Question Bank Elec &Recorders Level 2(15-II)

8/8/2019 Question Bank Elec &Recorders Level 2(15-II)

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Question bankDesign Electrical and Recorders, AURDC-NASHIK, level- II

1. AUTs-30 in Su-30MKI use for (a) Locating the target for R-73E missile.(b) Communication System.

(c) Target Designation Device for X-31P Missile.(d) For Landing & Take off.

2. Which one is not Air to Air Missile-(a) R-73E(b) RVV-AE.(c) X-29L.(d) R-27R

3. Which one is not Air to Ground Missile (a) X-29L(b) X-29T.(c) X-59ME.

(d) RVV-AE.

4. Cluster Bombs are-(a) Laser Guided.(b) TV Guided.(c) Heat Seeking.(d) None of Above.

5. Gun use in Su-30MKI is(a) Mouser.(b) Revolver.(c) TACAN.(d) Gsh-30-1.

6. Laser Designation Pod (LDP) installed in Su-30MKI Aircraft at Station Number-(a) 1.(b) 2.(c) 3.(d) 4.

7. KAB-1500KR is a (a) Unguided Bomb.(b) Guided rocket.(c) Guided Bomb.(d) All three.

8. Three different mode of Weapon Control System (WCS) (a) Automatic, Autonomous & Emergency.(b) Automatic ,Active & Passive.(c) Active ,Passive & Emergency.(d) Active Autonomous & Emergency.

9. Radio proximity fuse use in (a) Air to Air Missile.(b) Air to Ground Missile.

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(c) Air to Sea Missile.(d) Not use in missile.

10. Weapon Control System (WCS) use processor-(a) 8080.(b) 8085.

(c) 8086.(d) None of above.

11. AUTs-30 does not interface with (a) RIF.(b) RWR.(c) WCS.(d) Fuel System.

12. Which one is not Adapter Beam-(a) 11.8401.I.005.000.(b) 11.8801.I.050.901.(c) 11.8804.I.005.901.

(d) 11.MBD3.I.U6.901.

13. Abbreviation of AREE is-(a) Air Radio Electronic Equipment.(b) Air Radar Electronic Equipment.(c) Air Borne Electronic Equipment.(d) Aerial Electronic Equipment

14.One among the following is not a function of autopilot

(a) Attitude & heading hold(b) Bringing aircraft to level flight

(c) Attitude sensing(d) Path control

15.Dutch roll is related to

(a) Roll channel(b) Pitch channel(c) Roll & pitch channels(d) Roll & yaw channel

16.Heading hold signal for an Automatic flight control system are supplied to

(a) Yaw channel(b) Roll channel(c) Pitch channel

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(d) Roll & yaw channel

17.In case of spatial disorientation, the pilot engages which mode of Autopilot system

(a) Damper mode(b) Level Mode

(c) Stabilisation mode(d) All of the above

18.AFCS mode engaged using button located on control stick

(a) Damper mode(b) Level Mode(c) Stabilisation mode(d) Critical altitude mode

19.Which is not the category under aviation autopilot categories by ICAO

(a) CAT I(b) CAT II(c) CAT IIIA(d) CAT IV

20.In many flight control system the detection of error signal is accomplished by

(a) Synchro(b) Demodulator(c) Limiter(d) Integrator

21.In connection with command signal processing, the function of adapting controlsystem response to an aircraft handling qualities is known as

(a) Limiting(b) Integrating(c) Gain programming(d) Demodulating

22.In control channel of automatic flight control system synchro type used is

(a) Torque synchro(b) Differential synchro(c) Resolver synchro(d) Control synchro

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23.To which part of a selsyn system is the power supplied

(a) Stator(b) Rotor(c) Both stator & rotor(d) None of the above

24. In Su-30 MKI which of the following MFD has largest size

(a) MFD 1.1(b) MFD 1.3(c) MFD 2.4(d) MFD 2.1

25.At supersonic speed, wing position of MiG-27 aircraft is at ____ degree

(a) 16(b) 30(c) 45(d) 72

26.Main instrument board of MiG-27 aircraft is tilted at ___ degree w.r.t vertical plane.

(a) 10(b) 5(c) 8(d) 6

27.___ material is used for major load carrying frame.

