acg
問題一覧
1
A chip detector, a temperature sensor and a low level sensor
2
With the aircraft on the ground and NR less than 2%
3
4 (Four)
4
Duplex ball bearing
5
Duplex ball bearing located in the Tail Rotor Spider
6
An adjustable friction, a fixed friction and a collective balance spring
7
Carbon Fiber epoxy
8
There are no Cyclic Adjustable Stops
9
1 pin for collective, 1 pin for pitch and 1 pin for roll
10
It must be adjusted to the same length as the replaced rod
11
On the Mixing Unit
12
To verify freedom of movement of the Outer Sleeve and to check for dormant failures
13
A Performance Check must be carried out
14
Titanium
15
Titanium
16
Titanium
17
No Oil Drain Period is scheduled
18
Pilot only
19
The Engine flames out
20
Ignition System
21
From MIN to MAX in MANUAL
22
large chances in the aircraft pitch and roll attitude
23
The ENG MODE switch must stay in the IDLE or FLIGHT position
24
The engine flames out
25
EEC FAIL
26
The ECL should not be used for manual control of the engine
27
The ENG GOV to AUTO, the ECL to OFF
28
DCU records engine fatigue and exceedance data; contains engine trim data
29
Engine 1 Permanent Magnet Alternator
30
Two green triangles are displayed either around the TQ or the ITT legends on the MFD
31
EECs (Engine Electronic Control)
32
The Fuel Nozzles for cleaning
33
TQ LIMITER ON Advisory message
34
By moving the ENG MODE switch to IDLE either in AUTO or MANUAL
35
FLIGHT
36
MIN to MAX
37
FLIGHT
38
735°C with limiting parameter ITT
39
Achieve a safe OEI flight and move the ENG MODE to IDLE
40
Brand and type mixing is not allowed
41
IGN at 49 % Ng, START at 49 % Ng
42
Turn the ENG MODE switch to IDLE
43
The relevant loadmeter does not show amber dashes
44
GEN 1 loadmeter must be in the green range
45
GCU
46
10 seconds
47
The Main Battery is used to start the engine while the Aux Battery is only used to feed the essential bus-bars
48
They are EASA/FAA approved and can only be changed after additional approval from the Authority
49
Applicable aircraft model code
50
System difference code (eg: an item supplied by an alternate vendor)
51
Their indicated life is reached
52
AMPI, Chapter 05 – Scheduled/Unscheduled Maintenance, Section 05-50 – Unscheduled Maintenance Checks
53
In the Unscheduled Maintenance Check Tasks section of the IETP Are opportune at the occurrence of another maintenance task, or which cannot be included in an hourly/calendar schedule.
54
Reference Sections numbered from front to back, bottom to top and left to right
55
A dedicated magnetic pick-up
56
The air conditioning system cool air is mixed with the ambient air in the jet pump (Venturi duct) and distributes it to cockpit and cabin
57
The forward flapper valves are opened for ram air ventilation
58
After System Checks, before Taxiing
59
FD is powered and Guidance Controller is in STBY mode; Both Autopilots are not powered
60
four
61
Disengagement of the FD mode(s)
62
Modular Avionic Units (MAU)
63
Large changes in the aircraft pitch and roll attitude
64
To keep providing both aircraft stabilization and attitude holding, in case either AP1 or AP2 fails
65
To make large changes to the aircraft pitch and Roll attitude
66
The Flight Director is coupled to the Autopilot
67
Equal or greater than 60 knots
68
To set and control the volume of the Cabin Audio Control Panel
69
Load the Flight Software only
70
Left side of the Nose Compartment
71
The protection function is applicable during the starting phase
72
With the BUS TIE switch set to ON
73
The Main Battery is used to supply the Starter Generator, while the Auxilliary Battery is used to feed the Essential Bus Bars
74
When External Power is connected to the Aircraft
75
By the External Power
76
Pins 5 and 8 on the ELT/NAV Interface Unit connector must be jumpered
77
Two nylon ropes on the upper side, four clips on the bottom side
