- Hydraulic , Landing Gear and Flight Control.
- Pneumatic , Aircondition and Vacuum system.
- Engine - Starting and Ignition
- Fuel and Fire Protection.
The syllabus for EASA are as follows...
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13.7 Flight Controls (ATA
27)
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(a) Primary controls: aileron,
elevator, rudder, spoiler;
Trim control;
Active load control;
High lift devices;
Lift dump, speed brakes;
System operation: manual,
hydraulic, pneumatic;
Artificial feel, Yaw damper,
Mach trim, rudder limiter, gust locks.
Stall protection systems.
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-
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-
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2
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(b) System operation:
electrical, fly by wire.
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-
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-
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3
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13.11 Air Conditioning and
Cabin Pressurisation (ATA 21)
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13.11.1 Air Supply
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-
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-
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2
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Source of air supply including
engine bleed, APU and ground chart
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13.11.2 Air Conditioning
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Air Conditioning Systems;
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-
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-
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2
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Air cycle and vapour cycle
machines;
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-
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-
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3
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Distribution systems;
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-
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-
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1
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Flow, temperature and humidity
control system;
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-
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-
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3
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13.11.3 Pressurisation
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Pressurisation systems;
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-
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-
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3
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Control and indicating
including control and valves;
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Cabin pressure controllers;
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13.11.4 Safety and warning
devices
Protection and warning
devices.
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-
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-
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3
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13.12 Fire Protection (ATA2
6)
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(a) Fire and smoke detection
and warning systems;
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-
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-
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3
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Fire extinguishing systems;
System tests.
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(b) Portable fire extinguisher
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-
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-
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1
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13.13 Fuel Systems (ATA 28)
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System layout;
|
-
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-
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1
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Fuel tanks;
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-
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-
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1
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Supply systems;
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-
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-
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1
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Dumping, venting and draining;
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-
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-
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1
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Cross-feed and transfer;
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-
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-
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2
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Indications and warnings;
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-
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-
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3
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Refuelling and defueling;
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-
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-
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2
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Longitudinal balance fuel
systems;
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-
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-
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3
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13.14 Hydraulic Power (ATA
29)
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System lay-out
|
-
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-
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1
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Hydraulic fluids;
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-
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-
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1
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Hydraulics reservoirs and
accumulators;
|
-
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-
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1
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Pressure generation,
electrical, mechanical, pneumatic;
|
-
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-
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3
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Emergency pressure generation;
|
-
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-
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3
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Filters;
|
-
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-
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1
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Pressure control;
|
-
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-
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3
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Power distribution;
|
-
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-
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1
|
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Indication and warning
systems;
|
-
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-
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3
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Interface with other systems;
|
-
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-
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3
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13.15 Ice and Rain
Protection (ATA 30)
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Ice formation, classification
and detection;
|
-
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-
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2
|
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Anti-icing systems:
electrical, hot air and chemical;
|
-
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-
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2
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De-icing systems: electrical,
hot air, pneumatic, chemical;
|
-
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-
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3
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Rain repellent;
|
-
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-
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1
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|
Probe and drain heating;
|
-
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-
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3
|
|
Wiper systems;
|
-
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-
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1
|
|
13.16 Landing Gear (ATA 32)
|
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|
Construction, shock absorbing;
|
-
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-
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1
|
|
Extension and retraction
systems: normal and emergency
|
-
|
-
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3
|
|
Indications and warnings;
|
-
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-
|
3
|
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Wheel, brakes, antiskid and
autobraking;
|
-
|
-
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3
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Tyres
|
-
|
-
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1
|
|
Steering
Air ground sensing
|
-
-
|
-
-
|
3
3
|
|
13.18 Pneumatic/Vacuum (ATA
36)
|
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|
System lay-out
|
-
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-
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2
|
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Sources; engine/APU,
compressors, reservoir, ground supply
|
-
|
-
|
2
|
|
Pressure control;
|
-
|
-
|
3
|
|
Distribution;
|
-
|
-
|
1
|
|
Indicators and warnings;
|
-
|
-
|
3
|
|
Interfaces with other systems;
|
-
|
-
|
3
|
|
13.19 Water / Waste (ATA
38)
|
-
|
-
|
2
|
|
Water system lay-out, supply,
distribution, servicing and draining;
|
|||
|
Toilet system lay-out,
flushing and servicing
|
|||
|
14.1 Turbine Engines
|
|||
|
(a) Constructional arrangement
and operation of turbojet, turbofan, turboshaft and turbopropeller engines;
|
-
|
-
|
1
|
|
(b) Electronic Engine control
and fuel metering systems (FADEC).
|
-
|
-
|
2
|
|
14.2 Engine
Indicating Systems
|
-
|
-
|
2 UNDER TURBINE ENG/ INDICATION
AJB 30503
|
|
Exhaust gas
temperature/Interstage turbine temperature systems;
Engine speed;
Engine Thrust
Indication: Engine Pressure Ratio, engine turbine discharge pressure or jet
pipe pressure systems;
Oil pressure and
temperature;
Fuel pressure,
temperature and flow;
Manifold pressure;
Engine torque;
Propeller speed.
|
|||
|
14.3 Starting and Ignition
Systems
|
-
|
-
|
2
|
|
Operation of engine start
systems and components;
|
|||
|
Ignition systems and
components;
|
|||
|
Maintenance safety
requirements
|
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