ATPL A41 Q-BANK

1. When a dashed blue circle surrounds an airport on a sectional aeronautical chart, it will depict the boundary of. Special VFR airspace. Class B airspace. Class D airspace.

2. If an airplane is consuming 9.5 gallons of fuel per hour at a cruising altitude of 6,000 feet and the groundspeed is 135 knots, how much fuel is required to travel 490 NM?. 27 gallons. 30 gallons. 35 gallons.

3. Inbound on the 315 radial, a pilot selects the 320 radial, turns 5 degree to the left, and notes the time. While maintaining a constant heading, the pilot notes the time for the CDI to center is 12 minutes. The ETE to the station is. 10 minutes. 12 minutes. 24 minutes.

4. With a TAS of 115 knots, the relative bearing on an ADF changes from 090 degree to 095 degree in 1.5 minutes of elapsed time. The distance to the station would be. 12.5 nm. 24.5 nm. 34.5 nm.

5. GIVEN: Wingtip bearing change : 15 degree Elapsed time between bearing change : 7.5 min True airspeed : 85 kts Rate of fuel consumption : 9.6 gal/hr The time, distance and fuel required to fly to the station is. 30 minutes; 42.5 miles; 4.80 gallons. 32 minutes; 48 miles; 5.58 gallons. 48 minutes; 48 miles; 4.58 gallons.

6. The ADF is tuned to a non-directional radio beacon and the relative bearing change from 0850 to 0900 in 2 minutes of elapsed time. The time en route to the station would be. 15 minutes. 18 minutes. 24 minutes.

7. GIVEN: True course : 105 degree True heading : 085 degree True airspeed : 95 kts Groundspeed : 87 kts. Determine the wind direction and speed. 020 degree and 32 knots. 030 degree and 38 knots. 200 degree and 32 knots.

8. An airplane departs an airport under the following conditions: Airport elevation 1,500 ft Cruise altitude 9,500 ft Rate of climb 500 ft/min Average true airspeed 160 kts True course 145 degree Average wind velocity 080 at 15 kts Variation 50E Deviation -3 degree Average fuel consumption 14 gal/hr. Determine the approximate time, compass heading, distance, and fuel consumed during the climb. 14 minutes, 128 degree , 35 NM, 3.2 gallons. 16 minutes, 132 degree , 41 NM, 3.7 gallons. 16 minutes, 128 degree , 32 NM, 3.8 gallons.

9. (Refer to figure 8.) When taxiing up to an active runway, you are likely to be clear of the ILS critical area when short of which symbol?(如圖A41_Fig8). Bottom yellow. Top red. Middle yellow.

10 (Refer to figure 8.) Which symbol does not directly address runway incursion with other aircraft?(如圖A41_Fig8). Top red. Middle yellow. Bottom yellow.

11. When in the vicinity of a VOR which is being used for navigation on VFR flight, it is important to. make 900 left and right turns to scan for other traffic. exercise sustained vigilance to avoid aircraft that may be converging on the VOR from other directions. pass the VOR on the right side of the radial to allow room for aircraft flying in the opposite direction on the same radial.

12. When the approach procedure involves a procedure turn the maximum speed that should be observed from first overheading the course reversal IAF through the procedure turn is. 180 knots IAS. 200 knots TAS. 200 knots IAS.

13. An off-route altitude which provides obstruction clearance of 1,000 feet in nonmountainous terrain areas and 2,000 feet in designated mountainous areas within the United States is called. Minimum Vectoring Altitude (MVA). OROCA. Minimum Safe/Sector Altitude (MSA).

14. What type navigation system is Inertial Navigation System (INS)? A navigation computer which provides position. from information by compass, airspeed, and an input of wind and variation data. from radar-type sensors that measure ground speed and drift angles. by signals from self-contained gyros and accelerometers.

15. Where does the DME indicator have the greatest error between the ground distance and displayed distance to the VORTAC?. High altitudes close to the VORTAC. Low altitudes close to the VORTAC. Low altitudes far from the VORTAC.

