ATPL A46 Q-BANK (W&B)

1. Given: DOW=45680, MZFW=62600, MLDW=68040, MTOW=76850, TIF=5300, TOF=9800, what is maximum payload?. 15570. 16920. 16190.

2. Given: DOW=45680, MZFW=62600, MLDW=68040, MTOW=76850, TIF=4230, TOF=10400, what is maximum payload?. 15570. 16920. 16190.

3. Given: MZFW=130000, MLDW=140000, MTOW=170000, DOW=90000, TIF=20000, TOF=30000, Payload=40000, what is the zero fuel weight for this flight?. 120000. 130000. 140000.

4. Given: MZFW=140000, MLDW=140000, MTOW=170000, DOW=90000, TIF=20000, TOF=30000, Payload=40000, what is the zero fuel weight for this flight?. 120000. 130000. 140000.

5. Given: ZFW=A, LDW=B, TOW=C, DOW=D, TIF=E, TOF=F, Operating weight=G, Payload=H, I what is true?. D=A+E. G=D+F. B=C-F. None.

6. Given: ZFW=A, LDW=B, TOW=C, DOW=D, TIF=E, TOF=F, Operating weight=G, Payload=H, I what is true?. C=B+E. C=D+E. C=D+F.

7. Given: ZFW=A, LDW=B, TOW=C, DOW=D, TIF=E, TOF=F, Operating weight=G, Payload=H, I what is true?. C=D+F+H. C=D+E+H. C=A+F+H.

8. For fuel saving, the C.G. of the transport aircraft should be. in the forward of C.G.limitation. in the aftward of C.G.limitation. the C.G. position has no effect on fuel saving. None of them.

9. The main reason of carrying Ballast Fuel is because of. the C.G. out of trim. the weight out of limit. fuel not enough.

10. In case of carrying Ballast Fuel, what weight should the ballast fuel be included?. aircraft basic weight. take off fuel. zero fuel weight.

11. Which of the following description is FALSE. ZFW=DOW+Payload. TOW=ZFW+T/O fuel. LDW=TOW-T/O fuel.

12. Among ZFW,LDW,TOW, how to identify the most critical weight which limits the maximum allowable payload for specific flight?. the lightest weight of MZFW,MLDW,MTOW. the heaviest weight of MZFW,MLDW,MTOW. The weight which is closest to its respective max. weight. None of them.

13. For longitudinal stability, the relation between LIFT force center and C.G. for transport airplane is ?. lift force center is forward of C.G. lift force center overlap with C.G. lift force center is aftward of C.G. None of them.

14. For better control ability, which is TRUE?. AFT C.G. is preferred. FWD C.G. is preferred. independent of C.G.

15. For better maneuver ability, which is TRUE?. AFT C.G. is preferred. FWD C.G. is preferred. independent of C.G. None of them.

16. The aircraft C.G. is finalized when completely loaded. What direction will the C.G. move if we load something on specific direction ?. The reverse direction on which something was loaded. The same direction on which something was loaded. C.G. will not change.

17. For commerical airplane, what is the normal fuel usage sequence?. Center tank first, then main wing tank. Main wing tank, then center tank. Depend on aircraft type. None of them.

18. For long haul flight, the critical weight for allowable traffic load is normally limited by. Maximum landing weight. Maximum take off weight. Maximum zero fuel weight. None of them.

19. Which of the following weight factors determine ramp or taxi weight?. Payload plus operating weight. Zero fuel weight plus total fuel load. Zero fuel weight plus payload, fuel, and oil.

20. ZFW + TOF =?. DOW. Landing weight. TOW. TF.

21. Payload not includes?. Passenger. Fuel. Cargo.

22. Given: C.G. at 1419 inch,LEMAC at 1312 inch, MAC=295.8, How much percent MAC is C.G.position ?. 35.2% MAC. 35.8% MAC. 36.2% MAC. None of them.

23. Given: MTOW=283 tons, MLDW=207 tons, MZFW=195 tons, DOW=114 tons, Trip fuel = 70 tons, take off fuel=80 tons, traffic load =55 tons, what is the maximum Ballast Fuel Quantity can be carried if C.G. is out of trim?. 26 tons. 34 tons. Ballast fuel is not allowed. None of them.

24. Given: airplane weight =176000 kg, MAC= 327.8inch, LEMAC=1258 inch, C.G.=25% MAC, if we load 5000 kg cargo at location of 1500 inch, how much the CG position will be changed?. 1.24% MAC. 1.34% MAC. 1.44% MAC.

25. GIVEN: Empty weight 1100 with Arm 29 Pilot (fwd seat) weight 170 with Arm -45 Passenger (aft seat) weight 160 with Arm +2 Ballast weight 15 with Arm -50 the CG is located at station". +14.91. +16.48. +14.48.

