H 175 Course Syllabus

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1 HELICOPTERS Training Services H 175 Course Syllabus Additional Type Rating Pilot training 1

2 Contents #01 General Information p. 03 Course objective Prerequisites Registration Training duration Training location #02 Training p. 05 Theoretical Training program Practical Training program #03 Certificate p. 27 2

3 General Information Course Objective The Additional Type Rating course provides knowledge and proficiency to operate H 175 with a high level of safety and great efficiency, in accordance with EU 1178/2011 requirements. Pre-requisites A. Language The following language requirements are applicable in order to follow a course in English: ICAO English level 4 (Operational Level) is the minimum required proficiency level OR IELTS, International English Testing System, level 5 recommended, OR TOEIC, Test of English for International Communication, score of recommended. An Aeronautical English test is available for all trainees, free of charge, on the AHTS Learner Portal. In case English skills of the trainee are not in accordance with here above paragraph, the training shall be performed with the presence of an interpreter and the cost of the interpreter shall be met by the customer. Course duration may increase with an extra time of 20-30%. B. Medical aptitude Applicants to a type rating shall comply with course pre-entry requirements imposed by the Authorities. Consequently, they must provide a current valid medical certificate corresponding to the privileges of the license (class 1 or class 2 (EU) 1178/2011 regulation). C. Checks The eligibility conditions are checked by the instructor in charge of the first course during the trainee s registration, based on the information provided by the customer to the contract management/ahts-sales department prior to the arrival of the candidates. The requirements are confirmed by the instructor for each trainee (dates of licenses, etc.) on the first day of the first course. 3

4 General Information D. Technical Knowledge In order to undertake the training the candidate must satisfy the following conditions: Hold a Pilot s license issued by a relevant aviation authority; Have a minimum experience of 5 flight hours as a helicopter Pilot in Command (PIC) within the last 12 months; Depending on the qualification of the trainee, and based on the EU 1178/2011 regulation, the following requirements are to be met: o From SEP: Turbine pre-entry course / Multi-engine pre-entry course (1) / Valid ATPL(H) theory credit/ MCC/ Up-to date IR-H qualification o From SET: Multi-engine pre-entry course (1) / Valid ATPL(H) theory credit/ MCC/ Up-to-date IR-H qualification o From MET SP: Valid ATPL(H) theory credit/ MCC/ Up-do-date IR-H qualification (1) Or have passed at least the ATPL (H) theoretical knowledge. If this theoretical examination is not part of an integrate flying course the applicant shall have completed 70 Hours as PIC of helicopter Registration Information MANDATORY Passport / ID card (EU citizens only) Registration form (with personal address) Medical certificate Pilot license with type rating Last page of pilot logbook Copy to send by mail: support.registration.ahts@airbus.com contact.ahts@airbus.com In order to ease the administrative process, all documents shall be filled in and sent back to AHTS at the latest 45 days prior to the training session, to allow time for processing and eventually consideration by the relevant authorities or governments. Originals are to be presented the first day of the training course. Duration Single Pilot: Prog A: 24 Days VFR Prog C: 22 Days VFR Multi Pilot: Prog A: 24 Days VFR / 25 Days IFR Prog C: 22Days VFR / 23 Days IFR Location At AHTS site, Marignane, France OR at Customer s premises 4

5 Theoretical Program (73 hours 30 mins) Theoretical courses for initial and additional type rating training are the same except that for the Initial type rating, the applicant should have attended the relevant pre-entry turbine engine course. Consequently, the entire duration of all initial type rating courses shall take into account the duration of the pre-entry course at least. 1. OVERVIEW OF THE AIRCRAFT, STRUCTURE, TRANSMISSIONS, ROTORS AND EQUIPMENT, NORMAL AND ABNORMAL OPERATION OF THE SYSTEMS DIMENSIONS ENGINE - Engine type - Lubrication system - Fuel system - Ignition device - Starting circuit - Fire detection and protection system - Generators, alternators and drives systems - Power indicator - Engine controls - Utilization of the engine during the starting phases, malfunctions TRANSMISSION - Lubrication - Generator and generator drives system - Freewheels - Hydraulic pump drive - Indications and warnings 5

