57b860d7f27145bf5f36663eed4ca98961ab49880b8ed2f4ab38457f6e2ec0f2

1. AIRSPEEDS (IAS): Stall (no flap) Normal Climb Max Rate of Climb 2 eng (SL) 95 Kt Max Angle of Climb 2 eng (SL) 85 Kt Max Angle/ROC one eng. inop. 85 Kt Max Gear Extension 145 Kt Max Flap Extension 0°-10° 145 Kt Max Flap Extension 10°-30° 110 Kt Approx cross-country cruise 145 Kt Stall (full flap) 63 Kt Best power off glide 98 Kt Normal Approach 85 Kt Short Field Approach 82 Kt Max Gear Retraction 115 Kt Max Structural, Cruise 160 Kt Max Maneuvering 120 Kt Never exceed 188 Kt Max demonstrated crosswind 15 Kt 2. LOADING Max All Up Wt. (MAUW) 1723Kg (3800lbs) Wt.of usablefuel — tanks full 310Kg (684lbs) Approx useful load 484Kg*(1 0671bs) Max forward baggage compartment 34Kg (75lbs) Max rear baggage compartment 79Kg (175lbs) Group rating at MAUW 8 Note; Refer to a/c flight manual for correct empty weight 3. POWER SETTINGS: Max permissible FT / 2700 RPM Normal idle 1000 RPM Run up RPM 1800 RPM Normal Climb 25" / 2500 RPM Training & local cruise 21" / 2100 RPM Max Continuous FT / 2700 RPM Min idle 500 RPM Max magneto drop 175 RPM Cross Country Cruise 23'' / 2300 RPM 4. FUEL: Grade 100/130 X/C Cruise Fuel Consumption 65 litres/hr = 46.5 Kg/hr Climb Fuel Consumption 90 litres/hr = 65 Kg/hr UsableCapacity 431 litres 310 Kg/hr Local Cruise Fuel Consumption 53 litres/hr = 38 Kg/hr 5. OIL: Grade D100 Normal Level 6 U. S. Quarts Minimum Pressure (idle) 25 PSI Normal Operating Pressure 60–90 PSI Total Capacity 8 U.S. Quarts Minimum Level 4 U.S. Quarts Maximum Pressure 100 PSI Max Oil Temp 245°F 118°C 6. ELECTRICAL: Battery Voltage 12 volts Alternators (2) 60 amps each Capacity 25 ampere/hour 7. PROPELLERS: Type: Hartzell, Constant speed, full feathering. 8. ENGINES Type: Lycoming 0-320-DID Horsepower: 160HP at 2700 RPM

1. PRE-FLIGHT: Normal inspection and also: (a) Drain Fuel — Tank quick drain under each wing just outboard of undercarriage wells Drain Fuel — Sump drain under each wing at root (b) Note location of: Axe - beneath LH front seat Note location of: Fire Extinguisher - beneath RH front seat Note location of: First Aid Kit - At rear of cabin Note location of: Fuel Dipstick - front glovebox Note location of: Fuel Bottle - front glovebox Note location of: Control lock - pocket behind pilots seat 2. START—UP: Refer Check List Part A 3. RUN—UP: Refer Check List Part B 4. PRE—TAKE OFF: Refer Check List Part C 5. TAKE OFF: (a) Normal: Line up and advance throttles smoothly together to full power Normal: Rotate at 75 knots Normal: Once a positive rate of climb is established and a landing on the remaining runway is no longer possible, apply brakes and select undercarriage up Normal: Allow aircraft to accelerate to 100 kts and maintain. Trim if required (b) Maximum Performance: Line up and apply toe brakes Maximum Performance: Advance throttles evenly together to full power Maximum Performance: Release brakes Maximum Performance: Lift nose wheel as soon as possible and rotate at approximately 61 knots Maximum Performance: Retract undercarriage as soon as positive rate of climb is established Maximum Performance: Accelerate to and maintain 85 knots until all obstacles are cleared 6. CRUISE: Set power as required (refer Section One Part 3). Lean using EGTs 7. PRE-LANDING: Normal BUMFH checks 8. FINAL CHECKS: Normal CLIP checks 9. LANDING: Normal approach 85 knots with 30° flap Short field approach at 82 knots with 30° flap

ENGINE FAILURE ON TAKE OFF ROLL: Close both throttles Maintain direction with rudder Apply Maximum braking If collision unavoidable magnetos off, fuel off, master off 2. ENGINE FAILURE AFTER TAKE OFF PRIOR TO ACHIEVING 85 KNOTS: Close both throttles Maintain at least 75 knots, select full flap Turn only to avoid major obstacles If possible magnetos off, fuel off, master off 3. ENGINE FAILURE IN CLIMB: Control yaw Ensure airspeed at least 85 knots - Adjust as required FULL POWER — Mixtures, Pitch Controls and Throttles ALL FULL FORWARD RAISE flaps RAISE undercarriage IDENTIFY DEAD ENGINE - Dead leg, Dead Engine VERIFY — CLOSE throttle on suspected dead engine FEATHER DEAD ENGINE — Move Pitch Control fully back SECURE DEAD ENGINE - Fuel off, Fuel Pump Off, Ignition Off, Alternator Off MIXTURE LEAN — remain in VMC circle and land In certain conditions of temperature and density altitude the aircraft's single engine performance can be very marginal. The decision to continue must take these factors into account as well as obstacles in the takeoff area, weather and pilots ability. In any case control of the aircraft is the foremost consideration and if any doubt exists the pilot would be best advised to close both throttles and land straight ahead rather than to risk losing control of the aircraft. 4. ENGINE FAILURE IN CRUISE OR DESCENT: As above but prior to securing dead engine — Trouble checks — Refer Check List Section 2, Part A. If unsuccessful: Secure Engine - Refer Check list, Section 2 part B Safeguard Live Engine - Cowl Flap Open Safeguard Live Engine - Reduce Power if possible Safeguard Live Engine - Check fuel state - Crossfeed if necessary (Refer Check List) Safeguard Live Engine - Monitor temps / pressure Assess services affected - Alternator load Assess services affected - Gyro suction Proceed to nearest suitable airfield and land 5. ENGINE FIRE IN FLIGHT: Fuel: Off on Affected Engine Mixture Idle Cut Off Throttle Closed Feather Affected Engine Secure Engine — Fuel pump Off Secure Engine — Ignition Off Secure Engine — Alternator Off Secure Engine — Cowl Flap Closed Be prepared to land immediately if fire persists 6. ENGINE FIRE ON GROUND — STARTUP: Continue cranking starter to attempt to pull flame into manifold Fuel off on Affected Engine Throttle wide open IF FIRE PERSISTS — Evacuate aircraft, Use fire extinguisher if possible

