ISLAMIC RE-PUBLIC OF PAKISTAN OFFICE OF THE DIRECTOR GENERAL PAKISTAN CIVIL AVIATION AUTHORITY

Transcription

1 ISLAMIC RE-PUBLIC OF PAKISTAN OFFICE OF THE DIRECTOR GENERAL PAKISTAN CIVIL AVIATION AUTHORITY DOC.NO: CAAD REV. NO: 00 DATED: FLIGHT SIMULATOR QUALIFICATION FUNCTIONS AND SUBJECTIVE TESTS Operator Date Simulator Type/ID Location Inspection Team S = Satisfactory; U = Unsatisfactory; P = Potential; I = Information; E = Exceeds 1. INITIAL CHECKS 1.1 Documentation of Simulator Simulator Master Qualification Test Guide Simulator Qualification Test Guide Technical Logbook Open Item List Daily Functional Pre-Flight Cheek 1.2 Documentation of User/Carrier Flight Logs Simulator Operating / Instructor Manual Differences List (Aircraft Simulator) Flight Crew Operating Manuals Performance Data for Different Fields Flight Crew Training Manual Normal/Abnormal/Emergency Checklists 1.3 Simulator External Checks Appearance and Cleanliness Stairway/Access Bridge Emergency Rope Ladder "Motion On"& Flight in Progress Lights 1.4 Cockpit Equipment Quick Donning Oxygen Masks Head Sets Smoke Goggles Chart Holders Limit Placards Fire Extinguisher (Inspection date) 2. INITIAL CON DIT1ONS Record the following as a minimum: Airport QNH/OAT Wind/WA ZFW/Fuel/GW/CG 3. POWER SUPPLY AND APU START CHECKS 3.1 Batteries and Static Inverter 3.2 APU Start with Battery 3.3 APU Shutdown using Fire Handle 3.4 External Power Connection 3.5 APU Start with External Power 3.6 Abnormal APU Start/Operation Page 1 of 7

2 4. COCKPIT CHECKS 4.1 Cockpit Preparation Checks 4.2 Communications and Navigational Aids Checks 5. ENGINE START 5.1 Before Start Checks 5.2 Battery/External Power Unit start with Ground Air Supply unit 5.3 Engine Crossbleed Start 5.4 Normal Engine Start 5.5 Abnormal Engine Starts 5.6 Engine Idle Readings 5.7 After Start Checks 6. TAXI CHECKS 6.1 Pushback 6.2 Taxi Check 6.3 Ground Handling Power required to initiate ground roll Power lever friction Thrust response Nose Wheel and Pedal Steering Perform 180 o turns Brakes Response and Differential Braking using Normal (Primary) Alternate (Secondary) and Emergency (Reserve) Brake System Eye height and fore/aft position 6.4 Runway Roughness 7. VISUAL SCENE- GROUND ASSESSMENT Select 3 different visual models and perform the following checks with Day, Dusk and Night selected: 7.1 Visual Controls Daylight, Drink, Night Scene Controls Cockpit "Daylight" ambient lighting Environment Light Controls Runway Light Controls Taxiway Light Controls 7.2 Scene Content Check Ramp area for correct buildings, gates, aerobridges, maintenance ground equipment parked aircraft, daylight shadows, right time light pools, taxiway marking Taxiways for correct markings, taxiway/runway, marker boards. CAT I & II hold points, taxiway shape/grass areas, taxiway light, (Positions and colours) Runways for correct markings, nun-off marker, boards, runway slope, runway light positions, and colour, directionality of runway lights Airport environment for correct terrain and, significant features 7.3 Ground Traffic Selection 8. TAKEOFF Select one or more of the following test cases: 8.1 T/O Configuration Warnings 8.2 Engine Takeoff Readings 8.3 Rejected Takeoff- Dry/Wet, Icy Runway Autobrake function Page 2 of 7

3 . Anti-skid operation Motion/Visual effects during deceleration Record stopping distance ('use runway plot or runway lights remaining) Continue taxiing along the runway while applying brakes Centre line lights alternating red &white for 600m Centre line lights all red for 300m Runway end, red stop bars Braking effect fades Brake temperature indications 8.4 Engine Failure between V1 and V2 8.5 Normal Takeoff During Ground Roll Check. Runway Rumble Acceleration cues Groundspeed effects Engine Sounds Nosewheel and rudder steering During and after rotation Rotation Characteristics Column force during rotation Gear retraction noise/buffet Gear uplock sound/bumps Effect of slat/flap retraction during climbout 8.6 Crosswind Takeoff Tendency to turn into or out of the wind Tendency to lift up wind wing as airspeed increases 8.7 Windshear during Takeoff Controllable during windshear encounter Performance adequate when using correct techniques Windshear Indications satisfactory Motion cues satisfactory (particularly turbulence) 8.8 Normal Takeoff with Control Malfunction 8.9 Low Visibility T/O Visual cues Flying by instruments 9. CLIMB PERFORMANCE Select one or more of the following test causes: 9. 1 Normal Climb Climb while maintaining recommended seed profile and note fuel, distance and t/me 9.2 Single Engine Climb Trim A/C in a zero wheel climb at V2. (Note: UP to 5 degs bank towards the live engine is permissible). Climb for 3 minutes and note fuel, distance and time Increase speed toward en-route climb speed and retract flaps. Climb for 3 minutes and note fuel, distance and time. 10. SYSTEMS OPERATION DURING CLIMB Check normal operations and malfunctions as appropriate for the following systems: Page 3 of 7

