TPOH AFM Temporary Change Airplane Flight Manual (AFM) Temporary Change Information in this Temporary Change adds to, supersedes, or deletes information in the basic Pilot s Operating Handbook. Affected Publications: Filing Instructions: Purpose: Basic Airplane Flight Manuals: PN 13772-006 Original Issue (FAA Approved) PN 13772-006AR Original Issue (FAA Approved on behalf of ANAC-DA of Argentina) PN 13772-006E Original Issue (FAA Approved on behalf of EASA) PN 21400-006 Original Issue (FAA Approved on behalf of ANAC of Brazil) Insert the following revised pages and retain until further notice. Remove and discard the superseded pages. Insert this TPOH cover page adjacent to the last page of the List of Effective Pages and retain until further notice. This POH Temporary Change revises the Preflight Inspection procedure. Affected Sections: Section 4 - - Preflight Inspection, pages 4-4 thru 4-8.4 TPOH 17-02 1 of 2
TPOH AFM Temporary Change Intentionally Left Blank 2 of 2 TPOH 17-02
Section 4 Introduction This section provides amplified procedures for normal operation. Normal procedures associated with optional systems can be found in Section 9: Log of Supplements. Airspeeds for Normal Operation Unless otherwise noted, the following speeds are based on a maximum weight of 3600 lb. and may be used for any lesser weight. However, to achieve the performance specified in Section 5 for takeoff and landing distance, the speed appropriate to the particular weight must be used. Takeoff Rotation: Normal, Flaps 50%...73 KIAS Obstacle Clearance, Flaps 50%...84 KIAS Enroute Climb, Flaps Up: Normal...110-120 KIAS Best Rate of Climb, SL...108 KIAS Best Rate of Climb, 10,000...99 KIAS Best Angle of Climb, SL...88 KIAS Best Angle of Climb, 10,000...88 KIAS Landing Approach: Normal Approach, Flaps Up...90-95 KIAS Normal Approach, Flaps 50%...85-90 KIAS Normal Approach, Flaps 100%...80-85 KIAS Short Field, Flaps 100% (V REF )...79 KIAS Go-Around, Flaps 50%: Full Power...80 KIAS Maximum Recommended Turbulent Air Penetration: 3600 lb...140 KIAS 2900 lb...123 KIAS Maximum Demonstrated Crosswind Velocity: Takeoff or Landing...21 Knots TPOH 17-02 4-3
Section 4 Preflight Inspection (All Serials) Before carrying out preflight inspections, ensure that all required maintenance has been accomplished. Review your flight plan and compute weight and balance. Throughout the walk-around: check all hinges, hinge pins, and bolts for security; check skin for damage, condition, and evidence of delamination; check all control surfaces for proper movement and excessive free play; check area around liquid reservoirs and lines for evidence of leaking. In cold weather, remove all frost, ice, or snow from fuselage, wing, stabilizers and control surfaces. Ensure that control surfaces are free of internal ice or debris. Check that wheel fairings are free of snow and ice accumulation. Check that Pitot probe warms within 30 seconds of setting Pitot Heat to ON. 6 5 4 3 7 8 1 2 13 9 10 11 12 _FM04_5332 1. Cabin a. Required Documents...ON BOARD b. Avionics Power Switch...OFF (Continued on following page) 4-4 TPOH 17-02
