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Cessna Citation 550/551 Training Resources |
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Annunciator
Quiz |
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Generic
550 Systems Quiz |
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Standard Operating Procedure Calls |
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| Weight and Balance Spreadsheet for PDA (Excel File) | ||
Unit
Numbers 2 through 505
The selected inverter has failed.
550 and on:
AC Bus Failure,
One or both inverters have failed.
Triggers MASTER WARNING index
Steady Illumination: Battery temp has reached 145 degrees F.
Flashing indicated the battery has reached a temperature of 165 degrees F.
Triggers MASTER WARNING index
Cabin pressure is above 10,000 Feet
Triggers MASTER WARNING index
Oil pressure is below 35 PSI in the left or right engine.
Triggers MASTER WARNING index
Fuel quantity according to the float switch is between
169 and 219 pounds
useable in the indicated tank. index
Fuel pressure is low. index
Left or right hydraulic pump output is below normal.
Unit numbers 2 through 436 indicate "L/R HYD PRESS LOW". index
Either of the following:
1. Throttle is below the 60% N2 position
2. Nacelle Inlet Temp is below 104 degrees C
3. Engine Stator Anti-Ice Vale is not fully open
4. Failure of automatic temperature controller (light modulates on and
off)
5. Failure of wing leading edge to stay within range (one or more heating
elements inop.)
6. Wing leading edge temperature below 16 degrees C index
Indicates proper boot inflation pressure.
Illuminates twice during the 12 second
cycle. index
Generator power relay is open.
Illumination of both LH and RH triggers the
MASTER WARNING. index
Either the #1 or the #2 inverter has failed.
Illumination of either LH or RH
lights triggers the AC Fail
Annunciator, which in turn triggers the MASTER WARNING. index
Emergency pressurization has been manually selected, or the ACM has overheated.
During ACM overheat, if the ACM cools down with 12 seconds, it will revert to
normal
operation. During overheat on the Ground, the emergency pressurization valve
does
not open (de-activated by squat switch) but the light illuminates. index
Pressurization source selector is in the GNP position and the Ground Valve is
open. index
Brake hydraulic pressure is low. Anti Skid Inop will also illuminate. index
Filter bypassing of the indicated filter is impending or occurring. index
With fuel boost pump switch in the NORM position, this illuminates with the
Annunciator.
FUEL BOOST ON also illuminates with the switch in the ON Position. Automatically
illuminates with the switch in the
normal position during engine start, and crossfeeding. index
Fluid level is below .2 gallons. index
System is pressurized. On when T/R's are deployed, and when gear or speed brakes
are cycling. index
Pitot static heater is off, or with the switch on, power has been disconnected
from the pitot tube heater,
or one or both static port heaters. index
Left and right speed brakes are fully extended. index
Temp in the duct from the ACM to the cabin is excessively high temperature. index
Unit numbers 482, 485 and on... The ground valve has closed because
the secondary overpressure switch has activated. Normal DC power must be removed
to reset. index
Control switch is off, the unit is is test mode, or the Anti Skid Unit is
inoperative.
This Annunciator is off with the gear handle in the UP position. index
Indicates that either nose baggage door tailcone compartment door, or
main cabin door is not locked. index
The fuel and hydraulic shutoff valves are fully closed. They can be re-opened by
pressing the ENG FIRE switch a second time. index
1- With the control switch in either position, bleed air to the windshield
exceeds 146 degrees C. 2- With the control switch off it indicates that
the shutoff valve
has failed open, or is leaking bleed air, allowing line pressure to exceed 5 psi.
index
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