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STC - SUPPLEMENTAL TYPE CERTIFICATE

A Supplemental Type Certificate (STC) is required for any class I aeronautical product (Aircraft, Engine or Propeller) for which a major change has been made to the Type design, which is not significant enough to require a new Type Certificate.

STC- SUPPLEMENTAL TYPE CERTIFICATE

TC - TYPE CERTIFICATE

It is required for all class I aeronautical products (Aircraft, Engine or Propeller). The Type Certificate is issued by a regulatory agency and determines that the product is manufactured in accordance with an approved design and that this design ensures compliance with the required airworthiness requirements

TC - TYPE CERTIFICATE

PMA - PARTS MANUFACTURING APPROVAL

When a manufacturer does not have a Type Certificate (TC), but the products it manufactures are replacement parts that do not alter the design of the aircraft on which they are installed, a PMA can be issued. Design approval can be obtained for "similarity" by demonstrating compliance with the applicable standards. For production approval, it is necessary to demonstrate that the interested party has established a Manufacturing Inspection System that meets the requirements of the Aeronautical Authority

PMA - PARTS MANUFACTURING APPROVAL

PRODUCTION CERTIFICATE (CLASS I PRODUCTS)

Aircraft, Engines and Propellers. Companies dedicated to the manufacture of Class I products must obtain a Certificate of Production from the Aeronautical Authority. To obtain this certificate, the company must establish a Quality Control System dependent on a previously generated Quality Control Manual. In this way, the company guarantees that the Class I products it produces are in conformity with its approved Type Design.

PRODUCTION CERTIFICATE (CLASS I PRODUCTS)

PRODUCTION UNDER TYPE CERTIFICATE ONLY

When the holder of the certificate has the right to start the production "Under Type Certificate Only" with the obligation to establish, within the first six months after obtaining the TC, a "Production Inspection System" that must be "Approved" by the Aeronautical Authority.

PRODUCTION UNDER TYPE CERTIFICATE ONLY

TSOA - TECHNICAL STANDARD ORDER AUTHORIZATION

A TSO is a minimum performance standard defined for specific materials, parts and components used in civil aircraft. Receiving a TSO (TSOA) is both design and production approval; however, receiving a TSOA is not in itself an approval to install and use the product on the aircraft, but it means that the item meets the specific TSO and the applicant is authorized to manufacture it.

TSOA - TECHNICAL STANDARD ORDER AUTHORIZATION

RDA - TECHNICAL STANDARD ORDER AUTHORIZATION

When damages are found in an aircraft that are not considered in the technical documentation corresponding to the granted Certificate of Type (CT), it will require the development of a design for such repair. It is essential to determine whether it is a minor repair or a major repair. This must be determined by the TC holder, although there are exceptions where the user can classify the type of repair, which will then be validated by the Aeronautical Authority.

RDA - TECHNICAL STANDARD ORDER AUTHORIZATION

Continuous Airworthiness Management Service

We offer a complete set of services, from the Continuous Airworthiness Management (CAM) to the management of Airworthiness Review Certificates (ARC) to comply with the regulatory frameworks of each Aeronautical Authority: Argentina, Chile, Peru, Colombia, Ecuador, Panamá, etc.

We are proud of the precision and detail we apply to our records and management processes, understanding that keeping everything in order, on time, and under the regulations of the local Aeronautical Authority is translated into economic benefits for our customers.

 

 

 

 

 

• Complete technical administration of the aircraft/s.
• Monitoring and review of compliance with airworthiness regulations.
• Monitoring and review of Service Bulletins.
• Supervision: Damage Assessment, Repair Certification and to ensure that damage reports are up to date.
• Supervision: replacement of hard-time components (components with limited life).
• Supervision: replacement of serialized components.
• Production, development, amendment, control, administration, and implementation of an approved aircraft maintenance program.
• Production of reliability reports for each aircraft.
• Production, issuance, and management of base maintenance work programs and task cards in accordance with approved maintenance programs.
• Management, maintenance, and custody of aircraft technical records.
• Scanning and digitalization of technical records.
• CAM for aircraft “in storage”: storage program monitoring, production, and management of storage work packages.
• Complete management of Continuous Airworthiness.

OUR CLIENTS
barrick
Aeroptic-e1453762699103
invap
client-air_panama_bl
AAXOD
Agrisat
Sinaer

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