Gulfstream G150 Pilot Training Manual. Volume 2. Aircraft systems

دسته بندی: حمل و نقل: هواپیمایی
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تعداد صفحات: 474 
زبان: English 
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قیمت کتاب (تومان) : 32,000

FlightSafety International, New York, 2008. — 474 с. Aircraft general
Introduсtion
General
Dimensions
Air conditioning
APU
Engine indicating and crew alerting system (EICAS)
Electrical
Fire protection
Flight controls
Fuel
Hydraulics
Ice and rain protection
Landing gear and brakes
Lighting
Oxygen
Pneumatics
Powerplant
Pressurization
Limitations
Performance
Publications
Aircraft Walkaround
G150 Aircraft Dimensions
Electrical power systems
Introduction
General
DC power system
General
Batteries
General
Operations
Emergency power
Battery temperature monitoring
External DC power
General
Operation
Control
DC power distribution
General
Buses
Generators
General
Generator Control Units
Operation
Battery Charging
Load Operating Conditions
Engine Start
AC system
General
System Operation
Controls and Indications
MFD Indications
Circuit Breakers[/i]
Limitations
DC Starter-Generator Limits
Battery Limits
Emergency and abnormal operations
EICAS Messages
Questions
Lighting
Introduction
General
System description
Flight Compartment Lights (Cockpit)
Passenger Compartment Lighting (Cabin)
Exterior Lighting
Emergency Lighting
Baggage Compartment Lighting
Annunciator Lights
Limitations
Emergency and abnormal operations
Questions
Questions
Master warning system
Introduction
General
Fuel system
Introduction
General
Fuel storage system
Fuselage Tank
Center Tank
Wing Tanks
Drain Valves
Fuel tank vent system
Fuel distribution system
System Description
Engine Feed
APU Feed
Fuel Usage
Fuel quantity system
System Description
Measurement System
Indication System
Refueling
Defueling
Controls and indications
Overhead Panel
Center Pedestal
Instrument Panel
Limitations
Approved Fuels
Fuel Tank Capacities
Fuel Unbalance
Emergency and abnormal operations
Fuel EICAS Messages
Questions
Auxiliary power unit
Introduction
General
System description
Components
Operation
Controls
APU Fire Protection
Ignition/ Starting
Normal Operation
Normal Shutdown
Limitations
Emergency and abnormal operations
Indicating
EICAS Messages
Questions
Powerplant
Introduction
General
Powerplant Controls
Digital electronic engine control (DEEC)
Ignition System
Start System
Engine Fuel System
Engine Oil System
Synchronizing
ITT System
Automatic Power Reserve (APR)
Engine indicating
Vibration Monitoring
Thrust reversers
Components
Controls and Indications
Operation
Limitations
General
Engine Operating Limitations
Powerplant Limitations
Emergency and abnormal operations
Powerplant System EICAS Messages
Questions
Fire protection
Introduction
General
System description
Detection
APU
Extinguishing
Fire Extinguishing Bottles
Two-Way Check Valve
Thermal Relief Valve
Thermal Relief Disc
Portable Fire Extinguishers
Operation
Engine Controls
Fire Panel Operation
APU Controls
Additional Controls
Detection
Extinguishing
APU
Indication
Engine
APU
Smoke Detector System
Warning System
Emergency and abnormal operations
Warning
Questions
Pneumatics
Introduction
General
Pneumatic System
Bleed-Air Sources Description
APU Bleed Air Supply
Air Selection
Components
Bleed Switching Valves
Operating Mode
Closed Mode
APU Air Valve
Pneumatic System Operation
Warning and protection
OverPressure Switch
OverTemperature Switch
High Pressure Ducting
RAM-Air system
TemperatureControl System
Temperature control system
Operation
Automatic Mode
Manual Mode
Emergency and abnormal operation
Environmental System EICAS Messages
Warning messages
Status messages
Questions
Ice and rain protection
Introduction
General
System description
Airfoil deicing system
Components
Operation
Indications
Nacelle ante-ice system
Components
Controls
Indications
Pitот and static system
Components
Operation
Indications
Windshield and windows
Components
Controls
