1. CAR Section 2, Series F , Part V deals with:1.Renewal of Certificate of Airworthiness.2. Suspension of C. of A. & its Subsequent revalidation.3. Special Flight Permits. 4. Continue Airworthiness Maint. Programme

2. Which Part of Series F deals with Suspension of C. of A. & its subsequent revalidation:1. IV 2. V3. VI 4.VII

3. The Automatic suspension of C. of A., is provided by Rule:1. 55 (2) 2 55 (3)3. 55 (1) 4. 56 (1).

4. Which of the following Rule empower the DOCA to suspend/Cancel C. of A.:I. 51 (l) 2. 53(2)3. 54 (2) 4. 55(2)

5. DGCA can cancel the C. of A. or suspend whenever reasonable doubt exist to:1. A particular aircraft. 2. All types of Aircraft.3. I & 2 both are correct. 4. None of the above

6. The C. of A. cancelled of aircraft by DGCA. if:1. Aircraft cease or fail to conform conditions stipulated in Type Certificate.2. It is modified/repaired otherwise then in approved procedure.3. Suffer major/substantial damage (require extensive repair of major component)4. All the above.

7. It is the responsibility of operator to inform what authority when aircraft suffer majordamage or defect:1. DGCA. 2. RAO/Sub-RAO3. Q.C.M. 4. All above are correct..

8. The information to RAO by operator about major damage will contains information:1. Extent of damage. 2. Nature of defect.3. Circumstances which caused the damage. 4. All the above.

9. The suspended C. of A.:1. Will be revalidated up to the date of the previous currency of C of A had remain valid,if it had not been suspended. 2. Will be revalidated for another year.3. Can not revalidated 4. None of the above,

10. As condition for revalidation of C. of A., the Airworthiness Officer requires aircraft/aircraft component modified, repaired, replaced under supervision of:I. R.A.O. 2. A.M.E./Authorized Person3. Quality Control Manager 4. Inspector Incharge.

11. The owner/operator submit aircraft for Inspection, during Repair, Modification & Overhaul to:1. DGCA 2. Approved Organisation

3. Airworthiness Officer, 4. Q.C.M.

12. Suspended C of A can revalidated for One year after completion of Modification, Repair,Maintenance:1. When Modification, repair carried out by an AMO under supervision of DGCA2. Only if additional work is carried pout with renewal of C. of A. referred ion CARseries F Part IV.3. 1 & 2 both are correct. 4. None of the above.13. CAR Sec .II Series F Part. VI deals with:I. Continuous Airworthiness Maintenance programme.2. Airworthiness of Ageing Aircraft. 3. Inspection of Wooden aircraft.4. Rebuilding of Aircraft.

14. The requirement regarding use of materials to be used during manufacturing of aircraftare prescribed in Rule:1. 50 and 50 A. 2. 51 &51 A.3. 52and52A. 4. 53&53A.

15. Which Rule empower DGCA to issue/renew or revalidate C of A:1. 50. 2. 51, 3. 52. 4. 54.

16. CAR Series F Part VI laid down requirements for rebuilding of Aircraft:1. Which was damaged 2. Purchased as wreckage from Insurance companies.3. Purchased Parts/Spares from abroad. 4. All the above.

17. What type of aircraft will permit to rebuilt:I. Which were earlier type certified & flown with C of A.2. Have sufficient data regarding maintenance, performance standard.3. 1 & 2 both are correct. 4. Have special permission from DGCA.

18. CAR Series F covers the aircraft for rebuilding:1. Unpressurised with AUW 3000 kgs. & below.2. Unpressurised with AUW more than 3000 kgs.3. 1 & 2 both 4. Unpressurised aircraft having AUW less than 5700 kgs.

19. The owner/person apply to DGCA through RAO for registration of Rebuild the aircraftwill submit:1. Survey report indicating detail of parts 2. Fees.3. Details of source of procurement of parts. 4. All the above.

20. Upon receipt pf application & all documents for registration of Rebuilt the aircraft.The RAO will issue a:1. Certificate of Registration for One year. 2. Temporary C of R. for one year.3. Special Registration for One year. 4. None of the above.

21. The temporary C. of R. can be extended, in some exceptional cases, for a period of:1. 18 months. 2. Two years,3. Three years 4. an not extended.

