T-1 Annunciators Flashcards
Annunciator:
- Loss of Cabin Pressure
- Cabin Altitude Exceeds 9500 +/- 500’
Annunciator:
Left Fire Detector Failure
Annunciator:
Left Windshield Overheat
Annunciator:
Horizontal Stabilizer Anti-Ice System Failure
Annunciator:
Left Engine Oil Pressure <40 psi
Annunciator:
Left Engine Fuel Px < 5.0 +/- 0.5 psi
Annunciator:
7-Degree Main flap Section Asymmetry
Annunciator:
- Left Fuel Feed Chamber Low
- (70 pounds/11 gal usable)
Annunciator:
Fuel Px in left transfer lines below 5.0 +/- 0.5 psi
Annunciator:
< 200 pounds (32 gal) usable fuel remaining in the Left Wing Tank
Annunciator:
Left Wing Tank Px > 3.5 +/- 0.5 psi
Annunciator:
- Left fuel filter clogged
- Px differential > 2.3 +/- 0.2
Annunciator:
- Left oil filter clogged
- Check the oil Px guage
Annunciator:
- Left hydraulic pump failure
- Px <750 psi
Annunciator:
Left engine electronic fuel control failure
Annunciator:
Left stall warning system failure
Annunciator:
Left generator inoperative
Annunciator:
Left bus feeder failure
Annunciator:
Battery relay open
Annunciator:
- Inverter No. 1 Failure
- Frequency variance of +/- 4%
- Inverter No. 2 is powering the primary AC busses
- Secondary AC busses are powerless
Annunciator:
Left engine anti-ice temperature < 120° F
Annunciator:
Air conditioning overtemperature/overpressure
- >400° F
- >53 psi
Annunciator:
Bleed air duct rupture
- Px increase of 3.5 +/- 0.5 psi
and/or
- > 350° F
Dash-1: 1-33, 1-150
Annunciator:
Defog air temperature > 200° F
Annunciator:
High cabin area temperature sensed
- 390 +/- 15° F
Annunciator:
Anti skid system failure
Annunciator:
System failure:
- Cabin pressure > 11 +/-1 psi
Annunciator:
Right fire detector failure
Annunciator:
Right windshield overheat
Annunciator:
Wing anti-ice temperature high
- 212° F/350° F
Annunciator:
Right engine oil Px <40 psi
Annunciator:
Right engine fuel Px < 5.0 +/- 0.5 psi
Annunciator:
Avionics rack cooling blower failure
Annunciator:
Right fuel feed chamber low
- 70 lbs / 11 gal useable
Annunciator:
Fuel Px in right transfer lines < 5.0 +/- 0.5 psi
Annunciator:
< 200 pounds (32 gal) usable fuel remaining in the Right Wing Tank
Annunciator:
Right Wing Tank Px > 3.5 +/- 0.5 psi
Annunciator:
Right fuel filter clogged
Px differential > 2.3 +/- 0.2 psi
Annunciator:
Right oil filter clogged
Check the oil Px guage
Annunciator:
Right hydraulic pump failure
- < 750 psi
Annunciator:
Right engine electronic fuel control failure
Annunciator:
Right stall warning system failure
Annunciator:
Right generator inoperative
Annunciator:
- Right bus feeder power lost
- Feeder cable circuit breaker open
- Standby feeder activated
Annunciator:
Emergency bus feeder power lost
Emergency bus powerd by left hand load bus
Annunciator:
Inverter No. 2 Failure
Frequency variance of +/- 4%
Annunciator:
Right engine ant-ice temperature < 120° F
Annunciator:
Horizontal stabilizer deice system failure
Annunciator:
Door unlocked
Annunciator:
Pitot heat switch off or pitot heat system failure
Annunciator:
Hydraulic fluid level < 0.6 gallons
Annunciator:
Rudder boost system failure
Switch/Annunciator:
2x (P/CP) Illuminate when a comparator warning occurs or after an EFIS test
Pushing this button:
• Makes EFIS annunciators stop flashing
• Reset heading and attitude comparitor warnings
Dash-1:
1-189; EFIS Master Warning Switchlight
3-45
Switch/Annunciator:
Illuminates when:
- Excessive rate of descent w/ respect to terrain
- Excessive closure rate to terrain
- Descent after takeoff/go-around
- Insufficient terrain clearance
(Modes 1-4)
Dash-1: 1-387
Annunciator:
- Pitch trim follow-up function of the autopilot has failed.
