Hello, I' m very sorry , I haven't got scan to send you trim sheet.
I Will try to explain it.
When I compute UI for Hold 1 with Airbus data:
Hold1 Harm = 12.283 m from Airbus Doc
Unit Index = W*(Sta - Ref.Sta)/C This equation compute Index for An item
With
Sta = Harm= 12,283 from Airbus Doc
Ref.Sta = 18,850 from Airbus Doc
C=1000 from Airbus Doc
So Unit Index = 0,0064 for Hold 1
The first come from AirFrance A320-100
Hold 1 ==>1000 kg = ~6,4UI i can deduct For Hold1 0,0064 UI/Kg
there are the same calc for all Hold
The second (Trim sheet) come from NouvelAir
Hold 1 ==>500 kg = ~3,2UI i can deduct For Hold1 0,0064 UI/Kg
The third (Trim sheet) come from XL AirWay
Hold 1 ==> 500kg = ~1,1 UI
I will try to scan the LOADSHEET and i will send it to you
In fact I didn't use trim sheet to make my calcul, but i used electronic Loadsheet create by gaetan (airfrance software) to control my result
the
Unit
Index are compute from My software with airbus data or with reading trim sheet when when I have one
In fact to create one aircraft on my software, I have two opportunity:
Case 1 : I have Doc Airbus ou AHM:
- For Hold I hava Airbus Data.
- For Cabin I use Trim sheet (because earch aircraft have onwer configuration)
Case 2 : I don't have Doc or AHM
- For Cabin and Hold I use trim sheet If I have one
That's why I can treat any aircraft when I have got trimsheet, I study It and I save all informations in my soft
according to you, I found Aircraft manual about Boeing with Arm of Hold, can I use the same equation to compute Unit Index?
best regards