Class Rating Instructor Course ME (A)

(TM 051 - Appendix C) EU part FCL Class Rating Instructor Course ME (A) 1. Groundschool syllabus 2. Flight syllabus Note: The company name and logo SAI BV has been changed into the new company name and logo AVION TRAINING. COPYRIGHT Avion Training No part of this manual or its extracts may be reproduced in any form, by print, photoprint, microfilm or any other means, without written permission from Avion Training. Issue 01 Page 1-40

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1. GROUNSCHOOL SYLLABUS 7 1.1 PART 1: TEACHING AN LEARNING 7 1.2 PART 2: TECHNICAL THEORETICAL KNOWLEGE 7 1.2.1 Theoretical overview... 7 1.2.2 Lesson 1... 8 1.2.3 Lesson 2... 9 1.2.4 Lesson 3... 10 1.2.5 Lesson 4... 11 1.2.6 Lesson 5... 12 1.2.7 Lesson 6... 13 1.2.8 Lesson 7: long briefing 1... 14 1.2.9 Lesson 8: long briefing 2... 15 1.2.10 Lesson 9: long briefing 3... 16 1.2.11 Lesson 10: long briefing 4... 17 1.2.12 Lesson 11: long briefing 5... 19 1.2.13 Assessment form long briefings... 26 Issue 01 Page 5-40

2. FLIGHT SYLLBUS (PART 3) 27 2.1 FLIGHT TRAINING OVERVIEW FNPTII, ME(SP) 27 2.2 FLIGHT REGISTRATION FORMS 29 2.2.1 01: airscraft systems, emergencies, runup, shutdown... 29 2.2.2 02: TAXI, Take off, climbing, level flight, descending... 31 2.2.3 03: turns, slow flight, stalling... 33 2.2.4 04: effect assymetric trust, engine failures/engine fires... 35 2.2.5 05: IFR BASIC training, IFR AVANCE TRAINING... 37 2.2.6 06: Circuits... 39 Page 6-40 Issue 01

1. GROUNSCHOOL SYLLABUS 1.1 PART 1: TEACHING AN LEARNING The content of the teaching and learning part of the FI training course, as established in AMC1 FCL.930.FI FI, should be used as guidance for this course (doc nr. 051 TM, appendix A, chapter 1). 1.2 PART 2: TECHNICAL THEORETICAL KNOWLEGE This syllabus is concerned only with the training on ME aeroplanes. Therefore, other knowledge areas, common to both SE and ME aeroplanes, should be revised as necessary to cover the handling and operating of the aeroplane with all engines operative, using the applicable sections of the ground subjects syllabus for the FI course. Additionally, the ground training includes 25:30 hours of classroom work to develop the applicant s ability to teach a student the knowledge and understanding required for the air exercise section of the ME training course. 1.2.1 THEORETICAL OVERVIEW The breakdown of course classroom hours is as follows: Tuition Practice in class Topic Progress test Lesson 1 1:00 Aviation legislation 1:00 Lesson 2 2:00 0:30 Lesson 3 2:00 Lesson 4 2:00 Performance, all engines operating, including mass and balance Asymmetric flight Principles of flight Control in asymmetric flight Minimum control and safety speeds Feathering and un-feathering Lesson 5 2:00 Performance in asymmetric flight 1:00 Lesson 6 2:00 1:30 Specific type of aeroplane operation of systems Airframe and engine limitations 1:00 Lesson 7-11 4:30 5:00 Briefings for air exercises progress 15:30 7:00 3:00 Course total 25:30 (including progress tests) Remark: Mock-up training (M/U) will be performed as being practice in class. The ATPL books cover all the items and are leading in the theoretical course.the progress tests need to be passed by at least 75%. The theoretical knowledge course must be satisfactorily completed before starting the practical part of the course. Issue 01 Page 7-40

1.2.2 LESSON 1 ATE Planning Actual INSTRUCTOR Tuition 1:00 STUENT Practice 0:00. AIR LEGISLATION Aeroplane performance group definitions Methods of factoring gross performance. ATE PERFORME SCORE SIGNATURE INSTRUCTOR PROGRESS TEST 1 Page 8-40 Issue 01

