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Cessna 550/551/560 (PWC JT15D) Initial Aircraft Type Training Course CESSNA 550/551/560 (PWC JT15D) SPRINT AVIATION/ AVCADEMIA MAINTENANCE INITIAL

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Page 1: Cessna 550/551/560 (PWC JT15D) - AVCADEMIAavcademia.com/wp-content/uploads/2016/12/C560_Syllabus-Detailed.pdf · Cessna 550/551/560 (PWC JT15D) Initial Aircraft Type Training Course

Cessna 550/551/560 (PWC JT15D)

InitialAircraft Type Training

Course

CESSNA 550/551/560 (PWC JT15D) SPRINT AVIATION/ AVCADEMIA

MAINTENANCE INITIAL

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CONTENTS

INTRODUCTION 5 COURSE DESCRIPTION 6 COURSE OBJECTIVES 7 COURSE MATERIAL 8 TIMETABLE WEEK ONE 9 TIMETABLE WEEK TWO 10 LEVEL & DURATION 11 COURSE INTRODUCTION 12 MAINTENANCE MANUALS/PUBLICATIONS 12 AIRCRAFT INTRODUCTION MODULE 13 CHAPTER 05 - TIME LIMITS/MAINTENANCE CHECKS 13 CHAPTER 06 - AIRPLANE DIMENSIONS/AREAS 13 CHAPTER 07 - LIFTING AND SHORING 13 CHAPTER 08 - LEVELING AND WEIGHING 13 CHAPTER 09 - TOWING AND TAXIING 13 CHAPTER 10 - PARKING AND MOORING 14 CHAPTER 11 - PLACARDS AND MARKINGS 14 CHAPTER 12 - SERVICING 14 AIRFRAME STRUCTURES MODULE 14 CHAPTER 52 - DOORS 14 CHAPTER 53 - FUSELAGE 15 CHAPTER 54 - NACELLES/PYLONS 15 CHAPTER 56 - WINDOWS 15 CHAPTER 57 - WINGS 15 CHAPTER 21 - AIR CONDITIONING 15 CHAPTER 22 - AUTO FLIGHT 16 CHAPTER 23 - COMMUNICATIONS 16 CHAPTER 24 - ELECTRICAL POWER 17 CHAPTER 25 - EQUIPMENT & FURNISHINGS 18 CHAPTER 26 - FIRE PROTECTION 18 CHAPTER 27 - FLIGHT CONTROLS 19 CHAPTER 28 - FUEL 20 CHAPTER 29 - HYDRAULIC POWER 20 CHAPTER 30 - ICE AND RAIN PROTECTION 21 CHAPTER 31 - INDICATING & RECORDING SYSTEMS 22 CHAPTER 32 - LANDING GEAR 22 CHAPTER 33 - LIGHTS 23 CHAPTER 34 – NAVIGATION 23 CHAPTER 35 - OXYGEN 24 CHAPTER 36 - PNEUMATICS 24 CHAPTER 38 - WATER / WASTE 25 CHAPTERS 71- POWER PLANT & ENGINE 25 73 ENGINE FUEL & CONTROL 26 CHAPTER 74 - IGNITION 26 CHAPTER 75 - AIR (in Chapter 71) 26 CHAPTER 76 - ENGINE CONTROLS 27 CHAPTER 77 - ENGINE INDICATING 27 CHAPTER 78 - EXHAUST 27 CHAPTER 79 - OIL 28 CHAPTER 80 - STARTING (in Chapter 71 & 24) 28

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INTRODUCTION

Overview

The course is designed for the aircraft maintenance engineer to meet the standard of knowledge required for approval and licensing purposes. The initial entry standard for training is normally holders of the appropriate Transport Canada M2 license or Part-66 B1 Aircraft maintenance Licences.

The aim of the course is to provide an in depth understanding of the aircraft and its systems. On completion of the course the student will have sufficient knowledge to enable him/her to satisfactorily perform the duties of a certifying engineer for the above aircraft and to apply for issue or extension of a company authorisation, subject to all other TC conditions and company requirements being satisfied.