16. What DME indications should a pilot observe when directly over a VORTAC site at 12,000 feet?. 0 DME. 2 DME. 2.3 DME.

17. (Refer to figure 9.) Which RMI illustration indicates the aircraft to be flying outbound on the magnetic bearing of 235 degree FROM the station? (Wind 050 degree at 20 knots.)(如圖A41_Fig9). 2. 3. 4.

18. (Refer to figure 9.) What is the magnetic bearing TO the station as indicated by illustration 4?(如圖A41_Fig9). 285 degree. 055 degree. 235 degree.

19. (Reter to figure 9.) Which RMI Illustration indicates the aircraft is southwest of the station and proceeding TO the station?(如圖A41_Fig9). 1. 2. 3.

20. (Refer to figure 9.) Which RMI illustration indicates the aircraft is located on the 055 degree radial of the station and heading away from the station?(如 A41_Fig9). 1. 2. 3.

10. (Refer to figure 10 below.) What is the lateral displacement of the aircraft in nautical miles from the radial selected on the No. 1 NAV ?(如圖A41_Fig10). 5.0 nm. 7.5 nm. 10.0 nm.

22. (Refer to figure 10 below.) On which radial is the aircraft as indicated by the No. 1 NAV?(如圖A41_Fig10). R-175. R-165. R-345.

23. (Refer to figure 10.) Which OBS selection on the No. 1 NAV would center the CDI and change the ambiguity indication to a TO?(如圖A41_Fig10). 175. 165. 345.

24. (Refer to figure 10.) What is the lateral displacement in degrees from the desired radial on the No. 2 NAV?(如圖A41_Fig10). 1 degree. 2 degree. 4 degree.

25. (Refer to figure 10.) Which OBS selection on the No. 2 NAV would center the CDI?(如圖A41_Fig10). 174. 166. 335.

26. (Refer to figure 10.) Which OBS selection on the No. 2 NAV would center the CDI and change the ambiguity indication to a TO?(如圖A41_Fig10). 166. 346. 354.

27. (Refer to figure 12 below.) You receive this ATC clearance: "...HOLD EAST OF THE ABC VORTAC ON THE ZERO NINER ZERO RADIAL, LEFT TURNS..." What is the recommended procedure to enter the holding pattern?(如 A41_Fig12). Parallel. Direct. Teardrop.

28. (Refer to figure 12 above.) You receive this ATC clearance: "...CLEARED TO THE ABC VORTAC. HOLD SOUTH ON THE ONE EIGHT ZERO RADIAL..." What is the recommended procedure to enter the holding pattern?(如圖A41_Fig12). Teardop. Direct. Parallel.

29. (Refer to figure 12.) You receive this ATC clearance: "...CLEARED TO THE XYZ VORTAC. HOLD NORTH ON THE THREE SIX ZERO RADIAL, LEFT TURNS..." What is the recommended procedure to enter the holding pattern?(如圖A41_Fig12). Teardop. Direct. Parallel.

30. (Refer to figure 12.) You receive this ATC clearance: "...CLEARED TO THE ABC VORTAC. HOLD WEST ON THE TWO SEVEN ZERO RADIAL..." What is the recommended procedure to enter the holding pattern?(如圖A41_Fig12). Teardop. Direct. Parallel.

31. (Refer to figure 13 below.) A pilot receives this ATC clearance: "...CLEARED TO THE ABC VORTAC. HOLD WEST ON THE TWO SEVEN ZERO RADIAL..." What is the recommended procedure to enter the holding pattern?(如圖A41_Fig13). Parallel or teardrop. Parallel only. Direct only.

32. (Refer to figure 13.) A pilot receives this ATC clearance: "...CLEARED TO THE XYZ VORTAC. HOLD NORTH ON THE THREE SIX ZERO RADIAL, LEFT TURNS..." What is the recommended procedure to enter the holding paftern?(如圖A41_Fig13). Teardrop. Paralel. Direct.

33. (Refer to figure 13.) A pilot receives this ATC clearance: "...CLEARED TO THE ABC VORTAC. HOLD SOUTH ON THE ONE EIGHT ZERO RADIAL..." What is the recommended procedure to enter the holding paftern?(如圖A41_Fig13). Teardrop. Parallel. Direct.

