2013 Airborne Aviation Pty Ltd

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1 Aircraft Information Booklet BE60 Duke VH-TFD Last revised: 11 November Airborne Aviation Pty Ltd

2 THIS PAGE INTENTIONALLY LEFT BLANK

3 Contents Aircraft Overview General Information... 1 Recency and Restrictions... 1 Front Cockpit Diagram... 2 Performance Specifications Summary of Aircraft Performance and Specifications... 3 Operating Limitations Airspeeds... 4 Power Plant... 5 Fuel System... 5 Manoeuvre / Load Limits... 6 Weight & Balance Load Charts & Limitations Performance Charts Cruise Settings 75% Power Cruise Settings 65% Power Cruise Settings 55% Power Checklists Normal Operations Emergency Operations Resources Briefings Useful Information NOTICE The information and figures contained in this booklet are to be used for general purposes only. This document is not a substitute for the approved aeroplane flight manual. Report errors to webmaster@airborne-aviation.com.au

4 Aircraft Overview This BE-60 Duke is a twin engine six-seater low wing light aircraft with retractable undercarriage, pressurization, air-conditioning, autopilot, VHF and HF radios, DME, ADF, VOR, GPS, weather radar, HSI and radar altimeter. With a realistic cruise speed of over 170 knots at an effective range of 900 nautical miles, it s a great charter and cross-country aircraft, and your passengers will arrive relaxed and refreshed as the quiet cabin is outfitted with leather club seating and temperature control. Recency & Restrictions Private Hire: Dual Training: Recency: Company Pilots only with Manual Propeller Rating, Retractable Undercarriage Rating, Pressurization Rating, Type Rating, Company Check Flight. No restrictions. Flown type in last 45 days. VH-TFD (Version: )

5 Panel Layout VH-TFD (Version: )

6 Performance Standard Specifications SPEED: (ISA) Cruise, 65% MCP, 2500 RPM, 29.8 in. Hg. SL KTS Cruise, 65% MCP, 2500 RPM, 29.9 in. Hg FT KTS Cruise, 65% MCP, 2500 RPM, 30.3 in. Hg FT KTS Cruise, 65% MCP, 2500 RPM, 30.6 in. Hg FT KTS Range 65% MCP, FT NM VY at SL, 2750 RPM, 35.5 in. Hg lbs / 3073 kg FPM SERVICE CEILING... 30,000 FT STALL SPEED 6775 lbs / 3073 kg: Flaps Up, Gear Up, Power Off KIAS Flaps Down, Gear Down, Power Off KIAS MAXIMUM WEIGHT: Take-off LBS / 3175 KG Landing LBS / 3073 KG Useful Load LBS/ KG BASIC EMPTY WEIGHT LBS / KG FUEL CAPACITY Gallons (US) / 764 Litres OIL CAPACITY (per engine) Quarts ENGINES:.. Lycoming TIO-541-E1A4, 2900 RPM and 41.5 in. Hg. PROPELLERS: Two Hartzell constant speed, full feathering, three-bladed propellers. Diameter: inches VH-TFD (Version: )

7 Operating Information AIRSPEEDS - NORMAL OPERATIONS Takeoff: Rotation Speed kts Normal Climb Out kts Short Field Takeoff... NOT RECOMMENDED Enroute Climb, Flaps Up: Normal kts Single Engine Best Rate of Climb kts Two Engine Best Rate of Climb kts Single Engine Best Angle-of-Climb kts Two Engine Best Angle-of-Climb kts Landing Approach: Normal Approach, Flaps FULL, 6775 lbs / 3073 kg kts Short Field Approach... NOT RECOMMENDED Balked Landing: Take-off Power, Flaps FULL, Gear Down, 6775 lbs / 3073 kg kts V-Speeds: VNE kts VFE: Approach Flap (15 ) kts Landing Flap (30 ) kts VLE kts VMCA kts VA kts Maximum Demonstrated Crosswind: Take-off or landing kts STALL SPEED 6775 lbs / 3073 kg: Flaps Up, Gear Up, Power Off kts Flaps Down, Gear Down, Power Off kts VH-TFD (Version: )