1.2.3 LESSON 2 ATE Planning Actual INSTRUCTOR Tuition 2:00 STUENT Practice 1:00 MASS AN BALANCE (To be covered in conjunction with the flight/owner s manual/pilot s operating handbook) mass and balance documentation for aeroplane type revision of basic principles calculations for specific aeroplane type MASS AN PERFORMANCE (To be covered in conjunction with the flight/owner s manual/pilot s operating handbook) calculations for specific aeroplane type (all engines operating) take-off run take-off distance accelerate/stop distance landing distance landing run take-off/climb out flight path calculations for specific aeroplane type (one engine operating) Issue 01 Page 9-40

1.2.4 LESSON 3 ATE Planning Actual INSTRUCTOR Tuition 2:00 STUENT Practice 0:00 ASYMMETRIC POWER FLIGHT, PRINCIPLES OF FLIGHT THE PROBLEMS Asymmetry Control performance THE FORCES AN COUPLES offset thrust line asymmetric blade effect offset drag line failed engine propeller drag total drag increase asymmetry of lift uneven propeller slipstream effect effect of yaw in level and turning flight thrust and rudder side force couples effect on moment arms Page 10-40 Issue 01

1.2.5 LESSON 4 ATE Planning Actual INSTRUCTOR Tuition 2:00 STUENT Practice 0:00 CONTROL IN ASYMMETRIC POWER FLIGHT use, misuse and limits of: rudder aileron elevators effect of bank/sideslip/balance decrease of aileron/rudder effectiveness fin stall possibility effect of ias/thrust relationship effect of residual unbalanced forces foot loads and trimming MINIMUM CONTROL AN SAFETY SPEES minimum control speed (Vmc) definition Origin factors affecting Vmc thrust mass and centre of gravity position altitude landing gear flaps cowl flaps/cooling gills turbulence/gusts pilot reaction/competence banking towards the operating engine drag feathering critical engine take-off safety speed definition/origin of V2 other relevant V codes Issue 01 Page 11-40

1.2.6 LESSON 5 ATE Planning Actual INSTRUCTOR Tuition 2:00 STUENT Practice 0:00 AEROPLANE PERFORMANCE ONE ENGINE INOPERATIVE effect on excess power available single-engine ceiling cruising, range and endurance acceleration/deceleration zero thrust, definition and purpose PROPELLERS variable pitch general principles feathering/unfeathering mechanism and limitations (e g minimum rpm) ATE PERFORME SCORE SIGNATURE INSTRUCTOR PROGRESS TEST 2 Page 12-40 Issue 01

1.2.7 LESSON 6 ATE Planning Actual INSTRUCTOR Tuition 2:00 STUENT Practice 1:30 AEROPLANE AN ENGINE SYSTEMS operation normal operation abnormal emergency procedures LIMITATIONS AIRFRAME load factors landing gear/flap limiting speeds (Vlo and Vfe) rough air speed (Vra) maximum speeds (Vno and Vne) LIMITATIONS ENGINE rpm and manifold pressure oil temperature and pressure emergency procedures ATE PERFORME SCORE SIGNATURE INSTRUCTOR PROGRESS TEST 3 Issue 01 Page 13-40

1.2.8 LESSON 7: LONG BRIEFING 1 ATE Planning Actual INSTRUCTOR Tuition 1:00 STUENT Briefing 1:00 EXERCISE 1: FAMILIARISATION WITH THE AEROPLANE introduction to the aeroplane explanation of the cockpit layout systems and controls aeroplane power plant checklists and drills differences when occupying the instructor s seat emergency drills action in event of fire in the air and on the ground escape drills: location of exits and use of emergency equipment (for example fire extinguishers, etc.) pre-flight preparation and aeroplane inspection aeroplane documentation external checks internal checks harness, seat or rudder pedal adjustment engine starting procedures use of checklists checks before starting checks after starting Page 14-40 Issue 01

