3 - 2
3.2
Display Functions and Units of Measure
When operating in either pressure measuring or pressure controlling modes, the ADTS
405 can display the following information:
Aeronautical Functions
Altitude
Calibrated and True Airspeed
Mach
Rate of Climb
Rate of Airspeed
Rate of Mach
Pressure Functions
Static (Absolute)
Pitot (Absolute)
Dynamic or Impact (Differential)
Engine Pressure Ratio
Rate of Ps
Rate of Pt
Rate of Qc
Rate of EPR
Where [P] is the currently selected pressure units from the following list:
mbar, inHg, mmHg, inH
K114 Issue No. 9
Display Abbreviation
ALT
CAS, TAS
MACH
ROC
Rt CAS,
RtMCH
Display Abbreviation
Ps
Pt
Qc
EPR
Rt Ps
Rt Pt
Rt Qc
Rt EPR
O (4°C), inH
O (20°C), psi, hPa, kPa, inH
2
2
F
3-1 F
IGURE
RONT
Displayed Units
(if applicable)
ft, m
kts, km/h, mph
-
ft/m, m/m, m/s, hm/m
kts/m, km/h/m, mph/m
Mach/m
Displayed Units
(if applicable)
[P]
[P]
[P]
-
[P] /m
[P] /m
[P] /m
EPR/m
O (60°F), kg/cm
2
P
ANEL
Operation
, %FS
2