Examinations will be held at intervals through the course. These will be of the multi-choice type and a non-penalty marking system will be used. A minimum of 70% is required on each examination.

A certificate will be issued at the end of each course to each student who has satisfactorily completed the course and has passed all the examinations.

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COURSE DESCRIPTION

The Aircraft Maintenance Engineer Training Course is a CAR 566.18 company approved Type course.Upon successful completion and with regulatory agency approval, the technician may receive aircraft maintenance certification privileges for the Cessna 550/551/560 (PWC JT15D)The course is 10 days in length and focuses on the tasks required of the aircraft engineer operating in a line and base maintenance environment. The course provides extensive training on airframe and power plant systems as well as line oriented training on the aircraft’s avionics and electrical systems. The course will follow the subject syllabus.

The training is conducted at location of the customer’s choice.

Training is provided in the English language in the form of classroom lectures as well as supervised visits to the aircraft type in a maintenance environment. Classroom lectures make use of Computer Aided Instruction, slides, DVDs and a whiteboard.

Level 1: A brief overview of the airframe, systems and power plant as outlined in the Systems Description Section of the Aircraft Maintenance Manual/Instructions for Continued Airworthiness.

Level 2: Basic system overview of controls, indicators, principal components, including their location and purpose, servicing and minor troubleshooting. General knowledge of the theoretical and practical aspects of the subject.

Level 3: Detailed description, operation, component location, removal/ installation and bite and troubleshooting procedures to maintenance manual level.

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COURSE OBJECTIVES Level 1: A brief overview of the airframe, systems and power plant as outlined in the Systems Description Section of the Aircraft Maintenance Manual/Instructions for Continued Airworthiness.

Course objectives: Upon completion of Level 1 training, the student will be able to:

a) Provide a simple description of the whole subject, using common words and examples, usingtypical terms and identify safety precautions related to the airframe, its systems and power plant.

b) Identify aircraft manuals, maintenance practices important to the airframe, its systems andpower plant.

c) Define the general layout of the aircraft’s major systems.d) Define the general layout and characteristics of the power plant.e) Identify special tooling and test equipment used with the aircraft.

Level 2: Basic system overview of controls, indicators, principal components, including their location and purpose, servicing and minor troubleshooting. General knowledge of the theoretical and practical aspects of the subject.

Course objectives: In addition to the information contained in the Level 1 training, at the completion of Level 2 training, the student will be able to:

a) Understand the theoretical fundamentals; apply knowledge in a practical manner using detailedprocedures.

b) Recall the safety precautions to be observed when working on or near the aircraft, power plantand systems.

c) Describe systems and aircraft handling particularly access, power availability and sources.d) Identify the locations of the principal components.e) Explain the normal functioning of each major system, including terminology and nomenclature.f) Perform the procedures for servicing associated with the aircraft for the following systems: Fuel,

Power Plants, Hydraulics, Landing Gear, Water/Waste, and Oxygen.g) Demonstrate proficiency in use of crew reports and on-board reporting systems (minor

troubleshooting) and determine aircraft airworthiness per the MEL/CDL.h) Demonstrate the use, interpretation and application of appropriate documentation including

instructions for continued airworthiness, maintenance manual, illustrated parts catalogue, etc.

Level 3: Detailed description, operation, component location, removal/ installation and bite and troubleshooting procedures to maintenance manual level.

Course objectives: In addition to the information contained in Level 1 and Level 2 training, at the completion of Level 3 training, the student will be able to:

a) Demonstrate a theoretical knowledge of aircraft systems and structures and interrelationshipswith other systems, provide a detailed description of the subject using theoretical fundamentalsand specific examples and to interpret results from various sources and measurements andapply corrective action where appropriate.

b) Perform system, power plant, component and functional checks as specified in the aircraftmaintenance manual.

c) Demonstrate the use, interpret and apply appropriate documentation including structural repairmanual, troubleshooting manual, etc.

d) Correlate information for the purpose of making decisions in respect of fault diagnosis andrectification to maintenance manual level.

e) Describe procedures for replacement of components unique to aircraft type.