1.2.9 LESSON 8: LONG BRIEFING 2 ATE Planning Actual INSTRUCTOR Tuition 0:30 STUENT Briefing 1:00 EXERCISE 2: TAXIING pre-taxiing area precautions (greater mass: greater inertia) effect of differential power precautions on narrow taxiways pre take-off procedures use of checklist engine power checks pre take-off checks instructor s briefing to cover the procedure to be followed should an emergency occur during takeoff, for example engine failure the take-off and initial climb ATC considerations factors affecting the length of the take-off run or distance correct lift-off speed importance of safety speed crosswind take-off, considerations and procedures short field take-off, considerations and procedures engine handling after take-off: throttle, pitch and engine synchronisation climbing pre-climbing checks engine considerations (use of throttle or pitch controls) maximum rate of climb speed maximum angle of climb speed synchronising the engines Issue 01 Page 15-40

1.2.10 LESSON 9: LONG BRIEFING 3 ATE Planning Actual INSTRUCTOR Tuition 0:30 STUENT Briefing 1:00 EXERCISE 3. STRAIGHT AN LEVEL FLIGHT selection of power: throttle or pitch controls engine synchronisation fuel consumption aspects use of trimming controls: elevator and rudder (aileron as applicable) operation of flaps effect on pitch attitude effect on air speed operation of landing gear effect on pitch attitude effect on air speed use of mixture controls use of alternate air or carburettor heat controls operation of cowl flaps or cooling gills use of cabin ventilation and heating systems operation and use of the other systems (as applicable to type) descending pre-descent checks normal descent selection of throttle or pitch controls engine cooling considerations emergency descent procedure turning medium turns climbing and descending turns steep turns (45 of bank or more) Page 16-40 Issue 01

1.2.11 LESSON 10: LONG BRIEFING 4 ATE Planning Actual INSTRUCTOR Tuition 0:30 STUENT Briefing 1:00 EXERCISE 4. SLOW FLIGHT aeroplane handling characteristics during slow flight: flight at vs1 and vso +5 knots simulated go-around from slow flight at Vsse with flaps down note pitch trim change stalling power selection symptoms approaching the stall full stall characteristics recovery from the full stall recovery at the incipient stall stalling and recovery in the landing configuration recovery at the incipient stage in the landing configuration instrument flight (basic) straight and level climbing turning descending emergency drills (not including engine failure), as applicable to type Issue 01 Page 17-40

continued circuit approach and landing downwind leg air speed below vfe use of flaps (as applicable) pre-landing checks position to turn onto base leg base leg selection of power (throttle or pitch), flaps and trimming controls maintenance of correct air speed final approach power adjustments (early reaction to undershooting) use of additional flaps (as required) confirmation of landing gear down selection touch down point air speed reduction to Vat maintenance of approach path landing greater sink rate longer landing distance and run crosswind approach and landing crosswind considerations short field approach and landing short field procedure: considerations Page 18-40 Issue 01

1.2.12 LESSON 11: LONG BRIEFING 5 ATE Planning Actual INSTRUCTOR Tuition 2:00 STUENT Briefing 1:00 EXERCISE 5. FLIGHT ON ASYMMETRIC POWER introduction to asymmetric flight feathering the propeller: method of operation effects on aeroplane handling at cruising speed introduction to effects upon aeroplane performance note foot load to maintain a constant heading (no rudder trim) un-feathering the propeller return to normal flight finding the zero thrust setting comparison of foot load when feathered and with zero thrust set effects and recognition of engine failure in level flight forces and the effects of yaw types of failure sudden or gradual complete or partial yaw, direction and further effects of yaw flight instrument indications identification of failed engine the couples and residual out of balance forces: resultant flight attitude use of rudder to counteract yaw use of aileron: dangers of misuse use of elevator to maintain level flight use of power to maintain a safe air speed and altitude supplementary recovery to straight and level flight: simultaneous increase of speed and reduction in power identification of failed engine: idle leg = idle engine Issue 01 Page 19-40

