C HECK LIST K ATANA DA20 PILOT S NAME: AIRCRAFT REG: Martin Huber D-EAGJ

Transcription

1 C HECK LIST PILOT S NAME: AIRCRAFT REG: Martin Huber D-EAGJ K ATANA DA20

2 Copyright Oliver Hohnhold 2003 All rights reserved. The reproduction, transmission or use of this document is not permitted without express written authority. Oliver Hohnhold A-8430 Leitring, Maria Steflitschgasse 12 Tel:+43 (664) Disclaimer We have checked the contents of this checklist for agreement with the flight manual book of the aircraft. Since deviations cannot be precluded entirely, we cannot guarantee full agreement. However, the data in this checklist are reviewed regulary and any necessary corrections included in subsequent editions. When differences between flight manual book and checklist the flight manual book have priority before the checklist. Template: 24. February 2003 Text: 24. February 2003

3 Rechts AIRCRAFT DATA 1 Technical Data The following data are only for the Aircraft with the registration D-EAGJ. 1 - Dimensions Wing span... 10,84m Aircraft length... 7,17m Aircraft height... 2,11m Track width... 1,90m Wheelbase... 1,75m 2 - Mass Gross weight MTOM kg Empty Mass 03. July ,6kg Payload ,4kg Baggage compartment max.20kg 3 - Engine / Propeller Rotax Power at 2550 RPM...59,6kW...80PS Constant Speed Propeller..1,70m 4 - Fuelsystem / Oil / Coolant Allowed fuel...avgas 100LL Fuel capacity...76l Usable fuel...74l Unusable fuel...2l Oil quantity min...2,0l Maximum...3,0l Engine coolant min...2,4l Maximum...2,5l T ECHNICAL DATA Pressure Altitude Stand. Temp. Engine Power as % of max. continuous power (RPM * 100) ft m C [ F] 55% 65% 75% 85% 95% 104% RPM MP RPM MP RPM MP RPM MP RPM MP RPM MP [59] 19 24, , , , ,0 25,5 29, [52] 19 24, , , , , [45] 19 23, , , , [37] 19 23, , , [30] 20 21, , , [23] 21 20, , [16] 22 18, [12] 23 17,3 Consumption per hour 12,3 liters 14,5 liters 16,6 liters 19,3 liters 22,7 liters 24,7 liters Tab.1: Power Table Raise manifold pressure by 0,7 in Hg at ISA +10 C (18 F) Lower manifold pressure by 0,7 in Hg at ISA -10 C (-18 F) Template: 21. February 2003 Text: 21. February

4 Links 1 Technical Data AIRCRAFT DATA 5 - Airspeeds VNE kts Never exceed speed VNO kts Maximum Cruise Speed VA kts Manouevering Speed VFE kts Max. Speed Flap extended VS kts Stall Speed Clean configuration VS kts Stall Speed landing configuration 6 - Performance Data MTOW...730kg Cruise Speed 75% / 6000ft 116 KTS/TAS Climb rate 0ft...500ft/min Climb rate 8000ft...120ft/min Service ceiling ft Flight time 75% no reserve 4,5h. 7 - Stall speed Table Configuration: Idle Center of Gravity max. front position Maximum Take Off Weight This is a unfavourable configuration. B A N K Flaps 0 % IAS CAS IAS CAS IAS CAS IAS CAS UP T/O LDG Tab.2: Stall speed 8 - Start run distance Abb: 1: Requirements Maximum Power Take off speed 57 KIAS Climp speed over obstacle 60 KIAS 1-2 Template: 21. February 2003 Text: 21. February 2003

5 Rechts AIRCRAFT DATA 1 Technical Data Plane and asphalt Runway Flaps in T/O - position A bad maintenance status, difference from the mandatory procedures as well, wind, rain, temperature,... can make longer the start run. Dry short grass make start run 25% longer Soft grass runway with grass height more than 10cm make start run 40% longer. 9 - Landing distance Landing distance Landing rolling distance Altitude over MSL in ft Tab.3: Landing distance Weight & Balance M A S S Weight [kg] Arm Moment [kgm] Empty Mass 524,6 0, ,66 Pilot / Passenger 160 0,143 22,88 Baggage 8 0,824 6,592 Total without Fuel 692,6 179,132 Fuel 37,4 0,824 30,8176 T O T A L ,949 Tab.4: Weight & Balance example M A S S Weight [kg] Arm Moment [kgm] Empty Mass 524,6 0, ,66 Pilot / Passenger 0,143 Baggage 0,824 Total without Fuel Fuel 0,824 T O T A L Tab.5: Weight & Balance Check Weight and Center of gravity on following diagram. Template: 21. February 2003 Text: 21. February

