A.m.e Question Paper 1

8/11/2019 A.m.e Question Paper 1

1/104

PAPER I CAR A M E EXAMSCAR SERIES FPart V to VIII

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 s

uffer 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 rem

ain 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 Organisation3. Airworthiness Officer, 4. Q.C.M.

12. Suspended C of A can revalidated for One year after completion of Modification, Repair,


2/104

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 ionCARseries 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 theaircraft.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 Constructo


3/104

r 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/overhauledwhichare 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 notable 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., statedby 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. inlight 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.


4/104

4. All the above.

34. Special permits are not required in case of Test Flight for Renewal of C. ofA. & 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 theabove.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 RAOwill 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 Operations


5/104

3. 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 that

1. 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 withoutauthority 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 posses1 Valid Licence with specific entrustment of type of a/c

2 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 asrequired 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 by

I. D.G.C.A. 2 .A.M.E3. Manufacturer 4 QCM


6/104

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 certified

I. 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 within1. 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 by

1. 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 Air

transport 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 havingpassenger 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 spec


7/104

ially approve person3. Transmit inspection without snag rectification will by approved basic licenceholder 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 CFR

1. 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 Days3. 20 Hrs / 7 Days 4. 25 Hrs./30 Days

71. Aircraft from regular aerodromes shall FRC to aerial work category issue every 50

Hrs./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. Theinspection 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 aircraft

2. 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.


8/104

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. Firms name3. Date and place of issue

4. 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 damage3. Fatigue damage 4. Multiple site damage.


9/104

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 forflying 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 IV

3. Series F, Part-XII 4. Series F, Part-XIII.Series FPart-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 lifedcomponents

3. 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 inadvanceabout 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 periodof


10/104

years: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 dueto: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 f

light.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/renewalor 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 humidityareespecially prone to:

1. Timber shrinkage 2. Glue deterioration3. Both A and B are correct 4. None of the above.


11/104

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 command


12/104

3. 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 aircraft

3. Specially authorized person4. Both I and 2 are correct.

127. RAO can authorized a person to carried out duplicate inspection of aircraftif 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/renewalor 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 humidityareespecially 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/renewalor validation of C of A and thereafter every years:

1. One 2. Two3. Three 4. Ten.


13/104

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 aircraft

3. 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 testis not carried out during test flight of a glider, then its C ofA: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 thatLoop maneuversare 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.


14/104

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 thanage and

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


15/104

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 new

3. 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. RAO

3. 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 prepareload/trim

sheet is:1. 45 programmed Hrs. 2. 35 Programmed I-Irs.3. 40 Programmed Hrs. 4. 65 Programmed lIrs.


16/104


17/104

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 A

3. 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. DGCAshall 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 DGCAas requiredby rule:

1 31 of 1937 2. 33 of 19373. 36 of 1937 4. 37 A OF 1937.


18/104

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 surfaces

2. On inner sides of tail surfaces3. On the out board sides of the outer surfaces4. Not required any where as per series.X

PREPRATORY A M E EXAMSC A R Series H, PART I III

1. CAR Series H Part I deals with:1. Unusable fuel supply. 2. Calibration of fuel quantity gauge of A/c.3. Calibration of fuel quantity gauge of helicopter 4. All are correct.

2. The quantity of unusable fuel in most cases, is included in the appropriate:

1. Flying manual 2. Quality Control Manual3. Cockpit Checklist. 4. Emergency checklist.

3. Certain quantity of fuel in an aircraft will not be available for use becauseof:1. Shape of the tank. 2. Location of tank.3. Both 1 & 2 are correct. 4. None of the above.

4. Unusable fuel is the quantity of fuel supply remaining in each tank and not available is theengine under the most adverse feed condition in1. Intended flight maneuvers. 2. Any flight condition.

3. Stabilized cruise condition. 4. Both I & 3 are correct.

5. The unusable fuel quantity for each tank must be established:1. Every overhaul 2. Every C of A.3. Certificate of Aircraft. 4. All are correct.

6. Fuel gauges shall be calibrated at Zero-datum with:1. 5 liters fuel 2. 10 liters fuel3. Nil fuel 4. Unusable fuel

7. A fuel quantity gauge is calibrated on the following occasions:1. Every C of A. 2. Time of Installation3. Near Major Check 4. All are current.

8. The quantity of unusable fuel shall be deemed to be part of:1. Empty weight of aircraft 2. Total weight of aircraft1. Payload weight of aircraft 4. None of the above.

9. Properly calibrated dipstick has to be carried on board with:1. Every helicopter 2. Every light aircraft.3. Both 1 & 2 4. None of the above.

10. Aircraft fueling procedure is laid down in:1. CAR series H Part I 2. CAR Series H Part III3. IAR25A 4. Noneoftheabove.

11. Fueling means dispensation into an aircraft of:1. Aviation Fuel 2. Fuel & Power boost fluids


19/104


20/104

1. Main engines. 2. Aux. power units.3. Both 1 & 2 4. None of the above.

24. Fuelling operation shall be stop, when the spillage covers an area greater than:1. 2 Sq. meters. 2. 5 Sq. meters.3. 15 Sq. meters. 4. 20 Sq. meters.

25. In case of fuel spillage during fuelling operation, covering an area greaterthan 5 Sq. meten allpersons shall be evacuated from the affected area to a place away from the spillage by minimumdistance of:1. 6 meters. 2. 15 meters.3. 30 meters. 4. 43 meters.

26. CAR Series H Part III deal with:1. Quality Control of fuel. 2. Sample testing of fuel3. Inspection of installation 4. All are correct.

27. While delivering aviation fuel, the supplier will normally present:1. Release Note. 2. Delivery receipt Certificate3. Both ! & 2 4. None of the above.

28. An aviation fuel delivery vehicle shall be cleaned internally every:1. One year 2. Two years.3. Three years 4. Five years.

29. The minimum setting for fuel in tanks fitted with floating suction valves inrespect of horizontaltank is:1. One hour 2. Two hours.

3. One hour! Foot depth of fuel 4. Two hour/foot depth of fuel

30. Setting time for ATF, without floating suction device is:1. Half an hour/foot depth., 2. One hour/foot depth3. Total one hour 4. None of the above.

3 1. Floating sections of bulk fuel tanks should be inspected for satisfactory performanceonce in:1. Three months; 2. One month3. Fifteen days. 4. None of the above.

32. Tank bottom sample of ATF shall be tested for Microbiological growth once in:1. One year 2. Two years.3. Three years. 4. None of the above.

