TEST PRUEBA FAR

1. The applicant is entitled to a type certificate for an aircraft in the primary category if the aircraft: a) Weighs not more than 2,700 pounds. b) Weighs not more than 5,700 pounds. c) Has a maximum seating capacity of more than four persons, including the pilot. d) Has a pressurized cabin.

2. Standard airworthiness certificates are airworthiness certificates issued for aircraft type certificated in: a) Normal category. b) The normal, Utility, acrobatic, commuter categories and transport category. c) National transport category. d) All of the above are false.

3. Unless sooner surrendered, suspended, revoked, or a termination date is otherwise established by the FAA, airworthiness certificates are effective as follows: a) Standard airworthiness certificates, special airworthiness certificates, are effective as long as the maintenance, preventive maintenance, and alterations are performed in accordance with FAR ́s 43 and 91 and the aircraft are registered in the United States. b) A special flight permit is effective for any period of time specified by the operator. c) The aircraft conforms to a configuration determined solely by the operator. d) The aircraft has an unsafe condition and is likely to develop an unsafe condition.

4. An article that is listed on an FAA-approved Commercial Parts List included in a design approval holder's Instructions for Continued Airworthiness required by §21.50 is known as?. a) Commercial article. b) Commercial part. c) Product. d) Production approval.

5. For a new aircraft manufactured under a production certificate. An applicant for a standard airworthiness certificate for a new aircraft manufactured under a production certificate is entitled to: a) Operate an aircraft that does not conform to an approved type design. b) A standard airworthiness certificate without further showing. c) Use aircraft and surplus aircraft of the U.S. Armed Forces without notification. d) Operate the aircraft with an airworthiness certificate issued by a civil aviation authority different that the FAA.

6. A special flight permit may be issued for an aircraft that may not currently meet applicable airworthiness requirements but is capable of safe flight, if one of the following purposes is performed: a) Flying the aircraft to a base where repairs, alterations, or maintenance are to be performed, or to a point of storage. b) Conducting normal flights in any aircraft model. c) Delivering or importing the aircraft. d) Production flight testing old production aircraft.

7. If a person knows, or should know, that a replacement or modification article is reasonably likely to be installed on a typecertificated product, the person may not produce that article unless it is—. Which answer IS NOT true?. a) Produced under a type certificate. b) Produced under an FAA production approval. c) A standard part (such as a nut or bolt) manufactured in compliance with a government or established industry specification. d) Produced by an owner or operator for maintaining or altering somebody else’s product.

8. Unless an applicant shows at the time of application that his product requires a longer period of time for design, development, and testing, and the FAA approves a longer period, an application for type certification of a transport category aircraft is effective for... a) 6 years. b) 5 years. c) 4 years. d) 3 years.

9. Under FAA regulations, in which language are presented the manuals, placards, listings, and instrument markings required by the applicable airworthiness requirements?. a) English language. b) Spanish language. c) Aircraft manufacturing language. d) AAC design language.

10. The holder of a production certificate may: a) Obtain an aircraft airworthiness certificate without further showing, except that the FAA may inspect the aircraft for conformity with the type design,. b) In the case of other products, obtain approval from the FAA for installation on type-certificated aircraft. c) Issue a certificate of competency to persons successfully completing the approved training program, provided the certificate specifies the aircraft make and model to which the certificate applies. d) All answers are true.

11. An application for a type certificate is made on a ______ and in a manner prescribed by the FAA and is submitted to the appropriate aircraft certification office. a) Form. b) Invoice. c) Application. d) Order.

12. An aircraft need not meet a requirement specified in paragraph (a) of this section, as applicable, if: a) The importing country or jurisdiction accepts, in a form and manner acceptable to the FAA, a deviation from that requirement. b) The export certificate of airworthiness lists as an exception any difference between the aircraft to be exported and its type design. c) Only 1 is true. d) Both 1 and 2 are true.

13. The drawings and specifications, and a __________ of those drawings and specifications, necessary to define the configuration and the design features of the product shown to comply with the requirements of that part of this subchapter applicable to the product. a) FAA letter. b) Listing. c) Documentation. d) Order.