(a) D20AM(b) D19AT(c) AMG6BM(d) V95

28 .UTS of aluminum alloy D16 is ____

(a) 30

(b) 20(c) 40(d) 35

29.Aluminum alloy of ____ grade is weldable.

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(a) D16AM(b) D19AT(c) D16AT(d) D20AM

30.3170A screw is made from ______ material.

(a)30KHGSA(b) C10(c) LS59(d) D19

31.Radome is made from ________ material.

(a) Aluminum(b) Teflon coated fiber optic glass(c) Steel(d) none of above

32.3181A is ____ degree countersunk screw.

(a) 100(b) 120(c) 90(d) 45

33.VOR/ILS antenna is located _______ in SU-30MKI aircraft.

(a) In nose cone(b) In front of cockpit(c) In tail boom(d) In wing

34.INCOM control panel is located on ________ in cockpit of MiG-27 upgrade aircraft.

(a) Main instrument panel(b) RH console

(c) LH console(d) None of above

35. The capacity of each storage battery 15TSS-45B used on MiG-21 Aircraft is

(a) 45AH(b) 35 AH(c) 50 AH(d) 40AH

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36. During lading the flaps are selected to ______________0

(a)250

(b)500

(c) 160

(d)720

37. The service ceiling of Su-30 Aircraft is_________

(a) 17.5 km(b) 10 km(c) 25 km(d) 27.5 km

38. Single piece windshield is the feature of MiG-21, __________Aircraft

(a) T-77(b) T-96

(c) T-75(d) BisUpgrade

39. On MiG-27 Aircraft, with wing drop tank suspended, the Aircraft can be used onlyat wing sweep angle ___________

(a)160

(b)720

(c) 450

(d)250

40. The S, S2 & S3 openings on pitot static tube of aircraft are for dynamic pressure.

(a) True(b) False

41. The TTL/TCL life of MiG-27 aircraft is _____________________ hours.

(a) 30/1800(b) 40/3600(c) 40/3000(d) 35/3600

42. The max Mach No. For T-96 is _____________________.

(a) 2.1(b) 2.05(c) 1.7

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(d) 2.0

43. The Max Mach No. For T-77 is _____________________.

(a) 2.05(b) 2.1.(c) 1.7(d) 2.0

44.The TTL/TCL of BISON aircraft is _____________________.

(a) 35/3400(b) 30/1800(c) 40/3600(d) 41/3600

45. Cone additional extension on T-75 aircraft is___________mm.

(a) 15(b) 16(c) 17(d) 13 & 17

46.. Engagement of second A/B in T-75 aircraft is possible below__________km.

(a) Four(b) seven(c) three(d) nine

47. Take off speed of MiG-27 aircraft is_____________ kmph.

(a) 315(b) 345(c) 320(d) 300

48. Take off speed of T-75 aircraft is_____________kmph.

(a) 315(b) 345(c) 320(d) 300

49. Take off speed of T-96 aircraft is ___________kmph.

(a) 315(b) 345

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(c) 320(d) 300

50. Landing speed of MiG-27 aircraft is _____________kmph.

(a) 260

(b) 270(c) 245(d) 260

51. Landing speed of T-75 aircraft is_____________kmph.

(a) 260(b) 270(c) 245(d) 260

52- Landing speed of T-96 aircraft is_____________kmph.

(a) 260(b) 270(c) 245(d) 260

53. Landing speed of T-77 aircraft is_____________kmph.

(a) 260(b) 270(c) 245(d) 260

54. What Inventory of chaff & flare will display on Control Panel, when chaff 1x1 &flare 2x1 cartridges are loaded?

(a) C-30 F-30(b) C-15 F-15(c) C-30 F-15(d) C-15 F-30

55- In factory setup of fisting controller, at what inventory of chaff & flare will flickeras a critical quantity?

(a) C-3 F-6(b) C-6 F-3

(c) C-3 F-3(d) C-6 F-6

56. What error message will indicate on Control Panel after pressing Dispenseswitch when one of the interlocking is not mate?