33. Overall dimension of fuel Grade Labelshall be:1. 15cm x 10cm 2. 30cm x 10cm3. Not less than 15 cm x 10 cm 4. None of the above.

34. Color code of AVGAS Pipelines & grade label is:1. Black & White 2. Red & Blue3. Red & White 4. Black & Red.

35. Before commissioning a new hose on a particular fuel:1. 10,000 liters of fuel should be circulated through it.


21/104

2. Fuel should be stored in the hose for at least 24 h ours3. Both 1 &2 4. Either 1 or2

36. Fuel specification tests are to be carried out on AVGAS fuel, when no fuel has been added to the static bulk store during the last:1. Three months 2. Six months

3. One year. 4. None of the above.

37. Delivery of AVGAS from the vehicles to aircraft should be made through a Micro filter with a normal rating of:1. 100 mesh gauges. 2. 180 mesh gauge3. 5 Microns 4. None of the above.

38. Filtering elements of fuel dispensing vehicles should be inspected:I On significant reduction in flow rates. 2. On continuing unsatisfactory drainsample.

3. Both 1 & 2 4. None of the above.

39. Pressure differential checks on refuller filters, at the maximum possible flow rate. Should be carried out:1. Every day 2. Every week3. Every month 4. Once in a year

40. Checks should be carried out on de-hydrant system to verify the correct operation of shut-off valves & grade selection device:1. Every month 2. Every six months

3. Every two months 4. Every year.

41 As a matter of routine, elements of filler separators for the refuller & hydrant system should be replaced after every:I. One year 2. Two years3. Three years 4. None of the above.

42. Barrels should be stored on their sides with the bungs at:1. 3 Oclock position 2. 9 Oclock position3. Both 1 & 2 4. None of the above.

43. Suction stand pipe to be fitted to barrel should be such that fuel can not drain from the bottom:1. 3 inches. 2. 6 inches.3. 4 inches. 4. None of the above.

44. Laboratory tests are required before using barrel fuel when 6 months have elapsed since the filling of barrels in respect of:I. AVGAS 2. ATF3. Both 1 & 2 4. The statement is incorrect.

45. Suspended water in fuel can be detected by water finding:I. Paste. 2. Paper.3. Capsule 4. All are correct.46. Aircraft should be defuelled into:

I. Empty fuelling vehicle. 2.Directly into another aircraft.3. Refueling vehicle having spare capacity 4. Any one of the above.47. When changing fuel grades, extra precautions are to be observed from:


22/104

1. AVGAS to ATF 2. ATF to AVGAS3. One grade of AVGAS to another 4. None of the above48. Single tank composite sample means, mixing of fuel in equal quantity from samples taken: 1. During morning, afternoon & evening 2. Upper, Middle & lower level3. Top & Bottom 4. All are correct

1. CAR Series ApartIdeals with:a) Responsibilities of owner / operatorb) Supervision of Airworthiness standards. By airworthiness Directoratec) BothA&Bd) None of the above.

2. Aircraft flown for the test thr renewal of C of A cana) Vicinity of aerodrome b) With in the area of 200 Km. c) BothA&Barewrong d) Both A & B are correct

3. Who is responsible to ensure that aircraft has current and valid C of A: a) QCM b) AME

c) Owner/operator d) RAO.4. Airworthiness can be achieved by;a) Periodical inspections b)Replace held components. c) carry out repair / modifications d) All the above

5. Owner/operator is responsible for:a) Requiring his pilots to operate as per operating limitationsb) Reporting and recording all defectsc) BothAandBd) None of the above.6. If the aircraft is leased by owner, than the responsibility for C of A to becurrent and valid is of: a) Owner b) Operatorc) AME ` d) None of the above

7. During routine maintenance, owner/operator shall report all defects to:a) AME b) QCMc) Airworthiness Directorate d) All of above.8. Airworthiness standards observed by the operator/owner will be monitored by technical officers by the medium of airworthiness directorate:a) Spot checks b) Investigation of defects c) Both A and B d) Either A or B.9. CAR Series APart-lI lays out:a) Maintenance procedures b) Procedures of issue of CAR c) Revision of CAR d) Both Band C.

10. CAR is issued By:a) Airworthiness authority b) QCMc) RAO d) None of the above.11. CAR is issued under the provision of:a) Rule 133 b) Rule 133 A c) Rule 133 B d) Rule 133 C12. Promulgation and implementation of CAR is to meet:a) Duties and obligations of contracting state under Chicago conventionb) Harmonization of requirements with other regulatory authorityc) BothAandBd) None of the above.13. When CAR is issued., first page indicates:a) Date of issue b) As a) plus date of affectivity c) As b) plus total no. of pages d) None of above.

14. Subsequent pages other than first indicates: a) Date of affectivity b) Dateof revision c) Date of issue d) all the above.15. A change effected in CAR is tempered as: a) Amendment b) Change c) Re-issue


23/104

d) None of the above.16. First page and affected pages indicates: a) Revision number b) a) plus dateof revision c) b) Plus effective date d) None of the above.17. Unaffected pages by revision will contain: a) Effective date b) Issue numberc) Date of issue d) None of the above.18. A revision is indicated by: a) A sideline on left side of affected pages b)Underlining the affected part c) High lighting with dark ink d) Any one of above

.19. Major changes to CAR shall be treats as: a) Change b) revision c) Amendmentd) Major revision.20. Whenever a new CAR or significant revision is proposed to be issued, the draft CAR/proposed revision may be circulated to: a) Concerned operators b) Plus regional officer c) plus manufacturer d) None of the above.21. Revision notice indicates: a) Pages affected b) reason for revision c) BothA and B d) None of the above.22. Part III relates to: a) Objectives and targets of airworthiness directorateb) Airworthiness regulation and safety oversight c) Duties of owner/operator d)Both A and B.23. The most obvious objective of an airworthiness authority is: a) Ensuring des

ign levels of reliability b) Operating safety of civil registered aircraft c) Alert value of light aircraft d) Both A and B.24. On-Condition maintenance is accomplishment of: a) Bench/institute test b) visual inspection c) Physical measurement d) All of above.25. Condition maintenance is based on theory of: a) Fit and forget it b) fit until failure c) Both A and B d) None of the above.26. The parametric report for achieving max. Measures of safety is sent to: a) RAO b) DGCA c) QCM d) All the above.27. The parameters are obtained as: a) Accidents per 1000 Hrs. b) IFSD per 1000Hrs. c) IFSD per 100 Hrs. d) Both A & B.

