Quiz about 1401-1500

Question 1

1402. What can an A1 licensed engineer sign for? (Level 2)

Accepted Answer

b) Minor Scheduled Line Maintenance tasks on turbine engine aircraft.

Answer

a) Minor Scheduled Line Maintenance tasks on turbine engine helicopters.

Answer

c) Minor Scheduled Line Maintenance tasks on piston engine aircraft.

Question 2

1403. Which organisation carries out the specific training required for a category A licence? (Level 2)

Accepted Answer

a) Either a VAR Part 5 or a VAR Part 9 organisation.

Answer

b) A VAR Part 9 organisation only.

Answer

c) A VAR Part 5 organisation only.

Question 3

1404. With reference to the licensing of aircraft maintenance engineers, the requirements for the issue of a licence without type rating can be found in. (Level 2)

Accepted Answer

b) VAR Part 7.

Answer

a) VAR Part 4.

Answer

c) VAR Part 5.

Question 4

1405. An AMT level A VAR Part 7 licensed engineer can certify for work carried out (Level 2)

Accepted Answer

a) By him/herself only.

Answer

b) By anyone within an approved organisation.

Answer

c) By anyone, even if they are independent of an approved organisation.

Question 5

1407. Which article of the 2006 Vietnam Civil Aviation Law regulates to protect the public interest flight safety operations within the Country? (Level 1)

Accepted Answer

a) Article 8

Answer

b) Article 4

Answer

c) Article 5

Question 6

1408. With the aircraft registered Vietnam, who is the Airworthiness Directive issuer? (Level 1)

Accepted Answer

c) CAAV

Answer

a) Aircraft owner

Answer

b) Maintenance organization

Question 7

1409. Incase natural disasters or an airport emergency, who is responsible to suspension of flight operations at airport? (Level 1)

Accepted Answer

c) CAAV

Answer

a) Aircraft operator

Answer

b) Maintenance organization

Question 8

1410. Which cases CAAV will suspend the operation of aviation staff? (Level 1)

Accepted Answer

a) Violation of regulations on aviation safety and security or obstructing air traffic activities

Answer

b) Family conflict

Answer

c) Economic lawsuit

Question 9

1411. Who is responsible to supervise of civil aviation activities? (Level 1)

Accepted Answer

b) Individual/ Organization assigned by CAAV

Answer

a) Aircraft operator

Answer

c) Maintenance Organization

Question 10

1412. Who is responsible for supervising and directing the activities of the aviation security control force? (Level 1)

Accepted Answer

c) CAAV

Answer

a) Airlines

Answer

b) Airlines and Maintenance Organization

Question 11

1413. Who is responsible for supervising the maintenance of eligibility for grant, recognition and approval of licenses, certificates, ratings and documents on specialized operations of civil aviation? (Level 1)

Accepted Answer

c) CAAV

Answer

a) Vietnamairlines and other Operators

Answer

b) Maintenance Organization

Question 12

1414. To Define requirements of organization and service that owned by State or administrated by State, which article of Law on Civil Aviation of Vietnam regulations 2006? (Level 1)

Accepted Answer

a) Article 65

Answer

b) Article 74

Answer

c) Article 75

Question 13

1415. To determine the competition level between operators, implementation the role of controlling commercial aviation operators, which article of Law on Civil Aviation of Vietnam regulations 2006? (Level 1)

Accepted Answer

c) Article 5, 12, 112

Answer

a) Article 8, 12, 112

Answer

b) Article 4, 12, 112

Question 14

1416. Which is Article of Decrees Duties of Aviation Authority 66/2015 describing regarding aviation incidents and accidents? (Level 1)

Accepted Answer

b) Article 9

Answer

a) Article 8

Answer

c) Article 10

Question 15

1417. What CS applicable to Large Aeroplanes (EASA)? (Level 1)

Accepted Answer

b) CS 25

Answer

a) CS 23

Answer

c) CS 27

Question 16

1418. What is the type certificate? (Level 1)

Accepted Answer

a) A type certificate is a type of certification document issued by an aviation regulation agency of a country for an Aircraft, Propeller and Engine.