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7 Rechts PREFLIGHT CHECK 1 - Before Fly 2 Check 4 - Left Wing / Main Gear List Define Route / Flight Log PREPARED Weight and Balance CALCULATE Take Off / Landing Distance CHECKED Runway check for DEBRIS Meteorological Conditions CHECKED File a Flightplan DONE 2 - Aircraft Acceptance Maintenance Status CHECKED A.R.R.O.W. - M EXIST Airworthness Certificate Registration Radio Station License Operating Limits Weight and Balance Minimum equipment list Hobbstime NOTICE Tachtime NOTICE Minimum Equipment ON BOARD Aviation Card, Sunglasses, GPS incl. Battery Sickbag for Passenger 3 - Cockpit Structure Temperature CHECKED Only when outside Temperture >38 Celsius Flight Control Lock REMOVED Ignition Key Out TAKE OUT Avionics Main Switch OFF Parking Brake RELEASED Main Switch ON Circuit Breakers CHECKED Warning Lights CHECKED Generator Fuel Pump Canopy Outside Lights CHECKED Taxi- and Landinglight (Check lens) Strobes Navlight Flight Instruments Warning Flags... CHECKED Fuel Quantity VERIFY Trim full Range CHECKED Flaps full Range CHECKED Main Switch OFF ELT - Armed CHECKED Baggage Compartment SECURE Canopy Clean and no Damage..... CHECKED Tire (2,3bar) CHECKED Wheel Fairing CHECKED Brake lines & Pads CHECKED Chocks REMOVED Stall Warning CHECKED Leading Edge & Wing CHECKED Pitot / Static Probe CHECKED Tie Down REMOVED Wing Tip CHECKED Aileron Balance Tab CHECKED Aileron and Inspect Hole CHECKED Flap and Inspect Hole CHECKED Strut CHECKED 5 - Fuselage / Tail Section Fuel Drain CHECKED Fuel Tank Vent. Pipe CHECKED Fuel quantity CHECKED Fuselage CHECKED Antennas CHECKED Tie Down REMOVED Stabilizer CHECKED Trim Tab & Hinges CHECKED Anti Servo Tab CHECKED Rudder CHECKED 6 - Right Wing / Main Gear Strut CHECKED Flap and Inspect Hole CHECKED Aileron and Inspect Hole CHECKED Aileron Balance Tab CHECKED Wing Tip CHECKED Tie Down CHECKED Leading Edge & Wing CHECKED Chock REMOVED Brake lines & Pads CHECKED Wheel Fairing CHECKED Tire (2,3bar) CHECKED 7 - Nose Section Oil CHECKED Level gauge (Normal is max 1/3 from the lower mark) Coolant CHECKED C HECK LIST Template: 01. March 2003 Text: 01. March

8 Links 2 Check List PREFLIGHT CHECK Cowling CHECKED Propeller CHECKED When outside temperature low, then turn propeller clockwise 10 times Spinner CHECKED Air intakes CHECKED Nose gear CHECKED Wheel fairing CHECKED Tire (1,8 bar) CHECKED Chocks CHECKED 2-2 Template: 01. March 2003 Text: 01. March 2003