34. The maximum speed a propeller-driven airplane may hold at is. 265 knots. 230 knots. 156 knots.

35. Maximum holding speed for a civil turbojet aircraft at a joint use airport (civil/Navy) between 7,000 and 14,000 feet is. 200 knots. 265 knots. 230 knots.

36. What is the maximum holding speed for a civil turbojet holding at a civil airport at 15,000 ft MSL, unless a higher speed is required due to turbulence or icing, and ATC is notified?. 265 knots. 230 knots. 250 knots.

37. Civil aircraft holding at an altitude of 14,000 feet at a military or joint civil/military use airports should expect to operate at which holding pattern airspeed?. 250 knots. 260 knots. 230 knots.

38. When using a flight director system, what rate of turn or bank angle should a pilot observe during turns in a holding pattern?. 3 degree per second or 25 degree bank, whichever is less. 3 degree per second or 30 degree bank, whichever is less. 1-1/2 degree per second or 25 degree bank, whichever is less.

39. When entering a holding pattern above 14,000 feet, the initial outbound leg should not exceed. 1 minute. 1-1/2 minute. 1-1/2 minute or 10 nm, whichever is less.

40. When holding at an NDB, at what point should the begin for the second leg outbound?. Abeam the holding fix or when the wings are level after completing the turn to the outbound heading, whichever occurs first. At the end of a 1 -minute standard rate turn after station passage. when Abeam the holding fix.

41. (Refer to figure 14.) The Cugar Four Arrival ends(如圖A41_Fig14). At BANTY INT. At IAH VORTAC. when cleared to land.

42. (Refer to figure 14.) What action should the pilot take if communications were lost during the Cougar Four Arrival, after turning on the 305 radial of IAH? (如 圖A41_Fig14). Proceed direct to IAH VORTAC, then outbound on the IAH R-1 25 for a procedure turn for final approach. From BANTY INT, proceed to the IAF on the IAH R-290, then continue on the IAH 1 0 DME Arc to final approach. Proceed direct to IAH VORTAG, then to either IAF on the IAH 1 0 DME Arc to final approach.

43. (Refer to figure 14.) While arcing left on the IAH 10 DME Arc, the pilot experiences a left crosswind component. Where should the bearing pointer be referenced, relative to the 900 (wingtip) position to maintain the 10 DME range?(如圖A41_Fig14). On the left wingtip reference. Behind the left wingtip reference. Ahead of the left wingtip reference.

44. What functions are provided by ILS?. Azimuth, distance, and vertical angle. Azimuth, range and vertical angle. Guidance, range, and visual information.

45. Within what frequency range does the localizer transmitter of the ILS operate?. 108.10 to 118.1 0 MHz. 108.1 0 to 111.95 MHz. 108. 1 0 to 117.95 MHz.

46. Which component associated with the ILS is identified by the first two letters of the localizer identification group?. Inner marker. Middle compass locator. Outer compass locator.

47. If installed, what aural and visual indications should be observed over the ILS back course marker?. A series of two dot combinations and a white marker beacon light. Continuous dashes at the rate of one per second and a white marker beacon light. A series of two dash combinations and a white marker beacon light.

48. What aural and visual indications should be observed over an ILS inner marker?. Continuous dots at the rate of six per second. Continuous dashes at the rate of two per second. Alternate dots and dashes at the rate of two per second.

49. (Refer to figures 135 and 138 on page 320.) Which displacement from the localizer and glide slope at the 1.9 NM point is indicated?(如圖A41_Fig15). 710 feet to the left of the localizer centerline and 140 feet below the glide slope. 710 feet to the right of the localizer centerline and 140 feet above the glide slope. 430 feet to the right of the localizer centerline and 28 feet above the glide slope.

50. (Refer to table 136 and 138 on figure 15.) Which displacement from the localizer centerline and glide slope at the 1,300-foot point from the runway is indicated?(如圖A41_Fig15). 21 feet below the glide slope and approximately 320 feet to the right of the runway centerline. 28 feet above the glide slope and approximately 250 feet to the left of the runway centerline. 21 feet above the glide slope and approximately 320 feet to the left of the runway centerline.

