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

Transcription

1 Cessna 550/551/560 (PWC JT15D) Initial Aircraft Type Training Course

2 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 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

3 Intentionally Left Blank

4 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.

5 COURSE DESCRIPTION The Aircraft Maintenance Engineer Training Course is a CAR 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.

6 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, using typical 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 and power 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 detailed procedures. b) Recall the safety precautions to be observed when working on or near the aircraft, power plant and 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 interrelationships with other systems, provide a detailed description of the subject using theoretical fundamentals and specific examples and to interpret results from various sources and measurements and apply corrective action where appropriate. b) Perform system, power plant, component and functional checks as specified in the aircraft maintenance manual. c) Demonstrate the use, interpret and apply appropriate documentation including structural repair manual, troubleshooting manual, etc. d) Correlate information for the purpose of making decisions in respect of fault diagnosis and rectification to maintenance manual level. e) Describe procedures for replacement of components unique to aircraft type.

7 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 Introduction Module Chapter 31 Indicating/Recording Systems Chapters Airframe Structures Module Chapter 29 Hydraulic Power Chapter 24 Electrical Power Chapter 32 Landing Gear Chapter 36 Pneumatic Chapter Engine Module Chapter 21 Air Conditioning Chapter 25 Equipment and Furnishings Chapter Chapter 38 Water/Waste Chapter 26 Fire Chapter 35 Oxygen Chapter 33 Lights Phase 3 Chapter 23 Chapter 22 Chapter 34 Communications Auto Flight Navigation

8 TIMETABLE WEEK ONE PERIOD DAY 1 DAY 2 DAY 3 DAY 4 DAY 5 05 Time limits/maint checks 24 Electrical Power 21 Air Conditioning 35 Oxygen 06 Dimensions/Areas 24 Electrical Power 21 Air Conditioning 35 Oxygen Dimensions/Areas 24 Electrical Power 21 Air Conditioning 07 Lifting and Shoring 24 Electrical Power 21 Air Conditioning 35 Oxygen 35 Oxygen 08 Levelling and Weighing 24 Electrical Power 21 Air Conditioning 35 Oxygen 08 Levelling and Weighing 24 Electrical Power 21 Air Conditioning 35 Oxygen BREAK ( ) 09 Towing and taxiing 24 Electrical Power 21 Air Conditioning 33 Lights 10 Parking/mooring, Storing and RTS 24 Electrical Power 21 Air Conditioning 33 Lights Parking/mooring, Storing and RTS 11 Placards and Markings 24 Electrical Power 21 Air Conditioning 24 Electrical Power 21 Air Conditioning 33 Lights 33 Lights 12 Servicing 24 Electrical Power 21 Air Conditioning 33 Lights 12 Servicing 24 Electrical Power 21 Air Conditioning 33 Lights BREAK ( ) 52 Doors 24 Electrical Power 21 Air Conditioning Aircraft Visit 52 Doors 24 Electrical Power 21 Air Conditioning Aircraft Visit Doors 24 Electrical Power 21 Air Conditioning 53 Fuselage 24 Electrical Power 21 Air Conditioning Aircraft Visit Aircraft Visit 54 Nacelles/Pylons 24 Electrical Power 21 Air Conditioning Aircraft Visit 54 Nacelles/Pylons 24 Electrical Power 21 Air Conditioning Aircraft Visit BREAK ( ) 55 Stabilisers 36 Pneumatic 21 Air Conditioning 31 INDICATING Phase 1 Examination 55 Stabilisers 36 Pneumatic 21 Air Conditioning 31 INDICATING Phase 1 Examination 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

