A319 One Wing tip fence operation
Thread Starter
Join Date: Dec 2007
Location: Here.
Posts: 15
Likes: 0
Received 0 Likes
on
0 Posts
A319 One Wing tip fence operation
Hello all,
Id like to know if after removing completely in an A319 one wing tip fence , the penalty for take off and landing .
If theres penalty , to which data ive to substract , to the Maximum Structural TOW ?
How is affecting one winglet operation in an engine failure?
If there any Airbus support or reference we can check personally ?
Does anybody has the CDL for A319 , not for the 320 family?
Thank you.
Id like to know if after removing completely in an A319 one wing tip fence , the penalty for take off and landing .
If theres penalty , to which data ive to substract , to the Maximum Structural TOW ?
How is affecting one winglet operation in an engine failure?
If there any Airbus support or reference we can check personally ?
Does anybody has the CDL for A319 , not for the 320 family?
Thank you.
Join Date: Mar 2000
Location: Sunrise Senior Living
Posts: 1,338
Likes: 0
Received 0 Likes
on
0 Posts
From A319 CFM CDL 57-01 Wing Tip Fence
One may be missing provided exposed interior structure is covered, protective material is inspected before each flight and replaced if necessary.
Performance:
Take off and approach climb limiting weights are reduced by 10080kg (22223lbs)
En route performance limiting weight is reduced by 756kg (1667lbs)
Fuel consumption is increased by 1.69%
Caveat emptor!
mcdhu
One may be missing provided exposed interior structure is covered, protective material is inspected before each flight and replaced if necessary.
Performance:
Take off and approach climb limiting weights are reduced by 10080kg (22223lbs)
En route performance limiting weight is reduced by 756kg (1667lbs)
Fuel consumption is increased by 1.69%
Caveat emptor!
mcdhu
Join Date: Jun 2001
Location: UK
Posts: 114
Likes: 0
Received 0 Likes
on
0 Posts
A319 One Wing tip fence operation
For one fence removed on a 319
Takeoff and approach climb performance limiting weights are reduced by 10 080 kg (22 223 lb)
En-route performance limiting weight is reduced by 756 kg (1 667 lb)
Fuel consumption is increased by 1.69 %.
Sorry we crossed
Takeoff and approach climb performance limiting weights are reduced by 10 080 kg (22 223 lb)
En-route performance limiting weight is reduced by 756 kg (1 667 lb)
Fuel consumption is increased by 1.69 %.
Sorry we crossed
Thread Starter
Join Date: Dec 2007
Location: Here.
Posts: 15
Likes: 0
Received 0 Likes
on
0 Posts
Take off and climb performance
When you say limiting with 10.000 kgs less , to which data we have to substract ,to the general rtow A320 family ,to the MTOW A 319 (lets say 64500 kgs ), or an especific RTOW for the A319 to an especific runway?
Whats the reason for such reduction , engine failure? ,estructural stress? ..
Whats the reason for such reduction , engine failure? ,estructural stress? ..
Drag increase and subsequent performance decrease.....
Whatever your performance limited TOW is on the day for your flight no matter what method your company uses you have to then reduce that by 10,080 kg.
In ours we simply input the CDL code into our ACARS TO PERF calculations and it takes care of the calculations/corrections/penalties and gives me the figures.
PERF Limited TOW, FLEX, CONFIG, VMCG, V1 VR V2 etc etc
Whatever your performance limited TOW is on the day for your flight no matter what method your company uses you have to then reduce that by 10,080 kg.
In ours we simply input the CDL code into our ACARS TO PERF calculations and it takes care of the calculations/corrections/penalties and gives me the figures.
PERF Limited TOW, FLEX, CONFIG, VMCG, V1 VR V2 etc etc
Last edited by ACMS; 21st Jul 2015 at 10:51.
