Piper PA-28-161 Warrior II — danbury_flight_school_Piper_PA_28_161

Preflight Inspection — Cockpit COCKPIT POH and Documents AVAILABLE Control Wheel RELEASE BELTS Avionics OFF Parking Brake SET Electrical Switches OFF MAGNETO Switch OFF Mixture IDLE CUT OFF MASTER Switch ON Fuel Quantity Gauges CHECK Annunciator Panel CHECK MASTER Switch OFF Flight Controls CHECK Flaps CHECK Trim CHECK, SET NEUTRAL Pitot and Static Drain DRAIN, CLOSE Windows CHECK CLEAR Tow bar STOW Baggage SECURE Baggage Door CLOSE, SECURE

Preflight Inspection — Right Wing WALKAROUND RIGHT WING Wing FREE OF ICE, SNOW, FROST Control Surfaces CHECK FOR INTERFERENCE ICE, SNOW, FROST CHECK Hinges CHECK FOR INTERFERENCE Static Wicks CHECK Wing Tip and Lights CHECK Fuel Tank CHECK SUPPLY VISUALLY, SECURE CAPS Fuel Tank Sump DRAIN, CHECK FOR SEDEMENT AND PROPER FUEL Fuel Vent CLEAR Tie Down REMOVE Main Gear Strut PROPER INFLATION (4.5 IN. of strut exposed) Tire (24 psi) and Brakes CHECK Fresh Air Inlet CHECK CLEAR

Preflight Inspection — Nose NOSE Fuel and Oil CHECK FOR LEAKS Cowling SECURE Windshield CLEAN Propeller and Spinner CHECK Air Inlets CLEAR Alternator Belt CHECK TENSION Landing Light CHECK Nose Chock REMOVE Nose Gear Strut CHECK INFLATION (3.25 IN. of strut exposed) Nose Wheel Tire (30 psi) CHECK Oil CHECK LEVEL Dipstick PROPERLY SEATED Fuel Strainer DRAIN, CHECK FOR SEDEMENT AND PROPER FUEL

Preflight Inspection — Left Wing LEFT WING Wing FREE OF ICE, SNOW, FROST Fresh Air Inlet CHECK CLEAR Main Gear Strut PROPER INFLATION (4.5 IN. of strut exposed) Tire (24 psi) and Brakes CHECK Fuel Tank CHECK SUPPLY VISUALLY, SECURE CAPS Fuel Tank Sump DRAIN, CHECK FOR SEDEMENT AND PROPER FUEL Fuel Vent CLEAR Tie Down REMOVE Pitot Cover REMOVE, HOLES CLEAR Wing Tip and Lights CHECK Hinges CHECK FOR INTERFERENCE Static Wicks CHECK

Preflight Inspection — Fuselage FUSELAGE Antennas CHECK Empennage FREE OF ICE, SNOW, FROST Fresh Air Inlet CHECK CLEAR Stabilator and Trim Tab CHECK FOR INTERFERENCE Tie Down REMOVE MASTER Switch ON Cockpit Lighting CHECK Nav and Strobe Lights CHECK Stall Warning CHECK Pitot Heat CHECK All Switches OFF Passengers BOARD & BRIEFED Cabin Door CLOSE & SECURE Seat Belts and Harnesses FASTEN CHECK INERTIA REEL

Starting Engine When Cold Throttle 1/4" OPEN MASTER Switch ON Electric Fuel Pump ON Mixture FULL RICH Anti-Collision Light(s) ON Starter ENGAGE Throttle 1000 RPM Oil Pressure CHECK If engine does not start within 10 sec., prime and repeat START.

Starting Engine When Hot Throttle 1/2" OPEN MASTER Switch ON Electric Fuel Pump ON Mixture FULL RICH Anti-Collision Light(s) ON Starter ENGAGE Throttle ADJUST Oil Pressure CHECK

Starting Engine When Flooded Throttle FULL OPEN MASTER Switch ON Electric Fuel Pump OFF Mixture IDLE CUT OFF Anti-Collision Light(s) ON Starter ENGAGE Mixture ADVANCE Throttle RETARD Oil Pressure CHECK

Starting Engine with External Power Source MASTER Switch OFF ALL Elecrical Equipment OFF Terminals CONNECT External Power Plug INSERT IN FUSELAGE Proceed with Normal Start. Throttle LOWEST POSSIBLE RPM External Power Plug DISCONNECT FROM FUSELAGE MASTER Switch ON - CHECK AMMETER Oil Pressure CHECK

Warm-Up Throttle 800 to 1200 RPM Avionics ON & TUNED Transponder STBY CHECK ATIS 127.75 (KDXR) Contact Ground Control 121.60 (KDXR)

Ground Check Throttle 2000 RPM MAGNETOS MAX. DROP 175 RPM, MAX. DIFFERNCE 50 RPM Vacuum 4.8" - 5.1" HG Oil Temp CHECK Oil Pressuer CHECK Air Conditioner (If Equipped) CHECK Annunciator Panel PRESS-T0-TEST Carburetor Heat CHECK Engine is warm for takeoff when throttle can be opened without engine faltering. Electric Fuel Pump OFF Fuel Pressure CHECK Throttle RETARD

Before Takeoff MASTER Switch ON Flight Instruments CHECK Fuel Selector PROPER TANK Electric Fuel Pump ON Engine Gauges CHECK Carburetor Heat OFF Seat Backs ERECT Mixture SET Primer LOCK Belts / Harness FASTENED / CHECK Empty Seats SEAT BELTS SNUGLY FASTENED Flaps SET Trim Tab SET Controls FREE Doors LATCH Air Conditioner OFF Contact Tower 119.40 (KDXR)

0 Degree Flaps Takeoff Performance Flaps UP Accelerate to 40-52 KIAS (depending on weight) Control Wheel BACK PRESSURE TO ROTATE TO CLIMB ATTITUDE Accelerate to and maintain 44 to 57 KIAS (depending on weight) until obstacle clearance is achieved and climb out at 79 KIAS.

25 Degree Flaps Takeoff Performance Flaps 25 degrees (2nd NOTCH) Accelerate to 40-52 KIAS (depending on weight) Control Wheel BACK PRESSURE TO ROTATE TO CLIMB ATTITUDE Accelerate to and maintain 44 to 57 KIAS (depending on weight) until obstacle clearance is achieved and climb out at 79 KIAS. Flaps RETRACT SLOWLY

Soft Field, Obstacle Clearance Flaps 25 degrees (2nd NOTCH) Accelerate and lift off nose gear as soon as possible. Lift off at lowest possible airspeed. Accelerate just above ground to 52 KIAS to climb past obstacle height. Continue climbing while accelerating to best rate of climb speed, 79 KIAS. CHECK Flaps RETRACT SLOWLY

Soft Field, No Obstacle Flaps 25 degrees (2nd NOTCH) Accelerate and lift off nose gear as soon as possible. Lift off at lowest possible airspeed. Accelerate just above ground to best rate of climb speed (Vy) 79 KIAS. CHECK Flaps RETRACT SLOWLY

Climb Best Rate (Flaps up) 79 KIAS Best Angle (Flaps up) 63 KIAS En Route 87 KIAS Electric Fuel Pump OFF AT DESIRED ALTITUDE

Cruising Reference Performance charts and Engine Operators Manual. CHECK Normal Max. Power 75% Power SET PER POWER TABLE Mixture ADJUST

Descent — Power Off Carburetor Heat ON IF REQUIRED Throttle CLOSE Airspeed AS REQUIRED Mixture AS REQUIRED Power VERIFY WITH POWER EVERY 30 SECONDS

Approach and Landing Fuel Selector PROPER TANK Seat Backs ERECT Belts / Harnesses FASTEN / CHECK Electric Fuel Pump ON Mixture SET Flaps SET - 103 KIAS MAX. Air Conditioner OFF Trim to 70 KIAS Final Approach Speed (Flaps 40 degrees) 63 KIAS

Stopping Engine Flaps RETRACT Electric Fuel Pump OFF Air Conditioner OFF Radios OFF Throttle OFF Mixture IDLE CUT OFF Magnetos OFF MASTER Switch OFF

V-Speeds V-SPEEDS (KIAS) Vne — Velocity Never Exceed 160 Vno — Max Structural Cruising Speed 126 Vfe — Flap Extension Speed 103 Va — Max Design Maneuvering At 2440 LBS G.W. 111 Va — Max Design Maneuvering At 1531 LBS G.W. 88 Use linear interpretation for intermediate weights. Vr — Rotation Speed 45-55 Vx — Best Angle of Climb 63 Vy — Best Rate of Climb 79 Vs — Stalling Speed 60 Vso — Stalling Speed - Landing Configuration 44 Vg — Gliding Speed 73 Max Crosswind 17 Steep Turns 111 Lazy Eights 111 Chandelles 111

Engine Fire During Start Starter CRANK ENGINE Mixture IDLE CUT OFF Throttle OPEN Electric Fuel Pump OFF Fuel Selector OFF Abandon if fire continues.

