Daher-Socata TBM 900 Pilot's Information Manual page 516

PILOT'S OPERATING HANDBOOK
Information hereafter supplement or replace those of the standard airplane described in Section 7 "Description" of
the basic Pilot's Operating Handbook when the airplane is equipped with the option "ENGINE FIRE DETECTION
SYSTEM".
The engine fire detection system enables the monitoring and indication of a fire in the engine area.
The system includes :
- 7 detectors
- the test push-button
- the G1000 system.
DETECTORS
The 7 detectors are secured on supports positioned in the most sensitive engine areas. They consist of thermal
switches detecting a temperature greater than 200°C.
PUSH-BUTTON
The push-button enables the pilot to test the detection system by opening the grounding circuit. It is connected in
series with the 7 detectors. The push-button is located on the L.H. side instrument panel near the "FIRE TEST"
indication.
DISPLAY
Refer to the "GARMIN" G1000 Integrated Flight Deck Cockpit Reference Guide for the Socata TBM 850,
No. 190-00708-05, at its latest revision.
HANDLING, SERVICING AND MAINTENANCE
Installation and operation of "ENGINE FIRE DETECTION SYSTEM" do not change the basic handling, servicing
and maintenance procedures of the airplane described in Section 8 "Handling, Servicing and Maintenance" of the
basic Pilot's Operating Handbook.
Edition 1 -- October 31, 2013
Rev. 0
ENGINE FIRE DETECTION SYSTEM
SECTION 7
DESCRIPTION
SECTION 8
SUPPLEMENT 18
Page 9.18.7