(a) NO RESP(b) NO CAP(c) NO FIRE

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(d) IN FIRE

57.In flight, aircraft turn is executed with correct bank angle and with matched

airspeed, then aircraft will be in ..(a) Slip

(b) Skid

(c) Co-ordinated turn

(d) Critical angle of attack

58.The gyroscope utilized in a stabilized platform of inertial navigation system are of

the ..

(a) Displacement type

(b) Rate integration type

(c) Laser type

(d) Light type

59.NAVSTAR GPS satellite system is launched by

(a) India

(b) Russia

(c) America

(d) Europe

60.The pressure of the atmosphere

(a) Increases non-linearly with height

(b) Decreases non-linearly with height

(c) Decreases linearly with height

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(d) Remains constant with height

61.NAVSTAR GPS satellite system is made up of a constellation that comprises

..satellites distributed on 6 circular orbits.

(a) 24

(b) 20

(c) 18

(d) 06

62.L1 frequency for NAVSTAR GPS satellite system is ..

(a) 1575.42MHz

(b) 1475.42MHZ

(c) 1675.42MHz

(d) 1375.42MHz

63.For detection of aircraft turns, a ..is used.

(a) Rate gyroscope

(b) Flux gate detector

(c) Pressure head

(d) non of above

64.In case of gyroscope, gyro-motor speed is around .

(a) 2000 rpm

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(b) 22000 rpm

(c) 10000 rpm

(d) 8000 rpm

65.Two fundamental properties of gyroscope are

(a) Rigidity and precession

(b) Rotation and revolution

(c) Elasticity and electricity

(d) Stability and controllability

66.Earth rotation rate on the equator is

(a) 15 / hour

(b) 20 / hour

(c) 17 / hour

(d) 14 / hour

67.Setting the barometric pressure to make altimeter to read airport elevation above

sea level on landing and take off, is

(a) QFE

(b) QNH

(c) QNE

(d) QHE

68.Setting the barometric pressure to make altimeter to read airport elevation zero

on landing and take off, is

(a) QFE

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(b) QNH

(c) QNE

(d) QHE

69.INGPS system used on SU-30MKI aircraft is able to receive the signals from

satellite systems.

(a) only GPS

(b) only GLONASS

(c) Both GPS and GLONASS

(d) Only GALILEO

70-.Total number of cells in Battery for SU-30 MKI are(a) 12(b) 15(c) 10(d) 16

71.Total travel of cone movement in auto mode is ---------- mm(a) 125

(b) 145(c) 155(d) 200

72-.Medium used for RADAR cooling on MIG-21 T-75 aircraft is(a) air(b) alcohol(c) air+alcohol(d) none of these

73-.Flight Data Recorder used on MIG-21 E7FL aircraft is(a) K2-717(b) SARPP-21G(c) K2-417(d) U3L

74.Total number of parameters recorded in FDR for MIG-21 E7FL aircraft(continuous+ event) are:

(a) 2(b) 6(c) 10(d) 11

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75-.Additional extension of cone in MIG-21 T-96 aircraft are --------- mm(a) 13 & 17(b) 10 &15(c) 12 &16(d) 14 & 19

76-.Engine starting cycle for R-29 engine is ------- sec

(a) 45(b) 44(c) 40(d) 50

77.Total number of afterburner engagement in R-25 engine are

(a) 1(b) 2(c) 3(d) 4

78.Emergency jet nozzle operates the Jet nozzle in ------------- positions(a) 2(b) 3(c) 4(d) 5

79.It is prohibited to leave the relight circuit breaker cut in for longer than ----- Sec inMIG-21 BISON aircraft

(a) 30(b) 40(c) 45

(d) 50

80-.The engine oxygen system will permit ------ attempts at engine relight for MIG-21BISON aircraft provided the relight circuit breaker is kept on for not more than 30 secat each of the attempt

(a) 3(b) 4(c) 5(d) 6

81-.Maximum permissible Angle of attack in en route configuration is ________ Deg forMiG 21 BIS/BISON ac.

(a) 22(b) 24(c) 26(d) 28

82-.Maximum permissible high pressure rotor RPM for R25 engine is not more than__________ %

(a) 104.5(b) 105.5

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(c) 106.5(d) 107.5

83-.Maximum permissible Jet pipe Temperature must not exceed _________ Dec C atreheat setting and at emergency reheat power setting.