Section 4 c. Bat 2 Master Switch...ON d. PFD...VERIFY ON e. Essential Bus Voltage... 23-25 VOLTS f. Flap Position Light... OUT g. Bat 1 Master Switch...ON h. Avionics Cooling Fan...AUDIBLE i. Avionics Master Switch...ON j. Fuel Quantity...CHECK k. Fuel Selector... SELECT FULLEST TANK l. Flaps... 100%, CHECK LIGHT ON m. Lights... CHECK OPERATION n. Stall Warning System Inlet... UNOBSTRUCTED o. Stall Warning... TEST Note Test stall warning system by applying suction to the stall warning system inlet and noting the warning horn sounds. p. Pitot Heat...ON WARNING Pitot Heat Probe may be hot. (1) Verify probe is hot. q. Pitot Heat...OFF r. Avionics Master Switch...OFF s. Bat 1 and 2 Master Switches...OFF t. Alternate Static Source...NORMAL u. Circuit Breakers... IN v. Fire Extinguisher... CHARGED AND AVAILABLE w. Emergency Egress Hammer... AVAILABLE x. CAPS Handle... PIN REMOVED 2. Left Fuselage a. Door Lock... UNLOCK (Continued on following page) TPOH 17-02 4-5
Section 4 b. COM 1 Antenna (top)...condition AND ATTACHMENT c. Transponder Antenna (underside)... CONDITION AND ATTACHMENT d. COM 2 Antenna (underside)... CONDITION AND ATTACHMENT e. Wing/Fuselage Fairing... CHECK f. Baggage Door...CLOSED AND SECURE g. Static Button... CHECK FOR BLOCKAGE h. Parachute Cover... SEALED AND SECURE 3. Empennage a. Tiedown Rope... REMOVE b. Horizontal and Vertical Stabilizers...CONDITION Note Verify tape covering the forward and aft inspection holes located on outboard ends of horizontal stabilizer is installed and securely attached. c. Elevator and Tab... CONDITION AND MOVEMENT d. Rudder... FREEDOM OF MOVEMENT e. Rudder Trim Tab...CONDITION AND SECURITY f. Attachment hinges, bolts and cotter pins...secure 4. Right Fuselage a. Static Button... CHECK FOR BLOCKAGE b. Wing/Fuselage Fairings... CHECK c. Door Lock... UNLOCK 5. Right Wing Trailing Edge a. Flap and Rub Strips (if installed)... CONDITION AND SECURITY b. Aileron and Tab... CONDITION AND MOVEMENT c. Aileron Gap Seal...SECURITY d. Hinges, actuation arm, bolts, and cotter pins...secure (Continued on following page) 4-6 TPOH 17-02
Section 4 6. Right Wing Tip a. Tip... ATTACHMENT b. Strobe, Nav Light and Lens... CONDITION AND SECURITY c. Fuel Vent (underside)... UNOBSTRUCTED 7. Right Wing Forward and Main Gear a. Leading Edge and Stall Strips...CONDITION b. Fuel Cap...CHECK QUANTITY AND SECURE c. Fuel Drains (2 underside)...drain AND SAMPLE d. Wheel Fairings... SECURITY, ACCUMULATION OF DEBRIS e. Tire...CONDITION, INFLATION, AND WEAR f. Wheel and Brakes...FLUID LEAKS, EVIDENCE OF OVERHEATING, GENERAL CONDITION, AND SECURITY. g. Chocks and Tiedown Ropes...REMOVE 8. Nose, Right Side a. Vortex Generator...CONDITION b. Cowling... ATTACHMENTS SECURE c. Exhaust Pipe.. CONDITION, SECURITY, AND CLEARANCE d. Gascolator (underside)... DRAIN FOR 3 SECONDS, SAMPLE 9. Nose gear, Propeller, and Spinner WARNING Keep clear of propeller rotation plane. Do not allow others to approach propeller. a. Tow Bar... REMOVE AND STOW b. Strut...CONDITION c. Wheel Fairing... SECURITY, ACCUMULATION OF DEBRIS d. Wheel and Tire...CONDITION, INFLATION, AND WEAR e. Propeller...CONDITION (INDENTATIONS, NICKS, ETC.) f. Spinner... CONDITION, SECURITY, AND OIL LEAKS g. Air Inlets... UNOBSTRUCTED h. Alternator...CONDITION (Continued on following page) TPOH 17-02 4-7
