FFS EVALUATION INSPECTION RECORD & CHECKLIST

Transcription

1 Section/division PERSONNEL LICENSING Form Number: CA Telephone number: Fax Number: Physical address Ikhaya Lokundiza, 16 Treur Close, Waterfall Park, Bekker Street, Midrand, Gauteng Postal address: Private Bag X73, Halfway House 1685 Website: FFS EVALUATION INSPECTION RECORD & CHECKLIST PLEASE NOTE: ALL SECTIONS TO COMPLETED IN FULL AND ALL YES / NO BOXES TO BE FILLED IN Date of inspection Type of aircraft simulator Operator Town Operator s representative Telephone number Name of airline CAA inspector(s) SECTION A - FSTD AND SIMULATOR DETAILS FSTD DETAILS CAA reference number Country Cell phone number Fax number Purpose of inspection Initial Recurrent Manufacturer History of equipment Simulator computer Visual system Visual database used South African airports Motion system Serial number SIMULATOR DETAILS Auto flight system- YES NO Engines (same as airline) YES NO Local authority-obtain copy of certificate Obtain copy of JAR Approval documents certificate FAA Obtain copy of certificate MQTG/ ATG Checked Expiry date of approval Is level of qualification acceptable to SACAA? If NO, comments: Qualification level of approval CA NOVEMBER 2016 Page 1 of 20

2 1. PROCEDURES. SECTION B - FFS DOCUMENTATION MARK ITEMS CHECKED ACCEPTABLE YES NO Application for Evaluation as per AC No 1 SACAA-FSTD A.015, Page 2-C-1 only required for Initial Evaluation for Qualification. 2. FSTD DOCUMENTATION a. Review FSTD Qualification Documentation JAA, FAA, SACAA-FSTD A b. Review Qualification Certificates if presented. c. Review the last completed Evaluation Report issued by the Authority of Qualification. d. Review the last completed Evaluation report issued by any other Authority. e. Review Master QTG or ATG. f. Review previous 12 Months QTG s run in the required 4 Quarters of the past year. g. Review previous 12 Months Defect List. h. Review previous 12 months Maintenance Records. i. Review previous 12 Months Reliability / Lost Time reports. j. Review previous the actual Quarterly Flights Test Flight Out results. k. Review Qualification Certificates if presented. l. Review previous 12 Months Quality reports. m. Quality Manager Interview in accordance with the Quality reports submitted. n. Review Configuration Files for the FSTD Data Base. o. Review the Validity of the Airplane Flight Manual for latest Revisions. p. Review the Airplane Performance Manual for latest Revisions. q. Review the Airplane QRH for latest Revisions. 3. FSTD FACILITIES a. Inspect the premises as required in terms of Section 2 Quality Management Program. b. FSTD Surroundings emergency exit doors for correct operation. c. Escape routes. d. Emergency Escape Ladders. e. Placement of Emergency Equipment. f. Validity of First Aid Kits. g. All Fire Extinguishers for Expiry Date and Correct Types. h. Hydraulic Room Oil Leaks and Fire hazards. i. Electrical Room Hazards and Cleanliness. j. Inspect FSTD Spares and Spares Documentation. k. Inspect and review all Metrology Instruments used for testing. Note All Findings will be recorded in the Evaluation Report CA NOVEMBER 2016 Page 2 of 20

