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