Dear Airbus, please can you
Thread Starter

Joined: Apr 2011
Posts: 487
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From: Doha
Dear Airbus, please can you
Dear Airbus
In your latest FCOM for the A320 family, in Aircraft Systems, Aircraft General, Ground Clearance Diagrams, you’ve removed the actual figures and just left us with the dots to try and work out the actual numbers. Knowing from old FCOMs, I am ok, but anyone going onto the A320 will just have to try and guess what the actual figures are for expanse A321 9.7 and 11.2, A320 11.7 and 13.5 and A319 13.9 and 15.5.
Please can you put the figures back on the side lines
In your latest FCOM for the A320 family, in Aircraft Systems, Aircraft General, Ground Clearance Diagrams, you’ve removed the actual figures and just left us with the dots to try and work out the actual numbers. Knowing from old FCOMs, I am ok, but anyone going onto the A320 will just have to try and guess what the actual figures are for expanse A321 9.7 and 11.2, A320 11.7 and 13.5 and A319 13.9 and 15.5.
Please can you put the figures back on the side lines
Joined: Feb 2002
Posts: 115
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From: US
How's the exact number relevant?! There's no way to read the attitude to the 10th of a degree on your PFD. Let alone determine if the struts are compressed, semi-compressed or not compressed.
Don't you think it's more relevant to look at factors that influence the tail clearance? Significant crosswind, tailwind, high gross weight, (threats), high rotation rate, early rotation, incorrect performance calculation, incorrect oleo inflation (errors) etc. And try to eliminate them? I.e. use correct take off rotation techniques, consider using a higher flap setting or higher thrust setting when the above factors are present?
Don't you think it's more relevant to look at factors that influence the tail clearance? Significant crosswind, tailwind, high gross weight, (threats), high rotation rate, early rotation, incorrect performance calculation, incorrect oleo inflation (errors) etc. And try to eliminate them? I.e. use correct take off rotation techniques, consider using a higher flap setting or higher thrust setting when the above factors are present?
Thread Starter

Joined: Apr 2011
Posts: 487
Likes: 42
From: Doha
How's the exact number relevant?! There's no way to read the attitude to the 10th of a degree on your PFD. Let alone determine if the struts are compressed, semi-compressed or not compressed.
Don't you think it's more relevant to look at factors that influence the tail clearance? Significant crosswind, tailwind, high gross weight, (threats), high rotation rate, early rotation, incorrect performance calculation, incorrect oleo inflation (errors) etc. And try to eliminate them? I.e. use correct take off rotation techniques, consider using a higher flap setting or higher thrust setting when the above factors are present?
Don't you think it's more relevant to look at factors that influence the tail clearance? Significant crosswind, tailwind, high gross weight, (threats), high rotation rate, early rotation, incorrect performance calculation, incorrect oleo inflation (errors) etc. And try to eliminate them? I.e. use correct take off rotation techniques, consider using a higher flap setting or higher thrust setting when the above factors are present?
Last edited by Black Pudding; 8th March 2020 at 20:06.

Joined: Sep 2016
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From: USA
I would venture that if they're not supplied to the trainee, they won't be asked about? How can they? I'm lost.

Joined: Apr 2009
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From: Canada
Joined: Mar 2001
Posts: 4,563
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From: I wouldn't know.
How's the exact number relevant?! There's no way to read the attitude to the 10th of a degree on your PFD. Let alone determine if the struts are compressed, semi-compressed or not compressed.
Don't you think it's more relevant to look at factors that influence the tail clearance? Significant crosswind, tailwind, high gross weight, (threats), high rotation rate, early rotation, incorrect performance calculation, incorrect oleo inflation (errors) etc. And try to eliminate them? I.e. use correct take off rotation techniques, consider using a higher flap setting or higher thrust setting when the above factors are present?
Don't you think it's more relevant to look at factors that influence the tail clearance? Significant crosswind, tailwind, high gross weight, (threats), high rotation rate, early rotation, incorrect performance calculation, incorrect oleo inflation (errors) etc. And try to eliminate them? I.e. use correct take off rotation techniques, consider using a higher flap setting or higher thrust setting when the above factors are present?