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COURSE MATERIAL

Each delegate will receive Training Manuals to enable them to assimilate the required knowledge for satisfactory completion of the course.

Programme

The standard training programme should not be more 8 hours of instruction per day with appropriate breaks and will typically follow the timings outlined below. Aircraft visits (dependent on availability) and examinations are not included in the tuition hours.

08:30 – 10:00 Period 1 13:00 – 15:00 Period 3 10:00 – 10:30 Morning Break 15:00 – 15:30 Afternoon Break 10:30 – 12:30 Period 2 15:30 – 17:30 Period 4 12:00 – 13:00 Lunch

Examination Phases

Phase 1 Phase 2

Chapters 05 – 12 Introduction Module Chapter 31 Indicating/Recording Systems

Chapters 52 – 57 Airframe Structures Module Chapter 29 Hydraulic Power

Chapter 24 Electrical Power Chapter 32 Landing Gear

Chapter 36 Pneumatic Chapter 71 - 80 Engine Module

Chapter 21 Air Conditioning Chapter 25 Equipment and Furnishings

Chapter 30 Ice and Rain Protection Chapter 38 Water/Waste

Chapter 26 Fire Protection Chapter 35 Oxygen

Chapter 33 Lights

Phase 3

Chapter 23 Communications

Chapter 22 Auto Flight

Chapter 34 Navigation

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TIMETABLE WEEK ONE

PERIOD DAY 1 DAY 2 DAY 3 DAY 4 DAY 5

0800 – 10.00

05 Time limits/maint checks

24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

35 Oxygen

06 Dimensions/Areas 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

35 Oxygen

06 Dimensions/Areas 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

35 Oxygen

07 Lifting and Shoring 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

35 Oxygen

08 Levelling and Weighing

24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

35 Oxygen

08 Levelling and Weighing

24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

35 Oxygen

BREAK (10.00 – 10.30)

10.30 – 12.30

09 Towing and taxiing 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

33 Lights

10 Parking/mooring, Storing and RTS

24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

33 Lights

10 Parking/mooring, Storing and RTS

24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

33 Lights

11 Placards and Markings

24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

33 Lights

12 Servicing 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

33 Lights

12 Servicing 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

33 Lights

BREAK (12.30 – 13.00)

13.00 – 15.00

52 Doors 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

Aircraft Visit

52 Doors 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

Aircraft Visit

52 Doors 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

Aircraft Visit

53 Fuselage 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

Aircraft Visit

54 Nacelles/Pylons 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

Aircraft Visit

54 Nacelles/Pylons 24 Electrical Power 21 Air Conditioning 30 Ice and Rain Protection

Aircraft Visit

BREAK (15.00 – 15.30)

15.30 – 17.30

55 Stabilisers 36 Pneumatic 21 Air Conditioning 31 INDICATING Phase 1 Examination

55 Stabilisers 36 Pneumatic 21 Air Conditioning 31 INDICATING Phase 1 Examination

56 Windows 36 Pneumatic 21 Air Conditioning 31 INDICATING Phase 1 Examination

56 Windows 36 Pneumatic 21 Air Conditioning 31 INDICATING Phase 1 Examination

57 Wings 36 Pneumatic 21 Air Conditioning 31 INDICATING Phase 1 Examination

57 Wings 36 Pneumatic 21 Air Conditioning 31 INDICATING Phase 1 Examination

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TIMETABLE WEEK TWO

PERIOD DAY 6 DAY 7 DAY 8 DAY 9 DAY 10

08.00 – 10.00

29 Hydraulic Power 27 Flight Controls 25 Equipment and Furnishings

73 Engine Fuel and Control

23 Communications

29 Hydraulic Power 27 Flight Controls 25 Equipment and Furnishings

73 Engine Fuel and Control

23 Communications

29 Hydraulic Power 27 Flight Controls 25 Equipment and Furnishings

73 Engine Fuel and Control

23 Communications

29 Hydraulic Power 27 Flight Controls 25 Equipment and Furnishings

73 Engine Fuel and Control

22 Auto Flight

29 Hydraulic Power 27 Flight Controls 38 Water/Waste 73 Engine Fuel and Control

22 Auto Flight

29 Hydraulic Power 27 Flight Controls 38 Water/Waste 73 Engine Fuel and Control

22 Auto Flight

BREAK (10.00 – 10.30)

