W DOC AIRBUS | AMM A320F

TRAILING EDGE AND TRAILING EDGE DEVICES - DESCRIPTION AND OPERATION

** ON A/C NOT FOR ALL
1. General
F Trailing Edge and Trailing Edge Devices ** ON A/C NOT FOR ALL
F Trailing Edge and Trailing Edge Devices ** ON A/C NOT FOR ALL
The trailing edge is aft of the rear spar of the wing box, between the wing root and the wing tip. The trailing edge has a fixed structure and eight movable control surfaces.
** ON A/C NOT FOR ALL
2. Component Location
The fixed structure (Ref. AMM D/O 57-51-00-00) is between RIB1 and RIB27. It has attachments for the movable control surfaces and their drive mechanisms. The control surfaces are:
** ON A/C NOT FOR ALL
3. Description
A. Trailing Edge Structure

The main components of the trailing edge structure are:
  • the overwing and underwing panels
  • the fixed shroud and shroud box
  • the rear false spar.
The fixed structure also has attachments for the:
B. Trailing Edge Devices

There are eight trailing edge devices which are movable control surfaces. They are:
The inboard flap and the outboard flap are of the fowler type. Each flap is attached to two carriages. There is an interconnecting strut between the flaps (Ref. AMM D/O 27-51-00-00).

There are eight trailing edge devices which are movable control surfaces. They are:
  • the inboard (double-slotted) flap
  • the outboard (double-slotted) flap
  • the aileron
  • the spoilers 1 thru 5.

    The trailing edge devices are connected to brackets installed on the fixed structure. The inboard and outboard flaps are a 'double-slotted' type, with in-set tabs to increase the control surface area. The flaps are connected together by an interconnecting strut and a 'Z' coupling.
[Rev.10 from 2021] 2026.04.02 07:27:29 UTC
"WTRUIB" 2025