22. Permanent registration of rebuilt aircraft will allowed only when constructor forwards acertificate duly certified by:I. AME having licence endorsed in Cat. C.2. AME having licence endorsed in Cat. D.3. AME having licence endorsed in Cat. B.4. AME having licence endorsed in Cat. X.

23. Each rebuilt aircraft will have to be assigned a serial number by Constructor which isnormally assigned on:I. Wings. 2. Fuselage.3. Identification Plate. 4. None of the above.

24. The constructor, before assembling, the aircraft must ensure that:I. Parts purchased are genuine 2. Proper history of the parts.3. The fuselage has dc-registered from the country in which it was previously registered.4. All the above.

25. The aircraft parts used for rebuilding should be strip inspected/overhauled whichare stored:1. More than 5 years. 2. More than 6 years3. More than 7 years. 4. More than 8 years.

26. The Fuselage imported from outside the country used for rebuilding of aircraft should have:1. Proper history. 2. Export C of A.3. 1 & 2 both 4. Certificate given by RAO.

27. The Test Flight of Rebuild aircraft carried out b y:1. Pilot having PPL. 2. Pilot having CPL3. Pilot in Command 4. Chief Instructor of Flight.

28. In case original aircraft was issued with an approved Flight Manual, the constructor will produce a copy of the same & procedure evidence of that, it is updated to:1. DGCA 2. Q.C.M.3. R A O. 4. Pilot in Command.

29. The DGCA will refuse to issue of C. of A. & C opfR, if owner/constructor not able toproduce:1. Sufficient evidence regarding genuineness of Parts.2. Use of correct assembling Techniques.3. 1 & 2 both 4. Approved Flight Manual.

30. CAR Series F Part VII deals with:1. Special Flight Permits. 2. Inspection of wooden Aircraft.3. Approval of flight Manual & their Amendments4. Continue Airworthiness Maintenance Programme.

31. No person can not operate the aircraft possessing suspended C. of A., stated by Rule:1. 59 Sub Rule 3. 2. 57 Sub Rule 33. 56 Sub Rule III 4. 55 Sub Rule III.

32. Issue of a Special Flight permit to an Aircraft with a suspended C. of A. in light of:1. Sub Rule IV of 55. 2. Sub Rule 3 of 553. Sub Rule II of 55. 4. Sub Rule 1 of 55.

33. Special Flight Permit are given when:1. It is essential for aircraft top dispatch to base for Mod./Inspection/AD are to be performed.2. When aircraft have to flown for experimental/Test Flight.3. If aircraft is otherwise safe to conduct intended operation.4. All the above.

34. Special permits are not required in case of Test Flight for Renewal of C. of A. & if C. of A. is expired, AME after appropriate maintenance task & test Release a:1. Certificate of Maintenance for Test Flight.2. Temporary C. of A. for Test Flight.3. Certificate of Fitness for Test Flight.4. None of the above.

35. For what purpose the special Flight permits are given:1. Test Flying a production aircraft. 2. Flight for special purpose3. Evacuation of aircraft opr passengers from area impending danger. 4. All the above.36. For special Flight permit the owner/operator shall have to sub mit:1. An applicatyion as per Annexure A. 2. An application as per Annexure B.3. An application as per Annexure C. 4. An application as per Annexure D.37. The Application of Special Flight permit shall concurred & signed by:1. Engineering & Operational deptt. of operator.2. Engineering & operational Deptt. of A.M.O.3. Engineering & Operational deptt. of ICAO.4. Engineering & Operational deptt. of Airworthiness Office.

38. The Report sent along with an application for Special Flight Perm it to RAO will consistsinformation:I. Detailed condition of aircraft. 2. Steps taken for its safety.3. 1 & 2 both 4. Age of aircraft.

39. In case aircraft sustains damage/defect outside of country the application for ferry flight shall be submit to:I. Office of main station. 2. Office where aircraft is based.3. l&2both 4. DGCA.

40. As for as possible the initial; climb should not be over:1. Sea 2. Thickly populated area.3. Outside country 4. Poles.

41. A copy of special flight permit must be carried:

1. On board the aircraft. 2. In maintenance system.3. In Flight manual. 4. In organisation.

42. Who is responsible to ensure the safe flight for intended operation:I. A.M.E. 2. RAO3. Owner/Operator 4. A.M.O.

43. Special flight permit is valid till:I. For One year 2. Six months3. Arrival of aircraft at destination or specific date 4. One day.