Section 4 10. Nose, Left Side a. Landing Light...CONDITION b. Engine Oil... CHECK 6-8 QUARTS, LEAKS, CAP & DOOR SECURE c. Cowling...ATTACHMENTS SECURE d. External Power... DOOR SECURE e. Vortex Generator...CONDITION f. Exhaust Pipe(s)... CONDITION, SECURITY, AND CLEARANCE 11. Left Main Gear and Forward Wing a. Wheel fairings...security, ACCUMULATION OF DEBRIS b. Tire...CONDITION, INFLATION, AND WEAR c. Wheel and Brakes...FLUID LEAKS, EVIDENCE OF OVERHEATING, GENERAL CONDITION, AND SECURITY. d. Chocks and Tiedown Ropes... REMOVE e. Fuel Drains (2 underside)...drain AND SAMPLE f. Fuel Cap...CHECK QUANTITY AND SECURE g. Leading Edge and Stall Strips...CONDITION 12. Left Wing Tip a. Fuel Vent (underside)...unobstructed b. Pitot Mast (underside)... COVER REMOVED, TUBE CLEAR c. Pitot Probe... UNOBSTRUCTED d. Wing Tip Light and Lens...CONDITION AND SECURITY e. Tip... ATTACHMENT 13. Left Wing Trailing Edge a. Hinges, actuation arm, bolts, and cotter pins...secure b. Aileron Gap Seal...SECURITY c. Aileron... FREEDOM OF MOVEMENT d. Flap And Rub Strips (If installed)... CONDITION AND SECURITY 4-8 TPOH 17-02
Section 4 Supplemental Preflight Inspection (Serials w/ FIKI) 14. Cabin a. Circuit Breakers... SET b. Battery 1 Master Switch...ON c. Flaps...100% d. Avionics Master Switch...ON e. Cabin Speaker...ON f. Cabin Door...CLOSE g. WIND SHLD Push-Button...PRESS (1) Verify evidence of deicing fluid from spray nozzles. h. PUMP BKUP Switch...ON (1) Metering Pump Duty Cycle... VERIFY CONTINUOUSLY ON (2) Deicing Fluid and Endurance Indications... CHECK i. PUMP BKUP Switch...OFF j. ICE PROTECT System Switch...ON k. ICE PROTECT Mode Switch... NORM (1) Metering Pump Duty Cycle...VERIFY 30 SECONDS ON, 90 SECONDS OFF (2) Deicing Fluid and Endurance Indications... CHECK l. ICE Inspection Lights Switch...ON (1) Verify LH and RH Operation. m. PITOT HEAT Switch...ON 45 SECONDS, CHECK, THEN OFF WARNING Lift Transducer Faceplate and Vane may be hot. n. Lift Transducer Faceplate... PERCEPTIBLY HOT o. Lift Transducer Vane...VERIFY HOT (1) Verify Stall Warning audio alert after lifting stall vane with wooden toothpick or tongue depressor. (Continued on following page) TPOH 17-02 4-8.1
Section 4 15. Empennage a. Stabilizers Porous Panels...CONDITION AND SECURITY (1) Verify evidence of deicing fluid along length of panels and elevator horns. b. Vertical Porous Panels...CONDITION AND SECURITY (1) Verify evidence of deicing fluid along length of panels. 16. Right Wing Forward and Main Gear a. Fluid Tank...VERIFY DESIRED QUANTITY b. Filler Cap...CONDITION AND SECURITY c. Fluid Vent (underside wing)... UNOBSTRUCTED d. Porous Panels...CONDITION AND SECURITY (1) Verify evidence of deicing fluid along length of panels. 17. Nose, Right Side a. Ice Inspection Light...CONDITION AND SECURITY 18. Nose Gear, Propeller, Spinner a. Slinger Ring... EVIDENCE OF DEICING FLUID b. Propeller De-Ice Boots...CONDITION AND SECURITY 19. Nose, Left Side a. Ice Inspection Light...CONDITION AND SECURITY b. Windshield Spray Nozzles...CONDITION AND SECURITY 20. Left Wing Forward and Main Gear a. Fluid Tank...VERIFY DESIRED QUANTITY b. Filler Cap...CONDITION AND SECURITY c. Fluid Vent (underside wing)... UNOBSTRUCTED d. Porous Panels...CONDITION AND SECURITY (1) Verify evidence of deicing fluid along length of panels. (Continued on following page) 4-8.2 TPOH 17-02
Section 4 21. Cabin a. Fluid Quantity...VERIFY 5 GALLONS MINIMUM b. ICE PROTECT System Switch...OFF c. Flaps...0% d. Cabin Speaker...OFF e. Avionics Master Switch...OFF f. Battery 1 Master Switch...OFF TPOH 17-02 4-8.3
Section 4 Intentionally Left Blank 4-8.4 TPOH 17-02