Cabin Door Latched Seat Belts Adjusted Fuel Selectors On Cowl Flaps Open Carb Heats Cold Mixtures Rich Pitch Controls Full Forward Throttles Open ½" Landing Gear Handle Down Emergency Gear Knob Full In Brakes Parked Circuit Breakers In Master Switch On, Check u/c lights (3) External Lights As required Fuel Pumps On, check pressure, then off Left Magneto On Port Engine On Prime As required Left Starter Button Press WHEN RUNNING Right Magneto of Port Engine On Check Oil Pressure 25 PSI within 30 seconds Throttle 1000 RPM Port Alternator Switch On Port Ammeter warning light Charging Port Pressure Indicator Out REPEAT STEPS 16 to 20 FOR STD. ENGINE, THEN — Avionics Master On Electric Trim Master On

Park Brake Set Throttles 1000 RPM Magnetos Both Off / Check groundout / Both On Engine Instruments Check Throttles 2200 RPM Propellers Exercise (150–250 RPM Drop) Throttles 1800 RPM Magnetos Check each mag. (175 RPM max drop, 50 RPM between). Alternators Checked Carb Heats On/check drop off Instrument Pressure check 4.3 to 6.1 in Hg Throttles 1500 RPM Propellers Feather (allow 500 RPM drop max) Then full Fwd Throttles Slow Idle Throttles 1000 RPM

Brakes Parked Throttles 1000 RPM Trims (Elevator, Rudder, Aileron) set neutral Throttles Friction Firm Mixtures Full Rich Carb. Heats Cold Propellers Full Fine Fuel Selectors On Fuel Contents/Pressure Checked Fuel Pumps On Flaps Wing Up Flaps Cowl Open Ignition Switches All On Master/Alternator Switches All On Instruments Checked & Set Hatches Latched Harness Secure Autopilot Off Controls Checked Clearance (Airways/Take off) Obtained

Landing Clearance Obtained Traffic Sighted Brake Checked/Off Undercarriage Lowered (Check A/S below 145kt) Mixture Full Rich Fuel Selectors On appropriate tanks Fuel contents/ pressures Checked Fuel Pumps On Harness Secured Undercarriage Lights Green (3) Autopilot off Checked Landing Light As required

Carb. Heats Off Cowl Flaps Open Undercarriage Down Propellers Full Fine

Inoperative Engine Identify Inoperative Engine — Throttle Close / Check Fuel Pressure Check If INADEQUATE: Fuel Pump On Oil Pressure & Temp Check Magneto Switches On Mixture try various settings If Inoperative engine does not start: Secure (see Engine Securing Checklist following)

Inoperative engine Identify Inoperative Engine Throttle Close / Check Propellor Control Feather Mixture Control Idle-Cut-Off Cowl Flap Close Magneto Switches Off Alternator Switch Off Fuel Selector Off Fuel Pump Off

Fuel Selector On desired tank Fuel Pump On Throttle Open ½" Mixture Control beside operative engine Magneto Switches On Propellor Controls Full Forward Starter Operate (if engine not already windmilling) WHEN ENGINE IS RUNNING Fuel Pump Off Alternator On Oil Pressure Check Ammeter/Alt warning light Charging Warm up engine at 15", 2000 RPM As required Adjust power and trim as required

Fuel selector of operating engine Crossfed Fuel selector of inoperative engine Off Fuel Pumps Off unless required If engine driven pump has failed Auxiliary Fuel Pump on selected tank side must be used.

Shut off the affected wing or engine fuel selector and boost pump Secure the affected engine (Use securing inoperative engine checklist) Turn the navigation and strobe lights off Set the power & cowl flaps of the operating engine as required Move the cabin heat control of the affected engine to the cool position Reduce the electrical load as required and land as soon as practical

At the first sign of smoke, turn the master and alternator switches off Move the cabin air controls to cool and close all air vents Locate the source of smoke or fire and if necessary, use the fire extinguisher in accordance with the manufacturer's instructions Open ventilators after discharging the Extinguisher within the cabin Land the aeroplane as soon as possible to inspect for damage

In the event of an induction fire, pull the mixture control to the idle cutoff while continuing to crank the engine. Turn both fuel selectors off If the fire is not extinguished, turn the master, alternator, and magneto switches off Take the fire extinguisher from its mounting and evacuate the aeroplane. Take appropriate measures to extinguish the fire