(a) 770

(b) 820(c) 850(d) 860

84.Negative g loads may be developed for not longer than ______ sec at enginepower settings not higher than full throttle setting for MiG 21 series aircraft

(a) 5(b) 10(c) 15(d) 20

85-.The total time of operation in R25 engine in flight at all power setting with airbleeding for BLC system must not be more than __________ minutes.

(a) 3(b) 4(c) 5(d) 6

86-.W hen negative g loads are pulled at all altitudes, oil pressure will drop to zerofor a duration of -------- sec on MiG-21 BIS/BISON ac.

(a) 15(b) 16(c) 17(d) 18

87.The reservoir within the inner ear is called

(a) Vertigo(b) Common sac(c) Flicker vertigo(d) None of above

88.Hypoxia stands for

(a) Oxygen starvation

(b) Air starvation(c) Low pressure(d) Low temperature

89.Northerly turning errors of magnetic compass becomes greater nearer to

(a) Same at every place

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(b) Nearer to poles(c) Nearer to equator(d) Can not say

90-.With conventional gyro during take off attitude indicator has tendency to

(a) Read nose high(b) Read nose low(c) Both a) & b)(d) Level flight

91.APUS is

(a) Stability augmentation system

(b) Angle of attack indicator(c) (a) &( b)(d) Non of above

92.LSA system is used on

(a) MiG 21 BIS(b) MiG 21 Type 77(c) MiG 27 Upgrade(d) MiG 21 BISON

93.In MiG-21/27 variants Hydraulic system pressure is developed by pump of type

(a) Variable delivery piston pump(b) Constant delivery pump(c) Oil gear pump(d) Vane pump

94.Number of pistons in hydraulic pump of MIG-21/ MIG-27 aircraft(a) 3(b) 5(c) 7

(d) 9

95.In MIG-21 variants in case of Booster Hydraulic system failure pressure isdeveloped by emergency pump of type

(a) NP-17(b) NP-27(c) NP-54(d) NP-37

96.Which service is not operated by booster system in MIG-21 Variants

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(a) Air Brakes(b) Aileron(c) Stabilizer(d) All of the above

97.Pneumatic system pipeline in MiG-21 / 27 aircraft is painted

(a) Blue(b) Green(c) Brown(d) Black

98-.Low pressure pipeline of hydraulic system in MiG-21 aircraft is painted in(a) Blue(b) Grey(c) Brown(d) Yellow

99.Pneumatic system pipeline in SU-30MKI aircraft is painted completely in(a) Blue(b) Black(c) Yellow(d) Green

100.In SU-30 MKI aircraft, incase of failure of hydraulic pump regulator pressure inhydraulic system is maintained at 320 kg/cm by

(a) GA-186M-5(b) KE-53-6(c) GA-135T(d) KE-53-8

101.Hydraulic oil capacity in each system of SU-30 MKI aircraft is(a) 30 Litres(b) 40 Litres(c) 50 Litres(d) 20 Litres

102.Purity class of hydraulic fluid in SU-30MKI aircraft as per GOST-17216 is(a) 4(b) 6(c) 8(d) 10

103.What is landing speed of MIG- 21 aircraft in clean configuration?

(a) 270 IAS

(b) 300 IAS(c) 230 IAS(d) 430 IAS

104.What is balance speed of MIG-21 aircraft?

(a) 750 +-100 IAS(b) 700 +-100 IAS(c) 850 +-100 IAS

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(d) None of above

105.Which unit is responsible for providing uniform piloting?

