Pilot Training Manual Book Questions Flashcards
The EMB 120 is certified under:
Part 25
The EMB 120 has how many generators?
5
The EMB 120 forward entry door my be:
Raided and lowered manually
Raised hydraulically—lowered manually
The EMB 120 DV windows may be removed by the crew? T/F
True
If the main entry door is not securely closed and locked:
A door open light will illuminate in the cockpit
How many cycles can the forward entry door be operated without recharging its accumulator?
4
The EMB 120 has how many landing lights?
2
The EMB 120 has how many taxi lights?
2
Passenger cabin lighting is controlled by:
A 3 position switch located on the attendants panel
Taxi lights turn off automatically on landing gear retraction? T/F
True
The flight attendant my be called from:
The cockpit
The cabin
The lav
The emergency lights come on if:
The cockpit switch is in ARM and the EDC bus 1 fails
The cockpit switch is placed to ON
The attendants switch us placed to ON, regardless of the position of the cockpit switch
What warning systems does the EMB 120 have?
Visual
Aural
Vocal
The color of the alarm/indication system lights are:
Red and green
Amber and white
Visual alarm light dim levels are controlled automatically? T/F
False
How many power sources does the multiple alarm panel have?
2
Does the crew how the ability to lower the volume of the aural warning system?
No
The total usable fuel capacity is:
5732 pounds
The fuel system consists of what kinds of fuel pumps and how many of each?
4 Electric boost pumps
4 Scavenger jet pumps
2 Main jet pumps
The firewall shutoff valve is operated through the:
Fire extinguisher T-handle
What color light indicates crossfeed operation
White
When pressure fueling, the airplane must be electrically powered? T/F
False
APU fuel used goes through the fuel totalizer? T/F
True
What happens when fuel flow indicators loose power?
Digital indication goes blank
The APU provides a source of
Pneumatic and electrical power
Can the APU receive fuel from the left fuel tank?
Yes
The APU will automatically shutdown if rotating parts exceed
110%
During the APU start cycle, what commands starter disengagement?
ECU
Can the APU be operated in flight?
Yes
What engines does the EMB 120 have?
Pratt-Whitney 118 A/B
The engine has how many compressors?
2
The engine has how many turbines?
4
The engine power control is accomplished by the operation of
A combination of the EEC and the HMU
The device that provides essential fuel control functions in the absence of electrical power is
Hydromechanical metering unit (HMU)
The maximum torque allowed is
110% for 5 min
The EEC is normally used in what positions?
TO or ON positions
If the EEC light on the glareshield illuminates, this indicates
An electrical failure exists in the system
Which turbine provides power to the propeller shaft?
Power turbine
Maximum continuous torque
100%
Maximum continuous engine RPM
100%
Minimum oil temp for takeoff
45C
Oil pressure alarm light illuminates at
40 PSID
Condition lever positions are
MAX RPM
MIN RPM
FEATHER
FUEL CUT-OFF
The PW118 combustion section is defined as
Reverse flow annular combusor
Power lever movement provides direct control to
HMU
During engine start, with the ignition system set to AUTO
The igniters come on automatically
The igniters go off automatically
What if any indication does the pilot have to indicate that the engine igniters are energized
A white ignition light on the start/ignition panel will illuminate
After initiation the start cycle is automatically interrupted at approximately
50% Nh
How is the fuel heated
Engine oil
How many compressor bleed ports does each engine have?
2
How is fuel flow to the engine metered?
HMU/EEC
Failed fixed is a function of
The EEC
When does the EEC control function activate?
25% Nh
If the gust lock is set, power levers are restricted in movement? T/F
True
The condition lever has free movement from feather to fuel cut-off? T/F
False
Engine compressors are axial or centrifugal?
Centrifugal
The free power turbine is
A two stage axial flow
What are the engine bleed ports called?
P 2.5
P 3
Who makes the propeller
Hamilton-sundstrand
I’m normal operation, maximum governed propeller speed is
1300 - 1309 rpm
Normal operational pitch range is
79.2 (feather) to -15 (reverse)
In flight, Np is controlled by
PCU and condition lever
The main component for selecting propeller pitch is
PCU
The main component for changing propeller pitch is
Propeller servomechanism
If through a malfunction the propeller become fixed pitch, what items control Np
Power and speed changes
During taxi and reverse, which unit controls Np?
EEC
Pitch lock is term used to describe
A device which lock the propeller pitch in flight of the propeller oil pressure is lost
Which controls input sets the propeller speed
Condition lever
When operating in the beta range
The speed governor system has no control of propeller pitch
The beta valve position is adjusted by the
Power lever
Propeller blade angle at flight idle
17.6
In flight, if the engine has failed and propeller has not been feathered, it will then automatically feather? T/F
False
If an approach with autofeather armed and engine fail, with its propeller autofeather
No
Propeller syncs us activated by
System selected on and Np > 80%
The main purpose of the least selector value is to
Select the proper speed governor
(Normal or overspeed)
Engine bleed air is ducted from 3 separate ports? T/F
False
The duct leak warning system is activated when temperature is the duct region reaches
195* F
If a “duct leak” is detected, the bleed-air system will automatically shut off? T/F
False
If a “bleed overheat” is detected, the bleed-air system will automatically shut off? T/F
False
What prevents moisture from entering tubing or Deicers
A water separator system
Deicer boots are operated by pneumatic air flowing through
4 ejector flow control valves
