Engineering Guide Book 2 1998

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Engineering Guide Book 2 1998

Engineering Guide Book 2 1998
Change Summary Page
Lecture Guide List of Effective Pages
Lecture Guide List of Effective Pages-cont.
Lecture Guide List of Effective Pages-cont.
Examination
Lesson Guide
Lesson Examination
Lesson Objectives
Overview
Presentation
Cabin pressurization failure
Cabin altimeter failure
Summary
Review
Figure 1: Cockpit Pressurization Schedule
Lecture Guide
Lesson Preparation
Lesson Objectives
Overview
Presentation
Figure 1: GINA Major Related Component Locations
Controls/switches/indicators
Summary
Multi-Function Display (MFD)
Figure 2: ADI Display
Figure 3: MFD with Horizontal Situation Indicator (HSI) Display
Horizontal Situation Indicator (HSI)
Summary
Pitot static system major components
Figure 5: Standby Airspeed Indicators
Figure 6: Standby Vertical Speed Indicator (VSI)
Pitot tube
Angle of attack (AOA) major components
Figure 7: Angle of Attack System
AOA indexer
External approach lights
AOA transmitter probe
Independent instruments
Controls/switches/indicators
Standby attitude indicator
Standby turn and slip indicator
Figure 10: Standby Turn and Slip Indicator
Figure 11: Standby Compass
Figure 12: Clock/Stopwatch
Aircraft interfaces
GINA signals
Systems interface
Figure 13: HUD Indications
Lesson Notes
Summary
Progress Check
Summary
Lesson Guide
Lesson Preparation
Lesson Objectives
Overview
Presentation
Vertical speed indicator readout
Incongruent GINA GPS-INS positon and/or velocity computations
Pitot static system
Standby vertical speed indicator (VSI) failure
Angle of attack (AOA) system
Independent instruments
Standby attitude indicator (Standby AI) failure
Summary
Figures
Figure 1: GINA and Related Components: Summary of Malfunction Indications and Verifications
Figure 2: Pitot Static System: Summary of Malfunction Indications and Verifications
Figure 3: AOA Instruments: Summary of Malfunction Indications and Verifications
Figure 4: Independent Instruments: Summary of Malfunction Indications and Verifications
Lecture Guide
Lesson Preparation
Lesson Objectives
Overview
Presentation
Figure 1: Communications System--Major Components
Navigation
Figure 2: Communications Control Panel
Figure 4: IFF System--Major Components
Figure 5: GINA System--Major Components
VOR/ILS system
Figure 6: VOR/ILS System--Major Components
TACAN control panel
Figure 7: TACAN System--Major Components
Figure 8: HUD and HSI Displays with TACAN Selected
Controls and operational characteristics--communication system
UHF/VHF functionality
Frequency select switches
Throttle/stick
Aircraft interfaces--communication system
Figure 11: Communications Amplifier Block Diagram
COMM control panel
MIC switch: two-position toggle switch
Aircraft interfaces--COMM control panel/Intercom System (ICS)
IFF transponder
Identification of position (I/P) switch
Aircraft interfaces--IFF System (Transponder)
Controls and operational characteristics--navigation system
VOR/ILS system
ILS Operation
Figure 12: VOR/ILS System--Marker Beacon Lights
Controls and indicators--VOR/ILS System
Aircraft interfaces--VOR/ILS system
Figure 13: VOR/ILS Outputs
TACAN system
Controls and indicators
Aircraft Interfaces - TACAN System
Figure 14: TACAN Outputs
Navigation Control
Antenna locations (CNI)
Figure 15: T-45C CNI Antenna Locations
Forward fuselage (underside)
Summary
Lesson Guide
Lesson Examination
Lesson Objectives
Overview
Refresher
Communication system malfunctions
Intercom system (ICS) failure
Centralized warning system (CWS) audio failure
Navigation system malfunctions
INS failure
GINA GPS-INS mismatch
TACAN azimuth failure
Verifications
TACAN distance measurement equipment (DME) failure
Effects on flight safety
Instrument landing system (ILS) localizer failure
Marker beacon failure
Summary
Lecture Guide
Lesson Preparation
Lesson Objectives
Overview
Airborne data recorder (ADR) system
Figure 1: Airborne Data Recorder (ADR) Event Button
Figure 2: MFD - Maintenance (MANT) Display
Figure 3: Total Air Temperature (TAT)
Operating characteristics
Figure 4: ADR Monitoring
Armament control system (ACS) overview
Armament control system (ACS) major component identification
Figure 5: ACS Controls/Indicators
Gun trigger
Weight on wheels bypass switch
ACS operational characteristics
Figure 6: Gunsight
Figure 7: Wing Stations
Figure 8: Armament Controls/Indicators
Multi-Function display (MFD)
Weapons release button
Emergency jettison (PUSH TO JETT) button
HUD system
Figure 9: HUD Controls/Indicators
Video camera system (VCS)
ACS and HUD aircraft interfaces
Flight data inputs to HUD DEU
Figure 10: HUD Integrated Avionics System
Summary
Lecture Guide
Study Resources
Lesson Objectives
Motivation
Gyroscope characteristics
Real precession
Figure 3: Transport Apparent Precession
Instructor Notes
Mechanical INS gyroscopes – generic
Gimbaled: XYZ axes
Ring laser INS gyroscopes – generic-cont.
Litton GINA INS Design
Figure 5: Litton Ring Laser Gyro Assembly
Optical cavity mirrors – four
Instructor Notes
Accelerometers
Global Positioning System (GPS) characteristics
Figure 7: Optimum Satellite Array
Ranging and triangulation
Precise Positioning Service (PPS)
Receiver Autonomous Integrity Monitoring (RAIM) GPS feature
Instructor Notes
LITTON GINA Global Positioning System (GPS) design
Five (5) satellite communication channel capability
GPS antenna
Computes GPS data
GINA Components
Figure 11: GINA Components
Power supplies
Instructor Notes
GINA functions
Send/receive data to DEU and ADR
Instructor Notes
In-flight following loss of attitude information
Alignment (land)
Instructor Notes
Figure 12: SHIP Alignment
Instructor Notes
Instructor Notes-cont.
Figure 13: ACFT Data Page
Figure 14: GPS Data Page
NORM and APCH corridor monitor limit selection
Figure 15: BIT Display Page (Weight-On-Wheels)
GINA BIT checks
Figure 16: BIT Display Page (Weight-Off-Wheels)
GINA system faults
Figure 18: Got a Problem
Three (3) sigma deviation
Instructor Note
If INS is bad
Progress Check
Summary
Lesson Guide
Lesson Preparation
Lesson Objectives
Overview
Display system major components
Interfaces-cont.
Multi-Function Display
Display system interfaces
Display system bit
MFD Failure Indications
HUD Failure Indications
GINA system
GINA BIT status reported on BIT display
GINA Failure
INS failure
Inflight alignment
GINA Velocity/Position Mis-compare
HUD data effected
Effect on flight safety-cont.
Summary
Figures
Figure 1: Display System Major Components
Figure 2: DEU Interface Diagram
Figure 3: DEU Location
Figure 4: MFD Menu Display
Figure 5: Head-up Display (HUD)
Figure 6: DEU Functions as Bus Controller
Figure 7: Display System Electrical Diagram
Figure 8: Weight-Off-Wheels
Figure 9: Weight-On-Wheels
Figure 10: BIT Status Report
Figure 11: DEU Data Sources
Figure 12: Aircracft Data Display
Lecture Guide
Examination
Lesson Objectives
Overview
Engine start controls and indicators
Figure 1: Front Cockpit Component Locator
Figure 2: Engine Controls (FWD Cockpit)
GTS start button
Figure 3: Engine Start System
Throttle
Indicators
Figure 4: Engine Instruments and Indicators
Engine starting procedures
Interior check - left console
Figure 5: Engine Start Sequence
Engine switch - START
TGT and RPM indicators
Post-start
Progress Check
Unacceptable conditions during engine start
Wet Start
Oil Press warning light
Summary
Lesson Guide
Lesson Guide-cont.
Lesson Objectives
Lesson Objectives-cont.
Lesson Objectives-cont.
Lesson Objectives-cont.
Lesson Objectives-cont.
Lesson Objectives-cont.