10.30 – 12.30

27 Flight Controls 32 Landing Gear 26 Fire Protection 74 Ignition 34 Navigation

27 Flight Controls 32 Landing Gear 26 Fire Protection 74 Ignition 34 Navigation

27 Flight Controls 32 Landing Gear 26 Fire Protection 74 Ignition 34 Navigation

27 Flight Controls 32 Landing Gear 26 Fire Protection 74 Ignition 34 Navigation

27 Flight Controls 32 Landing Gear 26 Fire Protection 76 Engine controls 34 Navigation

27 Flight Controls 32 Landing Gear 26 Fire Protection 76 Engine controls 34 Navigation

BREAK (12.30 – 13.00)

13.00 – 1500

27 Flight Controls 32 Landing Gear 28 Fuel 76 Engine controls Aircraft Visit

27 Flight Controls 32 Landing Gear 28 Fuel 76 Engine controls Aircraft Visit

27 Flight Controls 32 Landing Gear 28 Fuel 77 Engine Indicating Systems

Aircraft Visit

27 Flight Controls 32 Landing Gear 28 Fuel 77 Engine Indicating Systems

Aircraft Visit

27 Flight Controls 32 Landing Gear 28 Fuel 77 Engine Indicating Systems

Aircraft Visit

27 Flight Controls 32 Landing Gear 28 Fuel 77 Engine Indicating Systems

Aircraft Visit

BREAK (15.00-15 30)

15.30 – 17.30

27 Flight Controls 32 Landing Gear 28 FUEL 78 Exhaust Phase 2 Examination

27 Flight Controls 32 Landing Gear 28 FUEL 78 Exhaust Phase 2 Examination

27 Flight Controls 32 Landing Gear 71 Powerplant 78 Exhaust Phase 2 Examination

27 Flight Controls 32 Landing Gear 71 Powerplant 78 Exhaust Phase 2 Examination

27 Flight Controls 32 Landing Gear 71 Powerplant 79 Oil Phase 2 Examination

27 Flight Controls 32 Landing Gear 71 Powerplant 79 Oil Phase 2 Examination

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LEVEL & DURATION

INTRODUCTION MODULE B1

05 Time limits/maintenance checks 1 0.50

06 Dimensions/Areas (MTOM, etc.) 1 0.50

07 Lifting and Shoring 1 0.50

08 Levelling and Weighing 1 0.50

09 Towing and taxiing 1 0.50

10 Parking/mooring, Storing and Return to Service 1 0.50

11 Placards and Markings 1 0.50

12 Servicing 1 0.50

AIRFRAME STRUCTURES MODULE B1

53 Fuselage 3 0.75

54 Nacelles/Pylons 3 0.50

55 Stabilisers 3 0.50

56 Windows 3 0.50

57 Wings 3 0.50

52 Doors 3 1.25

AIRFRAME SYSTEMS B1

21 Air Conditioning 3 8.00

24 Electrical Power 3 6.00

25 Equipment and Furnishings 3 1.25

26 Fire Protection 3 2.00

27 Flight Controls 3 8.00

28 Fuel Systems 3 2.50

29 Hydraulic Power 3 2.00

30 Ice and Rain Protection 3 6.00

31 Indicating/Recording Systems 3 2.00

32 Landing Gear 3 6.00

33 Lights 3 2.00

35 Oxygen 3 2.00

36 Pneumatic 3 2.00

38 Water/Waste 3 0.75

AVIONICS B1

22 Auto Flight 2 1.00

23 Communications 2 1.00

34 Navigation 2 2.00

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ENGINE B1

71 Power Plant (Includes Ch. 72 Engine) 3 1.25

73 Engine Fuel and Control 3 2.00

74 Ignition 3 1.25

76 Engine Controls 3 1.75

77 Engine Indicating Systems 3 1.25

78 Exhaust 3 1.25

79 Oil 3 0.75

AIRCRAFT PRACTICAL SESSIONS 4.00

TOTAL HOURS TUITION 76.00

EXAMINATIONS 4.00

COURSE DURATION DAYS 10

COURSE INTRODUCTION

Objectives

State the objectives of the Cessna 550/551/560 (PWC JT15D) B1 course Know the duration of the course, normal working hours and minimum attendance required Understand the examination requirements State the Fire Regulations relevant to the classroom location

