Week 1 Flashcards

(117 cards)

1
Q

How often are A checks?

A

600 hrs +- 50

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2
Q

How often are C checks?

A

12 months +- 1 month

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3
Q

Are CB’s mandatory or advisory?

A

Advisory

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4
Q

Are alert CB’s mandatory or advisory?

A

Mandatory

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5
Q

How do we troubleshoot?

A

CMP diagnostics

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6
Q

Where is the CDL (config deviation list) found?

A

Appendix B of the AFM

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7
Q

If not in the MMEL, must an item be operative for flight?

A

Yes, unless can be found in CDL

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8
Q

What do arrows at the end of wires mean on WDM’s?

A

Wires are physically pinned on the aircraft (poke home)

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9
Q

What is the difference between how hard breakers are soft breakers are drawn?

A

Hard breakers have crosses on top

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10
Q

How are relays and switches always drawn?

A

In the relaxed (de-energised) position

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11
Q

What are cockpit clocks required for?

A

Timed flight manoeuvres

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12
Q

When engaged, what does the crew restraint system prevent?

A

Forward movement

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13
Q

How long does the pax seat ECU need prior to working?

A

20 mins

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14
Q

What type of hydraulic system do the pax seats have?

A

Closed

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15
Q

What colour wires are fibre optic?

A

Purple

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16
Q

What must be avoided when using fibre optic cables?

A

Exceeding bend radius

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17
Q

What frequencies are ELT transmitted on?

A

121.5, 243.0 MHz

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18
Q

When are ELT’s tested?

A

5 past the hour

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19
Q

What two things can flashing ELT’s mean?

A
  • On indication

- Fault indication

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20
Q

In the MMEL, what does an M mean next to the resolution?

A

Maintenance action required prior to flight

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21
Q

What must customers use for part numbers?

A

The IPC

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22
Q

Where can’t crocodile clips be used for ESD grounding?

A

MAU’s and MRC’s

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23
Q

What is essential for a seat belt inspection?

A

Adequate lighting

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24
Q

What is to be pulled on the EBATT’s prior to maintenance or for down time of 5 days or greater?