Engine Power Loss During Takeoff If sufficient runway remains for a normal landing, land straight ahead. CHECK If sufficient runway remains: a. Maintain safe speed CHECK If sufficient runway remains: b. Make only shallow turns to avoid obstructions CHECK If sufficient runway remains: c. Flaps as situation requires CHECK IF SUFFICIENT ALTITUDE HAS BEEN GAINED TO ATTEMPT A RESTART Maintain safe airspeed CHECK Fuel Selector SWITCH TO TANK CONTAINING FUEL Electric Fuel Pump CHECK ON Mixture CHECK RICH Carburetor Heat ON Primer LOCKED If power is not regained, proceed with power off landing.

Engine Power Loss in Flight Fuel Selector SWITCH TO TANK CONTAINING FUEL Electric Fuel Pump ON Mixture RICH Carburetor Heat ON Engine Gauges CHECK FOR INDICATION OF CAUSE OF POWER LOSS Primer CHECK LOCKED If no fuel pressure is indicated, check tank selector position to be sure it is on a tank containing fuel. When power is restored: Carburetor Heat OFF Electric Fuel Pump OFF

Power Off Landing Locate Suitable Field CHECK Establish Spiral Pattern CHECK 1000 ft. above field at downwind position for normal landing approach. When field can easily be reached slow to 63 KIAS for shortest landing. Touchdowns should normally be made at lowest possible airspeed with full flaps. CHECK When committed to landing: Ignition OFF MASTER Switch OFF Fuel Selector OFF Mixture IDLE CUT OFF Seat Belts and Harnesses TIGHT

Fire in Flight Source of Fire CHECK ELECTRICAL FIRE (Smoke in Cabin): MASTER Switch OFF Vents OPEN Cabin Heat OFF Land as soon as practical. ENGINE FIRE: Fuel Selector OFF Throttle CLOSED Mixture IDLE CUT OFF Electrical Fuel Pump CHECK OFF Heater OFF Defroster OFF Proceed with POWER OFF landing procedure.

Electrical Failures ALT Annunciator Light Illuminated: Ammeter CHECK TO VERIFY INOP ALT. If Ammeter Shows Zero: ALT Switch OFF Reduce electrical loads to minimum. ALT Circuit Breaker CHECK AND RESET AS REQUIRED ALT Switch ON If Alternator output cannot be restored, reduce electrical loads and land as soon as practical. The battery is the only remaining source of electrical power.

Electrical Overload (Alternator over 20 amps above known electrical load) ALT Switch ON BATT Switch OFF If alternator loads are reduced: Land as soon as practical. Electrical Load REDUCE TO MINIMUM Due to increased system voltage and radio frequency noise, operation with ALT Switch ON and BATT Switch OFF should be made only when required by an electrical system failure. If alternator loads are not reduced: Land as soon as possible. Anticipate complete electrical failure. ALT Switch OFF BATT Switch AS REQUIRED

Spin Recovery Throttle IDLE Ailerons NEUTRAL Rudder FULL OPPOSITE TO DIRECTION OF ROTATION Control Wheel FULL FORWARD Rudder NEUTRAL (WHEN ROTATION STOPS) Control Wheel AS REQUIRED TO SMOOTHLY REGAIN LEVEL FLIGHT ALTITUDE

Open Door If both upper and lower latches are open, the door will trail slightly open and airspeeds will be reduced slightly. To close door in flight: Slow Airplane to 89 KIAS Cabin Vents CLOSE Storm Window OPEN If UPPER Latch is open LATCH If SIDE Latch is open PULL ON ARM REST WHILE MOVING LATCH HANDLE TO LATCHED POSITION If BOTH Latches are open LATCH SIDE LATCH THEN TOP LATCH

Engine Roughness Carburetor Heat ON If roughness continues after one minute: Carburetor Heat OFF Mixture ADJUST FOR MAX. SMOOTHNESS Electric Fuel Pump ON Fuel Selector Switch Tanks Engine Gauges CHECK Magneto Switch L then R then BOTH If operation is satisfactory on either one, continue on that magneto at reduced power and full RICH mixture to first airport. Prepare for POWER OFF LANDING.