44. After reaching aircraft at base the operator shall submit a copy of report, to authority who hadissued Special Flight Permit, will contains information:I. Any abnormality encountered during flight.2. Action taken at base to render aircraft airworthy.3. Result of Test Flight & any other information deemed necessary.4. All the above.

45. The application of Special Flight Permit will be signed by:I. Chief Engineer 2. Chief of Operations3. Q.C.M. 4. All the above.

46. CAR Series F Part VIII deals with:1. General Requirements regarding Maintenance & Certificate of Aircraft.2. Rebuilding of Aircraft. 3. Special Flight Permits.4. Suspension/Revalidation of C. of A.

47. Indian Registered aircraft5 before undertake any flight have to possess a current & validCertificate of Airworthiness in the light of:I. Rule 13 2. Rule 14.3. Rule 15. 4. Rule 16.48. D.G.C.A in respect of any ale, a/c component item of equipment specify standardsand conditions for its maintenance, in accordance withSub rule(1) of rule 60 2 Sub rule (2) of rule 603 Sub rule(3) of rule 60 4 Sub rule(a) of rule 60

49. According to series F part VII it is therefore obligatory that1. A/c maintenance as per approved maintenance schedule2. No. unapproved mod. Or repair carried out3. Maintenance and major maintenance shall carried out and certified by appropriately Licensed A.M.E4. All of above

50. Approved Pilot means pilot to carry out transmit/layover inspection without authority of invoking MEL item/snag rectification shall be approved by1 D.G.C.A 2 RAO3 QCM 4 Airworthiness officers of D.G.C.A.

51. An approved pilot should posses

1 Valid Licence with specific entrustment of type of a/c2 Have trained for 10 days by A.M.E3 Have checked by board formed by organization4 All of above

52. Certificate of flight release is valid for1 day 2 1 Week3 1 Month 1 4 Period specified in it

53. The scheduled airline as required to have their own maintenance facility as required by1. CAR sec 4 series C part II 2. CAR sec3 series C part II3. CAR sec2 series C part II 4. Car sec I series C part II

54. The contents of routine maintenance and inspection schedule including special inspection schedule, overhaul schedule of component and a/c operated by operator have minimum experience as scheduled operator1. 2year 2 3year3. 5year 4 l0year

55. The MPD (maintenance planning document) should submit for its approval to1. RAO/sub RAO 2. QCM3 D.G.C.A 4 AMO

56. Special inspection schedules of a/c such as heavy landing ,post lightning strike post propeller strike prepared by operator and approved byI. D.G.C.A. 2 .A.M.E3. Manufacturer 4 QCM

57. From approved schedule1. No item can be deleted with prior approval of D.G.C.A2. But addition to schedule may effected3. Both a & b4. The schedule once approved there will no change in that

58. The maintenance work carried out on a/c shall be certifiedI. In relevant log book 2. In a/c register3. In A/C manual 4. In maintenance system manual

59. The maintenance work recorded and signed and dated in relevant log book with in1. 24 Hours 2. 48 Hours3. 72 Hours 4. 96 Hours60. If the log book not available one copy of log book entry should be kept in1. Aircraft log book 2. MEL3. Journey log book 4. Radio log book

61. Certificate of flight release is given by1. A.M.E. 2. RAO3. D.G.C.A. 4. AMO

62. The issuance of FRC will implies that al maintenance work is concerned out in approvedmanner and alc is safe for flight provided1. All approved lower inspection schedule carried out2. A/C is satisfactory loaded3. Both a & b4. A/C have sufficient crew

63. The FRC in respect of a/c categorized as passenger! mail cargo operating schedule Airtransport service1. The validity of FRC shall approved by D.G.C.A.2. Certification of inspection shall be carried out by AME/ attendant person3. Both a & b4. Specially inspected by AMO

64. For a/c seating configuration up to 19 when away from base with maximum payload capacity2 tones inspected without snag rectification byI. Basic licensed holder approved 2. An approved Pilot3. AMO 4. Both a & b

65. The transmit inspection of a1c having passenger seating capacity more than 19 and withpayload capacity more than two tons away from base by1. An AME! approved person 2. Basic licence holder3. Approved pilot 4. All of above

66. The transmit inspection without snag rectification of turbo prop a/c having passenger seatingcapacity up to 75 with maximum payload 5 tons by when a/c away from baseI. Approved licensed person 2. Approved Pilot3. l3otha&b 4. AMO

