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Revision 6315 Super Quiz

Total questions: 25

Worksheet time: 15mins

Name
Class
Date
1.

The High Oil Temperature Switch in the transmission monitoring system, will indicate what alert at what temperature

a)

Green Advisory at 2.4 bar

b)

Amber warning at 110 degrees F

c)

Red Warning caption at 110 degrees C

d)

Amber Caution at 2.4 PSI

2.

How is a fire wire constructed

a)

Stainless steel capillary tube, copper wire conductor, paper filling

b)

Rubber capillary tube, nickel chromium steel central electrode glass and aluminium filling

c)

nickel chromium steel central electrode, glass and aluminium filling, copper capillary tube

d)

nickel chromium steel central electrode, glass and aluminium filling, stainless steel capillary tube

3.

With refence to maintaining fire wires, which statements are correct?

Select one or more of the following

a)

Elements found un capped are treated as serviceable

b)

All bends must exceed 1 inch

c)

Grease must to applied to coupling joints

d)

Replacement elements must be of the correct type

4.

With reference to maintaining a fire wire, which of the following statements are true?

Answer one or more of the following.

a)

An insulation test must be carried out for the longest time necessary to obtain a reading, to avoid polarisation of the firewire element

b)

When reconnecting, new copper crush washers must be fitted

c)

All firewire couplings must be correctly torque loaded.

d)

Bends must not commence less than half an inch from any clip or connection.

5.

With reference to the Merlin Fire Protection System.

Which of the following statements are correct?

a)

In a crossfeed system, Engine one is crossfed to 2 engine

b)

In a crossfeed system, Engine one is crossfed to APU

c)

In a crossfeed system, Engine one is crossfed to 3 engine

d)

In a crossfeed system, Engine 2 is crossfed to 2 engine

6.

Indication of an engine fire is indicated on which of the following components

Select one or more of the following answers

a)

CDS/IDU

b)

Aircraft Management System

c)

Engine Control Panel

d)

Master Warning Light

7.

Which of the following components can be utilised as aircraft sensors for a CWS?

Select one or more from the following answers

a)

Micro Switch

b)

Infra Red light

c)

Transducer

d)

Firewire

8.

The function of the Thermal Discharge is to indicate what?

a)

Low pressure of a fire Bottle

b)

Discharge of a fire bottle by normal operation

c)

Excessive pressure in a fire bottle to due overheating

d)

Inadvertant discharge of a fire bottle.

9.

With reference to EGRESS lighting, how is it operated? Select one or more of the following answers

a)

Loss of aircraft power when the system is selected OFF

b)

Inertia by a crash switch

c)

A freshwater activated switch

d)

A saltwater activated switch

10.

Which of the following are NOT examples of internal lights.

a)

Hoist Light

b)

Navigation Light

c)

Utility Light

d)

Hover Light

11.

With reference to windscreen anti-icing, how many temperature sensors are fitted to the pilots windscreen

a)

1

b)

2

c)

3

d)

4

12.

With reference to the Ice and Snow Detection system, what is the function of the measuring head.

a)

Detection of Ice

b)

Measure the rate of OAT

c)

Detection of Snow

d)

Measure the rate of Ice and snow formation

13.

With reference to Windscreen Anti Icing. The NORMAL channel cycles:-

a)

On at 24°C and Off at 30°C

b)

On at 44°C and Off at 50°C

c)

On at 24°F Off at 30°F

d)

On at 44°F and Off at 50°F

14.

With reference to the Wash/wipe system, the CREW switch can be selected to which position?

a)

OFF

b)

BOTH

c)

SLOW

d)

FAST

15.

With reference to the undercarriage. One of the functions of the WOW Micro-switches is to?

a)

Ensure the control handle can be selected whilst the aircraft is on the ground

b)

Lock the undercarriage in the up position when the aircraft is on the ground

c)

Lock the undercarriage in the down position when the aircraft is airborne

d)

Prevent inadvertent operation of the control handle when the aircraft is on the ground

16.

The RIPU can be assessed for serviceability by? Select one or more of the following answers.

a)

Carrying out a Start Up BIT

b)

Carrying out a shutdown BIT

c)

Carrying out a Serviceability BIT

d)

Carrying out a Continuous BIT

17.

With Reference to ECS . Conditioned Air and Pressurisation from the Air Distribution System is used to provide what? Select one or more answers

a)

flight critical and mission essential cooling

b)

defog control

c)

Conditioned air from the ACP

d)

supply air for protective flight garment supply systems

18.

With reference to a Fixed wing ECS, Primarily, what is used to cool mission systems? Select one or more correct answers

a)

An Air Liquid Loop

b)

A Hot Liquid Loop

c)

A Conditioned Liquid Loop

d)

A Cold Liquid Loop

19.

With reference to the Bladefold/Spread System. Which component will locate into the lugs of the swashplate

a)

PLRA

b)

RIA

c)

FCPA

d)

PLLA

20.

With reference to the Bladefolds/Spread Indication System. Which indicator will illuminate when the operator presses the master switch

a)

FAIL

b)

ON

c)

READY

d)

SECURE

21.

With reference to the Bladefold/Spread system. What component is used to rotate the Main Rotor Head

a)

FCPA

b)

PLLA

c)

RIA

d)

FMU

22.

With reference to Transmission Systems, What indication would the pilot get if oil pressure falls below 2.4 bar (Select one or more of the following)

a)

Warning

b)

Caution

c)

Advisory

d)

Audio message

23.

Polyalphaolefin (PAO) is used to cool what systems? Select one or more of the following answers

a)

Fuel Pumps

b)

RADAR

c)

Pilots G Suit

d)

PTMS Controller

24.

What is the function of the Electric Pump in the hydraulic system,

a)

Keep No3 hydraulics pressurised

b)

Top up the Emergency Accumulator

c)

Operate the Changeover Solenoid

d)

Crossfeed No3 System to No 1 or No 2 System

25.

The rescue hoist is controlled by?

a)

The cabin controller on the inter-seat console

b)

Switches on the Cockpit and Cabin

c)

No3 Hydraulic System

d)

Hydraulic Valves in the Cockpit