3 SECTION C - SACAA FLIGHT TEST PROFILE This Audit Checklist is to be used for each type of Flight Simulation Training Device Evaluation complying with the SACAA-FSTD A (Aeroplane) Standard. 1. INITIAL CONDITIONS Record the following as a Minimum Airport R/W Stand QNH OAT Wind ZFW Fuel GW SUBJECTIVE TESTS 2. SIMULATOR DOCUMENTATION NOTES YES NO a. Simulator Acceptance Test Manuals b. Simulator Approval Test Guide c. Technical Logbook d. Open Item List e. Daily Functional Pre-Flight Check Record 3. DOCUMENTATION OF USER/CARRIER a. Flight Logs b. Simulator Operating/Instructor Manual c. Difference List (Aircraft / Simulator) d. Flight Crew Operating Manuals e. Performance Data For Different Airports f. Crew Training Manual g. Normal/Abnormal/Emergency Checklists 4. SIMULATOR EXTERNAL CHECKS a. Appearance And Cleanliness b. Stairway/Access Bridge c. Emergency Rope Ladders d. Motion On / Flight In Progress Lights On entry to the simulator with no power applied to simulator, check no lights illuminated and cockpit noise satisfactory. There should be no light leakage from the Visual Out of The Window display system 5. SIMULATOR INTERNAL CHECKS a. Cleaning/Disinfecting Towels (For O 2 Masks) b. Cockpit Layout (Compare with aircraft differences) 6 EQUIPMENT a. Quick Donning Oxygen Masks b. Headsets c. Smoke Goggles d. Sunvisors e. Escape Ropes f. Chart Holders g. Limitation Placards h. Fire Extinguishers (Check Inspection Dates) i. Crash Axe j. Gear Pins CA NOVEMBER 2016 Page 3 of 20

4 SECTION C CONTINUED SIMULATOR EMERGENCY STOP BUTTONS 7 POWER SUPPLY AND APU START CHECKS a. Batteries And Static Inverter b. APU Start With Battery c. APU Shutdown Using Fire Handle d. External Power Connection e. APU Start With External Power f. Abnormal APU Start / Operation 8 COCKPIT CHECKS a. Cockpit Preparation Checks b. F M C Programming (Valid Update) c. Communications & Nav Aid Checks d. Flight Controls Check 9 ENGINE START a. Before Start Checks b. Battery Start With Ground Supply c. Engine Crossbleed Start d. Normal Start e. Hot Start f. Hung Start g. Other Abnormal Start (State) ENGINE IDLE READINGS (RECORD) N 1 EGT LEFT RIGHT NOTES YES NO N 2 Fuel Flow Oil Pressure Oil Temp After Start Checks 10 TAXI CHECKS???? NOTES YES NO Pushback Taxi Checks Ground Handling a. Thrust Required To Move b. Thrust Lever Friction c. Thrust Response d. Nose Wheel/Pedal Steering e. Nose Wheel Scuffing in 360 turn f. Brakes Response And Differential g. Normal System h. Alternate System i. Emergency System Turns: hard over tiller, or full pedal deflection at 15 knots after engine idle j. selected check degrees of turn before aircraft stops to record inertia record CA NOVEMBER 2016 Page 4 of 20

5 degrees of turn before aircraft stops k. Taxi-way Roughness Set & Checked 11. AIRPORT MARKINGS AND LIGHTS VISUAL SCENE GROUND ASSESSMENT Select 3 Different Airport Models and perform the following checks with Day, Dusk and Night selected (enter designator for each airport below, failure of any item to be noted) Visual Controls Check: a. Daylight, Dusk, Night Scene Controls b. Cockpit Daylight ambient lighting c. Environment Light Controls d. Runway Light Controls e. Taxiway Light Controls Scene Content Tick off on each item YES NO YES NO YES NO Ramp area for correct buildings Gates Air bridges Maintenance ground equipment Parked aircraft Daylight shadows Night time light Taxiway for correct Taxiway markings pools markings Taxiway/runway Cat i, ii & iii hold Marker boards markings points Taxiway shape/grass areas Taxiway lights (positions & colours) Runways for correct markings Runway light Turn off markers Runway slope positions and boards colours Directionality of runway lights Airport environment for correct terrain & significant features Visual scene aliasing Colour Occulting Other - specify Note All Findings will be recorded in the Evaluation report 12. TAKE OFF T/O Configuration Warnings Engine Take off Readings N1 EGT N2 F/F Oil T Oil P Acceleration characteristics Engine Sounds evaluate buffet at high power (brakes on) Nose-wheel steering and rudder Steering Runway rumble and nose wheel lights (check with varying runway roughness set) Instrument indications NOTES YES NO CA NOVEMBER 2016 Page 5 of 20