8 POWER PLANT Oil Type... Ashless Dispersant W100 Oil Quantities (Per Engine): Maximum Quarts Minimum Quarts Oil Temperatures: Minimum (Red Arc) C Normal Operating Range (Green Arc) C to 118 C Maximum (Red Arc) C Oil Pressures: Minimum Idle (Red Arc) psi Normal Operating Range (Green Arc) to 90 psi Maximum (Red Arc) psi Tachometer: Normal Operating Range (Green Arc) to 2900 rpm Maximum (Red Arc) RPM Manifold Pressure: Normal Operating Range (Green Arc) to 41.5 in. Hg Maximum (Red Arc) in. Hg Cylinder Head Temperature Normal Operating Range (Green Arc) to 232 C Maximum (Red Arc) C Turbine Inlet Temperature (Red Arc) C FUEL SYSTEM Total Usable Gallons (US) / 764 Litres Fuel Consumption per hour litres Fuel Flow: Green Arc to 330 pph 55% to 110 pph 65% pph 75% to 142 pph Approved Fuels: Preferred Grade LL Grade Aviation Fuel (Blue) Minimum Grade Grade Aviation Fuel (Green) MANOEUVRE / LOAD LIMITS VH-TFD (Version: )

9 This is a normal category aircraft. Aerobatic manoeuvers, including spins, are prohibited. Maximum Slip Duration...30 seconds Load Factor Limitations At design Gross Weight of 6775 lbs: Flaps Up G Flaps Down G VH-TFD (Version: )

10 Weight and Balance VH-TFD (Version: )

11 VH-TFD (Version: )

12 VH-TFD (Version: )

13 Performance VH-TFD (Version: )

14 VH-TFD (Version: )

15 VH-TFD (Version: )

16 Checklists Normal Operations PREFLIGHT INSPECTION Visually check the aeroplane for general condition during walk-around inspection. Aeroplane should be parked on level ground to ensure that fuel drain valves allow for accurate sampling. In cold weather, remove even small accumulations of frost, ice or snow from the aircraft. Pre-Flight Operational Documents 1. Dispatch -- Signed and Filed. 2. Maintenance Release -- CHECKED and SIGNED. 3. Weight and Balance -- CHECKED. (1) COCKPIT CHECK 1. Control Locks -- REMOVE and STOW. 2. Parking Brake -- SET. 3. All Switches -- OFF. 4. Landing Gear Handle -- DOWN. 5. Battery Switch -- ON. 6. Fuel Quantity Indicators -- CHECK QUANTITY (See LIMITATIONS for take-off fuel) 7. Cowl Flap Switches OFF (Cowl flaps should be in open position). 8. Battery Switch -- OFF. 9. Oxygen Pressure -- CHECK. 10. Trim Tabs (3) -- SET TO ZERO. VH-TFD (Version: )

17 (2) LEFT WING, TRAILING EDGE 1. Wing Root Fuel Sump -- DRAIN. 2. Flaps -- CHECK. 3. Aileron -- CHECK FREEDOM OF MOVEMENT, TAB NEUTRAL WHEN AILERON NEUTRAL. (3) LEFT WING, LEADING EDGE 1. Position Light -- CHECK. 2. Fuel VISUAL INSPECTION; Cap -- SECURE. 3. Stall Warning Vane -- CHECK FREEDOM OF MOVEMENT. 4. Deice Boots -- CHECK. 5. Tie Down, Chocks -- REMOVE. 6. Engine Oil -- CHECK QUANTITY; Cap -- SECURE. 7. Propeller and Propeller Deice Boots -- CHECK. 8. Engine Air Intakes -- CHECK FOR OBSTRUCTIONS. 9. Engine Cowling and Cowl Flap -- CHECK. 10. Fuel Sumps (2) -- DRAIN. 11. Wheel Well Doors, Tire, Brake and Shock Strut -- CHECK. 12. Landing Gear Down-Lock Mechanism and Up-Lock Rollers -- CHECK FOR CONDITION. 13. Pressurization Intercooler Inlet - CLEAR. (4) NOSE SECTION 1. Baggage Door -- CHECK. 2. Wheel Well Door, Tire and Shock Strut -- CHECK. 3. Heater Fuel Strainer -- DRAIN. 4. Pitot(s) -- REMOVE COVER, EXAMINE FOR OBSTRUCTIONS. 5. Nose Cone -- CHECK. 6. Ram Air Inlet -- CLEAR. (5) RIGHT WING, LEADING EDGE 1. Pressurization Intercooler Inlet -- CLEAR. 2. Wheel Well Doors, Tire, Brake and Shock Strut -- CHECK. 3. Landing Gear Down-Lock Mechanism and Up-Lock Roller -- CHECK FOR CONDITION. 4. Fuel Sumps (2) -- DRAIN. 5. Engine Cowling and Cowl Flap -- CHECK. 6. Engine Air Intakes -- CHECK FOR OBSTRUCTIONS. 7. Propeller and Propeller Deice Boots -- CHECK. VH-TFD (Version: )