A

CB1

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25
How many primary control surfaces when on EBHA power?
7
26
Which BPCU’s control AC and DC power?
- Left - AC | - Right - DC
27
What is the UPS battery used for?
Flight control system
28
When do EBATT’s kick in?
20V DC or less from main batteries
29
When turning main batteries off, how long should you wait before reapplying power and why?
2 mins for CMC shut down
30
Which battery should be selected on first? EBHA or UPS?
EBHA prior to UPS?
31
When does the EBHA heater pad come on?
Below 60 degrees Fahrenheit
32
Where does the ON light for the batteries get it’s signal?
Battery contactors
33
What battery is required for APU start?
Left main
34
How many stick shaker operations during EBHA SPOST?
8
35
Where does the TRU overtemp discrete originate? What temp does it operate? And where does it travel on its way to CAS?
- TRU itself - 310 degrees Fahrenheit - Via the DGIO to CAS
36
How is the ground service bus powered? (Three ways)
- Right main DC bus - External DC - RH battery
37
Where does the only RED power fail CAS message originate?
RAT door switch
38
What can do not do with the GCU whilst the APU is running?
Reset or remove
39
When is RAT deployment effective?
Between 0.925 Mach and 172 knots
40
How is the RAT deployed? And stowed?
- Stored actuator pressure | - Hand pump
41
What is aircraft power system priority?
- Onside - APU - External - Offside Essential over main Left over right
42
What must be ensured when stowing the rat?
Blade alignment lines are aligned
43
Where are power tiles loaded from? And where is the information kept?
MCDU and RIU’s
44
To pull SSPC breakers prior to powering aircraft, what mode must you be in? And to perform SSPC data loads, what mode must you be in?
- Standby
45
If overcurrent occurs from LEDC TRU, where is the power pulled from?
L BPCU
46
Where is external DC power monitored?
R BPCU
47
What are the emergency batteries looking for?
Voltage at essential DC bus
48
To close the MED with no batteries installed, what must we do?
- Ext DC power cart | - Battery switches off
49
To power the right essential battery bus, which contactors does power travel through?
- REDXC | - REDC
50
What type of bus is between the MAU and the DU?
Fibre (fee bray)
51
What bus is between the CCD and MAU for DU operation?
RS 422
52
What is the backup for CCD movement? What do they operate through?
- SMC | - Operate through control I/O
53
How do we get audio?
- Analog to digital conversion at NIM through digital audio bus - information goes to audio control panel - Digital to audio conversion and sound through speaker
54
How does the FDR collect data?
From custom I/O module on arinc 717 bus
55
How long does the event record button cause the aircraft to record for?
100 seconds before and after event
56
What are the 4 types of voice communication?
- VHF - HF - Satellite - In flight
57
How long does the CVR record for?
2 hours on loop
58
What 4 locations does the CVR record from?
- ACP 1 - 3 | - Area mic
59
What parameters are needed for CVR bulk erase?
- WOW | - MED open
60
What does RIPS provide to the CVR?
10 mins of power
61
What does RVSM dictate?
- reduction in vertical flight separation from 2000 to 1000 ft separation between FL 290 to FL 410
62
TAT probes 1 and 2 are powered by which Air Data Systems?
- 1 = 1 | - 2 = 4
63
In air data systems, if secondary channel fails, what colour CAS message do you get? If primary channel fails, what colour CAS message do you get?
- Secondary - amber | - Primary - cyan
64
Where does SMC receive air data from?
ADS 4
65
Where is the satellite interface unit located?
Tail compartment
66
Where is the Nav com module located?
REER mini cabinet
67
Where is barometric correction made?
The flight guidance panel
68
Why don’t we touch air data probes?
Get extremely hot and cause harm
69
Where are the aircraft personality modules located?
NIC/PROC’s 1 and 4
70
How many GPS systems are required for position and height?
- position = 3 | - height = 4
71
What does WAAS (wide area augmentation system) compliance do in GPS antennas?
Removes errors from GPS satellites
72
Where is the FMS software?
MAU NIC/PROC’s 2, 5, and 6
73
What does EGPWS prevent?
CFIT (controlled flight into terrain)
74
Which EGPWS function can’t be disabled?
Wind shear (mode 7)
75
What types of wire from EVS to processor and from processor to HUD computer?
- EVS to processor = fibre optic | - Processor to HUD computer = coax
76
EVS sapphire window has what length heating cycle when selected?
2 mins
77
What is unique about the EVS camera image?
Inverted
78
What does the NUC (none uniform correction) do in the EVS system?
Calibration and cooling of light sensors
79
What is the minimum permissible exposure distance for WX?
15 feet
80
What type of system in the WX?
X band
81
Where is the weather radar controlled from?
SMC (pilot and copilot independent)
82
In the AP system, which servo does pitch and which does roll?
- left = pitch | - right = roll
83
In the AP system, which AIOP lane commands, and which monitors?
- A = monitor | - B = command
84
How often is RVSM inspected?
24 months
85
Where is the CMC card?
MAU slot 11
86
What does CMC do?
Stores all fault history
87
Where is the CMC member system database?
LDI (loadable diagnostic information database)
88
Where does the ground maintenance test switch sends a discrete to where?
SGIO 1 and 4
89
What is CMC used for? 3 answers
- testing - real time data - rigging
90
How long is the CMC power up time?
2 mins
91
Where is the ACMF (aircraft conditioning monitor function) located?
CMC
92
Where is the auto throttle engage/disengage button located?
Aft side of throttle quadrant
93
Where is pitch and roll manually input to AP?
Flight guidance panel
94
If CMC is not available on DU2 but is available on DU3, what failure do you have?
RIB (remote image bus)
95
Where is the IRU alignment data stored?
Configuration modules
96
How is the IRS powered?
On switch removes the ground discrete to turn on IRU’s
97
Where is the attitude heading reference system (AHRS) used?
For flight information on the SMC’s
98
Where are the magnetometers, what are they used for, and what type of bus do they communicate on?
- located in aircraft tail - used in the AHRS system - communicate on the CAN bus
99
What is the primary source of altitude information?
RADALT between -20 and 2500 feet
100
How do you recalibrate the RADALT?
- press SW1 switch and watch the display go from 500ft to 0
101
How do you test RADALT?
Use SMC and watch figure go to 50 feet
102
When do you get 60hz power and why?
Only when something plugged in to sockets to provide ground discrete to the RIU’s. To prevent unnecessary power in oxygen rich environment
103
To enable SSEC (static source error correction), what configuration must the aircraft be in?
Power off
104
What provides the ground discrete to the APU ready light?
APU door fully open
105
How many consecutive APU start attempts can you carry out?
3 then must wait an hour?
106
What monitors x tie contactors?
Opposite side BPCU’s
107
How many buses comprise the ASCB (avionics standard communication bus)?
4 total - #1 primary and secondary - #2 primary and secondary
108
Cabin view is not receiving nav information. Where might our problem be?
The FMS maintenance data server
109
What type of bus is between GCMS and the cabin components?
Ethernet
110
If any of the TRU’s fail, what happens to cabin power?
Cabin power would drop off
111
If the remote terminal for CMC doesn’t work, what could be the problem?
The incorrect CMC software version is not installed on the remote terminal
112
What breakers have to be pulled to protect CMC when removing the EBATT’s?
MAU 1B primary and secondary
113
Before pulling the CMC card from the MAU, what breaker needs to be pulled?
EBATT CB1
114
Where would you download unsent AHTMU data from?
Directly from the AHTMU, via Ethernet cable into the maintenance laptop
115
If the AHTMU is up and running, why might it not record?
Avionics standard communication bus (ASCB) not up and running yet
116
What profile allows the operator to set specific settings on the aircraft?
The operator profile (OP)
117
The crew reports a P2 and P3 fault. What could be the issue?
Faulty SIM card