問題一覧
1
Advise ATC immediately.
2
The maximum top cells is 57,000 feet located 65 NM southeast the station.
3
Alternate Fuel
4
+16.43.
5
A. TORA
6
of some designated point on the runway.
7
The altimeter will indicate zero feet altitude
8
green arc
9
96.13 inches aft of datum
10
30 hours
11
variations in airplane loading
12
8 hours
13
After gear retraction
14
CG is too far rearward, and rotation is around the CG.
15
Takeoff safety speed.
16
an extension of the inboud final approach course.
17
the fuel mixture ignites instantaneously instead of burning progressively and evenly
18
Destination airport, en route altitude, and SID, if appropriate.
19
C. 250 knots
20
weight of fuel and weight of air entering the cylinder
21
32 hours in any 7 consecutive days
22
Advisory that inidcates an emergency situation is possible should an undue delay occur.
23
135 radial
24
250 knots.
25
Variable Pitch Propeller
26
Sustained winds of 65 knots or more.
27
Axial flow jet engine
28
A calm or light wind near the surface and a relatively strong wind just above the inversion.
29
lateral axis
30
2 DME miles.
31
evaporation of precipitation
32
is warmer than the air behind the overtaking cold front
33
1½ minutes
34
airspeed and RPM
35
45 mins. at normal cruising speed
36
Centrifugal Flow Jet Engine
37
30 days
38
Single-engine land, multi-engine land, single-engine sea, and multi-engine sea
39
108.10 to 111.95 MHZ
40
Date of check, place of operational check, bearing error and signature.
41
plus or minus 6°
42
Aft of the exhaust section
43
Azimuth, elevation, and distance information.
44
20,000 feet
45
50 gallons
46
At or above 24,000 feet MSL if VOR navigational equipment is required.
47
D. A and C are correct
48
Vs1
49
power and vertical velocity required to remain on the proper glide path
50
3,420 FT
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
Via · 78問 · 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
CPL HUMAN PERFORMANCE AND LIMITATIONS (1)
78問 • 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
Via · 81問 · 1年前CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
CPL HUMAN PERFORMANCE AND LIMITATIONS (2)
81問 • 1年前CPL Radio Telephony (1)
CPL Radio Telephony (1)
Via · 100問 · 1年前CPL Radio Telephony (1)
CPL Radio Telephony (1)
100問 • 1年前CPL Radio Telephony (2)
CPL Radio Telephony (2)
Via · 100問 · 1年前CPL Radio Telephony (2)
CPL Radio Telephony (2)
100問 • 1年前CPL Radio Telephony (3)
CPL Radio Telephony (3)
Via · 20問 · 1年前CPL Radio Telephony (3)
CPL Radio Telephony (3)
20問 • 1年前Met 1
Met 1
Via · 78問 · 1年前Met 1
Met 1
78問 • 1年前Met 2
Met 2
Via · 43問 · 1年前Met 2
Met 2
43問 • 1年前Met 3
Met 3
Via · 49問 · 1年前Met 3
Met 3
49問 • 1年前Met 4
Met 4
Via · 14問 · 1年前Met 4
Met 4
14問 • 1年前Met 5
Met 5
Via · 83問 · 1年前Met 5
Met 5
83問 • 1年前Met 6
Met 6
Via · 35問 · 1年前Met 6
Met 6
35問 • 1年前Met 7
Met 7
Via · 54問 · 1年前Met 7
Met 7
54問 • 1年前Met 8
Met 8
Via · 7問 · 1年前Met 8
Met 8
7問 • 1年前Human Performance 3
Human Performance 3
Via · 57問 · 1年前Human Performance 3
Human Performance 3
57問 • 1年前Met 9
Met 9
Via · 35問 · 1年前Met 9
Met 9
35問 • 1年前Met 10
Met 10
Via · 43問 · 1年前Met 10
Met 10
43問 • 1年前AGK 1
AGK 1
Via · 63問 · 1年前AGK 1
AGK 1
63問 • 1年前AGK 2
AGK 2
Via · 47問 · 1年前AGK 2
AGK 2
47問 • 1年前AGK 3
AGK 3
Via · 97問 · 1年前AGK 3
AGK 3
97問 • 1年前問題一覧
1
Advise ATC immediately.
2
The maximum top cells is 57,000 feet located 65 NM southeast the station.
3
Alternate Fuel
4
+16.43.
5
A. TORA
6
of some designated point on the runway.
7
The altimeter will indicate zero feet altitude
8
green arc
9
96.13 inches aft of datum
10
30 hours
11
variations in airplane loading
12
8 hours
13
After gear retraction
14
CG is too far rearward, and rotation is around the CG.
15
Takeoff safety speed.
16
an extension of the inboud final approach course.
17
the fuel mixture ignites instantaneously instead of burning progressively and evenly
18
Destination airport, en route altitude, and SID, if appropriate.
19
C. 250 knots
20
weight of fuel and weight of air entering the cylinder
21
32 hours in any 7 consecutive days
22
Advisory that inidcates an emergency situation is possible should an undue delay occur.
23
135 radial
24
250 knots.
25
Variable Pitch Propeller
26
Sustained winds of 65 knots or more.
27
Axial flow jet engine
28
A calm or light wind near the surface and a relatively strong wind just above the inversion.
29
lateral axis
30
2 DME miles.
31
evaporation of precipitation
32
is warmer than the air behind the overtaking cold front
33
1½ minutes
34
airspeed and RPM
35
45 mins. at normal cruising speed
36
Centrifugal Flow Jet Engine
37
30 days
38
Single-engine land, multi-engine land, single-engine sea, and multi-engine sea
39
108.10 to 111.95 MHZ
40
Date of check, place of operational check, bearing error and signature.
41
plus or minus 6°
42
Aft of the exhaust section
43
Azimuth, elevation, and distance information.
44
20,000 feet
45
50 gallons
46
At or above 24,000 feet MSL if VOR navigational equipment is required.
47
D. A and C are correct
48
Vs1
49
power and vertical velocity required to remain on the proper glide path
50
3,420 FT