Engine Bleed Air Supply System (ETOPS flights)
| 36-11-01B | Engine Bleed Air Supply System (ETOPS flights) |
|---|
Applicable to: -
- Flight preparation/limitations
APU fuel consumption with
the APU ON (APU GEN OFF and APU BLEED OFF):
APU ON
(IDLE) | |||||||
|---|---|---|---|---|---|---|---|
| FL | GND | 100 | 200 | 315 | 354 | 370 | 390 |
| KG/H | 80 | 60 | 42 | 28 | 24 | 22 | 20 |
| LB/H | 176 | 132 | 93 | 62 | 53 | 49 | 44 |
The flight crew should take
into account the severity of forecast icing conditions. The wing anti-ice
will be lost if the remaining engine bleed air supply system becomes
inoperative.
- After engine start
- ENG BLEED (AFFECTED) pb-swOFF
- X BLEED OPEN
If both PACKs are operative:
If Wing Anti-Ice is not required:
- PACK FLOW selectorLO
The PACK FLOW selector must be set to LO due to precooler performance.
If Wing Anti-Ice is required:
- PACK (AFFECTED) pb-swOFF
If one PACK is inoperative:
- PACK FLOW selectorHI
- Before takeoff
- APU MASTER SW pb-swON
- APU START pb-swON
- For takeoff
Set at
least one air conditioning pack to off, or use the APU bleed
air supply system.
- After takeoff
If the APU has been used to supply the air conditioning during
the takeoff:
- APU BLEED pb-swOff
- In flight
If Wing Anti-Ice is required and both PACKs are operative:
- PACK (affected side) pb-swOFF
In the case of failure of the remaining engine bleed air supply
system, or in the case of failure of the associated engine:
Apply the associated ECAM procedure, then
| 36-11-01B | Engine Bleed Air Supply System (ETOPS flights) |
|---|
Applicable to: -
- Flight preparation/limitations
APU fuel consumption with
the APU ON (APU GEN OFF and APU BLEED OFF):
APU ON
(IDLE) | |||||||
|---|---|---|---|---|---|---|---|
| FL | GND | 100 | 200 | 315 | 354 | 370 | 390 |
| KG/H | 80 | 60 | 42 | 28 | 24 | 22 | 20 |
| LB/H | 176 | 132 | 93 | 62 | 53 | 49 | 44 |
The flight crew should take
into account the severity of forecast icing conditions. The wing anti-ice
will be lost if the remaining engine bleed air supply system becomes
inoperative.
If the (If Installed) cargo heating is switched
off:
For live animal transportation,
use the Live Animal Transportation Calculation Tool.
- After engine start
- ENG BLEED (AFFECTED) pb-swOFF
- X BLEED OPEN
If both PACKs are operative:
If Wing Anti-Ice is not required:
- ECON FLOW pb-swON
The ECON FLOW pb-sw must be set to ON due to precooler performance.
- AFT CARGO HOT AIR (If Installed) pb-swOFF
If Wing Anti-Ice is required:
- PACK (AFFECTED) pb-swOFF
If one PACK is inoperative:
- ECON FLOW pb-swOff
- Before takeoff
- APU MASTER SW pb-swON
- APU START pb-swON
- For takeoff
Set at
least one air conditioning pack to off, or use the APU bleed
air supply system.
- After takeoff
If the APU has been used to supply the air conditioning during
the takeoff:
- APU BLEED pb-swOff
- In flight
If Wing Anti-Ice is required and both PACKs are operative:
- PACK (affected side) pb-swOFF
In the case of failure of the remaining engine bleed air supply
system, or in the case of failure of the associated engine:
Apply the associated ECAM procedure, then
| 36-11-01B | Engine Bleed Air Supply System (ETOPS flights) |
|---|
Applicable to: -
- Flight preparation/limitations
APU fuel consumption with the APU ON (APU GEN OFF and APU BLEED OFF):
APU ON
(IDLE) | |||||||
|---|---|---|---|---|---|---|---|
| FL | GND | 100 | 200 | 315 | 354 | 370 | 390 |
| KG/H | 80 | 60 | 42 | 28 | 24 | 22 | 20 |
| LB/H | 176 | 132 | 93 | 62 | 53 | 49 | 44 |
The flight crew should take
into account the severity of forecast icing conditions. The wing anti-ice
will be lost if the remaining engine bleed air supply system becomes
inoperative.
If the (If Installed) cargo heating is switched
off:
For live animal transportation,
use the Live Animal Transportation Calculation Tool.
- After engine start
- ENG BLEED (AFFECTED) pb-swOFF
- AFT CARGO HOT AIR (If Installed) pb-swOFF
If both PACKs are operative:
- PACK (AFFECTED) pb-swOFF
- X BLEED OPEN
- Before takeoff
- APU MASTER SW pb-swON
- APU START pb-swON
- After takeoff
If the APU has been used to supply the air conditioning during
the takeoff:
- APU BLEED pb-swOff
- In flight
In the case of failure of the remaining engine bleed air supply
system, or in the case of failure of the associated engine:
Apply the AIR ENG 1+2 BLEED FAULT ECAM procedure.
| CAUTION: | Reset ENG BLEED pb-sw as requested by ECAM procedure even if the ENG
BLEED pb-sw is placarded inoperative as per MMEL 36-11-01. |
In the case of failure of the opposite PACK:
- PACK (AFFECTED) pb-swON