18 8. Engine Oil - CHECK QUANTITY; Cap -- SECURE. 9. Tie Down, Chocks - REMOVE. 10. Deice Boots -- CHECK. 11. Fuel -- CHECK QUANTITY; Cap -- SECURE. 12. Position Light -- CHECK. (6) Right Wing, Trailing Edge 1. Aileron -- CHECK FOR FREEDOM OF MOVEMENT. 2. Flaps -- CHECK. 3. Wing Root Sump - DRAIN. (7) FUSELAGE, RIGHT SIDE 1. Static Port -- CLEAR OF OBSTRUCTIONS. 2. Antennas -- CHECKED. (8) EMPENNAGE 1. Position Light -- CHECK. 2. Rudder Mounted Rotating Beacon -- CHECK. 3. Control Surfaces -- CHECK. 4. Tab -- ELEVATOR TAB NEUTRAL WITH ELEVATOR NEUTRAL. 5. Deice Boots -- CHECK. 6. Tie Down -- REMOVE. (9) FUSELAGE, LEFT SIDE 1. Static Port -- CLEAR OF OBSTRUCTIONS. NOTE If night flight is anticipated, exterior lights should be checked for operation. VH-TFD (Version: )

19 BEFORE STARTING 1. Pre-flight Inspection -- COMPLETE. 2. Aircraft Dispatch -- COMPLETED / AUTHORISED. 3. Running Sheet Figures -- COMPLETE. 4. Maintenance Release -- CHECKED. 5. Air Sickness Bags -- AVAILABLE. 6. Passenger Briefing -- COMPLETE. 7. Cabin Door, Escape Hatch and Baggage -- SECURED. 8. Seat and Rudder Pedals -- ADJUSTED. 9. Seat Belts -- FASTENED. 10. Flight Controls -- FREEDOM OF MOVEMENT and PROPER RESPONSE. 11. Cowl Flaps -- CHECK OPEN. 12. Circuit Breakers -- IN. 13. Fuel Selectors -- ON. STARTING 1. Propeller Controls -- FORWARD (Low Pitch). 2. Mixture Controls -- IDLE CUT-OFF. 3. Battery Switch -- ON. NOTE If external power is used start right engine first. 4. Boost Pumps -- ON. 5. Start Engines. a. Cold Starts: 1. Throttle 1000 rpm position (approximately ½ inch open). 2. Mixture control FULL FORWARD for 2 to 3 seconds to prime then IDLE CUT OFF. 3. Magneto/Start Switch -- START. 4. When the engine starts, return the Magneto/Start switch to BOTH. Slowly advance the mixture control to FULL RICH. b. Flooded Engine: 1. Mixture Control -- IDLE CUT-OFF. VH-TFD (Version: )

20 2. Throttle -- ½ OPEN. 3. Magneto/Start Switch - START. 4. When engine starts, return the Magneto/Start switch to BOTH. Retard the throttle and slowly advance the mixture control to FULL RICH position. c. Hot Starts: 1. Throttle 1300 to 1500 rpm position (approximately 1 inch open). 2. Mixture Controls -- IDLE CUT-OFF. 3. Magneto/Start Switch -- Start. NOTE A small prime may be necessary if the engine does not start after a few revolutions 4. When the engine starts, return the Magneto/Start switch to BOTH. Slowly advance the mixture control to FULL RICH. 6. Throttle 1000 to 1500 rpm. 7. Oil pressure -- ABOVE RED ARC WITHIN 30 SECONDS. 8. Generator Switch -- ON. 9. External Power (if used) -- DISCONNECT. 10. Use the same procedure to start other engine. 11. Fuel Boost Pumps -- OFF. NOTE Continuous use of the fuel boost pumps is recommended for ground operation in ambient temperatures of 90 F (32 C) or above AFTER STARTING AND TAXI 1. Brakes -- CHECK. 2. Voltage and Loadmeters -- CHECK. 3. Avionics -- ON. 4. Lights -- AS REQUIRED. 5. Cabin Temperature and Mode -- AS REQUIRED. 6. Annunciator Warning Lights -- PRESS-TO-TEST. 7. Instruments -- CHECK. CAUTION Never taxi with a flat shock strut. VH-TFD (Version: )

