GE Druck ADTS 505, User Manual, Page: 122 / 124

6 - 42 Reference and Specification
K0260 Issue No. 8
Measurement and Control Range Specifications
Operating Range and Performance
Limits are set pre-defined tabular limits known as ARINC 565, CIVIL and EPR these can be selected
through the SETUP menu. Operators may also configure the display to aeronautical or pressure
units but should be aware that when units of pressure are selected, wider full-scale pressure limits
will be enabled for some parameters.
Performance expressed in aeronautical units
N
OTES
(1) Maximum operating range that can be achieved using the internal pump at airfield
altitudes to a maximum of 7,500 ft above sea level.
(2) Accuracy at a5° to +35°C.
(3) Not all combinations are available to prevent excessive Mach number. For the Mach
number 2.8 limit to be maintained:
Altitude of 60,000 ft means a CAS limit of 590.2 knots.
Airspeed of 650 knots means a limit of 55,147 ft.
Altitude
Rate of Climb
(ROC)
Calibrated Airspeed Mach
Units
feet
ft/min
knots
-
Operating Range
(1)
-2000 to 60,000
(3)
0 to 40,000
20 to 650
0.16 to 2.8
Measurement
up to 105,000
0 to 40,000
0 to 1000
10
Accuracy (2)
±3 at sea level
±7 at 30,000
±29 at 60,000
±2% of value
±0.5kts at 50kts
±0.5kts at 550kts
Better than
0.005
Repeatability
±1 at sea level
±2 at 30,000
±7 at 60,000
±0.5%
(measurement)
±0.4kts at 50kts
±0.02kts at 550kts
0.001
rising to
0.005
Resolution
1
1
0.1
0.001