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Why can't we use APU bleed for wing anti-icing? A320

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Why can't we use APU bleed for wing anti-icing? A320

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Old 14th May 2026 | 19:42
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Why can't we use APU bleed for wing anti-icing? A320

Hello everyone,

Long story short, I've started my TR few weeks ago, and during one of the sessions I've asked my instructor, what's the reason we can't use APU bleed air for wing anti-icing? He was puzzeled by this question and said that he doesn't know to be honest, so he gave me a "homework" till the next session to figure this out. I'm aware that it can be used for wing anti-ice testing for 30s before automatically stoping but that is not the answer hes looking for, the main question is why can't we use it regurally. I've tried looking into the FCOM and AFM but no luck. Could any one of you guys help me out?

Aircraft in question A320
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Old 14th May 2026 | 22:04
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Would that not require drawing bleed air from the APU and routing that air some possibly considerable distance from the APU to the wings?

If the APU doesn't already supply bleed air, then how would there be any available?
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Old 14th May 2026 | 22:23
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Would the APU provide sufficient bleed air to deice the entire aircraft?
Another factor may be the space / weight / complexity of the required ducting and wiring.
What would the be probability of needing the capability? ( the dreaded cost / benefit analysis ) .
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Old 14th May 2026 | 22:43
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Because the air from apu bleed air doesn’t go through the precooler and it’s too hot for the wing surface
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Old 14th May 2026 | 23:13
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Originally Posted by easymxp
Because the air from apu bleed air doesn’t go through the precooler and it’s too hot for the wing surface
Learning something new everyday.
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Old 15th May 2026 | 09:51
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Originally Posted by easymxp
Because the air from apu bleed air doesn’t go through the precooler and it’s too hot for the wing surface
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Old 15th May 2026 | 13:38
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Precooler?
And the difference with the 737 is...?
Honestly confused.
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Old 18th May 2026 | 14:06
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Nothing to do with bleed temps, just Airbus chose not to certify use of APU bleed for wing anti-ice on the A320 wheres Boeing did (with conditions).

Most of it is to do with continuous output being not sufficent through the flight envelope (from the APU) wheras it is from the engines when serviceable.

That's my understanding.
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Old 19th May 2026 | 16:09
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The APU is able to deliver +/- 1.2kg/s bleed flow.
The 2 air conditioning packs need +/- 1 kg/s bleed flow.
The 2 WAI valves need +/- 0.7 kg/s bleed flow.
Therefore, as the APU and the engine cannot deliver together bleed to the aircraft, if the APU is selected for the bleed, the APU is not able to deliver enough bleed flow for the Packs and the Wing Anti-Ice.
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Old 19th May 2026 | 21:16
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It cant deliver suitable mass flow on it's own to ensure equal and effective deicing of the leading edge.
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Old 23rd May 2026 | 12:29
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APU bleed vs engine bleeds

On the A320 series, the second the APU bleed is on, both engine PRVs close. It's designed that way.

It is hard to imagine a scenario where you would want your engine bleeds off and be using the APU bleed for wing anti ice.
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