continued use of engine instruments for identification fuel pressure or flow RPM gauge response effect of CSU action at lower and higher air speed engine temperature gauges confirmation of identification: close the throttle of identified failed engine effects and recognition of engine failure in turns identification and control side forces and effects of yaw uring turning flight effect of inside engine failure: effect sudden and pronounced effect of outside engine failure: effect less sudden and pronounced the possibility of confusion in identification (particularly at low power) correct use of rudder possible need to return to lateral level flight to confirm correct identification visual and flight instrument indications effect of varying speed and power speed and thrust relationship at normal cruising speed and cruising power: engine failure clearly recognised at low safe speed and climb power: engine failure most positively recognised high speed descent and low power: possible failure to notice asymmetry (engine failure) Minimum control speeds ASI colour coding: red radial line Note: this exercise is concerned with the ultimate boundaries of controllability in various conditions that a student can reach in a steady asymmetric power state, approached by a gradual speed reduction. Sudden and complete failure should not be given at the Flight Manual vmca. The purpose of the exercise is to continue the gradual introduction of a student to control an aeroplane in asymmetric power flight during extreme or critical situations. It is not a demonstration of vmca Techniques for assessing critical speeds with wings level and recovery: dangers involved when minimum control speed and the stalling speed are very close: use of Vsse Establish a minimum control speed for each asymmetrically disposed engine to establish critical engine (if applicable) Effects on minimum control speeds of bank zero thrust setting take-off configuration landing gear down and take-off flap set Page 20-40 Issue 01

continued landing gear up and take-off flap set Note: it is important to appreciate that the use of 5 of bank towards the operating engine produces a lower vmca and also a better performance than that obtained with the wings held level. It is now normal for manufacturers to use 5 of bank in this manner when determining the vmca for the specific type. Thus, the vmca quoted in the aeroplane manual will have been obtained using the technique. Feathering and un-feathering minimum heights for practising feathering or un-feathering drills engine handling: precautions (overheating, icing conditions, priming, warm-up, method of simulating engine failure: reference to aeroplane engine manual and service instructions and bulletins) Engine failure procedure once the maintenance of control has been achieved, the order in which the procedures are carried out will be determined by the phase of operation and the aeroplane type flight phase in cruising flight critical phase such as immediately after take-off or during the approach to landing or during a go-around Aeroplane type* In-flight engine failure in cruise or other flight phase not including take-off or landing immediate actions recognition of asymmetric condition and control of the aeroplane identification and confirmation of failed engine idle leg = idle engine closing of throttle for confirmation cause and fire check typical reasons for failure methods of rectification feathering decision and procedure reduction of other drag need for speed but not haste use of rudder trim subsequent actions live engine temperature, pressures and power remaining services electrical load: assess and reduce as necessary Issue 01 Page 21-40

continued effect on power source for air driven instruments landing gear flaps and other services re-plan flight ATC and weather terrain clearance, SE cruise speed decision to divert or continue fuel management: best use of remaining fuel dangers of re-starting damaged engine action if unable to maintain altitude: effect of altitude on power available effects on performance effects on power available and power required effects on various airframe configuration and propeller settings use of flight manual or equivalent document (for example owner s manual or pilot s operating handbook) cruising climbing: ASI colour coding (blue line) descending turning live engine limitations and handling take-off and approach: control and performance Significant factors significance of take-off safety speed effect of landing gear, flap, feathering, take-off, trim setting, systems for operating landing gear and flaps effect on mass, altitude and temperature (performance) significance of best SE climb speed (Vyse) acceleration to best engine climb speed and establishing a positive climb relationship of SE climb speed to normal climb speed action if unable to climb significance of asymmetric committal height and speed: action if baulked below asymmetric committal height Page 22-40 Issue 01

