Table 8-10. IOS Control/Display Interrelationships - Continued

Table 8-10. IOS Control/Display Interrelationships - Continued - TM-55-6930-212-10_152

Section IV. AUDIO RECORD PLAYBACK/PERFORMANCE PLAYBACK

TM-55-6930-212-10 Pyrometer and Thermocouple Tester Field Type N-3A Manual
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TM 55-6930-212-10 Table 8-10. IOS Control/Display Interrelationships - Continued Display Contents Display callup TRACK HISTORY ERASE Selection of another scale or approach (GPD) - continued redraws all relevant track history. ALERTS A maximum of 20 alerts can be dis- Automatic (TSD) played simultaneously on the GPD. Further indications of out-of-toler- ance are available continuously in the status area. An out-of-tolerance parameter links high/low intensity. During training mode, alerts are pro- grammed for variables that exceed pub- lished limits. Limits are established for the following: IAS A/S Yaw YW Roll RL Pitch PT Rotor speed RR Turn Rate RT Torque TQ (1 and 2) Fuel Qty FUEL Altitude ALT Vertical speed at landing VS CURRENT A current conditions display is On keyboard, type: CONDITIONS (AID) available for monitoring current 20 aircraft parameters and conditions. ENTER It is used to initiate parameter freeze, change aircraft location, change aircraft weight and balance, and change environmental conditions using the IOS keyboard. The following parameters can be frozen To freeze parameter and their current condition values On keyboard, type: monitored: LINE NUMBER SPACE Altitude Torque 2 * IAS Yaw ENTER Heading vertical speed Roll Rotor rpm To unfreeze Pitch Turn rate parameter Torque 1 Fuel qty On keyboard, type: LINE NUMBER SPACE ENTER 8-85

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