28. A parameter to be obtained from no. of emergency landings and total no. of Hrs. flown is:

a) Incidents /1000 Hrs. b) Accidents/I 000 Hrs.c) Dispatch reliability d) None of the above.

29. No. of notifiable accidents along with no. of lirs. flown gives:a) Emergency landing /1000 I-Irs. b) Accidents /I000Hrs.c) Dispatch reliability d) Accident/I00 departures.

30. Total number of engine hours flown is given by product of no. of airframe hoursa) any one engine Hrs. of aircraft b) Total no. of engines installedc) Both A and B d) None of the above.

31. Total engine Hrs. and total IFSD gives:a) IFSD / 1000 Hrs. b) Accidents /1000 Hrs.c) Dispatch reliability d) all the above.

32. Dispatch reliability provides:a) Cancelled flights b) Delayed flightsc) All flights d) Both A and B

33. Parameters i.e. no. of major defects / 1000 Hrs. includes no. of Hrs. of:a) Airframe b) Enginec) Either A or B d) None of the above.

34. Private operator will furnish information in parametric form to DGCA every:a) One month b) Three month


24/104

c) Six months d) One year.

35. Non-scheduled, aerial work, training aircraft operator should furnish information toDGCA every.a) One month b) Three monthc) Six Month d) On demand.

36. Monthly report should be sent to DGCA by:a) Scheduled operator b) a) plus non-scheduledc) b) plus aerial work d) c) plus private.

37. Dispatch reliability is parameters send by:a) Scheduled operator b) a) Plus non-scheduledc) Plus aerial work c) Plus private.

38. If there is nil information is there, the DGCA receives:a) Nil information b) No responsec) Previous information d) Any other except above.

39. It is the responsibility of owner/operator to procure the revision /CAR From:a) DGCA New Delhi, b) regional airworthiness officec) Sub regional airworthiness office d) Publisher.

40. Unintentional landing affected on account of failure/malfunctioning of an aircraft component system is:a) Hard landing b) Crash landingc) Belle landing d) Emergency landing.

41. Maintenance process requiring assembly, inspection of aircraft/components atfixed periods is:

a) On condition maintenance b) Condition monitoringc) Hard time maintenance d) Schedule maintenance.42. Achieving the maximum measures of safety the operator/owner should submit theregional or sub regional office the:a) The no. of emergency landing and Hours flownb) The no. of engine hours! in flightc) No. of accidents /No. of 15 minutes delaysd) All above are correct.

43. The frequency, scope, and contant of periodical inspection:a) Should be altered only after three monthsb) Should be altered only after six monthse) Should be altered only after 12 monthsd) Chair not be altered with out the approval of DGCA.

44. Technic& officers of airworthiness directorate may ask the operator to submit forinspection the:a) Aircraft b) Aircraft componentsc) Aircraft documents d) Both B and C

45. Revision notes:a) Need not to fieldb) Should be filed in a special file

c) Should be filed along with the affected CAR folderd) Both A and B are correct.


25/104

46. When ever a new CARl/Revision is issued, operator/owner should be provided with thea) Check list by DGCAb) Amendment list by DGCAc) Revision by DOCAd) Issue by DOCA.

47. The parameters mentioned in CAR series A Part-Ill will be recorded in graphical formand compared by:a) Regional airworthiness office b) Sub regional airworthiness officec) QCM of organization d) Both A & B.

48. Airworthiness office after investigating the parameter will can recommend:a) Varying the process of maintenanceb) Suggesting in corporation of modificationc) Increasing monitoring checks by airworthiness officed) All above.

49. The assessment of performance of operator will be provided as Birds eye viewby:a) Maintenance schedulec) Monitoring parametersb) Modification statusd) On condition and hard time maint

50. The operator shall him self take corrective action by observing:a) Qualification of AME b) Qualification of mechanicsc) Adverse trends in serviability d) Both A & B.

51. The aircraft rule of aircraft rules 1937 that lays the maintenance and certi

fication standard of civil registered aircraft is:a) Rule 5 b) Rule 59c) Rule 50 d) Rule 6052. The rule that lays that a major defect or major damage to aircraft shall bereported toDGCA is:a) Rule 60 b) Rule 50c) Rule 59 d) Rule 15.53. Aircraft component means a part filled on aircraft, the soundness and correct functioning of which is essential for:a) Its continuous airworthiness b) Safety of aircraftc) Safety of occupants d) All the above.

54. Major defects means defect of such nature that will:a) Take at least 72 Hrs. for rectificationb) Necessarily involve change of componentc) Result in emergencyd) Reduce the safety of aircraft occupants.

55. CAR section II series C Part I classifies major defects in:a) One group b) Two groupc) Three group d) Four group.

56. Failure of a component that result in taking emergency action:a) Defect b) Major defect

c) Minor defect d) Repetitive defect.

57. The aircraft operator that operator it fleet as per published schedule is ca


26/104

lled:a) Normal operator b) Private operatorc) Scheduled operator d) Non-scheduled operator.

58. All major defect will be reported to:a) DGCA b) RAOc) DAW d) QCM.

9. All major defect will be reported to RAO concerned:a) Within 48 Hrs. b) Within 24 Hrs.c) Within 12 Hrs. d) Immediately on telephone.

60. Investigation of major defect will be completed within:a) One moths b) two monthsc) six months d) three months

61. The final defect investigate report shall be sent to:a) DGCA in duplicate b) DGCA in triplicatec) RAO in duplicate d) RAO In triplicate.

62. The main purpose of investigation is to:a) Find the cause of defectb) Find the person who caused the defectc) Avodrecurcuce of defectd) Both A and C.

63. Mech. Delay is a delay of:a) 15 Minute or more b) 30 Minute or morec) 15 Minutes or more to scheduled servicesd) 30 Minute or more to scheduled services.

64. for computing statics for the purpose of determining components reliability o

ne has totake into account:a) Major defects b) Minor defectc) Repetitive defect d) all the above.

