the holder to issue certificates of release to service
following maintenance, including aircraft structure, powerplant and mechanical and electrical systems. Replacement
of avionic line replaceable units, requiring simple tests to prove their serviceability, shall also be included in
the privileges. Category B1 shall automatically include the appropriate A subcategory.
3. A category B2 aircraft maintenance licence shall permit the holder to issue certificates of release to service
following maintenance on avionic and electrical systems.
4. A category C aircraft maintenance licence shall permit the holder to issue certificates of release to service
Bird impact damage in complex aircraft structure has been investigated using explicit transient dynamic analysis by Abaqus/Explicit in order to fully employ its large library of elements, material models and the ability of implementing user defined materials. The numerical procedure has been applied on the very detailed large airplane secondary structure consisting of sandwich, composite and metallic structural items that have been modeled with 3D, shell and continuum shell elements, coupled with appropriate kinematic constraints. Bird has been modeled using Coupled Euler Lagrangian approach, in order to avoid the numerical difficulties connected with the mesh. The impact has been applied in the area that is the most probably subjected to the impact damage during the exploitation. The application point and velocity vector have been varied and the comparisons between total, kinetic, internal and damage energies have been performed. Various failure modes, such as CFRP face layer rupture, failure of composite matrix, damage initiation / evolution in the Nomex core and elastoplastic failure of a metallic structure have been investigated. Besides, general contact has been applied as to efficiently capture the contact between impactor and structure, as well as large deformations of the different structural components. Visualization of failure modes has been performed and damaged area compared to the available references. Compared to the classic Lagrangian modeling of the bird, the analysis has proven to be more stable, and the results, such as and damage areas, physically more realistic.
, Boston University, Massachusetts, On January 25, 2011
A proposal and cost benefit analysis for a space elevator that would use carbon nanotubes to reach space and once built would be used to mine meteorites and asteroids in space for their raw materials which have value in excess of 100's of Trillions of dollars
, Boston University, Massachusetts, On January 25, 2011
What are the Cultural ramifications from Scramjet technology which allow passengers to travel from NYC to Sydney in two hours at little cost and what are the implications for mass migration patterns as travel becomes so much more easily accessible