#1. In a turn at constant rate, turn indicator reading is
#2. What shall be apparent wander on DGI when flying on a Northerly track from 5S to 5N
#3. Both ball and the needle of the TSI are displaced to the right, A/c is
#4. The needle is displaced to the right and ball is displaced to the left in TSI, A/c is
#5. What would be immediate indications when left engine fails in climb?
#6. If ball and needle are displaced to the left in a turn, the ball can be centralized by
#7. A DGI is basically a:
#8. Inputs to FMS include
#9. What happens when FMC auto tunes DME & does not receive a satisfactory code
#10. The altimeter indicates true altitude:
#11. TAT is ……. than…… by an amount which is proportional to _
#12. SSR is a form of ….. radar with …. type emissions operating in the ….. band:
#13. Formula for TAT is
#14. TAT is
#15. A Rosemount probe employs an electrical heater to
#16. Arrow symbols on TCAS indicate
#17. What is principle of TCAS-II
#18. TCAS indicates relative height as
#19. Aircraft is tracking from NDB ‘A’ to NDB ‘B’ on a track of 050 (T). Aircraft HDG 060 (T) RBI indicates R.B. of NDB ‘A’ 180 and R.B. of ‘B’ as 330, aircraft is
#20. In order to Tune, Identify, Monitor non A1A NDB, the BFO should be ‘ON’ as follows
#21. DOC of NDB can’t be guaranteed by night because of
#22. In ADF the night effect is most pronounced
#23. Aircraft HDG 189. Maximum Quadrantal errors will be experienced if the NDB bears
#24. Aircraft is homing to VOR. Aircraft is on radial 152. Pilot has set 329 on the OBS, CDI would indicate (assuming 5 dots VOR)
#25. Aircraft on ILS approach path is receiving stronger 150hz signals than 90hz signals. The correct action to capture LLZ and glide nath would be to fly ..
#26. The indications from basic RNAV are erratic the reason is likely to be
#27. Ground controller will ask the pilot to cancel mode ‘C’ if discrepancy in altitude is more than …..and altimeter subscale is _?
#28. The transmission freq. of DME is 63 Mhz removed from aircraft interrogatory freg. to prevent
#29. The position used by FMC is
#30. The most significant errors of GNSS is
#31. Initial range calculation at receiver is known as pseudo range because it is yet to corrected for
#32. When turning through 180′ at constant attitude & bank angle a classic A/H indicates
#33. Aircraft magnetism is caused by hard iron:
#34. Which of the following statement is correct concerning TCAS-II?
#35. AWR is an example ….. of radar operating on freq of ….. in the ….. band
#36. You are using Doppler VOR, which statement is true?
#37. Aircraft ‘A’ is homing to NDB ‘PL’ on track 060M with 11 port drift. Aircraft ‘B’ is maintaining an outbound track of 320M with 13 S drift from the same NDB. What would be R.B. of aircraft A & B from NDB .PL’.
#38. Pilot hears a morse code as TST from NAV aid this means
#39. In GPS, the number of satellites needed to perform RAIM functions without isolating the faulty satellite is
#40. VOR which continues to transmit bearings but stops to transmit its identification
#41. Examples of secondary radar are
#42. Deviation due to co-efficient A is mainly caused by
#43. WX radar returns are available in the following EFIS / EHSI modes:
#44. In Plan mode the plan route display
#45. An armed mode on an EFIS EADI display will appear as
#46. What does a Radio altimeter measure of an a/c in landing configuration?
#47. Warning flags of FD on ADI will indicate failure of
#48. The magnitude of error in position lines derived from ADF bearing that are affected. by coastal refraction may be reduced by
#49. With automatic FD system in VNAV and LNAVmode, engaging second AP will
#50. LVL CHG, V/S and VNAV mode are inhibited when:
#51. For auto landing to continue below_1500’AGLwhichofthe following conditit must be satisfied?
#52. When a/c climbs at constant rectified airspeed; the TASwill …&the Machno,will
?
CHICKEN TIKKA MASALA
#53. GPWS mode 3 is active between
#54. What type of sensor is normally used to measure inlet air temperature where the signal is to be employed for altitude compensation in a conventional (Non-FADEC) engine fuel system?
#55. A flight control unit in FMS
#56. In order to know which mode of auto throttle is engaged, crew will check
#57. In an a/c which requires Mach trim system it will apply inputs to horizontal stabilizer.
#58. What happens to the glide slope signal at 50′ AGL in auto land?
#59. FMS is
#60. A TAT probe measures using the relationship?
#61. Control wheel steering (CWS) is engaged by
#62. An ADF is tuned to an NDB the needle is hunting the signal is fading growing louder alternatively the reason is
#63. If an alert message is generated by FMS:
#64. The frequency range of VOR receiver is:
#65. Function of INS stable platform is to
#66. In remote indicating compass the annunciator light will come on when
#67. In FMS the phases of flight are
#68. In AWR conical beam is used for mapping for distance
#69. Preventive R.A in TCAS includes
#70. If an alert msg is generated by FMS
#71. A/C goes around after descending to R. altitude of 190′ GPWS will provide alert w. A/C has lost about:
#72. On an EFIS tuned NAV aids are depicted
#73. You are approaching NDB on track 045, If you are drifted to the right
#74. According to Doc 8168, a pilot flying an NDB approach must achieve a tracking accuracy within …… of the published approach track:
#75. An a/c is Homing on to an NDB maintaining a RB of 0′, if the magnetic Hdg decreases, the a/c is experiencing:
#76. GPWS is active between
#77. A RA determines ac height by
#78. Marker beacons use the following wave length
#79. A Close traffic advisory is displayed on the Tcas II by
#80. What is measured to establish a/c position in relation to the Localizer on ILS?
#81. On the localizer modulations are 150Hz & 90Hz, which statement is correct?
#82. In GPWS BITE can be activated
#83. Descending through an isothermal layer at a constant TAS
#84. What is density altitude?
#85. From where does ADC obtain altitude data?
#86. Ac in level flight maintains M.N 072 later the ac descends maintaining same MN The TAS will be
#87. 2 aircraft are flying at different levels with same TAS. Which will have higher M.N?
#88. Can weather radar be operated on ground?
#89. The maximum drift error sensed by uncompensated DGI will be:
#90. If an ac flying at a constant height on a level surface meets a hot air mass ,the altimeter will,
#91. Some altimeter employ vibrator in order to
#92. What is indicated by lower and upper ends of the white arc on ASI?
#93. When climbing through an isothermal layer at a constant CAS
#94. Whom does the flux valve of a gyro magnetic compass transmit information to?
#95. In SSR, what code is used to indicate transponder altitude failure?
#96. What will happen to TAS when descending through an isothermal layer at a constant CAS?
#97. What inputs are fed to ADC?
#98. Servo altimeter are more accurate because
#99. What is the correct action to be taken when the static vent gets blocked of a VSI in a . unpressurized aircraft?
#100. What will be the effect on ASI if Pitot tube is blocked in an unpressurized aircraft?