6 Control force and position to rotate-(rotation characteristics) Motion cue for rotation and climb Gear and flap retraction-trim changes- (sound cues) Low Visibility Take-off Low Visibility Take-off (Normal) Low Visibility Take-off (with Engine Failure) Crosswind take-off (max demonstrated) Check for tendency to turn into or out of wind (record) Tendency for upwind wing to lift, wheel angle required (record) Engine Failures after V 1 Control positions and force required to maintain centreline Ease of rotation, control positions and forces, trim changes V 2 climb and acceleration to clean configuration Motion effects NOTES: Dry Wet Icy Rejected Take-Off - Record Stopping Distance (Use runway plot or runway lights remaining) Notes YES NO Patchy Ice Auto brake function Anti-skid operation Speed brake deployment Motion/Visual effects Wind shear during take-off Controllability during Wind shear encounter Performance adequate when using correct techniques Wind shear indications satisfactory Motion cues satisfactory (particularly turbulence effects) Normal Take-off with Control Malfunction (if detailed in Non-Normal drills) 13. CLIMB PERFORMANCE Select one or both of the following cases Normal Climb Climb for a minimum of 5 minutes while maintaining recommended speed profile and record altitude, fuel, distance & time to selected altitude, compare with data obtained from aircraft performance CA NOVEMBER 2016 Page 6 of 20

7 manual / QTG s FFS Recorded Parameters: Start of climb altitude and time Speed Engine Parameters N1, N2, EPR Oil Press & Temps Fuel flow Rate of climb Distance Cabin press diff & rate of climb QTG / Aircraft Parameters: Start of climb altitude and time Speed Engine Parameters N1, N2, EPR Oil Press & Temps Fuel flow Rate of climb Distance Cabin press diff & rate of climb FSTD parameters acceptable NOTES: One or more engines inoperative climb Trim A/C in a zero wheel climb at V 2 Note: Up to 5 degs bank towards the live engine(s) is permissible. When stabilized at V 2, climb for 5 minutes and note ease of trimming control positions and forces. Record time, altitude, engine parameters every minute, then increase speed toward enroute climb speed and retract flaps on schedule. Compare with data obtained from aircraft performance manual / QTG s FFS Recorded Parameters Start of climb altitude and time Speed Engine Parameters N1, N2, EPR Oil Press & Temps Fuel flow Rate of climb Distance Cabin press diff & rate of climb QTG / Aircraft Parameters Start of climb altitude and time Speed Engine Parameters N1, N2, EPR Oil Press & Temps Fuel flow Rate of climb Distance Cabin press diff & rate of climb FSTD parameters acceptable Carry out engine relight(s) within and out side of the Start Envelope, both windmill or assisted and check time to accelerate and engine parameters as well as check whether the engine will start out of the start envelope, above, below Speed requirements, above Altitude Requirements all readings to be recorded, refer to Simulator handbook for full details. CA NOVEMBER 2016 Page 7 of 20

