EASA PART 66 MODULE 11,P2- (Module 11.3 to 11.4)

EASA PART 66 MODULE 11 AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS PART 2
(11.3 Airframe Structures — Aeroplanes 11.3.1 Fuselage (ATA 52/53/56) 11.3.2 Wings (ATA 57) 11.3.3 Stabilisers (ATA 55) 11.3.4 Flight Control Surfaces (ATA 55/57) 11.3.5 Nacelles/Pylons (ATA 54) 11.4 Air Conditioning and Cabin Pressurisation (ATA 21) 11.4.1 Air supply 11.4.2 Air Conditioning 11.4.3 Pressurisation 11.4.4 Safety and warning devices)


11.3 Airframe Structures — Aeroplanes
11.3.1 Fuselage (ATA 52/53/56) 
Construction and pressurisation sealing;
Wing, stabiliser, pylon and undercarriage attachments;
Seat installation and cargo loading system;
Doors and emergency exits: construction, mechanisms, operation and safety devices;
Windows and windscreen construction and mechanisms.


11.3.2 Wings (ATA 57) 
Construction;
Fuel storage;
Landing gear, pylon, control surface and high lift/drag attachments.






11.3.3 Stabilisers (ATA 55)
Construction;
Control surface attachment.

11.3.4 Flight Control Surfaces (ATA 55/57)
Construction and attachment;
Balancing — mass and aerodynamic.

11.3.5 Nacelles/Pylons (ATA 54)
Construction;
Firewalls;

Engine mounts.

11.4 Air Conditioning and Cabin Pressurisation (ATA 21)
11.4.1 Air supply 
Sources of air supply including engine bleed, APU and ground cart;

11.4.2 Air Conditioning 
Air conditioning systems;

Air cycle and vapour cycle machines Distribution systems;
Flow, temperature and humidity control system.

11.4.3 Pressurisation 1 3
Pressurisation systems;
Control and indication including control and safety valves;
Cabin pressure controllers.

11.4.4 Safety and warning devices 

Protection and warning devices.

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  2. part 3 Air Conditioning and Cabin Pressurisation (ATA 21)

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