4 10.1 Air conditioning/pressurization/ventilation 10.2 Autoflight 10.3 Communications 10.4 Electrical 10.5 Fuel 10.6 De-icing systems 10.7 Indicating and Recording Systems 10.8 Navigation 10.9 Pneumatics 11. CRUISE CHECKS Select one or more of the following test cases: 11.1 Cruise Performance 11.2 High Speed/High Altitude Handling Overspeed warning High Speed buffet Aircraft control satisfactory Reduce Airspeed to below level flight buffet onset speed and commence a turn High Speed buffet increases with G loading Reduce throttles to idle and commence descent and select speed brake Speed brake indications Symmetrical deployment Airframe buffet Aircraft response hands off 11.3 Yaw Damper Operation Switch off yaw dampers and autopilot & initiate a Dutch roll Aircraft dynamics Simulator motion effects Switch on yaw dampers and re-initiate a Dutch roll Damped aircraft dynamics 11.4 APU Operations 11.5 Engine Gravity Feed 11.6 Engine Shutdown and Driftdown Aircraft performance 11.7 Engine Relight 12. DESCENT Select one of the following test cases: 12.1 Normal Descent Descend while maintaining recommend M speed profile and note fuel, distance and time 12.2 Cabin Depressurisation/Emergency Descent 13. MEDIUM ALTITUDE CHECKS Select one or more of the following test case: 13.1 High angle of Attack/Stall Page 4 of 7

5 Check System displays/operation satisfactory Handling characteristics satisfactory Stall indent/stick shaker speed Envelope limiting functions on CA.A Recover to straight and level flight Handling characteristics satisfactory Steep Turns Roll aircraft to left and establish a 30/45 deg bank angle Stick force required, satisfactory Wheel requirement to maintain bank angle Slip ball response, satisfactory Time to turn 180 Roll aircraft from 45 deg bank while maintaining altitude and an airspeed Controllability during manoeuvre representative 13.3 Degraded flight controls 13.4 Holding procedure Autopilot and Auto Throttle performance satisfactory 14. APPROACH AND LANDING Select one or more of the following test cases while monitoring flight control and hydraulic system for normal operation and with malfunctions selected: 14.1 Flaps/Gear normal operation Time for extension/retraction Buffet Characteristics 14.2 Normal Visual Approach and Lending Fly a normal visual approach and landing Aircraft handling Spoiler operation Reverse thrust operation Directional control on the ground Touchdown cues for main and nose wheel Visual cues Motion cues Sound cues Brake and Anti-skid operation 14.3 Flaps/Gear Abnormal Operation or with hydraulic malfunctions 14.4 Abnormal Wing Flat, Slats Landing 14.5 Manual Landing with Control Malfunction During the following approaches Aircraft handling Radio Aids and instruments Visual scene content and cues Motion cues Sound cues 14.6 Non-precision Approach - All Engines Operating Page 5 of 7

6 14.7 Circling Approach 14.8 Non-precision Approach - One Engine Inoperative 14.9 One Engine Inoperative Go-around CAT I Approach and Landing with raw ILS CAT I Approach and Landing with Limiting Crosswind CAT I Approach with Windshear Controllable during windshear encounter Performance adequate when using correct techniques Windshear indications/warnings Motion cues (particularly turbulence) CAT II Approach and Go-Around GPWS evaluation 15. VISUAL SCENE-IN-FLIGHT ASSESSMENT Select 3 different visual models and perform the following checks with Day, Dusk and Night selected. Reposition aircraft below 2000 ft, within 10 nm of airfield. Fly aircraft around airport environment and assess the following 15.1 Visual Controls Daylight 'Dusk' Night Scene Controls Cockpit "Daylight" ambient lighting Environment Light Controls Runway Light Controls Taxiway Light Controls Approach Light Controls 15.2 Scene Content Check Airport environment for correct terrain and significant features, runways for correct markings, runway slope, directionality of runway lights Reposition aircraft to long final approach for ILS runway. Select flight freeze when aircraft is 5 sm/8 Km Airfield features, satisfactory, Approach lights Runway definition Runway edge lights and VASI lights Storable lights Release fight freeze and continue flying the approach with A/P engaged. Select flight freeze when aircraft is 2 sm/3 Km. Runway threshold lights Touchdown zone lights At 200 fl RA Select Flight Freeze Runway markings Set WX to CAT II Cloudbase Visual Ground segment Set WX to CAT II. Release Flight Freeze and re-select Flight Freeze at 100 ft RA Page 6 of 7

7 Cloudbase Visual Ground segment Select night/dusk Runway markings visible within landing light lobes Reposition to final approach, set WX to clear and continue approach for an automatic landing Visual cues during flare to assess: Sink rate and Depth Perception Cockpit height above ground 16. AFTER LANDING OPERATIONS 16.1 After Landing Checks 16.2 Taxy back to gate Visual model satisfactory Parking brake operation satisfactory 16.3 Shutdown Checks 17. CRASH FUNCTION 17.1 Gear-up Crash 17.2 Excessive rate of descent Crash 17.3 Excessive bank angle Crash Page 7 of 7