7.10 - Cabin Air Temperature and Pressurization
NOTE
A list of abbreviations used in this chapter is given in
The airplane is equipped with an Environmental Control System (ECS), which
ensures cabin air temperature and pressurization control – see
-
Cabin Air Temperature corresponds to the cockpit / cabin air flow and
temperature management.
-
Pressurization corresponds to the cabin altitude / rate of change
management.
The ECS is composed of three sub-systems:
-
Engine Bleed Air System (EBAS),
-
Cabin Pressurization Control System (CPCS),
-
Dual-zone Temperature Control System (TCS).
The ECS controls are located on:
-
the PRESSURIZATION and the ECS panels on the right side of the left
control wheel,
-
a touchscreen control panel located above the passenger's table.
The pilot monitors the system through information and CAS messages displayed
in the CAS window. These indications are independent of the ECS controls and
internal sensors.
Section 7
Description
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 02
Page 7.10.1
PIM - DO NOT USE FOR FLIGHT OPERATIONS