67. A/C having MTOW more than 5700 Kg a/c categories in mail/cargo non scheduled Category with more than 19 seats or payload capacity more than 2 tons1. Validity of FRC by D.G.C.A.2. Certificate of inspection higher than transmit inspection will be by AME specially approve person3. Transmit inspection without snag rectification will by approved basic licence holder when a/c away from base4. All of above

68. A/C have MTOW up to 5700 Kg or have passenger configuration up to 19maximum payload weight 2 tons validity of CFR1. 30 Days 2. 50 Hrs./30 days which ever earlier3. 100 Hrs./3 Months which ever is earlier 4. 2 Months.

69. For aircraft operated by flying club and gliding club the FRC valid by:1. 24Hrs. 2. 48Hrs.3. 36 Hrs. 4. One week.70. Aircraft belonging to aerial work Category FRC issued by AME after every:1. 5 Hrs. /5 Days 2. 10 Hrs./7 Days

3. 20 Hrs / 7 Days 4. 25 Hrs./30 Days

71. Aircraft from regular aerodromes shall FRC to aerial work category issue every 50Hrs./30 Days if that subject to carry out inspection of:1. 25 Hrs./l5Days 2. 50 Hrs.130 Days3. 100 Hrs./3 Months 4. 200 Hrs.16 Months.

72. Aircraft seating capacity more than 19 in private category:1. Validity of FRC by DGCA 2. Transmit inspection by approved basic Licence if aircraft is away from base.3. Lay over inspection by AME 4. All of the above.

73. In case of diversionary landing where AME/approved person not available. The inspection with snag rectification will be carried out by:1. Pilot in command 2. Flight engineer3. Both 1 and 2 4. Crew members.

74. The certification of air born racks equipment carried out every 90 days elapsed time forcategory:1. All aircraft in private 2. All aerial work in aircraft3. Aircraft operated by flying club V 4. All of the above.

75. For aircraft equipped with communication equipment only certification will carried outafter every:1. Every 30 Days 2. 100 Days3. 180 Days 4. 6 Months.

76. The certification to radio equipment will be cancel if:1. Aircraft flown through electric storm since last inspection2. Operation of equipment is not properly work before flight3. Report observed defect of such natured rectified by AME4. All the above.

77. The FRC for radio should be used with every FRC for airframe and engine:I. Second 2. Third3. Fourth 4. Fifth

78. A basic Licence holder Should possess for approval:1. Three months on specific type aircraft2. Ten day course on engine and airframe3. Seven day relevant inspection under AME and certificate of it by QCM and passed oral cum practical by RAO.4. All the above.

79. The approval shall be valid for:1. One year 2. Two year3. Three year 4. Four years

80. The approved person for renewal of apprand should have:

1. Exercise privileges for three months during one year2. Exercise privileges for nine months during one year3. Exercise privileges for six months during one year4. Exercise privileges for one months during one year.

81. Record of FRC minimum preserved for period of:1. Three months 2. Six months3. Nine months 4. 12 Months.82. The form for certificate of maintenance will have:1. Signature of AME/approved person with Licence No. and approved No.2. Firm’s name3. Date and place of issue4. All the above.

83. The continuous aircraft maintenance program is documented in:1. Flight manual 2. Operation manual3. Maintenance system manual 4. all the above.

84. The maintenance program is sent for approval to the:1. DGCA 2. Manufacturer3. RAO/Sub.RAO 4. QCM.

85. Any alteration in the approved scheduled in concerned with:1. DGCA 2. Manufacturer3. RAO 4 .QCM.

86. The SSIP and CPCP are given or made by the:1. QCM 2. Operator3. Manufacturer 4. RAO

87. All completed maintenance schedule must be preserved for a minimum period of:1. 6 months from the date of final certification of such schedule2. 2 months from the date of final certification of such schedule3. 1 month from the date of final certification of such schedule4. As Suggested by QCM.

89. The subject airworthiness of ageing aircraft is related with:1. Series E, Part-IX 2. Series F, Part-XI3. Series F, Part-X 4. Series E, Part-VI

90. Design economic life of an aircraft is given by the:1. QCM 2. Operator3. Manufacturer 4. Regularity authority of country.

