DOC AIRBUS | MMEL OPS PROCANTI ICE ENG 1(2) CTL FAULT Alert
| 30-09-01A | ANTI ICE ENG 1(2) CTL FAULT Alert |
|---|
Applicable to: -
- General information
A higher idle speed is set on
both engines when the alert ANTI-ICE ENG 1(2) CTL FAULT is displayed on EWD with the ENG 1(2) A.ICE VALVE OPEN subtitle displayed.
- Flight preparation/limitations
Takeoff
performance:
The takeoff performance must
be determined by using OCTOPUS program or other equivalent program
with present failure case taken into account.
Launch PEP.
Flight planning:
Increase fuel consumption by:
Zp (ft) | ENG 1 CTL FAULT and ENG 2 CTL FAULT displayed | ENG 1(2) CTL FAULT displayed |
|---|---|---|
| 5000 | 1.2 % | 0.6 % |
| 10000 | 1.2 % | 0.6 % |
| 15000 | 1.2 % | 0.6 % |
| 20000 | 1.2 % | 0.6 % |
| 25000 | 1.2 % | 0.6 % |
| 30000 | 1.2 % | 0.6 % |
| 35000 | 1.2 % | 0.6 % |
| 40000 | 2.5 % | 1.3 % |
Single engine cruise:
Decrease drift down ceilings
by:
25 ft when OAT ≤ ISA + 5 °C
880 ft when OAT > ISA + 5 °C
Approach climb performance:
Decrease maximum climb limiting
weight by:
0 kg ( 0 lb) when OAT ≤ ISA + 10 °C
650 kg ( 1400 lb) when OAT > ISA + 10 °C
- During cockpit preparation
- ANTI ICE ENG (affected) pb-swON
| 30-09-01A | ANTI ICE ENG 1(2) CTL FAULT Alert |
|---|
Applicable to: -
- General information
A higher
idle speed is set on both engines when the alert ANTI-ICE ENG 1(2) CTL FAULT is displayed
on EWD with the ENG 1(2) A.ICE VALVE OPEN subtitle displayed.
- Flight preparation/limitations
Takeoff performance:
The takeoff performance must
be determined by using OCTOPUS program or other equivalent program
with present failure case taken into account.
Launch PEP.
Flight planning:
Increase fuel consumption by:
Zp (ft) | ENG 1 CTL FAULT and ENG 2 CTL FAULT displayed | ENG 1(2) CTL FAULT displayed |
|---|---|---|
| 5000 | 1.2 % | 0.6 % |
| 10000 | 1.2 % | 0.6 % |
| 15000 | 1.2 % | 0.6 % |
| 20000 | 1.2 % | 0.6 % |
| 25000 | 1.3 % | 0.6 % |
| 30000 | 1.3 % | 0.6 % |
| 35000 | 1.3 % | 0.6 % |
| 40000 | 2.3 % | 1.2 % |
Single engine cruise:
Decrease drift down ceilings
by:
0 ft when OAT ≤ ISA + 5 °C
950 ft when OAT > ISA + 5 °C
Approach climb performance:
Decrease maximum climb limiting
weight by:
0 kg ( 0 lb) when OAT ≤ ISA + 15 °C
500 kg ( 1200 lb) when OAT > ISA + 15 °C
- During cockpit preparation
- ANTI ICE ENG (affected) pb-swON