EMERGENCY MANEUVERS.

TM 55-6930-212-10 2-55. EMERGENCY MANEUVERS. 2-56. Training can be conducted for the following emergency aircraft maneuvers: Forced landings Engine beep trim malfunctions Hydraulic malfunctions Engine malfunctions Fuel system malfunctions Engine fire Electrical system malfunctions Transmission malfunctions AFCS malfunctions 2-57. INSTRUMENT MANEUVERS. 2-58. Training can be conducted for the following instrument maneuvers: ADF and VOR orientation, interception, and tracking Enroute navigation Holding ADF, GCA, VOR, and ILS approaches Missed approaches Two-way communication failure 2-59. SIMULATION SYSTEM CAPABILITIES. 2-60. The capabilities of various areas and systems of the simulator are: a. Visual area navigation: A simulated area of 80 km by 100 km is provided by a computer-generated data base. This data base is divided into four equal quadrants 45 km by 55 km in area with approximately a 5-km overlap. (See figure 2-4.) This visual training map (TAC map) shows the locations of the aircraft, aircraft track, rivers, lakes, islands, plateaus, mountain ranges, 200-meter level topological contour lines, and pinnacle locations associated with the gaming areas. When the aircraft flies off the display screen, a manual map update is used to change the quadrant displayed. NOTE The numbered asterisks show only the initial locations of the combined visual and EW threats. Editing a threat type or location on threat array page 025 does not cause a corresponding change on the TAC map. b. (Deleted) c. Aircraft weight and balance: These can be selected by the instructor to provide variable loading configuration (gross weight and center of gravity). Fuel quantity can also be varied. d. Atmospheric environment: The instructor can control the simulated environment to provide variable winds, turbulence levels (light, moderate, severe), gusts, temperature, and barometric pressure. Temperature (in degrees centigrade) and barometric pressure (in inches of mercury) are displayed at the instructor operator 2-10