6 Theoretical Program TYPE OF ROTORS - indications and warnings FUEL SYSTEM - Location of fuel tanks, pumps, lines, valves and gages - Filtering, draining, transfer, venting. - Fuel system indicators and monitoring components, quantity and flow rate indications - Fuel distribution in the different tanks, fuel supply, and fuel drainage AIR CONDITIONING SYSTEM - Components and protection devices - Indicator/ Indicating system in the cockpit; interpretation according to operational conditions - Normal operation during start-up, cruise flight, approach and landing; conditioned air flow and temperature control ICE PROTECTION WINDSHIELD WIPER - Components of the ice protection system, including engine and rotor protections - Operation of the ice protection system during take-off, cruise flight and descent - Controls and indications during windshield wiper operation HYDRAULIC SYSTEM - Hydraulic system components, tank pressurizing components, aircraft components - Controls, monitoring units and indicators in the cockpit, function LANDING GEAR - Main components - Landing gear extraction/ retraction - Required tire pressure and related placard - Cockpit controls and indications including Extraction/ Retraction warnings - Emergency landing gear extension system 6

7 Theoretical Program FLIGHT CONTROLS - Stabilization system - Auto-pilot - Control and indicators of the system, including warnings ELECTRICAL POWER - Number, power, voltage, frequency, and, if applicable, phase and location of the main power systems (AC/DC) - Location of cockpit controls and indicators - Main and emergency power supplies to flight instruments - Location of circuit breakers for vital circuits - Operation of the aircraft power systems and power supply checking procedures FLIGHT INSTRUMENTS, COMMUNICATION, RADAR AND NAVIGATION SYSTEMS, AUTOPILOT - Antennas - Cockpit controls and instruments of the system Flight instruments (ASI, pitot system, compass system, flight director) Flight management system Radar systems (Weather radar, Transponder) Communication and navigation systems (HF, VHF, ADF, VOR/DME ILS, Marker) Area navigation system (GPS) Stabilization system and AP Cockpit and flight data recorder, radio altimeter Anti-collision system (PSB) Ground proximity warning system (PSB) Engine health and usage monitoring system (HUMS, PSB) COCKPIT, CABIN AND CARGO COMPARTMENT - Operation of exterior lights, and cockpit, cabin and cargo compartment lights - Operation of cabin doors and emergency exits 7

8 Theoretical Program EMERGENCY EQUIPMENT - Functioning and operating procedures for the following on board emergency equipment Removable equipment (portable extinguishers, emergency transmitters) Fixed equipment (emergency floatation gear) 2. LIMITATIONS - Limitations according to Flight manual - Minimum equipment list 3. PERFORMANCE, FLIGHT PREPARATION AND CONTROLS PERFORMANCE, COMPUTING PERFORMANCE RELATED TO SPEEDS, SLOPES, AND WEIGHTS IN ALL TAKEOFF, EN-ROUTE, APPROACH, AND LANDING CONDITIONS - Take-off Hover performance IGE and OGE Profiles approved categories A and B Height/ Speed chart Take-off distances and landing stopping distances Take-off decision point Computing distances of 1 st and 2 nd legs Climb performance - En-route Correction of IAS Service ceiling Optimum/Best-range cruising altitude Maximum endurance Maximum flight range 8

