77-00 (CFMI) - ENGINE INDICATING - GENERAL
- PB.201 ENGINE INDICATING - GENERAL - FAULT ISOLATION PROCEDURES
-
77-00-00-810-823-A
[CFMI]
[8]
Disagree between the EGT Indication and the ECU Output on Engine 1 -
77-00-00-810-824-A
[CFMI]
[8]
Disagree between the EGT Indication and the ECU Output on Engine 2 -
77-00-00-810-827-A
[CFMI]
[8]
Disagree between the N1 Indication and the ECU Output on Engine 1 -
77-00-00-810-828-A
[CFMI]
[8]
Disagree between the N1 Indication and the ECU Output on Engine 2 -
77-00-00-810-831-A
[CFMI]
[8]
Disagree between the N2 Indication and the ECU Output on Engine 1 -
77-00-00-810-832-A
[CFMI]
[8]
Disagree between the N2 Indication and the ECU Output on Engine 2 -
77-00-00-810-833-A
[CFMI]
[8]
N1 Actual Lower than N1 Command on Engine 1 or 2 -
77-00-00-810-835-A
[CFMI]
[8]
Loss of N1 Indication on Engine 1 or 2 -
77-00-00-810-836-A
[CFMI]
[8]
Loss of N2 Indication on Engine 1 or 2 -
77-00-00-810-849-A
[CFMI]
[8]
EGT Overlimit on Engine 1 or 2 -
77-00-00-810-850-A
[CFMI]
[8]
N1 Overlimit on Engine 1 or 2 -
77-00-00-810-851-A
[CFMI]
[8]
N2 Overlimit on Engine 1 or 2 -
77-00-00-810-852-A
[CFMI]
[8]
Fluctuation of N1 or Auto Acceleration or Auto Deceleration or No Throttle Response to TLA Command on Engine 1 or 2 -
77-00-00-810-853-A
[CFMI]
[8]
EGT Indication Permanently Equal to 15 Deg.C on Engine 1 or 2 -
77-00-00-810-854-A
[CFMI]
[8]
Loss of the EGT Indication on Engine 1 or 2 -
77-00-00-810-855-A
[CFMI]
[8]
The EGT of one engine is significantly higher than on the other engine -
77-00-00-810-858-A
[CFMI]
[8]
N1/N2 Mismatch on the Same Engine, on Engine 1 or 2 -
77-00-00-810-859-A
[CFMI]
[8]
N1 Mismatch greater than 1% during Flex Take Off between Engine 1 and 2 -
77-00-00-810-860-A
[CFMI]
[8]
N1 Mismatch greater than 1% during Take Off between Engine 1 and 2 -
77-00-00-810-861-A
[CFMI]
[8]
N1 Mismatch greater than 1% at Climb between Engine 1 and 2 -
77-00-00-810-862-A
[CFMI]
[8]
Fan Vibration less than 4 Units with Noise / Rumble -
77-00-00-810-863-A
[CFMI]
[8]
Fan Vibrations Higher than or Equal to 4 Units and less than 6 Units on Engine 1 or 2 -
77-00-00-810-864-A
[CFMI]
[8]
Fan Vibrations Higher than or Equal to 6 Units on Engine 1 or 2 -
77-00-00-810-865-A
[CFMI]
[8]
Core Vibrations Higher than or Equal to 4.2 Units (1.68 Ips), and Less than 5.4 Units (2.16 Ips) on Engine 1 or 2 -
77-00-00-810-866-A
[CFMI]
[8]
Core Vibrations Higher than or Equal to 5.5 Units (2.2 Ips) on Engine 1 or 2 -
77-00-00-810-867-A
[CFMI]
[8]
Vibration Indications Fault -
77-00-00-810-874-A
[CFMI]
[8]
Loss of the Channel A of the FADEC on Engine 1 -
77-00-00-810-875-A
[CFMI]
[8]
Loss of the Channel A of the FADEC on Engine 1 -
77-00-00-810-876-A
[CFMI]
[8]
Loss of the Channel B of the FADEC on Engine 1 -
77-00-00-810-877-A
[CFMI]
[8]
Loss of the Channel B of the FADEC on Engine 1 -
77-00-00-810-878-A
[CFMI]
[8]
Loss of the Channel A of the FADEC on Engine 2 -
77-00-00-810-879-A
[CFMI]
[8]
Loss of the Channel A of the FADEC on Engine 2 -
77-00-00-810-880-A
[CFMI]
[8]
Loss of the Channel B of the FADEC on Engine 2 -
77-00-00-810-881-A
[CFMI]
[8]
Loss of the Channel B of the FADEC on Engine 2 -
77-00-00-810-882-A
[CFMI]
[8]
Loss of the Channels A and B of the FADEC on Engine 1 -
77-00-00-810-883-A
[CFMI]
[8]
Loss of the Channels A and B of the FADEC on Engine 1 -
77-00-00-810-884-A
[CFMI]
[8]
Loss of the Channels A and B of the FADEC on Engine 2 -
77-00-00-810-885-A
[CFMI]
[8]
Loss of the Channels A and B of the FADEC on Engine 2 -
77-00-00-810-886-A
[CFMI]
[8]
Loss of the Data on ARINC Bus from the EIU to the FADEC on Engine 1 -
77-00-00-810-887-A
[CFMI]
[8]
Loss of the Data on ARINC Bus from the EIU to the FADEC on Engine 2 -
77-00-00-810-888-A
[CFMI]
[8]
Failure of the Starter Shutoff Valve on Engine 1 -
77-00-00-810-889-A
[CFMI]
[8]
Failure of the Starter Shutoff Valve on Engine 2 -
77-00-00-810-890-A
[CFMI]
[8]
Type Disagree between Engine 1 and Engine 2 or between Engines and Aircraft Pin Programming -
77-00-00-810-910-A
[CFMI]
[8]
TO/GA Inputs Invalid on Engine 1 -
77-00-00-810-911-A
[CFMI]
[8]
TO/GA Inputs Invalid on Engine 2 -
77-00-00-810-914-A
[CFMI]
[8]
N2 Exceedance Indication on ECAM on Engine 1 -
77-00-00-810-915-A
[CFMI]
[8]
N2 Exceedance Indication on ECAM on Engine 2 -
77-00-00-810-916-A
[CFMI]
[8]
Vibration with Noise at approximately 51% N1 on Engine 1 -
77-00-00-810-917-A
[CFMI]
[8]
Vibration with Noise at approximately 51% N1 on Engine 2 -
77-00-00-810-920-A
[CFMI]
[8]
Throttle Control Lever in Reverse Thrust Position in Flight -
77-00-00-810-932-A
[CFMI]
[8]
ENG 1 FADEC without fault message associated -
77-00-00-810-933-A
[CFMI]
[8]
ENG 2 FADEC without fault message associated
-
77-00-00-810-823-A
[CFMI]
[8]