91. A damage caused to a metal structure characterized by initiation of the crack subsequentpropagation and as a result of continuous process whose effect is cumulative with respectof aircraft usage is term as:1. Accidental damage 2. Environmental damage

3. Fatigue damage 4. Multiple site damage.

92. Test flight of aged aircraft is carried out every/any:1. Any time as required by DGCA 2. Six months3. Both 1 and 2 4. One year.

93. All major defects should be reported to DGCA:I. Every month 2. With in 12 Hrs.3. Promptly 4. After rectification.

94. Design economic life for airbus is:1. 25 Years 2. 15 Years.3. 20 Years 4. None of the above.

95. In duplicate inspection, first inspection is carried out on the aircraft for flying controls by:1. Any person 2. Trainee technician3. AME in category A/B 4. None of the above.

96. The subject inspection of wooden aircraft is resisted with:1. Series D, Part-Ill 2. Series D, Part —IV3. Series F, Part-XII 4. Series F, Part-XIII.

Series —‘F’ Part-IX, X, XI, XII

97. Schedule maintenance includes the following work:1. Replacement of life limited items2. Heavy landing schedule3. Lighting strike schedule4. All are correct.

98. Unscheduled maintenance includes the following work1. Special inspections such as X-rays.2. Replacement of ‘lifed’ components3. Heavy landing schedule4. All are correct.

99. Ageing aircraft require more frequent inspection of structural components for damagedue to:1. Environmental deterioration. 2. Accidental damage3. Fatigue 4. All are correct.

100. To ensure structural integrity of ageing aircraft, manufactures have issued:1. SSIP 2. CPCP3. Both 1 and 2 are correct 4. None of the above.

101. The owner/operator shall inform RAO/sub-RAO in writing at least 15 days in advanceabout the commencement of the entire inspection schedule:1. Of 100 Hrs. and above 2. Of over elOO Hrs.

3. Of over 300 Hrs. 4. All are correct.

102. Regional airworthiness officer may grant ad-hoc extension to lives of inspectionschedules and TBOs of components up to a maximum of or1. 10%, 50 Hrs. 2. 3%, 3 Months3. 3%, 50 Hrs. 4. None of the above.

103. All completed maintenance schedules must be preserved for a minimum period ofyears:1. One 2. two 3. Five 4. Ten.

104. Damage due to environment in the form of corrosion and stress corrosion is:1. Environment damage 2. Corrosion damage3. Fatigue damage 4. Accidental damage.

105. Ageing aircraft are these, which have completed there:1. Technical life 2. Service life3. Designed service life 4. Designed economic life.

106. Multiple site damage is:1. Five or more dents on one site.2. Five or more crakes on one site which lick up into a longer crack.3. Fatigue crack at number of fasteners, which stand to link up into longer cracks.4. All are correct.

107. Damage to an aircraft can be termed as accident damage if it is caused due to:1. Environmental factors like corrosion2. One aircraft hitting another aircraft3. Wrong handling of ground equipment during routing inspection4. None of the above.108. Duplicate inspection when aircraft is away from base is carried out by:1. Any CPL holder2. Flight engineer whose Licence is endorsed for the aircraft3. Specially authorized person4. Both l and 2 are correct.

109. If control systems are disturbed after the second check, but before first flight.I. Disturbed portion should be checked in duplicate again2. Distorted portion should be checked by second person only3. Complete portion should be checked by second4. Complete portion should be checked in duplicate again.

110. Series F Part-XII deals with:1. Inspection of wooden aircraft2. Duplicate inspection of flying controls3. Duplicate inspection of engine controls4. Both 2 and 3 are correct.

111. Aircraft of composite construction shall be inspected before issue/renewal or validationof C of A and thereafter every year1. One 2. Two 3. Five 4. Ten.112. Factor causing wood deterioration is:1. Chemical action of glue due to ageing2. Mechanical forces mainly due to timber shrinkage3. Growth of fungus4. All are correct.

113. Wooden aircraft exposed to large cyclic changes of temperature and humidity areespecially prone to:1. Timber shrinkage 2. Glue deterioration3. Both A and B are correct 4. None of the above.

114. Weather proofing quality of fabric covering is affected by:1. Long exposure to inclement weather conditions.2. Exposure to strong sunlight3. Atmosphere air4. Both 1 and 2 are correct.

115. In wooden structures, old screws are usually replaced with new screws of:1. Identical length2. Identical length but one gauge larger3. Slightly longer length4. Slightly longer length and one gauge larger.

