W DOC AIRBUS | AMM A320F

HOT EXHAUST - DESCRIPTION AND OPERATION


** ON A/C NOT FOR ALL
1. General
The hot exhaust consists of a center body and a conical primary nozzle.
The nozzle directs the primary exhaust gas aft and regulates the gas stream flow.
A. Core Nozzle (or Primary Nozzle)
(1) Description
F Core Nozzle/Centerbody ** ON A/C NOT FOR ALL
The primary nozzle is composed of:
  • a forward flange for attachement to the engine outer primary exhaust frame (A6 flange) with 16 bolts,
  • a conventional stiffened sheet metal inner and outer skin,
  • and a forward bulkhead. A spring seal is attached to the outer barrel which interfaces with the pylon. The outer barrels are of skin and frame construction.
    The primary nozzle structural assembly is a riveted conventional sheet metal structure.
B. Centerbody
(1) Description
F Core Nozzle/Centerbody ** ON A/C NOT FOR ALL
The centerbody is composed of:
  • a forward flange for attachment to the engine inner primary exhaust frame (A7 flange) with 16 bolts and,
  • a stiffened sheet metal formed section with an open aft end for the engine center vent system.
[Rev.10 from 2021] 2026.04.01 12:57:18 UTC