21 BEFORE TAKE-OFF 1. Parking Brake -- SET. 2. Engine Warm-up TO 1500 RPM. 3. Fuel Boost Pumps -- ON. NOTE With engine speed below 2000 rpm, a diaphragm failure in the engine driven pump will cause engine roughness and a drop in rpm when the fuel pump is turned on. 4. Fuel Selectors -- CROSSFEED (for seconds). 5. Fuel Selectors -- RETURN TO BOTH ON. 6. Instruments -- CHECK, NORMAL INDICATION AND SET. 7. Flaps -- CHECK OPERATION AND SET. 8. Electric Trim -- CHECK OPERATION. 9. Trim -- SET TO TAKE-OFF RANGE. 10. Propeller Synchronizer -- OFF. 11. Landing Gear Safety System (If Installed) -- CHECK. 12. Autopilot -- CHECK. 13. Throttles RPM. 14. Magnetos -- CHECK (175 rpm maximum drop, within 50 rpm of each other). NOTE Avoid operation on one magneto for more than 5-10 seconds. 15. Pressurization -- SET. 16. Throttles RPM. 17. Propellers -- FEATHER CHECK (No more than 500 rpm drop) Repeat 2 to 3 times in cold weather. 18. Gyro Pressure and Load Meters - CHECK. 19. Throttles -- IDLE. 20. Self Brief TEM & EMERGENCY ACTIONS. 21. Parking Brake -- RELEASE. VH-TFD (Version: )

22 HOLDING POINT CHECKS 1. Clear -- CHECK BASE & FINAL FOR TRAFFIC (both directions). 2. Lights -- ON AS REQUIRED. 3. Engine -- INSTRUMENTS IN THE GREEN. 4. Airframe & Alt -- FLAPS, WINDOWS, HATCHES & TRANSPONDER SET. 5. Radios -- SET FREQUENCY AND OBTAIN CLEARANCE AS REQUIRED. TAKE-OFF POWER SETTINGS: Take-off and Maximum Continuous in. Hg RPM 1. Power -- SET take-off power before brake release. 2. Airspeed -- ACCELERATE to and maintain take-off speed. 3. Landing Gear -- RETRACT when aircraft is positively airborne. 4. Airspeed -- ESTABLISH DESIRED CLIMB SPEED when clear of obstacles. Cruise Climb 1. Power -- SET CRUISE CLIMB POWER (35.5 in. Hg rpm). 2. Fuel Flow LBS/HR/ENGINE. 3. Propeller Synchronizer - ON. 4. Airspeed -- ESTABLISH CRUISE-CLIMB SPEED. 5. Cowl Flaps -- AS REQUIRED (MAINTAIN 225 C CYLINDER HEAD TEMPERATURE OR LESS) NOTE Use of fuel boost pump may be discontinued at any time except that excessive fluctuations of fuel flow readings indicate a need for continued use. MAXIMUM PERFORMANCE CLIMB 1. Power -- SET MAXIMUM CONTINUOUS POWER. 2. Fuel Boost Pumps -- ON. 3. Mixtures -- FULL RICH. 4. Cowl Flaps -- OPEN. 5. Propeller Synchronizer -- ON. 6. Airspeed -- ESTABLISH 120 KTS. VH-TFD (Version: )

