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Lower aft pylon fairing for engine mounting structure inserted between wing and turbojet engine of aircraft, has extension traversing inner cross stiffening rib and fixed on spar, where extension and bracket are formed as single piece
Lower aft pylon fairing for engine mounting structure inserted between wing and turbojet engine of aircraft, has extension traversing inner cross stiffening rib and fixed on spar, where extension and bracket are formed as single piece
The fairing (30) has an anchoring unit including an attachment (60) permitting withdrawal of efforts along a longitudinal direction, where the fairing is in the form of caisson. The attachment has a bracket (62) that is fixed and is plated against a face of an inner cross stiffening rib (46). The attachment has a triangular bracket extension (70) that extends along the longitudinal direction. The extension and the bracket are formed as a single piece. The extension traverses the inner cross stiffening rib, and is fixed on a closing spar (41).
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