9 Theoretical Program Climb performance in cruise flight - Landing Hover IGE and OGE Landing distance Landing decision point - Knowledge and/or computing of: V1, VToss, Vy, VNE, etc. FLIGHT PREPARATION, NORMAL AND ABNORMAL CONDITIONS - Optimum/Maximum flight level - Minimum required flight altitude - Transition to descent procedure after engine failure in cruise flight - Power settings according to flight path and under various circumstances - Optimum and maximum flight level, and engine control after failure of one engine. EFFECT OF OPTIONAL EQUIPMENT ITEMS ON PERFORMANCE 4. WEIGHT AND BALANCE SERVICING WEIGHT AND BALANCE - Weight and balance sheets according to the maximum take-off and landing weights - CG limits - Influence of fuel consumption on CG - Attachment points, load tie-down, maximum ground load LINE OPERATION - Filling and draining points (fuel, oil, etc.) - Servicing safety rules. 9

10 Theoretical Program 5. EMERGENCY PROCEDURES Explain, analyse and summarize the Emergency procedures chapter, to use the helicopter in the conditions required for safe operations. 6. SPECIAL CONDITIONS REQUIRED FOR EXTENDING THE TYPE RATING TO COVER INSTRUMENT APPROACHES TO A DECISION HEIGHT OF LESS THAN 200 FT 7. SPECIAL CONDITIONS REQUIRED FOR HELICOPTERS EQIUPPED WITH ELECTRONIC FLIGHT INSTRUMENT SYSTEM (WHEN FITTED) DISPLAY SYSTEM - Flight control system Attitude/Heading Altitude/Height Speed Engine first limit indication Different configurations of flight control screens. - Selection of navigation sensors HSI mode Sector mode Sector/ Radar mode - Navigation screen symbology (Miscellaneous data) 10

11 Theoretical Program - Different navigation screen configurations Selection of navigation sensors Compass card mode Sector mode Sector/ Radar mode - Reconfiguration after failures Navigation sensors Attitude sensors Various data sensors FLIGHT CONTROL SYSTEM - Auto-pilot Architecture Trim actuators Sensors Safety devices related to auto-pilot - AFCS/ Auto-pilot Upper modes Coupling - Reconfiguration after failure Hydraulic actuator Electric actuator Computer 8. OPTIONAL EQUIPMENT 11

12 Practical program - VFR Flight N H 175 Flight titles SINGLE PILOT AND MULTI PILOT TRAINING PROGRAMS Prog. A Prog. C FFS FLIGHT FLIGHT 1 Handling VFR PF 02:00 01:30 2 Vehicle management VFR PF 02:00 01:30 3 Systems AFCS & FDS VFR PF + PM 02:00 02:00 4 Procedures (OEI) catb VFR PF + PM 01:30 01:30 5 Systems & Engines VFR PF + PM 01:30 01:30 6 Procedures (OEI) cat A VFR PF + PM 01:30 01:30 7 Navigation 2a VFR PF + PM 02:00 02:00 8 Navigation 3a IR PF + PM 9 Consolidation flight 1 VFR PF 01:30 10 Consolidation flight 2 VFR PF 01:30 V F R Total VFR Training by mean PF 12:30 03:00 11:30 Grand total VFR training PF 15:30 11:30 Skill Test 02:00 02:00 Total training and skill test PF 17:30 13:30 (Note: - Course duration may increase with an extra time of 20-30% with an interpreter - Flight 9 is performed as VFR flight when the training is VFR only). 12

13 Practical program - IFR Flight N H 175 Flight titles MULTI PILOT TRAINING PROGRAMS Prog. A Prog. C FFS FLIGHT FLIGHT ONLY 1 Handling VFR PF 02:00 01:30 2 Vehicle management VFR PF 02:00 01:30 3 Systems AFCS & FDS VFR PF + PM 02:00 02:00 4 Procedures (OEI) catb VFR PF + PM 01:30 01:30 5 Systems & Engines VFR PF + PM 01:30 01:30 6 Procedures (OEI) cat A VFR PF + PM 01:30 01:30 7 Navigation 2a IR PF + PM 02:00 02:00 8 Navigation 3a IR PF + PM 02:00 02:00 9 Consolidation flight 1 VFR PF 01:30 10 Consolidation flight 2 VFR PF 01:30 Total IR Ext Training by mean PF 04:00 04:00 I F R Total IR training by mean PF 14:30 03:00 13:30 Grand total IFR training - PF 17:30 13:30 Skill Test 02:00 02:00 Total IR training and skill test - PF 19:30 15:30 (Note: Course duration may increase with an extra time of 20-30% with an interpreter) 13

