background
x
loader
system description
arrow By ATA By Message Color By Observed Faults By CAIMS By Tips

Select color for CAS message that you wish to troubleshoot

(WARNING)
RED MESSAGE
(CAUTION)
AMBER MESSAGE
(ADVISORY)
CYAN MESSAGE
(STATUS)
WHITE MESSAGE
Require immediate crew attention. These messages are accompanied by flashing master warning, triple chime attenson with or without voice message or dedicated tone. Require immediate crew awareness and future crew action may be required in the form of alternate system selection or performance limitation. These message are accompanied by flashing master caution and a single chime. Indicate safe or normal system operation which require crew awareness, over and above the dark cockpit philosophy. Indicate minor failures or reduction in systems capability, which require no crew action.

This page includes :

     

For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

Overview

The function of the collector/nozzle is to mix the turbine exhaust with the bypass air. The cone assembly gives a smooth flow from the turbine and controls the mixer area.

The hot turbine gases and the bypass air become one air flow in the area between the exhaust unit and the exhaust cone. The turbine gases and the bypass air flow through lobes on the exhaust nozzle and mix. The result of this mixture of gases and air is a decrease of gas mixture velocity and a decrease in noise.


Exhaust Nozzle

The exhaust nozzle is a cylindrical shape with open ends. It has a flange around the forward edge and lobes around the circumference which decrease in depth to the forward edge. This flange attaches to the rear of the low pressure (LP) turbine exhaust case with bolts.

The exhaust mixer provides forced mixing of hot core gases and cold bypass air. This reduces the overall temperature of the engine exhaust to atmosphere increasing efficiency and reducing the noise signature of the engine.


06/02/16

Exhaust Cone

The front and rear cone forms a divergent duct (with the inner profile of the exhaust unit) and provides a smooth contour for the engine exhaust behind the turbine.

Front Cone

The front cone is a cylindrical structure with a flange at the forward and rear edges. The forward flange has bolt holes and the rear flange has captive nuts. The forward flange attaches to the rear of the LP turbine exhaust case with bolts.

Rear Cone

The rear cone has a round end and an internal flange around the front edge. Holes in the front flange align with the captive nuts on rear flange of the front cone. Access to the holes is through the outer surface of the cone. The rear cone attaches to the rear flange of the front cone with bolts.


09/22/20

Component Location Index

Component Location Index
IDENT DESCRIPTION LOCATION EMM REF 
     - EXHAUST NOZZLE ZONE(S) 430/440 78-10-01
     - EXHAUST CONE ZONE(S) 430/440 78-10-02


Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.