No worries — here is Chapter 5: Flight Mechanics — FULL 100 MCQs again (clean full version) #2: fs) Chapter 5: Flight Mechanics — 100 MCQs 1. Rate of climb depends on: — Excess power available 2. Angle of climb depends on: — Excess thrust 3. Maximum rate of climb occurs at: — Best rate of climb speed 4. Vy is: — Speed for best rate of climb 5. Vx is: — Speed for best angle of climb 6. In level flight, thrust equals: — Drag 7. In descent, thrust is: — Less than drag 8. Maximum glide ratio occurs at:— Minimum drag speed 9. Best glide speed gives: — Maximum distance per height lost 10. Load factor in level turn: — Increases with bank angle 11. A 60° banked turn load factor: 72g 12. Increased load factor increases: — Stall speed 13. Coordinated turn requires: — Aileron and rudder 14. Uncoordinated turn can cause: = Slip or skid 15. Rate of turn increases with: — Bank angle 16. Radius of turn decreases with: — Bank angle 17. Climbing turn requires: — More power 18. Glide angle depends on: — L/D ratio19. In climb, excess power used to: — Gain altitude 20. Stall speed increases with: — Load factor 21. Steep turn requires: — More lift 22. Coordinated turn has: — Ball centered 23. Centripetal force provided by: — Horizontal component of lift 24. Vertical lift in turn: — Balances weight 25. Adverse yaw in turns: — Opposes roll 26. Rate of climb reduces with: — Altitude 27. Service ceiling is: — Rate of climb = 100 ft/min 28. Absolute ceiling is: — Zero climb rate 29. Glide distance increases with:— Lower drag 30. In descent, rate increases with: — Forward speed 31. Wind affects: — Glide distance over ground 32. Higher altitude affects: — TAS for same IAS 33. Max endurance speed is: — Speed for minimum fuel flow per time 34. Max range speed is: — Speed for max distance per fuel 35. Turning performance depends on: — Lift, drag, power 36. Stall occurs earlier: — At higher load factor 37. Vertical lift in turn: — Supports weight 38. Horizontal lift causes: — Turn 39. Load factor formula: — Lift = weightAO. Accelerated stall occurs: — In steep turns 41. Bank angle for standard rate turn: = 15-2 42. Rate 1 turn is: — 3° per second 43. Slip ball shows: — Coordination 44. Glide angle increased by: — Increased drag 45. Descent angle decreased by: — Reduced drag 46. Max endurance achieved by: — Low power setting 47. Max range requires: — Optimum L/D ratio 48. Turns cause increased: — Stall speed 49. Load factor in level flight: aaa 50. In climb, lift equals:— Component of weight 51. Angle of bank affects: — Turn radius 52. Higher bank angle: — Higher load factor 53. Flight path angle: — Angle between path and horizon 54. Thrust-to-weight ratio affects: — Climb 55. Excess thrust used to: — Increase climb angle 56. Accelerated descent: — Steeper path 57. Glide performance best at: — Minimum drag 58. Increased weight in glide: — Same angle, higher speed 59. Bank angle limits: — Vary with aircraft 60. Steep bank requires: — Higher AOA61. Load factor in 45° bank: >1.41g 62. Turn rate increases with: — Lower TAS 63. Turn radius increases with: — Higher TAS 64. Standard rate turn: — 2 min for 360° 65. Tight turn requires: = High lift 66. Exceeding load limit causes: — Structural stress 67. Climb gradient important for: — Obstacle clearance 68. Descent angle controlled by: — Power and drag 69. Max rate of descent occurs at: — High drag 70. Turn rate depends on: — TAS and bank 71. Control inputs affect:— Turn performance 72. Power needed in climb: — Increases with rate 73. Climb gradient decreases with: — Altitude 74. Turn coordination requires: — Rudder 75. Skidding turn risks: — Overbanking 76. Slipping turn risks: — Underbanking 77. Glide range improves with: — Lower drag 78. Excess power improves: — Climb 79. TAS increases with: — Altitude (constant IAS) 80. Max rate of climb near: —2 WAY 81. Max angle of climb near: aaa UX82. Accelerated flight increases: — Load factor 83. Altitude gain per time: — Rate of climb 84. Angle of climb formula: — Altitude gained per distance 85. Turn radius at low TAS: — Smaller 86. Stall risk highest at: — High bank + low speed 87. Climb angle affected by: — Aircraft weight 88. Load factor causes: — Increased structural stress 89. Climb limited by: — Engine power 90. Glide path affected by: — Drag devices 91. Increased bank angle requires: — More lift 92. In climb, lift vector tilts:— Back 93. Glide at Vmd gives: — Best distance 94. Power-off glide: — L/D ratio dependent 95. In descent, forward speed affects: — Rate of descent 96. Turn rate inversely proportional to: 2 NS 97. Turn radius depends on: — TAS & bank angle 98. Shallow turn safer: — At low altitude 99. Rapid descent requires: — Increased drag 100. Maneuvering speed (Va) is: — Max control use without stall FULL 100 MCQs — Chapter 5: Flight Mechanics — sent again as you asked! 7 Would you like me to now send: Chapter 6: Performance & Limitations— 100 MCQs Just type: “Send Chapter 6” Or if you want PDF so far, just type: “Send PDF” — your choice! 4M