TRAINING NEEDS ANALYSIS COURSE SYLLABUS & CONTENT

TRAINING NEEDS ANALYSIS COURSE SYLLABUS & CONTENT Course Title: BOEING 787 GENERAL FAMILIARISATION FOUNDATION Mechanical (Electrical Power / Airframe / Powerplant / Avionics) General Standard This syllabus has been compiled in the sequence, which will normally be used for instruction. However, it may be necessary to vary this sequence from time to time in order to suit particular course planning requirements. Aircraft visits will occur during the course ideally at the times stated but more reasonably as aircraft are available. All visits are recorded on MON/PROC/138 Form 11. The course is designed for aircraft maintenance engineers to meet the standard of knowledge required for approval and licensing purposes. The course is based on the Boeing technical training requirement for entry on to a Boeing 787 B1/B2 line and base maintenance course, that the students are given a Foundation in B787 systems. The initial entry standard for training is normally holders of the appropriate PART 66 B1/2 or BCAR Section L Aircraft Maintenance Licences. In any case the student should be capable of full comprehension of the technical content. The course content and levels are to Part-66 Appendix II. Course Objective To provide a General Foundation and understanding with an introduction to the new technology of the B787 aircraft and its systems. On completion of the course the student will have sufficient knowledge to enable him/her to satisfactorily gain entry to the Boeing 787 B1/B2 Part 147 type approval course, subject to all other EASA / UK CAA conditions and company requirements being satisfied. Course Duration 30 hrs (5 Days @ 6hrs per day) Reference Material Manufacturers training material, maintenance, overhaul and repair manuals relevant to type. Service Bulletins, modification and newsletters. Examinations Certification There are no examination requirements for this course. A certificate will be issued at the end of each course to each student who has satisfactorily completed the course. Monarch Aircraft Engineering Ltd. Page 1 of 15 FOUNDATION GEN FAM TNA 14/10/2011

Hours of Tuition Monday To Friday, Six Hours Instruction Per Day. 08:30 10:00 Period 1 10:00 10:15 Morning Break 10:15 11:45 Period 2 11:45 12:30 Lunch 12:30 14:00 Period 3 14:00 14:15 Afternoon Break 14:15 15:45 Period 4 Monarch Aircraft Engineering Ltd. Page 2 of 15 FOUNDATION GEN FAM TNA 14/10/2011

BOEING 787 FOUNDATION AND GENERAL FAMILIARISATION COURSE (Electrical Power / Airframe / Powerplant/ Avionics ) Weekly Programme Week One Day Period 1 Subject Period 2 Subject Period 3 Subject Period 4 Subject 1 Introduction & Aircraft General Structures Common Core Systems Crew Alerting & Displays Doors Windows Core Information System Central Maintenance Computing Function 2 Electrical Systems Crew Information CIS Maintenance Laptop Data Management Indicating and Recording Oxygen Ice and Rain 3 Hydraulics Landing Gear & Brakes Flight Controls Fire Protection 4 Auto Flight Communication Navigation Lights Cabin Core Systems Water Waste 5 Air Conditioning Fuel Nitrogen Generation system APU Engine (GENX) Monarch Aircraft Engineering Ltd. Page 3 of 15 FOUNDATION GEN FAM TNA 14/10/2011

