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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
Q

FUEL LOW
LEVEL
LH. RH

A

Fuel Level Low

The amber fuel low heel light indicates the fuel in the wing is less than approximately 350 pounds

26
Q

FUEL LOW
PRESS
LH RH

A

Fuel Pressure Low

indicates the fuel pressure has been actuated by low fuel pressure.

27
Q

FUS TANK
VIL VLV

or

FUS TANK
FILL VLV

A

Fuselage Tank Fill Valve

the fuselage tank fill valve is not fully closed.

28
Q

FUS TANK
FUEL PUMP
1. 2

A

Fuselage Tank Fuel Pump

Fuselage tank fuel pumps are being powered

29
Q

FUS TANK
LOW

or

FUS TANK
LOW

A

Fuselage Tank Low

indicates the fuselage tank fuel quantity is low

30
Q

FUS TANK
XFER FAIL

A

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
Q

GEN
OFF

LH. RH

A

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
Q

GROUND
IDLE

A

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
Q

GUST
LOCK

A

Gust Lock

The control surface and throttle lock are not fully disengaged

34
Q

HP PRECLR
O’HEAT
LH. RH

A

High Pressure Preschooler Overheat

High pressure bleed air from the pre cooler has exceeded 550F

35
Q

HYD F/W SHUTOFF
LH. RH

A

Hydraulic Firewall Shutoff

hydraulic firewall shutoff valves are closed by the LH or RH ENG FIRE PUSH swithclight

36
Q

HYD PRESS
LOW

LH. RH

A

Hydraulic Pressure Low

Hydraulic pressures switches indicate low pressure output from the engine-driven pumps

37
Q

HYD VOL
LOW
LH RH

A

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
Q

Inverter
Faile
1. 2

A

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
Q

ISO VALVE OPEN

A

Isolation Valve - Open

the isolation valve between the cockpit and cabin environmental control unit is open

40
Q

No
Takeoff

A

No Takeoff

Improper takeoff configuration

  • Spoilers
  • Speedbrakes
  • Flaps
  • Stabilizer Trim
  • Gust Lock
  • APU On, if ground only
  • Unlocked door
41
Q

Oil Chip Detector

LH. RH

A

Oil Chip Detector

Magnetic contacts have been detected a metal chip in the oil pump discharge back to the oil tank.

42
Q

PAC HI

Not approved for ?
Prohibited when ?

A

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
Q

PAC HP
VLV OPEN

LH. RH

Automatically:
on ground below
in flight below

A

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
Q

PAC
O’HEAT
CKPT. CAB

A

PAC Overheat

The environmental control unit disable because of an overt condition in the compressor or turbine

45
Q

PARK
BRAKE

A

Parking Brake

The parking brake is not fully disengaged.

46
Q

P/S HTR
OFF
LH. RH

A

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
Q

Rudder
Bias

A

Rudder Bias

The solenoid bypass valve is open, reducing the effectiveness of the rudder assist cylinder

48
Q

SEC TRIM
FAULT

A

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
Q

SPEED
BRAKE

A

Speed Brake

The middle two spoiler segment son each wing are not fully stowed

50
Q

SPOILER
HOLDOWN

A

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
Q

SPOLIERS
UP

A

Spoilers UP

The inboard spoiler segments are not fully stowed.

52
Q

STAB
ANTI-ICE
LH. RH

A

Stabilizer Ice Protection - OFF

The horizontal stabilizer ice protection system is inoperative because of overheating, loss of power, or heater failure.

53
Q

STALL
WARN

A

Stall Warning

indicates the stall warning system is inoperative

54
Q

Wing
Anti-Ice

LH. RH

A

Wing Anti-Ice System - OFF

the wing anti-ice system is inoperative because of overheating or inadequate bleed air temperature.

55
Q

WING FUEL
XFER OPEN

A

Wing fuel transfer valve - open

The wing fuel transfer valve is energized open

56
Q

W/S Air

A

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
Q

W/S
FAULT
LH. RH

A

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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