Skip to main content

Modules

List of modules:-

Module 1: Reserved

Module 2: Reserved

: ELECTRICAL FUNDAMENTALS

: ELECTRONIC FUNDAMENTALS

: DIGITAL TECHNIQUES ELECTRONIC INSTRUMENT SYSTEMS

: MATERIAL AND HARDWARE

: MAINTENANCE PRACTICES
 Note: This module does not apply to category B3. Relevant subject matters for category B3 are defined in module 7B.

: MAINTENANCE PRACTICES
 Note: The scope of this module shall reflect the technology of  aeroplanes relevant to the B3 category.

:  BASIC AERODYNAMICS

: HUMAN FACTORS
Note: This module does not apply to category B3. Relevant subject matters for category B3 are defined in module 9B.

: HUMAN FACTORS
Note: The scope of this module shall reflect the less demanding environment of  maintenance for B3 licence holders.

: AVIATION LEGISLATION

: TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS

: TURBINE AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
Note 1:This module does not apply to category B3. Relevant subject matters for category B3 are defined in module 11C.
Note 2: The scope of this Module should reflect the technology of aeroplanes pertinent to  the A2 and B1.2 subcategory.

: PISTON AEROPLANE AERODYNAMICS, STRUCTURES AND SYSTEMS
Note: The scope of this module shall reflect the technology of aeroplanes pertinent to the B3 category.

: HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS

: AIRCRAFT AERODYNAMICS, STRUCTURES AND SYSTEMS

: PROPULSION

: GAS TURBINE ENGINE

: PISTON ENGINE

: PROPELLER
Note: This module does not apply to category B3. Relevant subject matters for category B3 are defined in module 17B.

: PROPELLER
Note: The scope of this Module shall reflect the propeller technology of aeroplanes pertinent to the B3 category.

Comments

Popular posts from this blog

Cessna-152

What is Cessna-152: Cessna-152 is a small aircraft. This aircraft is one of the largest produced aircraft mainly used to provide pilot training and also for personnel use. Details: Cessna-152 is made on all metal semimonococoque, high wing construction. The wings are supported by wing strut so called as semi cantilever construction. Landing gear: tricycle type with Fixed main landing gear and oleo pneumatic nose landing gear Seating Capacity: Two seat  Fuel Capacity: total 100 liters (each tank 50 liters - Standard tanks) Airframe control surfaces: Ailerons, Elevator, Rudder, Flaps, Trim Tax and Fixed tab Cabin Ventilation: Cabin Air control to provide more cool air and                                Cabin heat control to provide hot air  Instruments fitted:  Airspeed, Altimeter, Vertical speed indicator Attitude gyro, Directional gyro, suction Gauge and Turn Coordinator RPM Indicator, Oil Temperature indicator, EGT Fuel Qty Gauge, Out side temperature gau

Module 14

MODULE 14. PROPULSION 14.1 Turbine Engines         (a) Constructional arrangement and operation of turbojet, turbofan, turbo shaft and turbo               propeller engines;         (b) Electronic Engine control and fuel metering systems (FADEC). 14.2 Engine Indicating Systems         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        Operation of engine start systems and components; Ignition systems and components;        Maintenance safety requirements

Module 12

MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS 12.1 Theory of Flight — Rotary Wing Aerodynamics Terminology; Effects of gyroscopic precession; Torque reaction and directional control; Dissymmetry of lift, Blade tip stall; Translating tendency and its correction; Coriolis effect and compensation; Vortex ring state, power settling, overpitching; Auto-rotation; Ground effect. 12.2 Flight Control Systems Cyclic control; Collective control; Swashplate; Yaw control: Anti-Torque Control, Tail rotor, bleed air; Main Rotor Head: Design and Operation features; Blade Dampers: Function and construction; Rotor Blades: Main and tail rotor blade construction and attachment; Trim control, fixed and adjustable stabilisers; System operation: manual, hydraulic, electrical and flyby-wire; Artificial feel; Balancing and Rigging. 12.3 Blade Tracking and Vibration Analysis Rotor alignment; Main and tail rotor tracking; Static and dynamic balancing; Vibration types,