RKA - Annunciators Flashcards
Batt
O’Temp
1 2
Memory Item:
Battery Overheat (Batt O’Temp Light On)
Dual Battery installation only
Battery Overheat (Batt O’Temp Light On)
Single Battery installation only
Battery Overtemperature
Flashes when battery temperature exceeds 71C or when Bat TEMP is selected by the TEST knob.
Steady illumination indicates the battery temperatures is between 60C and 71C.
Triggers MASTER WARNING RESEST switch lights.
Memory Item:
Dual Battery
- Amperage…. Check
- Battery Disconnect Switch ….. Portion to overheated battery
- Average…… Note Decrease
Single Battery:
- Battery Switch….. OFF
EMERG
Decent MODE
or
EMER
Descent
Memory Item
Emergency Descent
Emergency Descent Mode
Automatic Emergency descent is initiated by the autopilot, if engaged, and the aircraft is above 34,275 feet with cabin altitude above 13,500 feet. Triggers MASTER WARNING RESET switchlights
Memory Item:
Emergency Descent
- Throttles……. Idle
- Speedbrakes / spoilers…….. deploy
- Initial Pitch Attitude…….20 deg down
OIL PRESS
WARN
LH RH
Oil Pressure Warning
Oil pressure is less than 25 psi. illumination of the annunciator triggers the MASTER WARNING RESET switch lights.
PRI
TRIM
FAIL
or
PRI TRIM
FAIL
Memory Item:
Pitch Trim Runaway OR Failures
Primary Trim Fail
Primary trim control or trim actuator is inoperative. Triggers MASTER WARNING RESET switchlights
Memory Item:
- AP/TRIM/NWS Disengage switch … Press and hold
- Secondary Trim switch …… ON (lift guarded cover)
- Trim……. As Required (SEC TRIM FAULT Light may be illuminated until the secondary trim is actuated)
SMOKE DETECT
Memory Item
Cockpit or Cabin Fire / Smoke Detect Light On
Smoke is detected in the aft cabin area. Triggers Master Warning Reset Switchlights
Memory Item
- Oxygen Masks ….. Don and Emergency
- Smoke Googles … Don, as required
W/S OVHT
W/S
O’Heat
LH RH
Windshield Bleed Air Overheat
Indicates a duct temperature of 294F or higher if the Aiplane is in Flight or on the ground with either or both throttles below 75% N1 and a duct temperature of 220F
DOOR Unlocked
ACC
ACC Door Unlocked
NOSE BAG
Access Door Unlocked
Left nose equipment door, baggage compartment door, toilet service door, and/or single point pressure refueling door is not locked.
Aft
J-Box
LMT CB
Aft Junction Box
A current limiter or circuit breaker in the aft power junction box is open.
AIL BOOST
OFF
Aileron boost pressure
The aileron boos pressure has been lost.
ANTI
SKID
Anti Skid
Indicates failure of the anti skid system or the antacid switch is off.
AUX HTR
O’HEAT
Cockpit Auxiliary Electric Heater Overheat
The cockpit electric auxiliary heater has overheated and has shutdown.
BAG HTR
O’Heat
Baggage Compartment Heater Overheat
The baggage compartment heater has overheated.
Cabin
Alt
8500 FT
or
CABIN ALT
8500 FT
Cabin Altitude
Cabin Altitude is greater than 8,500 feet
DOOR UNLOCKED
CAB
or
CAB DOOR
UNLOCKED
Cabin Door Unlocked
a. On steady in flight or flashing on ground indicates one of the four door pin switches or the handle is not in the locked position.
b. Citation III/VI - steady on the ground, door is open
DOOR SEAL
Door Seal
Indicates a loss of bleed air pressure to the primary cabin door seal.
Duct
O’HEAT
CKPT CAB
or
DUCT
O’HEAT
Duct Overheat
Temperature in the cockpit or cabin duct is excessive.
EMERG
PRESS ON
LH RH
Emergency Pressurization
Emergency pressurization is turned on by either the 13,500 barometric switch or by the ENG BLD AIR switch.
ENG
ANTI-ICE
LH RH
Engine Ani-Ice
Engine inlet anti-ice protection system is inoperative because of loss of power, inadequate bleed air heat, direct current wing root fairing heater failure or starter/generator inlet unit-ice sensor heater element failure.
FIRE DET
FAIL
LH RH
Fire Detection system Fail
indicates a failure in the fire detection system
Fire EXT
BOTTLE LOW
or
FIRE EXT
BOTL LOW
Fire Exit Bottle Low
Pressure switches indicate low pressure in one or both of the engine fire extinguishers bottles.
FUEL
BOOST ON
LH RH
Fuel boost pump on
the fuel boost pump has been turned on by either the low fuel pressure, fuel boost pump switch, wing fuel transfer has been selected or during engine start
FUEL COMP
MANUAL
LH RH
Fuel Control Computer Manual
The fuel control computer has failed and/or been switched to manual control
FUEL FLTR
BYPASS
LH RH
Fuel filters are approaching or are actually being bypassed because of filter contamination.
FUEL F/W
SHUTOFF
LH RH
Fuel Firewall Shutoff
the fuel firewall shutoff valve is closed by the LH or RH ENG FIRE PUSH switchlight.
FUEL LOW
LEVEL
LH. RH
Fuel Level Low
The amber fuel low heel light indicates the fuel in the wing is less than approximately 350 pounds
FUEL LOW
PRESS
LH RH
Fuel Pressure Low
indicates the fuel pressure has been actuated by low fuel pressure.