9 Rechts ENGINE STARTUP 2 Check List 1 - Before Engine Start Passenger Briefing DONE Use the restroom before flight. Don t touch the controls / pedals or instruments without authorization from Pilot. Inform Pilot when you become airsickness. Turbulence, and other things. Exiting the aircraft. Ruder Pedals ADJUSTED Flight Controls CHECKED Aileron, Elevator, Rudder Seat belts FASTENED Parking Brake SET Fuel Shutoff Valve ON Throttle FREE, IDLE Prop Control FREE, MAX Carburetor Heat COLD Throttle Friction ADJUST Avionics Master OFF Master Switch ON Strobes ON Generator Warning light CHECK ON Fuel Pressure Warning light CHECK ON Canopy closed (Warning Light OFF).CHECKED 2 - Start Engine Fuel Pump ON Fuel Pressure Warning light CHECK OFF IMPORTANT INFO YOU HAVE DIFFERENT PROCEED FOR STARTING ENGINE COLD OR WARM Throttle Engine cold IDLE Choke Engine cold PULL/HOLD Radio & Intercom ON VOR ON GPS ON Transponder / SBY Circuit Breakers CHECKED ATIS RECEIVED Flight Instruments CHECKED Airspeed READING ZERO Horizon WINGS LEVEL Altimeter QNH-Set AIRFIELD ELEV. CHECKED Turn Coord. WINGS LEVEL / NO WARNING FLAG Direct. Gyro COMPASS HEADING SET Vertical Ind. READING ZERO 4 - Before Taxi Taxi / Landing Light ON Flaps UP Engine Instruments CHECKED Volt- Amperemeter CHECKED Taxi Clearance RECEIVED Parking Brake RELEASE Taxi Area CLEAR 5 - During Taxi Magnetic Compass CHECKED Directional Gyro CHECKED Turn Coordinator CHECKED Brakes CHECKED Throttle Engine warm cm Choke Engine warm OFF Propeller Area CLEAR Ignition Key START Throttle max RPM Oil Pressure CHECKED If pressure after 10sec. lower 22 psi (1,5bar) turn off Engine immediately Generator Warning light CHECK OFF Fuel Pump OFF Throttle min RPM 3 - After Engine Start Warm up RPM Avionics Master switch ON Template: 01. March 2003 Text: 01. March

10 Links 2 Check List 6 - Engine Run Up DEPARTURE - T/O 11 - Short Field Take Off Parking Brake SET Fuel Pressure Light OFF Engine Instruments GREENARC Throttle RPM Prop. Cycle RPM (3 Times) CHECKED Prop. Cycle MAXIMUM Magnetos CHECKED Max. drop 150 RPM, Max. diff (L/R) 50RPM Min. drop must noticeable Ignition Key BOTH Throttle RPM Carburetor Heat max. 50 RPM CHECKED Throttle IDLE Carburetor Heat OFF 7 - Before Take Off Flaps T/O Trim NEUTRAL Canopy (Warning Light Off) CLOSED Main Switch (Generator/Battery).... ON Fuel Pump ON Transponder ALT 8 - Departure Briefing Rotate (Normal / Short Field ) /57 KTS Initial Climb (Vx) KTS Further Climb (Vy) KTS Runway Heading After T/O Check, (First turn, Altitude)... Leave Control Zone via T/O Clearance RECEIVED Brakes HOLD Throttle FULL OPEN T/O Power CHECKED Speed Indication CHECKED Rotate KTS 12 - After T/O (500ft AGL) Flaps UP Speed KTS Engine Instruments GREENARC Fuel Pump OFF Taxi / Landing Light OFF Reduce Prop. Cycle to Green Arc... EXECUTE 1 - On Ground Call Out STOP Throttle IDLE Brake AS REQ. 2 - After T/O Call Out BREAK Throttle when possible AS REQ. Pitch DOWN Speed when no Engine KTS Flaps AS REQ. 9 - Line Up Line Up Clearance RECEIVED Approach / Departure / Runway..... CLEAR Runway Heading CHECKED 10 - Take Off T/O Clearance RECEIVED Throttle FULL OPEN T/O Power CHECKED Speed Indication CHECKED Rotate KTS 2-4 Template: 01. March 2003 Text: 01. March 2003

