MAU A Fail
3-22-25
continued
6.
Landing.......................................
Engine power may remain at flight idle.
Reverse operation is not affected by this
fault.
---------- END -----------
MAU B Fail
3-22-26
1.
MAU CH. B1 circuit breaker
(Standby Bus
L
Z3).......................
Open, Wait 2 seconds and close
If failure remains:
2.
Display Reversion Control Panel
Set LOWER MFD control knob to
OFF/REV
3.
Display Reversion Control Panel
Set CO-PILOTS PFD control knob to
AGM1
If dual FMS is installed and access to FMS is desired:
4.
Pilot PFD controller.....................
Set NAV SEL to FMS 2
Note
If MAU Channel B cannot be reset, Autopilot, Flight Director, Yaw Damper and
XPDR 2 are not available for remainder of the flight.
For single FMS installations: FMS is not available for the remainder of the flight.
5.
Landing.......................................
Engine power may remain at flight idle.
Reverse operation is not affected by this
fault.
---------- END -----------
Air/Ground Fail
3-22-27
On ground:
1.
Aircraft.........................................
Do not fly, maintenance required
--- END ---
In flight:
1.
Aircraft.........................................
All systems will default to “In Air”
---------- END -----------
Section 3 - Emergency Procedures (EASA Approved)
APEX Failures
Pilot's Operating Handbook
Report No: 02406
Issue date: Mar 06, 2020
Page 3-22-13
12-C-A15-40-0322-00A-141A-A
FOR
GENERAL
AND
FAMILIARIZATION
PURPOSES
ONLY