Answer

b) A type certificate is a type of certification document issued by aircraft owner (operator).

Answer

c) A type certificate is a type of certification not mandatory for Aircraft, Propeller and Engine.

Question 17

1419. What is the certificate specification? (Level 1)

Accepted Answer

c) The certificate specification is a detailed description of the technical requirements and safety standards a product must meet to obtain a certain certification or certificate.

Answer

a) The certificate specification is a certificate only applicable to defective aircraft/ aircraft component has defect.

Answer

b) The certificate specification is a certificate only applicable to new aircraft/ aircraft component and is issued by the aircraft owner

Question 18

1420. To prevent accidents/ incidents, what types of reports will be collected and disseminated at organization? (Level 1)

Accepted Answer

a) Mandatory occurrence report

Answer

b) Delay report

Answer

c) AOG report

Question 19

1421. What does the aircraft owner need when changes the aircraft with minor/ major changes in type certificate? (Level 1)

Accepted Answer

b) Need to apply supplemental type certificate to CAAV

Answer

a) Need to apply new type certificate to CAAV

Answer

c) Need to notify to CAAV.

Question 20

1424. What Certificate of Airworthiness shall be issued by CAAV? (Level 1)

Accepted Answer

c) Standard Airworthiness Certificates; Standard Airworthiness Certificates; Export Certificate of Airworthiness

Answer

a) Standard Airworthiness Certificates; Standard Airworthiness Certificates

Answer

b) Standard Airworthiness Certificates; Export Certificate of Airworthiness

Question 21

1425. Which is responsible for approving minor changes in type design? (Level 2)

Accepted Answer

a) Approved by CAAV or DOA or accepted by CAAV

Answer

b) Approved by DOA and aircraft owner

Answer

c) Approved by CAAV and DOA

Question 22

1426. Which the organizations are allowed to request to issue type certificate? (Level 2)

Accepted Answer

c) Design Organization approved iaw Part 21

Answer

a) Approved maintenance organization.

Answer

b) Aircraft owner.

Question 23

1427. When there is a major change in type design, which organization is responsible for requesting the change of type certificate? (Level 2)

Accepted Answer

a) DOA Chapter J Part 21

Answer

b) AMO

Answer

c) Not applicable

Question 24

1428. Before operation day, how long does the application of change approval in the type design send to CAAV? (Level 2)

Accepted Answer

c) 06 months

Answer

a) 01 months

Answer

b) 03 months

Question 25

1429. Validity and effectiveness of production certificate? (Level 2)

Accepted Answer

a) 01 year

Answer

b) 02 year

Answer

c) 03 year

Question 26

1430. What is the period of validity for a temporary Certificate of Registration? (Level 2)

Accepted Answer

a) Not more than 12 months

Answer

b) Not more than 18 months

Answer

c) Not more than 24 months

Question 27

1431. How to operate EDTO with aircraft registered Vietnam? (Level 2)

Accepted Answer

b) Aircraft must be approved EDTO operations

Answer

a) Aircraft owner notifies to CAAV before each flight.

Answer

c) CAAV will accept all aircraft registered Vietnam for EDTO operations without approval.

Question 28

1432. Weather Operations: A decision height lower than 15m and runway visual range less than 175m but not less than 50m, which is classified category? (Level 2)

Accepted Answer

b) Category IIIB

Answer

a) Category IIIA

Answer

c) Category IIIC

Question 29

1433. Pitch is the nose up - nose down motion around the (Level 1)

Accepted Answer

c) Lateral axis

Answer

a) Vertical axis.

Answer

b) Longitudinal axis.