11 Rechts CRUISE/APPROACH 1 - Cruise 2 Check 5 - ABeam Threshold List Throttle / Prop. Cycle POWER T. Engine Instruments CHECK 2 - Cruise Descent Carburetor Heat AS REQ. Throttle AS REQ. Prop. Cycle RPM SET 3 - Fast Descent Carburetor Heat ON Throttle IDLE Prop. Cycle 2400 RPM SET Speed KTS 4 - Approach Briefing ATIS RECEIVED Altimeter QNH-SET Traffic Pattern Altitude We will join TRAFFIC P. Cross-, Downwind, Base, Final (left/right) Airfield Elevation Pressure Altitude Stand. Temp. Time NOTICE Fuel Pump ON Carburetor Heat ON Throttle MP Speed WHITE ARC Flaps T/O Prop. Cycle MAX. RPM Landing Light ON Approach Speed KTS 6 - Final Flaps AS REQ. Trim NEUTRAL Speed KTS Landing Clearance RECEIVED 7 - After Landing Throttle IDLE Flaps UP Carburetor Heat OFF Fuel Pump OFF Transponder OFF Engine Power as % of max. continuous power (RPM * 100) ft m C [ F] 55% 65% 75% 85% 95% 104% RPM MP RPM MP RPM MP RPM MP RPM MP RPM MP [59] 19 24, , , , ,0 25,5 29, [52] 19 24, , , , , [45] 19 23, , , , [37] 19 23, , , [30] 20 21, , , [23] 21 20, , [16] 22 18, [12] 23 17,3 Consumption per hour 12,3 liters 14,5 liters 16,6 liters 19,3 liters 22,7 liters 24,7 liters Raise manifold pressure by 0,7 in Hg at ISA +10 C (18 F) Lower manifold pressure by 0,7 in Hg at ISA -10 C (-18 F) 8 - GO AROUND Flaps UP Carburetor Heat OFF Minimum Safety Altitude First turn Throttle FULL OPEN Carburetor Heat OFF Template: 01. March 2003 Text: 01. March

12 Links 2 Check List SHUTDOWN / PARKING 1 - Shut Down Parking Brake SET Throttle IDLE ELT - Check 121,50MHz CHECKED Avionics Master Switch OFF Ignition Switch OFF Lights OFF Master Switch OFF Parking Brake RELEASE 2 - Secure Aircraft Wheel Chocks INSERTED Flight Control lock INSTALLED Aircraft log WRITE Canopy LOCKED Protection Cover INSTALLED Tie downs INSTALLED 2-6 Template: 01. March 2003 Text: 01. March 2003

13 Rechts GENERAL 3 Emergency 1 - Transponder Codes Emergency Communication Failure Hijacked Best glide Flaps T/O Speed 730kg KTS Glide :1 Glide distance is 0,32 Nm longer per 10kts following wind and 0,32 Nm shorter per 10kts Headwind. 3 - Bring to end spin Throttle IDLE Rudder full adverse spin direction... EXECUTE Control stick FORWARD Rudder neutral when spin end EXECUTE Flaps CRUISE Elevator careful pull EXECUTE 4 - Icing E MERGENCY Descent or fly in area with higher temperature Moving flight controls Carburetor heating ON Throttle HIIGHER Cabin air ON IMPORTANT INFO ON ICING CONDITIONS THE STALL SPEED ARE HIGHER IMPORTANT INFO WHEN ICE ON THE WING LEADING EDGE, THE FOLLOWING INSTRUMENTS SHOWS WRONG VALUES / WORKS NOT CORRECT SPEED INDICATOR, ALTIMETER, VARIO- METER, STALL WARNING 5 - Radio failure Headset connector CHECK Volume CHECK Squelch CHECK Try other Headset EXECUTE Template: 21. February 2003 Text: 21. February

