TEST - Module AIR 2

TEST - Module AIR 2

Trainer : Iuri BUDICI
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INSTRUCTIONS

This test is composed of 25 questions. You will have 50 minutes to answer them.

To pass the test, the minimum required is 70 %. At the end of this test, your score will appear.
At the end, a report will be sent to your manager with all the correct and incorrect answers.
Warning

Some questions may have several correct answers

Example:
ROUND shape: Choose one answer

option 1option 2option 3option 4
SQUARE shape: Choose several answers

option 1option 2option 3option 4

1. Does a standard repair need to be approved under Part 21 M ?*

A. Yes.B. No.C. Only if it is a major repair.
2. Standard repairs are defined in a document (CS-STAN) which is approved by...*

A. The European Union Aviation Safety Agency (EASA).B. The National Aviation Authority (NAA).C. The European Commission.
3. An EASA Form 1 issued in accordance with Part 21 Sub-part F needs to be signed by an inspector of the Competent Authority...*

A. Only in the case of aircraft engines.B. Only in the case of complete aircraft.C. Always.
4. Airworthiness is an aircraft's capacity to carry out its missions in acceptable safety conditions for...*

A. Passengers and crew.B. Populations flown over.C. Other airspace users.
5. Who can, under certain conditions, fabricate parts for repairs?*

A. DOA, POA and MOA.B. POA, MOA and CAMO.C. POA, MOA and CAO.
6. The life cycle of an aircraft can be represented as follows...*

A. Design – Production – Operation – Maintenance.B. Operation – Maintenance – Production -Design.C. Design – Maintenance – Production - Operation.
7. The approved production organisation shall demonstrate to the Competent Authority that it will continue to comply with Part 21 subpart G...*

A. before implementation of a significant change.B. 72 hours after implementation of a significant change.C. after implementation of a significant change.
8. An applicant for a major change to a Type Certificate (TC) who is not the TC-Holder, needs to apply in accordance with Part-21...*

A. Subpart B (Type Certificates).B. Subpart E (Supplemental Type Certificates).C. Subpart D (Changes to Type Certificates).
9. Wich of the following could be an eligible purpose for a flight under a Permit to fly :*

A. Private leisure flight with non-applied AD.B. Commercial leisure flight with overdue aircraft life limits.C. Record breaking.
10. Standard repairs can be applied to Rotorcraft...*

A. with an MTOM of 5700kg or less.B. with an MTOM of 3175 kg or less.C. Standard Repairs are only applicable to airplanes.
11. After receipt of notification of a level two finding the corrective action period granted by the Competent Authority shall be appropriate to the nature of the finding but in any case initially shall not be more than…*

A. twelve months.B. three months.C. six months.
12. CS-25 is applicable to...*

A. Aeroplanes with a MTOM greater than 2700 kg.B. Transport Aeroplanes.C. Turbine Powered Large Aeroplanes.
13. Regulation (EU) 748/2012 (Part-21) adresses...*

A. Airworthiness and Environmental Certification.B. Initial and Continuing Airworthiness.C. Initial, Continued and Continuing Airworthiness.
14. In accordance with Part 21 a restricted certificate of airworthiness shall be issued to aircraft...*

A. which conform to a restricted type-certificate issued in accordance with Part 21.B. which have been shown to comply with specific airworthiness specifications ensuring adequate safety.C. which conform to a type-certificate issued in accordance with Part 21.
15. Who can apply for an STC under Subpart E...*

A. DOA.B. ADOA.C. CP for ELA 1 or its engine/propeller.
16. Concerning all necessary airworthiness, noise, fuel venting and exhaust emissions data, the production organisation shall demonstrate that it has established a procedure to ensure that…*

A. airworthiness, noise, fuel venting and exhaust emissions data are reviewed and updated weekly.B. airworthiness, noise, fuel venting and exhaust emissions data are correctly incorporated in its production data.C. airworthiness, noise, fuel venting and exhaust emissions data are correctly revised before starting production.
17. Aircraft repair means...*

A. Replacement of parts or equipment without design activity being necessaryB. The elimination of damage and/or restoration to an airworthy condition following the initial release to service by the manufacturer of any product, part or applianceC. A list of all maintenance tasks and inspections that are required to be performed by an aircraft
18. Acceptance of an Aircraft Type Certificate performed by a State of Registry is :*

A. similar to initial type certification, but the actual amount of certification work is reduced.B. recognition and direct acceptance of the type certification already done by the State of Design.C. identical to work performed by the State of Design, but using national airworthiness codes.
19. An STC remains valid... *

A. As long as the holder continues to comply with Part 21.B. Until it’s next renewal date (3 years).C. As long as there is at least 1 aircraft in service.
20. In accordance with Part 21, when approval of the flight conditions is related to the safety of the design, the flight conditions for a Permit to fly shall be approved by:*

A. The Authority in charge of type certification of the aircraft (EASA in Europe) or a design organisation (DOA) with a corresponding privilege.B. Production organisation which manufactures this type of aircraft.C. An appropriately approved DOA or CAMO.
21. The capacity to replace the pre-modified equipment by the post-modifed equipment and vice-versa is called...*

A. Interchangeability.B. Intermixability.C. Interoperability.
22. Wich document is issued by a production organisation after maintenance of a NEW aircraft that is has produced :*

A. Form 52.B. Form 53.C. Form 27.
23. A Standard part :*

A. Needs to have an EASA Form 1.B. Has to be designated as such by the design approval holder.C. Shall be manufactured in accordance with officially recognised Standards.
24. What could justify use of Part 21 Subpart F for production activities ?*

A. Simple technology of the produced parts/aircraft.B. Lack of approved PO subcontactors.C. Small size of the production organisation.
25. An organisation can use AltMOCs on condition that they are :*

A. Sent to the competent authority.B. Approved by the accountable manager of the company.C. Approved beforehand by the competent authority.
Points
Note en %
Should be Empty: