First few questions were of Air Regulation: . Height and radius of VFR in congested Areas .Fl to be flown in case of unlawful interference . Fl to be flown, True Heading was given along with variation and deviation, but what flight, VFR or IFR wasn't given. . Steady green light when a/c is on ground . Series of red lights whn a/c is in flight . Two questions were there on the radio failure in IFR. Meteorology . Conditions in front of Stationary Front . Chart was given with Isobars and fronts along with TAF clearly showing features of cold front, had identify the station Human Performance . Two questions on stress a . What behavior is not good in team work . Alcohol is filtered by which organ Navigation . What is the Chart length between 180E and 180W on same lat . . Chart length was given on 59 lat, what is the chart length on some other lat . Three Alternates were given with the course and the wind component, which alternate is close in terms of time . A to B distance was given and wind component, what is the total time between A to B and then back to A. . What is the GS and Heading, Course and Wind component were given . QNH of ground is 1023 and elevation is 1500, how much you have to climb for FL 750 . In Mercator chart RL is a straight or curved line ? . What is the Drift on **lat? . What is the distance when an A/C descends 15000ft at the rate of 1500ft/min . Radio Altimeter turns Analog to Circular at - a. below 1000ft, b. at or below 1000ft, c. at DH. . One Altimeter is calibrated for Inst./Pos. error and other 1 is not, what happens is IAS changes . Power of NDB is 100KW what is the range? Technical . Increase in altitude but Angle of Attack, mass and IAS remains same, what happens to the Angle of Climb . With Increase in altitude what happens to the TAS and Drag Hey can u please explain me the solution for this question.. You are flying at FL 160. Outside air temperature is -27° C, and the pressure at sea level is 1003 hPa. What is the true altitude? A) 15090 feet. B) 16910 feet. C) 15630 feet. D) 16370 feet. Ans is (A) 15090 How are we getting 15090?? 18th May 2011, 18:06 #738 (permalink) planeboy_777 Join Date: Aug 2010 Location: mumbai Age: 21 Posts: 84 True altitude = Indicated altitude + (ISA dev x 4 x Thousands of feet) = 16000 + (-10 x 4 x 16) = 16000+(-640) = 16000-640 = 15360ft (on 1013.25) Height difference is 1013-1003=10Hpa therefore 10Hpa x 30= 300ft of height difference between 1013 and 1003 so 15360ft-300ft= 15060FT(1003hpa) silly numerical man!!! you made me remember my primar Regs: DGCA stuff, squawk code, type of transponder, class 'B' VFR above 10,000MSL etc. Met Find height of tropopause from charts Lapse rate questions A/C flying south in southern hemi with stbd drift, which pressure is it flying into? What is pressure alt? when are pressure alt n density alt same? Human Performance Stress Rate of alcohol consumption in body Middle and inner ear related questions Eye questions including fovea and rods Nav Diagrams of AH and you have to identify the one with the given condition Altimeter numerical flying from A to B, speed 0.84M. Distance 300nm, you have to increase your ETA by 2min, when will you decrease your speed? Previous ETA was given Speed/Time problems Gyro Local time numerical Tech AOA questions time &rel velocities hysterisis error combination of what all site errors adf has topple of DGI at pole topple/wander of DGI at somewhere else on earth where does the wing mounted compass send its signals..amplifier/dgi etc 1 question on taf with a miniature map asking you to identify the airport it applies to CDMVT 2-3 q bearing 2-3 q.. NDB bearing & qdm etc given what does attitude indicator indicate after straight level flight 180 deg turn... load factor in a turn stall speed stall angle VMU speed ...direction ....new latitude of place Lambert's departure cp pnr Eustachian tube stress REM sleep When an altimeter is used for SSR it is always referenced to: A) 1013. the non compensated altimeter will indicate a higher altitude.25 hPa B) The pressure setting in use C) QFE D) QNH Q2. and all other factors being equal: A) there will be no difference between them if air the data computer is functioning normally. The rate of climb: A) Is the downhill component of the true airspeed B) Is angle of climb times true airspeed C) Is the horizontal component of the true airspeed D) Is approximately climb gradient times true airspeed . VLO is defined as: A) Minimum possible speed that the aircraft could lift off the ground B) The maximum speed for landing gear operation C) The long range cruise speed D) Actual speed that the aircraft lifts off the ground Q4. Q3. D) ATC will get an erroneous altitude report SSR. B) At high speed the non compensated altimeter will indicate a lower altitude.Q1. If an aircraft is equipped with one altimeter which is compensated for position error and another altimeter which is not. C) at high speed. 15Vs C) 1.(increase in alt. decrease? or remain unchanged. remains constant. lesser or equal to max continous thrust how does change in altitude affect specific fuel consumption(sfc) .(since Vs is the reference speed) is max cruise thrust greater. for a jet engine. decrease.2Vs D) 1.5Vs Quote: increase in flaps will cause v2 to increase. For a single engine class B aeroplane. the AOA which results in a stall: (a) remains constant regardless of bank..increase. V2 may not be less than: A) not applicable B) 1. will dec. load or TAS . the amount of thrust reqd.divided by 100 Q5. so less fuel flow to the engin)e what is the best air:fuel ratio by weight for jet engines varies from 15:1(can vary)? at which point or region of a jet engine is the pressure at its highest the high pressure compressor? For a given aerofoil. What would you do to avoid damaging the aircraft and / or loosing control? (c) slow down to manoeuvring speed and fly upwind of ridge(not sure about flying upwind) On a cold. is to: (a) overcome yaw caused by lowered aileron on higher wing An aircraft is in a state of equilibrium in: (b) in a steady climb Adverse aileron yaw is reduced by the use of: (b) frise type ailerons Flying near high ground or mountains with winds in excess of 15km. radiation . while entering a turn from straight-and-level flight. humid night with a light wind. the separation point (c) moves towards the transition point The primary function of the rudder.The stall speed of an aircraft will increase with: (c) increase in the all up weight of the aircraft The three axis of an aircraft intersect at the: (b) centre of gravity When approaching the stall. you can expect strong turbulence and down draughts. clear. downward force on tail plane b. with PROB30. What happens when CG is ahead of CP ? . 7700 d. 7400 b. What would you set your transponder code (SSR) to in the even of an emergency ? a.fog will form. some other BS option 3.... 2... no force on tail plane d. What does PROB 30 mean ? ..) a. 7500 c. .. What might form when the wind picks up to 15kts? (c) stratus Which clouds are the least likely to produce airframe icing? (c) vertical development cloud 1.(or something like that... upward force on tail plane c. Some METAR was given . c. Some question related to VDF and ground equipment. 8. you notice flashing green light from tower. 9. execute climbing right 90 degree turn without being out of sight of intercepted a/c b.. How will an intercepting aircraft signal the intercepted aircraft that it may continue it's flight ? . Some question on scale .. probability of 30% b. d. ?? 4.. What does it mean ? 6. What frequency does a low altitude radar altimeter work on ? 7.a.. .. While taxiing. Some question on Mercator projection. (dont remember option) 5. (something like that) a. chances of some BS occuring within next 2 hours . overtake a/c from right c. (dont remember option) d. ... b.. QFE. Select the correct statement (direct reading compass) : a. (some more questions I recall ) . QNH....... .. one of them was DIHEDRAL) 15..... What is the Diameter of the earth ? 13.. ( Switch the words vertical/horizontal and inversely proportional in the above to sentences to get option c and d) 11. What is used to increase lateral stability in an a/c ? (dont remember the options ..10. WNE etc 14. Two questions related to altimeter setting. What are the typical values indicated wrt an a/c on an SSR display screen . What does anunciator in a Remote indicating compass indicate ? (Dont remember the options) 12. Accuracy of compass is inversely proportional to vertical earth's mag field.. Accuracy of compass is proportional to the vertical component of earth's mag field. . ? .... Deviation... and you were hyperventilating ?? (dont remember options .16. after flying through some volcanic ash. Some question related to VHF.. dont remember d... the free encyclopedia 19.. What do you mean by dysbarism ? Dysbarism .. What does an airspeed indicator display if the pitot hole gets blocked with ice... What are alveoli permeable to ? a.. but trust me they were comical options) 20. protein b. If you're flying through rain that freezes on impact. your pitot tube and static ports get blocked ? 22. (choose the correct one) a) You're flying near thunderstorms b) You're flying through a cold front c) The freezing level would be at a higher altitude .. 24. gases c. ..Wikipedia. but static vent remains open ? 23. what is metabolism ? 17. (CDMVT type) 21. Variation etc . Some problem related to Magnetic heading. What would you do if your breathing rate and heart rate were high on final approach. dont rememebr 18. increasing altitude and it's relationship to atmospheric attenuation. What would happen to your airspeed indicator reading if.... Compass heading. . dont remember the options well ) 29. ball right 28. How many planes of freedom does the gyro in a turn indicator have ? 27. (errr . 26. b) The bank angle is too less for the amount of rudder used . select the correct statement a) The bank angle is too much for the amount of rudder used.. In a right banked turn.. ball to the right c) wings to the left. : a) Wings to the right. Some question related to gyroscopes with a diagram.. turn coordinator indicates . ball to the left b) Wings to the left.. While taxiing and making a right turn. ball to the left d) wings to the right. There were atleast 2 questions related to GPS/GNSS/GLONASS and another question asking which of the 4 options was the most accurate system. the turn co ordinator shows wings banked right and ball to the left. (dont remember the 4 options well) .d) Descending would make the ice go away from the airframe 25. VMC (min control speed). a) VMU < V1 < VS b) V1>VS>VMC etc etc . V2. Several speeds were mentioned . 32. Vs and 4 options were given . One question related to drag curve and point of least Lift to Drag ratio.. what would be it's stalling speed at 45 degree bank angle turn ? a) 70 Knots b) 83 Knots c) 85 Knots d) 90 knots 34. VMU (Max unstick speed). If Stalling speed for an aircraft at bank angle of 10 degrees = 60 knots.. ie. An aircraft that inadvertently deviates from it's flight path should : a) inform ATC if ETA changes by more than 10 min b) ??? c) ??? d) ??? 35.30.. Correct option had to be ticked.. V1. A numerical problem related to calculating the Time of Sunset in UTC at a given place.. Time required for the eyes to adapt to the dark : . Vr. (Geographical Coordinates of the place is mentioned) 31. options like like . (so study up on all the V Speeds !) 33. having the 1st position followed by 4 different legs in NM calculate the final position.. Control airspace B... Lots of Human Factors 15 questions........ 5... PET and PSR questions with G/S already calculated 1 each 4.. A Mercator Chart on a parallel 46 deg N.a) 10 min b) 20-25 min c) ?? d) ?? . what will be the ROD? 5... a. G/S 150 kts... on RVR 4 Flying @ FL 22000 decent to 4000 Ft. Metrology atleast 15 questions. Departure questions X 2 nos. Metar's X 2 nos.... the Chart distance is 133 cms.. Mode C transponder can be operated in : A. Uncontrolled airspace and to be turned on when ATC instructs c.... Should be on at all times while flying . .. 3. What will be the scale factor at 36 deg N/S lat? 2. Radio aids like TCAS.180/30 Descending from FL 200 to FL 40 Horizontal Distance travelled . CRM X 4 questions. 8. TAS . Regarding take-off. the take-off decision speed V1: A) Is always equal to VEF (Engine Failure speed) B) Is an airspeed at which the aeroplane is airborne but below 35 ft and the pilot is assumed to have made a decision to continue or discontinue the take-off C) Is the airspeed of the aeroplane upon reaching 35 feet above the take-off surface D) Is the airspeed on the ground at which the pilot is assumed to have made a decision to continue or discontinue the take-off . 9. 6. Should be on at all times while flying. SSR. DME atleast 8 to 10 questions. Calculate range of 2 VOR's 7.39 NMs What is the ROD? Q6. but can be asked by the ATC to shut down.240 Wind . Lambert conical chat X 2 questions. Primary radar.d.197 kts Course . The measured course 042° T . How many feet you have to climb to reach FL 75? Given: Departure aerodrome elevation = 1500 ft QNH = 1023 hPa Temperature = ISA 1 hPa = 30 ft A) 7800 ft B) 6300 ft C) 6600 ft D) 6000 ft Q10.Q7. Given the following: True Course: 315° Wind velocity: 230/40 TAS: 420 knots What is the wind correction angle and the groundspeed? (WCA / GS) A) -6° / 415 B) +6° / 425 C) +6° / 415 D) -6° / 425 Q9. The load factor in a turn in level flight with constant TAS depends on: A) the radius of the turn and the weight of the aeroplane B) the radius of the turn and the bank angle C) the bank angle only D) the true airspeed and the bank angle Q8. C) descent. B) turn. B) 1 & 2. Clear ice is most often experienced. Q12. Which of the following statements. B) Minus 5° to minus 10° . D) Minus 5° to plus 5° . when the outside temperature is: A) 0° to minus 20° C. are correct? Euphoria is a possible result of hypoxia Euphoria can lead to degraded decisions in flight A) Neither. C) 0° to minus 5° C. Q13. C) 1 only. Linear acceleration can give a false impression of a: A) climb. D) spin. D) 2 only. the pilot must fly a compass heading of: A) 044° B) 058° C) 040° D) 052° Q11.The variation in the area is 6° W and the wind is calm The deviation is 4° W In order to follow this course. if any. Using an NDB it is possible to experience which of the following errors or limitations? A) Night effect. timing error and lack of a failure warning system. station interference and latitude error. x sin Long. B) CA=0. D) Night effect.5 x dlong x sin lat. an OAT -22° C is measured. FL 160. station interference and lack of a failure . FL 80. if you consider the temperature gradient of the Standard Atmosphere? A) -6° C B) 0° C C) +2° C D) -4° C Q15. D) CA=0. C) Coastal refraction. an OAT +06° C is measured.Q14. C) CA=(dlong-dlat) x 0. B) Coastal refraction.5 x dlat x sin Lat. An approximate equation for calculation conversion angle is: A) CA=dlong x sin Lat. Q17.5. if you consider the temperature gradient of the Standard Atmosphere? A) -4° C B) +4° C C) 0° C D) -8° C Q16. What will the temperature be at FL 130. timing error and night effect. What will the temperature be at FL 90. If the needle and the ball of a Turn & Slip indicator both show left. D) too high pitch-up and too low banking. Q22. On an EHSI display. Expanded VOR and Full VOR. Plan. C) Plan. wind velocity can be displayed in which of the following modes? A) Map. the artificial horizon indicates: A) too high pitch up and too high banking. D) at DH. Radio altitude is shown on the EADI and changes from a digital display to a circular scale: A) below 1000 ft AGL. Full ILS and Full VOR. C) at 2500 ft. Q18. Expanded ILS. The speed VLO is defined as: . Full ILS. Plan and Full ILS. B) attitude and banking correct. Expanded VOR. Following 180° stabilized turn with a constant attitude and bank.warning system. B) at 1000 ft and below AGL. D) turn to right & too much bank. B) turn to right & too little bank. C) turn to left & too little bank. Q20. C) too high pitch-up and correct banking. Full ILS and Full VOR. B) Expanded ILS. Q21. what does it indicate: A) turn to left & too much bank. Q19. D) Map. variation 11° W. with a constant power setting: A) decreases the rate of climb and the angle of climb B) improves the rate of climb if the airspeed is below VY C) improves the climb gradient if the airspeed is below VX D) decreases rate of climb and increase angle of climb Q24. Given true track 352° .A) the speed at which the aircraft leaves the ground. What is the advantage of the remote indicating compass (slaved gyro compass) over the direct reading magnetic compass? A) It senses the earths magnetic field rather than seeks it. deviation -5° and drift 10° S the required compass heading isSIMILAR) A) 347° B) 005° C) 358° D) 018° Q24. so is more sensitive. not more than V2 and not less than VR B) the maximum speed for extending or retracting the landing gear C) the minimum speed in the landing configuration with one engine inoperative at which it is possible to maintain control of the aeroplane within defined limits whilst applying varying power D) the stall speed in the landing configuration Q23. . Any acceleration in climb. D) Due south of A. D) Southern hemisphere. and Y 325° Consider the following statementsSIMILAR) A) Northern hemisphere. B) 0523 UTC. Rhumb line track is 322° . the sunrise is at: (SIMILAR) A) 0243 UTC.B) It is connected to a source of electrical power and so is more accurate. Rhumb line track is 331° . then 600 NM due west. Q27. Rhumb line track is 313° . What is the aircrafts final position in relation to A? A) Overhead A. then 600 NM due east. C) Southern hemisphere. On the same day. Rhumb line track is 322° .Y measured at x is 319° . C) Due west of A. The great circle track X . the 600 NM due north. at 52° S and 040° E. the sunrise is at 0243 UTC. Q26. C) 0743 UTC. D) 2143 UTC. D) It is not affected by aircraft deviation. On a typical computer generated SSR display the following data on a particular flight will be shown: . Q28. B) Due east of A. B) Northern hemisphere. From position A (04° N 030° W) an aircraft flies 600 NM due south. Q25. at 52° S and 035° W. On the 27th of February. C) It is lighter. Q29. D) each aircraft transmits pulses at a random rate. The transmission pattern is: (similar) A) 15000 pps for 100 seconds. D) Squawk code. Airplane callsign. then 30 pps. then 27 pps. Airplane callsign. D) 150 pps for 100 seconds. Airplane callsign. B) 270 pps for 100 seconds. An aircraft heading 325° (M) has an ADF reading of 330° Relative. Flight level . Ground speed. Ground speed. C) it will only accept the unique twin DME pulses. thereafter 60 pps until lock on. then 27 pps. A DME transponder does not respond to pulses received from radars other than DME because: A) DME only responds to the strongest 100 interrogators. B) DME transmits and receives on different frequencies. Flight level . C) Squawk code. Airplane callsign. C) 27000 pps for 100 seconds. The heading to steer to intercept the . thereafter 60 pps until lock on. Flight level . thereafter 150 pps until lock on. An aircraft DME interrogator transmits pair of pulses for limited periods at switch on. B) Destination.A) Squawk code. then 25-30 pps. True heading. Q31. Ground speed. Q30. thereafter 60 pps until lock on. Magnetic heading . 280° track inbound to the NDB at 50° is: A) 340(M) B) 330(M) C) 310(M) D) 320(M) Q32. should: A) Proceed direct to its destination. Q34. An aircraft on an IFR flight in VMC experiences radio communication failure. C) Carry out instrument approach at the nearest airfield. The aircraft is assumed to: A) Land at the destination aerodrome. B) Maintain at last cleared level and speed for 20 minutes and then continue in accordance with the flight plan. D) Land at the nearest suitable airfield. B) Return to the aerodrome of departure. The procedure for an aircraft that suffers communications failure during an IFR flight in visual met conditions. C) Land at the nearest suitable aerodrome. An aircraft encountering radio communication . D) Land at the alternate aerodrome. Q35. The maximum VHF range when flying at FL100 would beSIMILAR) A) 120 nm B) 100 nm C) 85 nm D) 12 nm Q33. converts . What effect might the pilot be exposed to. Q. B) Leave controlled airspace and continue the flight within uncontrolled airspace. Q. land at the nearest suitable aerodrome. cambered airfoil Q39. C) Squawk IDENT and proceed to the alternate aerodrome. Q36. Acknowledge code only b. a) Coriolis Force Q40. through electrical reactions. Acknowledge both code and mode Q37.When acknowledging mode and code. Decompression is caused by: c) Nitrogen coming out of solution Q41. pilot needs to: a. While turning the aircraft the pilot moves his/her head. The Retina b) Receives light.Lift and drag depend on a. Pressure distribution of wing aerofoil section b. What does series of green flashes indicate when on ground? Q38. report its arrival. Q.failure on an IFR flight in VMC is assumed to: A) Continue the flight to destination aerodrome in any case. D) Continue to fly in VMC. Q43. Q44. 5 litres a minute Q50. With pulse rate of 72 beats a minute and a stroke volume of 70ml. what is the cardiac output. Hyperventilation is likely to occur as a result of: B) the body attempting to compensate for a drop in partial oxygen pressure. the pilot should Turn off the strobe lights Q49. Generally a healthy person can compensate for the lack of oxygen with altitude upto: 10. Q42.000 feet.000-12.it into electrical signals. 100% Oxygen without direct pressure onto the face can be used up to: 40. Which illusion does linear acceleration cause? Climbing 46. Which gas diffuses from the blood to the lungs during external respiration? Carbon Dioxide Q45. When being affected by Flicker Effect. A person suffering from Glaucoma will have Increased pressure of the eye .000 feet Q47. 3 is correct 4 is false. The effect of carbon monoxide: Increases with altitude Q53. 3. Stand up and expel gases from the intestine.000 feet is.000 feet. A passenger complains of an inflated stomach at 8.000 feet Q52. 2. Drink large amounts of water. What action would you advised the passenger to take: 1. Decompression sickness symptoms can occur Following loss of cabin pressure at altitudes higher than 18. The time of useful consciousness (TUC) following loss of cabin pressurization at 35.Hyperventilation can after a long period of time lead to unconsciousness due to.Q51. 30-60sec Q58Under normal conditions which gas diffuses from the . 4. The metabolism of alcohol is affected by time Q56. low partial pressure of oxygen to the brain Q57. Q55. Clear Ice forms at temp: Near Freezing Q54.2. Avoid eating foods with fermentation qualities and or carbonated drinks. 1. Unbuckle the seat belt and rub the stomach. What can you say about the airmass over which the aircraft is flying: a. if necessary climb to the level where it first occurred. Q. Medium rain with large droplets Q64.000 feet Q61. Q.True altitude 10000ft. Should a pilot fly with a bad cold he/she could suffer from: Sinus Pain Q60. Q. An aircraft is flying over sea. Heavy rain with large droplets d. It is colder than ISA c.FL 100. Drizzle b. Q62.What does series of red flashes from ATC mean for aircraft in flight? . Its average temperature is same as that of ISA d.The information is not sufficient Q63.blood to the alveoli. It is warmer than ISA b. You suffer pain in an ear on a descent should you: Level off and. Above what height night vision can start to reduce? 5. Carbon dioxide Q59.Hail c.What kind of precipitation is from clouds found in middle latitudes: a.local QNH 1003. Time taken for body to adjust to circadian rhythm if flight time exceeds 24 hrs:IS 1-1.When excessive carbon dioxide has been removed .5 HR TIME CHANGE THEN 1 DAY a.5 hrs per day Q.airport unsafe to land Q65. Convex to nearer pole Q69. equalise pressue between middle ear and external atmosphere b. becomes acidic Q66. Rhumb line on direct Mercator: a. equalise pressure between sinuses and external atmosphere Q67. becomes alkaline attaching more oxygen to haemoglobin at lungs b. Straight line b. Body preparedness for a difficult task b. True track 358 Var 4 deg east. Apparent wander at 45 degrees north Q68. 1-1. Arousal: a. Q. All of the above Q70.High level of arousal means high vigilance c. Eustachian tube is to: a. the blood a. Flight level chosen will . Q. coma b) shivering tends to cease. A) Equator b) 45deg Lat . FL 75 b. What is random error. Hysteresis error of altimeter is due to. Initial phase of lock on Aircraft to DME.000 partial oxygen pressure is 1/2 of what at Sea level. Q. FL 65 d.be: a. a) A shooter mistakenly shoots from the gun b) A shooter shoots 1 in away from the target c) Pilot put wrong info in the FMS d) Q74. In an unaccelerated flight weight = Q. the Aircraft's transmits at what pulses. FL 70 Q71. Movement of air masses in the warm front. apathy Q72. choose from the following example. a) Oxygen 1/2 of what it is at sea level b) blood is 50% saturated with oxygen Q73. In fever below 35 deg C. At 18. FL 80 c. a) mental disorders. Q. what statement justifies it. Heading indicator will stop rotating in the vertical plane at. is max cruise thrust greater. lesser or equal to max continous thrust how does change in altitude affect specific fuel consumption(sfc) . decrease.5 deg to the right Q76. what is the best air:fuel ratio by weight for jet engines at which point or region of a jet engine is the pressure at its highest . remains constant.increase. At medium lat Coriolis force experienced: a) 7.5deg to right b) 15deg to left c) 7.5 deg to the left d) 10.c) 30deg Lat d) Poles Q75. decrease or remain unchanged. Range of NDB at 10 kw a) 500nm b) 100nm c) 1000nm d) 50nm Few more increase in flaps will cause v2 to increase. the AOA which results in a stall: (a) remains constant regardless of bank. the separation point (a) always stays in the same position (b) moves rearward (c) moves towards the transition point The primary function of the rudder. is to: (a) overcome yaw caused by lowered aileron on higher wing (b) overcome yaw caused by lowered aileron on lower wing (c) overcome yaw caused by raised aileron on higher wing .For a given aerofoil. while entering a turn from straight-and-level flight. load or TAS (b) varies directly with the degree of bank (c) varies with the speed of airflow around aerofoil The stall speed of an aircraft will increase with: (a) decrease in the load factor (b) increase in the pitch attitude for straight and level (c) increase in the all up weight of the aircraft The three axis of an aircraft intersect at the: (a) centre of pressure (b) centre of gravity (c) midpoint of the datum line When approaching the stall. radiation fog will form. clear. you can expect strong turbulence and down draughts. What might form when the wind picks up to 15kts? (a) dew (b) frost (c) stratus Which clouds are the least likely to produce airframe icing? (a) middle cloud (b) high cloud .An aircraft is in a state of equilibrium in: (a) a steady rate 1 turn (b) in a steady climb (c) during take off Adverse aileron yaw is reduced by the use of: (a) vortex generators (b) frise type ailerons (c) boundary layer fences Flying near high ground or mountains with winds in excess of 15km. humid night with a light wind. What would you do to avoid damaging the aircraft and / or loosing control? (a) maintain your heading and speed (b) slow down to manoeuvring speed (c) slow down to manoeuvring speed and fly upwind of ridge On a cold. (c) vertical development cloud --------------------------------------------------------- Q14. What will the temperature be at FL 130. FL 80. What will the temperature be at FL 90. if anyone thinks any of them are wrong. please feel free to correct me PS . if you consider the temperature gradient of the Standard Atmosphere? A) -4° C B) +4° C C) 0° C D) -8° C answers to the above questions are as follows. the test was way too tough and the options were way too confusing for me to recollect anything from the time i walked out of the exam hall.sorry for not contributing any questions. FL 160. trust me that's no excuse 1A 2C 3B 4D 5C 6D 7C 8A 9B 10D 11A 12B 13A 14D . an OAT +06° C is measured. an OAT -22° C is measured. if you consider the temperature gradient of the Standard Atmosphere? A) -6° C B) 0° C C) +2° C D) -4° C Q15. 15D 16D 17D 18A 19B 20A 21A 22B 23A ("decrease" word is missing infront of angle of climb) 24C 24A 25B 26C 27no idea.25 sq root ht of rec. of transmitter + 1. 300 = 62. root ht of reciever 300 =1.25 sq root ht of rec .option not present 72A 73B 74warm air will override cold air 74D 75A 76C anyone knows the answers to the extra questions posted? thanks An aircraft has to communicate with a VHF station at a range of 300 nm.600' d) 84.25 sq root ht.25 sq root 2500 + 1.378' c) 37. if the ground station is situated 2500' amsl which ofthe following is the lowest altitude at which contact is likely to be made? a) 190' b) 1. help! 28D 29C 30D 31B 32A 33C 34D 35D 36B 37continue to taxi until holding short for take off 38B 39spatial disorientation .5 + 1.25 sq root ht of rec 300-62.option not present 49what is the formula to calculate this? 62A 63A 65A 66A 68B 69C 70FL80 71"intense sweating" .25 sq.5 = 1.100' Range (nm) = 1. 25 sq root ht of rec 237.2nm as per the latest ICAO Annex .25 nm + 1.237.Charles law DME Accuracy is + . ( and 0. older than 1989) .25= sq.25 % of range for older aircraft. Henry's Law 2. root ht of rec ( Assume this to be X feet amsl ) 190 = sq root x sq.5 =1.0. Boyle Law 4.5/1. Dalton Law 3. both sides x= 36100 feet Hence.De Compression Sickness is related with 1. the close option is c Vs<V1< VR< Vmu <V2 Given TAS = 140 True Heading = 302 W/V = 45(T)/45Kt what is the Drift angle and Ground Speed? . The load factor will be: 1. The load factor (n) is approximately: a)1.74 Q-An aeroplane performs a steady horizontal turn with a TAS of 200 kt.49 0.4 c)1.0 What are the basic elements transmitted by NAVSTAR/GPS satellites? .8 d)2.1. A vertical up gust instantly changes the angle of attack by 3 degrees. The turn radius is 2000 m.49 2.71 1.1 b)1.Frangible = brakeable (easily broken) How does leading and trailing edge flaps affect critical angle of attack ? Why is Vmcg determined with nosewheel steering disconnected ?? The lift coefficient (CL) of an aeroplane in steady horizontal flight is 0.42. An increase in angle of attack of 1 degree increases CL by 0. ii. 2) Theory of Flight = Lot of questions of difficult standard. iii Two identical turbojet aeroplanes (whose specific fuel consumption is assumed to be constant) are in a holding pattern at the same altitude. iv B) ii. ii. its hourly fuel consumption is: A) 3787 kg/h B) 3426 kg/h C) 3259 kg/h (Mark scheme answer) D) 3602 kg/h Human Performance = 12-15 ques.offset of the satellite clock from GMT i ephemeris data ii health data iii ionospheric delays iv solar activity A) i. v D) i. iv C) i. iii. 5) Radio aids = 10-12 . iii. iv. ii. The mass of the first one is 95 000 kg and its hourly fuel consumption is equal to 3100 kg/h. Since the mass of the second one is 105 000 kg. 3) Met = 5-6 ques 3) Regs = 8-10 ques 4) Flight Instruments = Around 10. Nav = Around 20 Met --> Met ques were not easy and they were based on JAA. Airport signs.6) Gen. Eg. Freezing fog etc.What does a red flare in the air mean? Ans:Not withstanding previous instructions do not land. Regs --> Easy. Mountain wave. Gen... Interception signals. Human Performance --> In-Depth Knowledge reqd.Flashing green on ground? . Eg. Polar air mass. Nav --> 20% questions were tricky. I hope this helps ppl who will sit fr Indigo cae in the following months. 2. Transponder Codes.these are a few questions dat i remember from my exam on the 22nd : Regulations: 1. Theory of Flight --> 50% question were moderate and rest 50% question were tough. Flight Instruments + Radio Aids --> ques were simple.cloud minimas for VFR as well as IFR? 3.Visibilty. Transponder codes for radio failure and unlawful interferance..so how much are u actually climbing.25) Basic questions on Dme range and frequency(U r 750 nm from station at night what frequency should u use??(I think the lowest in the MF band should be ..vr.u have to climb to FL75.(in a turn) 4. Human Factors: 1.Cornea and Pupil remaining all questions were from oxford human performance book.QNH of aerodrome-1003.A simple question on the semicircular system.relation between v1.Relation between lift and weight in unaccelarated climb? 3.elevation 1500feet. and a couple of other easy questions on regs.Ans:Continue/Clear to taxi..ur heading was given so find the FL at which u can fly/ 5.vmc.. 4.(around 10 of them) Principles Of flight: 1..v2(this is a performance question but this was the only question from performance) 1.Relation between lift and drag wrt to aoa?? 2.A question on load factor..(just remember FLis always at 1013.Three layers of eye? Probable ans:Iris.. Vmu. drift provided.Vmca ? 13) During descend pilot will descend on Mach no or CAS ? 14) Relation b/w TAS and IAS as you climb or descend? 15) Standard atmosphere is defined by (couple of options given) 16) Yaw Dampers are used for ? . squak code? 9) Red flares shot from tower means ? 10) Tower shoots flashing red light.the answer) 1) Squak for radio failure. variation. a/c absolute altitude 9000msl. 2) DME slant range is 12 nm. what is the error is measured slant range 3) If there is misunderstanding due to “uncommon language” b/w controller and pilot what instruction will be issued for the a/c to make him land 4) Vitamin A causes loss of night vision due to ? 5) Some echoes are received 30 deg left of a/c track. what does it mean ? 11) Anti-collision light should be ON during ? 12) One performance ques asking relation b/w V1. DME stn height x msl. Mag heading of a/c is 020 (M). formation of due at night will be most profound in which case? 8) Unlawful interference. Plot true bearing of the echoes? 6) Divergence Is associated with? 7) One metar ques asking . static dynamic stability) 31) Scale in lambert conical. pressure based)? 23) Stereoscopic vision is? 24) Lassaire-fair cockpit ? 25) What is white out? 26) One on “seat of pants” when in IMC? 27) Illusion created by linear acceleration in IMC condition? 28) Function of semi-circular canals in ear ? 29) Pilot decided to divert from his route 30) Static stability leads to… (couple of options related to positive.17) Occluded front is formed when ? 18) Night vision is affected when ? 19) Stall speed given and a/c wt 6850 lbs what will be the stall speed when a/c wt is 5000? 20) Effect of camber in longitudinal stability? 21) Effect on landing distance when a/c is on ground effect? 22) You deploy flaps when coming in to land. at some point P he decides to divert . contracts b/w std parallel and expands outwards from it. knowledge based.D. he has three options C. negative. 32) Latent mistake causes (options given) 33) REM sleep relaxes _____ and slow wave sleep relaxes _____? 34) Effect of camber on longitudinal stability? 35) A pilot is going from A to B. rule based.E. . this behavior results from which type of knowledge (options : skill based. .(distance to C.mf.D.it is required to delay its eta by 2 mins.LF.hf. (NOTE: the reduced speed is not given) 3 2 questions regarding intercepting and intercepted a/c 4 1 ques on rem sleep 5 astigmatism is? 6 stress is .VHF…)? 2) 1 what happens to lift and drag(separate ques) as a plane climbs at const ias 2 a/c cruising at .MF.. Find the time? 37) NDB allotted freq is? 38) Some freq was given and ques asked which cat will it fall in(VLF.lf 8 to calculate range of transmission signal when . 36) Pilot goes from A to B and back. TAS also given. 4 options were given 7 an a/c is flying at a range of 750 nm on 320 fL which frequency should be used during night for r/t vhf.E and HW/TW component was provided) find the destination which takes least time.84 mach at some altitue with time of departure and time of arrival given.. when should it reduce its speed. TAS is 360 kts and HW is 60 kts. when should it be used? -Transponder code '2000' Mode A is for ... abv 10...7700 14 when cold front moves what happens to the stability of air ahead 15 what is vso 16 what is vlo 3) what does a red flare indicate to an a/c -squawk code Mode A for radio faliure -green flashes from light signals to an a/c on the ground -if equipped with transponder facility.. -clearance of the a/c above hilly terrain..000MSL .height of a/c and that of antennae is given 9 simple ques to calculate g/s and wca using cx2 10 coldest air in a cold front is where? 11 principle of vor 12 principle and frequency band of ssr 13 3 ques asking the squawk code 7500. congested area(along with the radius) -clearance from clouds in class B airspace.7600. line of sight range -how does a RL appear on a direct mercator chart?(staright line) -gyro errors. pressure altitude -turning errors. S=D/T.Vlof. height/temp of tropopause in summer/winter -a while dumbell indicates .. load factor qstns -1sm= ...as usual) -formation of hill fog -lapse rate... Track-Hdg-drift.-DME working rinciple qstns -Meterology: TAFs. (flaps and angle of attack) -lift-weight relation in an unaccelerated climb __________________________________ . temp deviation. departure..V2..Vmc... density altitude. ' -NAVIGATION PROBLEMS: mach no.V1. pitot-drain hole blockage -TCAS principle(transponders) -radio altimeter(system error) -avg. and the altitude maintained -factors affecting stall speed increase/decrease -CL can be increased by. -right of way -Human Factors (in depth... fronts.. CDMVT... altimeter errors -correlation betn Vs.Vr. cloud types(shapes) -rate of turn..Vmu(< > =) -what is the overall appearance of the a/c when the speed is reduced... scale. VOR indicator.. freq-wavelength numerics. decrease or remain unchanged. remains constant. gross weight 6500 kg.what is the stalling speed with gross weigth 5000kg? A)57 B)67 6)74 D)91 ncrease in flaps will cause v2 to increase. the AOA which results in a stall: (a) remains constant regardless of bank. load or TAS (b) varies directly with the degree of bank (c) varies with the speed of airflow around aerofoil The stall speed of an aircraft will increase with: (a) decrease in the load factor (b) increase in the pitch attitude for straight and level . what is the best air:fuel ratio by weight for jet engines at which point or region of a jet engine is the pressure at its highest For a given aerofoil.4) If aircraft stalling speed is 74 kts. decrease. lesser or equal to max continous thrust how does change in altitude affect specific fuel consumption(sfc) . is max cruise thrust greater.increase. (c) increase in the all up weight of the aircraft The three axis of an aircraft intersect at the: (a) centre of pressure (b) centre of gravity (c) midpoint of the datum line When approaching the stall. is to: (a) overcome yaw caused by lowered aileron on higher wing (b) overcome yaw caused by lowered aileron on lower wing (c) overcome yaw caused by raised aileron on higher wing An aircraft is in a state of equilibrium in: (a) a steady rate 1 turn (b) in a steady climb (c) during take off Adverse aileron yaw is reduced by the use of: (a) vortex generators (b) frise type ailerons (c) boundary layer fences . while entering a turn from straight-and-level flight. the separation point (a) always stays in the same position (b) moves rearward (c) moves towards the transition point The primary function of the rudder. clear.. y wont u get the indication? .hope dt wil b of sum help to any1 bt basically everyday d main topics in d xam r changin. radiation fog will form..radio altimeter measures ?? a)true altitude b)true height c)2 more irrelevant opns.Flying near high ground or mountains with winds in excess of 15km.if u r 210 NM away frm DME. you can expect strong turbulence and down draughts. humid night with a light wind. {thr were 2 same ques} 3. What might form when the wind picks up to 15kts? (a) dew (b) frost (c) stratus Which clouds are the least likely to produce airframe icing? (a) middle cloud (b) high cloud (c) vertical development cloud hey guys in today's attempt 13 ppl passed.accuracy of DME 2.. What would you do to avoid damaging the aircraft and / or loosing control? (a) maintain your heading and speed (b) slow down to manoeuvring speed (c) slow down to manoeuvring speed and fly upwind of ridge On a cold.... Nav-inst-radio 1.im jst postin few ques n topics rem... hw much speed u shud travel at 60 deg lat to travel at same tym.height of high clouds 2.ques to calculate radius of cone of confusion 15.wht is the diameter of the cone in (nm) Ans : VOR Cone of confusion radius cone of confusion = alt (in nm) x tan 50 .LSS in troposphere? 7. R/T ques 1.on SSR whr is transponer nd interrogator? 5..one ques on turning error 10. wt will b the base of cloud?(ans 2000 feet) 4.cumuliform two more optons i dnt rem 3. all the best Ques: Aircraft flying at 6000' enters cone of confusion..some basic radio call MET 1.phrase monitor 3..4.sfc temp +10 deg C dew point temp +15 deg C.if u travel at some speed on circumference of equator at some tym..VSI operates coz of difference in a)static b)dynamic c)total 6.phrase go ahead 4.circumference of earth 13.high clouds are a..speed of sound depends on? 12. speed at equator was given 16.circumference at 60N 14.2 ques on acceleration/deceleration error 9.readability 5 means? 2.2 ques related to subsidence lost comm alot of CG ques Vfe rate of turn/radius of turn thats al i rem.cirroform b.VSI blocked during descent 8. RIC ques 11.. .16 x 2 = 2.. 32m{105ft} c.15730 ft ANS-B{.how plz explain.QNH set as 1023. Colder than ISA C. MSA given as 12000ft.. You are flying at FL160 with an OAT OF -27*C.. 64m{210ft} d...} Q2.. 15m{50ft} ANS-D{.15540 ft b.hence the crossed air mass is on average. a.210 D..... 11. There is insufficient information ANS-B{.why plz explain. the Radio altimeter indicates a true altitude of 13500ft..} Q3.i would really appreciate if some one could help me out in these concepts Q1.how plz explain.} .Flying at FL135above the sea..what will the true altitude when 12000 ft is reached? a.. At ISAstandard atmospher b... the local QNH is 1019hpa..15090 ft c..98 x tan 50 = 1. Warmer than ISA D....3 nm TAN 0 = PERPENDICULAR/BASE Angle is 50 degrees Base is the altitude of a/c Perpendicular is the radius of cone of confusion I need help regarding solving of these questions. What is approximate vertical interval which is equal to a pressure change of 1hpa at an altitude of 5500m? a.. flying over mountains in temperatures +9*c . 8m{27ft} b. 12.940 b.16 nm so diameter = 1. 12. what is your true altitude? a. 11.} Q4.6000'/6080'=0.how plz explain..16330 ft d.98 nm 0..i am not able to get the concept to solve these meteorology problem.864 ANS -D{..148 c...QNH is 1003 hpa.... Readability 2 means readable now n then 2. So you will have to make an additional correction i.I understand and will comply with the message. @ 2. at a give alt is not ISA you need to make corrections to the indicated altitude to get True altitude. varies like this: @ S. Range of DME is correct within a.5 mhz 5.2 NM .1.2 % correction 7. 121.4.0.864ft.L= 27ft.ANSWERS 1) When the temp. Now since you are flying at FL 160 you will have set the altimeter setting as 1013. 121.25. 0.000 ft so the closest answer is 50ft. Sorry about Q no. Since ISA deviation here is -10*C you will need to subtract 4% of 16000ft from16000ft which is 16000-640 = 15360.000ft = 30ft.ISA (-9*C) = 9+9 = 18*C 10*C= 4% correction so 18*C = 7.3% of range b. ISA dev at 12000 ft = actual (9*C) . From what I can recall for every 1 hpa the change in ht..a. I'm not really good at explaining stuff as you can see.what frequency you will communicate this on.5 NM c.L upto 40.000ft = 50ft and @ 40.5 mhz to 125. Wilco 3.a. The correction is for every 10*C above/below ISA you need to apply (add/sub) a correction of 4% to the Indicated altitude to get the true altitude. An aircraft is intercepted by another aircraft.000ft.Roger ( Answer) b. But I will try to put it in words and get back. @20.000 ft. And your true altitude is based on your QNH which is 1003.2% of 12000 = 864ft So since the temp at the given altitude is above ISA add the correction of 864ft to the indicated altitude of 12.5 Mhz to 243 Mhz b. 4) There are some fixed values given is some books as to the how the value of 1mb changes from S.000ft = 100ft 5500m = about 18.e 1003-1013 = -10 x 27 (1mb = 27ft) = -270 So finally true altitude = 15360-270 = 15090. So the answer is 12. Perhaps if I could draw I could explain it better. Marshall's signal to apply brakes 4.000+864 = 12. 3) Again similar to Q no. I'm not able to explain it in words. the landing gear speed with full safety and related options 22.Civil twilight a.Which of the following is present in Middle Ear a.Time of Useful consciousness at 35000feet is39.NDB frequency a.330 c. a special system installed on board 13.A signal is received after fading at the receiver. Ossicles c.0. Find QTE? 26. 250 mts 11. theta =3 degree TAS=100 kts ROD=** ANS: 500 feet/minute 12. DME is able to discriminate between pulses intended for itself and for other a/c coz it rejects the pulses not synchronized with its own random PRF 8.An aircraft flyign with left static port blocked will. Semicircular canal d.Altitude information is displayed on PFD d. Beginning of July 28. a. Which is the most prominent error of NDB .Class B airspace Met Minima above 10000 feet 31.PFD is the main flying instruent c. VLE speed is a. Flashing green lights to a/c already taxing on ground means9. over read when side slipping towards port b. overread when side slipping towards starboard . vestibular apparatus 21. Night effect c. it will become colder c.DME uses frequency a. A/c is flying over a snow covered lake and related options 10.6 degree below the celestial horizon 29.A. 200 mts b.FMA related option Combination of correct answers was given 34. it will become warmer 37. Convergency. Embolym b. It will fly an Emergency triangle b. A-B 90Nm Along the track 60 nm from A. Definiton 24.a. Vyse b. SH.7700 40.Quadrental Error 16.Blue line speed is a.Which is the most likely reason a. C.Stage 2 sleep comprises of 50% of sleep.1000 MHZ b.mach No. Primary radar relies on target reflection and secondary radar on transponder replies 15.What is the correction required to track directly to B a. Declare emergency c. 35.Quadrental Error b. Whiteout means a. + . Increases as aircraft is flying at closer range 7.P-Q RL=? Ans is 088 Degree 27. lower stratosphere 18. 8 left 19.6.345 33.5 NM b.90% of water vapour is present in a. Divergence brings in what kind of weather 25. Echoes are received 30 degree to left. 100 Mhz c. Coastal error 17.190-1750 KHZ 20.Question related to Primary and Secondary Radar. troposphere b.100% Acuity is achieved at FOVEA 36. Vne d.A (45N 10 W)and B(48*30** N 15 W) Find the A-B RL track a. Perihelion occurs a. Vmo 23. it will stay at the same temperature b. transponder replies from other a/c b. Accuracy of DME is a.Met minima for 4500-9000 feet outside controlled airspace 32. Beginning of January b.TCAS operation uses a.ILS Cat III (a) RVR is a. An a/c has been hijacked and is asked to commence a descend. What SSR code is used for Emergency. aircraft is positioned 4nm to right. mountainous/terrain effect d. 12 left b.=7. 300 b. a. ND shows flight director bars b. 100 KHZ 14. P-Q=95 Degree GC .a.On reaching the saturation vapour pressure.It cannot notify ATC of its actions.A/c hdg is 120 M .Lines joining places of equal variation are ISOGONALS 30. Descend to an altitude which is at a deviation of 1000 ft wen flying FL290 above and 500fr if below FL290 38. Vmc c. .41.OAT is not given. 40000 52.Ice on the aircraft surfaces will increase the landing distance by a.Average height of Stratosphere is a.a. 60% of crew resources have been utilized c. Less than 1022 b. O2 and CO .Stress management is 50. TAS=250 Kts .100% oxygen corresponds to the FL of a. OAT= --12Degree Icing will occur. 1022 d. 60. 47.Avoid rapid head movement during the turns 57. A ( 004N 30W ) aircraft flies 600 NM south then 600 NM east. radiation 65. NDB bears (given in question) ..FL 150 .With respect to CO which of the following statements is correct.When is the coldest time of the day.Myopia is.?? 44. 11 to 50 KM b. Seek Aviation Medical Assistance immediately b.<1000 mts visibilty due to solid and ice particles b. Depends on Pilot expertise d. 10000 b. Altimeter error 63. O2 and CO2 b.Answer is 500ML 56.Tidal Volume is. a. <1000 mts visibility due to solid and liquid particles c.1. Moderate to severe Rime Ice 61.Geostrophic winds are proportional to a. Nearsightedness b.Variation is applied at beacon on VOR and at A/C for NDB. When acknowledging mode and code pulse from ATC.moderate to severe Mixed Ice b.a. 30 minutes after sunrise .3 dots 54. It causes Hypoxia 51.. Cognitive Stress is53. CU and CB are formed due to a. Information is not sufficient to determine 42. 600 NM north. Worload is defined as. an a/c is flying at a range of 100Nm on a airway. Aircraft's present position is? 58.A/C magnetic hdg is 120.pilot will reply by a.break the glass of Rate of climb indicator 43. 3040% c.5 dots b. Fog and Stratus b. it has 5 Times affinity to attach with hemoglobin than oxygen b. Aircraft is flying over a warmer airmass b.Physiological gases are a. Bi-lobar pattern c.What could be the possible reason for this? a. 40-50% b. clear sky 64..10-15% 49. Over flat terrain.Correct remedial action will be. Dew Point and Air temperature are less than 1 Degree apart.QNH = 1022 HPa . Fog is a.NDB signal transmits a signal pattern in the horizontal plane which is a. Availability of resources Combinations of answers is correct 45.What will be the NDB bearing to plot on a Polar stereo graphic chart? 62.away from fronts. Two more combinations were given 48. particles d. what kind of weather will occur as a result a. Flying over a colder airmass c. density if air b.A pilot experiences bends in joints after the Flight. omnidirectional b.90% of crew resources have been utilized b. repeat only code pulse 59.Airfield is 0 metres above MSL. Cardiod balanced at 30HZ freq..2 dots c. variation= 17W track is 15 degree to the left of HDG..a. 50 to 85 KM 67. Farsightedness 46.Upsloping runway will give an illusion of . curvature of isobars 66..A/C is going from A (QNH 1012HPa) to B (QNH 1012Hpa). Convection b.< = 1000 mts due to ice and ... On a 5 dot indicator. To prevent Vertigo. Repeating both mode and code pulse b. the altimeter reading differs. QFF=? a.moderate to severe Mixed Ice c. Pushed by clouds against the mountains.a. more than 1022 c. 600 NM west. < 1000 due to presence of precipitation 66.One or more several static ports have been blocked on board a unpressurised aircraft. How many dots will correspond to the deviation? a. Ignore as it will get better with time 55. .. what type of clouds are NS ST AS . ????? 5.Radiation c.. Series of green flashes 6.????? 9. continue in VMC n land at most suitable aerodrome n inform ATC b.a. ???? d.. sinking d. What kind of illusion pilot goes under when a/c is in bank and pilot tries to pick up a pen frm ground 2. 4.some questions which i can recall1.What kind of flaps are at rear of wing 3. question on v speeds. 2 questions on true heading variation magnetic correction!! 8. convection b. Questn on fohn winds 12. Very simple quest on PET 7. If radio failure in IFR in VMC what will u do a.. signal of adf is vertically/horizontally polarised to avoid diffraction/refraction/attenuation 13 Range and power of locator beacon .V1 Vmc V2 Vr etc. Height and type of high clouds 10 Height and temp at tropopause over poles n equator 11. fly accd to flight plan and select 7600A on transponder c. how does GC appear on polar stereographic chart 24...First step by crew when decompression happens.. meters apart 19..hardness of controls c.overexposure to light on fovea c.. what is autokinetic illusion 29....c ??? d ??? lt 22. sum 3-4 basic questions on pitot static instruments 21... static +dynamic b. what r symptoms of hypoxia 28.??? 27... rad alt 31. DME and VOR co-located when they r .same length represents x at 30 degrees. what is cocktail party effect :ugh: 30..dont rem the options 18.D-GPS 20...14.a pressure chart was given.lack of rods n cones on fovea b. What is centre of pressure 15.... what of the followin r experience by student pilot a. 4 quest on GPS....find x ...v had to analyse 25. Total pressure = a. static -dynamic .lack of rods and cones on iris d.. Height of base of clouds 23.length represents a distance of 90 miles at 45 degrees north.lack of rods and cones on optic nerve 17...sickness n loss of sleep d.nervousness b. Min length of clearway 16. 2 questions on radiation fog (how they r formed and dissipates) 26. Day Blind spot is due to a.. Mercator scale.... G/S 150 kts. what will be the ROD? 33. but can be asked by the ATC to shut down.. Calculate range of 2 VOR's . Uncontrolled airspace and to be turned on when ATC instructs c.32. Mode C transponder can be operated in : A. Should be on at all times while flying. Control airspace B. Should be on at all times while flying d. 34. Flying @ FL 22000 decent to 4000 Ft.