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emergency bus circuit breakers on each cockpit CB panel when the battery switch is in the EMER
position. If the battery switch is in the BATT position, generator power is supplied through the battery
relay to the battery bus to charge the battery and from the crossfeed bus through the emergency
relay to the emergency power buses. With the battery switch in the EMER position, both generators
OFF, and both engines running, power should be supplied to the following equipment:
Power is available for these items for at least 30 minutes from a normally charged battery. Some
indications are only operational for one side because some supporting equipment is not powered in
EMER. If an engine is not running, the N1, N2 and ITT for that engine will be inoperative (red ‘X’)
since the FADEC is only powered by the engine driven PMA while in EMER. The standby
instruments are powered by a separate standby battery.
A BATTERY DISCONNECT guarded switch, located above the pilot’s armrest, disconnects the
battery in the event that a start or battery relay fail to open when required. This switch provides a
direct loop from the power to the ground side of the battery to open the battery disconnect relay if the
battery switch is in the BATT (not EMER or OFF) position and the battery disconnect switch is
selected to DISCONNECT. When the battery disconnect relay is open, the battery ground is opened
and the battery cannot supply electrical power to the airplane or be charged by the generators.
(Continued Next Page)
• PFD 1 - Reversion Mode
• COM 1
• NAV 1 including Marker Beacon
• GPS 1
• ADC 1
• AHRS 1
• Transponder 1 (XPDR1)
• Pilot’s and Copilot’s Audio Panels
• L and R N1, N2, and ITT Indications
• L Oil Temperature
• L Fuel Flow
• Fuel Temperature
• Battery Voltage Indication
• AFCS Control Panel and Flight Director
(no AP or YD)
• Cabin Altitude and Differential Pressure
Indications
• Cabin Dump System
• Cockpit Flood Light
• Pilot’s Pitot-Static Heat
• Landing Gear Indicator Lights
• Avionics Audio Warnings
• Standby Instruments (Airspeed, Altitude,
and Attitude powered by the Standby
Battery)
• Magnetic Compass Lighting
• ELT GPS Position Interface
510FM-07 AD 3-161
SECTION III - OPERATING PROCEDURES MODEL 510
NORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
ELECTRICAL SYSTEM (Continued)
CAUTION
Do not use the battery disconnect switch for extended time. The battery
disconnect relay will continue to draw a small current from the battery until the
battery is discharged. The battery disconnect relay will then close resulting in a
very high charge rate and probable overheat.
Loss of a single generator is annunciated by an amber GEN OFF L or R message and steady
MASTER CAUTION light. Failure of the second generator is annunciated by a red GEN OFF L-R
message and a flashing MASTER WARNING light.
GROUND POWER
Ground power is supplied from the ground power receptacle on the right side of the tailcone. When
using ground power for prolonged ground operation, the battery should be disconnected to preclude
overheating the battery. Do not use the battery disconnect switch. Ground power can be used for
engine start by selecting the generator switches to OFF. When the starter is engaged, the battery
disconnect relay opens and all start current will be supplied by the ground power unit. The ground
power unit voltage should be 28 to 29 volts and it should have a capacity of 800 to 1100 amperes if
being used to start engines. An over-voltage sensor will open the ground power relay should voltage
exceed limits. If the ground power unit has a variable automatic over current feature, it should be set
to 1100 amps.
CAUTION
If the battery is charged using the ground power unit, it must be visually
monitored. Current from most ground power units is not regulated and a
battery overheat may occur.
ENGINE STARTS
The first engine start will be accomplished from the battery unless ground power is used. The second
start can be accomplished with ground power, (if the first generator switch is OFF); from the battery,
(if the first generator switch is off and ground power is not connected); or from the battery with assist
from the first generator (ground only) if the first generator is on. Generator assist start capability is
disabled in flight; therefore, all starter assist airstarts are from the battery.
CAUTION
If automatic ignition does not occur during start and the ignition circuit breakers
　
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本文鏈接地址：Citation Mustang airplane flight manual 1(111)