116. Compression failure of wooden structures generally occurs due to:1. Over tightening 2. Shock loads3. Rupture across the wood fibers 4. All are correct.

117. At present SSID have been issued for:1. B 200 C, C 90 A, B737 2. A35, B55, C90 A.3. B737, B747, HS 748 4. J 3C, PA 12, FA 152.

118. Design economic life of airbus is years.1. Ten 2. Twenty years3. Thirty 4. fifty.119. Design economic life of Douglas F-27 and HS-748 is years:1. Twenty 2. Thirty3. Fourty 4. Fifty

120. Design economic life of all models of Boeing is:1. 20 years 2. 20,000 life cycles3. 60,000 Hrs. 4. All are correct.

121. Duplicate inspection of control systems means:

1. Two inspections in a day by day the same person2. Inspection by an AME followed by the pilot in command3. Re-inspection of controls when reported sluggish by the flight crew4. Inspection and certification by two different approved/authorized/learned persons.

122. Duplicate inspection of all controls surfaces shall be made:1. Approved person in an approved organization2. Flight engineer3. QCM4. Both 2 and 3 are correct.

123. RAO can authorized a person to carry out duplicate inspection of aircraft if a person has at least three years general maintenance experience and months experience onthe tope of aircraft involved:1. Three 2. Six3. Nine 4. None of the above.

124. Duplicate inspection of all control surfaces shall be made:1. After rigging 2. Before first flight after C of A3. Before C of A flight 4. Before first flight of all aircraft after assembly and rigging.

125. Duplicate inspections at control system means:1. two inspection in a day by the same person2. Inspection by an AME followed by pilot in command3. Re-inspection of controls when reported sluggish by the flight crew4. Inspection and certification by two different approved/authorized heaved persons.

126. Duplicate inspection when aircraft is away from base is carried out by:1. Any CPL (commercial pilot Licence) holder.2. Flight engineer whose Licence is endorsed for the aircraft3. Specially authorized person4. Both I and 2 are correct.

127. RAO can authorized a person to carried out duplicate inspection of aircraft if a person was at least 3 years general maintenance experience and months experienceon the type of aircraft involved.I. Three 2. Six3. Nine 4. None of the above.

128. Duplicate inspection when aircraft is at base, is carried out by:1. Approved person in an approved organization.2. Flight engineer3. Quality control manager4. Aircraft maintenance engineer.

129. If control system is distributed after the second check, before first flight:

1. Disturbed portion should be checked in duplicate again 2. Disturbed portion should be checked by second person3. Complete portion should be checked by second person only4. Complete portion should be checked induplicate again.

130. F-XII deals with:1. Inspection of wooden aircraft2. Duplicate inspection of flying controls3. Duplicate inspection of engine controls4. None of the above.

131. Factor causing wood deterioration is:1. Growth of fougue2. Mechanical forces mainly due to timber shrinkage3. Chemical action of give due to ageing4. All are correct.

132. Aircraft of composite construction shall be inspected before issue/renewal or validation of C of A and the thereafter every years:1. One 2. Two3. Five 4. Ten.

133. Wooden aircraft exposed to large cyclic changes of temperature and humidity areespecially prone to:1. Timber shrinkage 2. Glue deterioration3. Both 1 and 2. 4. None of the above.

134. Aircraft of composite construction shall be inspected before issue/renewal or validation of C of A and thereafter every years:1. One 2. Two3. Three 4. Ten.

135. Weather proofing quality of fabric covering is affected by:1. Long exposure to inclement whether condition2. Exposure to stooge sunlight3. Atmosphere air4. Both 1 and 2 are correct.

136. In wooden structures, old screws are usually replaced with new screws of:1. Identical length2. Identical length but one gauge larger3. Slightly longer length4. Slightly longer length and one gauge longer.

137. Compression failure of wooden structure generally occurs due to:1. Over tightening 2. Shock loads3. Rupture across the wood fibers 4. All are correct.

138. F-XIII deals with1. Construction of gliders and their maintenance2. Inspection of wooden aircraft3. Rebuilding of aircraft4. Registration making on aircraft.

