AUXILIARY POWER
UNIT (APU)
GENERAL
The APU (Figure 6-1) is mounted on a skid
support assembly enclosed in a fireproof metal
container in the aft equipment bay.
MAJOR SECTIONS
The APU (Figure 6-2) can be divided into six
major sections as follows:
1. Air intake
2. Compressor
3. Combustor
6-2 CL 601-3A/R
CL-600-2B16 PILOT TRAINING MANUAL
Air Intake
The main air inlet to the compressor is located
around the waist of the APU. The air intake is
shrouded and connected by a rectangular duct
to a flush screened inlet (figure 6-3) at the top
of the rear fuselage compartment.
Compressor
The compressor is a single-stage centrifugal
type, which induces air through the intake,
compresses the air, and directs the airflow for
cooling, combustion, and bleed air extraction.
Figure 6-1. APU Installation
FOR TRAINING PURPOSES ONLY
FlightSafety Canada
4. Turbine
5. Exhaust
6. Accessory Gear
L t é e
L t d .