65. All faults malfunctioning defect or any other occurrence such may cause servicedifficulties or adverse effect on continuing airworthiness shall be reported byoperator/approved maintenance organization with in:a) 10 days b) 5 daysc) 7 days d) 15 days.66. Records associated with defect shall be preserved for:a) Two weeks b) Six weeksc) One weeks d) Two years.67. Component associated with major defect will be preserved for a period of:a) One week b) 15 daysc) 3 Weeks d) 2 weeks)

68. Which of the following is called major defect:a) Significant fuel contaminationb) Fuel starvation in flightc) None of the aboved) Both A and B.69. Operator other than scheduled operator will forward fleet performance:a) After one months b) After two months

c) After four months d) after three months.70. Scheduled operator shall forward fleet performance:a) After two months b) After fifteen months c) After one month d) After six mont


27/104

hs.

71. a fleet is constituted by:a) At least 25 aircraft b) At least 5 aircraftc) At least 3 aircraft d) None of the above.

72. Minor defects are classified:

a) Group A and B b) Group I and II c) Emergency and Non-Emergency type d) None of the above.

73. CAR sec.-II series C part-Il (Recording of in flight instruments is) Applicable to:a) Scheduled operator b) Non-scheduled operatorc) Public transport aircraft d) All the above.

74. Group I type major defect includes:a) Fires during flight b) false five warning during flightc) Both A & B d) None of the above.

75. Occurrence of major defect falling into group-I will require:a) renewal of C of A b) Registration of FRCc) Both A and B d) None of the above.

76. In flight instrument reading should be recorded:a) At least once in each of sectorb) At least once in each of sector under stabilized cruise conditionsc) In the even of emergency condition of flightd) Both B & C.

77. Only those defects must be entered in the relevant colors of flight reports,that areobserved during:

a) Preflight b) Post flightc) Course of flight d) all are correct.

78. If no defect is reported by crew during the previous day AME will:a) release the aircraft for flyingb) Release the aircraft after consulting QCMc) Release aircraft for flight only when NIL entry has been made by pilotd) None of the above.79. Defects observed at a place away from normal base are recorded in:a) Aircraft log book b) Journey log book couloum XIc) Job sheet d) Defect register80. In case performance deterioration and observed in aircraft test flight is carried out toascertain increase of drag from the parameter:a) Fuel flow and airspeed b) Fuel flow and true airspeedc) Fuel flow and altitude d) None of the above.

81. CAR series C Part-IV relates to:a) Public transport aircraftb) Public transport aircraft turbo jet onlyc) Aircraft other than public transportd) None of the above.

82. If detonation is observed of an engine RAO may:a) Curative measures to be taken

b) Flight test to ascertain increase Indyc) Replacement of engined) Both A & C are correct.


28/104

83. Reliability monitoring unit is part of:a) DOCA b) RAO c) Operators QC wings d) None.

84. RMU will gather information from:a) scheduled maintenance b) Unscheduled maintenancec) From Both A and B d) None.

85. If a system is over alert/alert notice will be issued by RMU and report willsent to:a) DGCA b) RAOc)QCM d) None.

86. Alert notice will be issued to all concerned and sent to RAO in duplicate: a) By 251h of every month b) By 30th of every monthc) On 25th of every month d) On 7th of every month.87. Roughly graphic display about reliability should summarize operating experience for at least the last:a) Three months b) two months c) six months d) One year.

88. Maintenance control by reliability method is given in series:a) B Part-I b) F Part-XXc) C Part-V d) H Part-Ill

89. C Part V is applicable to:a) Scheduled airlines b) Non-scheduled airlinesc) Private operator d) Both A & B.

90. Occurrence of major defect falling under group-I require:a) Rectification of defectb) Reporting to RAO within 72 Monthsc) Validation of FRC

d) Only A & C.

91. At the end of flight crew must put in the register:a) Any snag observed during flightb) Nil, even when no snag observedc) Heavy landing if happenedd) All the above.

92. Reliability displays for any reported failure or non-routine, removals are to be impressed in terms:a) 1000 Aircraft Hours. b) 1000 Aircraft Hrs. or 100 Landingsc) 1000 aircraft Hrs. or 3 months elapsed timed) 1000 aircraft hrs. or after appropriate devolutions.

93. Reliability displays for all reported removals are to be preserved for a period:a) Six months b) One yearc) Two years d) five years.

94. Regarding defects occurring on the aircraft system the role of RAO is to:a) Carry out speed checks on the records maintainedb) Ensure that defect are classified properlyc) Associate themselves seas to get the defects rectified

d) All the above.

95. CAR series D Part I deals with the reliability of aircraft engine operated by


29/104


30/104

d) DGCA by the 10th of the month.

108. Aircraft maintenance programme and their approval is covered under:a) JAR 60(2) b) IAR 60c) CAR Series D Part-Il d) Both A and C.

109. Condition monitoring implies the philosophy of:

a) fit and forget b) Fit until failurec) Both A and B are correct.

110. Hard time is a:a) Failure preventive process b) Not a failure preventive processc) Maintenance programmed d) I and III are correct.

111. It is not a failure preventive processa) Hard time b) condition monitoringc) On condition

112. This process has got direct relationship between reliability and the age:

a) Hard time maintenance process b) Condition monitoring maint. Process.c) On condition monitoring maintenance process.

113. If Reliability could be measured without stripping by physical measurementis:a) On Condition b) Condition monitoringc) Hard time.

114. Replacement of condition monitoring item is:a) Scheduled maintenance b) Unscheduled maintenancec) Hard time maintenance.

115. For older aircraft, manufacturers would issue a document called:

a) Supplemental structural inspection documentb) Log Bookc) Registerd) Both I and III.116. Restoring an aircraft part or component to its original design performancelevel afterreplacing reworking the parts is termed as:a) Overhaul b) Top overhaulc) Modification d) Both A and C are correct.

117. Am items is considered damage tolerant if:a) It can sustain damage and the remaining structural can withstand reasonable loadb) It can sustain damage and the structure can bear excessive load.c) Both A and B are correct.d) None of the above.118. Maximum deviation from the normal operating limit but with in the allowableoperating range.a) alert valve b)c) Both d) None of the above.

119. Occurrence of malfunction in-flight are recorded in the:a) Technical log book b) Journey log bookc) Both I and II d) None of the above.

120. The entry in technical logbook is filled by:a) Flight crew b) Cabin crewc) AME d) Pilot


31/104

121. The operator shall establish an alert level:a) In the pressure b) Based on experiencec) With concern to AME.

122. Alert level can be continuously up-dated by means of rolling average either:

a) Quarterly or 6 monthly b) 8 Monthlyc) 2 year d) 1 year.

123. Corrosion prevention schedule is included by the operators in:a) Maintenance system manual b) Technical log bookc) Register d) Journey log book.124. If in any programme approved by the airworthiness is deviated, it should bebrought tothe notice of:a) QCM b) RAOc) Operator d) AME.

