- Артикул:00-01058374
- Обложка: Твердая обложка
- Издательство: Alenia aeronautica tecnical publications (ISLA) (все книги издательства)
- Город: Италия
- Страниц: 730
- Год: 2003
- Вес: 1971 г
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Книга на английском языке
Мanual contains the necessary information for safe operation of the EF2000 aircraft. These instructions provide you with a general knowledge of the aircraft and its characteristics and specific normal and emergency procedures. Your experience is recognized therefore, basis flight principles are avoided. The technical content of this manual has been vetted through the Quality Assurance Procedures required by the Technical Publications Generating Plan PL-J-0-E-0076. Dissemination and reproduction of this publication and the use and disclosure of its contents are not permitted without specific approval of the publisher. Violation of this regulation will result in claims for damage.
Table of Contents
Section 1 - description and operation
The Aircraft
Aircraft Gross Mass
Aircraft Dimensions
Cockpit DISPLAYS AND CONTROLS
Electronic Displays and Controls
Electronic Display Formats HUD (AVS 3C)
Cockpit Controls and Indicators
Electronic Displays and Controls - MHDD
Electronic Displays and Controls - VTAS
Ground Proximity Warning System
Get-U-Home And Reversionaty Instruments
Utilities Control System (UCS)
UCS - Description and Operation
UCS - Data Bus and Interfaces
Engines
Engine Air System
Engine Oil System
Engine Fuel Control System
Digital Engine Control Unit
Engine Monitoring System (EMS)
Engine Starting System
Air Flow Control System
Throttles
Engine Controls and Indicators
Engine/APU Fire Protection System
Engine Operation
Engine Handling in Flight
Secondary Power System (SPS)
APU Operation
SPS controls and indicators
Fuel Supply System
Fuel Tanks
Fuel Transfer System
Fuel Pressurization and Vent System
Fuel Cooling System
Engine Fuel Supply System
Ground Refueling and Defueling
Air-to-Air Refueling
Fuel System Controls and Indicators
Fuel Masses
Electrical Power Supply System
Electrical Power System
Electrical System Controls and Indicators
AC Power Supply and Distribution
DC Power Supply and Distribution
Hydraulic Power Supply System
Hydraulic System - Main Components
Hydraulic System Controls and Indicators
Landing Gear System
Main/Nose Gear
Landing Gear Emergency System
Wheel Brake System
Anti Skid System
Landing Gear System Controls and
Indicators
Auxiliary Deceleration System
Brake Chute System
Arrester Hook System
Flight Control System
Foreplane
Flaperons
Rudder
Leading Edge System
Nosewheel Steering
Air Intake Cowls
Airbrake
Trim System
Flight Control System Controls and
Indicators
Flight Control System Built In Test
FCS Moding
Autothrottle System
AirData System
Air Data System Controls and Indicators
Canopy
Escape System
Ejection Seat
Parachute and Combined Harness
Ejection Sequence
Escape System Controls and Indicators
Minimum Ejection Heights
Aircrew Equipment Assembly
Environmental Control System (ECS)
Environmental Control System Modes of
Operation
Pressurization System
Cabin Air Supply System
Avionic Air Supply System
Avionic Liquid Cooling System
Antimist/Demist System
Emergency Ram Air
Anti-G System
Ice Detection
Environmental Control System Controls
and Indicators
Oxygen System
Molecular Sieve Oxygen Generation
Auxiliary Oxygen System
Lighting System
Avionics System Integration
System Software/Mission Data Loading
Navigation System
Navigation Fixing
Navigation Steering
Reversionary Navigation Mode
Laser Inertial Navigator System (LINS)
Navigation Computer
Global Positioning System (GPS)
Radar Altimeter (RA)
TACAN
Navigation MDE and X-Y Functions
Miscellaneous MDE and X-Y Functions
Communication Equipment
V/UHF Radio
Communication and Audio Management
Unit (CAMU)
Communication Controls and Indicators
Communication MDE and X-Y Functions
Audio Warning Equipment
Warnings Management and Failure
Analysis
Dedicated Warning Panel
Visual/Audio Warnings
Recorders
Integrated Monitoring Test and Recording
System
Fire Warning System