14 Links 3 Emergency 1 - Start Run Throttle IDLE Brakes AS REQ. 2 - After T/O not Enough Power Speed (IAS) KTS Throttle FULL OPEN Carburetor Heat ON Choke OFF Fuel Shutoff Valve OPEN Ignition Key BOTH Fuel Pump ON Prop Cycle MAX. RPM When Engine Power not immediately restored, land straight ahead, avoid obstacle. Fuel Shutoff Valve CLOSE Ignition Key OFF Main Switch OFF 3 - Engine Run Rough Carburetor Heat ON Fuel Pump ON Switch ignition Key in all Positions.. L / R / B Throttle FULL OPEN When no improvement reduce Engine Power to minimum, land as soon is possible. 4 - Oil pressure loss When Oil temperatue below green arc and Oil temperature normal. Land on next airfield when Oil temperatue below green arc and Oil temperature climb Reduce Engine Power to minimum, expect engine failure, look out for a landing field. 5 - Fuel pressure loss Fuel Pump ON ENGINE FAILURE Land on next airfield When Fuel Warning light not OFF, land on next airfield, expect engine failure, look out for a landig field. 6 - Restart Engine / Propeller Windmilling Speed (IAS) KTS Flaps TAKE OFF Prop. Cycle MAX. RPM Fuel Shutoff Valve OPEN Ignition Key BOTH Fuel Pump ON Throttle CM OPEN When the Engine within 10 seconds not start, use cold start procedure Oil pressure CHECK Choke OFF Electrical Equipment AS REQ. Oil temperature CHECK 7 - Restart Engine / Propeller stopped All electrical Equipment OFF Main Switch ON Prop. Cycle MAX. RPM Fuel Shutoff Valve OPEN Fuel Pump ON Throttle Engine cold IDLE Choke Engine cold PULL/HOLD Throttle Engine warm CM Choke Engine warm OFF Ignition Key START You can also restart the engine when you pitch down and acclerate to 108 kts. IMPORTANT INFO YOU LOSE 1000FT / 300M After Engine Start. Oil pressure CHECK Choke OFF Electrical Equipment AS REQ. Oil temperature CHECK 3-2 Template: 21. February 2003 Text: 21. February 2003

15 Rechts FIRE / ELECTRICAL 1 - Engine on Ground Fuel Shutoff Valve OFF Throttle FULL OPEN Main switch OFF Ignition key OFF Leave Aircraft Fast 2 - Electrical fire and smoke on ground Main switch (battery) OFF Throttle IDLE Fuel Shutoff Valve OFF Ignition key OFF Canopy OPEN Fire extinguisher AS REQ. 6 - Total Electrical Failure 3 Emergency Circuit Breakers press in EXECUTE Main switch CHECK 7 - Generator failure Main switch CHECK Generator Circuit breaker PUSH IN Generator control circuit breaker.... PUSH IN When generator not load, turn off all electrical equipment that you not need. 3 - Engine in fly Fuel Shutoff Valve OFF Speed KTS Flaps T/O Throttle FULL OPEN Fuel Pump OFF Cabin heating OFF Emergency Landing with stopped Engine 4 - Electrical fire and smoke in fly Main switch OFF Cabin air OPEN Avionics main switch OFF All electrical consumer OFF Main switch battery ON Avionics main switch ON Radio ON Land as soon as possible Emergency Landing with stopped Engine Use fire extinguisher when smoke hold s one 5 - Cabin fire in fly Main switch (battery) OFF Cabin air OPEN Cabin heating OFF Fire extinguisher AS REQ. Land as soon as possible Template: 21. February 2003 Text: 21. February

16 Links 3 Emergency 1 - Landing with stopped Engine Speed (IAS) Flaps (T/O or Land)... 57kts Flaps (Cruise)... 60kts Fuel Shutoff Valve CLOSE Ignition Key OFF Seat belts FASTENED ATC transmit position DONE Main switch OFF 2 - Landing with running Engine Landing field LOOK OUT Safety belts FASTENED Descent BEGIN Throttle AS. REQ. Trim AS REQ. Flaps AS. REQ. Overfly landing field in ft Overfly landing field in FT When possible climb FT ATC transmit position DONE Throttle AS. REQ Prop. Cycle AS REQ. Carburetor Heat ON Fuel pump ON Flaps FULL DOWN Speed KTS Nose wheel up as long as possible.. DONE Brakes AS REQ. Ignition key OFF Main switch OFF LANDING / RUDDER The Landing for each flap position is different. Flaps Cruise position Approach speed 5 kts higher EXECUTE Throttle AS REQ. Shallow descent EXECUTE Flaps T/O position Normal Approach speed EXECUTE Throttle AS REQ. Shallow descent EXECUTE Flaps Landing position Normal Landing EXECUTE 5 - Failure Trim System Blocked Trim Circuit Breakers CHECK Trim switch (Press in both direction) EXECUTE (Wait 5min then try again) Land as soon is possible EXECUTE Trim run off Control stick hold solid EXECUTE Circuit breaker for Trim PULL Check Trim switch CHECK 3 - Landing with defect tire Flaps FULL DOWN Land the aircraft on the opposite runway boundary with the defect tire. Land with the good tire first. When taxi give full aileron in the direction of the good tire. 4 - Flaps Failure Visual check flaps CHECK Speed white arc CHECK Try all flap positions EXECUTE 3-4 Template: 21. February 2003 Text: 21. February 2003

