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Mantenimiento línea para proveedores - Coggle Diagram
Mantenimiento línea para proveedores
Módulo 1
Documentacion técnica
Introduccion
DDPG
MMEL Structure
AMM Part 2 Structure
Flujo resolución de items
Descripción y uso del FIM
Aircraft general ATA 04
Características generales
Historia y variantes
Módulo 2
Sistema eléctrico ATA 24
Introduction
General description
Component location
AC generation
DC generation
Standby power system
Common Display System ATA 31
Introducción
General description
Component location
Módulo 3
NAVIGATION SYSTEM ATA 34
Introducción
Sistema Pitot – estático
Sistema inercial
Overspeed warning
Radio Altimeter
Weather radar
Instrument Landing System ILS
Very high frecuency omnidirectional range VOR
Marker beacon
Distance Measurement Equipment DME
Global Positioning System GPS
ATC Transponder
Traffic Alert and Collision Avoidance System
Ground Proximity Warning System
Standby instruments
Flight Management System FMS
Módulo 4
AUTOFLIGHT ATA 22
Digital flight control system
Stall Management Yaw Damper
Stall Warning System
Yaw Damper System
Wheel To Rudder Interconnect System
Performance data
Autothrottle system
PBN CONCEPT
RNP
PBN
COMMUNICATIONS SYSTEM ATA 23
Service interphone
Flight interphone
Ground crew call system
Flight crew call system
Passenger Address
VHF Communication
High Frequency Communication
SELCAL
ACARS
Voice and flight data recorder
Módulo 5
FUEL SYSTEM ATA 28
Pressure refueling system
Defuel and transfer
Engine fuel feed system
APU fuel feed system
Fuel quantity indicating system
Fuel temperature indicating system
Fuel measuring stick
Módulo 6
ENGINE ATA 72
Engine indicating
Engine controls
Engine fuel
Engine air
Engine oil
Engine ignition
Engine starting
Engine exhaust system
AUXILIARY POWER UNIT APU ATA 49
APU engine
APU fuel system
APU ignition and start system
APU bleed air system
APU lubrication system
APU electronic control system
APU speed sensor
APU T2 sensor
APU EGT indication
APU Data memory module
Módulo 7
HYDRAULIC SYSTEM ATA 29
Main hydraulics systems
Standby hydraulic power
PTU power transfer unit
Hydraulic indicating system
LANDING GEAR ATA 32
Main landing gear
Nose landing gear
Landing gear control system
MLG extension and retraction
NLG extension and retraction
Main landing gear manual extension
Nose landing gear manual extension
Nose wheel steering system
Tail skid
Air ground system
Landing gear position indicating and warning system
Tires and wheels
Hidraulic brakes
Parking brake system
Antiskid and autobrake system
Módulo 8
FLIGHT CONTROLS ATA 27
Aileron and aileron trim control system
Flight spoiler
Speed brake control system
Elevator and tab control system
Horizontal stabilizer trim control system
Rudder and rudder trim control system
Trailing edge flap system
Leading edge flap and slat control system
Leading edge flap and slat position indicating system
Leading edge autoslat system
Take off warning system
Módulo 9
PNEUMATIC SYSTEM ATA 36
Engine bleed
Bleed air precooler system
Manifold system
APU bleed system
Indicating system
AIR CONDITIONING SYSTEM ATA 21
Air conditioning system 700-800
Recirculation system
Temperature control -700
Temperature control -800
Pressurization control
Módulo 10
NITROGEN GENERATION SYSTEM ATA 47
ICE AND RAIN PROTECTION ATA 30
Wing leading edge
Engine inlet cowls
Air data probes
Flight compartment windows
FIRE PROTECTION ATA 26
Engine fire protection and extinguishing
APU fire protection system
Cargo compartment fire protection system
Cargo compartment extinguishing system