DOC AIRBUS | MMEL OPS PROCWing Anti-Ice Control Valve
| 30-11-01A | Wing Anti-Ice Control Valve |
|---|
Applicable to: -
- Flight preparation/limitations
Flight planning:
Increase fuel consumption by:
Zp (ft) | 5000 | 10000 | 15000 | 20000 | 25000 | 30000 | 35000 | 40000 |
|---|---|---|---|---|---|---|---|---|
| Fuel penalties | 5.2 % | 4.7 % | 7.3 % | 4.0 % | 4.0 % | 3.2 % | 3.1 % | 1.0 % |
Single engine cruise:
Decrease drift down ceilings
by:
880 ft when OAT ≤ ISA + 5 °C
5970 ft when OAT > ISA + 5 °C
Approach climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight by:
380 kg ( 840 lb) when OAT ≤ ISA + 5 °C
5760 kg ( 12700 lb) when OAT > ISA + 5 °C
- During cockpit preparation
After application of the maintenance procedure:
On the BLEED SD Page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow
symbol may be displayed amber or green.
The WING ANTI
ICE L(R) HI PR alert
must not be displayed on the EWD.
- Before engine start
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED
selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START
( Refer to FCOM) procedure to start
the engine 2.
Apply the procedure associated
with the WING
ANTI ICE R VALVE OPEN alert displayed on the EWD.
- After takeoff
When above 1500 ft:
Apply the automatic
recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
- In Flight
If the wing anti ice is operated
in flight, WING
ANTI ICE R HI PR alert
may be displayed on the EWD.
In the case of failure of a Bleed Air Supply System:
If both PACKs are operative:
- PACK (affected side) pb-swOFF
- After landing
Apply the automatic recall of
the WING ANTI
ICE R VALVE OPEN procedure
displayed on the EWD.
| 30-11-01A | Wing Anti-Ice Control Valve |
|---|
Applicable to: -
- Flight preparation/limitations
Flight planning:
Increase fuel consumption by:
Zp (ft) | 5000 | 10000 | 15000 | 20000 | 25000 | 30000 | 35000 | 40000 |
|---|---|---|---|---|---|---|---|---|
| Fuel penalties | 5.8 % | 5.3 % | 7.0 % | 4.6 % | 5.2 % | 2.9 % | 2.8 % | 2.7 % |
Single engine cruise:
Decrease drift down ceilings
by:
950 ft when OAT ≤ ISA + 5 °C
6400 ft when OAT > ISA + 5 °C
Approach climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight by:
300 kg ( 660 lb) when OAT ≤ ISA + 10 °C
5500 kg ( 12100 lb) when OAT > ISA + 10 °C
- During cockpit preparation
After application of the maintenance procedure:
On the BLEED SD Page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow
symbol may be displayed amber or green.
The WING ANTI
ICE L(R) HI PR alert
must not be displayed on the EWD.
- Before engine start
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED
selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START
( Refer to FCOM) procedure to start
the engine 2.
Apply the procedure associated
with the WING
ANTI ICE R VALVE OPEN alert displayed on the EWD.
- After takeoff
When above 1500 ft:
Apply the automatic
recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
- In Flight
If the wing anti ice is operated
in flight, WING
ANTI ICE R HI PR alert
may be displayed on the EWD.
In the case of failure of a Bleed Air Supply System:
If both PACKs are operative:
- PACK (affected side) pb-swOFF
- After landing
Apply the automatic recall of
the WING ANTI
ICE R VALVE OPEN procedure
displayed on the EWD.
| 30-11-01A | Wing Anti-Ice Control Valve |
|---|
Applicable to: -
- Flight preparation/limitations
Flight planning:
Increase
fuel consumption by:
Zp (ft) | 5000 | 10000 | 15000 | 20000 | 25000 | 30000 | 35000 | 40000 |
|---|---|---|---|---|---|---|---|---|
| Fuel penalties | 5.0 % | 4.5 % | 5.0 % | 4.0 % | 3.0 % | 2.5 % | 2.5 % | 2.5 % |
Single engine
cruise:
Decrease
drift down ceilings by:
500 ft when OAT ≤ ISA
3200 ft when OAT > ISA
Approach
climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight
by:
600 kg ( 1400 lb) when OAT ≤ ISA + 10 °C
3100 kg ( 6900 lb) when OAT > ISA + 10 °C
- During cockpit preparation
After application of the maintenance procedure:
On the BLEED SD Page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow
symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
- Before engine start
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED
selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START
( Refer to FCOM) procedure to start
the engine 2.
Apply the procedure associated
with the WING
ANTI ICE R VALVE OPEN alert displayed on the EWD.
- After takeoff
When above 1500 ft:
Apply the automatic
recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
- In Flight
If the wing anti ice is operated
in flight, WING
ANTI ICE R HI PR alert
may be displayed on the EWD.