8 Windmill Start outside of envelope speed Windmill Start accelerating to envelope speed Windmill Start outside of envelope above max altitude Windmill Start outside of envelope descending into envelope altitude Windmill Start within start envelope Assisted Start outside of envelope speed Assisted Start accelerating to envelope speed Assisted Start outside of envelope above max altitude Assisted Start outside of envelope descending into envelope altitude Assisted Start within start envelope Notes: 14. SYSTEMS OPERATION DURING CLIMB Air-conditioning Pressurisation Bleed Air Leak Rate Ventilation Auto flight Check normal operation and malfunctions as appropriate for the following systems: Notes YES NO Communications Electrical Fuel Icing Systems Indicating and Recording Systems Nav./Flight Management Systems Pneumatics 15. CRUISE CHECKS Cruise Performance Compare with data obtained from aircraft performance manual / QTG s High Speed/High Altitude Handling Check and compare with data obtained from aircraft performance manual / QTG s Trim changes (Mach tuck) Overspeed warning Aircraft control satisfactory High Speed Buffet onset (if applicable) Envelope limiting functions on CCA Recovery with power reduction and speedbrakes as required note trim changes with power reduction and speed-brakes Reduce Airspeed to just below level flight buffet onset speed and commence a turn then check: High Speed buffet increases with G loading Turns without spoilers (speedbrake) deployed Turns with spoilers (speedbrake) deployed Yaw Damper Operation Switch off yaw dampers and autopilot and initiate a Dutch Roll and check: Aircraft dynamics CA NOVEMBER 2016 Page 8 of 20

9 Simulator motion effects. Switch on yaw dampers and re-initiate a Dutch Roll and check: Damped aircraft dynamics Damped Simulator motion effects. 16. DESCENT FROM HIGH ALTITUDE Notes YES NO Reduce thrust levers to idle and commence descent and select/deploy speedbrake then check: Speed brake indications Symmetrical deployment Airframe buffet Aircraft response hands off Blow down APU Operation Start at maximum cleared altitude Engine Gravity Feed (if applicable) Engine Shutdown and Drift-down from above max single / 2 engine altitude, then check: FMC operation Aircraft performance Engine Relight Cabin Depressurisation / Emergency Descent checks: Check cockpit indications Cockpit crew mask ease of deployment Mask operation / communication / flow Pressurisation system operation 17. MEDIUM ALTITUDE CHECKS Stalling 1 g flight select one or several of the following test cases: High angle of attack/stall in clean Configuration High angle of attack in approach configuration Trim aircraft at 1.4V s for configuration power off and establish deceleration at 1 kt/sec without further trimming after passing final trim speed (aircraft will be in a descent) then check and compare with data obtained from aircraft performance manual / QTG s record all speeds, AFM QTG and FSTD System displays / operations Handling characteristics satisfactory including trim changes and forces Stall identification Stick shaker speed Buffet characteristics and onset speed Envelope limiting functions on CCA Trim Change at stall Stall hysteris modelled Notes: YES NO Recover to straight and level flight Repeat a stall with the autopilot engaged and check CCA function and aircraft/auto pilot behaviour, check: Flight handling characteristics Engine handling characteristics Turning Flight Clean and Approach configuration Roll aircraft into the turn and establish a 30/45 bank angle check: Stick force required, satisfactory Check normal acceleration indication on IOS Flight Page CA NOVEMBER 2016 Page 9 of 20

10 Wheel requirement to maintain bank angle Slip ball response, satisfactory (note no g force cue apparent) Roll aircraft from 45 deg bank to 45 deg bank while maintaining altitude and airspeed to check: Controllability during representative manoeuvre. 18. SYSTEM AND WEATHER CHECKS Degraded flight controls Check: Drills and Procedures in QRH Non-Normal Emergency Procedures in QRH Holding Procedure, Check FMC operation Auto pilot operation Auto Thrust performance Storm Selection, Check WX Radar Controls WX Radar Operation Visual scene content corresponds with WXR pattern and IOS selection and indication Fly through storm area, Check: Aircraft enters cloud Aircraft encounters representative turbulence Rain / hail sound effects evident As aircraft leaves storm area Check: Storm effects disappear. TCAS Check as follows: Traffic appears on visual and TCAS displays As conflicting traffic approaches take relevant avoiding action, Check; Visual and TCAS system display indicate correct results. If correctly executed there is no collision As conflicting traffic approaches take no avoiding action, Check; Visual and TCAS system display indicate correct indications Aircraft either fly through each other or collide with resultant crash (record result) 19. APPROACH TO LANDING, FLAP AND GEAR OPERATION Due to the large number of cases to be checked it is desirable to use the IOS repositioning facility to reposition back to a convenient point on the approach (5-10nm), after the landing checks are completed. It is important to reset any malfunctions, brake temperatures, initial conditions, weather, etc after repositioning and before the simulation is released Using IOS malfunctions check landing gear/flap and hydraulic operation under the following conditions Check the normal and non-normal operation and malfunctions as appropriate for the following systems Approach to Landing Normal Wing Flaps / Spoiler normal hydraulic / electric operation where applicable Time for extension Time for retraction / go-around Buffet characteristics Wing Flaps / Leading Edge Flaps / Slats / Spoilers, normal hydraulic / electric operation where applicable. Time for extension Time for retraction / go-around CA NOVEMBER 2016 Page 10 of 20

