Embraer EMB-505 Phenom Service Manual page 191

CAUTION: • ABORT THE DRY MOTORING CYCLE IF YOU SEE THAT
• FOR ENGINE GROUND-RUN PROCEDURES, OBEY THE
(2) Set the ENG START/STOP switch to RUN and momentarily set it to
START.
(3) After the engine stabilizes at idle speed, monitor the engine parameters
(ITT, oil pressure and temperature, N2, and fuel flow) on the EICAS. Make
sure that the N2 indication increases and the fuel flow indication stays at
ZERO.
D. Job Close-Up
(1) On the FUEL control panel, set the DC PUMP 1 or 2 switch to AUTO.
(2) On the ELECTRICAL and on the ICE PROTECTION control panels, set
the switches as applicable.
(3) Set the ENG START/STOP 1 or 2 switch to STOP.
(4) If applicable, remove the circuit breaker ring and tag from each of these
circuit breakers, and close them:
• TEMP PWR 1-LHCBP (DC BUS 1 AIR COND/PRESN)
• TEMP PWR 2-RHCBP (DC BUS 2 AIR COND PRESN)
• VOICE/DATA RECORDER-RHCBP (EMERGENCY BUS)
• E1 FIREX-LHCBP (HOT BATT BUS 1)
• E2 FIREX-RHCBP (HOT BATT BUS 2)
(5) On the FIRE/ENG/TRIM control panel, lift the guard and push the SHUT-
OFF 1 and SHUTOFF 2 push buttons again to open the fuel shutoff
valves.
(6) On the HYD PUMP control panel, set the SOV 1 and SOV 2 switches to
the CLOSED position.
(7) On the HYD PUMP control panel, set the SOV 1 and SOV 2 switches to
the OPEN position.
(8) De-energize the aircraft (GHSH TASK 24-41-00-860-802-A)
(9) Remove from the work area all tools, equipment, and materials that you
used.
EFFECTIVITY: ALL
Copyright © by EMBRAER S.A - All rights reserved - See title page for details.
THE N2 DOES NOT INCREASE OR THERE IS NO OIL
PRESSURE INDICATION.
POWERPLANT OPERATING LIMITATIONS. THIS IS TO
PREVENT DAMAGE TO THE EQUIPMENT.
GROUND HANDLING AND
SERVICING HANDBOOK
71-00-01-910-803-A/200
Page 203/204
Rev.01 - MAY 28/10