139. All gliders must process:1. Type certificate 2. As in A plus C of A3. As in B plus peaty to fly 4. None of the above.140. If ‘loop test’ is not carried out during test flight of a glider, then its C of A:1. Will not be renewal 2. Will not be renewed in any case3. Will not be renewed temporarily 4. Will be renewed provided theGlider is suitably pay carded that’Loop maneuvers’ are prohibited”

141. C of A for glider is not renewed if following that are not carried out:1. Stall/spin 2. Loop3. Both land2. 4. Either lor2.

142. Application for issue/renewal of C of A glider is made on:1. Prescribed form 2. Appropriate form3. Either lor2 4. CA25.

143. All gliders shall be equipped with:1. Vorimeter 2. RPM indicator3. VOR 4. Auto pilot

144. The C of A for glider is renewed provided is carried out during test flight:1. Loop test 3. Stall test 2. Spin test 4. All are correct.

145. Certificate of safety for glider is valid for:1. One day 2. One month3. Three month 4. One year.

146. New component and spare parts used on gliders should be covered by:1. Certificate of maintenance 2. Release note3. Both land2 4. None of the above.

147. Certificate of safety for gliders:1. Should be pressure for one month2. Should be pressure for two month 3. Should be pressure for one year4. None of the above.

148. When glider meets with an accident, resulting in damage beyond economic repair,glider logs book and procedure / work shall be pressure for a period of:1. One month 2. One year3. Two years 4. Five years.

149. Series F part XIV deals with:1. Registration of micro aircraft 2. Airworthiness of micro aircraft3. Both 1 and 2 4. None of the above.

150. The weight considered for declaring the aircraft micro light:1. MAUW 2. MTOW 3. Empty weight 4. None of the above.

151. The MAUW of micro light single seater aircraft should not exceed:1. 330Kg. 2. 450Kg.3. 2000 Kg. 4. None of the above.

152. The MAUW of micro weight two seater aircraft should not exceed:1. 330 Kg. 2. 450 Kg.3. 2000 Kg. 4. None of the above.

153. Which form is to be filled for registration of micro light?1. CA25 2. CA233. CA28 4. None of the above.154. How many items should be fixed on identification plate of micro light aircraft:1. 4 Items 2. 5 Items3. 6 items 4. None of the above.

155. Permit to fly is valid for:1. 6Months 2. lYear3. 2Years 4. NOA.

156. How many copies of manual should be admitted to DGCA:1. II 2. III3. IV 4. None of the above.

157. Sub of F-XX related to age of aircraft imported for:1. Schedule 2. Non-schedule3. Private 4. Both 1 and 2.

158. The aircraft, which landed with scehon of its upper fuselages:1. Aloha airline Boeing 73 7-200 2. Spice jet 7073. Airbus 4. None of the above.

159. Design economic life of jet aircraft extend to:1. 20 Years/30,000 Landing 2. 20 Years 60,000 Landing3. 10 Years/60,000 Landing 4. 15 Years/30,000 Landing.

160. For schedule / Non-scheduled No aircraft imported who complete age / designeconomic life of:1. 15/75% 2. 20/70%3. 15/70% 4. 20/75%.161. For cargo operation pressurize transport cat. Aircraft import not more than age and

design economic life:1. 20 /75% 2. 30/75%3. 70% 4. 60/45%

162. TSO stand for:1. Time service operation 2. Time since operation3. Time since overnight

163. TSN stands for:1. time since navigation 2. Time since new3. Time since.

164. Un press aircraft not import to India whose age is:1. More than 15 2. More than 203. More than 30 years 4. 70 Years.

165. Sub. OfF XXI:1. Import / export 2. Renewal /valid3. First aid kits.

166. DORT stands for:1. Director general of field trade 2. Director general of foreign trade.

167. Component include accessories or attachment:1. True 2. False 3. None of the above.

168. For impost of tool firm required:1. No Licence 2. No recommendation for DGCA. 3. Both.

169. NOC stands for:1. No objective component 2. No objection certificate3. Number of operated of component.170. o export spares, items of equity carry out necessary repair operator may approval:1. DGCA 2. RAO3. QCM 4. DAW.

171. NOC certificate made by:1. QCM 2. RAO3. DAW 4. DGCA.

172. CAR issued under rule:1. 55A 2. 133A3. 133C 4. 72A.

173. Conversion training conduct by:1. QCM 2. RAO3. Instructors.

174. Load / trim sheet get approved from:1. RAO 2. DGCA3. QCM.

175. Training program for person engaged in people of load / trim sheet include:1. Refresher/recurrent training 2. Schedule training3. Conventional training 4. None of the above.

