Vibration with Noise at approximately 51% N1 on Engine 1
TASK 77-00-00-810-916-A
Vibration with Noise at approximately 51% N1 on Engine 1
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
3. Fault Confirmation
Subtask 77-00-00-869-050-C ** ON A/C NOT FOR ALL
Subtask 77-00-00-810-200-C ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:37:35 UTC
Vibration with Noise at approximately 51% N1 on Engine 1
1. Possible Causes
2. Job Set-up Information
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 77-32-34-750-001 | Fan Trim Balance with the EVMU (one Shot Method) |
| AMM 77-32-34-860-042 | Acquire Unbalance Data During the Flight and Read Unbalance Data |
Subtask 77-00-00-869-050-C ** ON A/C NOT FOR ALL
A. Prior to perform the fault isolation, the flight vibration data must be available for the engine speeds listed below:
4. Fault Isolation| N1 SPEED A319 A320 | N1 SPEED A321 | N1 tolerance | Time |
|---|---|---|---|
| 51% 64% 84% 88% 92% | 51% 64% 88% 92% 96% | 2% 2% 2% 2% 2% | 15sec. 15sec. 15sec. 15sec. 15sec. |
- if these data are not available acquire these values and do the fault isolation at the first opportunity AMM 77-32-34-860-042.
Subtask 77-00-00-810-200-C ** ON A/C NOT FOR ALL
A. Balance the engine with the EVMU using the flight data as follows:
(1) Cold trim balance the engine using the one shot method AMM 77-32-34-750-001.
(4) If the vibration continues with engine N1 vib less than 2 units, cold trim balance the engine using the vectorial method with the 51% N1 speed only, using current vib manual input option, according to EVMU flight data print.
NOTE: For information, hereafter are the CFM56-5B One Shot Coefficients:
| N1 bearing vib sensor | N1 bearing vib sensor | TRF vib sensor | TRF vib sensor | |
|---|---|---|---|---|
| 96 92 88 84 64 51-52 | 205 235 300 225 365 500 | 160 175 200 170 185 205 | 305 330 400 370 285 550 | 185 225 245 230 230 45 |
NOTE: In SCREWS TO CHANGE menu, push the line key adjacent to the UPDATE indication to memorize the EVMU calculation.
- dispatch the aircraft.
NOTE: In SCREWS TO CHANGE menu, push the line key adjacent to the UPDATE indication to memorize the EVMU calculation.
- dispatch the aircraft.
(4) If the vibration continues with engine N1 vib less than 2 units, cold trim balance the engine using the vectorial method with the 51% N1 speed only, using current vib manual input option, according to EVMU flight data print.
NOTE: In SCREWS TO CHANGE menu, push the line key adjacent to the UPDATE indication to memorize the EVMU calculation.