[Review] VNHS/VAR/AW189/MBDC – LEVEL B

The cabin door allows the opening and closing in flight at speed up to:

Which chapter is the retirment lives, mandatory inspection belong to?

Flight hours are caculated from:

The madatory inspection is permitted using inspection interval tolerances?

Which chapter is the time limits belong to?

The certification maintenance requirements are identified in:

How is the next inspection after using the inspection interval tolerance?

In chapter 05, the time limit is divided into:

Can the discard time schedule be applied the tolerance?

Conditional inspections are required after:

The helicopter can be lifted through a sling secured to:

Which circuit breaker of system has to be off before jacking the helicopter?

The helicopter must be weighed when:

What must be paid attention when weighing the helicopter?

Where is the leveling tool placed on the helicopter?

Who responsible for A/C gross weight?

Maximum speed limitation when taxiing on paved surfaces:

Maximum ground speed for wheel brake application:

Who responsible for taxiing?

The main rotor blades tie-down must be installed when:

Park the helicopter in a safe area when:

Which statement below is correct about main rotor blades tie-down:

The replaceable parts can be found in:

The inspection requirements, maintenance procedures, removal and installation procedures, test and inspection can be found in:

The airborne equipments which are mandatory to achieve a safe flight condition can be found in:

The transmission vibration monitoring (TVM) system is a specific number of devices, accelerometers located on:

The structure vibration monitoring (SVM) system is a specific number of devices, accelerometers located on:

Function of the ECS check valve:

When the temperature control valve is fully closed (during normal operation or if failed closed), a minimum heating air flow is provided through:

For automatic heating regulation in auto mode, heater control box (HCB) uses the temperature signal from:

The air duct temperature sensor monitors the mixed air temperature at:

When air temperature exceeds 85 oC, the HCB cuts 28VDC power to close the engine SOVs and APU SOV using the signal come from:

ICS operating modes:

The purpose of remote memory unit on the ICS system:

Which indications are there on cockpit audio control panel?

What bus bars are not supplied power if only one generator operated?

The APU can operate in flight or on the ground within:

The two Starter Generator Control Units (SGCUs) are located:

The starter-generator converter unit is capable of rectifying:

ECS bus is powered in flight:

Which LRU stops the start cycle of the starter generator, removing the start command from the SGCU?

Operation of the automatic deployable emergency locator transmitter:

In case of helicopter ground crash, automatic deployment of the crash position indicator beacon is activated by:

The CPI beacon is installed on:

Which light will illuminate on the ADELT CCP after ADELT is activated?

Which statement below is correct?

Function of temperature compensated pressure switch:

Fire extinguishing procedure after the fire in red illuminated in relevant engine or APU fire control panel:

Indications when engine fire:

Indications when APU fire:

What is the purpose of the flame arrestor?

What is the purpose of the non-return fuel valve?

What does the fuel quantity gauging system use as a reference to compensate for fuel density?

What is the purpose of the false connector?

How many high level fuel switches are there in fuel system?

What does CAS message “FUEL LOW FAIL” mean?

Where are the fuel pressure transducers which provide fuel pressure information?

If the fuel pressure in feed line drops below the preset value, which does activate the crossfeed valve (in auto crossfeed mode)?

Where is the fuel flow displayed?

What is the purpose of the by-pass restrictor?

TRSOV valve used to isolate:

The hydraulic electrical pump No.3 can operate:

The solenoid of TRSOV closing is energized by:

When hydraulic pump No.2 failed:

Hydraulic system 2 fluid level at 40%:

Hydraulic system 2 fluid level at 28%:

Hydraulic system 2 fluid level at 22%:

Hydraulic system 1 fluid level at 40%:

Hydraulic system 1 fluid level at 28%:

Hydraulic system 1 fluid level at 22%:

Electrical power of pitot heating elements:

What is the purpose of the ULB?

What happen to the CVFDR data if pressed ERASE button more than 2s?

On the CVFDR system, the tri-axial accelerometer simultaneously measure:

The CVFDR records voice data:

Which statement below are correct:

The nose landing gear:

Normal operation of the landing gears is performed by using:

Emergency extension of the landing gears is performed by using:

The nose landing gear is extended:

Which statement below are correct:

The main landing gear is extended:

Weight on wheels (WOWs) proximity switches are fitted on:

Which device controls the supply of the hydraulic fluid to the extending or retracting of the landing gear in normal and emergency mode?