26. GIVEN: Empty weight 1100 with Arm 30 Pilot (fwd seat) weight 170 with Arm -40 Passenger (aft seat) weight 160 with Arm +5 Ballast weight 50 with Arm -50 the CG is located at station. +17.55. +16.55. +15.55.

27. GIVEN: Empty weight 1100 with Arm 30 Pilot (fwd seat) weight 170 with Arm -40 Passenger (aft seat) weight 300 with Arm +5 Ballast weight 50 with Arm -50 the CG is located at station. +15.56. +16.56. +17.56.

28. GIVEN: Weight A - 155 pounds at 55 inches aft of datum Weight B - 165 pounds at 155 inches aft of datum Weight C - 95 pounds at 195 inches aft of datum Based on this information, the CG would be located how far aft of datuM?. 126.8 in. 122.2 in. 124.5 in.

29. GIVEN: Weight A - 155 pounds at 55 inches aft of datum Weight B - 165 pounds at 155 inches aft of datum Weight C - 95 pounds at 185 inches aft of datum Based on this information, the CG would be located how far aft of datum?. 120.5 in. 116.8 in. 124.5 in.

30. Given: MZFW=15830, MLDW=17000, MTOW=18370, DOW=10530, PAYLOAD=4950, TIF=1370, min TOF=1920, what is maximum extra fuel the airplane can carry for this flight ?. 1990. 650. 970.

31. Given: MZFW=15830, MLDW=17000, MTOW=18370, DOW=10950, PAYLOAD=3640, TIF=610, min TOF=1030, what is maximum extra fuel the airplane can carry for this flight ?. 1990. 650. 970.

32. Given: MZFW=130634, MLDW=145149, MTOW=170000, DOW=89886, TIF=20000, TOF=30000, what is the maximum allowed traffic load for this flight?. 40748. 40114. 38263.

33. Given: MZFW=130634, MLDW=145149, MTOW=170000, DOW=89886, TIF=20000, TOF=40000, what is the allowed weight for take off for this flight?. 160634. 170000. 165149.

34. Given: MZFW=130634, MLDW=145149, MTOW=170000, DOW=89886, TIF=30000, TOF=40000, what is the maximum allowed traffic load for this flight?. 40748. 40114. 38263.

35. What is the maximum allowable weight that may be carried on a pallet which has the dimensions of 48 x 48 inches? Floor load limit: 159 lbs/sq ft Pallet weight: 63 lbs Tiedown devices: 37 lbs. 2444.0 lbs. 2624.0 lbs. 2464.0 lbs.

36. What is the maximum allowable weight that may be carried on a pallet which has the dimensions of 48 x 48 inches? Floor load limit: 169 lbs/sq ft Pallet weight: 50 lbs Tiedown devices: 30 lbs. 1948.0 lbs. 2624.0 lbs. 2784.0 lbs.

37. What minimum floor load limit must an aircraft have to carry the following pallet of cargo? Pallet size is 100 wide and 100 long Pallet weight - 190 lb Tiedown devices - 60 lb Cargo weight - 12000 lb. 166 lb/sq ft. 177 lb/sq ft. 188 lb/sq ft.

38. What minimum floor load limit must an aircraft have to carry the following pallet of cargo? Pallet size is 68.9 wide and 88.7 long Pallet weight - 161 lb Tiedown devices - 54 lb Cargo weight - 11810.5 lb. 283 lb/sq ft. 223 lb/sq ft. 183 lb/sq ft.

39. What minimum floor load limit must an aircraft have to carry the following pallet of cargo? Pallet size is 80 wide and 100 long Pallet weight - 170 lb Tiedown devices - 50 lb Cargo weight - 10000 lb. 182 lb/sq ft. 184 lb/sq ft. 183 lb/sq ft.

40. GIVEN: Total Weight 3037 lb CG location Station 65.6 Fuel consumption 12.7 gal/hr Fuel CG Station 68.0 After I hour 45 minutes of flight time, the CG would be located at station. 64.86. 65.49. 66.54.

41. GIVEN: Total Weight 3900 lb CG location Station 70 Fuel consumption 14 GPH Fuel CG Station 60 After 2 hour 30 minutes of flight time, the CG would be located at station. 71.13. 72.12. 70.57.

42. GIVEN: Total Weight 4000 lb CG location Station 70 Fuel consumption 14 GPH Fuel CG Station 60 After 2 hour 30 minutes of flight time, the CG would be located at station. 69.55. 70.55. 71.55.

