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Chapter 7. Reference
a.
To enter a alphabetic character (A to Z), press [ALPHA] and use the nudge keys to
change to the required character. Press [ALPHA] again to enter another alphabetic
character.
b.
Press [BACK] to delete the last character. When editing text use the CLEAR/QUIT key
to cancel editing.
7.4.6 MIN ALT, MAX ALT, MIN CAS, MAX CAS
These are the fundamental aeronautical unit limits.
7.4.7 MAX MACH
This limit only applies in aeronautical mode. It can be used to set a maximum Mach (e.g.,
Mach 1.05). If a Mach limit is not required, enter a high value (e.g. 10). The Mach limit can be
changed or disabled in full setup mode using SETUP, [MACH], see Section 7.3.15, "SETUP,
MACH," on page 88 for further details on Mach limits.
7.4.8 MAX ROC, MAX RATE CAS
These limits are the maximum rate of change for altitude and airspeed and only apply in
aeronautical units.
7.4.9 MIN Ps, MAX Ps, MIN Qc, MAX Qc
These are the fundamental pressure unit limits.
7.4.10 MAX RATE Ps, MAX RATE Qc
These limits are the maximum rate of change for Ps and Qc and only apply in pressure units.
7.4.11 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 setup
modes using SETUP, [ALT]. See Section 7.3.11, "SETUP, ALT," on page 87 for further details on
altitude correction.
7.4.12 ARINC LIMITS
1.
ARINC 565 operating limits are enabled by setting ARINC LIMITS ON and implemented
as shown in Figure 7-1.
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.
94 | ADTS 405 R/F Mk2 Instruction Manual-English
© 2017 General Electric Company – All Rights Reserved.
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