問題一覧
1
Which of the following will disengage the autopilot?
Activating a manual pitch trim switch
2
With ICING set to OFF in the MCDU, the anti-icing system turns on during takeoff
icing conditions encountered aircraft above 1700 feet or 2 minutes
3
The pressurization system consists of
All the Above
4
During rollout, the maximum deflection of the Multifunction Spoilers is
45 degrees
5
When the RAT is the only AC power source, the flight control system is subject to the following conditions:
All of B,C, and D
6
During flight, with HYD selector knobs in AUTO, when does the system 1 electric hydraulic pump operate continuously?
Both B&C
7
What is the maximum allowable fuel imbalance?
794 pounds
8
The electric PBIT is performed after aircraft is powered by
Any AC power source and takes approximately 3 minutes to complete
9
What is the bleed system priority in flight?
Onside engine, opposite side engine, APU (if available)
10
During a go-around, pitch up is limited to
between 8° and 18°
11
When Multifunction Spoilers are deployed for use as speed brakes, the maximum deflection is on a gain schedule based on airspeed.
true
12
Only one ice detector must be operable for detecting icing conditions and activating engine and wing anti-ice.
true
13
During takeoff and landing with the PTU switch in the AUTO position, with the flaps out of zero, the PTU:
is activated by system logic if engine 2 fails or engine 2. EDP fails and gear lever is selected UP or DOWN
14
What is the electrical power source for the engine fire protection?
Hot battery bus
15
Normal hydraulic system pressure is
3000psi
16
How many aircraft engine fire bottles are installed on the aircraft not including the APU
2
17
The HYD system 3 Unloader valve and Flow Limiter valve are used to
Avoid overloading the RAT during an electrical emergency
18
How many smoke detectors are installed in each cargo compartment?
3 in the forward and 2 in the aft
19
What is the EMB-175 maximum operating altitude?
FL410
20
What will happen if a generating IDG source fails?
Bus ties will automatically connect to ensure no system degradation occurs
21
With both IDG and the APU generators offline, the RAT will power.
The AC Standby Bus via the AC Essential BUS
22
With pressurization in manual mode, cabin altitude can be increased by
opening the outflow valve
23
The DC GPU receptacle is used for APU start when
Both A&C
24
When the Pressurization Dump Button is pressed,
D.Both A&C
25
What is the priority of the pitch trim system?
Backup, Captain, FO, Autopilot
26
The flight control system operates under which two modes?
normal and direct
27
The Smart probes and TAT probes are heated
When an engine is running
28
The minimum engagement altitude for the autopilot per Mesa Airlines policy is
1000’ AGL
29
Pulling the fire extinguishing handle (T-handle) is all that is required to discharge the fire bottle into the main engine compartment.
only on the ground
30
What is purpose of the scavenge pumps?
maintains fuel level in collector tank
31
One IDG can supply the entire electrical system.
true
32
After starting engine 1 and parking brake released, the electric hydraulic pump 2 automatically comes on to provide
Both A&B
33
The EMB-175 with enhanced winglets has a wingspan of
93’11”
34
The maximum takeoff weight of the EMB-175 is
85,517
35
When does the FADEC provide engine start protection?
Only on the ground for hot start, hung start, or no light-off
36
The number of Primary ACE units on board the aircraft is
3
37
What is the only primary flight control that is NOT fly-by-wire?
ailerons
38
Is a single pack capable of providing adequate temperature control and pressurization?
Yes up to Fl310
39
The emergency RAM Air valve opens when
In flight below FL250 and both ECS packs are off or failed
40
With no active AC source of power, how long will the main aircraft batteries last?
10 minutes
41
What is the EMB-175 maximum landing weight?
74,957
42
The purpose of the Transformer Rectifier Units (TRU) is to convert
115v AC to 28V DC
43
What is the purpose of the collector tank?
Both A&C
44
The minimum runway or taxiway width required for a 180 degree turn is
59’2”
45
The ATTCS (Automatic Takeoff Thrust Control System) provides
Maximum reserve thrust in the event of an engine failure
46
The number of FCMs on board the aircraft is
4
47
What will cause the amber light on the overhead panel to illuminate?
High oil temperature/low oil pressure
48
The primary ejector pumps are driven by what energy source?
Motive flow
49
HYD system 1 and HYD system 2 are able to mix in the bootstrap reservoir via the system filter casing.
False
50
Maximum Rudder deflection (without gain scheduling) is
30 degrees
51
Maximum differential over pressure is
8.8 PSID
52
The number of fire bottles installed for use in both cargo compartments is
2
53
If an engine fails, do both left and right wings receive anti-ice protecion
Yes, the crossbleed valve opens to provide symmetrical protection to both wings
54
When the HYD system 1 and 2 engine driven pump shutoff buttons are pressed, the:
Both B&C
55
With Battery 1 ON and Battery 2 in AUTO during initial power-up, which items will be available?
DU 2 & 3, IESS, clock, MCDU 2, CCD 1, mag compass light, backup trim switch
56
Ground Spoilers deploy when
only A&B
57
The Power Transfer Unit (PTU) uses HYD 1 system power to provide HYD 2 system pressure.
True
58
If fuel indication is 500 pounds high in the right tank the pilot should
turn the X-feed switch to Low 1