51. When is the course deviation indicator (CDI) considered to have a full-scale deflection?. When the CDI deflects from full-scale left to full-scale right, or vice versa. When the CDI deflects from the center of the scale to full-scale left or right. When the CDI deflects from half-scale left to halfscale right, or vice versa.

52. What facilities may be substituted for an inoperative middle marker during a Category I ILS approach?. ASR and PAR. The middle marker has no effect on straight-in minimums. Compass locator, PAR, and ASR.

53. When simultaneous ILS approaches are in progress, which of the following should approach control be advised of immediately?. Any inoperative or malfunctioning aircraft receivers. If a simultaneous ILS approach is desired. If radar monitoring is desired to confirm lateral separation.

54. When cleared to execute a published side-step maneuver, at what point is the pilot expected to commence this maneuver?. At the published DH. At the MDA published or a circling approach. As soon as possible after the runway environment is in sight.

55. When cleared to execute a published sidestep maneuver for a specific approach and landing on the parallel runway, at what point is the pilot expected to commence this maneuver?. At the published minimum altitude for a circling approach. As soon as possible after the runway or runway environment is in sight. At the MDA minimums and when the runway is in sight.

56. The lowest ILS Category II minimums are. DH 50 feet and RVR 1,200 feet. DH 1 00 feet and RVR 1,200 feet. DH 150 feet and RVR 1,500 feet.

57. What is the lowest Category IIIA minimum?. DH 50 feet and RVR 1,200 feet. RVR 1,000 feet. RVR 700 feet.

58. In addition to the localizer, glide slope, marker beacons, approach lighting, and HIRL, which ground components are required to be operative for a Category 11 instrument approach to a DH below 150 feet AGL?. RCLS and REIL. Radar and RVR. TDZL, RCLS, and RVR.

59. Which ground components are required to be operative for a Category II approach in addition to LOC, glide slope, marker beacons, and approach lights?. Radar and RVR. RCLS and REIL. HIRL, TDZL, RCLS, and RVR.

60. Aircraft navigating by GPS are considered, on the flight plan, to be. RNAV equipped. Astrotracker equipped. FMS / EFIS equipped.

61. The weather forecast requires an alternate for LUKACHUKAI (GPS RWY 25) ARIZONA. The alternate airport must have an approved instrument approach procedure, which is anticipated to be operational and available at the estimated time of arrival, other than. GPS or VOR. ILS or GPS. GPS or Loran C.

62. Overriding an automatically selected sensitivity during a GPS approach will. cancel the approach mode annunciation. require flying point-to-point on the approach to comply with the published approach procedure. have no effect if the approach is flown manually.

63. Authorization to conduct any GPS operation under IFR requires that. the equipment be approved in accordance with TSO C-115a. the pilot must review appropriate weather, aircraft flight manual (AFM), and operation of the particular receiver. procedures must be established for use in the event that the loss of RAIM capability is predicted to occur.

64. GPS instrument approach operations, outside the United States, must be authorized by. the FAA-approved aircraft flight manual (AFM) or flight manual supplement. a sovereign country or governmental unit. the FAA Administrator only.

65. If Receiver Autonomous Integrity Monitoring (RAIM) is not available when setting up for GPS approach, the pilot should. continue to the MAP and hold until the satellites are recaptured. proceed as cleared to the IAF and hold until satellite reception is satisfactory. select another type of approach using another type of navigation aid.

66. A GPS missed approach requires that the pilot take action to sequence the receiver. over the MAWP. after the MAWP. just prior to the MAWP.

67. If flying a published GPS departure,. the data base will contain all of the transition or departures From all runways. and if RAIM is available, manual intervention by the pilot should not be required. the GPS receiver must be set to terminal course deviation indicator sensitivity.

68. The ADF is tuned to a nondirectional radiobeacon and the relative bearing change from 270 to 265 in 2.5 minutes of elapsed time. The time en route to that beacon would be. 9 minute. 18 minute. 30 minute.

