DOC AIRBUS | TSM A320F76-11 (CFMI) - THROTTLE CONTROL
- PB.201 THROTTLE CONTROL - FAULT ISOLATION PROCEDURES
-
76-11-00-810-803-A
[CFMI]
[8]
Loss of the TLA Resolver Signal through the two Channels on Engine 1 -
76-11-00-810-804-A
[CFMI]
[8]
Loss of the TLA Resolver Signal through the two Channels on Engine 2 -
76-11-00-810-805-A
[CFMI]
[8]
Loss of the TLA Resolver Signal through the Channel A on Engine 1 -
76-11-00-810-806-A
[CFMI]
[8]
Loss of the TLA Resolver Signal through the Channel A on Engine 2 -
76-11-00-810-807-A
[CFMI]
[8]
Loss of the TLA Resolver Signal through the Channel B on Engine 1 -
76-11-00-810-808-A
[CFMI]
[8]
Loss of the TLA Resolver Signal through the Channel B on Engine 2 -
76-11-00-810-811-A
[CFMI]
[8]
Internal Failure of the ECU on Engine 1 -
76-11-00-810-812-A
[CFMI]
[8]
Internal Failure of the ECU on Engine 2 -
76-11-00-810-813-A
[CFMI]
[8]
Disagree between the two TLA Resolver Signals on Engine 1 -
76-11-00-810-814-A
[CFMI]
[8]
Disagree between the two TLA Resolver Signals on Engine 2 -
76-11-00-810-821-A
[CFMI]
[8]
Engine Throttle Control Levers too Tight or too Loose -
76-11-00-810-823-A
[CFMI]
[8]
Engine Thrust Levers not set at Correct Position
-
76-11-00-810-803-A
[CFMI]
[8]