125. The details of the any programme approved by AWO, it should be reflected inthe:a) Inspection schedule b) COSLc) Special inspection schedule d) All of the above.

126. Hidden function components must have some form of:a) Scheduled maintenance b) Unscheduled maintenancec) Both d) None of the above.

127. Who maintain a continuous record of the parameters in a graphical form or atabulated form:a) AME b) Every operatorc) QCM d) I and III.

128. It shall be the responsibility to mention the fatigue lives of the components in the engine log book.a) By QCM b) By overhauling agencyc) By organization d) All of the above.

129. It shall be the responsibility to report to RAO/sub RAO in writing all lifelimiting features:a) BY QCM b) By overhauling agencyc) By organization d) All of the above.

130. The parameters shall be recorded/plotted after:a) 24 Hrs. B) 60 Hrs.c) 5OHrs. d) 12 Hrs.

131. The operators shall inform in writing whenever alert values are reached orabnormalconditions.a) RAO/Sub RAO b) AMEc) QCM d) DGCA.132. The corrective maintenance action shall be spell out in:a) Journey logbook b) maintenance system manualc) CAR d) I and III.

133. Failed engines shall be preserved at least for:a) 1 Year b) 2 years

c) 5 Years d) All of the above.

134. Engine overhaul records shall be preserved by:


32/104

a) RAO b) Organizationc) Overhauling agencies d) QCM135. The average fuel and oil consumption of engines will be recorded in the engine log book by:a) RAO b) QCMc) Licence AME d) Operator.

136. When ever alert value exceeds who would initiate necessary corrective action:a) RAO b) Operatorc) QCM d) AME.

137. Primary maintenance process has been recognized by the:a) QCM b) Airworthiness authoritiesc) RAO.

138. Which aircraft require regular assessment of their structure?a) Transport aircraft b) Pressurized transport aircraftc) land II d) All of the above.

139. Average fuel and oil consumption of engines will be recorded in:a) Journey log book b) In engine log bookc) Propeller log book d) all of the above.

140. CAR supersedes the instructions contained in DGCA in:a) Circular letter No.10/7/64 b) Circular letter No. 12/8/64c) Circular letter no.1/9/64 d) None of the above.

141. Who can carried out periodical spot checks on the records of fuel and oil uplift?a) RAO b) AMEc) QCM d) Technician.

142. Who can change from one maintenance process to another?a) RAO b) AMEc) Operator d) QCM

144. Who may require an operator to submit samples to bench checking and in caseof engineseven to flight tests:a) QCM b) AMEc) RAO/Sub Rao d) all of the above.

145. Every operator shall maintain a continuous record of the engine parametersin:a) A graphical form b) A tabulated formc) Either A or B d) None

146. Every engine parameters has an alert value which is fixed by:a) Operator b) DGCAc) RAO d) Operator in consultations with RAO147. Life record of all engine accessories is available in:a) Journey log book b) Log cardsc) Overhaul manual d) Maintenance manual.

148. Alert values are:a) Reference values only b) Accepting limits

c) Both.

149. RAO May require immediate withdrawal of engines from service in case:


33/104

a) Parameter monitoring records are not kept.b) Alert values have been exceededc) Both A and B are correct.d) None of the above.

150. CAR series D Part-V regarding maintenance of fuel oil consumption is applicable in

respect of:a) All aircraft engines b) Scheduled aircraft enginesc) Light aircraft engines d) None of the above.

151. Daily uplift of fuel /oil consumption in fuel oil register is signed by:a) QCM b) Licensed AMEc) DY.QCM d) Authorized person.

152. Average fuel consumption is recorded:a) In engine logbook b) In airframe log bookc) By an AME.

153. Fuel and oil consumption records in logbooks are to be maintained by:a) Licensed AME b) Qualified techniciansc) QCM d) A and B are correct.

154. Work performed at predetermined intervals to maintain an aircraft in airworthy conditionScheduled maintenance b) Preventive maintenancec) Both A and B d) None

155. Any change from one maintenance process to another after getting approval from RAO needs to be documented in:a) QC manual b) Maintenance system manualc) BothAandB.

156. On the consideration of operating economy operator can increase the servicelife ofcomponents with the approval of:a) Manufacturer b) QCMc) DGCA d) Both B and C.

157. Condition monitoring of components follow:a) Hard time maintenance b) On-condition controlc) Operate to failure philosophy d) A and C are correct.

158. Service life of a component can be reduced by an operator.a) On his own b) On his own under intimation to DGCAc) On his own but with DGCA Permission d) At the behest of DGCA.

Series F

1.Procedure relating to registration/dc-registration of a/c are given in1. F series ,part I 2. F series, part II3. F series, part III 4. None of the above

2. The rule that requires that no person shall fly or assist in flying any a/c unless it has beenregistered is1. Rule 15 2. Rule 50

3. Rule 5 4. None of the above

3. The a/c should bear its nationality and registration marks and the name & the


34/104

residence of theowner affixed or painted in accordance with1. Rule 5 2. Rule 373. Rule 50 4. None of the above

4. An a/c in India is registered in1. Category A 2. Category B

3. Both a & b 4. None of the above

5. An a/c in India is registered in category A when the a/c is widely ownedI. By citizens of India2. By a company or corporation registered in India and the chairman and atleast2/3w of the directors of which are citizens of India3. By central government or any state government4. All above

6. An a/c owned by a company registered elsewhere than in India provided that company has given the a/c on lease to any person who is a citizen of India or to another company or to state or central government that that a/c will be registere

d inI. Cat. A2. Cat. B3. Both a & b 4. None of the above

7. An ale in India is registered in category B when the ale is wholly ownedI. By persons resident in or carrying on business in India, who are not citizensof India2. By a company or corporation registered elsewhere than in India and carrying on business in India3. Both a& b are correct4. None of the above

8. For applying for registration f a/c which document should be shown

1. Custom clearance certificate/bill of entry of a/c2. Certificate of- registration from the previous registering authority3. A copy of the import hence issued by director general foreign trade (DGFT)4. All above

9. If an application is made for the registration of an ale before it is imported in India a temporary C of R may be granted under the provision ofI. Rule 30 2. Rule 313. Both a & b 4. None of the above10. Registration marking shall not 1 : allotted which might be confused with international code ofsignals likeI. Registration beginning with the letter Q2. Registration SOS , XXX . PAN, and TTT3. Both a & b are correct4. None of the above11. Where a certificate has been lost the owner may apply to DGCA for the issueola duplicatecertificate with1. An affidavit, a copy of FIR lodged with the police 2. Prescribed fee3. Both a & h are correct 4. None of the above