continued Engine failure during take-off below vmca or unstick speed accelerate or stop distance considerations prior use of flight manual data if available above vmca or unstick speed and below safety speed immediate re-landing or use of remaining power to achieve forced landing considerations degree of engine failure speed at the time mass, altitude and temperature (performance) configuration length of runway remaining position of any obstacles ahead Engine failure after take-off simulated at a safe height and at or above take-off safety speed considerations need to maintain control use of bank towards operating engine use of available power achieving best SE climb speed mass, altitude, temperature (performance) effect of prevailing conditions and circumstances Immediate actions: maintenance of control, including air speed and use of power recognition of asymmetric condition identification and confirmation of failed engine feathering and removal of drag (procedure for type) establishing best SE climb speed Issue 01 Page 23-40

continued Subsequent actions: whilst carrying out an asymmetric power climb to the downwind position at SE best rate of climb speed cause and fire check live engine, handling considerations remaining services ATC liaison fuel management Note: these procedures are applicable to aeroplane type and flight situation Significance of asymmetric committal height Asymmetric committal height is the minimum height needed to establish a positive climb whilst maintaining adequate speed for control and removal of drag during an approach to a landing.* circuit approach and landing on asymmetric power definition and use of asymmetric committal height use of standard pattern and normal procedures action if unable to maintain circuit height speed and power settings required decision to land or go-around at asymmetric committal height: factors to be considered undershooting importance of maintaining correct air speed (not below vyse) Speed and heading control height, speed and power relationship: need for minimum possible drag establishing positive climb at best SE rate of climb speed effect of availability of systems, power for flap and landing gear operation and rapid clean up Note 1: The air speed at which the decision is made to commit the aeroplane to a landing or to goaround should normally be the best SE rate of climb speed and in any case not less than the safety speed. Note 2: On no account should instrument approach decision height and its associated procedures be confused with the selection of minimum height for initiating a go-around in asymmetric power flight. Page 24-40 Issue 01

continued Engine failure during an all engines approach or missed approach use of asymmetric committal height and speed considerations speed and heading control decision to attempt a landing, go-around or force land as circumstances dictate Note: at least one demonstration and practice of engine failure in this situation should be performed during the course Instrument flying on asymmetric power considerations relating to aeroplane performance during straight and level flight climbing and descending standard rate turns level, climbing and descending turns including turns onto pre-selected headings availability of vacuum operated instruments availability of electrical power source *Variations will inevitably occur in the order of certain drills and checks due to differences between aeroplane types and perhaps between models of the same type, and the flight manual or equivalent document (for example owner s manual or pilot s operating handbook) is to be consulted to establish the exact order of these procedures. For example, one flight manual or equivalent document (for example owner s manual or pilot s operating handbook) may call for the raising of flaps and landing gear before feathering, whilst another may recommend feathering as a first step. The reason for this latter procedure could be due to the fact that some engines cannot be feathered if the RPM drops below a certain figure. Again, in some aeroplanes, the raising of the landing gear may create more drag during retraction due to the transient position of the landing gear doors and as a result of this retraction would best be left until feathering has been accomplished and propeller drag reduced. Therefore, the order in which the drills and checks are shown in this syllabus under immediate actions and subsequent actions are to be used as a general guide only and the exact order of precedence is determined by reference to the flight manual or equivalent document (for example owner s manual or pilot s operating handbook) for the specific aeroplane type being used on the course * Because of the significantly reduced performance of many CS/JAR/FAR 23 aeroplanes when operating on one engine, consideration is to be given to a minimum height from which it would be safely possible to attempt a go-around procedure, during an approach when the flight path will have to be changed from a descent to a climb with the aeroplane in a high drag configuration. ue to the height loss which will occur during the time that the operating engine is brought up to full power, landing gear and flap retracted, and the aeroplane established in a climb at vyse a minimum height (often referred to as Asymmetric committal height ) is to be selected, below which the pilot should not attempt to take the aeroplane round again for another circuit. This height will be compatible with the aeroplane type, all up weight, altitude of the aerodrome being used, air temperature, wind, the height of obstructions along the climb out path, and pilot competence. Issue 01 Page 25-40

