ACFT systems Flashcards

1
Q

What materials are used in the construction of the EC fuselage

A

Aluminium
Composite material
Acrylic plastic
Titanium

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2
Q

3 main sections of the fuselage

A

Cabin structure
Main fuselage structure
Rear structure

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3
Q

Cabin roof is composite material, there for is a _____ area

A

No step

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4
Q

The body structure which carries the flight and landing gear is composed of?

A

Aluminium alloy

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5
Q

The primary function of the centre post is to _______

A

House vertical push rods

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6
Q

In forward flight the horizontal stabiliser creates a down force which will then pitch the aircraft ___

A

Up

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7
Q

Stabilises and tail bumper are cantered too one side in order too _____

A

Provide lift to counter torque of main rotor

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8
Q

Cargo door can only be operated from ______ the aircraft

A

Outside

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9
Q

Purpose of “spoiler position”

A

Allow increased speed with main cabin doors open

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10
Q

Cockpit doors are only to be jettisoned after _____

A

Touchdown

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11
Q

All 6 doors are made of _____

A

Composite material

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12
Q

In emergency, can the entire main cabin door can be jettisoned?

A

No

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13
Q

The gas springs on the cockpit and cargo doors are used to hold the doors _____

A

Open

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14
Q

The main cabin doors can only be locked in the closed position T/F

A

False

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15
Q

Maintenance steps must be ___ in order to prevent damage when opening

A

Flush / closed

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16
Q

3 hand operated panels that are located on each side of the fairing assembly are:

A

Transmission
Forward engine panel
Aft engine panel

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17
Q

Fuel filler neck access door must be opened with a _____

A

Key

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18
Q

An open engine cowling hatch will display?

A

Red

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19
Q

The external power receptacle access door/point should be opened with your ____ and has a _____ connection point

A

Hand
Inter communications system

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20
Q

Landing gear provides a mounting point for what 3 other items?

A

Wire deflector
Emergency floats
Ground handling wheels (manta ray)

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21
Q

How are the landing skids attached?

A

Shoes with clamping rings

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22
Q

Height of landing gear

A

Intermediate

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23
Q

The skids are installed on the landing gear to provide a _____ for the landing gear

A

Sacrificial wear surface

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24
Q

Grounding straps electrically connect the fuselage to the cross tubes and the cross tubes to the _____

A

Skids

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25
Function of wire strike system
Provide measure of protection against collision with HORIZONTALLY strung wires and cables
26
Cockpit seat have a ____ point harness
5
27
Cabin seats have a ____ point restraint harness
4
28
Can cabin seats be adjusted forward/ aft and vertically by crew?
No
29
Cockpit seats have a _____ shoulder harness inertia reel
Lockable
30
Characteristics of Martin Baker
Four point restraint harness Shoulder belts with lockable inertia reel Rotatable 360
31
Can you store under seats?
No it’s prohibited
32
Max floor loading is _____
600 kg/m2
33
Common feature of cockpit and MB seat
Crash attenuating
34
3 sections of instrument panel from L-R
Left hand section Centre section Right hand section
35
Top to bottom L/R hand display
Primary flight display Navigation display
36
2 indications available in cockpit for the firs detection system
Visual and Audio
37
How many fire detectors on each engine
2
38
Purpose of fire wall
Contain fire
39
How many bottles of extinguishing agent
1
40
Where are the fire detection elements located?
Under the starter generator Under combustion chamber casing
41
Will pressing fire button always release the extinguisher agent
No
42
Where are the float circuit breakers located?
Essential bus 1 and 2 on the overhead panel
43
What additional item is fitted on skids with hoist and floats fitted?
Cable deflector
44
Purpose of HEEL system
To guide crew to exits in emergency
45
Extinguishing agent in portable extinguisher
HALON
46
Frequencies for ELT
121.5 MHz and 406
47
Acceptable band for portable extinguisher
Green
48
Location of first aid kit
Clam shell door, LH side
49
Purpose of cockpit camera
Record video and audio
50
Where to view cockpit camera
Only on the ground through playback software
51
When is HEEL activated if EMER EX LT switched to arm
Crash, total power lost and contact with water
52
Where is the CVFDR located
On tail boom, underneath the left hand side engine cowl
53
The purpose of the data transfer unit is to?
Record maintenance data
54
MARMS is used for?
Records and stores flight data and usage monitoring of components
55
Does the cockpit camera send information to the CVFDR
No
56
CVFDR will record voice for____
CVFDR will record cockpit voice for 120 minutes
57
Data transfer unit records the UMS data on a ________
PCMCIA card
58
Venting lines allow the equalisation of _______ across the different tanks
Pressure
59
Thermal expansion will cause excess fuel to flow into the ______
Expansion tank
60
Difference between RH engine and LH engine
RH 4.5kg less
61
Total fuel in all tanks? Unusable fuel?
568kg 7.6kg
62
If we burn 200kg/h how much fuel will we burn a minute
3.3 kgs / min
63
Which supply tank has foam in it and why?
RH side, engine 2 So flame out of engines doesn’t occur at the same time
64
Crash worthy adaptations of EC135 fuel system
Flexible bladder Flexible hose Suction fuel feee Fuselage structure Fuel supply shut off
65
Fuel is provided from the main tank to the 2 supply tanks through the use of _____
Transfer pumps
66
Fuel is provided under pressure from the supply tanks to the engines during the start by the ______
Prime pumps
67
The F PUMP AFT/FWD caution light appear after ____ with no fuel pumped
3 minutes
68
Secondary fuel shut off
Depress the EMER OFF SW (Fire)
69
Once an engine has been started turning the Prime pumps will cause?
Do nothing as the engine will now draw fuel from the supply tank on its own
70
Fuel remaining in tanks with “Fuel” caution and “low fuel” warning
Caution: 36kgs for 1 or 32kgs for 2 Warning: 32 for 1 or 28 for 2
71
Flight time when low fuel warning light comes on
10 minutes
72
If the CAD lane fails what would your indicators be on remaining fuel quantity
Audible gong
73
If CAD displays 300kg of fuel but low fuel warning has come on which is assumed to be correct
Low fuel
74
Can you see the white position light when the EC135 is flying directly at you
No, it’s located rearward
75
What EC135 lights are NVD compatible
Position lights, anti collision, formation lights
76
Which light can be slewed
Search light (not landing light)
77
Do both landing lights and search lights have an IR operating mode
No, only search light has an IR mode
78
Hoist light is located next to the ____
Hoist/ standby switch/button