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Archer > Systems > Flashcards

Systems Flashcards

(94 cards)

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1
Q

How many master brake cylinders are installed?

A

3

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2
Q

Maximum arc of nose gear turn

A

20 degrees per side

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3
Q

Maximum horsepower

A

180 hp

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4
Q

Purpose of the servo regulator

A

Meters fuel flow proportionally with airflow and maintains the mixture as manually set for all engine speeds

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5
Q

Alternate air source

A

Heated and unfiltered air to be used in the event of blockage of the primary induction air source.

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6
Q

Flap positions

A

10, 25, 40 degrees

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7
Q

How are the flaps actuated

A

Manually and spring loaded to return to the up position

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8
Q

What provides rudder trim

A

A spring device is incorporated in the rudder pedal torque tube assembly

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9
Q

Normal extension of the main gear struts

A

4.5 inches

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10
Q

Normal extension of the nose strut

A

3.25 inches

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11
Q

Where is the brake reservoir located

A

On the top left front face of the firewall

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12
Q

ADAHRS acronym

A

Air Data/ Attitude and Heading Reference System

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13
Q

Where is slip information presented

A

It is a trapezoid under the bank pointer

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14
Q

OAT adjustments and presents what information

A

Adjusted for probe recovery factor and ram air effects to indicate static air temp

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15
Q

Will the AHRS align while the aircraft is in motion?

A

Yes but aligns faster with wings level

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16
Q

ATTITUDE FAIL indication

A

AHRS information became invalid and a red-x will be displayed over the invalid parameter

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17
Q

ADAHRS system

A

Combination of the ADC and the AHRS

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18
Q

ADC information

A

Airspeed, Altitude, VSI, and OAT

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19
Q

AHRS information

A

Attitude, Sideslip, and Heading

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20
Q

Reversionary mode (PFD) displays what information

A

Engine parameters including the full crew alerting system and autopilot annunciations and limited map functions

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21
Q

When is reversionary mode active?

A

If the MFD fails, or if the DISPLAY BACKUP button on the audio panel is pressed

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22
Q

Information displayed on MFD

A 
Engine parameters
Aircraft system parameters
Navigation map
Traffic map
Weather datalink
TAWS-B
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23
Q