BOEING 787 FOUNDATION AND GENERAL FAMILIARISATION COURSE (Electrical Power / Airframe / Powerplant/ Avionics) SYLLABUS DAY ONE General Introduction & Manuals Introduction to the B787 including the following sub topics: INTRODUCTION & MANUALS a) Training Philosophy b) Boeing Learning Management System c) Electronic Notes and Classroom d) Introduction to CBT e) The Maintenance Toolbox f) Desk Top Simulation ATA 07 and 09 Ground Handling a) Structural Philosophy b) Dimensions and Areas c) Equipment Bays d) Flight Deck and Flight Deck Panels e) Aircraft Jacking Points and Procedures f) Towing and Taxiing ATA 12 Servicing a) Ground Servicing ATA 50 SERIES LEVEL 1 General description of the Airframe Structure including, construction and maintenance practices. To include the following sub topics: Structure 50 Series a) General Structure b) Composite Material Usage c) Fuselage Construction and Station Numbering d) Wing Structure and Station Numbering e) Pylons/Nacelles and Attachments f) Wing Control Surfaces g) Horizontal Stabiliser h) Elevators i) Vertical Stabiliser j) Rudder k) Composite repair l) Current Return Network (CRN) ATA 42-21 LEVEL 1 General description of the Common Core System To include the following sub topics: Common Core Systems (CCS) Time 1:00 hrs a) Introduction b) System Architecture Description c) System Components d) Common Computing Resource (CCR) e) Common Data Network (CDN) ATA 31-51 LEVEL 1 General description of the Caution and Warning Systems including, the following sub topics: Master Warn and Caution a) Introduction b) System Architecture Description Time 0:15 hrs Monarch Aircraft Engineering Ltd. Page 4 of 15 FOUNDATION GEN FAM TNA 14/10/2011

ATA 31-51 LEVEL 1 General description of the Display and Crew alerting systems including, maintenance practices and trouble-shooting. To include the following sub topics: Primary Display System (PDS) a) Introduction b) System Architecture Description c) System Components d) Head Down displays e) Head Up Displays f) Maintenance pages ATA 52 LEVEL 1 Detailed description of the Doors including, the following sub topics: Doors a) Doors Introduction b) General Location and Identification c) Passenger / Crew Entry Doors d) Fwd & Aft Cargo Doors e) Miscellaneous Service Doors f) Flight Compartment Door ATA 56 LEVEL 1 General description of the Windows, to include the following sub topics: Windows Time 0:15 hrs a) Flight Compartment Windows b) Passenger Compartment Windows c) Electrically Dimmable windows control d) Door-Mounted Windows ATA 46-11 LEVEL 1 General Introduction and description of the Core Network System including, the following sub topics: Core Network System a) Introduction b) System Architecture Description c) System Components Time 0:45 hrs ATA 45-11 LEVEL 1 General introduction and description of the Computer Maintenance system to include the following sub topics: Central Maintenance Computing Function (CMCF) Time 0:45 hrs a) Introduction b) System Architecture Description c) Electronic Flight Bag d) Maintenance laptop Monarch Aircraft Engineering Ltd. Page 5 of 15 FOUNDATION GEN FAM TNA 14/10/2011

DAY TWO ATA 24 LEVEL 3 Detailed description of the Electrical Power Systems including, maintenance practices and operation including trouble-shooting. To include the following sub topics: Electrical Power a) Electrical Power Introduction b) Electrical Power And Control c) Distribution General Description d) Electrical Component Locations e) Electrical Power - Operation f) Variable Frequency Starter Gen (VFSG) g) Generator Drive - Servicing h) APU Starter Generator i) 235 V AC Generation Introduction j) Generator Control Unit (GCU) k) Electrical Load Control Units ELCU l) APU Generator Control Unit (AGCU) m) AGCU APB Control n) Hi Voltage DC System General Description o) Common Motor Start Control Unit (CMSC) p) Electric Brake Power Supply Units (EBPSU) q) Auto Transformer Rectifier Unit (ATRU) r) Bus Power Control Unit (BPCU) s) External Power Introduction t) Ram Air Turbine (RAT) u) Main Battery v) APU Battery w) External Power Supply Indication x) Circuit Breaker Indication and Control (CBIC) y) Electronic Systems Indication and Control (ESIC) z) Towing Power Time 1:30 hrs ATA 46-12 LEVEL 1 General introduction and description of the Computer Maintenance Crew Information Systems to include the following sub topics: Crew Information System (CIS) a) Introduction b) System Architecture Description c) Terminal Wireless d) Data Networks e) Wired Connection f) Electronic Flight Bag g) MCDF functions h) Maintenance laptop i) Airplane Fault Isolation Time 0:45 hrs ATA 45 LEVEL 1 General introduction and description of the Data Management system to include the following sub topics: Data Management e) Introduction f) System Architecture Description g) Onboard Data Load Function (ODLF) h) Aircraft Condition Monitoring (ACMF) i) Electronic Flight Bag Time 0:45 hrs Monarch Aircraft Engineering Ltd. Page 6 of 15 FOUNDATION GEN FAM TNA 14/10/2011