Overview
Electrical System & Electrical System Malfunctions
Power protection
Electrical system operational characteristics
Battery operations
Electrical system aircraft interfaces
Electrical system malfunctions
Verifications
Engine System
Power generation
Bleed air system
Engine system controls, switches, and indicators cockpit controls
Engine start switch
Cockpit indicators
Engine operating characteristics
Air intake and compression
Power generation
Normal fuel control
LP fuel pump
Manual fuel control system
Engine lubrication system
Engine starting system
Engine starting component function
Bleed air system
Engine/aircraft interfaces
Engine System Malfunctions
Engine icing
Engine overtemp
Engine fire
Verifications
Steam ingestion bleed valve failure
Aircraft fuel system
Fuselage tank
Fuel delivery
Fuel system operational characteristics
Fuel system controls, switches, and indicators
Caution/advisory
Fuel system interfaces
Venting: releases air/vapor to atmosphere through pressure relief valves
Pressure refueling operation
Fuel system malfunctions
Fuel tank pressurization failure
Hydraulic System
Engine-driven pump (EDP)
Flight control (FC) accumulator
Power supply package
Hydraulic system no. 2 (HYD 2)
Emergency package assembly
Emergency hydraulic system components
Hydraulic system operational characteristics
HYD 2 operational characteristics
HYD 2 output distribution
Warning/caution light panel (WCP), both cockpits
Checking/testing the hydraulic system
Aft fuselage (right side)
Left main wheelwell
Aircraft interfaces
Emergency HYD system
Hydraulic system malfunctions
Effects on flight safety
Hydraulic Subsystems
LDG Gear Door caution light
Nose wheel steering (NWS); dual-gain, full-time (low-gain)
Brakes/anti-skid
Controls and indicators
Launch bar
Arresting hook
Aircraft interfaces
Electrical system
Flight Control System
Major components
Aileron system
Stabilator system
Flaps/slats, speed brakes
Slat system
Slat position indication
Speed brake system
Flight controls/switches/indicators
Rudder Trim knob
Flaps/controls/switches/indicators
Slats controls/switches/indicators
Extend/retract switch
Flight control system malfunction
Canopy and egress systems
Navy aircrew common ejection seat (NACES)
Cockpit controls: command ejection panel
Operating characteristics
On-board oxygen generation system (OBOGS) and environmental control system (ECS)
Switches, indicators, and controls
Environmental control system (ECS)
Cockpit pressurization
ECS controls, switches and indicators
Flight instruments
GINA alignments
Pitot static system major components
Angle of attack (AOA) major components
Flight instruments aircraft interfaces
Systems interface
Flight Instrument Operation
Pitot static system
Standby compass
Flight instrument malfunction
Horizontal situation indicator (HSI) display failure
General GINA failure
CNI System
Navigation
Antenna locations (CNI)
CNI operation
COMM control panel/intercom system (ICS)
Intercom system (ICS)
TACAN system
Aircraft Interfaces - TACAN System
VOR/ILS system
CNI controls and switches
Frequency selector (outer knob)
Frequency select switches
COMM control panel
IFF system (transponder)
Status lights
Mode select/test switches
TACAN controls and indicators
VOR/ILS controls and indicators
CNI malfunctions
Verifications
TACAN azimuth failure
Display System
Display system operation
Display system bit
Display system interfaces
Engine start procedures
Engine start controls and indicators
Indicators
Engine starting procedures
Interior check
GTS start button
Throttle
TGT and RPM indicators
Post-start
Unacceptable conditions during engine start
Low battery voltage
Bleed air valve
Summary
Figures
Figure 1: Electrical System Block Diagram
Figure 2: Electrical Load Distribution
Figure 3: Basic Engine Block Diagram
Figure 4: Engine Fuel System Block Diagram
Figure 5: Engine Starting System Block Diagram
Figure 6: Simplified Fuel System Block Diagram
Figure 7: Aircraft Fuel System Block Diagram
Figure 8: Hydraulic System Block Diagram
Figure 9: Main Landing Gear (MLG) Major Components
Figure 10: Nose Landing Gear (NLG) Major Components
Figure 11: Nose Wheel Steering (NWS) System Major Components
Figure 12: Wheel Brake/Anti-Skid System Block Diagram
Figure 13: Flight Controls
Figure 14: Flight Controls--Rudder System Components
Figure 15: Flight Controls--Aileron System Components
Figure 16: Flight Controls--Stabilator System Components
Figure 17: Flaps/Slats, Speed Brakes
Figure 18: Canopy
Figure 19: Ejection Seat
Figure 20: Minimum Safe Ejection Altitudes
Figure 21: OBOGS Block Diagram
Figure 22: Pilot's Services Panel
Figure 23: ECS Block Diagram
Figure 24: Attitude Director Indicator (ADI) Display
Figure 25: Horizontal Situation Indicator (HSI) Display
Figure 26: AOA System
Figure 27: UHF/VHF Control Panel
Figure 28: IFF Control Panel
Figure 29: COMM Control Panel
Figure 30: Display System Major Components
Figure 31: BIT Status Report
Figure 32: DEU Interface Diagram
Figure 33: Engine Controls (Forward Cockpit)
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Engineering Guide Book 2 1998

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