10-57. 10-58. 10-59. 10-60. 10-61. 10-62. Minimum wing sweep limiting is NOT available under what method of control? Automatic Mechanical Electronic Bomb manual Aircraft that incorporate fuselage type speed brakes have an interconnect between the left-hand speed brake and the elevator nose down control cable for what purpose? 1. To stabilize aircraft yaw when the speed brakes are actuated 2. To prevent the aircraft from assuming a nose up attitude when the speed brakes are extended 3. To prevent the aircraft from assuming a nose down attitude when the speed brakes are extended 4. To assist the pilot in bringing the nose of the aircraft up when the speed brakes are applied To allow for automatic retraction under valve speed A A A A high air loads, what type of is installed in a fuselage brake system? check valve restrictor valve blow-back relief valve solenoid control valve During a malfunction, the null detector of the wingtip speed brake system causes the speed brakes to close when they reach what maximum amount of disparity? A trim system is provided for the pilot to lessen the need for a constant effort to maintain the desired heading and altitude. True False When the AFCS is engaged, what type of input controls the trim actuator in the aileron trim control system? 1. Hydraulic 2. Pneumatic 3. Electrical 4. Mechanical 10-63. A longitudinal trim actuator has what total number of operating speeds? 1. One 2. Two 3. Five 4. Four 10-64. The proper operation of gearboxes, interconnecting splined shafts, and screw jack actuators is essentially dependent upon which of the following maintenance functions? 1. Correct alignment 2. Correct adjustment 3. Proper lubrication 4. Proper installation 10-65. During the repair process for flap hydraulic components, you should verify spring alignment by performing which of the following procedures? 1. Testing them with a load tester 2. Rolling them on a smooth, flat surface 3. Rolling them on a smooth, curved surface 4. Testing them with a spring alignment tester 10-66. When a wing or stabilizer has been removed from an aircraft, it should be sent to what type of repair facility? Organizational-level Intermediate-level Manufacturer Depot-level 10-67. Which of the following tools are recommended for the removal of wing structural bolts? 1. A mallet and brass drift pin 2. A ball peen hammer and chisel 3. A setting hammer and prick punch 4. A sledge hammer and sheet metal punch 10-68. Before disconnecting cable linkage from flight control surfaces, you should perform what function first? Jack the aircraft Relieve the tension Collapse the struts Apply hydraulic power 53