ATA 31 LEVEL 1 General description of the Indicating and Recording Systems. To include the following sub topics: Indicating and Recording Systems Recorders a) DFDR/ACMS flight Data Recorder System b) FDRS - General Description c) Flight Deck Printer d) Video Surveillance Time 1:00 hours ATA 35 LEVEL 1 Detailed description of the Oxygen Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Oxygen a) General Description b) Control Panels c) Crew System Presentation d) Crew System Control and Indication e) Crew System Components f) Passenger System - General g) Passenger System Control and Indication h) Passenger System Components i) Portable Oxygen Equipment ATA 30 LEVEL 1 Detailed description of the Ice and Rain Protection Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Ice & Rain Protection Time 1:30 hrs a) Ice and Rain Protection Introduction b) Primary Ice detection system (PIDS) c) Engine Anti Ice Protection (EAI) d) Wing Ice Protection System (WIPS) e) Cabin Air Compressor Inlet Ice Protection (CIPS) f) Window heat g) Washer wiper system DAY THREE ATA 29 LEVEL 1 General description of the Hydraulic Power Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Hydraulic Power a) Hydraulic Schematic System diagram symbols b) Hydraulic Power c) Hydraulic Power Distribution d) Controls and Indications e) Panel Description f) Hydraulic Component Locations g) Engine-Driven Pump Hydraulic Control h) Engine-Driven Pump Electrical Control i) Electric Motor-Driven Pump (EMDP) j) Ram Air Turbine (RAT) Time 1:30 hrs Monarch Aircraft Engineering Ltd. Page 7 of 15 FOUNDATION GEN FAM TNA 14/10/2011

ATA 32 LEVEL 1 General description of the Landing Gear Systems. To include the following sub topics: Landing Gear Time 1:30 hrs a) Landing Gear -- General Description a) Proximity Sensor Electronic b) Main Landing Gear c) Landing Gear - Downlock Pins d) Main Landing Gear and Doors e) Nose Landing Gear f) Nose Landing Gear and Doors g) Landing Gear - Components h) Landing Gear - Controls and Indications i) MLG alternate Extension System - Control Mechanism Braking Systems a) Electric Brake System Description b) Brake System Components c) Controls and Indications d) Antiskid/Autobrake System e) Parking Brake System f) Brake system sensing g) Towing Power Nose wheel Steering a) Nose wheel steering. b) Electronic control. ATA 27 LEVEL 1 General description of the Flight Controls Systems including, operation. To include the following sub topics: Flight Controls a) Flight Controls - General Description. b) Flight Control Electronics (FCE) c) Primary Flight Control Function (PFCF) d) Flight Controls Hydraulic e) Controls and Indications f) Maintenance pages g) Rigging Ailerons a) Aileron and Aileron Trim Control System b) Flaperons Spoiler Systems a) Flight Spoiler Control System - General Description b) Speedbrake Operation c) Ground Spoiler d) Auto Speedbrake Rudder a) Rudder and Rudder Trim Control System b) Rudder Pressure Reducer c) Gust suppression system Elevator a) Elevator and Tab Control System Introduction b) Elevator System Components Overview a) Stall Warning System c) Elevator Feel Computer d) Elevator Feel and Centring system e) Elevator backdrive Horizontal Stabiliser a) Horizontal Stabilizer Trim Control System Introduction Time 2:00 hrs Monarch Aircraft Engineering Ltd. Page 8 of 15 FOUNDATION GEN FAM TNA 14/10/2011

