► Continuing
Table 7.9.2 - Breaker Panel (Typical arrangement)
ENGINE AIRFRAME 2 Powerplant cont. protection: Ng, flowmeter & ITT
FUEL GAGE 1 Left-side fuel gauge protection
FUEL GAGE 2 Right-side fuel gauge protection
F
ADEC CH. A FADEC channel A protection
ESS BUS 2
ESS BUS 2 Essential bus 2 circuit protection
PASS MASKS Passengers' oxygen masks protection
STBY INSTR Standby Attitude Module (MD302) protection
AUDIO Audio control panel protection
TOUCH CTRL 1 Touchscreen controller 1 protection
XPDR 1 Transponder 1 protection
AHRS 1 Attitude and Heading Reference System 1 protection
LDG SIG Landing gear indicating system protection
CPCS PWR1
Cabin Pressurization Control System power supply 1
protection
CAB BLEED Cabin bleed air system protection
IGNITION Powerplant ignition protection
BUS 1
AP CTRL Flight controller protection
PFD 2 Primary Flight Display 2 protection
COM 2 VHF 2 & radio protection
GPS/NAV 2 GPS NAV 2 protection
ADC 2 Air Data Computer 2 protection
XPDR 2 Transponder 2, if installed protection
VDL
Controller-Pilot Data Link Communications system, if
installed protection
AIRFRAME DE ICE Empennage and wing leading edges deicing
INERT DE ICE Inertial separator protection
Continue ►
Section 7
Description
Pilot's Information Manual
PIM TBM 960 - Edition 0
Rev. 02
Page 7.9.9
PIM - DO NOT USE FOR FLIGHT OPERATIONS
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