GE Druck ADTS 405 R/F Mk2 Instruction Manual page 111

6.2.59.6 ALTITUDE CORRECTION
The altitude correction value for a specific aircraft may be entered as well as its limits.
The altitude correction value can be changed during operation in full and minimum set-up modes
using SETUP, [ALT]. See SETUP, [ALT] for further details on altitude correction.
6.2.59.7 ARINC LIMITS (Figure 6-7)
1. ARINC 565 operating limits are enabled by setting ARINC LIMITS ON and implemented as
shown in Fig. 6-7.
2. Due to the shape of the altitude/airspeed envelope, these limits cannot be implemented
using the above altitude, airspeed and Mach limits. Using the [ON/OFF] function key select
the required ARINC limits ON or OFF.
3. When used in combination with another set of limits, the lower (more restricting) limits
apply.
4. If ARINC limits are selected and any of the other limits are greater than the values of the
ARINC limits a display message requests confirmation that the lower, ARINC limit, is to be
used before the limit is saved.
6.2.59.8 SAVING LIMITS
When all limits and associated functions are set, press CLEAR/QUIT to exit the limit editing screen.
If changes have been made, the display shows a request for confirmation before saving the
changes. If the system detects any errors (e.g., duplicate aircraft names, values out of range or
editing system-defined limits) the display changes to the edit screen for the error to be corrected.
© 2015 General Electric Company – All rights reserved.
Figure 6-3: ARINC 565 OPERATING LIMITS
Introduction
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