b) Electric Motor EMCU c) Nose gear pressure transducers d) Stab Trim Stall Warning System b) SWS -- Control Column Shaker c) SWS -- Stall Warning Test Panel d) SWS - SMYD - Stall Management Yaw Damper e) Sws - Stall Management Yaw Damper f) CPC g) SWS - SMYD - Analog Interfaces - SMYD 1 h) SWS - SMYD - Digital Interface i) SWS - SMYD - BITE j) SWS - WSMYD BITE - Ground Tests High Lift Function a) High Lift Function (HLF) b) HLF modes c) TE Flap System - Controls and Indications d) TE Flap System Component Location e) Variable Camber trim Unit (VCTU) f) Alternate Flap Operation Leading Edge Flap Lift Augmentation a) LE Flap and Slat Control System Controls b) LE Flap and Slat Control System -- Indications c) LE Flap and Slat Control System -- Component Location ATA 26 LEVEL 1 General description of the Fire Protection Systems including the following sub topics: Fire Protection Time 1:00 hours a) Fire Protection - Fire Detection - Fire Alarms Engine Fire Protection a) Engine Fire Detectors b) Fire Protection -- Fire Extinguishing c) Engine Fire Extinguishing APU Fire Protection a) APU Fire Detection b) Overheat/Fire Test c) APU Ground Control Panel P40 Cargo Fire Protection a) Cargo Compartment Smoke Detection Lower b) Cargo Compartment Fire Extinguishing DAY FOUR ATA 22 LEVEL 1 General Description and operation of Automatic Flight Control System, Displays.To include the following sub topics: Automatic Pilot Flight Director System Time 1:30 hours General a) Control systems backdrive b) ATC uplink c) Autopilot Indications d) Flight Director Indications Thrust Management a) Locations b) Interface schematic c) Autothrottle Monarch Aircraft Engineering Ltd. Page 9 of 15 FOUNDATION GEN FAM TNA 14/10/2011

d) TMF input e) MCP operation f) PFD and EICAS Displays ATA 23 LEVEL 1 Description and Operation of Communications System including Trouble-shooting limited to the use of BITE systems. To include the following sub topics: Communications Emergency Locator Transmitter a) ELT - Component Location b) ELT - Interface c) ELT - Control Panel d) ELT - Transmitter e) ELT - Antenna f) ELT - Functional Description Data Comm Management Function (DCMF) a) General Description b) Operation Flight Interphone a) General b) Operation c) Audio Control Panel d) Interfaces e) Funct. Description Service Interphone a) Ground Crew Call System Introduction b) Ext. Comp. Location c) Flight Comp. Locations d) Interfaces Audio Gateway Unit (AGU) e) Flight Crew Call / Cabin Interphone VHF Communication a) Very High Frequency System b) VHF- Antenna Component Locations c) VHF - VHF 1 / 2 Transceiver Interfaces d) VHF-Tuning Control Panel (TCP) e) Audio Gateway Unit (AGU) f) VHF Communication System - Vhf Antenna g) VHF Communication System - Operation Selcal a) General SELCAL - Functional Description b) Selective Calling System - Introduction c) SELCAL - Flight Comp. Location HF Communication General a) High Frequency Communication b) HF - General Description c) HF - Flight Compartment Locations d) HF - Transceiver Location e) HF - Antenna Component Location f) HF - Interfaces g) HF - Control Panel Satcom a) General Functional description b) Sattellite High Gain antenna c) Diplex Module d) Operation Ground Crew Call a) General Functional description b) Crew Call Horn c) Operation Manual d) Operation Automatic. Time 1:30 hours Monarch Aircraft Engineering Ltd. Page 10 of 15 FOUNDATION GEN FAM TNA 14/10/2011