69. If a standard rate of turn is maintained, how long would it take to turn 360?. 1 min. 2 mins. 3 mins.

70. While cruising at 135 knots and on constant headin, the ADF needle decreases from a relative bearing of 315 to 270 in 7 minutes. The approximate time and distance to the station being used is. 7 minutes and 16 NM. 14 minutes and 28 NM. 19 minutes and 38 NM.

71. What are the standard temperature and pressure values for sea level?. 15 c and 29.92"Hg. 59 F and 1013.2" Hg. 15 C and 29.92 Mb.

72. Which is true about homing when using ADF during crosswind conditions? Homing. to a radio station results in a curved path that leads to the station. is a practical navigation method for flying both to and from a radio station. to a radio station requires that the ADF have an automatically or manually rotatable azimuth.

73. (Refer to figure 17.)which statement is true regarding illustration 2, if the present heading is maintaind? The airplane will(如圖A41_Fig17). cross the 180 radial at 45 angle outbound. intercept 225 radial at a 45 angle. intercept 360 radial at a 45 angle.

74. (Refer to figure 17.)which illustration indicates the airplane will intercept the 060 radial at a 75 angle inbound, if the present heading is maintained?(如 圖A41_Fig17). 4. 5. 6.

75. (Refer to figure 172.)which illustration indicates the airplane should be turned 150 left to intercept the 360 radial at a 60 angle ?(如圖A41_Fig17). 1. 2. 3.

76. (Refer to figure 17.) Which is ture regarding illustration 4 if the present heading is maintained? The airplane will(如圖A41_Fig17). cross the 060 radial at a 15 angle. intercept the 240 radial at a 30 angle. cross the 180 radial at a 75 angle.

77. How should the pilot make a VOR receiver check when the aircraft is located on the designated check-point on the airport surface?. Set the OBS on 180 plus or minus 4; the CDI should center with From indication. Set OBS on the designated radial. The CDI must center within plus or minus 4 of that radial with a FROM indication. Whith the aircraft headed directly toward the VOR and OBS set 000, the CDI should center within plus or minus 4 of that radial with a to indication.

78. While maintaining a magnetic heading of 270 and a true airspeed is 120 knots, the 360 radial of VOR is crossed at 1237 and the 350 radial is crossed at 1244.The approximate time and distance to this station are. 42 minutes and 84NM. 42 minutes and 91NM. 44 minutes and 96NM.

79. A higher elevation airports the pilot should know that indicated airspeed. will be unchanged, but groundspeed will be faster. will be higher, but groundspeed will be unchange. should be increased to compensate for thinner air.

80. What is an operational difference between the turn coordinator and the turn-and-slip indicator? The turn coordinator. is always electric; the turn-and slip indicator is always vacuum-driven. indicates bank angle only; the turn-and slip indicator indicates rate of turn and coordination. indicates roll rate, rate of turn, and coordination; the turn-and-slip indicator indicates rate of turn and coordination.

81. (refer to figure 24.) If the time flown between aircraft positions 2 and 3 is 15 minutes, what is the estimatesd time to the station?(如圖A41_Fig24). 15 minutes. 30 minutes. 60 minutes.

82. Which situation would result in reverse sening of a VOR receiver?. Flying a heading that is reciprocal to the bearing selected on the OBS. Setting the OBS to a bearing that is 90 from the bearing on which the aircraft is located. Failing to change the OBS from the selected inbound course to outbound course after passing the station.

83. Pressure altitude = 12,000ft, True air temperature = +50 degree F. From the conditions given, the approximate density altitude is. 11,900 feet. 14,130 feet. 18,150 feet.

84. If the relative bearing to a nondirectional radiobeacon is 045 and the magnetic heading is 355, the magnetic bearing to that radiobeacon would be. 040. 065. 220.

85. An aircraft is maintaining a magnetic heading of 265 and the ADF shows a relative bearing of 065, this indicates that aircraft is crossing the. 065 magnetic bearing FROM the radio beacon. 150 magnetic bearing FROM the radio beacon. 330 magnetic bearing FROM the radio beacon.

86. The ADF is tuned to radiobeacon. If the magnetic heading is 040 and the relative bearing is 290, the magnetic bearing TO that radiobeacon would be. 150. 285. 330.