11 Buffet characteristics Gear Operation-check hydraulic / electric operation where applicable Time for extension Time for retraction / go-around Buffet characteristics Approach to Landing Non-Normal Wing Flaps / Spoilers, hydraulic / electric operation where applicable. Time for extension Time for retraction / go-around Buffet characteristics Wing Flaps / Leading Edge Flaps / Slats / Spoilers non-normal hydraulic / electric operation where applicable Time for extension Time for retraction / go-around Buffet characteristics Gear non-normal Operation-check hydraulic / electric operation where applicable Time for extension Time for retraction / go-around Buffet characteristics Notes: 20. MANUAL LANDINGS Normal Operation, Flaps / Leading Edge Flaps / Slats / Spoilers / Gear / Brakes Fly a normal approach and manual landing to one of the operator s airfields, while monitoring flight control and hydraulics systems for normal operations, check: Notes: YES NO Aircraft handling Spoiler operation Reverse thrust operation Directional control on the ground Touch down cues for main and nose wheel Radio aids and instrument indications Visual cues Motion cues Sound cues Brake and anti-skid operation Abnormal Operation, Flaps / Leading Edge Flaps / Slats /Spoilers / Gear / Brakes Using the IOS Malfunctions check the above items as test cases, while monitoring flight control and hydraulic systems for normal operations as laid out in the AFM for the malfunctions. Fly non-normal approach s and manual landings to one of the operator s airfields, check: Aircraft handling Spoiler operation Reverse thrust operation Directional control on the ground Touch down cues for main and nose wheel CA NOVEMBER 2016 Page 11 of 20

12 Radio aids and instrument indications Visual cues Motion cues Sound cues Brake and anti-skid operation Precision and Non-precision Approaches All Engines Operating: Approaches to conform to Approach Plate all must be flown, check: NDB VOR, RNAV GPS, TACAN DME arc ILS/LOC and /BC if installed. GNSS RNP NDB VOR, RNAV Circling Approach GPS, TACAN One Engine Inoperative Precision and Non-precision Approaches: Approaches to conform to Approach Plate all must be flown, check: NDB VOR, RNAV GPS, TACAN DME arc ILS/LOC and /BC if installed. GNSS RNP ILS/LOC and /BC if installed. One Engine Inoperative Go-around NDB VOR, RNAV GPS, TACAN ILS/LOC CAT I Approach and Landing with raw ILS CAT I Approach and Landing with limiting Crosswind CAT I Approach with Windshear, at least two scenarios Check: Controllable during Windshear encounter Performance adequate when using correct techniques Windshear indications / Warnings/ Callouts Motion cues (particularly turbulence) Crash cues when using incorrect techniques or max selected on IOS Approach and Landing with Flight Controls System failure modes as dictated by aircraft certification and operators training program 21. AUTOMATIC COUPLED APPROACHES AND LANDINGS CAT II Approach and Automatic Go-around CAT II Approach and Landing System Malfunction CAT III Approach and Landing System Notes: YES NO CA NOVEMBER 2016 Page 12 of 20