1.2.13 ASSESSMENT FORM LONG BRIEFINGS Nr: Subject ate Results TR T AT I Remarks 1. Familiarisation with the aeroplane 2. Taxiing 3. Straight and level flight 4. Slow flight 5. Flight on asymmetric power extra extra extra extra extra Page 26-40 Issue 01

2. FLIGHT SYLLABUS (PART 3) 2.1 FLIGHT TRAINING OVERVIEW FNPTII, ME(SP) Exercise Type of flight Flight duration Score Planned Flight Total TR T AT 01 ME aeroplane 1:00 02 ME aeroplane 1:30 03 ME aeroplane 1:30 04 ME aeroplane 1:30 05 FNPT II 1:30 06 ME aeroplane 1:00 TOTAL 8:00 Issue 01 Page 27-40

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2.2 FLIGHT REGISTRATION FORMS 2.2.1 01: AIRSCRAFT SYSTEMS, EMERGENCIES, RUNUP, SHUTOWN ate / / ME aeroplane Total Instructor Planning: 1:00 1:00 Student Name Block time: Pre-session briefing Flight authorization and aeroplane acceptance 0 Technical log/certificate of maintenance release 0 Mass and balance and performance considerations 0 Action in the event of fire in the air and on the ground 0 (engine, cabin, electrical) systems failure (gear, heater) 0 Exercise TR T AT External features/checks Cockpit layout Escape drills Use of emergency equipment Actions in event of fire Gearfailure procedure Heater failure Cockpitcheck, adjustment of harness Freedom of rudder movement Check lists Starting and warming up engines Checks after starting Radio nav/com checks Altimeter checks and setting procedures ATC considerations Checks before taxiing Pre take off checklist, engine power and system checks Instructor s briefing in event of emergencies during take-off Running down and switching off engines Completion of ships papers Legend: = emo, C = coaching Issue 01 Page 29-40

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2.2.2 02: TAXI, TAKE OFF, CLIMBING, LEVEL FLIGHT, ESCENING ate / / ME aeroplane Total Instructor Planning: 1:30 2:30 Student Name Block time: Pre-session briefing ifferent powersetting 0 Effect cowl flaps, flapsetting, landing gear 0 Instrument appreciation 0 Exercise TR T AT Rolling and stopping Control of speed Control of direction and turning Turning in confined spaces Brake/steeringfailure Normal take-off, lift-off speed Levelling Off Power Selection Pre-Climbing checks Power selection for normal and maximum rate climb Power selection for maximum angle of climb Engine and RPM limitations Climbing with flaps down Recovery to normal climb En Route Climb (Cruise Climb) Effect of Altitude on Manifold Pressure, Full Throttle Altimeter Setting Procedures Prolonged Climb and use of Cowl Flaps/Cooling Gills Straight and lever normal cruise (Cruise power, synch, trimming, perform. considerations) Effect flapsettings Effect selection landinggear Use of Mixture Controls Use of Alternate Air/Carburettor Control Operation of Cowl Flaps/Cooling Gills Operation of Cabin Ventilation/Heating Systems Pre-escent Checks Power Selection Manifold Pressure/RPM Powered escent (Cruise escent) Engine Cooling Considerations Levelling Off escending with Flaps own escending with Landing Gear own Altimeter Setting Procedure Emergency escent uring all fases of flight Instrument Appreciation ALL EXERCISES WITH FULL VISIBILITY Legend: = emo, C = coaching Issue 01 Page 31-40

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2.2.3 03: TURNS, SLOW FLIGHT, STALLING ate / / ME aeroplane Total Instructor Planning: 1:30 4:00 Student Name Block time: Pre-session briefing Steep turn powersettings 0 Slow flights 0 Stalls 0 Exercise TR T AT Short field take-off, lift-off speed Levelling Off Power Selection Medium turns Medium turns Climbing and descending Turns Climbing and descending Turns Steep turns 45 deg.bank Steep turns 45 deg.bank SLOW FLIGHT Safety Checks Vs1 + 5 kt Vs1 + 5 kt Vso + 5 kt GA from Vso + 5 kt (IAS not below Vsse/Vmca+10 kt) Vso + 5 kt GA from Vso + 5 kt (IAS not below Vsse/Vmca+10 kt) STALLING airmanship considerations selection of RPM stall symptoms full stall characteristics recovery from the full stall care in application of power recovery from the full stall care in application of power recovery at the incipient stage recovery at the incipient stage Instrument Appreciation C C C C C C C C C C ALL EXERCISES WITH FULL VISIBILITY Legend: = emo, C = coaching Issue 01 Page 33-40

