Digital Air Data Computer (Dadc) Self--Test Mode - Honeywell SPZ-8000 Pilot's Manual

Digital integrated flight control system
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SPZ--8000 Digital Integrated Flight Control System
DIGITAL AIR DATA COMPUTER (DADC) SELF--TEST
MODE
The digital air data computer (DADC) incorporates a self--test mode
that is activated with a cockpit test switch. The DADC outputs static test
data that is displayed on the altimeter, vertical speed indicator,
Mach/airspeed indicator and EFIS. Table 3--2 describes the DADC test
data.
Parameter
Pressure altitude
Baro altitude
Altitude rate
Indicated airspeed
True airspeed
Mach
Total air temperature
Static air temperature
Preselect altitude
V
MO
Dynamic pressure
M
MO
Baro set (inHg)
Baro set (mB)
DADC Self--Test Mode Display Results
Air Data System (ADS)
3-6
4000 ft
Present altitude
5000 ft/min
320 kts
301 kts
Mach .790
--16 _C
--45 _C
12,000 ft
301 kts
9.0 inHg
Mach .835
29.921 inHg
1013.3 mB
Table 3--2
Data Output
A28--1146--055
REV 2

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