190-01717-B1
G500/G600 TXi Part 23 AML STC Maintenance Manual
Rev. 1
Page 5-31
5.12 EIS Sensors
In addition to the data in this manual, replacement or re-installation of each probe/sensor and wire must be
accomplished in accordance with the sensor manufacturer instructions, or as recommended by the engine
manufacturer. Wire routing and clamping must follow procedures defined in aircraft maintenance manual,
standard practices manual, or practices defined in Chapter 11,
Electrical Systems
of advisory circular AC
43.13-1B,
Aircraft Inspection and Repair
.
Sensors must be connected using hoses and fittings approved as part of aircraft or engine type certificated
design, or standard aircraft parts (AN/MS).
After removing or replacing any EIS sensor perform the EIS ground checkout procedure for the specific
sensor that was affected in Section 6.5 of the G500/G600 TXi Part 23 AML STC Installation Manual (P/N:
190-01717-B3)
CAUTION
Check hose routing for sharp bends. Check sensors and fittings for leaks during engine
run-up and correct prior to flight.
