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CE-650 FSI GS > RKA - Annunciators > Flashcards

RKA - Annunciators Flashcards

1
Q

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

A

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

  1. Amperage…. Check
  2. Battery Disconnect Switch ….. Portion to overheated battery
  3. Average…… Note Decrease

Single Battery:

  1. Battery Switch….. OFF
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2
Q

EMERG
Decent MODE

or

EMER
Descent

Memory Item

Emergency Descent

A

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

  1. Throttles……. Idle
  2. Speedbrakes / spoilers…….. deploy
  3. Initial Pitch Attitude…….20 deg down
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3
Q

OIL PRESS
WARN
LH RH

A

Oil Pressure Warning

Oil pressure is less than 25 psi. illumination of the annunciator triggers the MASTER WARNING RESET switch lights.

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4
Q

PRI
TRIM
FAIL

or

PRI TRIM
FAIL

Memory Item:

Pitch Trim Runaway OR Failures

A

Primary Trim Fail

Primary trim control or trim actuator is inoperative. Triggers MASTER WARNING RESET switchlights

Memory Item:

  1. AP/TRIM/NWS Disengage switch … Press and hold
  2. Secondary Trim switch …… ON (lift guarded cover)
  3. Trim……. As Required (SEC TRIM FAULT Light may be illuminated until the secondary trim is actuated)
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5
Q

SMOKE DETECT

Memory Item

Cockpit or Cabin Fire / Smoke Detect Light On

A

Smoke is detected in the aft cabin area. Triggers Master Warning Reset Switchlights

Memory Item

  1. Oxygen Masks ….. Don and Emergency
  2. Smoke Googles … Don, as required
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6
Q

W/S OVHT

W/S
O’Heat
LH RH

A

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

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7
Q

DOOR Unlocked
ACC

ACC Door Unlocked
NOSE BAG

A

Access Door Unlocked

Left nose equipment door, baggage compartment door, toilet service door, and/or single point pressure refueling door is not locked.

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8
Q

Aft
J-Box
LMT CB

A

Aft Junction Box

A current limiter or circuit breaker in the aft power junction box is open.

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9
Q

AIL BOOST
OFF

A

Aileron boost pressure

The aileron boos pressure has been lost.

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10
Q

ANTI
SKID

A

Anti Skid

Indicates failure of the anti skid system or the antacid switch is off.

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11
Q

AUX HTR
O’HEAT

A

Cockpit Auxiliary Electric Heater Overheat

The cockpit electric auxiliary heater has overheated and has shutdown.

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12
Q

BAG HTR
O’Heat

A

Baggage Compartment Heater Overheat

The baggage compartment heater has overheated.

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13
Q

Cabin
Alt
8500 FT

or

CABIN ALT
8500 FT

A

Cabin Altitude

Cabin Altitude is greater than 8,500 feet

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14
Q

DOOR UNLOCKED
CAB

or

CAB DOOR
UNLOCKED

A

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

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15
Q

DOOR SEAL

A

Door Seal

Indicates a loss of bleed air pressure to the primary cabin door seal.

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16
Q

Duct
O’HEAT
CKPT CAB

or

DUCT
O’HEAT

A

Duct Overheat

Temperature in the cockpit or cabin duct is excessive.

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17
Q

EMERG
PRESS ON
LH RH

A

Emergency Pressurization

Emergency pressurization is turned on by either the 13,500 barometric switch or by the ENG BLD AIR switch.

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18
Q

ENG
ANTI-ICE
LH RH

A

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.

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19
Q

FIRE DET
FAIL
LH RH

A

Fire Detection system Fail

indicates a failure in the fire detection system

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20
Q

Fire EXT
BOTTLE LOW

or

FIRE EXT
BOTL LOW

A

Fire Exit Bottle Low

Pressure switches indicate low pressure in one or both of the engine fire extinguishers bottles.

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21
Q

FUEL
BOOST ON
LH RH

A

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

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22
Q

FUEL COMP
MANUAL
LH RH

A

Fuel Control Computer Manual

The fuel control computer has failed and/or been switched to manual control

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23
Q

FUEL FLTR
BYPASS
LH RH

A

Fuel filters are approaching or are actually being bypassed because of filter contamination.

24
Q

FUEL F/W
SHUTOFF
LH RH

A

Fuel Firewall Shutoff

the fuel firewall shutoff valve is closed by the LH or RH ENG FIRE PUSH switchlight.

25
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
26
FUEL LOW PRESS LH RH
Fuel Pressure Low indicates the fuel pressure has been actuated by low fuel pressure.
27
FUS TANK VIL VLV or FUS TANK FILL VLV
Fuselage Tank Fill Valve the fuselage tank fill valve is not fully closed.
28
FUS TANK FUEL PUMP 1. 2
Fuselage Tank Fuel Pump Fuselage tank fuel pumps are being powered
29
FUS TANK LOW or FUS TANK LOW
Fuselage Tank Low indicates the fuselage tank fuel quantity is low
30
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
31
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.
32
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.
33
GUST LOCK
Gust Lock The control surface and throttle lock are not fully disengaged
34
HP PRECLR O'HEAT LH. RH
High Pressure Preschooler Overheat High pressure bleed air from the pre cooler has exceeded 550F
35
HYD F/W SHUTOFF LH. RH
Hydraulic Firewall Shutoff hydraulic firewall shutoff valves are closed by the LH or RH ENG FIRE PUSH swithclight
36
HYD PRESS LOW LH. RH
Hydraulic Pressure Low Hydraulic pressures switches indicate low pressure output from the engine-driven pumps
37
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
38
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.
39
ISO VALVE OPEN
Isolation Valve - Open the isolation valve between the cockpit and cabin environmental control unit is open
40
No Takeoff
No Takeoff Improper takeoff configuration - Spoilers - Speedbrakes - Flaps - Stabilizer Trim - Gust Lock - APU On, if ground only - Unlocked door
41
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.
42
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
43
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
44
PAC O'HEAT CKPT. CAB
PAC Overheat The environmental control unit disable because of an overt condition in the compressor or turbine
45
PARK BRAKE
Parking Brake The parking brake is not fully disengaged.
46
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.
47
Rudder Bias
Rudder Bias The solenoid bypass valve is open, reducing the effectiveness of the rudder assist cylinder
48
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.
49
SPEED BRAKE
Speed Brake The middle two spoiler segment son each wing are not fully stowed
50
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.
51
SPOLIERS UP
Spoilers UP The inboard spoiler segments are not fully stowed.
52
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.
53
STALL WARN
Stall Warning indicates the stall warning system is inoperative
54
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.
55
WING FUEL XFER OPEN
Wing fuel transfer valve - open The wing fuel transfer valve is energized open
56
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.
57
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.

CE-650 FSI GS (32 decks)

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