23 CRUISE 1. Power -- SET AS DESIRED (Use Horsepower Calculator or Cruise Power Settings tables) 2. Fuel Flow -- LEAN AS REQUIRED (Lean to recommended fuel flow if Turbine Inlet Temperature (TIT) is below 900 C). 3. Fuel Boost Pumps -- OFF (Unless needed to prevent fuel flow fluctuations). 4. Cowl Flaps -- AS REQUIRED (Maintain 225 C cylinder head temperature or less) DESCENT 1. Self Brief -- COMPLETE (Arrival plan/expectations, TEM, contingencies) 2. QNH -- Set aerodrome QNH. 3. Cowl Flaps -- CLOSED. 4. Windshield Anti-ice and Defroster -- AS REQUIRED (ON before descent into warm, moist air). 5. Pressurization -- SET. 6. Power -- AS REQUIRED. BEFORE LANDING 1. Brake -- PRESSURE and PARKING BRAKE off. 2. Undercarriage -- DOWN and LOCKED. 3. Mixtures -- FULL RICH. 4. Fuel -- SUFFICIENT and BOOST PUMPS ON. 5. Instruments -- TEMPERATURES and PRESSURES & ELECTRICAL in the GREEN. 6. Switches -- MAIN INVERTER on, MASTER on, BATTERY & GENERATORS on, FUEL BOOST PUMPS confirm on, MAGS both, LIGHTS as required PROPELLER SYNCHRONIZER off, YAW DAMPENER off. 7. Heat, Height, Harnesses and Hatches -- HEATER OFF, PRESSURIZATION SET, LOCKED and SECURE. ON FINAL 1. Props - FULL FINE. 2. Undercarriage -- DOWN and LOCKED (Vg 174). 3. Flaps -- IDENTIFIED & SET (FULL DOWN Vfe kts). 4. Flaps -- COWL FLAPS OPEN. VH-TFD (Version: )

24 BALKED LANDING 1. Power RPM and 41.5 in. Hg. 2. Airspeed -- BALKED LANDING CLIMB SPEED 120 kts. 3. Flaps -- UP. 4. Gear -- UP. 5. Cowl Flaps -- AS REQUIRED. AFTER LANDING 1. Clear -- CLEAR OF ACTIVE RUNWAYS. 2. Lights -- AS REQUIRED. 3. Engine -- INSTRUMENTS in the GREEN and FUEL BOOST PUMPS OFF*. 4. Airframe & Alt -- FLAPS IDENTIFIED and UP, COWL FLAPS OPEN, TRIM TABS SET TO ZERO. 5. Radios -- FREQUENCY SET, CLEARANCE OBTAINED, TRANSPONDER TO STANDBY. (SARTIME?) *NOTE Fuel boost pumps may be turned off if ambient temperature is below 32 C. SHUT DOWN/SECURING AEROPLANE 1. Brake -- SET (if required). 2. After Landing Checks -- CONFIRM COMPLETED. 3. Throttle RPM. 4. Lights -- OFF. 5. Inverter and Avionics Master -- OFF. 6. Cabin Temp Mode & Air Conditioning -- OFF. 7. Propellers -- FULL FINE. 8. Fuel Boost Pumps - OFF. 9. Mixtures -- IDLE CUT-OFF Ensure that engines have run at idle (1000 rpm) for no less than 3 minutes prior to shutting down. 10. Magnetos -- OFF. 11. Battery and Generators -- OFF. 12. Aeroplane interior -- TIDY. 13. Running Sheet Figures -- COMPLETE. 14. BRAKE -- OFF, chock if necessary. 15. Controls -- LOCKED. 16. Pitot Covers -- INSTALL. VH-TFD (Version: )

25 Checklists Emergency Procedures INTRODUCTION Emergencies caused by aeroplane or engine malfunctions are extremely rare if proper pre-flight inspections and maintenance are performed. The following procedures are not exhaustive and if a situation arises in flight that does not have an appropriate checklist in this booklet then Section lll of the approved flight manual should be consulted. The following information is presented to enable you to form, in advance, a definite plan of action for coping with the most probable emergency situations which could occur. Where practicable, the emergencies requiring immediate corrective action are treated in check list form for easy reference and familiarization. Other situations, in which more time is usually permitted to decide on and execute a plan of action, are discussed at some length. In order to supply one safe speed for each type of emergency situation the airspeeds presented are derived at 6775 lbs. LANDING GEAR MANUAL EXTENSION 1. Airspeed -- BELOW 174 kts (Lower airspeeds make landing gear extension easier). 2. Landing Gear Relay Circuit Breaker (Right Upper Side Panel) -- PULL. 3. Landing Gear Position Handle -- DOWN. 4. Remove safety boot from handcrank handle at rear of front seats. Engage handcrank and turn clockwise as far as possible (approximately 50 turns). 5. If electrical system is operative, check landing gear position lights and warning horn. 6. Disengage Handcrank. CAUTION The manual extension system is designed only to lower the landing gear; do not attempt to retract the gear manually. WARNING After emergency landing gear extension do not move any landing gear controls or reset any switches or circuit breakers until aircraft is on jacks as failure may have been in the gear up circuit and gear might retract on ground. VH-TFD (Version: )