Elements

Objectives and level of course Syllabus Duration and working hours Minimum attendance Examinations Fire Regulations Course critique Human Factors – Cessna 550/551/560 (PWC JT15D)

MAINTENANCE MANUALS/PUBLICATIONS

Objectives

Name the maintenance publications available to the technician as reference when maintaining the aircraft Select the appropriate service publication for instructor-selected maintenance tasks Describe the use of the Cessna 550/551/560 (PWC JT15D) Maintenance Manual

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AIRCRAFT INTRODUCTION MODULE 4.00 Hours Tuition – Level 1

Objectives

State the wing span, length (nose to tail), and tail height of the aircraft Explain the method used in determining the location of work areas and system components Explain the method for identifying access plates and inspection panels State the location of aircraft jacking points Name the publication that should be utilised when weighing the aircraft State the maximum nose gear turn limits that must not be exceeded when towing the aircraft Identifying the chapter of the maintenance manual that should be referred to when locating placards and markings

Elements

CHAPTER 05 - TIME LIMITS/MAINTENANCE CHECKS

COMPONENT TIME LIMIT

CHAPTER 06 - AIRPLANE DIMENSIONS/AREAS

AIRCRAFT LOCATIONS

AIRCRAFT ZONING

ACCESS PLATES AND PANEL IDENTIFICATION

CHAPTER 07 - LIFTING AND SHORING

JACKING

MAINTENANCE CONSIDERATIONS

CHAPTER 08 - LEVELING AND WEIGHING

LEVELLING

WEIGHING

CHAPTER 09 - TOWING AND TAXIING

TOWING

TAXIING

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CHAPTER 10 - PARKING AND MOORING

PARKING

MOORING

STORAGE

CHAPTER 11 - PLACARDS AND MARKINGS

INTERIOR PLACARDS

EXTERIOR PLACARDS

CHAPTER 12 - SERVICING

FUEL SYSTEM

ENGINE OIL SYSTEM

HYDRAULIC SYSTEM

BRAKE SYSTEM

AIRFRAME STRUCTURES MODULE 4.00 Hours Tuition – Level 3

Objectives

State the wing span, length (nose to tail), and tail height of the aircraft Explain the method used in determining the location of work areas and system components Explain the method for identifying access plates and inspection panels State the location of aircraft jacking points Name the publication that should be utilised when weighing the aircraft State the maximum nose gear turn limits that must not be exceeded when towing the aircraft Identifying the chapter of the maintenance manual that should be referred to when locating placards and markings

CHAPTER 52 - DOORS

PASSENGER/CREW DOOR

CABIN ENTRANCE STEP

DOOR WARNING SYSTEM

EMERGENCY EXIT DOOR

BAGGAGE DOORS

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CHAPTER 53 - FUSELAGE

RADOME

MAIN FRAME

FORWARD SIDE CONSOLES

STINGER ASSEMBLY

NOSE WHEEL WELL STRUCTURES

FLOOR PANELS

CHAPTER 54 - NACELLES/PYLONS

NACELLES & PYLONS

CHAPTER 56 - WINDOWS

FLIGHT COMPARTMENT WINDOWS

PASSENGER COMPARTMENT WINDOWS

LIMITATIONS

CHAPTER 57 - WINGS

WING ASSEMBLY

WING TIPS

CHAPTER 21 - AIR CONDITIONING 8.00 Hours Tuition – Level 3

Objectives

Name the major components of the air-conditioning system Explain the operating principle of the air cycle machine Explain how both Cabin and Flight Compartment Temperature is controlled in the automatic and manual modes Describe the abnormal indications of the air conditioning systems State the normal and maximum pressure differential of the pressurisation system Name the components of the pressurisation system and state their functions in maintaining cabin pressure Perform basic fault analysis, using the appropriate maintenance publications