12. Where a certificate has been mutilated the owner may apply for issue of a Duplicatecertificate to DGCA with

1. Mutilated certificate & prescribed fee 2. Mutilated certificate3. Only prescribed fee 4. None of the above


35/104

13. The registration of an ale registered in India may be cancelled at any timeby DGCA of itssatisfied thatI. The registration has been obtained by furnishing false information2. The a/c has been destroyed or permanently3. The lease in respect of the a/c registered has expired4. All above

14. The nationality mark of all Indian Registered ale is1. EI 2. JO3. AVU 4. VT

15. IAR 30 improves the government of IndiaI. To register an a/c in India 2. To import an ale into India3. To flu ale in India 4. None of the above

16. C of R is valid forI. One year 2. Two Year3. Six months 4. None of the above

1 7. Registration of the ale by the DGCA1. Is for the purpose of controlling the safety of aviation in India2. Is for the establishing the legal ownership of an ale3. Both a & b4. None of the above

18. A/C Rule 49 empowers the DGCA1. To revalidate C of A 2. To issue C of A3. To issue type certificate for ale 4. All are correct

19. DGCA issues type certificate to engine/propeller manufactured in India underthe purview of

ale Rule1. 49A 2. 49B3. 49C 4. 49

20. Application for revalidation of type certificate of rotor-craft is submittedin the form as perCAR series F1. Part IAnnexure 1 2. Part IAnnexure II3. Part IIAnnexure II 4. Part IIAnnexure I

21. Application for issue/revalidation of type certificate of ale is to be submitted in the form as inSeries F Part II Annexure I 2. Series F Part II Annexure II3. JAR 49 Sub- Rule 2 4. None of the above

22. For issuance of type certificate of aircraft or its components, the DGCA should be satisfiedon the points:1. The design has been approved by DGCA2. The design on forms to approved airworthiness requirements/specifications offoreign airworthiness authorities and acceptable to DGCA.3. Both I and 24. None of the above.23. For revalidation of type certificate of an imported light and transport aircraft the DGCA

confirms that the aircraft meets earth the requirements of:1. FAR 23 and 25. 2. BCAR 23 and JAR 253. FAR 27 and 29 4. Both 1 and 2 are correct.


36/104

24. Type certificate of a rotorcraft imported in India can be revalidation by the DGCA if itsdesign and construction can form earth.1. FAR 23 and 25 2. BCAR 23 and JAR 253. FAR 27 and 29 4. BCAR 27 and 29.

25. An Aero engine manufactured outside India can he type certified by the DGCAif it conformsto:1. FAR33 2. FAR233. FAR 30 4. Both I and 3 are correct.

26. DGCA revalidation the type certificate in respect of engine /propeller underthe purview ofaircraft rule:1. 49 2. 49A3. 49B 4. 49C.

27. Before revalidation of type certificate, DGCA may discuss specific design/manufacturingissues with:1. Representatives of the manufacturer2. Airworthiness authority of the country of manufacturer3. Both 1 and 2 are correct.4. None of the above.

28. DGCA has to revalidation the type certificate of an imported aircraft:1. Just as it is 2. It can be modified3. After importing special condition for safe operation 4. It cannot modify it.

29. For revalidation of type certificate of aircraft imported into India which o

f the followingdocuments is not required:1. Type certificate 2. Type design data-sheet3. The basis on ETOPS certification if applicable 4. Quality control and maintenance system manual.

30. The certification of aircraft /aircraft components manufactured in India shall he done byapproved/authorized person as per aircraft rule:1. 53 2. 53A3. 53B 4. 53 C.

31. All relevant inspection records concerning manufacture of an aircraft shallbe preserved for aperiod of:I. two years 2. Four years3. Five years 4. Ten years.

32. Test flight of a newly manufactured aircraft shall be carried out in accordance with:1. Manufactures test flight schedule2. Test flight schedule approved by DGCA3. Both I and 2 are correct.4. None of the above.

33. Prior to carrying out the test to substantiate the design the manufacturer shall submit toDGCA:


37/104

1. Test flight report of the aircraft2. Test flight schedule or scouting and approval 3. Test schedule of scouting and approval 4. None of the above.34. Manuals that should be submitted in respect of a type component/item of equipment forapproval are:1. Type service manual and flight manual

2. Maintenance manual and structural repair manual3. Both I and 2 are correct4. None of the above.

35. A minor modification is one which has appreciable effect on:1. Weight and balance 2. Structural strength3. Flight characteristics 4. None of the above.

36. A major modification is one that shall be:1. Classified as minor modification2. Not classified as minor modification3. Equal to overhaul

4. None of the above.37. Design submitted for type approval shall beer:1. Description title and drawing number2. As in A plus date of issue3. As in 13 plus issue number4. All are correct.

38. If an alteration is made to a drawing then:1. A new issue number will be issued2. Date shall be allocated3. Both 1 and 2 are correct.4. None of the above.

39. If at any time the DGCA feds that the safety of aircraft is jeopardized it can:1. Cancel or suspend a type certificate2. Endorse a type certificate3. Incorporate a modification in type certificate4. All above are correct.

40. For incorporating any modification in type certification of aircraft /aircraft component:1. Approval of DGCA is a must2. Written approval of manufacturer is a must3. Approval of QCM/CEM is a must4. All above are correct.

41. A major modification is a one which has:I. No appreciable effect on the weight and balance.2. No appreciable effect on the structural strength3. Appreciable effect on the reliability and operational characteristic effecting the airworthiness of the aircraft / aircraft component4. None of the above.

42. For type certification of aircraft as per CAR Series EPart-Il Annexure I---------------unmounted photograph of the aircraft have to be submitted: size ---------------------

I. Three, l0 X 15 cm.2. Three, not less than 10 x 15 cm.3. Five, 10 X 15cm.


38/104

4. Five, not less than 10 X 15 cm.

43. For obtaining type certificate of an aircraft the manufacturer has to submitthe followingdimension to the DGCA.I. Length of fuselage2. Length overall, height overall

3. Both I and 2 are correct. 4. None of the above.

44. for obtaining type certificate of a rotorcraft the manufacturer has to submit the followingdimension to the DGCA:1. Length of fuselage2. Overall length3. Diameter of main rotor and tail rotor main rotor blade chard.4. All above are correct.