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2.2.4 04: EFFECT ASSYMETRIC TRUST, ENGINE FAILURES/ENGINE FIRES ate / / ME aeroplane Total Instructor Planning: 1:30 5:30 Student Name Block time: Pre-session briefing Basic failure management 0 Effect gear/flaps on single engine performance 0 Live engine precautings 0 Relation engine out/instruments and elect. consumers 0 Effect one engine out on performance/engine out ceiling 0 Restarting procedure and dangers 0 Fuelmanagement 0 Exercise TR T AT Closing one throttle (note yaw) Closing second trhrottle (note counteryaw) Alternative/supplementary method of control (simultaneously lower nose reduce power) Effect inside engine failure during turn Effect outside engine failure during turn Possibility of confusion in identification Establish Vyse Effect altitude on single engine operations Engine failure during VFR cruise (including BFM) Engine failure during VFR cruise (including BFM) Engine fire during VFR cruise (including BFM) Engine fire during VFR cruise (including BFM) Engine failure during VFR cruise descent (including BFM) Engine failure during VFR cruise descent (including BFM) Engine failure at safetyspeed Engine failure below safetyspeed, above Vma Engine failure during take off (VFR conditions) Engine failure during take off (VFR conditions) C C C C ALL EXERCISES WITH FULL VISIBILITY Legend: = emo, C = coaching Issue 01 Page 35-40

Remarks Page 36-40 Issue 01

2.2.5 05: IFR BASIC TRAINING, IFR AVANCE TRAINING ate / / FNPTII (ME config) Total Instructor Planning: 1:30 7.00 Student Name Block time: Pre-session briefing Scanning pattern 0 Single engine procedure during IFR conditions 0 Single engine go aroud during IFR conditions 0 Exercise TR T AT SP INSTRUMENT FLIGHT (BASIC) straight and level Climbing Turning escending SP INSTRUMENT FLIGHT (AVANCE) Pre-flight briefing Take-off Rotation speed Keeping on the centre line After take-off checks SI Steep turn Approach to stall landing configuration Approach preparation escent, descending turn ILS approach Engine failure on initial segment Single engine go around Radar vectors NB approach Shut down Use of checklist Radar vecor setup for ILS ownwind on 3000 ft escending turn to 2000 ft Interceptcourse ILS Engine failure ILS approach C C C C C ALL EXERCISES WITH IFR TO THE MINIMUMS Legend: = emo, C = coaching Issue 01 Page 37-40

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2.2.6 06: CIRCUITS ate / / ME aeroplane Total Instructor Planning: 1:00 8:00 Student Name Block time: Pre-session briefing Manual gear extention 0 Take off procedures 0 Powersettings/speeds in the circuit 0 Short field/soft field landing 0 Enfine failure during take off 0 Single engine approach and go around 0 Exercise TR T AT Airmanship and ATC considerations Normal take-off Short field take-off irectional control and use of power Crosswind effects and procedure After take-off procedures (gear, flaps, climbpower, synch) Levelling Off Power Selection All legs speedcontrol, flap selection, trimming, checks Upwind leg ownwind leg Base leg Selection of touchdown point Maintaining correct approach path/use of power Confirmation of landing gear down Final approach Airspeed reduction to Vat Landing Control of sink rate during flare Crosswind considerations Longer landing roll short/soft field approach and landing considerations and precautions Engine failure during take off Single engine circuit and approach Single engine go-around Legend: = emo, C = coaching Issue 01 Page 39-40

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