Elements

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COMPRESSION

HEATING AND TEMPERATURE CONTROL SYSTEM

COOLING SYSTEM

AIR DISTRIBUTION

PRESSURISATION CONTROL

COOLING FANS

CHAPTER 22 - AUTO FLIGHT 1.00 Hours Tuition – Level 2

Objectives

Name the major components of the Avionics System

Elements

Honey Primus 1000 Auto Pilot System

CHAPTER 23 - COMMUNICATIONS 1.00 Hours Tuition – Level 2

Objectives

Name the major components of communications system

Elements

STATIC DISCHARGING

AUDIO INTEGRATING SYSTEM

AUDIO CONTROL PANELS OPERATION

HONEYWELL VHF COMM SYSTEM

COCKPIT VOICE RECORDER SYSTEM

UNDERWATER ACOUSTIC LOCATING BEACON

PASSENGER ADDRESS

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CHAPTER 24 - ELECTRICAL POWER 6.00 Hours Tuition – Level 3

Objectives

State the sources of electrical power Explain where electrical components are located Explain the AC and DC power distribution systems Explain the functional and operational checks of the AC and DC generating systems State the procedure to use when inspecting and/or checking the generator system Describe the procedure for replacing the generating system State the procedure for testing the generating system

Elements

POWER DISTRIBUTION SYSTEM

NICAD BATTERY SYSTEM

LEAD ACID BATTERY SYSTEM

EXTERNAL POWER

STARTER-GENERATORS

GENERATOR CONTROL UNITS

MAINTENANCE CONSIDERATIONS

GCU ADJUSTMENT

PRINTED CIRCUIT BOARDS

STARTING SYSTEM

STARTER DISENGAGE LIGHTS

AC POWER

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CHAPTER 25 - EQUIPMENT & FURNISHINGS 1.25 Hours Tuition – Level 3

Objectives

Recall the construction details and operation of cockpit seating Recall the cockpit furnishings Describe the operation of all interior doors Describe the passenger service units Describe removal and fitment of passenger and flight attendant seats List the emergency equipment carried

Elements

EQUIPMENT AND FURNISHINGS

CREW SEATS

CABIN SEATS

EMERGENCY LOCATOR TRANSMITTER SYSTEM

CHAPTER 26 - FIRE PROTECTION 2.00 Hours Tuition – Level 3

Objectives

Name the fire protection system components and state their location Name the type of agent used in the fire extinguishing systems State the number and types of fire detectors installed on the aircraft State the fire protection system operational check procedures Perform basic fault analysis using the appropriate maintenance publications

Elements

FIRE PROTECTION

FIRE DETECTION

ENGINE FIRE EXTINGUISHING

PORTABLE FIRE EXTINGUISHER

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CHAPTER 27 - FLIGHT CONTROLS 8.00 Hours Tuition – Level 3

Objectives

Identify and state the location of flight control system components Explain operations and indications of the flight control systems Perform basic fault analysis, using the appropriate maintenance publications State the basic rigging procedure for the flight control systems

Elements

FLIGHT CONTROLS

AILERON CONTROL SYSTEM

AILERON TRIM CONTROL SYSTEM

RUDDER CONTROL SYSTEM

RUDDER TRIM CONTROL SYSTEM

ELEVATOR CONTROL SYSTEM

ELEVATOR TRIM CONTROL SYSTEM

FLAP SYSTEM

SPEEDBRAKE SYSTEM

CONTROL LOCK SYSTEM

STICK SHAKER SYSTEM

SAFE FLIGHT ANGLE-OF-ATTACK SYSTEM

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CHAPTER 28 - FUEL 2.50 Hours Tuition – Level 3

Objectives

State the location of the major fuel system components Explain the type and function of the fuel quantity indicating and warning systems Explain the annunciation’s that indicate fuel boost pump and/or jet pump operation Describe the refuelling and defueling procedures Name the proper equipment for calibrating the fuel quantity indicating system Perform basic fault analysis using the appropriate maintenance publications

Elements

FUEL SYSTEM

FUEL STORAGE

FUEL TANK DRAIN VALVES

VENT SYSTEM

SURGE TANK

FUEL INDICATIONS

FUEL DISTRIBUTION SYSTEM

CHAPTER 29 - HYDRAULIC POWER 2.00 Hours Tuition – Level 3

Objectives

State the location of the hydraulic systems components Explain the procedure for servicing the hydraulic system reservoirs Explain the normal operation of the hydraulic systems Describe the purpose and function of the hydraulic system indicators and annunciators Perform basic fault analysis, using appropriate maintenance publications

Elements

COMPONENTS

HYDRAULIC FILTERS

FIREWALL SHUTOFF VALVES

ENGINE-DRIVEN PUMPS

HYDRAULIC MANIFOLD

LOADING VALVE

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RELIEF VALVE

CONTROL VALVES

SHUTTLE VALVE

CONTROLS AND INDICATIONS

HYDRAULIC SYSTEM OPERATION

LIMITATIONS

DIAGNOSTICS

BLEED HYDRAULIC SYSTEMS

HYDRAULIC SYSTEM CONTAMINATION

CHAPTER 30 - ICE AND RAIN PROTECTION 6.00 Hours Tuition – Level 3

Objectives

Identify and state the location of the ice and rain protection components Name the areas that are either anti-iced or de-iced Explain the purpose and function of the ice protection controls and indicators Perform basic fault analysis using appropriate maintenance publications

Elements

ANTI ICE SYSTEMS

ENGINE INLET ANTI-ICE

WINDSHIELD BLEED AIR ANTI-ICE

WINDSHIELD ALCOHOL ANTI-ICE

RAIN REMOVAL SYSTEM

PITOT-STATIC ANTI-ICE SYSTEM

HORIZONTAL STABILISER DE-ICE SYSTEM

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CHAPTER 31 - INDICATING & RECORDING SYSTEMS 2.00 Hours Tuition – Level 3

Objectives

Identify and state the location of the Avionics System components Explain the basic operation of the Systems State the controls and indications State the procedure for testing the equipment Perform in-situ checks to ascertain serviceability

Elements

INDICATING AND RECORDING SYSTEMS

INDEPENDENT INSTRUMENTS

DIGITAL CLOCK

CHAPTER 32 - LANDING GEAR 6.00 Hours Tuition – Level 3

Objectives State the location of the components in the landing gear system Explain normal landing gear extension and retraction operations Explain the control and indications of normal landing gear extension and retraction Explain alternate main gear extension operation and indications Name the appropriate maintenance publication used for repairing landing gear components Explain the operation and indications of the normal Brake System and the Anti-skid Systems Explain the operation and indication of the Emergency/Park Brake System Explain the normal operation of the Nose Wheel Steering System Perform basic fault analysis, using the appropriate maintenance publications

Elements

MAIN GEAR

NOSE GEAR

COMPONENTS

CONTROLS AND INDICATIONS

NOSE-WHEEL STEERING

WHEELS

BRAKE SYSTEM

ANTISKID SYSTEM

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CHAPTER 33 - LIGHTS 2.00 Hours Tuition – Level 3

Objectives

Describe the normal operation of the interior, exterior and emergency lighting systems Explain the periodic servicing, operational check and replacement requirements of the interior, exterior and emergency lighting systems. Perform basic fault analysis using the appropriate maintenance publications

Elements

LIGHTING SYSTEMS

INTERIOR LIGHTING SYSTEM

FLIGHT COMPARTMENT LIGHTING

PASSENGER COMPARTMENT LIGHTING

EMERGENCY LIGHTING

CARGO AND SERVICE COMPARTMENT LIGHTING

EXTERIOR LIGHTING

CHAPTER 34 – NAVIGATION 2.00 Hours Tuition – Level 2

Objectives

Identify and state the location of the Avionics System components

Elements

Honeywell Primus Avionics System

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CHAPTER 35 - OXYGEN 2.00 Hour Tuition – Level 3

