W DOC AIRBUS | AMM A320F

MOUNTS - DESCRIPTION AND OPERATION


** ON A/C NOT FOR ALL
1. General
F Mounts ** ON A/C NOT FOR ALL
F Engine Mount Loads ** ON A/C NOT FOR ALL
The engine/pylon connection is achieved by means of a two-mount system:
  • the forward mount: it is attached to the engine via the intermediate casing. It takes the X loads (thrust), Y loads (lateral) and Z loads (vertical),
  • the aft mount: it is attached to the engine via the exhaust casing. It takes the loads in a plane normal to the engine centerline i.e.: Y loads (lateral), Z loads (vertical) and Mx (engine rotational inertia moment + Y load transfer moment).
The engine mounts support the engine by transmitting loads from the engine case to the pylon structure.
They allow for thermal expansion of the engine without inducing additional load into the mount system.
Engine mount bolts locking is achieved as follows:
  • Engine/nacelle interface: mechanical locking
  • Nacelle/pylon: wirelocking (each screw has an independent lockwire or safety cable).
    Each engine mount design provides dual load paths to ensure safe operation if one member fail.
[Rev.10 from 2021] 2026.04.01 12:54:31 UTC