NORMAL PROCEDURES CHECKLIST XL2
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1 NORMAL PROCEDURES CHECKLIST XL2 AIRSPEEDS FOR NORMAL OPERATION Unless otherwise noted, the following speeds are based on a maximum weight of 1653 lbs, and may be used for any lesser weights. Takeoff Rotation Speed (V r ): Flaps KIAS Takeoff Safety Speed: Flaps 20 (At 50 ft)...65 KIAS Enroute Climb, Flaps Up: Normal, sea level KIAS Normal, 10,000 feet MSL KIAS Best Rate of Climb Speed, Flaps Up (V y ): Sea level...80 KIAS 10,000 ft...75 KIAS Best Angle of Climb Speed, Flaps Up (V x ): Sea level...70 KIAS 10,000 ft...65 KIAS Normal Approach Speed: Flaps Up KIAS Flaps KIAS Flaps KIAS Balked Landing Climb Speed: Wide Open Throttle, Flaps KIAS Maximum Recommended Turbulent Air Penetration (V a ): 1653 lbs KIAS 1450 lbs...94 KIAS Maximum Demonstrated 90 Crosswind Velocity: Takeoff or Landing...15 Knots The maximum demonstrated crosswind velocity reflects the greatest crosswind available during certification tests and is not considered a limitation. PREFLIGHT PREPARATION 1. Airplane... AIRWORTHY, REQD DOCUMENTS ON BOARD 2. Weather...SUITABLE 3. Baggage... WEIGHED, STOWED, SECURE 4. Weight and C.G....WITHIN LIMITS 5. Navigation... PLANNED 6. Charts and Navigation Equipment... ON BOARD 7. Performance and Range...COMPUTED AND SAFE PREFLIGHT INSPECTION Figure 7-1 WALK- AROUND Preflight inspection path, starting in cockpit, then out and around aircraft in clockwise direction, ending back in cockpit. 1 2 CAUTION Do not step on flap when entering or leaving the cockpit.
2 1. COCKPIT a. Seat Belt... RELEASE, IF USED TO SECURE CONTROL STICK b. Ignition Switch...OFF c. FADEC PWR A and B switches...off d. Avionics Master Switch...OFF e. Battery Master Switch...ON f. Fuel Quantity Indicator...CHECK (Fuel Sufficient for Flight) g. Voltmeter...CHECK (Min V) h. Flaps... EXTEND FULL DOWN (30 ) i. Lights...CHECK OPERATION j. Stall Warning Vane...PULL UP (Check Audible Voice Warning) k. Battery Master Switch...OFF l. Fire Extinguisher... AVAILABLE m. Emergency Egress Hammer... AVAILABLE 2. COWLING, ENGINE PROPELLER a. Upper and Lower Cowling Fasteners...SECURE b. Propeller/Spinner... CONDITION, SECURITY c. Nose Landing Gear Leg...CONDITION d. Nose Wheel Steering Bearing...SECURITY e. Nose Wheel Tire... CONDITION, PROPER INFLATION f. Cowling Right/Left Air Intakes...CLEAR g. Alternator Belt...CONDITION, TENSION h. Engine Oil...CHECK QUANTITY (Min. 5 Qts.) i. Exhaust... CONDITION, SECURITY j. Windshield...CONDITION, CLEANLINESS 3. FWD FUSELAGE, RIGHT a. Right Cabin Air Intake...CLEAR b. Fwd Fuselage...CONDITION, CHECK FOR DAMAGE c. Right Cabin Door...CONDITION d. Right Main Landing Gear Leg...CONDITION e. Brakes...CONDITION, NO EVIDENCE OF LEAKS f. Tire... CONDITION, PROPER INFLATION g. Chocks... REMOVE 4. RIGHT WING, LEADING EDGE a. Leading Edge... CONDITION b. Stall Strip... SECURE c. Right Wing (Top and Underside)... CONDITION d. Inspection Access Panels (Underside)...FASTENERS SECURE e. Tie-down Rope...REMOVE f. Wingtip and Lights...CONDITION, SECURITY 5. RIGHT WING, TRAILING EDGE a. Aileron...CONDITION, FREE AND CORRECT MOVEMENT b. Aileron Hinges (2)...CONDITION, SECURITY c. Aileron Mass Balance Weights... UNOBSTRUCTED, SECURE d. Aileron Pushrod...CHECK JAMNUT SECURE e. Flap... CONDITION f. Flap