NOTE: With EVS inoperative or with one or more EVS SSPCs pulled or tripped a blue “Landing Gear System Fault” CAS message may be displayed.
None required.
None required.
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
1) EVS Window Heat
***
D
1
0
None required.
None required.
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
2) Secondary (non-HUD)
*** EVS Display Repeater
D
1
0
May be inoperative provided procedures are not dependent on its use.
None required.
None required.
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
31. Terrain Server
Function/EGPWM
Modules
C
2
0
NOTE: Synthetic Vision PFD synthetic terrain will not be available with dual Terrain Server failures, but the full PFD may be used without restriction.
None required.
None required.
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
32. Advanced Graphics
Module (AGM)
C
4
3
(M)(O) May be inoperative provided:
Inoperative AGM is located in the AGM 3 position, and
Crew actions for subsequent failures are established.
Maintenance will move the inoperative AGM module to the AGM 3 position.
Flight crew may accomplish this task if properly qualified and authorized.
Flight crew will discuss the alternate procedures for sharing displays including if a display fails during all phases of flight including takeoff, approach, landing, and go-around.
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
C
4
3
(O) May be inoperative provided:
Inoperative AGM is electronically switched to the AGM 3 position, resulting in DU 3 Red Xing, and
Crew actions for subsequent failures are established.
None required.
Flight crew will ensure:
a) The failed AGM is electronically switched to the number 3 position,
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
35. Cursor Control
Devices
C
2
0
(M)(O) May be inoperative provided:
Both Standby Multi-Function Controllers (SMCs) are operative, and
Current terminal charts for the origin, destination and alternate airports are verified to be current and onboard the aircraft and available to the flight crew.
Maintenance will pull and collar the circuit breaker for the inoperative CCD.
Flight crew will ensure that terminal charts for the origin, destination and alternate airports are verified to be current and/or EFB’s are carried on board the aircraft prior to dispatch.
An Inoperative Placard will be displayed in a prominent position to be seen by flight crew and will be noted on ADLS.
36. Multi-function Control
Display Units (MCDU)
C
3
2
(M) May be inoperative provided:
The FMS functions and Radio Tuning functions are operative on the remaining MCDU’s,