13 Malfunction CAT III Approach and Landing One Engine Inoperative Check HUD Operation to Decision Height as per AFM 22. GPWS OPERATION Use a visual database with Height Above Terrain (HAT) to check the different modes of operation Instrument indication Voice Commands Notes: 23. AFTER LANDING OPERATION Landing, Check: Ease of handling during flare and landing Control forces and positions required Assessment of touch down height Touchdown motion cues Touchdown Sound cues Spoiler and reverse thrust operation Braking Motion cues with reverse thrust operation Directional control on the ground, with reverse thrust. Directional control on the ground, without reverse thrust. Brake and anti-skid operation dry. Brake and anti-skid operation wet. Brake and anti-skid operation dry, wet and icy conditions Brake and anti-skid operation dry icy conditions Representative stopping distances After Landing Checks Instrument Indications Check list Items Taxi back to gate Check: Visual model satisfactory Parking brake operation satisfactory Shutdown Checks as per AFM 24. CRASH FUNCTIONS Gear-up Crash Motion cues Sound cues Excessive rate of decent Crash Motion cues Sound cues Excessive bank angle crash Motion cues Sound cues NOTES: Notes: YES NO CA NOVEMBER 2016 Page 13 of 20

14 25. VISUAL SCENE IN-FLIGHT ASSESMENT Select 3 Different Airport Models and perform the following checks with Day, Dusk and Night selected (enter designator for each airport below, failure of any item to noted) Reposition the aircraft below 2000ft, within 10nm of the airfield. Fly around airport environment check and assess the following, for each airfield Visual Controls Check: Airfield 1 Daylight, Dusk, Night Scene Controls Cockpit Daylight ambient lighting Environment Light Controls Runway Light Controls Taxiway Light Controls Approach Light Controls. Scene Content - Airfield 1 Tick off on each item YES NO YES NO YES NO Airport environment Airport for correct Significant features for correct terrain buildings built up areas, roads etc; Runways for correct markings directionality of runway directionality of taxiway shape / taxiways grass areas runway slope directionality of runway lights Cat I, II & III hold points Visual scene aliasing Colour Occulting Other - specify Reposition aircraft to long final approach for each ILS runway. Select flight freeze when aircraft is 5nm: Check: Airfield Features Y N Approach Lights Runway definition Runway edge lights and PAPI / VASI Strobe lights Release flight freeze and continue flying the approach with A/P engaged. Select flight freeze when aircraft is 3 nm Check Runway centre lights Taxiway definition and lights Release flight freeze and continue flying the approach with A/P engaged. Select flight freeze when aircraft is 2 nm Check Runway threshold lights. Touchdown Zone lights. Release flight freeze and continue flying the approach with A/P engaged. At 200ft RA Select flight freeze, Check Runway Markings Detailed notes on airfield visual scenes discrepancies, additional notes if necessary CA NOVEMBER 2016 Page 14 of 20

15 Visual Controls Check: Airfield 2 Daylight, Dusk, Night Scene Controls Cockpit Daylight ambient lighting Environment Light Controls Runway Light Controls Taxiway Light Controls Approach Light Controls. Scene Content - Airfield 2 Tick off on each item YES NO YES NO YES NO Airport environment Airport for correct Significant features for correct terrain buildings built up areas, roads etc; Runways for correct markings directionality of runway directionality of taxiway shape / taxiways grass areas runway slope directionality of runway lights Cat I, II & III hold points Visual scene aliasing Colour Occulting Other - specify Reposition aircraft to long final approach for each ILS runway. Select flight freeze when aircraft is 5nm, Check: Airfield Features Y N Approach Lights Runway definition Runway edge lights and PAPI / VASI Strobe lights Release flight freeze and continue flying the approach with A/P engaged. Select flight freeze when aircraft is 3 nm Check Runway centre lights Taxiway definition and lights Release flight freeze and continue flying the approach with A/P engaged. Select flight freeze when aircraft is 2 nm Check Runway threshold lights. Touchdown Zone lights. Release flight freeze and continue flying the approach with A/P engaged. At 200ft RA Select flight freeze, Check Runway Markings Detailed notes on airfield visual scenes discrepancies, additional notes if necessary CA NOVEMBER 2016 Page 15 of 20