In the case of failure of a Bleed Air Supply System:
If both PACKs are operative:
- PACK (affected side) pb-swOFF
- After landing
Apply the automatic recall of
the WING ANTI
ICE R VALVE OPEN procedure
displayed on the EWD.
| 30-11-01A | Wing Anti-Ice Control Valve |
|---|
Applicable to: -
- Flight preparation/limitations
Flight planning:
Increase
fuel consumption by:
Zp (ft) | 5000 | 10000 | 15000 | 20000 | 25000 | 30000 | 35000 | 40000 |
|---|---|---|---|---|---|---|---|---|
| Fuel penalties | 4.5 % | 4.0 % | 5.0 % | 4.0 % | 4.0 % | 3.5 % | 3.0 % | 2.5 % |
Single engine
cruise:
Decrease
drift down ceilings by:
600 ft when OAT ≤ ISA
2300 ft when OAT > ISA
Approach
climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight
by:
1100 kg ( 2500 lb) when OAT ≤ ISA + 5 °C
4500 kg ( 10000 lb) when OAT > ISA + 5 °C
- During cockpit preparation
After application of the maintenance procedure:
On the BLEED SD Page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow
symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
- Before engine start
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED
selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START
( Refer to FCOM) procedure to start
the engine 2.
Apply the procedure associated
with the WING
ANTI ICE R VALVE OPEN alert displayed on the EWD.
- After takeoff
When above 1500 ft:
Apply the automatic
recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
- In Flight
If the wing anti ice is operated
in flight, WING
ANTI ICE R HI PR alert
may be displayed on the EWD.
In the case of failure of a Bleed Air Supply System:
If both PACKs are operative:
- PACK (affected side) pb-swOFF
- After landing
Apply the automatic recall of
the WING ANTI
ICE R VALVE OPEN procedure
displayed on the EWD.
| 30-11-01A | Wing Anti-Ice Control Valve |
|---|
Applicable to: -
- Flight preparation/limitations
Flight planning:
Increase
fuel consumption by:
Zp (ft) | 5000 | 10000 | 15000 | 20000 | 25000 | 30000 | 35000 | 40000 |
|---|---|---|---|---|---|---|---|---|
| Fuel penalties | 4.5 % | 4.5 % | 6.0 % | 4.5 % | 3.5 % | 2.5 % | 2.5 % | 2.5 % |
Single engine
cruise:
Decrease
drift down ceilings by:
1100 ft when OAT ≤ ISA
4500 ft when OAT > ISA
Approach
climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight
by:
800 kg ( 1800 lb) when OAT ≤ ISA + 5 °C
4900 kg ( 10900 lb) when OAT > ISA + 5 °C
- During cockpit preparation
After application of the maintenance procedure:
On the BLEED SD Page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow
symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
- Before engine start
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED
selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START
( Refer to FCOM) procedure to start
the engine 2.
Apply the procedure associated
with the WING
ANTI ICE R VALVE OPEN alert displayed on the EWD.
- After takeoff
When above 1500 ft:
Apply the automatic
recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
- In Flight
If the wing anti ice is operated
in flight, WING
ANTI ICE R HI PR alert
may be displayed on the EWD.
In the case of failure of a Bleed Air Supply System:
If both PACKs are operative:
- PACK (affected side) pb-swOFF
- After landing
Apply the automatic recall of
the WING ANTI
ICE R VALVE OPEN procedure
displayed on the EWD.
| 30-11-01A | Wing Anti-Ice Control Valve |
|---|
Applicable to: -
- Flight preparation/limitations
Flight planning:
Increase
fuel consumption by:
Zp (ft) | 5000 | 10000 | 15000 | 20000 | 25000 | 30000 | 35000 | 40000 |
|---|---|---|---|---|---|---|---|---|
| Fuel penalties | 4.5 % | 4.0 % | 6.0 % | 4.5 % | 3.5 % | 2.5 % | 2.5 % | 2.5 % |
Single engine
cruise:
Decrease
drift down ceilings by:
900 ft when OAT ≤ ISA
3300 ft when OAT > ISA
Approach
climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight
by:
800 kg ( 1800 lb) when OAT ≤ ISA + 20 °C
4100 kg ( 9100 lb) when OAT > ISA + 20 °C
- During cockpit preparation
After application of the maintenance procedure:
On the BLEED SD Page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow
symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
- Before engine start
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED
selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START
( Refer to FCOM) procedure to start
the engine 2.
Apply the procedure associated
with the WING
ANTI ICE R VALVE OPEN alert displayed on the EWD.
- After takeoff
When above 1500 ft:
Apply the automatic
recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
- In Flight
If the wing anti ice is operated
in flight, WING
ANTI ICE R HI PR alert
may be displayed on the EWD.