問題一覧
1
A chip detector, a temperature sensor and a low level sensor
2
With the aircraft on the ground and NR less than 2%
3
4 (Four)
4
Duplex ball bearing
5
Duplex ball bearing located in the Tail Rotor Spider
6
An adjustable friction, a fixed friction and a collective balance spring
7
Carbon Fiber epoxy
8
There are no Cyclic Adjustable Stops
9
1 pin for collective, 1 pin for pitch and 1 pin for roll
10
It must be adjusted to the same length as the replaced rod
11
On the Mixing Unit
12
To verify freedom of movement of the Outer Sleeve and to check for dormant failures
13
A Performance Check must be carried out
14
Titanium
15
Titanium
16
Titanium
17
No Oil Drain Period is scheduled
18
Pilot only
19
The Engine flames out
20
Ignition System
21
From MIN to MAX in MANUAL
22
large chances in the aircraft pitch and roll attitude
23
The ENG MODE switch must stay in the IDLE or FLIGHT position
24
The engine flames out
25
EEC FAIL
26
The ECL should not be used for manual control of the engine
27
The ENG GOV to AUTO, the ECL to OFF
28
DCU records engine fatigue and exceedance data; contains engine trim data
29
Engine 1 Permanent Magnet Alternator
30
Two green triangles are displayed either around the TQ or the ITT legends on the MFD
31
EECs (Engine Electronic Control)
32
The Fuel Nozzles for cleaning
33
TQ LIMITER ON Advisory message
34
By moving the ENG MODE switch to IDLE either in AUTO or MANUAL
35
FLIGHT
36
MIN to MAX
37
FLIGHT
38
735°C with limiting parameter ITT
39
Achieve a safe OEI flight and move the ENG MODE to IDLE
40
Brand and type mixing is not allowed
41
IGN at 49 % Ng, START at 49 % Ng
42
Turn the ENG MODE switch to IDLE
43
The relevant loadmeter does not show amber dashes
44
GEN 1 loadmeter must be in the green range
45
GCU
46
10 seconds
47
The Main Battery is used to start the engine while the Aux Battery is only used to feed the essential bus-bars
48
They are EASA/FAA approved and can only be changed after additional approval from the Authority
49
Applicable aircraft model code
50
System difference code (eg: an item supplied by an alternate vendor)
51
Their indicated life is reached
52
AMPI, Chapter 05 – Scheduled/Unscheduled Maintenance, Section 05-50 – Unscheduled Maintenance Checks
53
In the Unscheduled Maintenance Check Tasks section of the IETP Are opportune at the occurrence of another maintenance task, or which cannot be included in an hourly/calendar schedule.
54
Reference Sections numbered from front to back, bottom to top and left to right
55
A dedicated magnetic pick-up
56
The air conditioning system cool air is mixed with the ambient air in the jet pump (Venturi duct) and distributes it to cockpit and cabin
57
The forward flapper valves are opened for ram air ventilation
58
After System Checks, before Taxiing
59
FD is powered and Guidance Controller is in STBY mode; Both Autopilots are not powered
60
four
61
Disengagement of the FD mode(s)
62
Modular Avionic Units (MAU)
63
Large changes in the aircraft pitch and roll attitude
64
To keep providing both aircraft stabilization and attitude holding, in case either AP1 or AP2 fails
65
To make large changes to the aircraft pitch and Roll attitude
66
The Flight Director is coupled to the Autopilot
67
Equal or greater than 60 knots
68
To set and control the volume of the Cabin Audio Control Panel
69
Load the Flight Software only
70
Left side of the Nose Compartment
71
The protection function is applicable during the starting phase
72
With the BUS TIE switch set to ON
73
The Main Battery is used to supply the Starter Generator, while the Auxilliary Battery is used to feed the Essential Bus Bars
74
When External Power is connected to the Aircraft
75
By the External Power
76
Pins 5 and 8 on the ELT/NAV Interface Unit connector must be jumpered
77
Two nylon ropes on the upper side, four clips on the bottom side