Read the following sentences and cross a, b, c or d that corresponds to the appropriate answer :
1. The main body of the aircraft is called : C
A. the frame
B. the gear C.the fuselage D. the flight deck
2. The ..................... are control surfaces : B
A. wheels B. flaps C. windshield D. hold
3. The .......................... is the fixed part of the vertical stabilizer : B
A. fin B. rudDER C. elevato D. slats
4. The landing gear is composed of : B
A. spoilers B. strut C. nose D. aerials
5. The windscreen is also called the : A
A. windshield B. wipers C. dents D. scratches
6. The door is ...........................
A. flashing B. full C. flus D. dim
7. The safety pin is ........................... D
A. unlocked B. safe C. cold D. inserted
8. The ground is ............................. A
A. wet B. empty C. row D. explosive
9. The lights are ................................. B MOUCHI3
A. rough B. bright C. empty D. loose
10. The electrical circuit is ................................... C
A. protruding B. stea C. de-energized D. extended
11. A hose is .............................. C
A. flexible B. porous C. rigid D. smooth
12. The tank is ..................................... B
A) A. worse B. empty C. shiny D. soft
13. Use emery paper if the surface is ...........................................
A. matt B. dirty C. rough D. warm
14. The pressure is ................................... B
A. slow B. low C. full D. loose
15. Do not touch the generator before they are ................................... B
A. hot B. cool C. soft D. clean
16. Work .......................... a temperature of 20°C B
A) A. on B. at C. off D. in
17. Remove bolts ......................... the flange C
A. to B. on C. from D. of
18. Adjust pressure ....................... 44 1 psi A
A. to B. in C. on D. at
19. Keep all the equipment ......................... from the battery C
A. back B. around C. away D. off
20. Cut the shrinkable sleeve .............................. lengthC
A. at B. to C. in D. over
21. Make sure the reading on the gage is .................. these limits B
A. along B. within C. behind D. over
22. Enclose parts ........................ polythene bags C
A. on B. of C. in D. withi
23. Put the aircraft ........................... to its initial configuration B
A. behind B. back C. below D. at
24. Air is ducted to both ......................... of the airplane C
A. edges B. tips C. sides D. boarders
25. The flange ...................... attachment for the shaft C
A. supplies B. gives C. provides D. assembles
26. The rotation speed is ........................... by a sensor D
A) A. controlled B. caused C. increased D.monitored
27. The fasteners ...................... quick removal and installation A
A) A. allow B. bond C. disconnect D. latch
28. The assembly ......................... eight parts D
A) A. complies with B. displays C. bring D. consists of
29. ............................. the leading edge B
A. test B. examine C. improve D. point
30. ............................. the fault continues, replace the control and monitoring unit B
A. due to B. if C. so D. when
31. The control handle is pushed in ...................... the valve B
A) A. closing B. by closing C. so closing D. thus
32. The fault confirmation is not necessary ................ GEN 2 was set to off B
A) A. because of B. as C. in order to D. so
33. Do the test ........................ the fault isolation manual B
A) A. despite B. according to C. until D. within
34. Insert the safety pin ......................... prevent slide deployment A
A) A. to B. for C. as to D. in order
35. Monitor the pressure gage ......................... recharging the cylinder C
A) A. whereas B. during C. while D. when
36. The A320 is a short-haul narrow-body ................... the B747 is a long-haul wide-body B
A. whether B. whereas C. when D. so as
37. Fill the tank ...................... the high level is reached B
A. unless B. until C. despite D. if
38. The disc pops out ............................. relieve pressure A
A. so as to B. thus C. because D. whereas
39. The test can be performed ....................... an EXT PWR source is connected B
A. as well as B. although C. provided D. though
40. The dust cover ........................ by two quarter-turn foasteners C
A. attach B. is attaching C. is attached D. will attach
41. Use the guides ........................ make sure that the two plates are aligned D
A. unless B. because C. whatever D. in order to
42. The main assembly ...................... a chassis, a frame, the board and three modules B
A.supplies B. consists of C. feeds D. installs
43. Measure the ....................... between the two edges D
A. housing B. shaft C. shim D. gap ( fajwa)
44. Apply a thin ............................. of sealant to the screw heads C
A. cap B. level C. coating D. length
45. Electrical supply is ........................ by the control unit A
A. monitored B. held C. translated D. driven
46. ........................... the starter when the shaft is turning can cause damage C
A. disengage B. disengage C. disengaging D. to disengage
47. The unit ..................... automatically to the standby mode A
A. switch B. switching C. to switch D. switches
48. Compare two indications is to ............................. B
A. cross – check B. readjust C. inspect D. to overlook
49. The bleed valve enables one engine to supply .................... wings B
A. one B. both C. none D. either
50. Two budsbars are ............................. together A
A. connected B. linked C. attached D. put
