W DOC AIRBUS | AMM A320F

FORWARD MOUNT - DESCRIPTION AND OPERATION


** ON A/C NOT FOR ALL
1. Description
F Forward Engine Mount ** ON A/C NOT FOR ALL
The forward mount connects the engine aft fan case with the engine pylon forward structure. The forward mount is a damage tolerant design.
It consists of :
  • the support beam assembly : for pylon connection via 4 tension bolts and 2 alignment pins.
    This fail-safe designed fitting is an assembly of 3 components : 2 half-fittings and 1 plate.
  • one bearing fitted on the support beam assembly which carries y and z loads. The outer cage is axially free in the engine aft fan frame aperture and therefore carries no x loads. In case of lateral link failure, the bearing partially carries the x loads.
  • one link/beam/bracket assembly which carries the x thrust loads. The beam is hinged to the main bracket at its center.
    A link is installed at each end of the beam.
    A bracket attached to the engine casing supports the front of the link.
    The link ends have bearings.
** ON A/C NOT FOR ALL
2. Material
The forward engine mount beam is machined from an Inconel 718 forging. The crossbeam, links and engine attach brackets are machined from 6-4 Titanium.
[Rev.10 from 2021] 2026.04.02 06:32:19 UTC