Slot... CLEAR g. Flap Hinges (3)...CONDITION, SECURITY (cotter pins) 6. AFT FUSELAGE, RIGHT a. Marker Beacon Antenna (Underside)...CONDITION, SECURITY b. Aft Fuselage... CONDITION, CHECK FOR DAMAGE c. Fuselage Mounted Antennas (Top)...CONDITION, SECURITY 7. EMPENNAGE a. General Condition...CHECK b. Stabilator and Trim Tab...CHECK c. Rudder...CHECK 8. AFT FUSELAGE, LEFT a. Aft Fuselage... CONDITION, CHECK FOR DAMAGE b. Fuel Filler Cap...CLOSED AND LOCKED c. Fuel Vent (Underside)... UNOBSTRUCTED d. Transponder Antenna (Underside)...CONDITION, SECURITY e. Outside Air Temp Probe (Underside)...ATTACHMENT f. Fuselage Belly Fairing...FASTENERS SECURE 3 4
3 9. LEFT WING, TRAILING EDGE a. Check Same As Right Wing (REVERSE ORDER) b. Aileron Trim Tab (if installed)... CONDITION, SECURITY 10. LEFT WING, LEADING EDGE a. Check Same As Right Wing (REVERSE ORDER) b. Pitot-Static Blade... CONDITION, OPENINGS CLEAR 11. FWD FUSELAGE, LEFT a. Left Main Landing Gear Leg...CONDITION b. Brakes...CONDITION, NO EVIDENCE OF LEAKS c. Tire... CONDITION, PROPER INFLATION d. Chocks... REMOVE e. Fuselage Belly Fairing... FASTENERS SECURE f. Fuel Tank Sump...SAMPLE, CHECK FOR CONTAMINATION g. Fuel Strainer...SAMPLE, CHECK FOR CONTAMINATION h. Left Cabin Air Intake...CLEAR i. Left Cabin Door...CONDITION BEFORE STARTING ENGINE 1. Preflight Inspection... COMPLETE 2. Passenger Briefing... COMPLETE 3. Seat Belts and Harnesses...ADJUST, SECURE 4. Rudder Pedals...ADJUST AS DESIRED 5. Doors... AS REQUIRED 6. Circuit Breakers...CHECK IN If the aircraft has been exposed to temperatures below -7 C / 20 F for more than 2 hours, preheating is required. If engine does not start on the first try, allow 2 minutes for the starter to cool before trying again. WARNING If an abnormal HSA indication is observed during any operational check, takeoff is prohibited, abort flight and notify maintenance. Do not attempt flight until the discrepancy has been corrected. 5 STARTING ENGINE 1. Fuel Selector Valve...VERIFY ON 2. Brakes...CONFIRM PARKING BRAKE SET 3. Alternate Air... OFF 4. Fuel Boost Pump Mode Switch... AUTO The FUEL BOOST PUMP MODE and FADEC PWR A and B switches are lever lock type. The switch handle must be pulled slightly away from the instrument panel to allow the switch to be moved. 5. Master (battery and alternator) Switch...ON 6. Annunciator Lights... TEST/SET 7. VM VOLTS> FADEC PWR A and B Switches... ON 9. Ignition Switch...L (Left) 10. Fuel Boost Pump...LISTEN FOR OPERATION 11. HSA / Annunciator Lights... TEST/SET 12. Throttle...FULL FORWARD 13. HSA WOT Annunciator... CHECK ON 14. Throttle...1/4 INCH FORWARD OF IDLE 15. Propeller Area... CLEAR 16. Ignition Switch...START If airplane has not been operated for an extended period, HSA PPWR FL and/or EBAT FL may remain illuminated before, and for a few minutes after, engine start. AFTER START 1. Throttle RPM 2. Lights...AS REQUIRED 3. Cockpit Rheostat switches...as REQUIRED 4. VM IN LIMITS (no blinking values) 5. Avionics Master Switch...ON 6. Flaps...UP (0 ) 7. Transponder... STANDBY 8. Flight Instruments/Nav/Comm...CHECK/SET 9. Fuel Boost Pump Mode Switch...AS REQUIRED 6