16 Visual Controls Check: Airfield 3 Daylight, Dusk, Night Scene Controls Cockpit Daylight ambient lighting Environment Light Controls Runway Light Controls Taxiway Light Controls Approach Light Controls. Scene Content - Airfield 3 Tick off on each item YES NO YES NO YES NO Airport environment Airport for correct Significant features for correct terrain buildings built up areas, roads etc; Runways for correct markings directionality of runway directionality of taxiway shape / taxiways grass areas runway slope directionality of runway lights Cat I, II & III hold points Visual scene aliasing Colour Occulting Other - specify Reposition aircraft to long final approach for each ILS runway. Select flight freeze when aircraft is 5nm, Check: Airfield Features YES NO Approach Lights Runway definition Runway edge lights and PAPI / VASI Strobe lights Release flight freeze and continue flying the approach with A/P engaged. Select flight freeze when aircraft is 3 nm Check Runway centre lights Taxiway definition and lights Release flight freeze and continue flying the approach with A/P engaged. Select flight freeze when aircraft is 2 nm Check Runway threshold lights. Touchdown Zone lights. Release flight freeze and continue flying the approach with A/P engaged. At 200ft RA Select flight freeze, Check Runway Markings Detailed notes on airfield visual scenes discrepancies, additional notes if necessary CA NOVEMBER 2016 Page 16 of 20

17 Set WX to CAT I, then Check and record the following : Cloud base Visual Ground Segment Set WX to CAT II Release flight freeze and re-select flight freeze at 100 ft RA, then Check and record the following: Cloud base Visual Ground Segment Select Night / Dusk then Check Runway markings visual within landing light lobes Set WX to CAT II Release flight freeze and re-select flight freeze at 50 ft RA, then Check and record the following: Cloud base Visual Ground Segment Set WX to CAT III Release flight freeze and re-select flight freeze at 15 ft RA, then Check and record he following Cloud base Visual Ground Segment Release flight freeze when on ground stop aircraft.set 0 ft RVR and ensure strobe/beacon lights are switched on, Check Visual effect of strobe and beacon switch each off in turn check different in lights effect. Reposition to final approach, set WX to clear and continue approach for Automatic Landing and check Visual cues during flare to assess: Sink rate and Depth perception Cockpit height above ground Detailed notes on airfield visual scenes, Visual Ground Segment discrepancies, additional notes if necessary CA NOVEMBER 2016 Page 17 of 20

18 CA NOVEMBER 2016 Page 18 of 20

19 Operator Representatives DE BRIEF CAA Representatives Simulator performance and suitability Flight recording / training file RECOMMENDATIONS Simulator be APPROVED NOT APPROVED Conditions / Restrictions SIGNATURE OF ATO INSPECTOR PILOT NAME IN BLOCK LETTERS DATE SIGNATURE OF ATO INSPECTOR PILOT NAME IN BLOCK LETTERS DATE I, the undersigned, acknowledge that I was de-briefed on the inspection and understand the contents of the findings and recommendations. I acknowledge that non-compliance or failure to meet the recommendations may result in the suspension of the FSTD certificate. SIGNATURE OF INSPECTED ORGANISATION S REPRESENTATIVE NAME IN BLOCK LETTERS DATE CA NOVEMBER 2016 Page 19 of 20

20 RECOMMENDATION ISSUE RECURRENT Z - RECOMMENDED COMMENTS / RESTRICTIONS Qualification of this simulator certificate number NOT RECOMMENDED SIGNATURE OF MANAGER: TRAINING Approved For issue NAME IN BLOCK LETTERS Not approved For renewal DATE SIGNATURE OF SM:PEL NAME IN BLOCK LETTERS DATE CA NOVEMBER 2016 Page 20 of 20