Function of the safety plug on main landing gear wheels:

Function of the fusible plugs on main landing gear wheels:

Which statement below is correct?

On the miscellaneous control panel with the mode switch set to “night” position, what happen to the cockpit lighting?

CAS message “RH LDG LT ON” presented in green and the “LH LDG LT EXTD” presented in white indicate that the right landing light is on:

How can the pilot and co-pilot independently operate the onside landing lights?

What is the communications link between AMMS and the CDS?

The APU can operate the environment control system:

The axial expansion of the APU is permitted by the movement of:

The lateral expansion of the APU is permitted by the movement of:

The thermostatic valve is located (of APU fuel system):

The APU fuel filter is equipped with:

Function of the fuel metering pump (FMP):

Function of the fuel flow divider manifold:

Purpose of the de-oiling valve:

Function of high pressure relief valve:

The APU oil filter is equipped with:

The oil pressure switch:

The cooling air flow of air/oil heat exchanger (of APU) is provided by:

The APU bleed air can performed:

The crew door consist of:

The passenger doors consist primarily of:

The door is not monitored by position microswitch:

Function of cut out section on the horizontal stabilizer:

Function of the strake located on the left side of the tail boom:

The fuselage is divided into:

The main cabin is constructed of:

The connection between rear fuselage and tail unit by:

Function of the tail plane (or horizontal stabilizer):

The vertical fin improves the the aerodynamic stability along:

The cabin windows can be jettisoned in case of emergency by:

Material of the the flight compartment windshield:

The rotating controls consist of:

The AW189 main rotor blade is made predominantly from:

The components permit lead-lag, flap and pitch change movement of the MR blade is:

The main rotor hub is made of:

What is the function of the flapping limiter?

What is the function of the droop stop assembly?

What is type of the MR lag damper?

What is the function of the beanie?

The MRH azimuth sensor is installed on:

Which does the statement below indicate the function of the freewheel?

What are the purposes of the coupling assembly?

Which statement below is correct?

Which statement below about MCD of the MGB is correct?

Which following condition is not permit to use MGB fuzz burners?

The pilots can operate the fuzz burner to burn off any very small particles using:

The oil filter differential pressure transducer measures the difference in pressure between the oil filter inlet and outlet and generate:

Which following condition can activate the MGB low oil level switch?

Which is the most critical part in the input module?

In case of the loss of oil in the lubrication system, the emergency oil system will lubricate:

The rotor brake actuator caliper is automatically raised to the braking position when the aircraft is on the ground and:

When is the rotor braking operation permitted?

If the RBCL is moved from the off position with one or both engines in flight, which message will appear?

The components permit lead-lag, flap and pitch change movement of the TR blade is:

Which components transfer the rotating motion of the hub about the mast axis to the spider and slider assembly?

Which statement below about the TR pitch links is correct?

The function of the damper assembly:

The IGB is a bevel gearbox that changes:

The IGB and TGB lubrication oil is monitored by:

After 3 burn attempts, the chip still present, which message will appear on the CAS list?

The rotors flight control is transmitted:

Component provides the position of the collective lever to the electronic engines control unit (EECU):

The mixing unit combines the output from:

The load sharing on engine comprises:

The interturbine temperature (ITT) is designated:

The function of the scroll case:

The permanent magnet alternator (PMA) which makes the engine independent of the aircraft’s power generation systems once:

The differential pressure across the filter to activate the fuel filter bypass switch:

The engine maximum fuel flow is limited by:

Parameters are used for computation of engine fuel flow:

The primary NG signal for EECU comes from:

When the engine shutdown, fuel inside the manifold and injectors is blown back by:

Power is supplied to the ignition exciter assembly by:

Permanent magnetic alternator (PMA) has:

The variable geometry system components include:

At engine maximum power:

Starting bleed modulation is controlled as a function of:

The (T2) temperature signal is sent to the EECU for:

The P3 air pressure signal is sent to the EECU for:

The P0 sensor is used for:

All of the sump seals are pressurized by:

The air/oil separator is located in:

The backup NG signal for EECU comes from: