Engineering Lecture Guide Book 1

Click here to make tpub.com your Home Page

Page Title: Engineering Lecture Guide Book 1

Click here for thousands of PDF manuals

Web
www.tpub.com

Information Categories

....

Administration
Advancement
Aerographer
Automotive
Aviation
Construction
Diving
Draftsman
Engineering
Electronics
Food and Cooking
Logistics
Math
Medical
Music
Nuclear Fundamentals
Photography
Religion

Engineering Lecture Guide Book 1

Engineering Lecture Guide Book 1
T-45C Lecture Guide Change Summary Page
Lecture Guide List of Effective Pages
Lecture Guide List of Effective Pages-cont.
Lecture Guide List of Effective Pages-cont.
Lecture Guide
Lecture Guide-cont.
Engineering Contents
Lesson Objectives
Lesson Objectives-cont.
Overview
Presentation
Figure 1: T-45C General Description
Progress Check
Major aircraft systems overview
Figure 2: Electrical System Block Diagram
Figure 3: T-45C Engine
Figure 4: T-45C Fuel System Diagram
Figure 5: T-45C Hydraulic System Block Diagram
Flaps/slats, speed brakes
Landing gear system
Figure 6: T-45C Landing Configuration
Figure 7: Landing Gear C Controls and Indicators
Figure 8: Wheel Brake/Anti-Skid System Block Diagram
Figure 9: Nose Wheel Steering Major Components
Launch bar system
Figure 10: Arresting Hook Operation
Figure 12: Canopy System and Controls
Figure 13: Ejection Seat and Controls
Figure 14: Command Ejection Selector/Seat Light Switch (Aft Cockpit Only)
Figure 15: OBOGS
Environmental control system (ECS)
Figure 16: Environmental Control System
COMM/NAV instrument (CNI) system
Figure 17: CNI Cockpit Controls
Figure 18: Display System
Figure 19: Display System and Controls
Armament control system (ACS)
Figure 21: HUD Controls/Indicators
Figure 22: T-45C Wing Pylon (Underside View)
Function
Figure 23: Cockpit Armament Controls/Indications
Indicator location
Centralized warning system (CWS)
Warning light panel
Centralized warning system master test
Intercom system (ICS) interface
Summary
Lecture Guide
Examination
Lesson Objectives
Overview
Electrical system major component identification
Power control
Overvoltage unit
Power protection
Power distribution relays and contactors
Figure 2: Electrical System Block Diagram -- AC Power Relays Removed
Electrical system operational characteristics
Battery operations
Ground power system
Figure 3: Ground Power Panel
Fault protection analysis
Undervoltage
Undervoltage unit failure
Single inverter failure
Power system controls, switches, and indicators
Figure 4: Power Panels
Warning and caution advisory panels
Aircraft lighting system
Anti-collision lights
Figure 7: Interior/Exterior Light Controls
Interior lighting
Electrical system aircraft interfaces
Figure 8: Electircal Load Distribution
28 VDC ground services bus: equipment powered
115 VAC essential bus: equipment powered
Summary
Lesson Guide
Lesson Examination
Lesson Objectives
Motivation
Refresher
Double inverter failure
Undervoltage condition
Generator failure
Total electrical failure
Effects on flight safety-cont.
Summary
Figure 1: Electrical System Diagram
Figure 2: AC Inverter Failure
Figure 3: Undervoltage Condition
Figure 4: Generator Failure with Low Battery Voltage
Figure 5: Electrical Load Distribution
Lecture Guide
Lesson Preparation
Lesson Objectives
Overview
Figure 1: Engine Fuel System Block Diagrams
Figure 2: Engine Starting System Block Diagram
Air turbine starter (ATS)
Engine operating characteristics
Combustion (N2 compressor air)
Exhaust gas temperature (EGT)
Engine fuel system
Lesson Notes
Two independent control modules
Manual fuel control system
Engine lubrication system
Functional description
Engine starting system
Start control unit
Engine starting component function
Bleed air system
External air flow
Catapult launch to preclude compressor surge due to steam ingestion
Engine system controls, switches, and indicators
Figure 5: Engine Controls
Idle stop lever
Fuel Shutoff handle
Lesson Notes-cont.
Cockpit indicators
Progress Check
Figure 6: Engine Oil Fill Gauge
Figure 7: Simplified Fuel System Block Diagram
Outputs
Progress Check
Summary
Lesson Guide
Lesson Preparation
Lesson Objectives
Motivation
Refresher
Reduced thrust on takeoff
Engine failure on takeoff
Verifications
Engine stalls
Engine overspeed
ECA failure (full trim)
ECA failure (no trim)
Initial shot solenoid failure
Effects on flight safety
Summary
Figures
Figure 1: Engine Components
Figure 2: Engine/Fuel Control System
Figure 3: Engine Oil System
Figure 4: Engine Starting System
Figure 5: Engine Operating Limitations
Figure 6: Indications of Engine Overtemp
Lesson Guide
Lesson Preparation
Lesson Objectives
Overview
Presentation
Low pressure fuel pump failure
Engine seizure
Stuck throttle/throttle linkage failure
Summary
Figures
Figure 1: ENG-05 Malfunction Indications and Verifications (Partial Listing)
Figure 2: ENG-05 Additional Malfunction Indications and Verifications
Figure 3: Tailpipe Overtemp
Figure 4: Engine Bleed Valve
Figure 5: LP Pump Failure
Figure 6: Oil Pressure Failure
Figure 7: ENG-06 Malfunction Indications and Verifications
Lecture Guide
Lesson Preparation
Lesson Objectives
Overview
Figure 1: Simplified Fuel System Block Diagram
Aircraft fuel system major component identification
Figure 2: Air Craft Fuel System Block Diagram
Collector tank
Fuel delivery
Engine fuel supply
Operational characteristics
Fuel delivery
Venting
Refueling
Pressure refueling operation
Controls, switches, and indicators
Fuel Flow
Figure 4: Fuel System Caution Advisory
Figure 5: Fuel System Controls (Forward Cockpit Only)
Progress Check
Aircraft interfaces
Progress Check
Summary
Lesson Guide
Lesson Examination
Lesson Objectives
Overview
Presentation
Fuel leaks
Low fuel
Conclusion
Figures
Figure 1: Caution Advisory Panel Indications
Figure 2: Fuel Quantity Indicator
Figure 3: Multi-Function Display (MFD)
Lecture Guide
Lesson Preparation
Lesson Objectives
Overview
Presentation
Figure 1: Hydraulic System Pressure Gauges/Reset Button
Figure 2: Warning and Caution Advisory Light Panels
Hydraulic system no. 1 (HYD 1)
HYD 1 components
Flight control (FC) accumulator
Power supply package
Hand pump
HYD 1 operational characteristics
HYD 1 controls, switches, and indicators
Figure 4: Wheel Brake/Emergency Flap Accumulator Pressure Gauge
Figure 5: HYD 1 FC Accumulator Pressure Gauge
Figure 6: HYD 1 Filter Indicator
Figure 7: HYD 1 Reservoir Indicator
HYD 1 malfunctions
Hydraulic system no. 2 (HYD 2)
Engine-driven pump (EDP)
Emergency package assembly
HYD 2 operational characteristics
Output distribution
HYD 2 controls, switches, and indicators
Figure 8: HYD 2 FC Accumulator Pressure Gauge
Figure 9: Left Side External Locator
HYD 2 malfunctions
Lesson Notes
Emergency hydraulic system
RAT accumulator
Emergency hydraulic system: RAT
Emergency hydraulic system malfunctions
Emergency hydraulic system summary
Aircraft interfaces
Emergency hydraulic system
Progress Check
Summary
Conclusion
Lecture Guide
Lesson Examination
Lesson Objectives
Motivation
Presentation
HYD 1 and HYD 2 slow pressure loss
Effects on flight safety
RAT failure
HYD 1 and HYD 2 failure (RAT operating)
Total system failure
Summary
Figures
Figure 1: Hydraulic System
Figure 2: Caution Advisory Panel
Figure 3: Hydraulic Pressure Gauges
Figure 4: Indications Summary
Lecture Guide
Lesson Preparation
Lesson Objectives
Lesson Objectives-cont.
Overview
Figure 1: Main Landing Gear (MLG) Major Components
Figure 2: MLG PIN
Figure 3: Landing Gear Doors
Nose landing gear (NLG)
Figure 4: Nose Landing Gear (NLG) Major Components
Controls and indicators
Figure 5: Landing Gear Controls and Indicators
LDG GEAR position indicator
Figure 6: NLG Strut Pressure Gauges
Figure 7: NLG Strut Inflation Chart
Figure 8: Landing Gear Indications
Sequence of nose gear/door extension
Sequence of main gear/door retraction
Emergency extension system
Limitations
Summary
Landing gear-related hydraulic components
Figure 10: Wheel Brake/Anti-Skid System Block Diagram
Figure 11: Brake System Controls and Indicators
PK Brake caution light
Figure 12: Wheel Brake/Emergency Flap Accumulator Pressure Gauge
Anti-Skid switch
Operating characteristics
Figure 14: Brake Unit Inspection
Following a HYD 1 failure
Summary
Brake Pressure Release System
Operating characteristics
Operating characteristics-cont.
Summary
Figure 15: Nose Wheel Steering (NWS) System Major Components
NWS button
Figure 16: NWS System Controls and Indicators
Figure 17: NWS System Component Locator
Summary
Launch bar
Controls and indicators
Figure 19: Launch Bar System Controls and Indicators (FWD Cockpit)
Summary
Arresting hook
Figure 20: Arresting Hook System Major Components
Controls and indicators
Figure 22: Arresting Hook System Controls and Indicators (FWD Cockpit)
Figure 23: Arresting Hook Operation
Progress Check
Aircraft interfaces
Electrical system
Figure 24: Centralized Warning System Interface
Figure 25: Weight-On-Wheels (WOW)
Weight-on-wheels condition
Interface summary
Interface summary-cont.
Summary
Lesson Guide