45. DGCA is empowered to issue/review or revalidate the C of A vide:1. Aircraft rule 5 2. Aircraft rule 15

3. Aircraft rule 15 4. None of the above.46. All aircraft registered in India must posses a current and valid C of A before they are flown isa requirement as per aircraft rule:1. 50 2. 303. 15 4. 50A.

47. The procedure for issuing Indian C of A is given in:I. FSeries Part-I 2. FSeries part-Il3. FSeries part-Ill 4. None of the above.

48. For issue of C of A the DGCA has to satisfy itself that the aircraft/rotorcr

aftmanufactured/imported meets the approved airworthiness standards of:I. BCAR 23 and JAR 25 2. FAR 23 and FAR 253. FAR 27and 29 4. All above are correct.

49. C of A for aircraft, which do not fulfill the airworthiness standards as laid down by theDGCA:I. Cannot be issued/renewed 2. The operator may consult the DGCA ( DAW ) beforebuying / importing such aircraft so that acceptance standards are conveyed to him.3. Both I and 2 are correct.4. None of the above.

50. Application for obtaining C of A is to he submitted on form:1. CA23A 2. CA-253. CA-28 4. CA-27.

51 . Before C of A In respect of an imported aircraft is issued, the DGCA satisfy himself with the:I. Airworthiness standards of the aircraft2. Design standards of the aircraft3. Both 1 and 24. None of the above.52. For aircraft type imported into the country for the first time the documents

accompanying theexport C of A will be:1. A copy of type certificate


39/104

2. Data sheet of the aircraft3. Both 1 and 2 are correct4. None of the above.

53. Aircraft with MTOW greater that 5700 Kg. And categorized as passenger/mail /good shall

have at least engines:1. One 2. Two3. Three 4. None of the above.54. For issuance of C of A for an aircraft type which is imported for the firsttime. theowner/operator shall supply, free of cost to DGCA:I. Airplane flight manual2. Type certification3. MMEL4. All above are correct.

55. The set of documents that shall be submitted to RAO/Sub-RAO of DGCA where th

e aircraft is bused with up to date amendments will he:Aircraft maintenance manual, engine maintenance manual2. Overhaul manual, structural repair manual3. Service bulletins, SSID, CPCP.4. All of the above.

56. For issuance of C of A partially filled Indian C of A will be forwarded by the DGCA:1. To the manufacturer for completion2. To the owner/operator for completion3. To the RAO/Sub-RAO for completion4. All above are correct.57. RAO/Sub-RAO may issue/validate the C of A on the basis of:

1. ExportCofA2. Physical inspection of the aircraft3. Scrutiny of other related documents4. All of the above.

58. The airworthiness officer is required to:Inspect the aircraft to the extent possible2. To establish that all instruments and equipment have been installed and are inserviceable condition.3. Aircraft is airworthy4. All of the above. a

59. The validity of C of A is:I. for one year2. For six months3. Not exceeding one year4. 1 and 3 are correct.

60. C of A validity of imported aircraft is:1. For one year2. for six months3. Beginning from the date of issue of original export C of A.

4. Both 1 and 3 are correct.

61. Short term C of a issued for:


40/104

I. Un-airworthy aircraft2. Aircraft imported from outside the country under Indian registration markiig3. Aircraft imported from outside the country under foreign registration marking4. Aircraft having service life of less than one year.

62. The DGCA may refuse a C of A to an aircraft if:1. He feels like it

2. Required data are not made available3. Reasonable apprehension exists regarding its airworthiness4. Both2 and 3 are correct.63. The document, which must accompany the application for issue of C of A, is:I. Form CA-83 2. form CA-843. Both I are 2 are correct 4. None of the above.

64. Normal category aircraft are:1. Private passenger 2. Goods, banal work3. Passenger, Mail 4. All are correct.

65. Aircraft certified in normal category shall not be used in:

1. Special category 2. Aerobatics category3. Private category 4. Both 1 and 2 are correct.

66. The three general categories of aircraft are:1. Normal, special aerobatics 2. Passenger, mail, goods3. Aerial , private, agricultural 4. Passenger, normal special.

67. Aircraft certificate in normal category can be used:I. In all subdivisions 2. In special category3. In specific sub-division(s) 4. None of the above.

68. Private aircraft:1. Means all aircraft other than aerial work aircraft or public transport aircra

ft2. Shall not be used for here or reward3. Shall not be used for any kind of remuneration4. All above are correct.

69. A state government aircraft certified in normal category subdivision shall be a aircraftI. Passenger 2. Private3. Research 4. Racing.

70. Research aircraft is a subdivision of:I. Normal category 2. Aerobatics category3. Special category 4. Experimental category.

71. Racing aircraft is a subdivision of:I. Normal 2. Aerobatics3. Experimental 4. Special.

72. Aircraft certified in aerobatics category may be used:I. In special category 2. In normal category3. For experimental work 4. For racing.

73. Aircraft and other aeronautical products to be eligible for export to Indiamust meet therequirements of:

1. FAR 15 2. FAR 263. FARAD(87-0l-40) 4. FAR2I.


41/104


42/104

85. The rule that empowers DGCA to issue C of A is:I. Rule 5 2. Rule 153. Rule 50 4. None of the above.

86. Validity period of C of A is limited to a maximum period of:

1. Six Months 2. Nine months3. One year 4. None of the above.

87. Validity period of C of A for all aircraft of over 20 years of age is:1. One year 2. Six months3. Nine months 4. None of the above.

88. Validity of C of A can be extended for:1. 3% 2. 10%3. 0% 4. None of the above.89. Regular and timely renewal of C of A of an aircraft will involve:1. Less effort to the owner/operator

2. Will cost less to the owner/operator3. Both I and 24. None of the above.

90. Operation of an aircraft may apply [or the renewal of C of A along with necessary fees asper:1. RuIe5X 2. Rule6I3. Rule 62 4. None of the above.

91. Application of renewal of C of A should be made preferably days in advance of expiry of C Of A:1. 10 2. 15

3. 15 4. None of the above.

92. For the purpose of renewal of C of A the aircraft would simply be required to be inspected inaccordance with:1. 25 Hrs. inspection schedule 2. 50 Hrs. inspection schedule3. 100 Hrs. inspection schedule 4. None of the above.