ATA 34 LEVEL 1 General Description and operation of Navigation system and Displays including Trouble- Shooting limited to the use of BITE systems. To include the following sub topics: Navigation Integrated Surveillance System a) General Description b) TCAS c) Weather radar Air Data Reference System a) Standby Indicators b) Description c) Air Data System Components d) Description e) Air Data SystemTest Earth Reference System a) Purpose b) General Description c) Attitude Heading Reference Units (AHRU) d) Inertial reference Unit (IRUS) e) ERS alignment f) Indications on PFD and ND Integrated Navigation Radio a) General b) GNSS c) ILS d) VOR e) GLS f) Components Locations g) Operation Integrated Standby Flight Display a) Purpose b) General Description Low Range Radio Altimeter a) General Description b) RA / DH - Control and Indication c) Operation d) Bite DME a) General Description b) Control and Indication c) Component Description d) DME Operation, Description ADF a) Control and Indication b) Components c) ADF Operation Flight Management Function (FMF) a) General b) FMS Components c) FMS Schematic d) LNAV e) VNAV Time 2:00 hours ATA 33 LEVEL 1 General description of the Lighting System including,, operation. To include the following sub topics: Lights a) Lights General Description b) Flight Compartment Lighting Time 1:00 hrs Monarch Aircraft Engineering Ltd. Page 11 of 15 FOUNDATION GEN FAM TNA 14/10/2011

c) Passenger Compartment Lighting d) Cargo and Service Compartment Lighting e) Exterior Lighting f) HID Lighting g) Emergency Lighting Power Supplies h) Anti Collision lights i) Runway Turnoff and landing j) Position lights ATA 44 10 LEVEL 1 General description of the Cabin Core system including, operation to include the following sub topics: Cabin Core Systems a) General Introduction b) Cabin Services Systems Controllers (CSSC) c) Cabin Zone Units d) Cabin attendants Panel e) Operation Time 1:00 hrs ATA 38 LEVEL 1 General description of the Water and Waste Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Water & Waste a) Potable Water b) Passenger Water System c) Water Service Panel d) Servicing Procedure e) Ultra Violet water treatment system f) Water Tank Air Pressurization g) Potable Water Tank - Pressurization Components h) Water Pressurisation - Electrical i) Water/Waste -- Toilet System j) Vacuum Toilet System k) Toilet System - Toilet Service Panel l) Toilet Flush Motor/Pump-Filter Assembly Function m) Vacuum Blowers DAY FIVE ATA 21 LEVEL 3 General description of the Air Conditioning and Pressurisation Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Air Conditioning / Pressurisation a) Cabin Air Compressors (CACs) b) Pack Valve Operation Operational Logic c) Pack Flow Operation d) Cooling e) Lower recirculation f) Air Cycle Machine g) Temperature Control Operation and Logic h) Pack/Zone Temperature Control i) Supplemental heating j) Fluid Cooling Systems (PECS) k) Equipment Cooling Systems l) Integrated Cooling system (ICS) Time 2:00 hrs Monarch Aircraft Engineering Ltd. Page 12 of 15 FOUNDATION GEN FAM TNA 14/10/2011

Pressurisation Digital System a) Digital Pressure Control b) Automatic Pressurization Control c) Manual Pressurization Control d) Data Input Interface e) Outflow Valve Interface f) Fwd and Aft Outflow Valve Assembly g) Positive Pressure Relief Valve h) Negative Pressure Relief Valve ATA 28 LEVEL 3 Detailed description of the Airframe Fuel Systems including, maintenance practices, operation and trouble-shooting. To include the following sub topics: Airframe Fuel System a) Introduction into System b) Fuel General Description and Operation c) Fuel - Storage - Integral Fuel Tanks d) Fuel -- Storage - Wing Fuel Tank Access Panels e) Fuel Tank Vent Operation f) Pressure Fuelling System g) Fuelling Operation h) Engine Fuel Feed System i) APU DC Boost Pump j) Main and Centre Tank Boost Pump Power Control k) Defueling l) Fuel Tank Scavenge System m) Fuel Quantity Indicating System - Operation n) Fuel Indication - Tank and Compensator Units o) Fuel Balance System Time 1:00 hrs ATA 49 LEVEL 3 Detailed description of the Auxiliary Power Unit(s) used on this aircraft including, construction, maintenance practices, operation and trouble-shooting. To include the following sub topics. Auxiliary Power Unit (APU) a) Introduction b) Auxiliary Power Unit General Description c) Auxiliary Power Unit (Allied Signal / GTCP) d) Airborne Auxiliary Power Controls e) APU Indications f) APU Engine g) Fuel Control Unit h) APU Fuel System i) Auxiliary Power Unit -- Ignition And Start System j) APU Ignition And Start System - SPU And SCU k) APU Starter-Generator l) Ignition System - General Description m) APU Controls - Electronic Control Unit - Inputs n) APU Indicating System o) APU Indicating System - Data Memory Module (DMM) p) APU Exhaust System - Exhaust Duct q) APU Exhaust System - Aft Fairing r) APU Lubrication System - Lube Module - Functional Description Monarch Aircraft Engineering Ltd. Page 13 of 15 FOUNDATION GEN FAM TNA 14/10/2011

