T-1 Annunciators Flashcards
(90 cards)
1
Q
A
Annunciator:
- Loss of Cabin Pressure
- Cabin Altitude Exceeds 9500 +/- 500’
2
Q
A
Annunciator:
Left Fire Detector Failure
3
Q
A
Annunciator:
Left Windshield Overheat
4
Q
A
Annunciator:
Horizontal Stabilizer Anti-Ice System Failure
5
Q
A
Annunciator:
Left Engine Oil Pressure <40 psi
6
Q
A
Annunciator:
Left Engine Fuel Px < 5.0 +/- 0.5 psi
7
Q
A
Annunciator:
7-Degree Main flap Section Asymmetry
8
Q
A
Annunciator:
- Left Fuel Feed Chamber Low
- (70 pounds/11 gal usable)
9
Q
A
Annunciator:
Fuel Px in left transfer lines below 5.0 +/- 0.5 psi
10
Q
A
Annunciator:
< 200 pounds (32 gal) usable fuel remaining in the Left Wing Tank
11
Q
A
Annunciator:
Left Wing Tank Px > 3.5 +/- 0.5 psi
12
Q
A
Annunciator:
- Left fuel filter clogged
- Px differential > 2.3 +/- 0.2
13
Q
A
Annunciator:
- Left oil filter clogged
- Check the oil Px guage
14
Q
A
Annunciator:
- Left hydraulic pump failure
- Px <750 psi
15
Q
A
Annunciator:
Left engine electronic fuel control failure
16
Q
A
Annunciator:
Left stall warning system failure
17
Q
A
Annunciator:
Left generator inoperative
18
Q
A
Annunciator:
Left bus feeder failure
19
Q
A
Annunciator:
Battery relay open
20
Q
A
Annunciator:
- Inverter No. 1 Failure
- Frequency variance of +/- 4%
- Inverter No. 2 is powering the primary AC busses
- Secondary AC busses are powerless
21
Q
A
Annunciator:
Left engine anti-ice temperature < 120° F
22
Q
A
Annunciator:
Air conditioning overtemperature/overpressure
- >400° F
- >53 psi
23
Q
A
Annunciator:
Bleed air duct rupture
- Px increase of 3.5 +/- 0.5 psi
and/or
- > 350° F
Dash-1: 1-33, 1-150
24
Q
A
Annunciator:
Defog air temperature > 200° F
25
Annunciator:
High cabin area temperature sensed
* 390 +/- 15° F
26
Annunciator:
## Footnote
Anti skid system failure
27
Annunciator:
System failure:
* Cabin pressure \> 11 +/-1 psi
28
Annunciator:
## Footnote
Right fire detector failure
29
Annunciator:
## Footnote
Right windshield overheat
30
Annunciator:
Wing anti-ice temperature high
* 212° F/350° F
31
Annunciator:
## Footnote
Right engine oil Px \<40 psi
32
Annunciator:
## Footnote
Right engine fuel Px \< 5.0 +/- 0.5 psi
33
Annunciator:
## Footnote
Avionics rack cooling blower failure
34
Annunciator:
Right fuel feed chamber low
* 70 lbs / 11 gal useable
35
Annunciator:
## Footnote
Fuel Px in right transfer lines \< 5.0 +/- 0.5 psi
36
Annunciator:
## Footnote
\< 200 pounds (32 gal) usable fuel remaining in the Right Wing Tank
37
Annunciator:
## Footnote
Right Wing Tank Px \> 3.5 +/- 0.5 psi
38
Annunciator:
## Footnote
Right fuel filter clogged
Px differential \> 2.3 +/- 0.2 psi
39
Annunciator:
## Footnote
Right oil filter clogged
Check the oil Px guage
40
Annunciator:
Right hydraulic pump failure
* \< 750 psi
41
Annunciator:
## Footnote
Right engine electronic fuel control failure
42
Annunciator:
## Footnote
Right stall warning system failure
43
Annunciator:
## Footnote
Right generator inoperative
44
Annunciator:
* Right bus feeder power lost
* Feeder cable circuit breaker open
* Standby feeder activated
45
Annunciator:
## Footnote
Emergency bus feeder power lost
Emergency bus powerd by left hand load bus
46
Annunciator:
## Footnote
Inverter No. 2 Failure
Frequency variance of +/- 4%
47
Annunciator:
## Footnote
Right engine ant-ice temperature \< 120° F
48
Annunciator:
## Footnote
Horizontal stabilizer deice system failure
49
Annunciator:
## Footnote
Door unlocked
50
Annunciator:
## Footnote
Pitot heat switch off or pitot heat system failure
51
Annunciator:
## Footnote
Hydraulic fluid level \< 0.6 gallons
52
Annunciator:
## Footnote
Rudder boost system failure
53
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
54
Switch/Annunciator:
Illuminates when:
1. Excessive rate of descent w/ respect to terrain
2. Excessive closure rate to terrain
3. Descent after takeoff/go-around
4. Insufficient terrain clearance
(Modes 1-4)
Dash-1: 1-387
55
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
56
Switch/Annunciator:
* Push to initiate the GPWS self-test on the ground
* Remains illuminated for the duration of the test
57
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
58
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
59
Annunciator:
The AHRS is in the initialization mode
Dash-1: 1-228
60
Annunciator:
Smoke particles have entered the path of the pulsed beam
Dash-1: 1-414
61
Switch/Annunciator:
* Power is applied to the aircraft electrical system (top)
* Standby battery is connected to the standby bus (bottom)
Dash-1: 1-59
62
Switch/Annunciator:
* Power is applied to the aircraft electrical system (top)
* Loss of all primary (or main) electrical power (bottom)
Dash-1: 1-59
63
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
64
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
65
Switch/Annunciator:
Left Hydraulic/Fuel Valve Open
Left Hydraulic/Fuel Valve Closed
66
Switch/Annunciator:
Right Hydraulic/Fuel Valve Open
Right Hydraulic/Fuel Valve Closed
67
Switch/Annunciator:
Firebottle #1 Armed
68
Switch/Annunciator:
Firebottle #2 Armed
69
Switch/Annunciator:
Fire detected in the left engine
70
Switch/Annunciator:
Fire detected in the left engine
71
Annunciator
The AHRS battery power subsystem is functional
Dash-1: 1-59
72
Annunciator
* 0.020 inches of ice on the probe detector
* Annunciator cycle lasts for 50-70 seconds
Dash-1: 1-150
73
Annunciator
* Ice detector failure or
* Ice detector has lost power
Dash-1: 1-150
74
Annunciator
Temperature in the wing anti-ice ducts is below 140º F
Dash-1: 1-150
75
Pitch trim is in the center T.O. position
Dash-1: 1-103
76
* Landing light(s) extended with gear retracted,
or
* landing light(s) actuator has not reached the retracted position (white).
Dash-1: 1-416
77
Passenger oxygen system operating
## Footnote
Dash-1: 1-416
78
Fuel crossfeed system operating
Dash-1: 1-416
79
Right load bus not powered
Dash-1: 1-416
80
Hydraulically actuated speed brakes extended
Dash-1: 1-416
81
Pitch trim position set more nose down than optimum
Dash-1: 1-416
82
Engine synchronization control switch in fan or turbine position.
Dash-1: 1-416
83
Engine electronic fuel control auxiliary power in use
## Footnote
Dash-1: 1-416
84
Guarded emergency light control switch off or in test/on position.
Dash-1: 1-416
85
Pitch trim position set more nose up than optimum
Dash-1: 1-416
86
Landing gear horn silenced
Dash-1: 1-416
87
88
89
90
