RENEW2024_4
問題一覧
1
Saving will occur both in fuel usage as well as crew time and increase airspace
2
GMM
3
GMM
4
static source error correction
5
near pitot/static
6
FL290-FL410
7
Pitot tube
8
AOA,TAT,Pitot probe ,static port
9
"BITE may be used for fault isolation and trouble shooting."
10
"To be dispatched for a non-RVSM airspace is allowed."
11
72 hours
12
"malfunction of aircraft equipment and operational errors"
13
ALL
14
approved tester on the RVSM Maint program
15
Any structure repairs or modification around pitot/static probes , altimeter accuracy check and pitot-static leakage check
16
Do a leakage check
17
A/P ALT Mode ,ADC,ATC,ALT ALERT
18
QA
19
1000 feet
20
MEL
21
發動機總使用時間
22
26年
23
Level 1
24
三個月
25
七年
26
從飛機製造廠出廠時間
27
十四年
28
五年
29
M9
30
MS
31
M8
32
Maintenance personnel shall inform Maintenance Operation Center and the next station via telex on the current status of the CAT capability. The flight crew shall be informed orally.
33
contact Maintenance Operation Center to determine the actual aircraft status
34
The latest AUTOLAND operation date + 28days
35
Minimum Equipment List
36
Fail safe
37
The TLB shall indicate which action caused the upgrading.
38
DH is the wheel height above the runway elevation
39
sensors and computers must be separated, but also the electrical and hydraulic power supply and even all electrical wires.
40
100 ft
41
CAT II/III Maintenance Program operation and CAT II/III system maintenance audit.
42
An automatic landing system is the only equipment providing automatic control of the aircraft during the approach and landing and is not related to particular weather condition.
43
CAT II / III authorized maintenance only.
44
Airworthiness Directive affects the CAT operation.
45
Perform maintenance actions or inspections to determine the aircraft CAT status in accordance with fleet MEL.
46
To trace and analyze the reliability of CAT II/III systems/components and provide recommendations for improvements.
47
Significantly increase stall speed, reduce controllability, and alter aircraft flight characteristics.
48
SAE specifications.
49
"The latest revision of Aircrft Maintenance Manual."
50
The holdover time starts with the first application of anti-icing fluid.
51
De-icing.
52
Anti-icing.
53
heated.
54
To prevents the accumulation of frost, ice, or snow on a clean airplane surface for a certain period of time called holdover time.
55
fluid type, fluid name and dilution concentration.
56
The local time of de/anti-icing operation commenced and Result of Post De/anti- icing Check.
57
True.
58
Pilot-In-Command or designated Maintenance Representative.
59
Glycol.
60
Only the last leg time
61
0.20 QT/HR
62
Add oil/accumulated APU hours since last oil full service
63
OCR confirmation or maintenance action is required to entry into TLB.
64
Pre-Departure Service Check
65
APU can perform in-flight start test at return (to home base) portion of non- ETOPS flight
66
Cargo compartment fire suppression capacity be suitable for the duration of the approved diversion time plus 20 minutes
67
4 hours
68
Check cargo compartment liners for tears and punctures.
69
In case of no system abnormal and no “M” procedure (for DD) required to be performed for the flight. No need to do PDSC check again, but check oil consumption rate is mandatory.
70
120 min.
71
Performed by one mechanic and inspected by any other additional one mechanic.
72
Configuration, Maintenance and Procedures
73
VHF1 system unavailable during flight.
74
12 months
75
12 months
76
Extended Diversion Time Operations
77
Human error
78
Never, until the cause has been determined
79
WDM.
80
"Tightened by hand plus a maximum 1/8 turn more."
81
SWPM
82
De-icing fluids
83
Hydraulic oils
84
AMM and SWPM
85
SWPM
86
TSM
87
Electrical Wiring Interconnection System
88
Normally available lighting
89
"Open the circuit breaker of the safety sensitive system"
90
Up or forward
91
to allow for drainage of moisture
92
SWPM and ESPM
93
continuity check
94
WDM and AWM
95
Tools should have the certification acceptance recorded on the Tool Record Card or Tool Label
96
BITE
97
To check or deactivate a system.
98
TLB or TLB-DD
99
within 180 days
100
Remove the failed component and install a balace weight to that position.