Objectives

State the importance of the oxygen system State the location of the oxygen system components Explain the procedure for servicing the oxygen bottle Explain the operation of the oxygen system controls Explain the operation of the overpressure relief system State the safety precautions to be observed

Elements

OXYGEN SYSTEM

STORAGE SYSTEM

CREW OXYGEN SYSTEM

PASSENGER OXYGEN SYSTEM

OXYGEN SYSTEM INSPECTIONS

LIMITATIONS

CHAPTER 36 - PNEUMATICS 2.00 Hour Tuition – Level 3

Objectives

Name the major components of the Pneumatic System Recall the Component Location in the Pneumatic System Understand the detailed operation of the Pneumatic system Recall the indications of the Pneumatic System

Elements

BLEED-AIR SYSTEM

PNEUMATIC CABIN ENTRY DOOR SEAL SYSTEM

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CHAPTER 38 - WATER / WASTE 0.75 Hours Tuition – Level 3

Objectives

Name the major components of the Water/Waste System Recall the Component Location in the Water/Waste System Understand the detailed operation of Water/Waste system Recall the indications of the Water/Waste System

Elements

WATER WASTE SYSTEMS

POTABLE WATER

TOILET SYSTEM

RELIEFTUBE

CHAPTERS 71- POWER PLANT & ENGINE 1.25 Hours Tuition – Level 3

Objectives

State the type of engine fitted to the aircraft Detail the checks required after installation Detail the starting and running procedures Describe the general operation of the engine Describe the engine cowlings and mountings State the location of the fire seals State the electrical system requirements Describe the engine air intake systems Describe the engine drains system

Elements

POWERPLANT JT15D

COMPRESSOR SYSTEM

GEARBOX ASSEMBLY

ACCELERATION BLEED-AIR FLOW

HP BLEED-AIR FLOW

BLEED VALVE CONNECTION

ENGINE COWLS

ENGINE DRAINS

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73 ENGINE FUEL & CONTROL 2.00 Hours Tuition – Level 3

Objectives

Explain the operation of the fuel and control system Describe the indicating and warning systems State the engine operating limitations

Elements

ENGINE FUEL SYSTEM

THROTTLE POWER CONTROL SYSTEM

ENGINE TT2 SENSOR

FUEL MANIFOLD

FUEL NOZZLE

LP SHAFT TRIP SENSOR

CHAPTER 74 - IGNITION 1.25 Hour Tuition – Level 3

Objectives

Understanding of the safety precautions regarding the ignition system Detail the operation of the system Locate the system components

Elements

ENGINE IGNITION SYSTEM

IGNITION OPERATION

CHAPTER 75 - AIR (in Chapter 71)

Objectives

State the sources of bleed air

Elements

ENGINE AIRFLOW

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CHAPTER 76 - ENGINE CONTROLS 1.75 Hours Tuition – Level 3

Objectives

Describe the power control systems State location of system components State the purpose of the emergency shutdown system

Elements

ENGINE SYNCHRONISER

GROUND IDLE SWITCH

CHAPTER 77 - ENGINE INDICATING 1.25 Hours Tuition – Level 3

Objectives

State the engine indicating parameters Describe maintenance practices associated with engine indicating systems Locate system components Perform basic fault finding techniques

Elements

ENGINE INDICATING SYSTEMS

INTERTURBINE TEMPERATURE INDICATION

CHAPTER 78 - EXHAUST 1.25 Hour Tuition – Level 3

Objectives

Describe the exhaust system State the maintenance practices associated with the exhaust system

Elements

Exhaust Nozzle Thrust Reverser System

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CHAPTER 79 - OIL 0.75 Hours Tuition – Level 3

Objectives

State the oil system indicating parameters Describe the oil system State the maintenance practices associated with the oil system State oil system limitations

Elements

LUBRICATION SYSTEM

OIL SYSTEM OPERATION

OIL INDICATIONS

CHAPTER 80 - STARTING (in Chapter 71 & 24)

Objectives

State the engine starting systems Describe the removal and replacement of the starter motor Describe the check of the starter motor brushes

Elements

Starting Control

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