問題一覧
1
Main AC busses
2
RAT generator
3
Main battery
4
Generator drive oil pressure is low.
5
Engine generators
6
BUS TIE switches in AUTO, BATTERY switch ON, GENERATOR CONTROL switches ON
7
External power is connected to the airplane and the voltage and frequency are within limits.
8
The load shedding sequence is galleys first and the utility busses.
9
APU
10
The APU starts automatically, regardless of the APU selector position.
11
The main battery, the standby inverter, the RAT generator and its associated generator control unit
12
Both AC transfer buses
13
The standby inverter can not receive DC power from the RAT generator through TRU
14
The Battery Bus and the Standby Bus
15
Emergency Locator Transmitter
16
Left forward main tank fuel pump
17
D-TO
18
The engines will produce maximum rated thrust.
19
The engines will produce maximum rated thrust.
20
Engine oil pressure is low.
21
Engine oil temperature is high.
22
The spar or engine fuel valve on the left engine has not reached its commanded position.
23
The spar or engine fuel valve on the right engine has not reached its commanded position.
24
After START has been selected on the START/IGNITION selector
25
Left hydraulic system
26
Right hydraulic system
27
The right engine reverser will not deploy or will be limited to idle on landing.
28
The left engine reverser will not deploy or will be limited to idle on landing.
29
The secondary engine indications
30
When the flaps are commanded to 25 or greater
31
Hot start
32
Auto-relight provides flameout protection by activating both ignitors.
33
The APU has automatically shut down.
34
An APU limit has been exceeded.
35
APU controller failure
36
TO
37
The EEC automatically uses the alternate mode.
38
Reference and target N1 are displayed on the N1 indication.
39
A fault is detected in the left engine control system.
40
The right fuel control switch is in RUN at low engine RPM with the autostart switch OFF.
41
The left engine start/ignition selector remains in the START position or the start valve is open when commanded closed.
42
The line displays at all times on the ground.
43
The engine RPM is below idle and the fuel control switch is in RUN.
44
The spar fuel valve is armed.
45
A Fuel Control switch is moved to CUTOFF on the ground.
46
The EICAS message "ENG AUTOSTART" is displayed if the fuel control switch is moved to RUN before the rpm specified in the manual start procedure.
47
The EEC alternates ignitors for successive starts on the ground.
48
The auto speedbrakes deploy when the reverse thrust levers are pulled back to the interlock position.
49
The amber REV indication changes to green REV when the reverser interlock is released.
50
The EICAS message "ENG FAIL (L or R)" is displayed if actual thrust is not increasing to commanded thrust and airspeed is below V1.
B777 - Part 9
B777 - Part 9
Angelo Ortiz · 28問 · 3年前B777 - Part 9
B777 - Part 9
28問 • 3年前B777 - Part 7
B777 - Part 7
Angelo Ortiz · 50問 · 3年前B777 - Part 7
B777 - Part 7
50問 • 3年前B777 - Part 8
B777 - Part 8
Angelo Ortiz · 50問 · 3年前B777 - Part 8
B777 - Part 8
50問 • 3年前B777 - Part 2
B777 - Part 2
Angelo Ortiz · 50問 · 3年前B777 - Part 2
B777 - Part 2
50問 • 3年前B777 - Part 5
B777 - Part 5
Angelo Ortiz · 50問 · 3年前B777 - Part 5
B777 - Part 5
50問 • 3年前B777 - Part 6
B777 - Part 6
Angelo Ortiz · 50問 · 3年前B777 - Part 6
B777 - Part 6
50問 • 3年前B777 - Part 3
B777 - Part 3
Angelo Ortiz · 50問 · 3年前B777 - Part 3
B777 - Part 3
50問 • 3年前B777 - Part 1
B777 - Part 1
Angelo Ortiz · 50問 · 3年前B777 - Part 1
B777 - Part 1
50問 • 3年前AIA - VUL
AIA - VUL
Angelo Ortiz · 100問 · 2年前AIA - VUL
AIA - VUL
100問 • 2年前Underwriting
Underwriting
Angelo Ortiz · 66問 · 2年前Underwriting
Underwriting
66問 • 2年前Airplanes and Aerodynamics
Airplanes and Aerodynamics
Angelo Ortiz · 49問 · 2年前Airplanes and Aerodynamics
Airplanes and Aerodynamics
49問 • 2年前Airplane Instruments, Engines and Systems
Airplane Instruments, Engines and Systems