14 Practical program When the course is including synthetic training sessions, the name of the training course stipulates how the course is performed: - A when FFS level C/D is used; - C when training is entirely performed on actual aircraft FLIGHT N 1: Handling VFR (Prog A & C) NORMAL PROCEDURE - External check: Pre-flight check Internal checks Power up test Pre-start test and symbology of controls centring selection of VMS pages validation of weight data - Start-up procedure ENG switches on IDLE automatic ENG shut down not operative while N1 25% - After start-up check Start-up test OK Pre-flight test - Taxiing Check AFCS ON Rolling effect Anti-collision watch Speed and radius - Hovering: FLI correlation, follow-up trim efficiency 14

15 Practical program - Take-off procedure CAT.B respect of H/V diagram variation of TOP/MCP/RMCP on FLI - Climbing Variation of TOP/MCP/RMCP on FLI NR variation due to NR law - Cruising flight Environment and symbology of Flight Display System part time display NR variation due to NR law - AFCS basic modes flight controls and responses various turns stabilization and fly through modes (follow up, beep trim, over-ride, trim release) DSAS/SAS - Demonstration of limit light, VNE, aural warnings - Approach and Landing: Traffic pattern recommended approach procedure in CAT.B normal landing - Ground work - Anti-collision watch in flight - Engine shut down procedure: ENG switches on IDLE 60sec 15

16 Practical program FLIGHT N 2: Vehicle management VFR (Prog. A & C) NORMAL PROCEDURE - Traffic pattern: take-off and landing on clear areas - Concept of power reserve - Display of parameters - AFCS 3 axis coupled modes: engagement, modification - AFCS 4 axis coupled modes : engagement, modification - Improper references - AFCS demonstration: protections EMERGENCY PROCEDURE - Take-off and landings with OEI on clear areas - Use of AFCS upper modes in OEI situations - FLI symbology Internal battery overheating 16

17 Practical program FLIGHT N 3: Systems AFCS & FDS VFR (Prog. A & C) NORMAL PROCEDURE - Multi pilot focus: Declutch procedure must be tightly monitored if applied(if fitted) - Multi pilot focus: Re clutch procedure must be tightly monitored if applied(if fitted) - Take-offs and landings: Recommenced clear airfield procedure CAT.B, respect of H/V diagram, - Crosswind take-offs and landings - MTOW take-off and landing - Multi pilot focus: Taxiing and in flying situation EMERGENCY PRCEDURE - Flight Display System (FDS) AFCS failures (MCC): Analyse, confirmation, X-checks and QRH reading) MFD failures RADALT failure APIRS total failure AIR DATA failures Pitot clogging AMC failures - AFCS failures APCP failures Loss of APM Pitch, roll, yaw, Coll., SEMA failures - Multi pilot focus: aircraft management facing PF incapacity (if needed) 17

18 Practical program FLIGHT N 4: Procedures OEI Cat B. VFR (Prog. A & C) NORMAL PROCEDURE - Multi pilot focus: Engine fire on ground procedure must be tightly monitored - Take-offs and landings on clear areas - Running landing - Multi pilot focus: running landing monitoring: limitations, braking actions - Multi pilot focus: Taxiing and in flying situation, at least one crew member must watch outside for anti-collision EMERGENCY PROCEDURE - Engine fire on ground PNF actions management checked and confirmed by PF(FFS only) - Emergency CAT.B procedures with simulated engine failure - Multi pilot focus: Analyse, confirmation, X-checks and QRH reading) OEI in cruise MCP OEI in hover IGE 8ft OEI during take-off at height 50ft (aborted and continued take-off) OEI at landing OEI in cruise 3 and 4 axis coupled - Fire in engine bay - Inflight engine relighting (FFS only) - Autorotation and engine off landing (FFS only) - Fire in cargo bay - Multi pilot focus: as Engine Fire or Engine Failure is an important stress generator, the PNF must perform the dedicated actions after a tight and confirmed PF call out - Multi pilot focus: aircraft management facing PF incapacity (if needed) 18