4 ENGINE RUNUP 1. Fuel Selector...SET 2. Parking Brake...SET 3. Throttle...APPROX RPM 4. Alternate Air... CHECK (slight RPM decrease) 5. Fuel Boost Pump Mode Switch...ON 6. HSA FUEL PMP Annunciator...CHECK ON 7. Fuel Boost Pump Mode Switch...OFF 8. HSA FUEL PMP Annunciator...CHECK ON 9. Fuel Pressure... CHECK IN LIMITS 10. Fuel Boost Pump Mode Switch...AUTO 11. HSA FUEL PMP Annunciator... CHECK OFF 12. Annunciator Lights...TEST/SET 13. HSA Annunciator Lights...TEST/SET 14. VM IN LIMITS 15. FADEC PWR B Switch...OFF 16. Engine... CHECK, NO RPM DROP OR SURGE 17. HSA EBAT FL Annunciator...CHECK ON 18. FADEC PWR B Switch...ON 19. HSA... CHECK ALL LAMPS EXTINGUISHED 20. FADEC PWR A Switch...OFF 21. Engine...NO RPM DROP OR SURGE 22. HSA PPWR FL and EBAT FL Annunciators...CHECK ON 23. FADEC PWR A Switch...ON 24. HSA... CHECK ALL LAMPS EXTINGUISHED 25. Ignition Switch... R (Right) POSITION 26. RPM DROP...10 RPM MINIMUM, 150 RPM MAXIMUM 27. HSA...FADEC CAUTION light 28. Ignition Switch...BOTH 29. HSA... CHECK ALL LAMPS EXTINGUISHED 30. Ignition Switch... L (Left) POSITION 31. RPM DROP RPM MIN, 150 RPM MAX (Maximum difference between L and R is 75 RPM.) 32. HSA...FADEC CAUTION light 33. Ignition Switch...BOTH 34. HSA... CHECK ALL LAMPS EXTINGUISHED 35. Throttle...IDLE 7 8 WARNING If any abnormal HSA indications are observed after all operational checks are complete, takeoff is prohibited, abort flight and notify maintenance. Do not attempt flight until the discrepancy has been corrected. BEFORE TAKEOFF During cold weather operations, the engine should be properly warmed up before takeoff. The minimum oil temperature for takeoff is 100 F. 1. Flight Controls... FREE AND CORRECT 2. Fuel Quantity... VERIFY 3. Flight Instruments/Nav/Comm...CHECK, SET 4. Flaps Trim... SET FOR TAKEOFF 6. Canopy Doors...CLOSED AND SECURE 7. Seat Belts & Harness... SECURE 8. Brakes...RELEASE CLIMB 1. Flaps...SET to 0 2. Throttle...VERIFY FULL FORWARD 3. HSA WOT Annunciator... CHECK ON 4. Airspeed KIAS CRUISE 1. Airspeed... MAINTAIN POWER UNTIL CRUISE AIRSPEED IS ATTAINED 2. Power...SET CRUISE POWER 3. Elevator Trim... ADJUST AS REQUIRED 4. Fuel Boost Pump Mode Switch...CHECK AUTO 5. Lights...AS REQUIRED 6. Engine Instruments and HSA... CHECK OFTEN For optimum fuel economy, do not change the throttle position for approximately five minutes after setting cruise power.
5 DESCENT 1. Flight Instruments/Nav/Comm... CHECK, SET 2. Elevator Trim...ADJUST AS REQUIRED 3. Engine Instruments and HSA... CHECK OFTEN BEFORE LANDING 1. Fuel Boost Pump Mode Switch... CHECK AUTO 2. Flaps... AS DESIRED (At 80 KIAS or less) 3. Lights... AS REQUIRED 4. Seat Belts and Harnesses... SECURED AFTER LANDING 1. Flaps...RETRACT 2. Transponder...STANDBY 3. Lights... AS REQUIRED SHUTDOWN 1. Avionics Master Switch...OFF 2. Ignition Key...OFF 3. FADEC PWR A and B Switches...OFF 4. All Light Switches...OFF 5. All Electrical Switches...OFF 6. Master Switch...OFF 7. Parking Brake... AS REQUIRED CAUTION If the secondary power (PWR B) switch is left in the ON position after engine shutdown, the aircraft s backup battery will discharge and be drained of power. Be sure to turn the primary (PWR A) and secondary (PWR B) switches off after engine shutdown. SECURING AIRPLANE 1. Wheels...CHOCKED 2. Control Stick...SECURED by SEAT BELT 3. Pitot Cover...ON (as required) 4. Rudder Gust Lock...ON (as required) 5. Wings and Tail...TIE-DOWN 6. Doors...CLOSED AND LATCHED 9
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