POH
AQUILA AT01-200C
SECTION 3
EMERGENCY PROCEDURES
Document Nr.:
Issue:
Supersedes Issue:
Date:
Page:
FM-AT01-1010-106
A.01
--- (first issue)
02.03.2020
3 - 23
3.13.7 AHRS Failure
1. Attitude
Natural horizon
NOTE
In the event of an AHRS Failure, the horizon is no longer displayed on the PFD. Additionally a
red “X” and in yellow “AHRS FAILURE” is displayed. A Navigation System Failure, as described
in section 3.13.6, accompanies an AHRS Failure.
3.13.8 ADC Failure
1. Continue flight
Using stand-by instruments (see 3.13.4)
NOTE
Failure of the Air Data Computers (ADC) is indicated through a red X and yellow text above the
airspeed indicator, the altimeter, the vertical speed indicator, the TAS and the OAT indicators.
Certain functions, such as TAS and wind calculation, are no longer usable.
3.13.9 Complete MVP-50P-AQ Failure
1.
Engine Instr 1
circuit breaker
(see 3.1.1)
RESET, if tripped
If the MVP-50P-AQ failure cannot be corrected, maintain power settings and land at the nearest
suitable airfield.
NOTE
During a total failure of the Glass Engine Monitoring Instrument AND modified power settings a
RPM overshoot is not possible with the following settings:
1) Throttle (MP):
100% indexed position
2) Propeller Control Lever (rpm):
⇒
During climb:
HIGH RPM
⇒
All other flight phases:
below marking „MCP“