In the case of failure of a Bleed Air Supply System:
If both PACKs are operative:
- PACK (affected side) pb-swOFF
- After landing
Apply the automatic recall of
the WING ANTI
ICE R VALVE OPEN procedure
displayed on the EWD.
| 30-11-01A | Wing Anti-Ice Control Valve |
|---|
Applicable to: -
- Flight preparation/limitations
Flight planning:
Increase
fuel consumption by:
Zp (ft) | 5000 | 10000 | 15000 | 20000 | 25000 | 30000 | 35000 | 40000 |
|---|---|---|---|---|---|---|---|---|
| Fuel penalties | 4.0 % | 4.0 % | 4.5 % | 3.5 % | 3.5 % | 3.0 % | 2.5 % | 2.0 % |
Single engine
cruise:
Decrease
drift down ceilings by:
500 ft when OAT ≤ ISA
2300 ft when OAT > ISA
Approach
climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight
by:
1100 kg ( 2500 lb) when OAT ≤ ISA + 5 °C
4300 kg ( 9500 lb) when OAT > ISA + 5 °C
- During cockpit preparation
After application of the maintenance procedure:
On the BLEED SD Page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow
symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
- Before engine start
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED
selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START
( Refer to FCOM) procedure to start
the engine 2.
Apply the procedure associated
with the WING
ANTI ICE R VALVE OPEN alert displayed on the EWD.
- After takeoff
When above 1500 ft:
Apply the automatic
recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
- In Flight
If the wing anti ice is operated
in flight, WING
ANTI ICE R HI PR alert
may be displayed on the EWD.
In the case of failure of a Bleed Air Supply System:
If both PACKs are operative:
- PACK (affected side) pb-swOFF
- After landing
Apply the automatic recall of
the WING ANTI
ICE R VALVE OPEN procedure
displayed on the EWD.
| 30-11-01A | Wing Anti-Ice Control Valve |
|---|
Applicable to: -
- Flight preparation/limitations
Flight planning:
Increase
fuel consumption by:
Zp (ft) | 5000 | 10000 | 15000 | 20000 | 25000 | 30000 | 35000 | 40000 |
|---|---|---|---|---|---|---|---|---|
| Fuel penalties | 7 % | 6.5 % | 5.5 % | 4 % | 4 % | 2.5 % | 2.5 % | 2.5 % |
Single engine
cruise:
Decrease
drift down ceilings by:
1400 ft when OAT ≤ ISA
4600 ft when OAT > ISA
Approach
climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight
by:
800 kg ( 1800 lb) when OAT ≤ ISA + 5 °C
4900 kg ( 10900 lb) when OAT > ISA + 5 °C
- During cockpit preparation
After application of the maintenance procedure:
On the BLEED SD Page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow
symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
- Before engine start
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED
selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START
( Refer to FCOM) procedure to start
the engine 2.
Apply the procedure associated
with the WING
ANTI ICE R VALVE OPEN alert displayed on the EWD.
- After takeoff
When above 1500 ft:
Apply the automatic
recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
- In Flight
If the wing anti ice is operated
in flight, WING
ANTI ICE R HI PR alert
may be displayed on the EWD.
In the case of failure of a Bleed Air Supply System:
If both PACKs are operative:
- PACK (affected side) pb-swOFF
- After landing
Apply the automatic recall of
the WING ANTI
ICE R VALVE OPEN procedure
displayed on the EWD.
| 30-11-01A | Wing Anti-Ice Control Valve |
|---|
Applicable to: -
- Flight preparation/limitations
Flight planning:
Increase
fuel consumption by:
Zp (ft) | 5000 | 10000 | 15000 | 20000 | 25000 | 30000 | 35000 | 40000 |
|---|---|---|---|---|---|---|---|---|
| Fuel penalties (%) | 3.5 % | 2.5 % | 2.5 % | 3.0 % | 3.5 % | 3.5 % | 3.5 % | 3.5 % |
Single engine
cruise:
Decrease
drift down ceilings by:
1500 ft when OAT ≤ ISA + 20 °C
2700 ft when OAT > ISA + 20 °C
Approach
climb performance:
When the engine bleed air supply system is closed:
No penalty.
When the engine bleed air supply system is open:
Decrease maximum climb limiting weight
by:
2300 kg ( 5100 lb)
- During cockpit preparation
After application of the maintenance procedure:
On the BLEED SD Page, check that the anti-ice arrow symbol is displayed.
The anti-ice arrow
symbol may be displayed amber or green.
The WING ANTI ICE L(R) HI PR alert must not be displayed on the EWD.
- Before engine start
Maintain the X BLEED selector at SHUT before engine start when the APU bleed is used.
Start the engine 1.
Maintain the X BLEED
selector at SHUT during the start of engine 1.
Use the CROSS BLEED ENGINE START
( Refer to FCOM) procedure to start
the engine 2.
Apply the procedure associated
with the WING
ANTI ICE R VALVE OPEN alert displayed on the EWD.
- After takeoff
When above 1500 ft:
Apply the automatic
recall of the WING ANTI ICE R VALVE OPEN procedure displayed on the EWD.
- In Flight
If the wing anti ice is operated
in flight, WING
ANTI ICE R HI PR alert
may be displayed on the EWD.
In the case of failure of a Bleed Air Supply System:
If both PACKs are operative:
- PACK (affected side) pb-swOFF
- After landing
Apply the automatic recall of
the WING ANTI
ICE R VALVE OPEN procedure
displayed on the EWD.