(a) Artificial feel unit (AFU)(b) Automatic transmission ratio control unit (ARU)

(c) Booster(d) None of above

106.ARU works based on

(a) Static and Dynamic Pressure(b) Hydraulic pressure(c) Pneumatic pressure(d) Oxygen pressure

107.Dmean adjusted for

(a) Longitudinal balancing(b) Lateral Balancing(c) Directional Balancing(d) None of above

108.Max. Armament load capacity of MiG-21 Bis. A/c is(a) 980kg(b) 1000kg

(c) 1500kg(d) 2000kg

109.MiG-27 Upgrade a/c carries Laser Designator Pod on station no.(a) 1(b) 2(c) 3(d) 7

110.P-72-1DB2 is a(a) Rail launcher(b) multiple ejection rack(c) catapult launcher(d) missile

111.AKU-170E is a(a) Rail launcher(b) catapult launcher(c) bomb rack(d) aircraft tyre

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112.APU-470M is a(a) Rail launcher(b) Bomb Rack(c) zero length launcher(d) gun

113.AKU-470 is a(a) rail launcher(b) gun(c) Bomb rack(d) zero length launcher

114.P-62-IMD is a twin launcher(a) True(b) False

115.MiG-27 Trainer a/c (Twin seater) has no. Of weapon station.(a) 1(b) 2(c) 3(d) 4

116.The PTS-250S inverter in MiG-21 BISON is installed in(a) Conformal container(b) nose(c) cockpit(d) Fuselage

117.The PTS-250S inverter in SU-30MKI a/c is installed in the(a) Station adapter beam(b) bomb rack BD3(c) nose cone(d) Fuselage

118.The MiG-21 BISON a/c has ______ no. of static inverter PTS-250S(a) 1(b) 2(c) 3(d) 4

119.The MiG-21 BISON a/c has_______ no. of rotary inverter type PO-750A

(a) 1(b) 2(c) 3(d) 4

120.In MiG-27M aircraft the gun pod SPPU-22 of can be carried on(a) Wing stations only(b) Fuselage stations(c) Wing & Fuselage stations

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(d) Centerline fuselage stations only

121.The BD3-60-21D1racks in MiG-21 Bis aircraft release store by(a) Ejector release unit(b) Electromagnetic Release unit(c) Rail launch unit

(d) Catapult launch unit

122.Hydraulic system pressure in SU 30 MKI is

(a)210 kg/cm2(b)280 kg/cm2

(c) 250 kg/cm2

(d)330 kg/cm2

123.Following is used in SU-30 MKI aircraft to increase the Longitudinal stability(a) Rudder(b) Stabilizer(c) Canard(d) None of the above

124.In SU-30 MKI aircraft, incase of hydraulic system failure, the following system isalso operated by pneumatic system.

(a) Wheel brakes(b) Refueling probe extension(c) Landing gear extension(d) Both b & c

125.Thrust vector control in SU-30 MKI aircraft is operated by

(a)1st

Hydraulic system(b)2nd Hydraulic system(c) Both a & b(d) None of the above

126.What is Angle of attack?

(a) Angle between chord line and free stream air(b) Angle between stabilizer and fuselage center line(c) Angle between stabilizer and Flap center line(d) Angle between Aileron and Flap center line

127.In straight & Level flight forces are to be considered

(a) Lift = Drag & Thrust = Weight(b) Lift = Thrust & Weight = Drag(c) Lift = Weight & Thrust = Drag(d) None of above

128. In aircraft Boundary layer control used during

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(a) Hydraulic power ON(b) Electric Power ON(c) Hydraulic Power OFF(d) None of above

136.In which Type Mig-21 aircraft boundary Layer control system does not exist?

(a) T-69(b) T-77(c) T -96(d) T-75

137.In snag sheet, L & D balancing stands for

(a) Lift & Drag balancing(b) Lateral & Directional balancing(c) Left & Down Balancing(d) None Of above

138.Trim speed of aircraft is also known as(a) Longitudinal balancing(b) Lateral balancing(c) Directional Balancing(d) None Of above

139.In aircraft Oxygen is required for

(a) For Pilot only(b) For Engine only(c) For Pilot and Engine(d) None of above

140.Canard is also known as

(a) Fore plan(b) Tail plane(c) Stabilizer(d) None of above

141.Flaperons are deflected

(a) In similar direction only(b) In opposite direction only(c) In both a and b(d) None of above

142.The stalling angle is that after which

(a) Aircraft lift increase(b) Aircraft drag increase(c) Aircraft angle of attack cannot increase further(d) none of above

143.Advantage of using fly by wire system is

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(a) To reduced weight and complexity(b) To increase lift(c) To increase lift and reduced drag(d) none of above

144.In aircraft trim motor are used for

(a) Reducing lift(b) Reducing Weight(c) Reducing Thrust(d) Reducing load from control stick