Joined: Feb 2000
Posts: 4,704
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From: 500 miles from Chaikhosi, Yogistan
That’s how you can gauge a trainee’s understanding of a topic, rather than a rote leaned number.
That said, I see no harm in having in the manuals, although it may be encouraging pilots to look at their PFD s rather than the picture outside. Get that right and inside will be just fine.
Only half a speed-brake

Joined: Apr 2003
Posts: 4,459
Likes: 136
From: Commuting not home
Agreed with the concept stated above. Although wish this was discussed over a different parameter such as safety (overpressure) release valve trigger setting.
For Tailstrike pitch limit, both with oleos extended or compressed, a proper practice for PM is to observe the PFD and call out "pitch, pitch" if approaching the limiting attitude. AFAIK most aircraft today are modded with auto-callout to do exactly that for landing.
Headless rota learning? No thanks.
Knowing your A/C limits properly to safeguard the operation? Well, nobody wants to devaluate the profession, do we.

Sorry to spoil the party.
For Tailstrike pitch limit, both with oleos extended or compressed, a proper practice for PM is to observe the PFD and call out "pitch, pitch" if approaching the limiting attitude. AFAIK most aircraft today are modded with auto-callout to do exactly that for landing.
Headless rota learning? No thanks.
Knowing your A/C limits properly to safeguard the operation? Well, nobody wants to devaluate the profession, do we.

Sorry to spoil the party.

Joined: Jul 2006
Posts: 1,100
Likes: 111
From: Somewhere over the rainbow
I agree with Ollie Onion. I think what it's really important is for the PM to closely monitor the pitch during the flare and to do the standard call out in due time when applicable: >10 degrees for 319/320 or >7.5 degrees for A321.
From the old FCOM, the tail strike value for A321 was at 9.5 degrees and A320 11.5 degrees with the gears fully compressed.
From the old FCOM, the tail strike value for A321 was at 9.5 degrees and A320 11.5 degrees with the gears fully compressed.
Thread Starter

Joined: Apr 2011
Posts: 487
Likes: 42
From: Doha
I agree with Ollie Onion. I think what it's really important is for the PM to closely monitor the pitch during the flare and to do the standard call out in due time when applicable: >10 degrees for 319/320 or >7.5 degrees for A321.
From the old FCOM, the tail strike value for A321 was at 9.5 degrees and A320 11.5 degrees with the gears fully compressed.
From the old FCOM, the tail strike value for A321 was at 9.5 degrees and A320 11.5 degrees with the gears fully compressed.
Joined: Oct 2006
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From: Earth
Soooo how's that bit of information going to help one prevent a tail strike? Seems more of a gotcha type question than anything to me.
Joined: Mar 2001
Posts: 4,563
Likes: 35
From: I wouldn't know.
Know how to rotate? Rotation rate as the main culprit for many. That said, having flown A321s in a previous company, it was actually not the A321 which had the highest tail strike risk, it was the A320. Most pilots were really aware that an A321 is a bit longer than the A320, but they often rotated the A320 like an A319.
It is less about knowing an exact figure, it is more knowing how to fly and adjust your flying technique according to the variant you're sitting in. Even more so if flying several types at once of course.
It is less about knowing an exact figure, it is more knowing how to fly and adjust your flying technique according to the variant you're sitting in. Even more so if flying several types at once of course.

Joined: Jul 2006
Posts: 1,100
Likes: 111
From: Somewhere over the rainbow
Same as Denti. Rotation technique is the key to avoid tailstrike during take off.
Saying that on the NEOs, they added up a rotation mode which helps to prevent the tail strike during take off.
Saying that on the NEOs, they added up a rotation mode which helps to prevent the tail strike during take off.







