SPIDER 8 - Page 30

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ADC 2
Perform a system function test.
Verify correct display of airspeed,
altitude, TAT, TAS.
☐
HEATER / ECS
Operate in all modes.
☐
FUEL QUANTITY
Monitor for erroneous or erratic
indications.
☐
FUEL SYSTEM
Monitor for erroneous or erratic
indications.
☐
HYDRAULIC SYS
Cycle hydraulic pumps. Monitor
f o r e r r o n e o u s o r e r r a t i c
indications.
☐
FUEL CONTROL
Cycle system to manual and back
to auto. Monitor for erroneous or
erratic indications.
☐
FIRE DETECTION
SYSTEM(S)
Monitor for erroneous or erratic
indications.
☐
ENGINE
INDICATING
Run engines. Verif y proper
functioning. Monitor for erroneous
or erratic indications. Transfer
electrical busses to all engine
driven generator(s).
☐
AC/DC
ELECTRICAL
SYSTEMS
Configure the electrical systems
in different modes. Verify no
interference when switching loads
from one bus to another.
☐
MAST MOMENT
INDICATOR
Monitor for erroneous or erratic
indications.
☐
FADEC / DECU
Run engines in all modes. Monitor
f o r e r r o n e o u s o r e r r a t i c
indications.
☐
VEMD
Run engines in all modes. Monitor
f o r e r r o n e o u s o r e r r a t i c
indications.
☐
PITOT STATIC
HEAT
Confirm correct operation.
☐
EMERGENCY
LIGHTS
Monitor for inadvertent activation.
☐
PARTICLE
SEPERATOR
Monitor for erroneous indications.
☐
Aircraft System
Under Test
Test Instructions
Passed
Observations
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