Question 30

1434. The primary flight controls are (Level 1)

Accepted Answer

b) The ailerons and roll spoiler, elevator and rudder

Answer

a) The ailerons and elevator

Answer

c) The ailerons, elevator and rudder

Question 31

1435. Way to reduce the wave drag (Level 1)

Accepted Answer

c) Use vortex generators and apply the "Area rule"

Answer

a) Use vortex generators

Answer

b) Apply the "Area rule"

Question 32

1436. The inlet design must slow the air with the weakest possible series or combination of shock waves in order to minimize the energy losses caused by temperature (Level 1)

Accepted Answer

a) Increases

Answer

b) Decreases

Answer

c) Increases or decreases depend on air speed

Question 33

1437. Which lift device increase lift 70%? (Level 1)

Accepted Answer

b) Slotted flap

Answer

a) Plain flap

Answer

c) Fowler flap

Question 34

1438. A normal shock wave takes place at Mach (Level 1)

Accepted Answer

a) 1.2

Answer

b) 2.1

Answer

c) 1.3

Question 35

1439. Forward and backward movement of the side stick is used for pitch control by (Level 1)

Accepted Answer

a) The elevators

Answer

b) The ailerons

Answer

c) The rudder

Question 36

1440. The function of the spoilers is to (Level 1)

Accepted Answer

c) Increase the drag and reduce the lift

Answer

a) Increase the drag

Answer

b) Reduce the lift

Question 37

1441. On A/C has slotted flaps, when the flaps extend the slots allow (Level 2)

Accepted Answer

a) Air from the lower side of the wing to flow to the upper side to prevent an early flow separation

Answer

b) Air from the upper side of the wing to flow to the lower side to prevent and early flow separation

Answer

c) Air from the lower side of the wing to flow to the upper side to prevent and a late flow separation

Question 38

1442. If an aircraft is flying with a left wing low, to balance the A/C, you should move the left aileron trim tab? (Level 2)

Accepted Answer

c) Up

Answer

a) Moving the aileron trim tab will not correct the situation

Answer

b) Down

Question 39

1443. On aircraft fitted with spoilers for lateral control, roll to the right is caused by. (Level 2)

Accepted Answer

b) Right spoilers extending, left spoiler remain retracted

Answer

a) Left and right spoilers extending

Answer

c) Left spoilers extending, right spoiler remain retracted

Question 40

1444. All speeds around the aircraft are below the speed of sound is called (Level 2)

Accepted Answer

a) The subsonic region

Answer

b) The transonic region

Answer

c) The supersonic region

Question 41

1445. The flaps are used in which flight phase? (Level 2)

Accepted Answer

c) Landing and Take-off

Answer

a) Landing

Answer

b) Take-off

Question 42

1447. The A/C equipped with elevons (Level 2)

Accepted Answer

a) Does not have separated aileron

Answer

b) Does not have separated rudder

Answer

c) Use as a combination of elevator and flap

Question 43

1448. In supersonic flight, (Level 2)

Accepted Answer

c) Velocity decreases, temperature increases

Answer

a) Velocity decreases, temperature decreases

Answer

b) Velocity increases, temperature increases

Question 44

1449. Which is not true about semi-monocoque structure (Level 1)

Accepted Answer

c) All the strength of the structure is carried in the outside skin.

Answer

a) The semi-monocoque fuselage is constructed primarily of the alloys of aluminium, although steel and titanium are found in areas of high temperatures.

Answer

b) The bulkheads, frames, stringers and longerons facilitate the design and construction of a streamlined fuselage, and add to the strength and rigidity of the structure.

Question 45

1450. Which part has function to transfer directly the pressure load from the skin to the frame? (Level 1)

Accepted Answer

b) Clip

Answer

a) Stringer

Answer

c) Longegron

Question 46

1451. Which process is the most important treatment for aluminium alloys (Level 1)

Accepted Answer

a) Anodizing process

Answer

b) Alodizing process

Answer

c) Cleaning process

Question 47

1452. Which one is not purpose of primer layer: (Level 2)

Accepted Answer

c) The primer has the function to protect the layers of the bare material and gives the aircraft the necessary appearance.

Answer

a) The primer increases the corrosion resistance 1properties because it contains corrosion inhibitors

Answer

b) The primer also protects the surface against corrosive agents and gives a good surface for the adhesion of the subsequent paint coatings.