145.Service ceiling of aircraft means

(a) Maximum attainable height(b) Minimum attainable height(c) Aircraft always fly(d) None of above

146.MIg-27M avionics Up gradation activity is caviled out at birch of the following HALdivisions:(a) Nasik(b) Bangalore(c) koraput(d) kanpur

147.MiG-21 is a:(a) Flight aircraft(b) helicopter(c) turbo prop a/c(d) Transport aircraft

148. MiG-21 Bison a/c has no. of weapon station.(a) 1(b) 2(c) 3(d) 5

149.SU-30MKI a/c has no. of weapon station.(a) 6(b) 10(c) 8(d) 12

150.SU-30MKI a/c has built in gun of(a) Single barrel(b) twin barrel(c) six- barrel(d) Five barrel

151.Battery capacity of MiG-21 a/c is of(a) 45AH(b) 80AH

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(c) 21 AH(d) 16 AH

152.Max. Armament load that can be carried on MiG-27 a/c is(a) 200kg

(b) 3000kg(c) 4000kg(d) 1000kg

153.Capacity of ventral drop tank of MiG-27 a/c is(a) 800l(b) 490l(c) 650l(d) 7730

154.MiG-21 a/c can carry a maximum of nos. of fuel drop tanks(a) 5(b) 3(c) 4(d) 2

155.MiG-27 a/c can carry a maximum of nos. of fuel D/Ts(a) 3(b) 2(c) 1(d) 6

156.SU-30MKI a/c can carry laser-guided missile of type(a) Air-to-air(b) Surface-to-air(c) Air-to- surface(d) Air to Water

157.The weapon control system of MiG-27 a/c is called(a) SUV-2-26L(b) PRRV-23L(c) SUV-27(d) SUO-27M

158.R-73E is a

(a) Heat seeking missile(b) laser-guided missile(c) TV guided missile d) missile(d) Unguided Missile

159.SU-30MKI a/c has canard configuration(a) Yes(b) No

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160.The radar installed in MiG-21 Bison a/c is(a) Elta(b) INCOM(c) KOPYO(d) Almaz

161.MiG-21 Bison a/c has got no. of MFDs in cockpit(a) 1(b) 2(c) 3(d) None

162.In SU-30MKI a/c, fitment of gun is at(a) RH-side(b) LH-side(c) center line bottom(d) Upper side

163.S-24B is a(a) Unguided rocket(b) guided missile(c) bomb(d) six- barrel gun

164.Missile lock on audio tone is MiG-21 Bison a/c is(a) Controllable(b) Uncontrollable(c) Can not say(d) None of above

165.Ejection seat used in SU-30MKI a/c is(a) KM-1M(b) K-36P-3.5E(c) K-3M5(d) KM-2M

166.Twin seater Trainer a/c of MiG-21 a/c is called(a) MiG-21 T-96(b) MiG-21 T-69(c) MiG-21 T-75(d) MiG-21 T-77

167.MFD used in MiG-21 Bison a/c is of(a) Russian origin

(b) French origin(c) Israeli origin(d) Indian origin

168.Inverter used on MiG-21 Bis is of type.(a) Rotary(b) static(c) engine driver

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(d) Self Driver

169.No. Of storage batteries used on MiG-21 Bis a/c is(a) One(b) two(c) three

(d) four

170.The film movement in gun camera S SH 45 on MiG-21 a/c is operated by(a) Switching on radar(b) switching on gun sight(c) switching on power supply(d) Pressing timing button or gun trigger

171.R-73E missile is carried on MiG-21 T-77 a/c(a) True(b) false

172.Inverter PT-500 Ts is installed in the cockpit of MiG-21 a/c(a) True(b) false

173.Inverter PO-1500 VT generates(a) Single phase, 115V, 400Hz AC Supply(b) Three phase, 115V, 400Hz AC Supply(c) Three phase, 36V, 1000Hz AC Supply(d) Single Phase 36 V AC supply

174.Engine auto relighting system operates MiG-21 a/c during(a) Release of bombs(b) firing of gun(c) firing of rocket & missile(d) Automatic

