Pilot Operating Handbook - Ecoflight.ch

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Rev. 02 – July 16 th , 2009 7 Normal Procedures 7.7 Best Rate of Climb Speed (V Y ) The maximum climb rate is achieved at an airspeed of about 75 mph (65 kts). Please monitor CHT, oil and water temperature during long periods of climbing. Oil temperature regulation flap must be set to position "open" or "cooler". 7.8 Cruise The cruising speed is related to relevant aircraft weight and selected power setting. For continuous operation the engine speed must not exceed 5.500 rpm. In no case the never exceed airspeed (V NE ) of 155 mph (134 kts) shall be exceeded. 7.9 Approach To prepare for approach, switch on the electric fuel pump and set the elevator trim as required, set carburetor heat to "warm" (pull) as necessary. When entering final, we recommend establishing an airspeed of 75 mph (65 kts) and extending flaps to the 40° position. 7.10 Normal Landing The airspeed for touch down should indicate about 50 mph (45 kts). The touch down should be first onto the main gear. The maximum demonstrated crosswind component is 17 mph (15 kts). Landings shall be done with full flap setting (40°). In case of a headwind component of more than 17 mph (15 kts) it is recommended to carry out the landing with a flaps setting of 15° only instead of full flap setting. Normal Procedures 7 - 7
Rev. 02 – July 16 th , 2009 7 Normal Procedures 7.11 Short Field Take-Off To perform a short field take-off, set flaps to 15° position, apply brakes and move the throttle to the full power position. Release brakes with stick held back. Rotate until nose-gear is off the ground, keep that attitude and wait until the airplane lifts-off by itself. Do not climb above 3ft AGL until the airspeed exceeds V X = 56 mph (49kts). At safe altitude accelerate up to V Y = 75 mph (65kts) until all obstacles are cleared. 7.12 Aborted Landing Procedure Apply full throttle, establish an airspeed of 75 mph (65 kts) while climbing. After all obstacles have been cleared, retract flaps. Climb to required altitude. 7.13 Low Airspeed and Stall If the center of gravity is within the permissible range, the aircraft will be fully controllable until reaching the stall speed. If stall speed is reached, the pilot should lower the nose of the aircraft to re-establish a safe airspeed. Performing a stall from level flight CG at most rearward position (airspeeds as IAS) Flap Position 0° 15° 30° 40° V min. at idle 51 mph (44 kts) 47 mph (41 kts) 45 mph (39 kts) 44 mph (38 kts) V min. at full power 50 mph (43 kts) 47 mph (41 kts) 44 mph (38 kts) 44 mph (38 kts) Normal Procedures 7 - 8
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Pilot Operating Handbook including
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Page 11 and 12: Rev. 02 - July 16 th , 2009 2 Airpl
Page 27 and 28: Rev. 02 - July 16 th , 2009 3 Opera
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Page 31 and 32: Rev. 02 - July 16 th , 2009 4 Weigh
Page 37 and 38: Rev. 02 - July 16 th , 2009 5 Perfo
Page 43 and 44: Rev. 02 - July 16 th , 2009 6 Emerg
Page 49 and 50: Rev. 02 - July 16 th , 2009 7 Norma
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Page 61 and 62: Rev. 02 - July 16 th , 2009 8 Aircr
Page 77 and 78: Rev. 02 - July 16 th , 2009 9 Requi
Page 87 and 88: Rev. 02 - July 16 th , 2009 10 Supp
Page 89 and 90: Rev. 01 - January 7 th , 2008 10.1
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Rev. 02 - July 16 th , 2009 5 Perfo
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Rev. 02 - July 16 th , 2009 7 Norma
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Rev. 02 - July 16 th , 2009 Imprint
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