14. Production approval means a document issued by the FAA to a person that allows the production of a product or article in accordance with its __________ and approved quality system, and can take the form of a production certificate, a PMA, or a TSO authorization. a) Type. b) Approved design. c) Make. d) Designer.

15. Each person manufacturing aircraft engines under a type certificate must subject each engine (except rocket engines for which the manufacturer must establish a sampling technique) to a(n) ____________ run that includes the following. a) Complicated test. b) A FAA order. c) Owner Application. d) Acceptable test.

16. Each type certificate is considered to include the type design, the _______________, the certificate data sheet, the applicable regulations of this subchapter with which the FAA records compliance, and any other conditions or limitations prescribed for the product in this subchapter. a) The operating limitations. b) Invoice. c) Owner Application. d) Operation manual.

17. If a person holds the Type Certificate (TC) for a product and alters that product by introducing a major change in type design that does not require an application for a new TC under §21.19, that person must either apply to the appropriate aircraft certification office for an STC or apply to amend the __________ under subpart D of FAR part 21. a) Original data. b) Additional data. c) Original type certificate. d) According data approved.

18. Standard airworthiness certificates are airworthiness certificates issued for ____________ certificated in the normal, utility, acrobatic, commuter, or transport category, and for manned free balloons, and for aircraft designated by the FAA as special classes of aircraft. a) Aircraft Type. b) Invoice. c) Owner Application. d) Manual Operation.

19. FAR part 43 prescribes rules governing the maintenance, preventive maintenance, rebuilding, and alteration of any. a) Foreign-registered Military aircraft used in common carriage or carriage of mail. b) Aircraft having a U.S. airworthiness certificate. c) Any aircraft for which the FAA has issued an experimental certificate. d) This part applies to all life-limited parts that are removed from a non-certificated product for commercial use.

20. No person may perform maintenance, preventive maintenance, and alterations as provided in Part 65 of this chapter. Except: a) The holder of a mechanic certificate. b) The holder of a parachuting certificate. c) A person working without the supervision of a holder of a mechanic. d) The holders of a sport pilot certificate.

21. The holder of a pilot certificate issued under part 61 may perform __________on any aircraft owned or operated by that pilot which is NOT used under part 121, 129, or 135 of this chapter. a) Line maintenance. b) Major maintenance. c) Light maintenance. d) Preventive maintenance.

22. As stated in FAR 43.9, each person who maintains, performs preventive maintenance, rebuilds, or alters an aircraft, airframe, aircraft engine, propeller, appliance, or component part shall make an entry in the maintenance record of that equipment containing the following information: a) A description of work performed. b) The date of completion of the work performed. c) The name of the person performing the work. d) All of the above.

23. No person may approve for return to service any aircraft, airframe, aircraft engine, propeller, or appliance that has undergone maintenance, preventive maintenance, rebuilding, or alteration unless: a) Those operating limitations or flight data are not appropriately revised and set forth as prescribed in §91.9 of this chapter. b) The maintenance record entry required by §43.9 or §43.11, as appropriate, has been made. c) The repair or alteration form authorized by or furnished by the Administrator hasn't been executed in a manner prescribed by the Administrator. d) Changes in the operating limitations or flight data are NOT appropriately revised after a repair or an alteration that results in any change in the aircraft operating limitations or flight data contained in the approved aircraft flight manual occurs.

24. Additional performance rules for inspections (FAR 43.15). Each person performing an inspection required by FAR parts 91, 125, or 135, shall: a) Not performed the inspection in accordance with the instructions and procedures set forth in the inspection program for the aircraft being inspected. b) Perform the inspection so as to determine whether the aircraft, or portion(s) thereof under inspection, meets all applicable airworthiness requirements. c) Perform an inspection required by Part 91 on a rotorcraft without using the maintenance manual or instructions for continued airworthiness of the manufacturer. d) Not use a checklist while performing an annual or 100-hour inspection.