Flight Test Instrumentation
Servicing
Section 2 - normal procedures
Table of ContentsPage
Preparation for Flight
External Checks
Ejection Seat Checks
Strapping and Unstrapping
Internal Checks
Engines Start
Before Starting Engines
Starting Engines
Starting Failures/Cancelling Engines Start
Dry Crank
Taxi/Takeoff
Pre Taxi
Taxi Checks
Before Takeoff Checks
Line-Up
Takeoff
After Take-off Checks
Flight
Climb
Cruise Checks
Descent/Recovery
Landing
Pre Landing
Landing
Braking Technique
After Landing
Shut Down
Weapon Configuration/Selective Jettison
Package
AMRAAM Firing Normal Mode
Selective Jettison Package
Fuel Balance/Difference Monitoring
FCS 2B2 Fuel Asymmetry Limits, Clean
Aircraft
Performance Data Chart
Recovery (Two Engines and Single Engine)
Section 3 - emergency procedures
Table of ContentsPage
Introduction
Emergency Procedures Advice
Abandoning
Emergency Ground Egress
Ejection
Takeoff
Abort
FCS Failures during Takeoff
Tire Failure during Takeoff
Engine Failure During Take Off
Engine Reheat Failure During Take Off
Fires
APU/Engine Fire on Ground
Engine Fire during Take-Off
Engine Fire in Flight
Flameout/Relighting
Double Engine Flame Out
Single Engine Flame Out
Engine Failures
L/R Engine Vibration/Mechanical Failure
Engine Surge (Locked In Surge)
Engine Oil Pressure Low
Engine Oil Overtemperature
Engine Control Failures
L/R DECU
Engine Airflow Control System Failure
L/R REHEAT Failure
L/R Engine Performance
Fuel System Failures
Low Fuel / Fuselage Fuel Leak
Fuel Supply Low Pressure
Fuel Balancing
L/R Fuel Overtemp
Fuel Transfer Failure
Transfer Valve Failure
Vent Failure
Single Fuel Computer Failure
Air-to-Air Refueling Probe
Electrical System Failures
Double AC Failure
Single AC Generator Failure
Electrical Level 3 Failure
Electrical Level 2 Failure
Electrical Level 1 Failure
Gearbox Failures
POT Shaft Failure
Gearbox Failure
ATS/M Failure
SPS - Overpressure
L/R SPS Computer Failure
Gearbox Over-Temperature
Hydraulic System Failures
Double Hydraulic System Failure
Single Hydraulic System Failure
Single Utility System Failure
Double Utility System Failure
Hydraulic Overtemperature
Air in Hydraulics
Flight Control System Failures
FCS/Airdata Failures
Air Intake Cowl Failure
Datum Adjust Trim Switch Failure
Airbrake Failure
Slats Failure
Avionic System Failures
Loss of HUD Symbology
Inertial Navigation Failure
Radar Altimeter Failure
Navigation Computer Failure
TACAN Failure
Attack Computer Failure
Single / Double CIU Failure
Single / Double CSG Failure
GPS Failure
IFF Transponder Warnings
DASS Computer Failure
Radar Shut Down/Total Failure
IFF Interrogator Warnings
Environmental Control System Failures
Pressurization/ECS Failures
ECS Compatibility Area
Smoke or Fumes in Cockpit
Oxygen Failures
UCS Front Computer Failure
Windscreen Heater Failure
Single Engine Operation
Engine Failure on Approach
Single Engine Operations
Approach/Landing Emergencies
NWS Failure Airborne/Approach
NWS Failure - Pre Takeoff/Landing
Anti Skid Failure
Wheel Brake Failure
Hook Down
Cable Engagement
Landing Gear Emergencies
Landing Gear Retraction Failure
Landing Gear Fails to Lower
Landing with Gear Unsafe
Landing Gear Collapsing
Landing with a Known Blown Tire
Armament Control System Failures
Jettison External Stores (EMGY or SEL)
Section 8 - attack and ident
Table of Contents Page
Surveillance/Attack and Identification
Subsystem 1
Bogus Weapons
Controls and Indicators
Radar
Radar Modes and Operation
Radar Cockpit Controls
Radar MDE and X-Y Functions
Defensive Aids and Subsystem (DASS)
Defensive Aids Computer
Forward Looking Infra Red
Forward Looking Infra Red Controls and displays
Forward Looking Infra Red Modes
Identification System (IFF)
Identification System Controls and indicators
Identification System Modes and operation
Identification System MDE and X-Y Functions
Armament Control Subsystem (ACS)
Weapon System Controls and Indicators
Stores MDE and X-Y Functions
AMRAAM
AMRAAM Principle Function
AMRAAM Firing
Armament Carriage and Installation
System (ACIS)
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