26 SINGLE-ENGINE OPERATION Two major factors govern single-engine operation; airspeed and lateral/directional control. The aeroplane can be safely manoeuvred or trimmed for normal hands-off operation and sustained in this configuration by the operative engine AS LONG AS SUFFICIENT AIRSPEED IS MAINTAINED. SINGLE-ENGINE BEST RATE-OF-FLIMB SPEED, 110 kts The single-engine best rate-of-climb speed is the airspeed which delivers the greatest gain in altitude in the shortest possible time with gear up, flaps up, and inoperative propeller feathered. SINGLE-ENGINE BEST ANGLE-OF-CLIMB SPEED, 100 kts The single engine best angle-of-climb speed is the airspeed which delivers the greatest gain in altitude in the shortest possible horizontal distance with gear up, flaps up, and inoperative propeller feathered MINIMUM SINGLE-ENGINE CONTROL SPEED, 85 kts The minimum single-engine control speed is the airspeed below which the airplane cannot be controlled laterally and directionally in flight with one engine operating at take-off power and the other engine with its propeller windmilling ENGINE OUT PROCEDURE The following ENGINE OUT PROCEDURE should be committed to memory: 7. Establish VYSE. 8. Mixtures, Props, Throttles -- FULL. 9. Undercarriage -- UP. 10. Flaps -- RETRACTED. 11. Identify -- DEAD FOOT = DEAD ENGINE. 12. Verify -- RETARD THE DEAD ENGINE THROTTLE. 13. Feather or Fix -- FEATHER DEAD ENGINE S PROPELLER.* 14. Raise the dead -- RAISE DEAD ENGINE APPROX 5 AOB. 15. Let the ball out of the cage -- REDUCE RUDDER PRESSURE. 16. Cowl Flap on dead engine -- CLOSED. *If height is sufficient troubleshoot and attempt to fix the problem. VH-TFD (Version: )

27 SECURING INOPERATIVE ENGINE PROCEDURE The following SECURING INOPERATIVE ENGINE PROCEDURE should be committed to memory: 1. Mixture -- IDLE CUT OFF. 2. Fuel Selector -- OFF. 3. Fuel Boost Pump -- OFF. 4. Magneto/Start Switch -- OFF. 5. Generator Switch -- OFF. 6. Cowl Flap -- CLOSED. ENGINE FAILURES ENGINE FAILURE DURING TAKEOFF ROLL 7. Throttle -- CLOSED. 8. Braking -- MAXIMUM. 9. Fuel Selector Valves -- OFF. 10. Battery & Generator Switches -- OFF. ENGINE FAILURE AFTER LIFT-OFF The most important aspect of engine failure is the necessity to maintain lateral and directional control, and to achieve and maintain normal take-off airspeed or above. The following procedures provide for minimum diversion of attention while flying the airplane. NOTE If airspeed is below 85 kts or terrain clearance is insufficient, reduce power as required to maintain lateral and directional control. 1. Establish VYSE kts. 2. Mixtures, Props, Throttles -- FULL. 3. Undercarriage -- UP. 4. Flaps -- RETRACTED. 5. Identify -- DEAD FOOT = DEAD ENGINE. 6. Verify -- RETARD THE DEAD ENGINE THROTTLE. 7. Feather or Fix -- FEATHER DEAD ENGINE S PROPELLER. 8. Raise the dead -- RAISE DEAD ENGINE APPROX 5 AOB. 9. Let the ball out of the cage -- REDUCE RUDDER PRESSURE. 10. Cowl Flap on dead engine -- CLOSED. VH-TFD (Version: )