19 Practical program FLIGHT N 5: Systems and engines VFR (Prog. A & C) NORMAL PROCEDURE - Take-offs and landings: Recommenced clear airfield elevated heliport procedures CAT.A - Multi pilot focus TDP Call out PF assistance by PNF on request - Equipment: TCAS - Multi pilot focus LDP, call out and PF assistance by PNF on request Taxiing and in flying situation, at least one crew member must watch outside for anticollision EMERGENCY PROCEDURE - Multi pilot focus: Analyse, confirmation, X-checks and QRH reading - Smoke in helicopter On the ground or in hover, over a possible landing site Inflight when immediate landing is impossible - Electric power system failure Battery overheating Generator failure Use of emergency Generator Short circuits - Power plant system failure Lubrication failure ENG CHIP detection Fuel filter clogging Engine governing malfunctions 19

20 Practical program - Fire in engine bay - Main Gearbox lubrication system failure Backup oil pump degradation Main oil pump failure MGB high oil temperature MGB CHIP detection IGB and TGB CHIP detection - Hydraulic system failure High temperature HYD 1 and/or 2 High pressure HYD 1 and/or 2 Low level HYD 1 and/or 2 AUX PUMP HYD 2 Brake low pressure HYD 2 Landing gear emergency extension 20

21 Practical program FLIGHT N 6: Procedure OEI Cat A. - VFR (Prog. A & C) NORMAL PROCEDURE - Take-offs and landings: CAT.A profiles on clear areas and elevated helipads (when available) - Multi pilot focus TDP Call out PF assistance by PNF on request - Multi pilot focus Taxiing and in flying situation, at least one crew member must watch outside for anticollision EMERGENCY PROCEDURE - On CAT.A profiles - Multi pilot focus: Analyse, confirmation, X-checks and QRH reading Simulated engine failure in hover 8ft Take-off with simulated engine failure before or at TDP Take-off with simulated engine failure after or at TDP Landing with simulated engine failure Aborted landing and OEI climb - Multi pilot focus: during OEI situation of flight, the PNF is in charge of parameters watching, radio pan call, and cockpit QRH reading and actions under PF request 21

22 Practical program FLIGHT N 7: Navigation 2a - VFR/IFR (Prog. A & C) NORMAL PROCEDURE - Special checks Radio com Radio navigation aids Radar Optional equipment - Preparation of radio navigation aids - Multi pilot focus Preparation of navigation systems and avionic (radio navigation-com, FMS or GPS) by PNF followed with a visual, called control and cross-check of PF AHCAS and departure briefing done with task sharing and PF control. Clear use of cockpit systems assistance(ap-coupling) - Take-off clear area with upper modes engagement - Navigation management during departure, cruise and approach Confirmation of legs displayed Radio navigation aids preparation and selection Respect of flight path Respect of altimeter settings Flight organization Radar display Efficient use of FMS Arrival preparation and briefing Control of armed and coupling system - Multi pilot focus Flight Organization Radio com monitoring 22

23 Practical program Log following Management of en-route systems Fuel endurance Task sharing clearly defined by PF - Approach and Landing Traffic pattern Recommended approach Landing procedure in CAT.A - Go around procedure - Multi pilot focus: Taxiing and in flying situation in VMC conditions, at least one crew member must watch outside for anti-collision EMERGENCY PROCEDURE - OEI during departure - OEI during cruise - System failure management - Multi pilot focus: Use of QRH for Reconfiguration - Any cockpit configuration change must be confirmed or called out - Unusual attitude recovery - Emergency descent in autorotation in IMC (IR) with NR control (full landing with ground recovery on FFS only) 23