9 TIMETABLE WEEK TWO PERIOD DAY 6 DAY 7 DAY 8 DAY 9 DAY 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 Hydraulic Power 27 Flight Controls 29 Hydraulic Power 27 Flight Controls 25 Equipment and Furnishings 25 Equipment and Furnishings 73 Engine Fuel and Control 73 Engine Fuel and Control 23 Communications 22 Auto Flight 29 Hydraulic Power 27 Flight Controls 38 Water/Waste 29 Hydraulic Power 27 Flight Controls 38 Water/Waste BREAK ( ) 73 Engine Fuel and Control 73 Engine Fuel and Control 22 Auto Flight 22 Auto Flight 27 Flight Controls 32 Landing Gear 26 Fire 74 Ignition 34 Navigation 27 Flight Controls 32 Landing Gear 26 Fire 74 Ignition 34 Navigation Flight Controls 32 Landing Gear 26 Fire 74 Ignition 34 Navigation 27 Flight Controls 32 Landing Gear 26 Fire 74 Ignition 34 Navigation 27 Flight Controls 32 Landing Gear 26 Fire 76 Engine controls 34 Navigation 27 Flight Controls 32 Landing Gear 26 Fire 76 Engine controls 34 Navigation BREAK ( ) 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 Flight Controls 32 Landing Gear 28 Fuel 27 Flight Controls 32 Landing Gear 28 Fuel 77 Engine Indicating Systems 77 Engine Indicating Systems Aircraft Visit 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 ( ) 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 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

10 LEVEL & DURATION INTRODUCTION MODULE B1 05 Time limits/maintenance checks Dimensions/Areas (MTOM, etc.) Lifting and Shoring Levelling and Weighing Towing and taxiing Parking/mooring, Storing and Return to Service Placards and Markings Servicing AIRFRAME STRUCTURES MODULE B1 53 Fuselage Nacelles/Pylons Stabilisers Windows Wings Doors AIRFRAME SYSTEMS B1 21 Air Conditioning Electrical Power Equipment and Furnishings Fire Flight Controls Fuel Systems Hydraulic Power Indicating/Recording Systems Landing Gear Lights Oxygen Pneumatic Water/Waste AVIONICS B1 22 Auto Flight Communications Navigation

11 ENGINE B1 71 Power Plant (Includes Ch. 72 Engine) Engine Fuel and Control Ignition Engine Controls Engine Indicating Systems Exhaust Oil AIRCRAFT PRACTICAL SESSIONS 4.00 TOTAL HOURS TUITION EXAMINATIONS 4.00 COURSE DURATION DAYS 10 COURSE INTRODUCTION 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 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 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

12 AIRCRAFT INTRODUCTION MODULE 4.00 Hours Tuition Level 1 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 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

13 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 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

14 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 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

15 COMPRESSION HEATING AND TEMPERATURE CONTROL SYSTEM COOLING SYSTEM AIR DISTRIBUTION PRESSURISATION CONTROL COOLING FANS CHAPTER 22 - AUTO FLIGHT 1.00 Hours Tuition Level 2 Name the major components of the Avionics System Honey Primus 1000 Auto Pilot System CHAPTER 23 - COMMUNICATIONS 1.00 Hours Tuition Level 2 Name the major components of communications system STATIC DISCHARGING AUDIO INTEGRATING SYSTEM AUDIO CONTROL PANELS OPERATION HONEYWELL VHF COMM SYSTEM COCKPIT VOICE RECORDER SYSTEM UNDERWATER ACOUSTIC LOCATING BEACON PASSENGER ADDRESS

16 CHAPTER 24 - ELECTRICAL POWER 6.00 Hours Tuition Level 3 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 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

17 CHAPTER 25 - EQUIPMENT & FURNISHINGS 1.25 Hours Tuition Level 3 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 EQUIPMENT AND FURNISHINGS CREW SEATS CABIN SEATS EMERGENCY LOCATOR TRANSMITTER SYSTEM CHAPTER 26 - FIRE PROTECTION 2.00 Hours Tuition Level 3 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 FIRE PROTECTION FIRE DETECTION ENGINE FIRE EXTINGUISHING PORTABLE FIRE EXTINGUISHER

