Aircraft Instruments
問題一覧
1
Chromel/alumel thermocouples
2
2, 3, 7, 8
3
Deviation
4
Dampen the oscillation of the float.
5
Display alphanumeric data and representations of aircraft instruments.
6
Not perform repairs to aircraft instruments.
7
Transmitting a signal and receiving back a reflected signal.
8
Magnetic influence deviation
9
Install another instrument.
10
Minimum and/or maximum safe operating limits.
11
29.92 Mb
12
Dry-type vacuum pumps with carbon vanes are very susceptible to damage from solid airborne particles and must take in only filtered air.
13
Vacuum relief valve improperly adjusted
14
By an expanding-type clamp secured to the back of the panel and tightened by a screw from the front of the instrument panel.
15
The existing atmospheric pressure.
16
Allow the pilot to select the appropriate system configuration for the current flight situation.
17
A blue radial line.
18
Electrically
19
Digital signals
20
10 degrees
21
Electrically with wires.
22
1 and 2
23
1, 3, 4, and 5
24
Receive and process input signals from aircraft and engine sensors and send the data to the appropriate display.
25
5
26
3
27
1, 4, 5, 6
28
The altimeter and airspeed indicator will both read low.
29
Bonding straps must be installed across the instrument mounts as a current path.
30
100-hour inspections of instruments.
31
Inspections and function checks on aircraft instruments.
32
1, 3, and 5
33
Iron or steel cases
34
1 and 3
35
Represent the nose of the aircraft.
36
Negative pressure
37
Equipment is added that could affect compass deviation.
38
Not parallel to the true angle of attack of the aircraft.
39
Lubber line
40
Cylinder head temperature gauge, airspeed indicator
41
Both roll and yaw.
42
Only No. 1 is true.
43
The mechanic installing the instrument.
44
Design of the instrument case
45
Isolating portions of the line and testing each portion systematically starting at the instrument connections.
46
Low frequency, high-amplitude shocks.
47
Provide current return paths.
48
100 feet in 1 minute.
49
Low-frequency, high-amplitude shocks.
50
2 or 4
51
White
52
29.92" Hg
53
Altitude above ground level.
54
Pressure altitude
55
Part 43, appendix E
56
Bourdon tube
57
3
58
Not be altered and are designed for a specific installation.
59
Altimeter after suction has been applied to the static system to cause a prescribed equivalent altitude to be indicated.
60
That function is inoperative.
61
The specific aircraft maintenance or flight manual.
62
Three
63
The desirable temperature range.
APCAR/ PCAR
APCAR/ PCAR
Lenard Espiritu · 37問 · 1年前APCAR/ PCAR
APCAR/ PCAR
37問 • 1年前APCAR/PCAR (Optimized)
APCAR/PCAR (Optimized)
Lenard Espiritu · 63問 · 1年前APCAR/PCAR (Optimized)
APCAR/PCAR (Optimized)
63問 • 1年前Airframe Check
Airframe Check
Lenard Espiritu · 13問 · 1年前Airframe Check
Airframe Check
13問 • 1年前Data & Entry
Data & Entry
Lenard Espiritu · 37問 · 1年前Data & Entry
Data & Entry
37問 • 1年前Docs & Forms
Docs & Forms
Lenard Espiritu · 37問 · 1年前Docs & Forms
Docs & Forms
37問 • 1年前Engine Check
Engine Check
Lenard Espiritu · 28問 · 1年前Engine Check
Engine Check
28問 • 1年前Limit and privileges
Limit and privileges
Lenard Espiritu · 32問 · 1年前Limit and privileges
Limit and privileges
32問 • 1年前Aircraft Electric Current
Aircraft Electric Current
Lenard Espiritu · 100問 · 1年前Aircraft Electric Current
Aircraft Electric Current
100問 • 1年前Aircraft Electrica Current (2)
Aircraft Electrica Current (2)
Lenard Espiritu · 30問 · 1年前Aircraft Electrica Current (2)
Aircraft Electrica Current (2)
30問 • 1年前Aircraft Fitting
Aircraft Fitting
Lenard Espiritu · 80問 · 1年前Aircraft Fitting
Aircraft Fitting
80問 • 1年前Aircraft Structures
Aircraft Structures
Lenard Espiritu · 100問 · 1年前Aircraft Structures
Aircraft Structures
100問 • 1年前Aircraft Structures (2)
Aircraft Structures (2)
Lenard Espiritu · 33問 · 1年前Aircraft Structures (2)
Aircraft Structures (2)
33問 • 1年前Electricity Fundamentals
Electricity Fundamentals
Lenard Espiritu · 13問 · 1年前Electricity Fundamentals
Electricity Fundamentals
13問 • 1年前問題一覧
1
Chromel/alumel thermocouples
2
2, 3, 7, 8
3
Deviation
4
Dampen the oscillation of the float.
5
Display alphanumeric data and representations of aircraft instruments.
6
Not perform repairs to aircraft instruments.
7
Transmitting a signal and receiving back a reflected signal.
8
Magnetic influence deviation
9
Install another instrument.
10
Minimum and/or maximum safe operating limits.
11
29.92 Mb
12
Dry-type vacuum pumps with carbon vanes are very susceptible to damage from solid airborne particles and must take in only filtered air.
13
Vacuum relief valve improperly adjusted
14
By an expanding-type clamp secured to the back of the panel and tightened by a screw from the front of the instrument panel.
15
The existing atmospheric pressure.
16
Allow the pilot to select the appropriate system configuration for the current flight situation.
17
A blue radial line.
18
Electrically
19
Digital signals
20
10 degrees
21
Electrically with wires.
22
1 and 2
23
1, 3, 4, and 5
24
Receive and process input signals from aircraft and engine sensors and send the data to the appropriate display.
25
5
26
3
27
1, 4, 5, 6
28
The altimeter and airspeed indicator will both read low.
29
Bonding straps must be installed across the instrument mounts as a current path.
30
100-hour inspections of instruments.
31
Inspections and function checks on aircraft instruments.
32
1, 3, and 5
33
Iron or steel cases
34
1 and 3
35
Represent the nose of the aircraft.
36
Negative pressure
37
Equipment is added that could affect compass deviation.
38
Not parallel to the true angle of attack of the aircraft.
39
Lubber line
40
Cylinder head temperature gauge, airspeed indicator
41
Both roll and yaw.
42
Only No. 1 is true.
43
The mechanic installing the instrument.
44
Design of the instrument case
45
Isolating portions of the line and testing each portion systematically starting at the instrument connections.
46
Low frequency, high-amplitude shocks.
47
Provide current return paths.
48
100 feet in 1 minute.
49
Low-frequency, high-amplitude shocks.
50
2 or 4
51
White
52
29.92" Hg
53
Altitude above ground level.
54
Pressure altitude
55
Part 43, appendix E
56
Bourdon tube
57
3
58
Not be altered and are designed for a specific installation.
59
Altimeter after suction has been applied to the static system to cause a prescribed equivalent altitude to be indicated.
60
That function is inoperative.
61
The specific aircraft maintenance or flight manual.
62
Three
63
The desirable temperature range.