Friday, 26 January 2018
EASA MODULE 13 AIRCRAFT STRUCTURES AND SYSTEMS
EASA MODULE 13 AIRCRAFT STRUCTURES AND SYSTEMS
SUB-MODULE 01 THEORY OF FLIGHT
SUB-MODULE 03 AUTOFLIGHT (ATA 22)
SUB-MODULE 04 COMMUNICATION / NAVIGATION (ATA 23/34)
SUB-MODULE 05 ELECTRICAL POWER (ATA 24)
SUB-MODULE 06 EQUIPMENT AND FURNISHINGS (ATA 25)
SUB-MODULE 07 FLIGHT CONTROLS (ATA 27)
SUB-MODULE 08 INSTRUMENTS (ATA 31)
SUB-MODULE 09 LIGHTS (ATA 33)
SUB-MODULE 10 ON BOARD MAINTENANCE SYSTEMS (ATA 45)
SUB-MODULE 11 AIR CONDITIONING AND CABIN PRESSURISATION (ATA 21)
SUB-MODULE 12 FIRE PROTECTION (ATA 26)
SUB-MODULE 13 FUEL SYSTEMS (ATA 28)
SUB-MODULE 14 HYDRAULIC POWER (ATA 29)
SUB-MODULE 15 ICE AND RAIN PROTECTION (ATA 30)
SUB-MODULE 16 LANDING GEAR (ATA 32)
SUB-MODULE 17 OXYGEN (ATA 35)
SUB-MODULE 18 PNEUMATIC/VACUUM (ATA 36)
SUB-MODULE 19 WATER/WASTE (ATA 38)
SUB-MODULE 20 INTEGRATED MODULAR AVIONICS (ATA 42)
SUB-MODULE 21 CABIN SYSTEMS (ATA 44)
SUB-MODULE 22 INFORMATION SYSTEMS (ATA 46)
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RMS Voltage Tutorial
What is RMS Voltage ? The RMS or effective value of a sinusoidal waveform gives the same heating effect of an equivalent DC supply In ou...
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EASA MODULE 13 AIRCRAFT STRUCTURES AND SYSTEMS SUB-MODULE 01 THEORY OF FLIGHT SUB-MODULE 03 AUTOFLIGHT ...
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Easa
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Angular displacement of the control coils with respect to the reference coils in a two phase induction motor are a) 0o, 180o Ans b) 90o, 2...
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