18 CHAPTER 27 - FLIGHT CONTROLS 8.00 Hours Tuition Level 3 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 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

19 CHAPTER 28 - FUEL 2.50 Hours Tuition Level 3 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 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 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 COMPONENTS HYDRAULIC FILTERS FIREWALL SHUTOFF VALVES ENGINE-DRIVEN PUMPS HYDRAULIC MANIFOLD LOADING VALVE

20 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 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 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

21 CHAPTER 31 - INDICATING & RECORDING SYSTEMS 2.00 Hours Tuition Level 3 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 INDICATING AND RECORDING SYSTEMS INDEPENDENT INSTRUMENTS DIGITAL CLOCK CHAPTER 32 - LANDING GEAR 6.00 Hours Tuition Level 3 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 MAIN GEAR NOSE GEAR COMPONENTS CONTROLS AND INDICATIONS NOSE-WHEEL STEERING WHEELS BRAKE SYSTEM ANTISKID SYSTEM

22 CHAPTER 33 - LIGHTS 2.00 Hours Tuition Level 3 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 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 Identify and state the location of the Avionics System components Honeywell Primus Avionics System

23 CHAPTER 35 - OXYGEN 2.00 Hour Tuition Level 3 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 OXYGEN SYSTEM STORAGE SYSTEM CREW OXYGEN SYSTEM PASSENGER OXYGEN SYSTEM OXYGEN SYSTEM INSPECTIONS LIMITATIONS CHAPTER 36 - PNEUMATICS 2.00 Hour Tuition Level 3 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 BLEED-AIR SYSTEM PNEUMATIC CABIN ENTRY DOOR SEAL SYSTEM

24 CHAPTER 38 - WATER / WASTE 0.75 Hours Tuition Level 3 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 WATER WASTE SYSTEMS POTABLE WATER TOILET SYSTEM RELIEFTUBE CHAPTERS 71- POWER PLANT & ENGINE 1.25 Hours Tuition Level 3 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 POWERPLANT JT15D COMPRESSOR SYSTEM GEARBOX ASSEMBLY ACCELERATION BLEED-AIR FLOW HP BLEED-AIR FLOW BLEED VALVE CONNECTION ENGINE COWLS ENGINE DRAINS

25 73 ENGINE FUEL & CONTROL 2.00 Hours Tuition Level 3 Explain the operation of the fuel and control system Describe the indicating and warning systems State the engine operating limitations 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 Understanding of the safety precautions regarding the ignition system Detail the operation of the system Locate the system components ENGINE IGNITION SYSTEM IGNITION OPERATION CHAPTER 75 - AIR (in Chapter 71) State the sources of bleed air ENGINE AIRFLOW

26 CHAPTER 76 - ENGINE CONTROLS 1.75 Hours Tuition Level 3 Describe the power control systems State location of system components State the purpose of the emergency shutdown system ENGINE SYNCHRONISER GROUND IDLE SWITCH CHAPTER 77 - ENGINE INDICATING 1.25 Hours Tuition Level 3 State the engine indicating parameters Describe maintenance practices associated with engine indicating systems Locate system components Perform basic fault finding techniques ENGINE INDICATING SYSTEMS INTERTURBINE TEMPERATURE INDICATION CHAPTER 78 - EXHAUST 1.25 Hour Tuition Level 3 Describe the exhaust system State the maintenance practices associated with the exhaust system Exhaust Nozzle Thrust Reverser System

27 CHAPTER 79 - OIL 0.75 Hours Tuition Level 3 State the oil system indicating parameters Describe the oil system State the maintenance practices associated with the oil system State oil system limitations LUBRICATION SYSTEM OIL SYSTEM OPERATION OIL INDICATIONS CHAPTER 80 - STARTING (in Chapter 71 & 24) State the engine starting systems Describe the removal and replacement of the starter motor Describe the check of the starter motor brushes Starting Control