28 SECURING INOPERATIVE ENGINE 1. Mixture -- IDLE CUT OFF. 2. Fuel Selector -- OFF. 3. Fuel Boost Pump -- OFF. 4. Magneto/Start Switch -- OFF. 5. Generator Switch -- OFF. 6. Cowl Flap -- CLOSED. ENGINE FAILURE DURING FLIGHT (adequate performance & terrain clearance) 1. Establish VYSE kts. 2. Mixtures, Props, Throttles -- FULL. 3. Undercarriage -- UP. 4. Flaps -- RETRACTED. 5. Identify -- DEAD FOOT = DEAD ENGINE. 6. Verify -- RETARD THE DEAD ENGINE THROTTLE. 7. Feather or Fix -- TROUBLESHOOT DEAD ENGINE: a. Fuel flow -- CHECK. b. Fuel Pump -- ON. c. Fuel quantity -- CHECK. d. Fuel selector -- ON. e. Oil temperature & pressure -- CHECK. f. Magnetos -- CHECK. If the reason for the engine failure can be determined and eliminated, attempt an air start. If the engine cannot be restarted, complete the checklist. 8. Feather -- FEATHER DEAD ENGINE S PROPELLER. 9. Raise the dead -- RAISE DEAD ENGINE APPROX 5 AOB. 10. Let the ball out of the cage -- REDUCE RUDDER PRESSURE. 11. Cowl Flap on dead engine -- CLOSED. 12. Secure Inoperative engine using SECURING INOPERATIVE ENGINE PROCEDURE. VH-TFD (Version: )

29 SINGLE ENGINE LANDING 1. Seat Belts - FASTENED. 2. Fuel Boost Pump (operative Engine) -- ON. 3. Mixture -- FULL RICH. 4. Propeller Synchroniser -- OFF. 5. Propeller -- Set to 2750 rpm, advance to full fine after final power reduction. 6. Approach Flaps (15 ) -- BELOW 174 KTS IAS. 7. Gear -- EXTEND BELOW 174 KTS IAS. 8. Pressurisation -- ZERO DIFFERENTIAL. 9. Rudder and Aileron Trim -- ZERO. 10. Full Flap (30 ) -- Below 134 KTS IAS and WHEN LANDING IS ASSURED. SINGLE ENGINE GO-AROUND A single engine go-around is not recommended. The published procedure for a single engine go-around is as follows: A Single engine go-around may be executed when it appears that this is the only way to avoid a possible accident. Early recognition of the need to go around is essential. 1. Apply Maximum Power in. hg. And 2900 rpm. 2. Raise Landing Gear. 3. Raise Flaps Cautiously. 4. Accelerate to 110 KTS IAS (best single engine rate of climb speed). ENGINE FIRE IN FLIGHT 1. Oxygen Masks -- ON. 2. Mixture Control -- IDLE CUT OFF. 3. Fuel Selector -- OFF. 4. Propeller Control -- FEATHERED. 5. Pressurisation Air Shut-Off -- PULL. 6. Fuel Boost Pump -- CHECK OFF. 7. Magneto/Start Switch -- OFF. 8. Generator Switch -- OFF. VH-TFD (Version: )

30 PRESSURISATION SYSTEM Any time the differential pressure goes into the red arc, either reschedule the cabin altitude selector or dump all pressure with the DUMP switch. EMERGENCY DESCENT 1. Oxygen Masks -- ON. 2. Propeller Controls rpm. 3. Throttles -- CLOSED NOTE! IDLE POWER ON BOTH ENGINES WILL CAUSE A LOSS OF PRESSURISATION. 4. Airspeed KTS IAS. 5. Landing Gear -- DOWN AND LOCKED. 6. Flaps -- EXTEND 15 (Approach Flap). 7. Maintain 174 KTS IAS. OPERATIONAL SPEEDS Minimum Single Engine Control Speed kts Single Engine Best Angle of Climb Speed kts Single Engine Best Rate of Climb Speed kts Two Engine Best Angle of Climb Speed kts Two Engine Best Rate of Climb Speed kts Cruise Climb Speeds: Sea Level feet kts feet feet kts feet feet kts VH-TFD (Version: )

31 PASSENGER BRIEFINGS It is important to brief your passengers thoroughly prior to flight, and also keep passengers updated during the flight. Included are some suggestions for items to be included in your briefs. PRIOR TO GOING AIRSIDE Passengers should stay with you while airside for security and safety. No smoking anywhere while airside or in the aircraft. Stay away from other aircraft and be alert to hazards. Overview of flight and expected flying conditions. Does anybody require the toilet before we take-off? ON THE GROUND Don t scare your passengers by talking about engine failures, fires, or similar simply ensure they are told to follow your instructions and know how to operate the doors and/or emergency exits. Adjustment of seat belts and seat position. Location of sick bags. An intercom is provided so passengers can easily communicate. Passengers to minimise chat when radio is busy, or as requested. Front seat passenger should be encouraged to point out any aircraft spotted that might be of conflict another set of eyes is always useful. Front seat passenger briefed on not interfering with controls. If any passengers have any concerns during the flight they should be encouraged to raise them. Be sure to ask your passengers if they have any questions. Encourage passengers to read the self-briefing cards if available. IN FLIGHT A running commentary of sights that can be seen, locations flown over and how the flight is progressing can be useful. Update your passengers about any change of plans. Check on the status of your passengers regularly. Should a situation arise in flight you should remain calm. Communicate clearly and confidently the situation and your intentions to passengers. VH-TFD (Version: )

32 SELF BRIEFING - DEPARTURE A takeoff briefing should clearly state your plan-of-action for both when everything goes as planned and when they do not! He who fails to plan, plans to fail! You should brief yourself on the following points: How you plan on taking off and departing the aerodrome. Consider any threats relevant to the departure and manage them. Reasons for an aborted takeoff and how to execute it. Dealing with an engine failure with runway remaining. Dealing with an engine failure at low level with no runway remaining. SELF BRIEFING - ARRIVAL The arrival is the single most demanding phase of flight, and the one that carries the highest risk. As with a departure briefing, a thorough self brief on arrival is the key to a smooth and arrival. You should brief yourself on the following points: How you plan on conducting your approach to the aerodrome, and what clearance or joining procedure you anticipate based on ATIS / AWIS. Example: Join upwind for RWY 06 at 1,800ft descending on upwind to 1,300ft. Any NOTAMS relevant to your approach and landing. Example: RWY 10/28 closed due soft wet surface. Consider any threats relevant to the arrival and manage them. Example: Particularly strong crosswind and in-to-wind runway not available. - Revise crosswind procedure, be go-around minded if unstable. - Consider diversion if necessary. The type of approach and landing you plan on making. Example: Reduced flap setting due to strong winds, final speed 65-75kts. If needing to go-around, the actions required to execute the procedure. Example: Full power, raise nose, establish positive climb, flaps up slowly, communicate with ATC or other aircraft. VH-TFD (Version: )

33 THREAT AND ERROR MANAGEMENT TEM is an approach to flying that seeks to equip the pilot with the skills to recognise and counter everyday problems which, if ignored, could result in accidents or incidents. Not all threats can be anticipated, it is unrealistic to make contingency plans to try to cover unexpected events. Experience shows that many threats can be anticipated, the first step is to identify likely threats. Once a threat has been identified, it must be managed. If you identify a threat that cannot be managed you should not go flying! Example Threat High number of aircraft operating at aerodrome Tower closed, CTAF procedures in operation Short Runway Terrain or obstacles Landing in to setting sun Adverse Weather ie. Crosswind on landing Your recency Aircraft status ie. COM1 distorted / unreadable NOTAMS Management Extra vigilance of traffic in the circuit through visual means and radio monitoring. Without additional safety of tower protection maintain an enhanced lookout and radio monitoring. Ensure correct short field take-off or landing procedures are used and that performance has been confirmed. Maintain enhanced situational awareness, also modify departure or arrival as appropriate. Use another runway if possible. Wear sunglasses and be go-around minded if unhappy with any aspect of the approach. Ensure correct crosswind procedures are adopted and you are up to the task (aircraft and/or crosswind recency). Be go-around minded if the approach or landing becomes unstable. Request an alternate runway if operationally required or preferred. Study aircraft procedures prior to flight and take extra time to perform checks and monitor your own performance, or take a safety pilot. Utilise COM2 for primary communications if available, otherwise divert or abort flight after troubleshooting. Familiarise yourself with changes to regular procedures and include in departure or arrival briefs. ERROR MANAGEMENT The TEM model accepts that it is unavoidable that pilots, as human beings, will make errors. While errors may be inevitable, safety of flight requires that errors that occur are identified and managed before flight safety margins are compromised. Identification of errors requires aircraft/systems/procedure knowledge and situational awareness. Analyse your own performance and identify errors before they lead to an undesired aircraft state or more serious error. VH-TFD (Version: )

34 USEFUL INFORMATION Location Frequency Camden Tower / CTAF(R) Ground ATIS / AWIS NDB 281 Training Area Sydney Radar Bankstown Preferred diversion airport Tower / CTAF(R) Ground ATIS / AWIS NDB 416 Wedderburn CTAF The Oaks CTAF Airborne Aviation Airborne Base Phone (02) SYDNEY/Bankstown (YSBK) VH-TFD (Version: )

35 Notes

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