43. GIVEN: Total Weight 4037 lb CG location Station 68.7 Fuel consumption 12.7 gal/hr Fuel CG Station 68.0 After I hour 45 minutes of flight time, the CG would be located at station. 68.63. 68.72. 68.81.

44. GIVEN: Total Weight 4137 lb CG location Station 72 Fuel consumption 13.7 GPH Fuel CG Station 68.0 After 1 hour 30 minutes of flight time, the CG would be located at station. 67.79. 72.12. 70.78.

45. An aircraft is loaded to a gross weight of 4,800 pounds with three pieces of luggage in the rear baggage compartment. The CG is located 95 inches aft of datum, which is 1 inch aft of limits. If luggage which weights 90 pounds is moved from the rear baggage compartment (145 inches aft of datum) to the front compartment (45 inches aft of datum), what is the new CG?. 93.13 inches aft of datum. 95.13 inches aft of datum. 94.13 inches aft of datum.

46. An aircraft is loaded to a gross weight of 4,800 pounds with three pieces of luggage in the rear baggage compartment. The CG is located 97 inches aft of datum, which is 1 inch aft of limits. If luggage which weights 90 pounds is moved from the rear baggage compartment (145 inches aft of datum) to the front compartment (45 inches aft of datum), what is the new CG?. 96.12 inches aft of datum. 95.13 inches aft of datum. 94.13 inches aft of datum.

47. An aircraft is loaded to a gross weight of 4,800 pounds with three pieces of luggage in the rear baggage compartment. The CG is located 98 inches aft of datum, which is 1 inch aft of limits. If luggage which weights 500 pounds is moved from the rear baggage compartment (145 inches aft of datum) to the front compartment (45 inches aft of datum), what is the new CG?. 93.13 inches aft of datum. 87.58 inches aft of datum. 83.58 inches aft of datum.

48. An aircraft is loaded with a ramp weight of 3,650 pounds and having a CG of 96.0, approximately how much baggage would have to be moved from the rear baggage area at station 180 to the forward baggage area at station 40 in order to move the CG to 92.0?. 52.14 lbs. 104.29 lbs. 78.14 lbs.

49. An aircraft is loaded with a ramp weight of 3,650 pounds and having a CG of 96.0, approximately how much baggage would have to be moved from the rear baggage area at station 180 to the forward baggage area at station 60 in order to move the CG to 94.0?. 73.0 lbs. 36.5 lbs. 60.83 lbs.

50. An aircraft is loaded with a ramp weight of 3,650 pounds and having a CG of 96.0, approximately how much baggage would have to be moved from the rear baggage area at station 180 to the forward baggage area at station 80 in order to move the CG to 95.0?. 52.14 lbs. 36.5 lbs. 26.07 lbs.

51. The limit of Zero Fuel Weight is to prevent: insufficent fuel. extra fuel. airplane overweight. damage to airplane structure.

52. When an airplane gross weight is heavier, then the shift of cargo or passenger will affect the balance of airplane: more. less. same. not affected.

53. What kinds of factor will reduce an airplane maximum takeoff weight?. High temperature or tail wind takeoff. Low temperature or head wind takeoff. High temperature and tail wind takeoff.

54. If an airplane MAC is 124 inches and the C.G of FWD LIMIT and AFT LIMIT are 22% and 41%. The range of CG is?. 78.12 in. 27.28 in. 50.84 in. 23.56 in.

55. An airplane maximum gross weight is the sum of. airplane, passengers, and crew members. airplane, passengers, crew members, and cargo. a list of the airplane specification that includes the airplane and the maximum certificated weight of its inside parts. CAA certification that includs the airplane and the maximum certificated weight of its inside parts.

56. An airplane gross weight is 125000 lbs, CG exceeds AFT LIMIT for 4 inches. If we shift some cargo from 720 inches station to 420 inches station, make the CG shift. 1621 lbs. 16671 lbs. 16861 lbs. 17661 lbs.

57. An airplane gross weight is 146000 lbs. If we load cargo in the after cargo compartment, the CG is at 702 inches. Now, we want to shift CG 3 inches forward, how many cargo we need to shift to forward cago compartment ? ( forward cargo compartment at 510 inches, after cargo compartment at 1030 inches ). 6291 lbs. 7341 lbs. 7691 lbs. 8421 lbs.

58. To compute the balance between a 10 lbs and a 20 lbs objects , the arm of a 10 lbs object should ___ far than the arm of a 20 lbs object. 2 times. 3 times. 4 times. 5 times.

59. What kind of percentage do we usually use to represent CG?. Chord. Inch. Index. MAC.

60. The sum of airplane net weight, oil, crews and their baggage, cabin and emergency equipments is: Basic operation weight. Gross weight. Dry operating weight. Zero fuel weight.