Lesson Preparation
Lesson Objectives
Overview
Figure 1: Hydraulic System
Figure 2: (FWD) Cockpit Instrument Panel and Consoles
Presentation
Figure 3: Landing Gear/Door System Operation
Wheel brake failure
Figure 4: Wheel Brake/Anti-Skid System Operation
Anti-skid failure
NWS failure
Figure 5: Nose Wheel Steering System Operation
Figure 6: Launch Bar System Operation
Tail hook malfunctions in the landing phase
Lecture Guide
Training Aids
Summary
Lesson Objectives
Lesson Objectives-cont.
Overview
Major flight control components
Figure 1: Flight Control System, Flaps/Slats, Speed Brakes
Flight controls
Aileron actuators (power control units [PCUs])
Figure 3: Aileron Controls/Indicators
Operating characteristics/limitations
Figure 4: Aileron System Components--Simplified
Stabilator system
Figure 5: Flight Controls--Stabilator System Components
Speedbrake interconnect actuator
Figure 6: Stabilator Controls/Indicators
Operating characteristics/limitations
Rudder system
Figure 8: Flight Controls--Rudder System Components
Trim/Yaw damper actuator
Cockpit controls/switches/indicators
Rudder Trim knob
Paddle switch
Figure 10: Rudder System Components--Simplified
Yaw damping system and Aileron Rudder Interconnect (ARI)
Aircraft interfaces
Flaps/slats, speed brakes
Cockpit controls/switches/indicators
Figure 12: Flap Controls/Indicators
Operating characteristics/limitations-cont.
Slat system
Cockpit controls/switches/indicators
Figure 14: Slat Controls and Indicators
Operating characteristics/limitations
Speed brake system
Figure 16: Speed Brake Controls/Indicators
Operating characteristics/limitations
Summary
Figure 17: Flap System Components
Speed brakes
Figure 18: Slat System Components
Figure 19: Speed Brake System Components
Figure 20: hydraulic System Block Diagram
Electrical system
Summary
Lesson Guide
Lesson Preparation
Lesson Objectives
Overview
Presentation
Runaway aileron trim
Runaway rudder trim
Rudder hardover condition
Summary
Figures
Figure 1: Flap System Operation
Figure 2: Slat System Operation
Figure 3: Stabilator Trim Operation
Figure 4: Speed Brake Operation
Figure 5: Aileron Trim Operation
Figure 6: Rudder Trim Operation
Figure 7: Summary
Lecture Guide
Examination
Lesson Objectives
Overview
Presentation
Cockpit controls/indicators and operational characteristics
Canopy external handle
Canopy damper/locking strut
Figure 3: Lost Motion Units
Mild detonating cord (MDC) controls/indicators and operational characteristics
Summary
T-45 aircraft boarding ladder & aircraft boarding system
Figure 4: T-45 Ladder & Aircraft Boarding System
Pull-out footsteps
Navy aircrew common ejection seat (NACES)
Parachute assembly
Figure 5: Main Beam Assembly
Ejection seat bucket
Seat height adjustment switch
Ejection handle
Emergency restraint release handle
Leg restraint system
Survival kit (seat pan)
Survival aids
Cockpit controls: command ejection panel
Command ejection selector positions
Ejection
Canopy fragmentation system
Ejection event sequence from initiation through end of catapult stroke
End of catapult travel
Figure 6: Modes of Operation
Mode 1
Summary
NATOPS ejection parameters
Figure 7: Minimum Safe Ejection Altitudes
Ejection seat - Inspect
Figure 8: Ejection Seat Inspection
Figure 9: Aft Cockpit
Aft Cockpit (solo flight)-cont.
In The Cockpit
Lap belt
Summary
Lesson Guide
Lesson Examination
Lesson Objectives
Overview
Presentation
Canopy damper locking strut failure
Command ejection selector malfunction
Unable to eject--ejection seat failure
Conclusion
Figures
Figure 1: Caution Advisory Panel
Figure 2: Canopy Control Lever
Figure 3: Canopy Controls
Figure 4: Command Ejection Selector
Figure 5: Ejection Seat Controls
Lecture Guide
Examination
Lesson Objectives
Overview
Major OBOGS components
OBOGS operating characteristics
Overheat temperature switch/sensor
Oxygen monitor
Pilots personal gear
OBOGS controls, switches, and indicators
Oxygen monitor (fwd cockpit only)
OBOGS operational check requirements
Evaluation criteria
Major ECS components
Air conditioning system--major components
ECS operating characteristics
Inducer pressure regulator and shutoff valve (IPRSOV)
Cockpit air distribution
Cockpit pressurization system
ECS controls, switches and indicators
Cockpit pressurization system
Avionics equipment cooling system
ECS aircraft interfaces
Summary
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page
Blank Page

Engineering Lecture Guide Book 1

Privacy Statement - Press Release - Copyright Information. - Contact Us