Indications
Limitations
Anti-Ice System Limitations
Emergency and abnormal operations
Questions
Air conditioning
Introduction
General
Air distribution system description
Conditioned Air
Gasper Air
Emergency Air
Check Valves
Bleed air routing
Ozone Converter
Bl ееd-Air Precooler
Refrigeration unit
Air Cycle Machine
Water Separator
Trim-Air Valve
Temperature control system
Description
Components
Nose compartment cooling description
Limitations
Emergency and abnormal operations
Air Conditioning System EICAS Messages
Questions
Pressurization
Introduction
General
Pressurization system description
Components
Controls and Indications
Operation
Limitations
Cabin Pressurization
Operation
Emergency and abnormal operation
Pressurization System EICAS Messages
Questions
Hydraulic power system
Introduction
General
Main Hydraulic System
Auxiliary Hydraulic System
Hydraulic Fluid
Components
Main Hydraulic System
Auxiliary Hydraulic System
Other Components
Operation
Main Hydraulic System
Auxiliary Hydraulic System
Limitations
Approved Hydraulic Fluids
Emergency and abnormal operation
Questions
Landing gear and brakes
Introduction
System description
Landing gear
Nose Landing Gear
Main Landing Gear
Other Components
Emergency Landing Gear Extension System
Position and Warning
Wheels and Brakes
Normal Brake System
Parking/Emergency Brakes
Antiskid System
Nose wheel Steering
Operation
Landing Gear Normal Operation
Landing Gear Emergency Extension
Landing Gear Position and Warning
Normal Braking—Antiskid
Operation—Without Antiskid
Parking/Emergency Brake Operation
Limitations
Emergency and abnormal Procedures
EICAS Indications
Questions
Flight controls
Introduction
General
System description
Primary Flight Controls
Secondary Flight Controls
Operations
Primary Flight Controls
Secondary Flight Controls
Limitations
Slats/Flaps
Trim System
Emergency and abnormal Procedures
EICAS Indications
Questions
Illustrations
Flight Controls
Aileron System
Aileron Servoactuator
Rudder Control System
Rudder Trim Tab System
Elevator Control System
Horizontal Trim Actuator
Wing Flaps
Flap Drive System
Slat Drive System
Flap/Slat Electronic Control Unit (FSECU)
Slat Power Drive Unit (PDU)
Ballscrew Actuator
Airbrakes Deployed
Gust Lock
Control Wheels
Aileron/Rudder Trim Switches and Indications
Override Trim Engaged
Emergency Trim Engaged
Slats/Flaps Control Lever
Airbrake Control Switches
Gust Lock Engaged
Flight Controls EICAS Indications
Avionics
Cockpit Instruments and Displays
Oxygen system
Introduction
Oxygen systems
General
System description
Crew Oxygen System
Crew Oxygen Mask Stowage
Passenger oxygen system
Therapeutic oxygen
Components
Oxygen Cylinder
Overpressure Discharge Valve
Pressure Transducer
Pressure Reducer
Oxygen Filler Valve
Charging Pressure Gauge
Shutoff Valve
Pressure Relief Valve
Control and indications
Oxygen supply Valve
Crew Oxygen Mask
Vent Valve
Oxygen Pressure Indication
Passenger Oxygen Controller
Oxygen ON Light
Therapeutic Oxygen
Limitations
Emergency and abnormal operations
EICAS Messages
Questions
Maneuvers and procedures
Before takeoff
Flight Planning
Weight and Balance
Preflight Inspection
Maneuvers
Takeoff Profile
Normal Takeoff
Takeoff with Engine Failure At or Above V1
Steep Turns
Approaches to Stall
Maneuvering at Minimum Speed (Slow Flight, FAA Ballet)
Maneuvering with Engine Failure
Trim and Pitch Change Characteristics
Unusual Attitudes (Jet Upset)
Holding
ILS Approach — Two Engines
ILS Approach — Single Engine
Nonprecision Approach — One or Two Engines
Circling Approaches
Normal Landing
Visual Approach with No-Flap/Partial-Flap Landing
Crosswind Takeoffs and Landings
Landing with Simulated Engine Failure
Missed Approach Procedures
Aborted Takeoff
Special maneuver considerations
Runaway Pitch Trim
Emergency Descent
Flight in Adverse Weather Conditions
Bird Strike
Black Hole Phenomena
Appendix
List of Abbreviations
Centigrade to Fahrenhiet conversion table
Answers to Questions
Flash Cards