FUS TANK
VIL VLV
or
FUS TANK
FILL VLV
Fuselage Tank Fill Valve
the fuselage tank fill valve is not fully closed.
FUS TANK
FUEL PUMP
1. 2
Fuselage Tank Fuel Pump
Fuselage tank fuel pumps are being powered
FUS TANK
LOW
or
FUS TANK
LOW
Fuselage Tank Low
indicates the fuselage tank fuel quantity is low
FUS TANK
XFER FAIL
Fuselage Fuel Transfer Fail
indicates the fuselage fuel transfer system has failed to supply adequate pressure
Failure of either pump will activate light.
Light inhibited for 8 seconds after turning On
GEN
OFF
LH. RH
Generator Power
The light advises of the loss of 28 volt direct current generator power. Loss of both left and right generators triggers the MASTER WARNING RESEST switchlights.
GROUND
IDLE
Ground Idle
indicates the engines are configured for reduced idle. The annunciator should be illuminated for all ground operations. On landing, it should illuminate 8 seconds after touchdown with the switch in NORM.
GUST
LOCK
Gust Lock
The control surface and throttle lock are not fully disengaged
HP PRECLR
O’HEAT
LH. RH
High Pressure Preschooler Overheat
High pressure bleed air from the pre cooler has exceeded 550F
HYD F/W SHUTOFF
LH. RH
Hydraulic Firewall Shutoff
hydraulic firewall shutoff valves are closed by the LH or RH ENG FIRE PUSH swithclight
HYD PRESS
LOW
LH. RH
Hydraulic Pressure Low
Hydraulic pressures switches indicate low pressure output from the engine-driven pumps
HYD VOL
LOW
LH RH
Hydraulic Pressure Low
The fluid level is at or below 150 cube inches as indicated by a mircorswith activated mechanically by the reservoir
Emergency/Abnormal Procedures:
Q1
Hydraulic system failure (HYD VOL LOW and/or both LH and RH HYD Press Low lights on
Inverter
Faile
1. 2
Inverter Fail
The inverter fail light advise that the alternating current inverter voltage or frequency is outside the allowable limits. Loss of both inverters triggers the MASTER WARNING RESET switchlights.
ISO VALVE OPEN
Isolation Valve - Open
the isolation valve between the cockpit and cabin environmental control unit is open
No
Takeoff
No Takeoff
Improper takeoff configuration
- Spoilers
- Speedbrakes
- Flaps
- Stabilizer Trim
- Gust Lock
- APU On, if ground only
- Unlocked door
Oil Chip Detector
LH. RH
Oil Chip Detector
Magnetic contacts have been detected a metal chip in the oil pump discharge back to the oil tank.
PAC HI
Not approved for ?
Prohibited when ?
PAC High
the CKPT PAC and/or CAB PAC switch is positioned to high causing the flow control valve to be in high flow.
- Not approved for takeoff or landing
- Prohibited when using: windshield bleed air, wing anti-ice or engine anti-ice
PAC HP
VLV OPEN
LH. RH
Automatically:
on ground below
in flight below
PAC High Pressure Valve - Open
High Pressure bleed air to the environmental control unit was turned on automatically or manually
Automatically:
on ground below 55% N1
in flight below 75% N1
PAC
O’HEAT
CKPT. CAB
PAC Overheat
The environmental control unit disable because of an overt condition in the compressor or turbine
PARK
BRAKE
Parking Brake
The parking brake is not fully disengaged.
P/S HTR
OFF
LH. RH
Pitot/Static Heater - OFF
Current sensing relays indicate one or more of the pitot or static anti-ice heaters are inoperable or the switch is off.
Rudder
Bias
Rudder Bias
The solenoid bypass valve is open, reducing the effectiveness of the rudder assist cylinder
SEC TRIM
FAULT
Secondary Trim Fault
Secondary trim is on, but the clutch is not engaged (actuation of the trim switches should engage clutch, or secondary trim is turned off by the clutch has not disengaged.
SPEED
BRAKE
Speed Brake
The middle two spoiler segment son each wing are not fully stowed
SPOILER
HOLDOWN
Spoiler Holdown
The hold down return line is pressured, spoilers/speedbrakes cannot be extended. Roll spoilers are operable if auxiliary hydraulic pump is operating.
SPOLIERS
UP
Spoilers UP
The inboard spoiler segments are not fully stowed.
STAB
ANTI-ICE
LH. RH
Stabilizer Ice Protection - OFF
The horizontal stabilizer ice protection system is inoperative because of overheating, loss of power, or heater failure.
STALL
WARN
Stall Warning
indicates the stall warning system is inoperative
Wing
Anti-Ice
LH. RH
Wing Anti-Ice System - OFF
the wing anti-ice system is inoperative because of overheating or inadequate bleed air temperature.
WING FUEL
XFER OPEN
Wing fuel transfer valve - open
The wing fuel transfer valve is energized open
W/S Air
Windshield Air
Depending on the service bulletin, with the system in the use the windshield bleed air temperature is too hot or too cold. with the system off, the light indicates trapped pressure in the air duct.
W/S
FAULT
LH. RH
Windshield Fault
the amber windshield or temperature sensor fault light indicates the electric windshield controller has vailed or a phase imbalance has been detected in the system.