176. Basic indoctrination ground training for newly hired staff used for prepare load/trimsheet is:1. 45 programmed Hrs. 2. 35 Programmed I-Irs.3. 40 Programmed Hrs. 4. 65 Programmed lIrs.

177. Competency check is included in:Ground training 2. Initial of transition ground training3. Refresher training 4. Conversion training.

178. Competency check in initial and transition training gives by:1. Supervisor/ground instructor 2. QCM3. RAO 4. All are correct. a

179. Certificate of successful completion training in recurrent training to airline given by:I. QCM 2. Shop3. Staff instructor 4. RAO.

180. The written practical test in conversion training is coordination with:I. DAW 2. RAO3. Operator 4. QCM

181. Written test will conduct by:I. Instructor 2. QCM3. Operator.

182. Load of trim sheet approved by:1. RAO 2. DGCA3. QCM 4. None of the above.

183. Weight of aircraft at time of take off not exceed:1. RTOW 2. Payload3. Removable Weight

184. I oad/trim sheet prepared in:I. Triplicate 2. Duplicate3. A copies 4. None of the above.

185. The load /trim contain:1. Weight schedule 2. C.G.

3. AVW 4. All of the above.

1 86. A group of characters affixed on aircraft surface to identify the country to which theaircraft belongs is called:1. Nationality mark 2. Common mark3. Registration mark 4. Both I and 2.

187. Disputes with regard to the legal ownership of aircraft is decided by:1. DGCA Head Qtr. 2. RAWO3. AWO 4. court of law.

188. Detailed requirements for registration of aircraft are as per:1. Aircraft rule 1937 2. ICAO Annex 73. CAR Series F Part-IV 4. Both 1 and 2.

189. Legislation with regard to registration of aircraft is described in:I. Rule 30 of 1937 2. Rule 25 to 30 of 19373. Rule 30 to 37A of 1937 4. Rule 38 to4l of 1937.

190. Any aircraft supported chiefly by buoyancy in the air is:1. Lighter than air aircraft 2. Heavier than air aircraft3. l3oth I and 2 4. None of the above.

191. Application for registration of aircraft is put on:1. CA 28 2. CA 253. CA 3O 4. CA 23.

192. If an aircraft is sold to another person or company it should he notified to DGCA as per:I. Rule 30 2. Rule 32 A3. Rule 33 4. Rule 37 A.

193. Until the certificate of registration is not granted to the new owner, aircraft:1. Shall not be law full to fly2. Assist in flying by any person3. Can fly with written permission of DGCA4. All above are correct.

194. An aircraft brought from out side by air, temporary certificate of registration:I. Valid only up to first reaching at custom aerodrome in India.2. Should he surrendered to DGCA.3. Should have the aero mobile station Licence.4. All above are correct.

195. The following registration marking can be granted to an aircraft:1. VT-SOS 2. VT-XXX3. VT-TTT 4. None of the above.

196. Certificate of registration is valid up to:

I. One year 2. Two years.3. Five years 4. Date indicated on it.

197. Certificate of registration shall be in language:1. Hindi 2. English3. Hindi and English 4. Hindi or English.

198. When a new type of aircraft is registered and entered in the register. DGCA shall advise the:I. Owner 2. Operator3. State of design 4. None of the above.

199. Duplicate certificate of registration shall be issue in case of:1. Lost 2. Mutilated3. Lost and mutilated 4. Lost or mutilated.

200. The registered owner may apply for cancellation of registration under the clause of:1. Rule 30 of 1937 2. Rule 33A of 19373. Rule 37 A o f1937 4. None of the above.

201 . [)GCA may cancel the registration of aircraft if:1. Aircraft has been destroyed 2. Permanently with drawn3. Registration is due to false statement 4. All above are correct.

202. A register of all aircraft registered in India is to be maintenance by DGCA as requiredby rule:1 31 of 1937 2. 33 of 19373. 36 of 1937 4. 37 A OF 1937.

203. The registration marks on the un-manned free balloons shall be affixed on:I. Left side 2. Right side3. Right and left side 4. Identification plate.

204. On multi vertical tail surfaces aircraft the registration marks shall appear on:1. Both the sides of tail surfaces2. On inner sides of tail surfaces3. On the out board sides of the outer surfaces4. Not required any where as per series”.X