- Disconnect the autopilot and be prepared for out-of-trim forces.
Dash-1: 3-23
Switch/Annunciator:
- Push to initiate the GPWS self-test on the ground
- Remains illuminated for the duration of the test
Annunciator
- Roll trim follow-up function of the autopilot has failed.
- Disconnect the autopilot and be prepared for out-of-trim forces.
Dash-1: 3-23
Switch/Annunciator:
- Illuminates when the threshold of mode 5 has been exceeded
- 1000’ AGL and/or
- >1.3 dots below
- Automatically rearmed when
- AC descends below 30’ AGL
- AC climbs through 1500’ AGL
- Tuning NAV 1 off the ILS frequency
- Acompanied by Bob’s “GLIDESLOPE”
Dash-1: 1-389, 1-395
Annunciator:
The AHRS is in the initialization mode
Dash-1: 1-228
Annunciator:
Smoke particles have entered the path of the pulsed beam
Dash-1: 1-414
Switch/Annunciator:
- Power is applied to the aircraft electrical system (top)
- Standby battery is connected to the standby bus (bottom)
Dash-1: 1-59
Switch/Annunciator:
- Power is applied to the aircraft electrical system (top)
- Loss of all primary (or main) electrical power (bottom)
Dash-1: 1-59
Switch/Annunciator:
GPWS Tactical mode activated.
- Used to reduce nucance warnings when flying low levels
- Decreases modes 2B & 4B warning boundaries
- Automatically resets above 2450’ AGL
(The top portion is always iluminated when power is on)
Dash-1: 1-389
Switch/Annunciator:
Illuminated when power is on (top)
Pressing it
- Iluminates ACTIVE
- disables Bob’s “TOO LOW FLAPS”
Automatically Resets
- When the AC descends below 30’ AGL and <80 KIAS
Dash-1: 1-389
Switch/Annunciator:
Left Hydraulic/Fuel Valve Open
Left Hydraulic/Fuel Valve Closed
Switch/Annunciator:
Right Hydraulic/Fuel Valve Open
Right Hydraulic/Fuel Valve Closed
Switch/Annunciator:
Firebottle #1 Armed
Switch/Annunciator:
Firebottle #2 Armed
Switch/Annunciator:
Fire detected in the left engine
Switch/Annunciator:
Fire detected in the left engine
Annunciator
The AHRS battery power subsystem is functional
Dash-1: 1-59
Annunciator
- 0.020 inches of ice on the probe detector
- Annunciator cycle lasts for 50-70 seconds
Dash-1: 1-150
Annunciator
- Ice detector failure or
- Ice detector has lost power
Dash-1: 1-150
Annunciator
Temperature in the wing anti-ice ducts is below 140º F
Dash-1: 1-150
Pitch trim is in the center T.O. position
Dash-1: 1-103
- Landing light(s) extended with gear retracted,
or
- landing light(s) actuator has not reached the retracted position (white).
Dash-1: 1-416
Passenger oxygen system operating
Dash-1: 1-416
Fuel crossfeed system operating
Dash-1: 1-416
Right load bus not powered
Dash-1: 1-416
Hydraulically actuated speed brakes extended
Dash-1: 1-416
Pitch trim position set more nose down than optimum
Dash-1: 1-416
Engine synchronization control switch in fan or turbine position.
Dash-1: 1-416
Engine electronic fuel control auxiliary power in use
Dash-1: 1-416
Guarded emergency light control switch off or in test/on position.
Dash-1: 1-416
Pitch trim position set more nose up than optimum
Dash-1: 1-416
Landing gear horn silenced
Dash-1: 1-416