EIS acronym

A

Engine Indicating System

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24
Q

CAS acronym

A

Crew Alerting System

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25
Where do CAS text messages appear
In the lower right area of the PFD during both normal and reversionary mode operations
26
Duration of all CAS text messages
Text message will persist until the initiating condition is removed
27
Warning CAS message indications
Flashing red Master WARNING softkey, a flashing CAS Warning text message, a continuous triple chime. If caused by a parameter on the EIS the text message will be replaced by that parameter's indication flashing
28
Amber Caution message indications
A flashing amber Master Caution softkey, a non-repeating double aural chime, and a flashing CAS text message If caused by a parameter on the EIS the text message will be replaced by that parameter's indication flashing
29
White Advisory message indications
White text message, single chime when not a nuisance | messages are not acknowledgeable
30
TAS acronym
Traffic advisory system
31
TAS test duration
10 seconds
32
TAS mode change
8 seconds after takeoff | 24 seconds after landing
33
TAS aural alerts muted
GPS altitude <400' agl
34
Maximum targets on TAS
45 Mode A or C transponders | 30 Mode S transponders
35
TAS range
<2nm-12nm | +/- 10,000' of aircraft
36
TAS for aircraft with out transponders
Unavailable
37
TAS altitude trend indication
Shown when relative climb or descent speed is >500 fpm
38
Traffic is overlaid on what pages
``` Nav map Traffic map Trip planning Nearest Active flight plan PFD insert map PFD forward looking depiction area ```
39
Non-Threat Traffic Indication
Open white diamond with black center | >6nm and greater than +/- 1200'
40
Proximity Advisory (PA)
Solid white diamond | <6nm and less than +/- 1200'
41
Traffic Advisory (TA)
Solid yellow circle, Traffic annunciation on Attitude indicator, Aural "Traffic" and bearing/altitude Displayed when traffic is considered potentially hazardous Display for 8 seconds
42
Traffic Advisory Off Scale
Half TA symbol indicating a TA which is detected but outside the range of the map Text box will appear in lower left of map
43
TAWS acronym
Terrain Awareness and Warning System
44
TAWS alerts
No warning annunciations or voice alerts
45
TAWS altitude
Uses GPS altitude converts to MSL
46
TAWS requirements
Valid 3D position | Valid terrain/obstacle database
47
TAWS display pages
``` Nav map Terrain proximity page Trip planning Flight plan PFD insert map Must select the terrain softkey ```
48
Orientation on Terrain page
Always heading up unless no heading information available
49
Red terrain page
Above or within 100'
50
Yellow terrain page
Between 100' and 1000'
51
Black terrain page
More than 1000' below the aircraft
52
Safe taxi database
Aid in following ground instructions Contains detailed airport diagrams for selected airports. Updated every 56 days and doesn't expire
53
Terrain Database
Updated periodically and have no expiration date. | World wide coverage
54
Obstacle Database
Contains data for obstacles 200' and higher Covers whole US Updated every 56 days and has no expiration date
55
Navigation Database
Covers Americas | Updated on a 28 day cycle
56
FliteCharts Database
Contains procedure charts | Updated on a 28 day cycle (unusable beyond 180 days)
57
JeppView Database
Contains procedure charts & contains position info | Updated on a 14 day cycle (unusable beyond 70 days)
58
Playback button timeframe
Records 2.5 minutes
59
Fail-safe communication path
Direct connection between pilot side and microphone and comm 1
60
Activate fail-safe communication path
Pull the AUDIO MKR CB
61
EBD acronym
Evolution Backup Display
62
EBD provides:
``` Attitude Altitude (baro) Airspeed Heading VSI Slip/skid Turn Rate ```
63
EBD power source
Essential bus | Primary battery
64
EBD duration following electrical failure
30 minutes
65
EBD display in alternator failure
ON BAT annunciation | Display of estimated battery charge state
66
Fuel tank capacity
24 usable | 25 total
67
FOB SYNC
Syncs the totalizer with the current fuel in the tank. Necessary for flight planning page
68
Fuel at tabs
17 gal usable
69
Aux fuel pump usage
Takeoff, landing, and switching tanks
70
Fuel level detector
One float type fuel sensor in each wing. The signal corresponding to the position of the floats is sent to the GEA unit where it is converted into fuel quantity
71
GEA
Garmin Engine Airframe interface unit
72
Electrical system overview
28V system 24V primary battery 24V secondary battery 70 amp 28V alternator
73
Primary battery location
In the Aft Fuselage area
74
How is the alternator driven?
Belt driven
75
Max Voltage on alternator
32 V
76
Emer batt powers:
``` Emer bus (STBY instruments, PFD functions, NAV/COM 1, audio panel) ```
77
Primary battery powers:
Starter Essential Bus Non-Essential Bus Lighting Bus
78
Duration of Emer batt
Minimum 30 minutes
79
Location of Emer Batt
Shelf in aft fuselage area just forward of the primary battery
80
Non-Essential bus equipment
Vent fan | Engine Starter
81
Hot Batt Bus equipment
Courtesy lights Hour meter ELT
82
Essential Bus equipment
``` Pitot heat Fuel pump Stby instruments ADAHRS Audio/MKR Com 1 GEA Integ AV 1 PFD XPDR LTNG PROT ```
83
Lighting Bus equipment
``` Avionics dimmer ANIT COLL NAV lights Panel dimmer LDG/TAXI lights Cabin Lights ```
84
Avionics Bus equipment
``` Com 2 DME INTEG AV 2 MFD Auto pilot TAS XM radio Pitch trim ```
85
Emergency Bus equipment
``` Avionics lights ADAHRS Audio/MKR COM 1 GEA INTEG AV 1 PFD STBY INSTR ```
86
PANEL dimmer switch controls:
Intensity of the LED light strip located under the glareshield
87
SWITCH dimmer switch controls:
Backlighting of the overhead witches, instrument panel switches, CB placards, AP buttons, and all backlit placards on the lower instrument panel
88
AVIONICs dimmer switch controls:
Lighting intensity of the PFD, MFD, and audio panel
89
Location of Pitot Static source
Left wing
90
Location of alternate static source
Left side of the instrument panel
91
Conditions for alternate static source use
Storm window and cabin vents must be closed | Cabin heater and defroster must be on
92
How is cabin heated
Heater muff attached to the exhaust system
93
Size of baggage compartment
24 cubic feet
94
Max baggage
200 lbs

Archer (4 decks)

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