Question 48

1453. Which layer is directly applied before applying top coat layer (Level 2)

Accepted Answer

b) Primer

Answer

a) Wash primer

Answer

c) Pre-treatment

Question 49

1454. Which one is true about special coatings (Level 2)

Accepted Answer

a) This is used to cover protected surfaces or to protect unprotected surfaces

Answer

b) It helps the surface is roughened which provides a good contact for paint coatings

Answer

c) The purpose is to remove all dirt, oil, fuel, fluid, dust deposits and accumulated dirt from landing gear and wheel for inspection and maintenance purposes

Question 50

1455. In some locations on an aircraft where it is not possible to reach both sides of the structure, which type of fastener must be used? (Level 2)

Accepted Answer

c) Blind rivet

Answer

a) Bolt and nut

Answer

b) Solid rivet

Question 51

1456. Which structure member carry and distribute different loads of the fuselage (Level 2)

Accepted Answer

a) Bulkhead

Answer

b) Stringer

Answer

c) Skin

Question 52

1457. What is primary structure (Level 1)

Accepted Answer

a) Primary structure is that structure which contributes significantly to carrying flight, ground and pressurization loads.

Answer

b) Primary structure is that structure which carries only air or inertial loads generated on or within the secondary structure.

Answer

c) Primary structure is that structure which contributes significantly to carrying flight and pressurization loads

Question 53

1459. How many type of aircraft fuselage construction? (Level 1)

Accepted Answer

b) 2

Answer

a) 1

Answer

c) 3

Question 54

1460. How far are frames normally spaced used in constructing the fuselage? (Level 2)

Accepted Answer

a) 20 inches

Answer

b) 22 inches

Answer

c) 24 inches

Question 55

1461. Where is the keel beam located? (Level 1)

Accepted Answer

a) Through the center wing section of the fuselage

Answer

b) Through the aft wing section of the fuselage

Answer

c) Through the mid section of the fuselage

Question 56

1462. In case of emergency, which doors can be used as emergency exit doors for a quick passenger and crew evacuation? (Level 1)

Accepted Answer

c) Main entry doors

Answer

a) Cargo doors

Answer

b) Service doors

Question 57

1463. The basic construction of the doors comprises (Level 1)

Accepted Answer

c) The door structure, the linings and the different mechanisms

Answer

a) The door structure and the different mechanisms

Answer

b) The door structure and the linings

Question 58

1464. The door structure consists of (Level 1)

Accepted Answer

b) The door frame, beams, formers and intercostals

Answer

a) The door frame, beams and intercostals

Answer

c) The door frame, formers and intercostals

Question 59

1465. The door is supported by (Level 2)

Accepted Answer

a) The support arm

Answer

b) The guide arms

Answer

c) The support arm and the guide arms

Question 60

1466. The overhead hatch provides an emergency exit for (Level 1)

Accepted Answer

b) The flight crew from the cockpit

Answer

a) The passengers from the cockpit

Answer

c) The flight crew from the cabin

Question 61

1467. To check the reservoir pressure gage? (Level 2)

Accepted Answer

a) Check permitted pressures on the pressure-temperature chart

Answer

b) Check the yellow band on the reservoir pressure gage

Answer

c) Check the green band on the reservoir pressure gage

Question 62

1468. When working around or with the reservoir or any mechanism connected to it (Level 1)

Accepted Answer

c) You must install the safety pins

Answer

a) You must install the safety caps

Answer

b) You must install the safety collars

Question 63

1469. The bulk cargo door is different from the other cargo doors; it opens? (Level 2)

Accepted Answer

a) Inwards and is operated manually

Answer

b) Outwards and is operated manually

Answer

c) Inwards and is operated electrically

Question 64

1470. On Airbus aircraft, a piano hinge connects the cargo door to the fuselage (Level 2)

Accepted Answer

b) At the top of cargo door

Answer

a) At the bottom of cargo door

Answer

c) At the center of cargo door

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