Angelo Ortiz · 77問 · 2年前Airplane Instruments, Engines and Systems
Airplane Instruments, Engines and Systems
77問 • 2年前Airport, ATC and Airspace
Airport, ATC and Airspace
Angelo Ortiz · 88問 · 2年前Airport, ATC and Airspace
Airport, ATC and Airspace
88問 • 2年前Federal Aviation Regulations - Part 1
Federal Aviation Regulations - Part 1
Angelo Ortiz · 100問 · 2年前Federal Aviation Regulations - Part 1
Federal Aviation Regulations - Part 1
100問 • 2年前Federal Aviation Regulations - Part 2
Federal Aviation Regulations - Part 2
Angelo Ortiz · 89問 · 2年前Federal Aviation Regulations - Part 2
Federal Aviation Regulations - Part 2
89問 • 2年前Airplane Weight and Balance
Airplane Weight and Balance
Angelo Ortiz · 10問 · 2年前Airplane Weight and Balance
Airplane Weight and Balance
10問 • 2年前Medical Factors and Decision Making
Medical Factors and Decision Making
Angelo Ortiz · 25問 · 2年前Medical Factors and Decision Making
Medical Factors and Decision Making
25問 • 2年前Weather and Services
Weather and Services
Angelo Ortiz · 87問 · 2年前Weather and Services
Weather and Services
87問 • 2年前Navigation
Navigation
Angelo Ortiz · 30問 · 2年前Navigation
Navigation
30問 • 2年前問題一覧
1
Main AC busses
2
RAT generator
3
Main battery
4
Generator drive oil pressure is low.
5
Engine generators
6
BUS TIE switches in AUTO, BATTERY switch ON, GENERATOR CONTROL switches ON
7
External power is connected to the airplane and the voltage and frequency are within limits.
8
The load shedding sequence is galleys first and the utility busses.
9
APU
10
The APU starts automatically, regardless of the APU selector position.
11
The main battery, the standby inverter, the RAT generator and its associated generator control unit
12
Both AC transfer buses
13
The standby inverter can not receive DC power from the RAT generator through TRU
14
The Battery Bus and the Standby Bus
15
Emergency Locator Transmitter
16
Left forward main tank fuel pump
17
D-TO
18
The engines will produce maximum rated thrust.
19
The engines will produce maximum rated thrust.
20
Engine oil pressure is low.
21
Engine oil temperature is high.
22
The spar or engine fuel valve on the left engine has not reached its commanded position.
23
The spar or engine fuel valve on the right engine has not reached its commanded position.
24
After START has been selected on the START/IGNITION selector
25
Left hydraulic system
26
Right hydraulic system
27
The right engine reverser will not deploy or will be limited to idle on landing.
28
The left engine reverser will not deploy or will be limited to idle on landing.
29
The secondary engine indications
30
When the flaps are commanded to 25 or greater
31
Hot start
32
Auto-relight provides flameout protection by activating both ignitors.
33
The APU has automatically shut down.
34
An APU limit has been exceeded.
35
APU controller failure
36
TO
37
The EEC automatically uses the alternate mode.
38
Reference and target N1 are displayed on the N1 indication.
39
A fault is detected in the left engine control system.
40
The right fuel control switch is in RUN at low engine RPM with the autostart switch OFF.
41
The left engine start/ignition selector remains in the START position or the start valve is open when commanded closed.
42
The line displays at all times on the ground.
43
The engine RPM is below idle and the fuel control switch is in RUN.
44
The spar fuel valve is armed.
45
A Fuel Control switch is moved to CUTOFF on the ground.
46
The EICAS message "ENG AUTOSTART" is displayed if the fuel control switch is moved to RUN before the rpm specified in the manual start procedure.
47
The EEC alternates ignitors for successive starts on the ground.
48
The auto speedbrakes deploy when the reverse thrust levers are pulled back to the interlock position.
49
The amber REV indication changes to green REV when the reverser interlock is released.
50
The EICAS message "ENG FAIL (L or R)" is displayed if actual thrust is not increasing to commanded thrust and airspeed is below V1.