93. In case the C of A of the aircraft has expired, for renewal the quantum of work required has to he decided by:I. Officer in charge RAO 2. Operator/QCM3. Manufacturer 4. None of the above.

94 During C of A renewal operator should submit to the concerned airworthiness officer:I. All log books 2. Major maintenance schedules3. Registers 4. All of the above.

95. For renewal of C of A, the operator has to submit to RAO:1. C of A, C of R 2. W/T Licence3. Both 1 and 2 are correct. 4. None of the above.

96. Renewal of C of A Indian registered aircraft abroad: a1. cannot be carried and should be avoided

2. Can be carried out with full justification of such exigencies to the DGCA3. C of A will be renewed in normal manner4. Both 2 and 3 are correct.


43/104

97. C of A shall be cease to be valid of:I. Approved inspection schedule is completed when due2. Lifed components are replaced on expiry of stipulated lives3. Un approved repairs / modification are carried out4. All are correct.

98. If mendatory modification are not carried out as and when called for:I. The C of R will lease to be valid2. The C of A will lease to be valid3. The W/T will lease to be valid.4. All are correct.

99. The AME /approved firm undertaking the C of A renewal work must ensure the availabilityof -------------- for the type of aircraft.1. Up to date technical literature2. Special tools, SSID CPCP , COSL3. List of mandatory modification / inspection

4. All are correct.100. Before the C of A is renewed the operator/owner has to satisfy the airworthiness officer about the --------------- aspects of aircraft since the C of A ofaircraft was last renewal:I. All mandatory modification / inspections have been complied with2. All major repairs and overhauls have been carried out3. The flight manual is amended and up to date4. All of the above.

101. At the time of C of A renewal, the operator must submit to airworthiness office:I. approved test flight report2. A certificate that the radio, communication navigation and radar equipment on

board have been checked for performance.3. All documents relating to log book entries4. All of the above.

102. Aircraft with AUW of 15,000 Kg. And above are required to be maintained by:1. Individual AMEs 2. Airlines3. Approved organizations 4. All are correct.

103. Certificate of maintenance review in cases of aircraft with AUW of 15,000 Kg. And above isissued by:1. DGCA 2. RAO3. QCM 4. All are correct.104. Aircraft with AUW more than 15,000 Kg. Can maintained by:1. Individual AMEs 2. Authorized personnel3. Approved organizations 4. All are correct.

105. Certificate of maintenance review of case of aircraft with AUW of 15,000 Kg. And below isissued by:1. Individual AMEs2. AME having his Licence endorsed in category Bto cover the type of aircraft inlv ed3. AME having his Licence endorsed in category Dto cover the type of engine invo

lved4. Both 2 and 3 are correct.


44/104

106. If the airworthiness officer completes the final inspection of the aircraftand its documentafter the expiry of the C of A then the validity of the next currency of C of Awill start from:1. The date of inspection 2. The expiry of last C of A3. The date of submitting the application 4. All are correct.

107. Application for renewal of C of A is submitted on form:1. CA25 2. CA 283. CA23 4. AS PER GIVEN FORMAT.

Prepatory Exam CA Series: E Part-I and II1. A firm approved in category A carries out:a) Maintenance of aircraft b) Manufacture of aircraftc) Testing of aircraft d) Both A and B are correct.

2. A firm approved for carrying out NDT of aircraft is approved in category:a) A b) B c) C d) E.

3. A organization approved for carrying out propeller overhaul is approved in category:a) A b) B c) C d) None of the above.

4. A firm approved for carrying out C of A of aircraft belongs to category:a) B b) C c) D d) E.

5. A firm approved for carrying out repair and flight testing of Avionics set isin category:a) A b) E c) D d) C.

6. An organisation under taking calibration of instruments of master-gauges and

tools as applied to the activities of CAD is approved in:a)A b) D c) E d) F.7. A firm carrying out chemical analysis is approved in:a) Category E b) Category Dc) Both A and B are correct d) None of the above.

8. Firm approved in category F can carryout:a) Maintenance of aircraft b) Manufacture of aircraftc) Distribution of fuels/lubrication d) None of the above.

9. Aircraft goodsmeans:a) Aircraft components and items of equipmentb) Aircraft components or materialsc) Aircraft components or materials, including special petroleum products.d) Both A and B are correct.

10. Certificate of approval means a document issued by:a) DGCA to an approved organization giving the scope of approval.b) An approved organization defining the scope of the approval.c) An organization stating is approval in any particular category.d) None of the above.11. A document accompanying the sale of aircraft components, spares, materials,goods and certifying that the same were obtained from an approved source it termed as:a) sales certificate b) Delivery note

c) Release note d) None of the above.

12, rejection note is a document issued by:


45/104

a) DOCA b) RAO c) Approved organization d) Both A and B are correct.

13. The QCM and the deputy QCM are approved by:a) Airlines chief Engineer b) Managing Director of the organization.c) Technical Centre d) DGCA

14. A nodal officer is to be appointed by:

a) Owner/operator of state govt. b) Owner/operator of private category aircraft.c) All scheduled/non-scheduled operator d) Both A and B.

15. An organization seeking approval in any of the categories A-G, should applyto:a) RAO b) DGCAc) DGCA through the nearest regional office d) Any of the above.

16. An organization seeking approval in any of the activities under any category(series-E) shall apply on prescribed form:a) CA 182 b) CA-9c) CA-28 d) None of the above.

17. An organization seeking approval will Preferably submit:a) Two different types of manual b) Three different types of manualc) Three different types of manual in three copies eachd) None of the above.

18. Three different types of manual are:a) QC, MS and Engineering organization manualb) QC, MS and repair manualc) QC, MS and engine overhaul manuald) QC, MS and engine repair manual.

19. Engineering organization manual is approved by:

a) DGCA b) RAOc) DGCA in consultation with RAO d) None of the above.

20. Quality control cum Quality Assurance manual for scheduled operator is approved by:a) DOCA b) RAOc) DGCA is consultation with RAO d) QCM.21. The manner of preparing inspection schedule and assigning periodicity, whenever applicable inrespect of periodic maintenance is contained in:a) Engineering organization manual b) Qc cum Assurance manualc) MS manual d) None of the above.

22. Maintenance system manual is approved by:a) DGCA b) RAOc) DGCA in consultation with RAO d) RAO in consultation with DGCA.

23. The procedure for duplicate inspection of flight and engine controls is listed in:a) QC cu

A.m.e Question Paper 1

Documents

Transcript of A.m.e Question Paper 1