DOC AIRBUS | MMEL OPS PROCDC Main Generation (TR 1 inoperative)
| 24-32-01A | DC Main Generation (TR 1 inoperative) |
|---|
Applicable to: -
- Flight preparation/Limitations
Maximum
landing capability is CAT 3 SINGLE.
- During preliminary cockpit preparation
- TR 1/CNTOR/SPLY (125VU CF01) C/BPull
On the ELEC SD Page, disregard the indications related to the deactivated TR 1.
On the ELEC SD Page, check that the TR 2 and the ESS TR voltages are both equal to or above 27 V.
The batteries must be set to
OFF for the following check: On the battery voltage indicator, check
that the BAT 1 and the BAT 2 voltages are both
equal to or above 25.5 V.