175.The MiG-21 a/c Inverter PTO-1000/1500 M is located in the(a) Nose(b) Cockpit(c) Rear fuselage(d) Rear equipment bay

176. The inverter PO-750A Generator(a) 36V, 3, 400 Hz AC supply(b) 36V, 3, 1000Hz AC supply

(c) 1, 115V, 400Hz AC supply(d)3, 115V, 400Hz AC supply

177.AC Generator installed on MiG-27M aircraft is(a) GSr57-12/40D(b) SGK-30/1.5(c) PGL-30(d) KZU

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178.RNU-204K unit on MiG -27 aircraft is

(a)AC voltage regulator(b) DC

(c) Over-voltage pop-up circuit breaker

(d) Under voltage protection unit

179.IN Su-30MKI aircraft in-flight refueling pod is carried on(a) Using station(b) Fuselage station(c) Station 7(d) Station 12

180.Su-30 MKI aircraft can configured as in-flight refueling tanker(a) True(b) False

181.IN Su-30MKI aircraft the wing tip stations can be used to carry(a) R73E missiles only(b) RV-E and R-73E missiles only(c) R-27R,RW-E & R73E missiles(d) R-60 Missile

182.In Su-301MKI aircraft the bullet carrying capacity or max rounds that can be firedin

(a) 150(b) 260(c) 300(d) 325

183.In MiG-27M aircraft the fuel reminder warning indicator comes on in cockpitwhen total fuel capacity becomes

(a) 600L(b) 700L(c) 800L(d) 750L

184.In MiG-21 aircraft the fuel reminder warning indicator comes on in cockpit whentotal fuel capacity becomes

(a) 450L(b) 650L

(c) 800L(d) 500L

185.In MiG-21Bison aircraft the outboard wings station can carry fuel drop tanks ofindividual capacity

(a) 800L(b) 490L(c) 660L(d) 900 L

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186.The storage battery type for 27V DC power used Su-30MKI aircraft is of(a) Ni-Cd(b) silver zinc(c) lithium

(d) Pb battery

187.No. of chaffs/ flares reminder is displayed on the MFDs in Su-30MKI aircraft on(a) TSD page(b) RWR page(c) MASD page(d) MFWS page

188-.Minimum number of satellite required to cover whole earth-

(a) 2

(b) 3

(c) 4

(d) 5

189.Armament loaded availability readiness & selection is displayed on the MFDs ofSu-30MKI aircraft in the

(a) TSD page(b) RWR page(c) MASD page(d) MFWS page

190.The firing of built in gun in the belly part of MiG-27 aircraft is not interlockedwith the MASTER switch

(a) True(b) False

191.The HUD unit in Su-30MKI aircraft gives display stations suspension of armament(a) True(b) False

192.Main Braking in SU-30 MKI aircraft is performed by depressing

(a) Brake lever on control stick(b) Rudder pedal toe deflection(c) Button on control stick(d) None of the above

193.Pneumatic system in SU-30 MKI aircraft uses working medium as

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(a) Air(b) Nitrogen(c) Halon(d) Both a & b

194.Air intake panel control system in SU-30 MKI aircraft is(a) ARM-70(b) ARV-40(c) ARB-20(d) None of the above

195.Brakes in SU-30 MKI aircraft is provided on(a) All the wheels(b) Only main wheels(c) Only nose wheel(d) none of the above

196-Which of the following is the most economical method of starting a single-phase

motor?

(a) Resistance start method (b) Inductance start method(c) Capacitance start method (d) Split-phase method

197- Out of the following motors, which will give the highest starting torque?

(a) Universal motor (b) Capacitor start motor

(c) Shaded pole motor (d) All have zero starting torque

198- A universal motor is one

(a) which can run on any value of supply

voltage

(b) which has infinitely varying speed

(c) which can operate on AC as well asDC voltage

(d) which can work as single phase orthree phase motor

199-. The short circuit test on a transformer determines

A) eddy current loss B) hysterisis loss C) iron loss D) copper loss

200- The brushes in an electrical machine are made of

A) carbon B) copper C) rubber D) mild steel

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Question Bank Elec &Recorders Level 2(15-II)

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Transcript of Question Bank Elec &Recorders Level 2(15-II)