RENEW
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chia-chun Fang · 12問 · 1年前RENEW2024_6
RENEW2024_6
12問 • 1年前問題一覧
1
Saving will occur both in fuel usage as well as crew time and increase airspace
2
GMM
3
GMM
4
static source error correction
5
near pitot/static
6
FL290-FL410
7
Pitot tube
8
AOA,TAT,Pitot probe ,static port
9
"BITE may be used for fault isolation and trouble shooting."
10
"To be dispatched for a non-RVSM airspace is allowed."
11
72 hours
12
"malfunction of aircraft equipment and operational errors"
13
ALL
14
approved tester on the RVSM Maint program
15
Any structure repairs or modification around pitot/static probes , altimeter accuracy check and pitot-static leakage check
16
Do a leakage check
17
A/P ALT Mode ,ADC,ATC,ALT ALERT
18
QA
19
1000 feet
20
MEL
21
發動機總使用時間
22
26年
23
Level 1
24
三個月
25
七年
26
從飛機製造廠出廠時間
27
十四年
28
五年
29
M9
30
MS
31
M8
32
Maintenance personnel shall inform Maintenance Operation Center and the next station via telex on the current status of the CAT capability. The flight crew shall be informed orally.
33
contact Maintenance Operation Center to determine the actual aircraft status
34
The latest AUTOLAND operation date + 28days
35
Minimum Equipment List
36
Fail safe
37
The TLB shall indicate which action caused the upgrading.
38
DH is the wheel height above the runway elevation
39
sensors and computers must be separated, but also the electrical and hydraulic power supply and even all electrical wires.
40
100 ft
41
CAT II/III Maintenance Program operation and CAT II/III system maintenance audit.
42
An automatic landing system is the only equipment providing automatic control of the aircraft during the approach and landing and is not related to particular weather condition.
43
CAT II / III authorized maintenance only.
44
Airworthiness Directive affects the CAT operation.
45
Perform maintenance actions or inspections to determine the aircraft CAT status in accordance with fleet MEL.
46
To trace and analyze the reliability of CAT II/III systems/components and provide recommendations for improvements.
47
Significantly increase stall speed, reduce controllability, and alter aircraft flight characteristics.
48
SAE specifications.
49
"The latest revision of Aircrft Maintenance Manual."
50
The holdover time starts with the first application of anti-icing fluid.
51
De-icing.
52
Anti-icing.
53
heated.
54
To prevents the accumulation of frost, ice, or snow on a clean airplane surface for a certain period of time called holdover time.
55
fluid type, fluid name and dilution concentration.
56
The local time of de/anti-icing operation commenced and Result of Post De/anti- icing Check.
57
True.
58
Pilot-In-Command or designated Maintenance Representative.
59
Glycol.
60
Only the last leg time
61
0.20 QT/HR
62
Add oil/accumulated APU hours since last oil full service
63
OCR confirmation or maintenance action is required to entry into TLB.
64
Pre-Departure Service Check
65
APU can perform in-flight start test at return (to home base) portion of non- ETOPS flight
66
Cargo compartment fire suppression capacity be suitable for the duration of the approved diversion time plus 20 minutes
67
4 hours
68
Check cargo compartment liners for tears and punctures.
69
In case of no system abnormal and no “M” procedure (for DD) required to be performed for the flight. No need to do PDSC check again, but check oil consumption rate is mandatory.
70
120 min.
71
Performed by one mechanic and inspected by any other additional one mechanic.
72
Configuration, Maintenance and Procedures
73
VHF1 system unavailable during flight.
74
12 months
75
12 months
76
Extended Diversion Time Operations
77
Human error
78
Never, until the cause has been determined
79
WDM.
80
"Tightened by hand plus a maximum 1/8 turn more."
81
SWPM
82
De-icing fluids
83
Hydraulic oils
84
AMM and SWPM
85
SWPM
86
TSM
87
Electrical Wiring Interconnection System
88
Normally available lighting
89
"Open the circuit breaker of the safety sensitive system"
90
Up or forward
91
to allow for drainage of moisture
92
SWPM and ESPM
93
continuity check
94
WDM and AWM
95
Tools should have the certification acceptance recorded on the Tool Record Card or Tool Label
96
BITE
97
To check or deactivate a system.
98
TLB or TLB-DD
99
within 180 days
100
Remove the failed component and install a balace weight to that position.