ATA 71 LEVEL 3 General description of the Power Plant, To include the following sub topics: Power Plant & Installation a) General Introduction & Description of Engine b) Engine Station Numbering c) Airflow Paths & Stations d) Engine Cowlings & Opening/Closing Procedures e) Cowling Specific Features ATA 72 LEVEL 3 General description of the Engine including, construction,. To include the following sub topics: Engine Construction a) Engine -- General Description b) Engine Specification and Characteristics c) Engine -- General Dimensions d) Engine -- Accessory Drive Gearbox ATA 77 LEVEL 3 General description of the Engine Indicating Systems. To include the following sub topics: Engine Indicating a) Engine Indicating b) Fan Trim Balance ATA 76 LEVEL 3 General description of the Engine Controls. To include the following sub topics: Engine Controls and Power Management a) Engine Control System b) Forward Thrust Control System c) Reverse Thrust Control System d) Start Control System e) Engine Control Components ATA 73 LEVEL 3 Detailed description of the Engine Fuel and Control Systems,. To include the following sub topics: Engine Fuel & Control a) Engine Fuel And Control - b) Engine Fuel And Control - Distribution - Component Location c) Fuel Manifolds And Fuel Nozzles d) Engine Fuel And Control - Engine Control e) Engine Control - Interfaces f) EEC Modes g) Fuel Indicating - Introduction ATA 74 LEVEL 3 Detailed description of the Start and Ignition Systems including, maintenance practices, operation and trouble-shooting. Ignition System a) Engine Ignition -- Introduction b) Ignition System Monarch Aircraft Engineering Ltd. Page 14 of 15 FOUNDATION GEN FAM TNA 14/10/2011

ATA 80 LEVEL 3 General description of the Start and Ignition Systems including, maintenance practices, operation and trouble-shooting. Start a) Introduction into System b) Flight Deck Controls & Indications c) Electric Start ATA 75 LEVEL 3 General description of the Air Systems, To include the following sub topics. Air System a) Engine Air Systems Introduction b) Compressor Control c) Forward and Aft Bearing Sump Pressurizing d) Turbine Clearance Control e) Compressor Control ATA 79 LEVEL 3 General description of the Oil Systems including, To include the following sub topics: Oil System a) Introduction to System b) Oil Tank Mounting & Other Features c) Lube & Scavenge Pump d) Pressure Filter e) DMS f) Fuel/Oil Heat Exchanger ATA 78 LEVEL 3 Detailed description of the Exhaust Systems. To include the following sub topics: Exhaust & Thrust Reverser a) Introduction into Thrust Reverser System b) Thrust Reverser System Description c) Thrust Reverser Construction & Component Location d) Directional Control e) Drive System Installation & Maintenance Practices f) Deploy and Stow Operation & Control g) Cowl Opening & Systems Monarch Aircraft Engineering Ltd. Page 15 of 15 FOUNDATION GEN FAM TNA 14/10/2011