24 Practical program FLIGHT N 8: Navigation 3a IFR (Prog. A & C) NORMAL PROCEDURE - Multi pilot focus Preparation of navigation and avionics systems (radio navigation-com, FMS or GPS) AHCAS and departure briefing done with task sharing and PF control - Take-off clear area with upper modes engagement - Navigation management during departure, cruise and approach Confirmation of legs displayed Radio navigation aids preparation and selection Respect of flight path Respect of altimeter settings Efficient use of FMS Arrival preparation and briefing Control of armed and coupling system - Systems (TCAS, public address) - Multi pilot focus Flight Organization Radio com monitoring Log following Management of en-route systems Fuel endurance and Task sharing clearly defined by PF - Approach and Landing Traffic pattern recommended approach and landing procedure in CAT.A: degraded situation - Go around procedure - Multi pilot focus: Taxiing and in flying situation in VMC conditions, at least one crew member must watch outside for anti-collision 24

25 Practical program EMERGENCY PROCEDURE - Multi pilot focus: Use of QRH for Reconfiguration, Any cockpit configuration change must be confirmed or called out. On CAT.A profiles OEI in cruise Landing with simulated engine, Aborted landing and OEI climb (Go around). - System failure and reconfiguration - Unusual attitude recovery - Emergency descent in autorotation in IMC with NR control (full landing with ground recovery on FFS only) FLIGHT N 9: Consolidation flight 1 - VFR (Prog. A) NORMAL PROCEDURE - Taxiing: various exercises - Use of AFCS while hovering - On CAT.A profiles: various take-off and landing - Slope landing - AFCS basic modes: change of flight parameters - Demonstration of limit light - AFCS upper modes exercises: 3 and 4 axis EMERGENCY PROCEDURE - Unusual attitude recovery - NR management in autorotation 25

26 Practical program FLIGHT N 10: Consolidation flight 2 - VFR (Prog. A) NORMAL PROCEDURE - Taxiing: various exercises - Use of AFCS while hovering - On CAT.A profiles: various take-off and landing - Equipment (TCAAA, HTAWS, DMAP, ECS, Floatation if fitted) EMERGENCY PROCEDURE - On CAT.A profiles Simulated engine failure in hover 8ft Take-off with simulated engine failure before or at TDP Take-off with simulated engine failure after or at TDP Landing with simulated engine Aborted landing and OEI climb - Emergency CAT.B procedures with simulated engine failure OEI in cruise MCP OEI in hover IGE 8ft OEI during take-off at height 50ft (aborted and continued take-off) 26

27 Certificate Evaluation A multiple choice question type examination covering theoretical knowledge will be proposed to the student. The pass mark is at least 75% per week for the theoretical knowledge examination. Certificate After successful completion, the trainee will be awarded a PART FCL certificate of approved training for the type rating. For more information on this course, please do not hesitate to contact us: contact.ahts@airbus.com support.sales.ahts.ah@airbus.com +33 (0) We are looking forward to seeing you at Airbus Helicopters Training Services! Thank you! 27

28 AIRBUS HELICOPTERS TRAINING SERVICES and its contents may not be disclosed. AIRBUS HELICOPTERS TRAINING SERVICES All Training rights reserved Services. 28 AIRBUS HELICOPTERS TRAINING SERVICES, Aeroport International Marseille Provence Marignane Cedex France 2017 All rights reserved, Airbus logo and the names of its products and services are registered trademarks. Airbus Helicopters Training Services reserves the right to make configuration and data changes at any time without notice. The facts and figures contained in this document and expressed in good faith do not constitute any offer or contract with Airbus Helicopters Photos by Airbus Helicopters, Anthony PECCHI, Jérome DEUILIN.

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