17 Rechts ATC 1 - Flight Plan - AIS 4 Info s 4 - Transponder Codes and Hints Lokal / Inbound / Outbound Callsign / Typ Starttime - ETD (Estimated Time of Departure) Route Flight Time Endurance Persons on Board Pilot in Command Privat Emergency Communication Failure Hijacked Transponder Codes Above 5000ft-MSL (German) Below 5000ft-MSL (German) Ident. Zone when TAS>150kts VFR (Austria) Spell alphabet Alpha Bravo Charlie Delta Echo Foxtrott Golf Hotel India Kilo Juliett Lima Mike November Oscar Papa Quebec Romeo Sierra Tango Uniform Viktor Whiskey X-Ray Yankee Zulu 3 - Position Message Short Position Message Call Sign Position Altitude Long Position Message Call Sign Aircraft Type VFR / IFR From / To Position Altitude Request I NFO S A ND H INTS Template: 12. April 2003 Text: 26. Mai

18 Links 4 Info s and Hints 1 - Light Signals SIGNALS areas. Aerodrome unsafe do not land Taxi clear of landing area in use The taxiway or runway closed. Return for landing Cleared to taxi Give way to another aircraft and enter holding pattern Airfield or Airport closed, landing not allowed. Stop Cleared to land Attention for bad condition on runway or taxiways. Cleared for take off Land on this aerodrome and proceed to apron white flashing Return to starting point on the aerodrome This landing T shows you the landing or T/O direction. Red pyrotechnic Irrespective of any previous instruction or clearance Do not land for the being! The airfield are used from glider. 2 - Sign s For T/O, Landing and taxi, use only the runway and taxiway. This arrow show s you that you have a right hand traffic pattern. For T/O and landing use only the runway, for other movements on ground you can use all 4-2 Template: 12. April 2003 Text: 26. Mai 2003

19 Rechts NAV / VFR - RULES 4 Info s and Hints 1 - Compass turn fault 2 - Semi Circle rules When fly VFR and above 3000ft then coin follwing Track over Ground. 3 - Airspace structure Special VFR - Flight are only allowed when all following conditions exist. On day in controlled Airspace Visibility min. 1,5km Clouds ceiling 660ft Template: 12. April 2003 Text: 26. Mai

20 Links 4 Info s and Hints 1 - Convert C to F Convert C to F C = 5 9 ( F 32) Convert F to C F = ( 9 5 C) + 32 CONVERSION / PHONE 2 - Conversion Unit multiply Result by kilogram (kg) 2,2046 pounds (lbs) Tab.1: Weight and Mass Unit x to Unit Nautical Miles (kts) 1,852 Kilometer (km) Statute miles (mph) 1,6093 Kilometer (km) Feet (ft) 0,3048 Meters (m) Meters (m) 3,28084 Feet (ft) Inch (in) 2,54 Centimeter (cm) Centimeter 0,3937 Inch (in) Tab.2: Distance Unit x to Unit U.S. Gallon (USgal) 3,78541 litre (l) quart (qt.) 0,9464 litre (l) Tab.3: Fill 3 - Phonenumbers ICAO Name Number LOWG Graz - Tower +43(5) LOWG Graz - AIS +43(5) LOWG Graz - BP +43(664) LOWK Klagenfurt - Tower +43(5) LOWK Klagenfurt - AIS +43(5) Tab.4: Phonenumbers 4-4 Template: 12. April 2003 Text: 26. Mai 2003

21 Rechts SHORTCUT 5 CAS IAS GS TAS VFE VA VNO VNE VS0 VS Vx Vy Calibrated Airspeed Indicated Airspeed Ground Speed True Airspeed Maximum Flaps Extended Speed Manoeuvering Speed Max. Structural Cruising Speed Never Exceed Speed Power Off Stall (Landing configuration) Power Off Stall Speed Clean configuration (Flaps Up) Best angle of Climb Best Rate of Climb Template: 01. March 2003 Text: 01. March

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